Civil Turbojet/Turbofan Specifications
	(sorted by engine manufacturer)
	Manufacturer	Model	Application(s)	Thrust	Thrust	SFC	SFC	Airflow	OPR	FPR	BPR	Thrust	SFC	Cruise	Cruise	TIT	Number	Fan	LPC	HPC	HPT	IPT	LPT	Fan	Length	Width/	Dry
				(dry)	(wet)	(dry)	(wet)	(static)	(static)	(static)	(static)	(cruise)	(cruise)	Speed	Altitude		Spools	Stgs	Stgs	Stgs	Stgs	Stgs	Stgs	Diameter		Diameter	Weight
				[lbf]	[lbf]	[lb/lbf hr]	[lb/lbf hr]	[lb/s]				[lbf]	[lb/lbf hr]	[M]	[ft]	[K]								[in]	[in]	[in]	[lb]
	ACEA	CJ-500	ARJ21 (proposed)	18,000													2	1	4	10	2	-	7
	ACEA	CJ-1000A	C919 (proposed)	28,200													2	1	3	10	2	-	6
	ACEA	CJ-1000B	C919 (proposed)	29,500													2	1	3	10	2	-	6
	ACEA	CJ-2000	C929 (proposed)	78,000													2	1	4	10	2	-	7
	Agilis Engines	TF800		800	-
	Agilis Engines	TF1000	S-26 Safire (not produced)	1,000	-	0.4	-					270	0.64	0.6	30,000										56	23	285
	Agilis Engines	TF1200		1,288	-	0.41	-					400	0.66	0.6	30,000										56	23	285
	Agilis Engines	TF1400		1,400	-	0.41	-					400	0.66	0.6	30,000										56	23	300
	Agilis Engines	TF1500		1,500	-	0.41	-					397	0.68	0.6	30,000										56	23	300
	Agilis Engines	TJ60		60	-	1.24	-					30	1.5	0.9	20,000										13.5	5	9
	Agilis Engines	TJ75		75	-	1.24	-					48	1.5	0.9	20,000										13.5	7	10
	Agilis Engines	TJ80		72	-	1.24	-					48	1.5	0.9	20,000										13.5	5	9
	Agilis Engines	TJ400		403	-	0.9	-																		30	15	136
	AlliedSignal (Honeywell)	AS905	Falcon 7X (candidate engine)		-		-
	AlliedSignal (Honeywell)	AS907-1-1A	Challenger 300	6,944	-	0.42	-		21		4.5						2	1	4B	1C	2	-	3	34.2	92.4	46.3	1,534
	AlliedSignal (Honeywell)	AS907-2-1A	Challenger 300	7,530	-		-				4.5						2	1	4B	1C	2	-	3	34.2	92.4	46.3	1,534
	AlliedSignal (Honeywell)	AS907-2-1G	G280	7,765	-		-				4.5						2	1	4B	1C	2	-	3	34.2	92.4	46.3	1,534
	AlliedSignal (Honeywell)	AS907-2-1S	Citation Longitude	7,550	-		-				4.5						2	1	4B	1C	2	-	3	34.2	92.4	46.3	1,534
	AlliedSignal (Honeywell)	AS907-3-1E	Legacy 450/500, Praetor 500/600	7,638	-		-				4.5						2	1	4B	1C	2	-	3	34.2	92.4	46.3	1,514
	AlliedSignal (Honeywell)	AS977-1A	RJX-70/-85/-100/-115, SL-100 (not produced)	7,100	-	0.416	-		23		4.5						2	1	4B	1C	2	-	3	34.2	92.4	49.9	1,364
	Allison (Rolls-Royce)	AE3007A	ERJ-135ER, ERJ-145/EP/ER/EU	7,580	-	0.36	-	294	24		5.3						2	1	-	14	3	-	2	38.5	115.1	55.7	1,615
	Allison (Rolls-Royce)	AE3007A1	ERJ-135ER, ERJ-145EP/ER/EU/LR/LU/MK/MP/MR	7,580	-	0.36	-	294	24		5.3						2	1	-	14	3	-	2	38.5	115.1	55.7	1,625
	Allison (Rolls-Royce)	AE3007A1P	ERJ-145EP/ER/EU/LR/LU/MK/MP/MR, Legacy 600	8,338	-		-				5.3						2	1	-	14	3	-	2	38.5	115.1	55.7	1,657
	Allison (Rolls-Royce)	AE3007A1/1	ERJ-135ER/LR, ERJ-145EP/ER/EU/LR/LU/MK/MP/MR	7,580	-		-				5.3						2	1	-	14	3	-	2	38.5	115.1	55.7	1,625
	Allison (Rolls-Royce)	AE3007A1/2	ERJ-145EP/ER/EU/LR/LU/MK/MP/MR	7,580	-		-				5.3						2	1	-	14	3	-	2	38.5	115.1	55.7	1,625
	Allison (Rolls-Royce)	AE3007A1/3	ERJ-135ER/KE/KL/LR, ERJ-140	7,580	-		-				5.3						2	1	-	14	3	-	2	38.5	115.1	55.7	1,625
	Allison (Rolls-Royce)	AE3007A1E	ERJ-135BJ, ERJ-145XR, Legacy 600	8,895	-		-										2	1	-	14	3	-	2	38.5	115.1	55.7	1,657
	Allison (Rolls-Royce)	AE3007A2	Legacy 650	9,278	-		-										2	1	-	14	3	-	2	38.5	115.1	55.7	1,681
	Allison (Rolls-Royce)	AE3007A3	ERJ-135/ER	7,201	-		-				5.3						2	1	-	14	3	-	2	38.5	115.1	55.7	1,657
	Allison (Rolls-Royce)	AE3007C	Citation X	6,442	-		-				5.3						2	1	-	14	3	-	2	38.5	115.1	55.7	1,614
	Allison (Rolls-Royce)	AE3007C1	Citation X	6,764	-		-				5.3						2	1	-	14	3	-	2	38.5	115.1	55.7	1,617
	Allison (Rolls-Royce)	AE3007C2	Citation X	7,042	-		-										2	1	-	14	3	-	2	38.5	115.1	55.7	1,641
	Allison (Rolls-Royce)	AE3010/12	Yak-77 (not produced)	9,920
	Allison/Rolls-Royce/BMW	AE3012	AIR 70 (not produced)
	Avco Lycoming	ALF301	BH200 (not produced)	2,730	-	0.44	-	100	9		5.6						2	1	-	5 + 1C	2	-	2
	Avco Lycoming	ALF501	Technology demonstrator	5,800	-	0.4	-	221	9.3		6						2	1G	-	7 + 1C	2	-	2
	Avco Lycoming	ALF502L	Challenger 600	7,500	-	0.428	-	256	13.6		5.2	2,150	0.73	0.75	30,000		2	1G	2B	7 + 1C	2	-	2		65.6	50	1,311
	Avco Lycoming	ALF502L-2	Challenger 600	7,500	-	0.428	-		13.6								2	1G	2B	7 + 1C	2	-	2		65.6	50	1,311
	Avco Lycoming	ALF502L-2A	Challenger 600	7,500	-	0.414	-		13.8								2	1G	2B	7 + 1C	2	-	2		65.6	50	1,321
	Avco Lycoming	ALF502L-2C	Challenger 600	7,500	-	0.414	-		13.8								2	1G	2B	7 + 1C	2	-	2		65.6	50	1,321
	Avco Lycoming	ALF502L-3	Challenger 600	7,500	-	0.415	-		13.8		5						2	1G	2B	7 + 1C	2	-	2		65.6	50	1,321
	Avco Lycoming	ALF502R-3	BAe 146-100/-200	6,700	-	0.411	-		11.6		5.7						2	1G	1B	7 + 1C	2	-	2		63.8	50	1,336
	Avco Lycoming	ALF502R-3A	BAe 146-100/-200/-300	6,970	-	0.408	-		12.2		5.6						2	1G	2B	7 + 1C	2	-	2		63.8	50	1,336
	Avco Lycoming	ALF502R-4	BAe 146-100/-200/-300	6,970		0.408											2	1G	1B	7 + 1C	2	-	2		63.8	50	1,336
	Avco Lycoming	ALF502R-5	BAe 146-100/-200/-200ER/-300	6,970	-	0.408	-		12.2		5.6	2,250	0.72	0.7	25,000		2	1G	2B	7 + 1C	2	-	2		63.8	50	1,336
	Avco Lycoming	ALF502R-6	BAe 146-200/-200ER/-300	7,500	-	0.415	-	192	13.8		5.6						2	1G	2B	7 + 1C	2	-	2		65.6	50	1,375
	Avco Lycoming (Textron Lycoming)	LF507-1F	RJ-70/-85/-100/-115	7,000	-	0.406	-	192	13.8		5.7						2	1G	7B	1C	2	-	2	40	58.6	41.7	1,385
	Avco Lycoming (Textron Lycoming)	LF507-1H	RJ-70/-85/-100/-115	7,000	-		-		13.8		5.7						2	1G	7B	1C	2	-	2	40	58.6	41.7	1,375
	Avco Lycoming (Textron Lycoming)	LF507-1N	Yak-40TL	7,000	-		-										2	1G	7B	1C	2	-	2	40	58.6	41.7
	Aviadvigatel	D-21A1	S-21 (not produced)	16,535	-		-		20.2	2.99	0.83						2	5	-	10	2	-	2				4,630
	Aviadvigatel	D-100		42,000	-		-		35		8						2	1	2B	13	2	-	4
	Aviadvigatel	D-110		44,090	-		-		31	1	3						2	2G	2B	13	2	-	4
	Aviadvigatel	D-120			-		-			1	5						2	2	2B	13	2	-	4
	Aviadvigatel	PD-10	SSJ300	24,000													2	1	1	8	2	-	5	66			5,180
	Aviadvigatel	PD-14	MC-21-200	31,000													2	1	3	8	2	-	6	75			6,330
	Aviadvigatel	PD-14A	MC-21-300	28,000													2	1	3	8	2	-	6	75			6,330
	Aviadvigatel	PD-14M	MC-21-400	34,000													2	1	4	8	2	-	6	75			6,550
	Brandner	E-300-C1	Project 206 (not produced)		-		-			-	-						1	-	-	9	2	-	-
	Brandner	E-300-C2	(cancelled)		-		-			-	-						1	-	-	9	2	-	-
	Brandner	E-300-AF	(cancelled)		-		-
	Bristol/Curtiss-Wright	Olympus Mk.551	Avro 740, Avro 750 (not produced)	13,500													2	-	7	7	1	-	1
	Bristol Siddeley	Orpheus BOr.3 Mk.803	JetStar prototype	4,130	-	1.08	-			-	-						1	-	-	7	1	-	-	-
	Bristol Siddeley	Orpheus BOr.3/5 Mk.810D	JetStar prototype	4,850	-		-			-	-						1	-	-	7	1	-	-	-	100.52	36.95	990
	Bristol Siddeley (Rolls-Royce)	Viper Mk.520	DH 125-1	3,100	-		-			-	-						1	-	-	7	1	-	-	-
	Bristol Siddeley (Rolls-Royce)	Viper Mk.521	DH 125-1A, HS 125-1B	3,100	-	0.99	-	53	5.6	-	-						1	-	-	8	1	-	-	-	92.97	28.7	758
	Bristol Siddeley (Rolls-Royce)	Viper Mk.522	HS 125-1A-522/-1B-522/-3/-3A/-3B/-400A/-400B/-403B	3,330	-	1	-		5.6	-	-						1	-	-	8	1	-	-	-	92.97	28.7	773
	Bristol Siddeley (Rolls-Royce)	Viper Mk.525	PD.808 prototype	3,330	-	1	-		5.6	-	-						1	-	-	8	1	-	-	-	105.55	28.7	772
	Bristol Siddeley (Rolls-Royce)	Viper Mk.601-22	HS 125-600A/B	3,675	-		-	58.4	5.8	-	-						1	-	-	8	2	-	-	-	64.6	24.5	760
	Bristol Siddeley (Rolls-Royce)	Viper Mk.601-22A	HS 125-600A/B	3,675	-		-	58.4	5.8	-	-						1	-	-	8	2	-	-	-	64.6	24.5	760
	CFE	CFE738-1-1B	Falcon 2000	5,918	-	0.369	-	240	30	1.7	5.3	1,310	0.645	0.8	40,000		2	1	-	5 + 1C	2	-	3	35.5	68.3	48	1,325
	CFM	CFM56-2A2	(see military turbofan specifications)		-		-
	CFM	CFM56-2A3	(see military turbofan specifications)		-		-
	CFM	CFM56-2B1	(see military turbofan specifications)		-		-
	CFM	CFM56-2C1	DC-8-71F/-72/-72F/-73F, DC-8-71/-73 (option)	22,000	-	0.35	-	788	24.7		6	4,980	0.671	0.8	35,000		2	1	3B	9	1	-	4	68.3	95.7	72	4,635
	CFM	CFM56-2C2	Trident	24,000	-	0.36	-		26.5								2	1	3B	9	1	-	4	68.3	95.7	72
	CFM	CFM56-2C3	DC-8-71/-71F/-72/-72F/-73/-73F (option)		-		-										2	1	3B	9	1	-	4	68.3	95.7	72	4,635
	CFM	CFM56-2C5	DC-8-72, DC-8-71/-71F/-72F/-73/-73F (option)		-		-										2	1	3B	9	1	-	4	68.3	95.7	72	4,635
	CFM	CFM56-2C6	DC-8-71/-71F/-72/-72F/-73/-73F (option)		-		-										2	1	3B	9	1	-	4	68.3	95.7	72	4,635
	CFM	CFM56-3B1	737-300/-300(QC)/-500, 737-400 (option)	20,000	-	0.38	-	655	22.6		6	4,650	0.667	0.8	35,000		2	1	3B	9	1	-	4	60	93.1	63	4,276
	CFM	CFM56-3B2	737-300/-300(QC)/-300F/-400	22,000	-	0.39	-	683	24.3		5.9	5,040	0.667	0.8	35,000		2	1	3B	9	1	-	4	60	93.1	63	4,301
	CFM	CFM56-3C1	737-300/-300(QC)/-300F/-400/-500	23,500	-	0.33	-	710	25.7		6	5,370	0.667	0.8	35,000		2	1	3B	9	1	-	4	60	93.1	63	4,301
	CFM	CFM56-3C3	737-300, 737-300(QC)/-300F/-400/-500 (option)		-		-										2	1	3B	9	1	-	4	60	93.1	63
	CFM	CFM56-5A1	A320-111/-211/-311	25,000	-	0.33	-	852	26.5		6	5,000	0.596	0.8	35,000		2	1	3B	9	1	-	4	68.3	95.4	72	4,995
	CFM	CFM56-5A1/F	A320-211	25,000	-	0.33	-	852	26.5		6	5,000	0.596	0.8	35,000		2	1	3B	9	1	-	4	68.3	95.4	72	4,995
	CFM	CFM56-5A3	A320-212	26,500	-	0.33	-	876	27.8		6	5,000	0.596	0.8	35,000		2	1	3B	9	1	-	4	68.3	95.4	72	4,995
	CFM	CFM56-5A4	A319-113	22,000	-	0.32	-	816	24.1		6.2	5,000		0.8	35,000		2	1	3B	9	1	-	4	68.3	95.4	72	4,975
	CFM	CFM56-5A4/F	A319-113	22,000	-	0.32	-	816	24.1		6.2	5,000		0.8	35,000		2	1	3B	9	1	-	4	68.3	95.4	72	4,975
	CFM	CFM56-5A5	A319-114	23,500	-	0.32	-	842	25.4		6.2	5,000		0.8	35,000		2	1	3B	9	1	-	4	68.3	95.4	72	4,975
	CFM	CFM56-5A5/F	A319-114	23,500	-	0.32	-	842	25.4		6.2	5,000		0.8	35,000		2	1	3B	9	1	-	4	68.3	95.4	72	4,975
	CFM	CFM56-5B1	A321-111/-212	30,000	-	0.35	-	943	32		5.5	5,840	0.596	0.8	35,000		2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B1/P	A321-111/-212	30,000	-	0.35	-	943	32		5.5						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B1/2	A321-111/-212	30,000	-	0.35	-	943	32		5.5						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B1/2P	A321-111/-212	30,000	-	0.35	-	943	32		5.5						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B1/3	A321-111/-212	30,000	-	0.35	-	943	32		5.5						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B2	A321-112/-213	31,000	-	0.35	-	956	32.9		5.5	5,840	0.545	0.8	35,000		2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B2/P	A321-112/-213	31,000	-	0.35	-	956	32.9		5.5						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B2/2	A321-112/-213	31,000	-		-										2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B2/2P	A321-112/-213	31,000	-		-										2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B2/3	A321-112/-213	31,000	-	0.35	-	956	32.9		5.5						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B3	A321-211	32,000	-	0.36	-	956	33.7		5.4	5,840		0.8	35,000		2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B3/P	A321-211	32,000	-	0.36	-	956	33.7		5.4						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B3/P1	A321-211	32,000	-	0.36	-	956	33.7		5.4						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B3/2P	A321-211	32,000	-	0.36	-		33.7								2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B3/2P1	A321-211	32,000	-	0.36	-		33.7								2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B3/3	A321-211	32,000	-	0.36	-		33.7								2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B3/3B1	A321-211	32,000	-	0.36	-		33.7								2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B4	A320-214	27,000	-	0.34	-	897	29.1		5.7	5,000	0.545	0.8	35,000		2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B4/P	A320-214	27,000	-	0.34	-	897	29.1		5.7						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B4/P1	A320-214	27,000	-	0.34	-	897	29.1		5.7						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B4/2	A320-214	27,000	-	0.34	-	897	29.1		5.7						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B4/2P	A320-214	27,000	-	0.34	-	897	29.1		5.7						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B4/2P1	A320-214	27,000	-	0.34	-	897	29.1		5.7						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B4/3	A320-214	27,000	-	0.34	-	897	29.1		5.7						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B4/3B1	A320-214	27,000	-	0.34	-	897	29.1		5.7						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B5	A319-111, A320-215	22,000	-	0.32	-	818	24.4		6						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B5/P	A319-111, A320-215	22,000	-	0.32	-	818	24.4		6						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B5/3	A319-111, A320-215	22,000	-	0.32	-	818	24.4		6						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B6	A319-112, A320-216	23,500	-	0.33	-	844	25.8		5.9						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B6/P	A319-112	23,500	-	0.33	-	844	25.8		5.9						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B6/2	A319-112	23,500	-	0.33	-	844	25.8		5.9						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B6/2P	A319-112	23,500	-	0.33	-	844	25.8		5.9						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B6/3	A319-112, A320-216	23,500	-	0.33	-	844	25.8		5.9						2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B7	A319-115/-115CJ/-115XCJ	27,000	-	0.34	-		29.1								2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B7/P	A319-115/-115CJ/-115XCJ	27,000	-	0.34	-		29.1								2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B8/P	A318-111	21,600	-		-										2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B8/3	A318-111	21,600	-		-										2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B9/P	A318-112	23,300	-		-										2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5B9/3	A318-112	23,300	-		-										2	1	4B	9	1	-	4	68.3	102.4	72	5,250
	CFM	CFM56-5C2	A340-211/-311	31,200	-	0.32	-	1027	31.5		6.6	6,915	0.545	0.8	35,000		2	1	4B	9	1	-	5	72.3	103	76.6	5,700
	CFM	CFM56-5C2/P	A340-211/-311	31,200	-		-										2	1	4B	9	1	-	5	72.3	103	76.6
	CFM	CFM56-5C2/4	A340-211/-311	31,200	-		-										2	1	4B	9	1	-	5	72.3	103	76.6
	CFM	CFM56-5C2/F	A340-211/-311	31,200	-		-										2	1	4B	9	1	-	5	72.3	103	76.6
	CFM	CFM56-5C2/F4	A340-211/-311	31,200	-		-										2	1	4B	9	1	-	5	72.3	103	76.6
	CFM	CFM56-5C2/G	A340-211/-311	31,200	-		-										2	1	4B	9	1	-	5	72.3	103	76.6
	CFM	CFM56-5C2/G4	A340-211/-311	31,200	-		-										2	1	4B	9	1	-	5	72.3	103	76.6
	CFM	CFM56-5C3	A340-212	32,500	-	0.32	-	1045	32.6		6.5	6,910	0.545	0.8	35,000		2	1	4B	9	1	-	5	72.3	103	76.6	5,700
	CFM	CFM56-5C3/P	A340-212/-312	32,500	-	0.32	-	1045	32.6		6.5	6,910	0.545	0.8	35,000		2	1	4B	9	1	-	5	72.3	103	76.6	5,700
	CFM	CFM56-5C3/F	A340-212/-312	32,500	-	0.32	-	1045	32.6		6.5						2	1	4B	9	1	-	5	72.3	103	76.6	5,700
	CFM	CFM56-5C3/F4	A340-212/-312	32,500	-		-										2	1	4B	9	1	-	5	72.3	103	76.6
	CFM	CFM56-5C3/G	A340-212/-312	32,500	-	0.32	-	1045	32.6		6.5						2	1	4B	9	1	-	5	72.3	103	76.6	5,700
	CFM	CFM56-5C3/G4	A340-212/-312	32,500	-		-										2	1	4B	9	1	-	5	72.3	103	76.6
	CFM	CFM56-5C4	A340-213/-213X/-313/-313X/-8000	34,000	-	0.33	-	1065	33.9		6.4	7,100	0.545	0.8	35,000		2	1	4B	9	1	-	5	72.3	103	76.6	5,700
	CFM	CFM56-5C4/P	A340-313/-313X	34,000	-	0.33	-	1065	33.9		6.4	7,100	0.545	0.8	35,000		2	1	4B	9	1	-	5	72.3	103	76.6	5,700
	CFM	CFM56-5C4/1	A340-213/-213X/-313/-313X	34,000	-	0.33	-	1065	33.9		6.4	7,100	0.545	0.8	35,000		2	1	4B	9	1	-	5	72.3	103	76.6	5,700
	CFM	CFM56-5C4/1P	A340-313/-313X	34,000	-	0.33	-	1065	33.9		6.4	7,100	0.545	0.8	35,000		2	1	4B	9	1	-	5	72.3	103	76.6	5,700
	CFM	CFM56-7B18/3	737-600	18,500	-	0.35	-	667	21.7		5.6	5,420		0.8	35,000		2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B20	737-600/-700	20,600	-	0.36	-	686	22.7		5.6	5,450	0.633	0.8	35,000		2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B20/2	737-600/-700	20,600	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B20/3	737-600/-700	20,600	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B20E	737-600/-700	20,600	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B22	737-600/-700/-700BBJ/-800/-800BBJ2	22,700	-		-	726	24.6		5.4	5,450		0.8	35,000		2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B22/B1		22,700	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B22/2	737-600	22,700	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B22/3	737-600/-700	22,700	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B22/3B1		22,700	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B22E	737-600/-700	22,700	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B22/EB1		22,700	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B24	737-700/-800/-900/-900ER, 737-700BBJ/-800BBJ2 (option)	24,200	-	0.37	-	754	26		5.3	5,480	0.627	0.8	35,000		2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B24/2	737-700	24,200	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B24/3	737-700/-800/-900/-900ER	24,200	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B24/3B1	737-800/-900/-900ER	24,200	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B24E	737-700/-800/-900/-900ER	24,200	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B24E/B1	737-800/-900/-900ER	24,200	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B24/B1		24,200	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26	737-700/-700BBJ/-800/-800BBJ2/-900/-900ER	26,300	-	0.38	-	783	27.9		5.1	5,480		0.8	35,000		2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26/2	737-800	26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26/3	737-800/-900/-900ER	26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26/3B1		26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26/3B2		26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26/3B2F		26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26/3F	737-700/-800/-900/-900ER	26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26/B1	737-700	26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26/B2		26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26E	737-700/-800/-900/-900ER	26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26E/B1	737-700	26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26E/B2	737-700		-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26E/B2F	737-700	26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B26E/F	737-700/-800/-900/-900ER	26,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27	737-600/-900/-900ER	27,300	-	0.38	-		28.9								2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27/2		27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27/B1	737-800/-900/-900	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27/B3	737-700/-900ER	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27/3	737-900ER	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27/3B1	737-800/-900/-900ER	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27/3B1F	737-800/-900ER	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27/3B3	737-700/-800/-900/-900ER	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27/3F	737-900ER	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27A		27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27A3		27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27E	737-900ER	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27E/B1	737-800/-900/-900ER	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27E/B1F	737-800/-900ER	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27E/B3	737-700/-800/-900/-900ER	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-7B27E/F	737-900ER	27,300	-		-										2	1	3B	9	1	-	4	61	98.9	65	5,216
	CFM	CFM56-9	A316/A317 (A31X), BRJ-X, AE-100, N-2130 (not produced)	20,000	-	0.38	-		23.2								2	1	2B	9	1	-	3		91.7	56	4,252
	CFM	LEAP-1A22	A319-152N	22,000													2	1	3	10	2	-	7		131
	CFM	LEAP-1A23		24,000													2	1	3	10	2	-	7		131
	CFM	LEAP-1A24	A319-151N, A320-252N	24,000													2	1	3	10	2	-	7		131
	CFM	LEAP-1A24E1	A319-151N	24,000													2	1	3	10	2	-	7		131
	CFM	LEAP-1A26	A319-153N, A320-251N	27,100													2	1	3	10	2	-	7		131
	CFM	LEAP-1A26CJ		27,100													2	1	3	10	2	-	7		131
	CFM	LEAP-1A26E1	A319-153N, A320-251N	27,100													2	1	3	10	2	-	7		131
	CFM	LEAP-1A29	A320-253N	29,300													2	1	3	10	2	-	7		131
	CFM	LEAP-1A29CJ		29,300													2	1	3	10	2	-	7		131
	CFM	LEAP-1A30	A321-252N/-252NX	32,160													2	1	3	10	2	-	7		131
	CFM	LEAP-1A32	A321-251N/-251NX	32,160													2	1	3	10	2	-	7		131
	CFM	LEAP-1A33	A321-253N/-253NX	32,160													2	1	3	10	2	-	7		131
	CFM	LEAP-1A33A5	A321-253N	32,160													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1A33B2	A321-253N	32,160													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1A35	A321-253N/-253NX	32,160													2	1	3	10	2	-	7		131
	CFM	LEAP-1B35		32,160													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B21		25,000													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B23		25,900													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B25G05	737-8	26,785													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B25G06	737-8	26,785													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B27G05	737-8/-9	28,000													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B27G06	737-8/-9	28,000													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B28G05	737-8/-9	29,300													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B28G06	737-8/-9	29,300													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B28B1G05	737-8/-9	29,300													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B28B1G06	737-8/-9	29,300													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B28B2		29,300													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B28B2C		28,000													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1B28B3		29,300													2	1	3	10	2	-	5		123.9
	CFM	LEAP-1C28	C919 (proposed)	29,220													2	1	3	10	2	-	7		131
	CFM	LEAP-1C30	C919 (proposed)	30,830													2	1	3	10	2	-	7		131
	CFM	LEAP-1C30B1	C919 (proposed)	30,830													2	1	3	10	2	-	7		131
	Continental	Model 420	(see Turbomeca Aspin II)
	Curtiss-Wright	TJ38
	Curtiss-Wright	TJ70		53,200	-		-	600	9	-	-																6,340
	de Havilland	Ghost 50 Mk.1	Comet 1	5,000	-		-										1	-	-	1C	1	-	-		129	52.7
	de Havilland	Ghost 50 Mk.2	Comet 1A	5,020	-		-										1	-	-	1C	1	-	-		129	52.7
	de Havilland	Ghost 50 Mk.3			-		-			-	-						1	-	-	1C	1	-	-	-	129	52.7
	de Havilland	Ghost 50 Mk.4	Comet 1XB	5,500	-		-			-	-						1	-	-	1C	1	-	-	-	129	52.7
	Engine Alliance	GP7168	747-500X/-600X (not produced)	68,000	-		-	2000	42.3		7						2	1	3B	9	2	-	4		169	99	11,500
	Engine Alliance	GP7172	767-400ERX, (not produced)	71,000	-		-										2	1	3B	9	2	-	4
	Engine Alliance	GP7268	(cancelled)	68,000	-		-		46		8						2	1	5B	9	2	-	6
	Engine Alliance	GP7270	A380-861	74,735	-		-		45.6		8.7	12,633		0.85	35,000		2	1	5B	9	2	-	6	116	185.8	123.7	14,798
	Engine Alliance	GP7272		76,470	-		-		45.6		8.7						2	1	5B	9	2	-	6	116	185.8	123.7	14,798
	Engine Alliance	GP7277	A380-863F (not produced)	80,290	-		-	2600	45.6		8.7	13,700		0.85	35,000		2	1	5B	9	2	-	6	116	185.8	123.7	14,798
	Garrett	ATF3-6A-4C	Falcon 200	5,440	-		-	162	21.3		2.8						3	1	5	1C	1	3	2		102	33.6	1,165
	Garrett	ATF3-??	HFB 330 (not produced), Sabreliner 60 (candidate engine)	4,050	-	0.44	-	140	17		3						3	1	5	1C	1	3	2
	Garrett	TFE731-2	Falcon 10, Learjet 31/31A, SA-28T	3,500	-	0.504	-	113	13	1.54	2.66	755	0.815	0.8	40,000		2	1G	1C	4	1	-	3	28.2	49.7	39.4	743
	Garrett	TFE731-2-2A	Learjet 35/36	3,500	-	0.504	-	113	13	1.54	2.66						2	1G	1C	4	1	-	3	28.2	49.7	39.4	743
	Garrett	TFE731-2-2B	Learjet 35A/36A	3,500	-	0.504	-	113	13	1.54	2.66						2	1G	1C	4	1	-	3	28.2	49.7	39.4	743
	Garrett	TFE731-2-2N	IA 63 NGA	3,500	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	743
	Garrett	TFE731-2A-2A	K-8E	3,600	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	772
	Garrett	TFE731-2B		3,500	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	773
	Garrett	TFE731-2BR		3,650	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	773
	Garrett	TFE731-2C		3,500	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	753
	Garrett	TFE731-3	JetStar II	3,700	-	0.511	-	118	14.6	2.8	2.8	817	0.819	0.8	40,000		2	1G	1C	4	1	-	3	28.2	49.7	39.4	754
	Garrett	TFE731-3-1C	Falcon 50	3,700	-		-	118	14.6	2.8	2.8						2	1G	1C	4	1	-	3	28.2	49.7	39.4	754
	Garrett	TFE731-3-1D	Sabreliner 65	3,700	-		-	118	14.6	2.8	2.8						2	1G	1C	4	1	-	3	28.2	49.7	39.4	754
	Garrett	TFE731-3-1G	1124 Westwind	3,700	-		-	118	14.6	2.8	2.8						2	1G	1C	4	1	-	3	28.2	49.7	39.4	754
	Garrett	TFE731-3-1H	HS 125-600F	3,700	-		-	118	14.6	2.8	2.8						2	1G	1C	4	1	-	3	28.2	49.7	39.4	754
	Garrett	TFE731-3-100S	Citation III	3,700	-		-	118	14.6	2.8	2.8						2	1G	1C	4	1	-	3	28.2	49.7	39.4	754
	Garrett	TFE731-3A-2B	Learjet 55/55B/55C/55C-LR	3,700	-	0.515	-	118	14.6	2.8	2.8	838	0.823	0.8	40,000		2	1G	1C	4	1	-	3	28.2	49.7	39.4	775
	Garrett	TFE731-3A-300G	Astra, Astra SP	3,700	-		-	118	14.6	2.8	2.8						2	1G	1C	4	1	-	3	28.2	49.7	39.4	775
	Garrett	TFE731-3AR		3,880	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	775
	Garrett	TFE731-3B-100	Citation VI	3,650	-	0.507	-	118	14.4	2.8	2.8	844	0.816	0.8	40,000		2	1G	1C	4	1	-	3	28.2	49.7	39.4	769
	Garrett	TFE731-3BR		3,850	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	769
	Garrett	TFE731-3C		3,700	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	777
	Garrett	TFE731-3CR		3,880	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	777
	Garrett	TFE731-3D		3,700	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	767
	Garrett	TFE731-3DR		3,880	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	767
	Garrett	TFE731-3RH	HS 125-700A/B	3,880	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	754
	Garrett	TFE731-4	Citation VII, Citation IV (not produced)	4,080	-	0.517	-		14.8		2.4	929	0.796	0.8	40,000		2	1G	1C	4	1	-	3	28.2	51	39.4	822
	Garrett	TFE731-4R		4,080	-		-										2	1G	1C	4	1	-	3	28.2	49.7	39.4	822
	Garrett	TFE731-5	HS 125-800, Sabreliner 85	4,304	-	0.484	-	143	14.4	3.48	3.65	955	0.802	0.8	40,000		2	1G	1C	4	1	-	3	29.7	54.7	40.5	852
	Garrett	TFE731-5A		4,500	-		-										2	1G	1C	4	1	-	3				884
	Garrett	TFE731-5AR	Falcon 20RE	4,500	-	0.469	-	143	14.6	3.48	3.65	986	0.771	0.8	40,000		2	1G	1C	4	1	-	3	29.7	80.8	40.5	884
	Garrett	TFE731-5AR-1C	Falcon 900	4,500	-		-										2	1G	1C	4	1	-	3	29.7	80.8	40.5	884
	Garrett	TFE731-5AR-2C	Falcon 20C-5/D-5/E-5/F-5	4,500	-		-										2	1G	1C	4	1	-	3	29.7	80.8	40.5	884
	Garrett	TFE731-5B		4,750	-		-										2	1G	1C	4	1	-	3				899
	Garrett (Allied-Signal)	TFE731-5BR	Falcon 20RE, Hawker 750/800XP/850XP	4,750	-	0.47	-	143	15.1	3.48	3.5	1,052	0.756	0.8	40,000		2	1G	1C	4	1	-	3	29.7	80.8	40.5	899
	Garrett (Honeywell)	TFE731-5BR-1C	Falcon 900B/900C	4,750	-		-										2	1G	1C	4	1	-	3	29.7	80.8	40.5	899
	Garrett (Honeywell)	TFE731-5BR-2C	Falcon 20C-5/D-5/E-5/F-5	4,750	-		-										2	1G	1C	4	1	-	3	29.7	80.8	40.5	899
	Garrett	TFE731-5R	Hawker 800	4,500	-		-										2	1G	1C	4	1	-	3				852
	Garrett (AlliedSignal)	TFE731-20		3,500	-		-										2	1G	1C	4	1	-	3	28.2	51	39.4	895
	Garrett (Honeywell)	TFE731-20AR	Learjet 40/45	3,650	-	0.441	-	123	21	3.7	3.1	876	0.728	0.8	40,000		2	1G	1C	4	1	-	3	28.2	51	39.4	895
	Garrett (Honeywell)	TFE731-20BR	Learjet 40XR/45XR	3,500	-		-										2	1G	1C	4	1	-	3	28.2	51	39.4
	Garrett (AlliedSignal)	TFE731-20R		3,650	-		-										2	1G	1C	4	1	-	3	28.2	51	39.4	895
	Garrett (AlliedSignal)	TFE731-40	Falcon 50EX, Hawker 450	4,250	-	0.457	-	145	22		2.9						2	1G	1C	4	1	-	3	28.2	51	39.4	885
	Garrett (AlliedSignal)	TFE731-40R-200G	G100 (Astra SP), G150 (Astra SPX), IA 63 NGB	4,462	-		-										2	1G	1C	4	1	-	3	28.2	51	39.4	885
	Garrett (Honeywell)	TFE731-40AR-200G	G150	4,420	-		-										2	1G	1C	4	1	-	3	28.2	51	39.4
	Garrett (Honeywell)	TFE731-40BR	Learjet 70/75	3,850	-		-										2	1G	1C	4	1	-	3	28.2	51	39.4
	Garrett (Honeywell)	TFE731-50R	Hawker 900XP	4,750	-		-										2	1G	1C	4	1	-	3	28.2	51	39.4
	Garrett (AlliedSignal)	TFE731-60	Falcon 900DX/900EX/900LX	5,000	-	0.405	-	187	22		3.9						2	1G	1C	4	1	-	3	30.7	72	42.4	988
	GE	Affinity	Aerion AS2	18,000	-		-				3.1						2	2	-	9	1	-	2	52
	GE	CF6-6	DC-10-10 (option)	39,300	-		-	1343	26.6	1.64	6.2						2	1	1B	16	2	-	5		172.5	92	7,350
	GE	CF6-6D	DC-10-10/-10F/-10F(CF)	39,300	-	0.354	-	1303	24.3		5.72	9,080	0.646	0.8	35,000		2	1	1B	16	2	-	5	86.4	188.0**	105	7,896
	GE	CF6-6D1	DC-10-10/-10F/-10F(AF)	40,300	-	0.35	-	1328	25.2		5.76	9,220	0.646	0.8	35,000		2	1	1B	16	2	-	5	86.4	188.0**	105	7,896
	GE	CF6-6D1A	DC-10-10/-10F/-10F(AF)	40,900	-	0.35	-	1328	25.2		5.76	9,220	0.646	0.8	35,000		2	1	1B	16	2	-	5	86.4	188.0**	105	7,896
	GE	CF6-6E	DC-10-10/-10F (option)	40,600	-		-										2	1	1B	16	2	-	5	86.4
	GE	CF6-6F	DC-10-10/-10F (option)	42,000	-		-										2	1	1B	16	2	-	5	86.4
	GE	CF6-6K	DC-10-10/-10F	39,300	-	0.346	-		25								2	1	1B	16	2	-	5	86.4	188.0**	105	8,176
	GE	CF6-6K2	DC-10-10/-10F (option)	40,900	-	0.346	-		25								2	1	1B	16	2	-	5	86.4	188.0**	105	8,176
	GE	CF6-32	757 (proposed)
	GE	CF6-45A	747-100SR/-100SR(SF)	45,600	-		-	1393	26.3		4.64	11,250	0.63	0.8	35,000		2	1	3B	14	2	-	4	86.4	188.0**	105	8,768
	GE	CF6-45A2	747-100SR/-100SR(SF)	45,600	-		-	1393	26.3		4.64	11,250	0.63	0.8	35,000		2	1	3B	14	2	-	4	86.4	188.0**	105	8,768
	GE	CF6-45B	747-100SR/-100SR(SF)	46,500	-		-	1393	26.3		4.64	11,250	0.63	0.8	35,000		2	1	3B	14	2	-	4	86.4	188.0**	105	8,768
	GE	CF6-45B2	747-100SR/-100SR(SF), A300B10 (A310) (candidate engine)	46,500	-		-	1393	26.3		4.64	11,250	0.63	0.8	35,000		2	1	3B	14	2	-	4	86.4	188.0**	105	8,768
	GE	CF6-50	DC-10-30/-30F	49,000	-		-						0.645	0.8	35,000		2	1	3B	14	2	-	4	92			8,100
	GE	CF6-50A	DC-10-30/-30F, A300B1	48,400	-	0.389	-	1444	28.6	1.69	4.4		0.654	0.8	35,000		2	1	3B	14	2	-	4	86.4	183.0**	92	8,201
	GE	CF6-50B		49,000	-	0.389	-	1444	28.6	1.69	4.4		0.654	0.8	35,000		2	1	3B	14	2	-	4	86.4	183.0**	92	8,201
	GE	CF6-50C	A300B2-1A/-1C/-101, A300B4-1C, DC-10-30/-30CF/-30F	50,400	-	0.394	-	1451	29.3		4.26	11,100	0.657	0.8	35,000		2	1	3B	14	2	-	4	86.4	183.0**	105	8,721
	GE	CF6-50C1	DC-10-30, A300B2-202, A300B4-103	51,800	-	0.371	-	1470	30.1		4.24	11,555	0.657	0.8	35,000		2	1	3B	14	2	-	4	86.4	183.0**	105	8,721
	GE	CF6-50C2	A300B2-203, A300B4-2C/-203/-203F, A300C4-203, A300F4-203, DC-10-30/-30F/-30F(CF), A300B1 (option)	52,500	-	0.371	-	1476	30.4		4.31	11,555	0.63	0.8	35,000		2	1	3B	14	2	-	4	86.4	183.0**	105	8,731
	GE	CF6-50C2B	DC-10-30/-30ER	53,200	-	0.385	-	1504	31.1		4.25	11,555	0.63	0.8	35,000		2	1	3B	14	2	-	4	86.4	183.0**	105	8,731
	GE	CF6-50C2D		51,800	-		-										2	1	3B	14	2	-	4	86.4	183.0**	105	8,731
	GE	CF6-50C2F	DC-10-15	46,500	-		-	1393	26.3		4.64	11,555	0.63	0.8	35,000		2	1	3B	14	2	-	4	86.4	183.0**	105	8,731
	GE	CF6-50C2R	A300B2-1C/-101, A300B2K-3C, A300B4-2C, DC-10-30	51,500	-	0.368	-		29.2								2	1	3B	14	2	-	4	86.4	183.0**	105	8,731
	GE	CF6-50D	DC-10-10	51,000													2	1	3B	14	2	-	4	86.4	183.0**	105	8,325
	GE	CF6-50D1	(see military turbofan specifications)
	GE	CF6-50E	747-200B	51,800	-	0.376	-	1470	30.1		4.24	11,555	0.657	0.8	35,000		2	1	3B	14	2	-	4	86.4	183.0**	105	8,490
	GE	CF6-50E1	747-200B	51,800	-	0.371	-	1470	30.1		4.24	11,555	0.657	0.8	35,000		2	1	3B	14	2	-	4	86.4	183.0**	105	8,490
	GE	CF6-50E2	747-200B/-200B(M)/-200B(SF)/-200C(M)/-200F/-300/-300(M)/-300(SF)	51,800	-	0.371	-	1476	30.4		4.31	11,555	0.63	0.8	35,000		2	1	3B	14	2	-	4	86.4	183.0**	105	8,768
	GE	CF6-50E2B	747-200/-300 (option)	53,200	-	0.375	-	1504	30.9		4.24	11,730	0.63	0.8	35,000		2	1	3B	14	2	-	4	86.4	183.0**	105	8,768
	GE	CF6-80A	767-200/-200ER/-200PC	46,930	-	0.344	-	1435	27.3		4.66	11,045	0.623	0.8	35,000		2	1	3B	14	2	-	4	86.4	157.4	98	8,496
	GE	CF6-80A1	767-200/-200ER (option)	46,990	-	0.344	-	1435	27.3		4.66	11,045	0.623	0.8	35,000		2	1	3B	14	2	-	4	86.4	157.4	98	8,420
	GE	CF6-80A2	767-200/-200ER/-300	48,670	-	0.349	-	1460	28.4	1.7	4.59	11,045	0.623	0.8	35,000		2	1	3B	14	2	-	4	86.4	157.4	98	8,496
	GE	CF6-80A3	A310-203/-203C/-203F	48,970	-	0.357	-	1460	28.4	1.7	4.59	11,045	0.623	0.8	35,000		2	1	3B	14	2	-	4	86.4	157.4	98	8,420
	GE	CF6-80C2	767-200ER/-300 (option)	52,500	-	0.329	-	1769	30.4		5.2	11,330		0.85	35,000		2	1	4B	14	2	-	5	93	160.9		9,135
	GE	CF6-80C2A1	A300B4-601	57,860	-	0.334	-	1754	30.4		5.15	11,810	0.576	0.8	35,000		2	1	4B	14	2	-	5	93	160.9	106	9,360
	GE	CF6-80C2A2	A310-204/-304/-304ET/-304F	52,460	-	0.317	-	1769	30.4	1.66	5.05	11,330	0.578	0.8	35,000		2	1	4B	14	2	-	5	93	160.9	106	9,360
	GE	CF6-80C2A3	A300B4-603, MD-11 (option)	58,950	-	0.329	-	1769	30.4	1.73	5.05	11,340	0.576	0.8	35,000		2	1	4B	14	2	-	5	93	160.9	106	9,360
	GE	CF6-80C2A5	A300B4-605R, A300C4-605R, A300F4-605R	60,100	-	0.34	-		31.5		5.05						2	1	4B	14	2	-	5	93	160.9	106	9,389
	GE	CF6-80C2A5F	A300B4-605R, A300C4-605R, A300F4-605R	60,100	-	0.34	-		31.5		5.05						2	1	4B	14	2	-	5	93	160.9	106	9,389
	GE	CF6-80C2A6		64,000	-		-										2	1	4B	14	2	-	5
	GE	CF6-80C2A6F		63,000	-		-										2	1	4B	14	2	-	5
	GE	CF6-80C2A7	A310-308, A310-308ET (option)	59,000	-		-										2	1	4B	14	2	-	5	93	160.9	106	9,389
	GE	CF6-80C2A8	A300B4-608ST, A310-308/-308ET	57,860	-	0.344	-	1769	30.4		5.05						2	1	4B	14	2	-	5	93	160.9	106	9,389
	GE	CF6-80C2B1	747-300/-300(M)	55,980	-	0.323	-	1710	30.4		5.19	12,820	0.576	0.8	35,000		2	1	4B	14	2	-	5	93	160.9	106	9,388
	GE	CF6-80C2B1F	747-400/-400D/-400ER/-400(M)/-400F	57,160	-	0.316	-	1764	30.4		5.15	12,820	0.564	0.8	35,000		2	1	4B	14	2	-	5	93	160.9	106	9,499
	GE	CF6-80C2B1F1		60,030	-		-										2	1	4B	14	2	-	5	93	160.9	106	9499
	GE	CF6-80C2B1F2	747-400/-400D/-400ER/-400(M)/-400F	60,030	-		-										2	1	4B	14	2	-	5	93	160.9	106	9,499
	GE	CF6-80C2B2	767-200ER/-300/-300ER, 737-200 (option)	51,590	-	0.318	-	1650	30.4		5.31	12,000	0.576	0.8	35,000		2	1	4B	14	2	-	5	93	160.9	106	9,388
	GE	CF6-80C2B2F	767-200/-200ER/-300, 767-300ER (option)	52,010	-		-										2	1	4B	14	2	-	5	93	160.9	106	9,499
	GE	CF6-80C2B2F2	767-200/-200ER/-300, 767-300ER (option)		-		-										2	1	4B	14	2	-	5	93	160.9	106	9,499
	GE	CF6-80C2B3	747-300/-400 (option)	52,010	-		-										2	1	4B	14	2	-	5	93	160.9	106	9,388
	GE	CF6-80C2B3F	747-300/-400 (option)	52,010	-		-										2	1	4B	14	2	-	5	93	160.9	106	9,499
	GE	CF6-80C2B4	767-200ER/-300/-300ER	57,180	-	0.326	-		29.9		5.15						2	1	4B	14	2	-	5	93	160.9	106	9,399
	GE	CF6-80C2B4F	767-200ER/-300/-300ER	57,280	-	0.317	-		29.9		5.14						2	1	4B	14	2	-	5	93	160.9	106	9,760
	GE	CF6-80C2B5F	747-400/-400ER/-400F/-400FER	60,030	-	0.323	-		31.4								2	1	4B	14	2	-	5	93	160.9	106	9,760
	GE	CF6-80C2B6	767-300/-300ER, 767-200ER (option), An-218-200/-300 (proposed)	60,070	-	0.334	-		31.1		5.06						2	1	4B	14	2	-	5	93	160.9	106	9,670
	GE	CF6-80C2B6F	767-300ER, 767-200ER (option)	60,030	-	0.323	-		31.4		5.06						2	1	4B	14	2	-	5	93	160.9	106	9,760
	GE	CF6-80C2B6FA	767-200ER	60,030	-	0.323	-		31.4								2	1	4B	14	2	-	5	93	160.9	106	9,760
	GE	CF6-80C2B7F	767-300ER/-300F, 767-200ER (option)	60,030	-	0.323	-		31.4								2	1	4B	14	2	-	5	93	160.9	106	9,760
	GE	CF6-80C2B8F	767-400ER/-400FER	60,030	-		-		31.4								2	1	4B	14	2	-	5	93	160.9	106	9,970
	GE	CF6-80C2B9F	747-400XQLR/-XQLRF	63,300	-		-		31.4								2	1	4B	14	2	-	5	93	160.9	106
	GE	CF6-80C2B10F	747-XQLRF		-		-		31.4								2	1	4B	14	2	-	5	93	160.9	106
	GE	CF6-80C2D1F	MD-11/-11F/-11F(AF)/-11F(C)	60,690	-	0.322	-		31.8		5.03						2	1	4B	14	2	-	5	93	160.9	106	9,850
	GE	CF6-80C2G2	767-400ERX, 747-400X (not produced)		-		-										2	1	4B	14	2	-	5	93	160.9	106
	GE	CF6-80C2L1F	(see military turbofan specifications)	51250
	GE	CF6-80E1	A330-200/-300 (option)	65,500	-	0.329	-	1913	32		5.3						2	1	4B	14	2	-	4		164.3	114	11,162
	GE	CF6-80E1A1	A330-200/-300 (option)	63,290	-		-		32		5.3						2	1	4B	14	2	-	5		164.3	114	11,162
	GE	CF6-80E1A2	A330-201/-301	64,530	-		-		32.6		5.3						2	1	4B	14	2	-	5		164.3	114	11,162
	GE	CF6-80E1A3	A330-203/-303	68,530	-		-		33.7		5						2	1	4B	14	2	-	5		171	114	10,726
	GE	CF6-80E1A4	A330-202/-302, KR-860 (not produced)	66,870	-	0.338	-		33.7		5						2	1	4B	14	2	-	5		171	114	10,726
	GE	CF6-80E1A4/B	A330-202/-302	68,530	-		-		33.7		5						2	1	4B	14	2	-	5		171	114	10,726
	GE	CF34-1A	Challenger 601-1A	9,140	-	0.36	-				6.2						2	1	-	14	2	-	4	44	103.2	49.6	1,625
	GE	CF34-3A	Challenger 601-3A	9,220	-	0.357	-	332	21		6.3						2	1	-	14	2	-	4	44	103.2	49.6	1,625
	GE	CF34-3A1	CRJ100ER/CRJ100LR, Challenger 601-3R	9,220	-	0.357	-	332	21		6.3						2	1	-	14	2	-	4	44	103.2	49.6	1,655
	GE	CF34-3A2	Challenger 601-3A/ER	9,220	-	0.357	-	332	21		6.3						2	1	-	14	2	-	4	44	103.2	49.6	1,625
	GE	CF34-3B	Challenger 604/605/650	9,220	-	0.346	-		21		6.3						2	1	-	14	2	-	4	44	103.2	49.6	1,670
	GE	CF34-3B1	CRJ200ER/200LR, CRJ440ER/LR, Challenger 800/850	9,220	-	0.346	-		21		6.3						2	1	-	14	2	-	4	44	103.2	49.6	1,670
	GE	CF34-8C1	CRJ701/-701ER	13,790	-	0.37	-		27		4.9						2	1	-	10	2	-	4	46.2	152.3	60.7	2,704
	GE	CF34-8C5	CRJ550, CRJ705/-705ER, CRJ900/900ER, CRJ900 NextGen	14,510	-	0.39	-				4.9						2	1	-	10	2	-	4	46.2	151.6	60.7	2,780
	GE	CF34-8C5A1	CRJ1000 NextGen	14,510	-		-										2	1	-	10	2	-	4	46.2	151.6	60.7	2,780
	GE	CF34-8C5A2		14,510	-		-										2	1	-	10	2	-	4	46.2	151.6	60.7	2,780
	GE	CF34-8C5A3		14,510	-		-										2	1	-	10	2	-	4	46.2	151.6	60.7	2,780
	GE	CF34-8C5B1	CRJ700 NextGen	13,790	-		-										2	1	-	10	2	-	4	46.2	151.6	60.7	2,780
	GE	CF34-8D??	SL-200/-300 (not produced)		-		-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8D1	728-100, 528-100 (not produced)	13,830	-	0.39	-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8D3	728-200 (not produced)	14,240	-	0.39	-		27		4.9						2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8D5		14,470	-	0.39	-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8D6	Envoy 7 (not produced)	14,470	-	0.39	-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8E2	E170/170LR, E175/175LR	13,300	-	0.39	-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8E2A1		13,300	-		-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8E5	E170/170LR, E175/175LR	14,510	-		-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8E5A1	E170/170LR, E175/175LR	14,510	-		-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8E5A2		14,510	-		-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8E5A3			-		-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8E6		14,050	-		-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8E6A1		14,050	-		-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-8E??	RRJ (candidate engine)		-		-										2	1	-	10	2	-	4	46.2	121.2	62.7	3,148
	GE	CF34-10A	ARJ21-700/-900	18,000	-		-										2	1	3B	9	1	-	4
	GE	CF34-10A16		17,640	-		-										2	1	3B	9	1	-	4		158.6	79.3	4,644
	GE	CF34-10D5	928-100 (not produced)	17,355	-	0.38	-		29		5						2	1	3B	9	1	-	4		90	57	3,800
	GE	CF34-10D6	928-200 (not produced)	18,750	-	0.38	-		29		5						2	1	3B	9	1	-	4		90	57	3,800
	GE	CF34-10E2A1		16,960	-		-										2	1	3B	9	1	-	4		177.93	86.59	4,584
	GE	CF34-10E5	E190/190LR, E195/195LR	18,820	-	0.38	-										2	1	3B	9	1	-	4		177.93	86.59	4,584
	GE	CF34-10E5A1	E190/190LR/190SR, E195/195LR	18,820	-	0.38	-										2	1	3B	9	1	-	4		177.93	86.59	4,584
	GE	CF34-10E6	E190/190LR, E195/195LR	18,820													2	1	3B	9	1	-	4		177.93	86.59	4,584
	GE	CF34-10E6A1	E190/190LR, E195/195LR	18,820													2	1	3B	9	1	-	4		177.93	86.59	4,584
	GE	CF34-10E7	E190/190LR/190SR, E195/195LR	20,360													2	1	3B	9	1	-	4		177.93	86.59	4,584
	GE	CF34-10E7-B	Lineage 1000	20,360													2	1	3B	9	1	-	4		177.93	86.59	4,584
	GE	CF700-2B	Falcon 20		-		-	84			1.9						2	1 aft	-	8	2	-	1		53.6	33.2
	GE	CF700-2C	Falcon 20C	4,200	-	0.652	-	84	6.9		1.9						2	1 aft	-	8	2	-	1		53.6	33.1	765
	GE	CF700-2D	Mystere 20, Falcon 20D	4,325	-	0.652	-	84	6.2		1.9						2	1 aft	-	8	2	-	1		53.6	33.1	799
	GE	CF700-2D2	Falcon 20E/F, Sabreliner 75A/80A	4,500	-	0.643	-	84	6.9		1.9						2	1 aft	-	8	2	-	1		53.6	33.1	829
	GE	CJ610-1	Learjet 23, HFB 320, 1121A Commdore	2,850	-	0.99	-	44		-	-						1	-	-	8	2	-	-	-	50.4	17.6	403
	GE	CJ610-2B	HFB 320	2,400	-		-			-	-						1	-	-	8	2	-	-	-	51.1	17.7	399
	GE	CJ610-4	Learjet 23/24A, ViperJet	2,850	-	0.99	-	44		-	-						1	-	-	8	2	-	-	-	50.4	17.6	393
	GE	CJ610-5	HFB 320, 1121B/1122 Commodore	2,950	-	0.98	-	44	6.8	-	-						1	-	-	8	2	-	-	-	50.4	17.6	406
	GE	CJ610-6	Learjet 24B/D, Learjet 24C (not produced)	2,950	-	0.98	-	44	6.8	-	-						1	-	-	8	2	-	-	-	50.4	17.6	418
	GE	CJ610-8	HFB 320	3,100	-		-	44		-	-						1	-	-	8	2	-	-	-	40.5	17.6	411
	GE	CJ610-8A	Learjet 24E/F/25B/25C/25D/28/29	2,950	-		-	44		-	-						1	-	-	8	2	-	-	-	40.5	17.6	433
	GE	CJ610-9	HFB 320, 1123 Commodore	3,100	-	1	-	44	6.8	-	-						1	-	-	8	2	-	-	-	40.5	17.6	421
	GE	CJ805-3	Convair CV-880	11,200	-		-										2	1 aft	-	17	3	-	1		110.4	48.8	2,850
	GE	CJ805-3A	Convair CV-880-22	11,200	-		-										2	1 aft	-	17	3	-	1		110.4	48.8	2,850
	GE	CJ805-3B	Convair CV-880-22M	11,650	-		-										2	1 aft	-	17	3	-	1		110.4	48.8	2,875
	GE	CJ805-11			-		-										2	1 aft	-	17	3	-	1
	GE	CJ805-13			-		-										2	1 aft	-	17	3	-	1
	GE	CJ805-23		15,850	-		-										2	1 aft	-	17	3	-	1		130.6	56	3,810
	GE	CJ805-23A		15,850	-		-										2	1 aft	-	17	3	-	1		130.6	56	3,810
	GE	CJ805-23B	Convair CV-990/-990A	16,100	-	0.53	-	171	13								2	1 aft	-	17	3	-	1		130.6	56	3,810
	GE	CJ805-23C	Caravelle 7/10A	16,100	-		-										2	1 aft	-	17	3	-	1		130.6	56	3,810
	GE	GE1	Technology demonstrator	5,000	-	0.7	-	77	11	-	-						1	-	-	14	2	-	-	-
	GE	GE4/F6A		27,200	45,000			550	11	2.2	1.1																7,670
	GE	GE4/J4C		38,900	58,100			475	9.5	-	-																8,351
	GE	GE4/J5P	B-2707-200/-300 (not produced)	50,000	63,200	1.04	1.86	646	12.5	-	-					1497	1	-	-	9	2	-	-	-	308	89.5	11,300
	GE	GE39	Technology demonstrator														2	2 UDF	-			-	-
	GE	GE90-76B	777-200	81,070	-		-		39.3	1.65	8.4	17,500	0.545	0.83	35,000		2	1	3B	10	2	-	6	123	286.9	155.6	17,400
	GE	GE90-77B	777-200	81,700	-		-		39.3	1.65	8.4						2	1	3B	10	2	-	6	123	286.9	155.6	17,400
	GE	GE90-85B	777-200	88,870	-		-		39.3	1.65	8.4	17,500	0.52	0.83	35,000		2	1	3B	10	2	-	6	123	286.9	155.6	17,400
	GE	GE90-90B	777-200	94,000	-		-		40	1.65	8.4						2	1	3B	10	2	-	6	123	286.9	155.6	17,400
	GE	GE90-92B	777-200 (option)	92,000	-		-		40	1.65	8.3						2	1	3B	10	2	-	6	123	286.9	155.6	17,400
	GE	GE90-94B	777-200	97,300	-		-		40	1.65							2	1	3B	10	2	-	6	123	286.9	155.6	17,400
	GE	GE90-110B1	777-200LR/777F, 777-300ER (option)	110,760	-		-										2	1	??	??	??	-	??	123	286.9	155.6	19,316
	GE	GE90-113B		113,530	-		-										2	1	??	??	??	-	??	123	286.9	155.6	19,316
	GE	GE90-115B	777-200LR/-300ER/777F	115,540	-		-		42								2	1	4B	9	2	-	6	123	286.9	155.6	19,316
	GE	GE9X-105B1A	777-8/-9/-10X	105,000	-		-		60		10						2	1	3	11	2	-	6	134
	GE	GEnx-1B54	787-3 (proposed)	57,400	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B54/P1	787-3 (proposed)	57,400	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B54/P2	787-3 (proposed)	57,400	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B58	787-3 (proposed)	61,000	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B58/P2	787-3 (proposed)	61,000	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B64	787-8	67,000	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B64/P1	787-8	67,000	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B64/P2	787-8	67,000	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B67	787-8/-9	69,400	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B67/P1	787-8	69,400	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B67/P2	787-8/-9	69,400	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B70	787-8/-9	72,300	-		-	2559	53.3		9						2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B70/P1	787-8/-9	72,300	-		-	2559	53.3		9						2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B70/P2	787-8/-9	72,300	-		-	2559	53.3		9						2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B70C/P1	787-8/-9	72,300	-		-	2559	53.3		9						2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B70C/P2	787-8/-9	72,300	-		-	2559	53.3		9						2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B70/75/P1	787-8														2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B70/75/P2	787-8/-9														2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B72/P1		72,300	-		-	2559	53.3		9						2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B74	787-9	76,700	-		-	2624	55.4		8.8						2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B74/75/P1	787-9														2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B74/75/P2	787-9/-10														2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B75	787-9	76,700	-		-	2624	55.4		8.8						2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B75/P1	787-9	77,604	-		-				8.8						2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B75/P2	787-9	77,604	-		-				8.8						2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B76	787-10	76,100	-		-	2658	58.1		8.8						2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B76/P2	787-10	78,500	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B76A/P2	787-9/-10	78,500	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-1B78/P2		80,392	-		-										2	1	4	10	2	-	7		194.9	139.1	13,552
	GE	GEnx-2B67	747-8	67,400	-		-										2	1	3	10	2	-	6		185	127.3	12,397
	GE	GEnx-2B67/P	747-8	67,400	-		-										2	1	3	10	2	-	6		185	127.3	12,397
	GE	GEnx-2B67B	747-8	67,400	-		-	2297	52.4		8						2	1	3	10	2	-	6		185	127.3	12,397
	GE	I-A	Technology demonstrator	1,250	-		-		3	-	-						1	-	-	1	1	-	-	-	70.5	44	780
	GE	J85/J1	FH-V4, FH-V6 (not produced)	3,600	5,000	0.95		53	8.3	-	-						1	-	-	9	2	-	-	-
	GE	J97-GE-17	O4-1B (not produced)	11,760
	GE	Passport 20-17BB1A		17,745					45		5.6						2	1	3	10	2	-	4	52	132.5	54.32	4,554
	GE	Passport 20-18BB1A		18,435					45		5.6						2	1	3	10	2	-	4	52	132.5	54.32	4,554
	GE	Passport 20-19BB1A	Global 7500/8000	18,920					45		5.6						2	1	3	10	2	-	4	52	132.5	54.32	4,554
	GE Honda Aero	HF120	Citation CJ/CJ1/CJ1+, S-40	2,095					24		2.9						2	1	-	2	1	-	2		59.5	30.5	466
	GE Honda Aero	HF120-H1A	HondaJet	2,095					24		2.9						2	1	-	2	1	-	2		59.5	30.5	466
	Honeywell	FX5	Falcon 7X (candidate engine)	6,000
	Honeywell	HTF7000	(see Allied Signal AS907-1-1A)
	Honeywell	HTF7250G	(see Allied Signal AS907-2-1G)
	Honeywell	HTF7350	(see Allied Signal AS907-2-1A)
	Honeywell	HTF7500E	(see Allied Signal AS907-3-1E)
	Honeywell	HTF7700L	(see Allied Signal AS907-2-1S)
	Instytut Lotnictwa	D-18A		3,968	-	0.74	-		8	2.07	0.7						2	2	-	5	1	-	1		76.4	35.4	838
	Instytut Lotnictwa	K-15	I-22	3,307	-	1.006	-	52	5.3	-	-						1	-	-	6	1	-	-	-	61.4	35.1	705
	International Aero Engines	V2500 SuperFan	(cancelled)	30,000	-		-				17.5						2	1	3	10	2	-	3
	International Aero Engines	V2500-A1	A320-231	24,800	-	0.35	-	783	29.4	1.65	5.4						2	1	3B	10	2	-	5	63.5	126.0**	67.5	5,300
	International Aero Engines	V2522-A5	A319-131	23,040	-	0.34	-	738	25.2		4.9						2	1	4B	10	2	-	5	63.5	126.0**	67.5	5,300
	International Aero Engines	V2522-D5	MD-90-10 (not produced)	22,000	-	0.34	-	848	25.2		4.9						2	1	4B	10	2	-	5	63.5	126.0**	67.5
	International Aero Engines	V2524-A5	A319-132/-132CJ	24,480	-	0.36	-	772	27.1		4.9						2	1	4B	10	2	-	5	63.5	126.0**	67.5	5,300
	International Aero Engines	V2525-D5	MD-90-30	25,000	-	0.35	-	784	27.7		4.8						2	1	4B	10	2	-	5	63.5	126.0**	67.5	5,720
	International Aero Engines	V2527-A5	A319-133CJ/-133XCJ, A320-232	24,800	-	0.36	-	784	27.7		4.8						2	1	4B	10	2	-	5	63.5	126.0**	67.5	5,300
	International Aero Engines	V2527E-A5	A320-233	24,800	-		-										2	1	4B	10	2	-	5	63.5	126.0**	67.5	5,300
	International Aero Engines	V2527M-A5	A319-133/-133CJ/-133XCJ	24,800	-		-										2	1	4B	10	2	-	5	63.5	126.0**	67.5	5,300
	International Aero Engines	V2528-D5	MD-90-30/-30ER	28,000	-	0.35	-	825	30.4		4.7						2	1	4B	10	2	-	5	63.5	126.0**	67.5	5,720
	International Aero Engines	V2530-A5	A321-131/-232	29,900	-	0.36	-	849	31.6		4.6						2	1	4B	10	2	-	5	63.5	126.0**	67.5	5,300
	International Aero Engines	V2530-D5	MD-90-50 (not produced)	31,600	-	0.36	-		31.6		4.6						2	1	4B	10	2	-	5	63.5	126.0**	67.5
	International Aero Engines	V2531-E5		31,330	-		-										2	1	4B	10	2	-	5	63.5	126.0**	67.5	5,300
	International Aero Engines	V2533-A5	A321-231	31,600	-	0.37	-	872	35.2	1.79	4.5						2	1	4B	10	2	-	5	63.5	126.0**	67.5	5,300
	Ivchenko (Klimov)	AI-25	Yak-40	3,300	-	0.57	-	33	8	1.7	2.1	976	0.795	0.5	20,000		2	3	-	8	1	-	2		78.5	35.3	705
	Ivchenko (Klimov)	AI-25A	Yak-40A	3,850	-		-			1.7	2.1						2	3	-	8	1	-	2
	Kuznetsov	NK-8-2	Tu-154	20,944	-	0.579	-	462	21.5	2.15	1						2	2	2B	6	1	-	2		187.5	56.8	4,629
	Kuznetsov	NK-8-2U	Tu-154A/B	23,150	-	0.569	-	503	23.2	2.15	1.05						2	2	2B	6	1	-	2		187.5	56.8	4,629
	Kuznetsov	NK-8-3	Il-62	20,950	-		-										2	2	2B	6	1	-	2
	Kuznetsov	NK-8-4	Il-62	23,150	-	0.588	-	489	23.2	2.15	1.02						2	2	2B	6	1	-	2		201	56.8	4,629
	Kuznetsov	NK-8-6	(see NK-86)
	Kuznetsov	NK-44
	Kuznetsov	NK-44K
	Kuznetsov	NK-86	Il-86	28,660	-		-	644	13.4		1.15						2	2	2B	6	1	-	2		143	63	5,401
	Kuznetsov	NK-93	Il-96M, Tu-204-230, Tu-330 (proposed)	39,683	-	0.235	-	2205	37	1	16.6						3	2 DPF	7	8	1	1	3	114.2	235.1		8,047
	Kuznetsov	NK-144	Tu-144/-144D/-144LL	28,660	38,580			551	14.2		0.6						2	2	3B	11	1	-	2
	Kuznetsov	NK-144A	Tu-144S (not produced)	33,070	40,000				17		0.53						2	2	3B	11	1	-	2
	Kuznetsov	NK-321	Tu-144	30,843	55,077			805	28.4		1.4						3	3	5	7	1	1	2		236	57.5	7,588
	Lotarev (Motor Sich)	D-18T	An-124-100, An-225	51,660	-	0.36	-	1687	25		5.6	10,716	0.57	0.75	36,100		3	1	7	7	1	1	4	91.7	212.6	115.6	9,039
	Lotarev (Motor Sich)	D-18T-1	An-218-100	48,148	-		-				5.6	11,596	0.615	0.8	36,100		3	1	7	7	1	1	4	91.7	212.6	115.6	9,039
	Lotarev (Motor Sich)	D-18T-3	An-124-100M (proposed)	51,660	-		-										3	1	7	7	1	1	4	91.7	212.6	115.6	9,039
	Lotarev (Progress)	D-18TM	An-218 (proposed)	55,777	-		-	1698			5.5						3	1	7	7	1	1	3		224.5	117.6	10,472
	Lotarev (Progress)	D-18TR	An-218-200/-300 (proposed)	60,627	-		-										3	1	7	7	1	1	3		224.5	117.6	10,472
	Lotarev (PSLM)	DV-2	Il-208 (not produced)	4,850	-		-										2	1	2	7	1	-	2
	Lotarev (PSLM)	DV-2S	(see military turbofan specifications)	5,508	-	0.593	-		15.5		1.4						2	1	2	7	1	-	2
	Lyulka (Saturn)	AL-5	Tu-110	12,125	-		-		10		1						2	2	2B	6	1	-	2
	Maverick	MC-750	MC-2400 Legend	750	-		-			-	-						1	-	-	10	2	-	-
	Mikulin	RD-3	Tu-104	14,881	-		-
	Mikulin	RD-3M	Tu-104A/D/V	19,180	-		-
	Mikulin	RD-3M-500	Tu-104B	21,385	-		-
	Napier	Oryx NOr.1	P.74														1	-	-	12	2	-	-		83.5	19.3	495
	Napier	Oryx NOr.5		950													1	-	-	12	2	-	-		83.5	19.3	515
	Pirna	014-A0	Prototype	6,900	-		-									1050	1	-	-	12	2	-	-		135.7	39	2,340
	Pirna	014-A1	Baade 152	7,300	-		-									1070	1	-	-	12	2	-	-
	Pirna	014-C		7,300	-		-									1070	1	-	-	12	2	-	-
	Pirna	016		7,700	-		-									1035	1	-	-	12	3	-	-
	Pirna	020			-		-										1	-	-	12	3	-	-
	Pratt Whitney	J60-P-3A	S-69	3,000	-	0.96	-	50	6.5								1	-	-	9	2	-	-			22	448
	Pratt Whitney	JT3C-1	Prototype		-		-										2	-	9	7	1	-	2
	Pratt Whitney	JT3C-2	DC-8-11/-12	11,200	13,750		0.95										2	-	9	7	1	-	2	38.8	138.6	38.9	3,870
	Pratt Whitney	JT3C-4	707-120, 720	11,200	11,500												2	-	9	7	1	-	2	38.8	138.6	38.9	4,234
	Pratt Whitney	JT3C-5		11,200													2	-	9	7	1	-	2	38.8	138.6	38.9
	Pratt Whitney	JT3C-6	707-120, DC-8-11/-12	11,200	13,500	0.775											2	-	9	7	1	-	2	38.8	138.6	38.9	4,234
	Pratt Whitney	JT3C-7	720, 720F	12,000	-	0.785	-	187	13								2	-	9	7	1	-	2	38.8	138.6	38.9	3,495
	Pratt Whitney	JT3C-10	DC-8-12														2	-	9	7	1	-	2	38.8	138.6	38.9
	Pratt Whitney	JT3C-12	720, 720F, 707-120 (option)	13,000	-		-										2	-	9	7	1	-	2	38.8	138.6		3,550
	Pratt Whitney	JT3D-1	707-120B/-120BF/-320B, 720B, 720BF, DC-8-51/-52/-53/-54/-55/-55F/-61	17,000	-	0.52	-	450	12.5		1.4						2	2	6B	7	1	-	3	53.1	136.3	53	4,145
	Pratt Whitney	JT3D-1 (HK)	707-120B	17,000	-	0.52	-	450	12.5		1.4						2	2	6B	7	1	-	3	53.1	136.3	53
	Pratt Whitney	JT3D-1 (HK3)	707-120B	17,000	-	0.52	-	450	12.5		1.4						2	2	6B	7	1	-	3	53.1	136.3	53
	Pratt Whitney	JT3D-1 (Q)	707-120B	17,000	-	0.52	-	450	12.5		1.4						2	2	6B	7	1	-	3	53.1	136.3	53
	Pratt Whitney	JT3D-2	(see military turbofan specifications TF33-P-3)
	Pratt Whitney	JT3D-3	707-120B/-320B/-320C, 720B, DC-8-51/-51F/-52/-52F/-53/-53F/-54/-54F/-55/-55F/-61/-61F/-62F (option)	18,000	-	0.535	-										2	2	6B	7	1	-	3			53	4190
	Pratt Whitney	JT3D-3A															2	2	6B	7	1	-	3
	Pratt Whitney	JT3D-3B	707-120B/-320B/-320BH/-320C/-320CH, 720B, 720BF, DC-8-51/-52/-53/-53F/-54/-55/-55F/-61/-62/-62F/-63/-63F	18,000	-	0.51	-	450	13	1.66	1.4						2	2	6B	7	1	-	3	53.1	145.5	53	4,340
	Pratt Whitney	JT3D-3B (HK)	707-120B/-320B/-320BH/-320C/-320CH, 720B, 720BF, DC-8-51/-51F/-52/-53/-53F/-54/-55/-55F/-61/-62F(AF)/-63/-63F	18,000	-	0.51	-	450	13	1.66	1.4						2	2	6B	7	1	-	3	53.1		53
	Pratt Whitney	JT3D-3B (HK2)	707-320B/-320C, DC-8-51/-51F/-52F/-54F/-55F/-61F/-62F(CF)	18,000	-	0.51	-	450	13	1.66	1.4						2	2	6B	7	1	-	3	53.1		53
	Pratt Whitney	JT3D-3B (HK3)	707-320B, DC-8-51/-51F/-52/-54F/-55F/-61/-61F/-62/-62F/-62F(AF)/-62F(CF)	18,000	-	0.51	-	450	13	1.66	1.4						2	2	6B	7	1	-	3	53.1		53
	Pratt Whitney	JT3D-3B (Q)	707-120B, DC-8-51/-51F/-52/-52F/-54/-55/-55F/-61/-61F(AF)/-62/-62F(CF)	18,000	-	0.51	-	450	13	1.66	1.4						2	2	6B	7	1	-	3	53.1		53
	Pratt Whitney	JT3D-3C		18,000	-	0.51	-	450	13	1.66	1.4						2	2	6B	7	1	-	3	53.1	136.3	53	4,340
	Pratt Whitney	JT3D-5	(see military turbofan specifications TF33-P-7)
	Pratt Whitney	JT3D-5A		21,000	-		-										2	2	7B	7	1	-	3	53.1	142.58	53	4,675
	Pratt Whitney	JT3D-7	707-320B/-320C, DC-8-62/-62F/-63/-63F	19,285	-	0.52	-	472	13.5	1.82	1.43						2	2	7B	7	1	-	3	53.1	136.3	53	4,340
	Pratt Whitney	JT3D-7 (HK)	707-320B/-320C	19,285	-	0.52	-	472	13.5	1.82	1.43						2	2	7B	7	1	-	3	53.1		53
	Pratt Whitney	JT3D-7 (HK2)	707-320B/-320C	19,285	-	0.52	-	472	13.5	1.82	1.43						2	2	7B	7	1	-	3	53.1		53
	Pratt Whitney	JT3D-7 (HK3)	707-320B/-320C, DC-8-62/-62F/-62F(AF)/-62F(CF)/-63/-63F/-63F(CF)	19,285	-	0.52	-	472	13.5	1.82	1.43						2	2	7B	7	1	-	3	53.1		53
	Pratt Whitney	JT3D-7 (Q)	DC-8-62F/-63F/-63F(AF)	19,285	-	0.52	-	472	13.5	1.82	1.43						2	2	7B	7	1	-	3	53.1		53
	Pratt Whitney	JT3D-7A		19,285	-	0.52	-	472	13.5	1.82	1.43						2	2	7B	7	1	-	3	53.1	136.3	53	4,340
	Pratt Whitney	JT4A-3	707-220, DC-8-21/-21F/-31/-32/-33 (option)	15,800	-	0.77	-			-	-						2	-	8	7	1	-	2	42.5	188.8	58.5	5,020
	Pratt Whitney	JT4A-5	707-220, DC-8-21/-21F/-31/-32/-33 (option)	15,800	-	0.77	-			-	-						2	-	8	7	1	-	2	42.5	188.8	58.5	5,020
	Pratt Whitney	JT4A-7	707-320 (option)	15,800	-	0.77	-			-	-						2	-	8	7	1	-	2
	Pratt Whitney	JT4A-9	707-220, 707-320, DC-8-21/-21F/-31/-32/-33F/-33F(AF) (option)	16,800	-	0.81	-			-	-						2	-	8	7	1	-	2	42.5	188.8	58.5	5,050
	Pratt Whitney	JT4A-10	707-220, 707-320, DC-8-21/-21F/-31/-32/-33F/-33F(AF) (option)	16,800	-	0.81	-			-	-						2	-	8	7	1	-	2	42.5	188.8	58.5	5,050
	Pratt Whitney	JT4A-11	DC-8-33F/-33F(AF), 707-320 (option)	17,500	-	0.84	-	256	12.5	-	-						2	-	8	7	1	-	2	42.5	188.8	58.5	5,100
	Pratt Whitney	JT4A-12	707-320/-320F, DC-8-21/-31/-32/-33F (option)	17,500	-	0.84	-	256	12.5	-	-						2	-	8	7	1	-	2	42.5	188.8	58.5	5,100
	Pratt Whitney	JT8D-1	Caravelle 10B1R/10B3, DC-9-15	14,000	-	0.585	-	315	15.4	1.9	1.06						2	2	4B	7	1	-	3	42.5	123.5	42.5	3,205
	Pratt Whitney	JT8D-1A		14,000	-	0.585	-	315	15.4	1.9	1.06						2	2	4B	7	1	-	3	42.5	123.5	42.5	3,205
	Pratt Whitney	JT8D-1B		14,000	-	0.585	-	315	15.4	1.9	1.06						2	2	4B	7	1	-	3	42.5	123.5	42.5	3,205
	Pratt Whitney	JT8D-3	(see military turbofan specifications TF33-P-102)
	Pratt Whitney	JT8D-5	DC-9-11	12,250	-	0.565	-										2	2	4B	7	1	-	3	42.5	123.5	42.5	3,205
	Pratt Whitney	JT8D-7	727-100/-100C/-100QC/-100F/-200/-200F, 737-100/-200A/-200CA, DC-9-15/-15F(RC)/-31, Caravelle 10B1R/10B3/11R	14,000	-	0.585	-	315	15.8	1.93	1.07	4,270	0.796	0.8	30,000		2	2	4B	7	1	-	3	42.5	123.5	42.5	3,205
	Pratt Whitney	JT8D-7 (HK3)	727-100/-100C, DC-9-15/-15F(RC)	14,000	-	0.585	-	315	15.8	1.93	1.07	4,270	0.796	0.8	30,000		2	2	4B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-7A	727-100/-100C/-100QC/-100F/-200, 737-100/-200, DC-9-14/-15/-15F(MC)/-31/-31	14,000	-	0.585	-	315	15.8	1.93	1.07	4,270	0.796	0.8	30,000		2	2	4B	7	1	-	3	42.5	123.5	42.5	3,205
	Pratt Whitney	JT8D-7A (HK3)	727-100/-100C, DC-9-15/-15F(RC)/-32	14,000	-	0.585	-	315	15.8	1.93	1.07	4,270	0.796	0.8	30,000		2	2	4B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-7B	727-100/-100C/-100F/-200/-200A/-200F, 737-100/-200, DC-9-14/-15/-15F(MC)/-15F(RC)/-31/-31F/-32	14,000	-	0.585	-	315	15.8	1.93	1.07	4,270	0.796	0.8	30,000		2	2	4B	7	1	-	3	42.5	123.5	42.5	3,205
	Pratt Whitney	JT8D-7B (HK)	727-200F	14,000	-	0.585	-	315	15.8	1.93	1.07	4,270	0.796	0.8	30,000		2	2	4B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-7B (HK3)	727-100/-100C/-100F/-200/-200A/-200AF/-200F, 737-200, DC-9-14/-15/-15F(MC)/-15F(RC)/-31/-32/-32F	14,000	-	0.585	-	315	15.8	1.93	1.07	4,270	0.796	0.8	30,000		2	2	4B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-7B (Q)	727-100/-100F	14,000	-	0.585	-	315	15.8	1.93	1.07	4,270	0.796	0.8	30,000		2	2	4B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-9	727-100/-100C/-200/-200A, 737-200/-200A/-200C/-200CA, DC-9-32/-32F/-33F/-33F(RC), Caravelle 10B3/12	14,500	-	0.565	-	319	15.9	1.91	1.03	4,540	0.8	0.8	30,000		2	2	4B	7	1	-	3	42.5	123.5	42.5	3,252
	Pratt Whitney	JT8D-9 (HK3)	727-200F, DC-9-31/-32/-32F/-33F	14,500	-	0.565	-	319	15.9	1.91	1.03	4,540	0.8	0.8	30,000		2	2	4B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-9A	727-100/-100C/-100F/-200/-200A/-200AF/-200F, 737-100/-200/-200A/-200C/-200CA/-200AF, DC-9-31/-32/-32F/-33F(RC)	14,500	-	0.565	-	319	15.9	1.91	1.03	4,540	0.8	0.8	30,000		2	2	4B	7	1	-	3	42.5	123.5	42.5	3,402
	Pratt Whitney	JT8D-9A (HK3)	727-100/-200/-200A/-200AF/-200F, 737-200/-200A/-200C/-200CA, DC-9-31/-32/-33F(CF)/-33F(RC)	14,500	-	0.565	-	319	15.9	1.91	1.03	4,540	0.8	0.8	30,000		2	2	4B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-11	DC-9-21/-32/-41	15,000	-	0.62	-	327	16.2		1.05	4,750	0.806	0.8	30,000		2	2	6B	7	1	-	3	42.5	123.5	42.5	3,389
	Pratt Whitney	JT8D-11 (HK)	DC-9-21	15,000	-	0.62	-	327	16.2		1.05	4,750	0.806	0.8	30,000		2	2	6B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-11 (HK3)	DC-9-21/-32/-33F/-41	15,000	-	0.62	-	327	16.2		1.05	4,750	0.806	0.8	30,000		2	2	6B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-15	727-200/-200A/-200F/-200AF, 737-200A/-200CA, DC-9-33/-34/-41, Mercure-100	15,500	-	0.63	-	322	16.5		1.03	4,920	0.81	0.8	30,000		2	2	6B	7	1	-	3	42.5	123.5	42.5	3,414
	Pratt Whitney	JT8D-15 (HK)	727-200A, 737-200/-200A	15,500	-	0.63	-	322	16.5		1.03	4,920	0.81	0.8	30,000		2	2	6B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-15 (HK3)	727-200A/-200AF, 737-200/-200A/-200C/-200CA, DC-9-31/-32/-41	15,500	-	0.63	-	322	16.5		1.03	4,920	0.81	0.8	30,000		2	2	6B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-15A	727-200A, 737-200A/-200CA, DC-9-30/-40/-50 (option)	15,500	-	0.59	-	327	16.6		1.04	4,920	0.81	0.8	30,000		2	2	6B	7	1	-	3	42.5	123.5	42.5	3,474
	Pratt Whitney	JT8D-15A (HK3)	727-200A/-200AF, 737-200A/-200CA	15,500	-	0.59	-	327	16.6		1.04	4,920	0.81	0.8	30,000		2	2	6B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-17	727-200A/-200AF, 737-200/-200A/-200CA/-200F/-200AF, DC-9-31/-32/-34/-34F(CF)/-51	16,000	-	0.6	-	324	16.9		1.01	5,140	0.814	0.8	30,000		2	2	6B	7	1	-	3	42.5	123.5	42.5	3,430
	Pratt Whitney	JT8D-17 (HK3)	727-200A/-200AF, 737-200A/-200CA, DC-9-51	16,000	-	0.6	-	324	16.9		1.01	5,140	0.814	0.8	30,000		2	2	6B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-17A	727-200A, 737-200A/-200CA/-200AF, DC-9-41/-51	16,000	-	0.6	-	328	17.1		1.02	5,140	0.773	0.8	30,000		2	2	6B	7	1	-	3	42.5	123.5	42.5	3,475
	Pratt Whitney	JT8D-17A (HK3)	727-200A/-200AF, 737-200A/-200CA, DC-9-41/-51	16,000	-	0.6	-	328	17.1		1.02	5,140	0.773	0.8	30,000		2	2	6B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-17AR	727-200A, 737-200	17,400	-		-	331	17.3	2.16	1	5,140	0.78	0.8	30,000		2	2	6B	7	1	-	3	42.5	123.5	42.5	3,500
	Pratt Whitney	JT8D-17R	727-200/-200A/-200AF	17,400	-		-	331	17.5		1	5,140	0.82	0.8	30,000		2	2	6B	7	1	-	3	42.5	123.5	42.5	3,495
	Pratt Whitney	JT8D-17R (HK3)	727-200A/-200AF	17,400	-		-	331	17.5		1	5,140	0.82	0.8	30,000		2	2	6B	7	1	-	3	42.5		42.5
	Pratt Whitney	JT8D-209	MD-81	19,250	-	0.51	-	471	17.4		1.82	4,945	0.724	0.8	35,000		2	1	6B	7	1	-	3	49.2	154.2	59.2	4,588
	Pratt Whitney	JT8D-216	MD-95-30 (not produced)		-		-										2	1	6B	7	1	-	3	49.2	154.2
	Pratt Whitney	JT8D-217	MD-81/-82	20,850	-	0.53	-	486	18.6		1.77	5,240	0.753	0.8	35,000		2	1	6B	7	1	-	3	49.2	154.2	59.2	4,623
	Pratt Whitney	JT8D-217A	MD-81/-82/-82(SA)	20,850	-	0.53	-	486	18.6		1.77	5,240	0.753	0.8	35,000		2	1	6B	7	1	-	3	49.2	154.2	59.2	4,623
	Pratt Whitney	JT8D-217C	727-100(RE)/-200A(RE)/-200AF(RE), MD-81/-82/-87/-88	20,850	-	0.5	-	497	20.1		1.72	5,240	0.736	0.8	35,000		2	1	6B	7	1	-	3	49.2	154.2	59.2	4,684
	Pratt Whitney	JT8D-218	MD-95-30 (not produced)		-		-										2	1	6B	7	1	-	3	49.2	154.2
	Pratt Whitney	JT8D-219	MD-82/-83/-87/-88, 707-330C(RE), 727-200AF(RE), Aerion SBJ (not produced)	21,700	-	0.519	-	497	20.1	1.91	1.72	5,250	0.737	0.8	35,000		2	1	6B	7	1	-	3	49.2	154.2	59.2	4,684
	Pratt Whitney	JT9D-1	747-100 (option)	42,000				1484	21.5	1.6	5						2	1	3B	11	2	-	4	95.6	154.2
	Pratt Whitney	JT9D-3	747-100 (option)	43,500		0.346			22	1.51	5.2						2	1	3B	11	2	-	4	95.6	154.2		8,430
	Pratt Whitney	JT9D-3A	747-100	43,500	45,800	0.346		1509	21.5	1.51	5.2	10,200	0.624	0.85	35,000		2	1	3B	11	2	-	4	95.6	154.2		8,713
	Pratt Whitney	JT9D-7	747-100/-200B	45,500	47,000	0.355		1521	22.3		5.2	10,200	0.62	0.85	35,000		2	1	3B	11	2	-	4	95.6	154.2		8,880
	Pratt Whitney	JT9D-7A	747-SF/-SP/-100/-100A/-100(SF)/-100F/-100SR/-100SRB/-100SR(SF)/-200/-200B/-200C	46,150	47,670	0.364		1534	22.5		5.1	10,830	0.625	0.85	35,000		2	1	3B	11	2	-	4	95.6	154.2		8,880
	Pratt Whitney	JT9D-7AH	747-SP/-100/-100(SF)/-100F/-200B	46,150	47,670												2	1	3B	11	2	-	4	95.6	154.2		8,880
	Pratt Whitney	JT9D-7ASP	747-SP (option)	46,950	48,570	0.364		1534	22.5		5.1	10,680	0.63	0.85	35,000		2	1	3B	11	2	-	4	95.6	154.2		8,880
	Pratt Whitney	JT9D-7AW	747-200B/-200(SF)/-100SR/-200F, 747-100/-100B (option)														2	1	3B	11	2	-	4	95.6	154.2		8,880
	Pratt Whitney	JT9D-7F	747-SP/-100B/-200/-200B/-200B(M)/-200(SF)/-200F	46,750	48,650	0.367		1565	22.8		5.1	11,050	0.631	0.85	35,000		2	1	3B	11	2	-	4	95.6	154.2		8,880
	Pratt Whitney	JT9D-7FW	747-SP/-200B(SF)/-200C(M)	48,000	50,000												2	1	3B	11	2	-	4	95.6	154.2		8,880
	Pratt Whitney	JT9D-7H	747-100/-200B	45,500	47,000												2	1	3B	11	2	-	4	95.6	154.2		8,880
	Pratt Whitney	JT9D-7J	747-100F/-200B/-200B(M)/-200B(SF)/-200C/-200F	48,650	-		-	1590	23.5		5.1	11,050	0.631	0.85	35,000		2	1	3B	11	2	-	4	95.6	154.2		8,880
	Pratt Whitney	JT9D-7Q	747-200B/-200B(M)/-200B(SF)/-200F	51,900	-		-	1640	24.5		4.9	11,950	0.631	0.85	35,000		2	1	3B	11	2	-	4	93.6	153.6	97.03	9,295
	Pratt Whitney	JT9D-7Q3	747-200B/-200B(M)/-200B(SF)	51,900	-		-	1640	24.5		4.9	11,950	0.631	0.85	35,000		2	1	3B	11	2	-	4	93.6	153.6	97.03	9,295
	Pratt Whitney	JT9D-7R	767-200/-200ER/-200ET/-200PC/-300	48,000	-		-	1585	23.4		4.9	11,200	0.615	0.85	35,000		2	1	4B	11	2	-	4	93.4	153.6		8,915
	Pratt Whitney	JT9D-7R4	A300B4-620, A300C4-620	48,000	-		-	1585	23.4		4.9	11,200	0.615	0.85	35,000		2	1	4B	11	2	-	4	93.4	153.6		8,915
	Pratt Whitney	JT9D-7R4D	767-200/-200ER/-200ET/-200PC/-300	48,000	-	0.343	-	1585	23.4		4.9	11,200	0.615	0.85	35,000		2	1	4B	11	2	-	4	93.4	153.6	96	8,935
	Pratt Whitney	JT9D-7R4D1	A310-221	48,000	-	0.343	-	1585	23.4		4.9	11,200	0.615	0.85	35,000		2	1	4B	11	2	-	4	93.4	153.6	96	8,915
	Pratt Whitney	JT9D-7R4E	767-200ER	50,000	-	0.343	-	1615	24.2		4.9	11,700	0.62	0.85	35,000		2	1	4B	11	2	-	4	93.4	153.6	96	8,915
	Pratt Whitney	JT9D-7R4E1	A310-222/-222F/-322	50,000	-	0.343	-	1615	24.2		4.9	11,700	0.62	0.85	35,000		2	1	4B	11	2	-	4	93.4	153.6	96	8,935
	Pratt Whitney	JT9D-7R4E3	767-200ER	50,000	-	0.343	-	1615	24.2		4.9	11,700	0.62	0.85	35,000		2	1	4B	11	2	-	4	93.4	153.6		9,100
	Pratt Whitney	JT9D-7R4E4	767-200ER	50,000	-	0.343	-	1615	24.2		4.9	11,700	0.62	0.85	35,000		2	1	4B	11	2	-	4	93.4	153.6	96	8,935
	Pratt Whitney	JT9D-7R4G2	747-200B/-200B(SF)/-200F/-300/-300(M)/-300(SF)	54,750	-	0.36	-	1695	26.3		4.8	12,250	0.639	0.85	35,000		2	1	4B	11	2	-	4	93.4	153.6	96	9,170
	Pratt Whitney	JT9D-7R4H1		56,000	-	0.364	-	1695	26.7		4.8	12,250	0.628	0.85	35,000		2	1	4B	11	2	-	4	93.4	153.6	96	8,915
	Pratt Whitney	JT9D-7W	747-200B								4.9						2	1	3B	11	2	-	4	95.6	154.2
	Pratt Whitney	JT9D-9		53,000	-		-										2	1	3B	11	2	-	4	95.6	154.2
	Pratt Whitney	JT9D-15	DC-10-20/-40 (option), MD-11 (proposed)	45,500	47,000	0.355											2	1	3B	11	2	-	4	95.6
	Pratt Whitney	JT9D-17		48,000													2	1	3B	11	2	-	4	95.6
	Pratt Whitney	JT9D-20	DC-10-40, MD-11 (proposed)	44,500	47,500	0.37		1521	21.1		5.2	10,680	0.624	0.85	35,000		2	1	3B	11	2	-	4	95.6	153.6		8,470
	Pratt Whitney	JT9D-20J	DC-10-40, MD-11 (proposed)	48,050	47,500	0.37		1521	21.1		5.2	10,680	0.624	0.85	35,000		2	1	3B	11	2	-	4	95.6	153.6		8,580
	Pratt Whitney	JT9D-25	DC-10-20 (option), MD-11 (proposed)	47,000	50,000						5.2						2	1	3B	11	2	-	4	95.6	153.6
	Pratt Whitney	JT9D-59		53,000	-	0.375	-	1639	24.5		4.9	11,950	0.631	0.85	35,000		2	1	4B	11	2	-	4	95.6	153.6	97.03	9,140
	Pratt Whitney	JT9D-59A	A300B4-120, DC-10-40(D)/-40(I)/-40F, A300B4-220/-220F/-220FF/-320 (option)	51,720	-		-										2	1	4B	11	2	-	4	95.6	153.6		9,140
	Pratt Whitney	JT9D-59B	A300B4-220/-220F/-220FF	54,500	-		-	1660	25.2		4.8	12,200	0.631	0.85	35,000		2	1	4B	11	2	-	4	95.6	153.6		9,160
	Pratt Whitney	JT9D-70A	747-200B/-200B(M)/-200B(SF)/-200F	51,140	-		-										2	1	4B	11	2	-	4	95.6	153.6	97.03	9,155
	Pratt Whitney	JT9D-70B		54,500	-		-	1660	25.2		4.8	12,200	0.631	0.85	35,000		2	1	4B	11	2	-	4	95.6	153.6		9,175
	Pratt Whitney	JT10D-132	(see PW2037)
	Pratt Whitney	JT11D-20	(see military turbofan specifications J58-P-4)
	Pratt Whitney	JT11F-4		33,190	50,400			640	8.2	2.5	1.06																9,555
	Pratt Whitney	JT11F-12		33,800	51,100			640	9.5	2.5	1.08																9,135
	Pratt Whitney	JT12A-3	(see military turbofan specifications)
	Pratt Whitney	JT12A-5	(see military turbofan specifications)
	Pratt Whitney	JT12A-6	Sabreliner 40/50	3,000	-	0.96	-			-	-						1	-	-	9	2	-	-	-	78.3	22.1	448
	Pratt Whitney	JT12A-6A	Sabreliner 40/50, JetStar I	3,000	-	0.96	-			-	-						1	-	-	9	2	-	-	-	78.3	22.1	448
	Pratt Whitney	JT12A-8	Sabreliner 60, JetStar I	3,300	-	0.995	-	51	6.7	-	-						1	-	-	9	2	-	-	-	78.3	22.1	468
	Pratt Whitney	JT12A-8A	Sabreliner 60, JetStar I	3,300	-	0.995	-	51	6.7	-	-						1	-	-	9	2	-	-	-	78.3	22.1	468
	Pratt Whitney	JTF10A-2	Model 2086 (not produced)	10,000	-	0.82	-										2	3	6B	7	1	-	3			42.1	2,715
	Pratt Whitney	JTF14	Technology demonstrator		-		-
	Pratt Whitney	JTF15A-1		32,600	51,200			630	11	2.5	1.3																8,485
	Pratt Whitney	JTF17A-21	L-2000-7B (not produced), B-2707-200/-300 (candidate engine)	38,300	61,000	0.75	1.78	675									2	2	-	6	1	-	2
	Pratt Whitney	PW1122G-JM	A319-172N (proposed)	24,240	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1124G-JM	A319-171N (proposed)	24,240	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1124G1-JM	A320-272N	24,240	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1127G-JM	A320-271N	27,075	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1127GA-JM	A320-271N	27,075	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1127G1-JM	A319-173N (proposed)	27,075	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1129G-JM	A320-273N	29,245	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1130G-JM	A321-272N/-272NX	33,110	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1133G-JM	A321-271N/-271NX	33,110	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1133GA-JM	A321-271N/-271NX	33,110	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1135GA-JM	A321-273N (proposed)		-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1215G	MRJ70	15,600	-		-										1	1G	3	8	2	-	3		113.5	62.0	3,800
	Pratt Whitney	PW1217G	MRJ90	19,190	-		-										1	1G	3	8	2	-	3		113.5	62.0	3,800
	Pratt Whitney	PW1428G-JM	MC-21	29,761	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1428GA-JM	MC-21	29,761	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1428GH-JM	MC-21	29,761	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1431G-JM	MC-21	31,572	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1431GA-JM	MC-21	31,572	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1431GH-JM	MC-21	31,572	-		-										1	1G	3	8	2	-	3	56	133.9	57.6	6,300
	Pratt Whitney	PW1519G	A220-100/-300	19,775	-		-										1	1G	3	8	2	-	3	56	125.4	79	4,800
	Pratt Whitney	PW1521G	A220-100/-300	21,970	-		-										1	1G	3	8	2	-	3	56	125.4	79	4,800
	Pratt Whitney	PW1521G-3	A220-100/-300 (option)	21,970	-		-										1	1G	3	8	2	-	3	56	125.4	79	4,800
	Pratt Whitney	PW1521GA	A220-100/-300	21,970	-		-										1	1G	3	8	2	-	3	56	125.4	79	4,800
	Pratt Whitney	PW1524G	A220-100	24,400	-		-										1	1G	3	8	2	-	3	56	125.4	79	4,800
	Pratt Whitney	PW1524G-3	A220-300	24,400	-		-										1	1G	3	8	2	-	3	56	125.4	79	4,800
	Pratt Whitney	PW1525G	A220-100/-300 (option)	24,400	-		-										1	1G	3	8	2	-	3	56	125.4	79	4,800
	Pratt Whitney	PW1525G-3	A220-100/-300 (option)	24,400	-		-										1	1G	3	8	2	-	3	56	125.4	79	4,800
	Pratt Whitney	PW1715G	E175-E2	15,000	-		-										1	1G	3	8	2	-	3	56	125.4	79	6,300
	Pratt Whitney	PW1919G	E190-E2	22,550	-		-										1	1G	3	8	2	-	3	73	125.4	79	4,800
	Pratt Whitney	PW1921G	E195-E2	22,550	-		-										1	1G	3	8	2	-	3	73	125.4	79	4,800
	Pratt Whitney	PW1922G	E190-E2	23,815	-		-										1	1G	3	8	2	-	3	73	125.4	79	4,800
	Pratt Whitney	PW1923G		23,815	-		-										1	1G	3	8	2	-	3	73	125.4	79	4,800
	Pratt Whitney	PW1923G-A	E195-E2	23,815	-		-										1	1G	3	8	2	-	3	73	125.4	79	4,800
	Pratt Whitney	PW2037	757-200/-200ET	37,530	-	0.335	-	1210	27.9	1.63	5.8	6,500	0.582	0.85	35,000		2	1	4B	12	2	-	5	78.5	141.4	84.8	7,300
	Pratt Whitney	PW2037D	757-200/-200ET	37,530	-	0.335	-	1210	27.9	1.63	5.8	6,500	0.582	0.85	35,000		2	1	4B	12	2	-	5	78.5	141.4	84.8	7,300
	Pratt Whitney	PW2037M	757-200/-200ET	37,530	-	0.335	-	1210	27.9	1.63	5.8	6,500	0.582	0.85	35,000		2	1	4B	12	2	-	5	78.5	141.4	84.8	7,300
	Pratt Whitney	PW2040	757-200/-200ET/-200F	40,900	-	0.33	-	1255	27.6	1.66	5.9	6,500	0.582	0.85	35,000		2	1	4B	12	2	-	5	78.5	141.4	84.8	7,300
	Pratt Whitney	PW2040D	757-200/-200ET/-200F	40,900	-	0.33	-	1255	27.6	1.66	5.9	6,500	0.582	0.85	35,000		2	1	4B	12	2	-	5	78.5	141.4	84.8	7,300
	Pratt Whitney	PW2043	757-300, 757-200/-200ET/-200F (option)	43,000	-	0.35	-		31.2		6						2	1	4B	12	2	-	5	78.5	141.4	84.8	7,300
	Pratt Whitney	PW2143	A340-521, A340-621 (not produced)	43,000	-	0.35	-		31.2		6						2	1	4B	12	2	-	5	78.5	141.4	84.8	7,300
	Pratt Whitney	PW2237	Tu-204-140/-140C (proposed)	36,600	-	0.335	-	1210	27.9	1.63	5.8	6,500	0.582	0.85	35,000		2	1	4B	12	2	-	5	78.5	141.4	84.8	7,300
	Pratt Whitney	PW2240	Tu-204-240/-240C, Tu-330 (Tu-204-330) (proposed)	40,100	-	0.33	-	1255	27.6	1.66	5.9	6,500	0.582	0.85	35,000		2	1	4B	12	2	-	5	78.5	141.4	84.8	7,300
	Pratt Whitney	PW2337	Il-96M/T	36,600	-	0.335	-	1210	27.9	1.63	5.8	6,500	0.582	0.85	35,000		2	1	4B	12	2	-	5	78.5	141.4	84.8	7,300
	Pratt Whitney	PW2643		43,000	-	0.35	-		31.2		6						2	1	4B	12	2	-	5	78.5	141.4	84.8	7,300
	Pratt Whitney	PW4050		50,000	-		-		27.5	1.7	4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4052	767-200ER/-300ER	52,200	-	0.312	-	1705	27.5	1.7	4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4056	747-400/-400(M)/-400F, 767-200ER/-300/-300ER, Stratolaunch	56,750	-	0.32	-	1705	30.2	1.7	4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4060	767-300/-300ER, An-218-200/-300 (proposed)	60,000	-	0.33	-	1705	31.5		4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4060A	767-200ER	61,570	-	0.33	-	1705	31.5		4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4060C		60,000	-	0.33	-	1705	31.5		4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4062	767-300ER, 747-400/-400ER/-400F/-400FER, 767-200ER/-200FER/-300F/-400ER (option)	62,000	-		-		32.3	1.8	4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4062A		62,000	-		-		32.3	1.8	4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4074	777-200	77,440	-		-	2550	30.3		6						2	1	6B	11	2	-	7	112	191.7	118.5	15,095
	Pratt Whitney	PW4077	777-200	76,960	-		-	2550	31.5		6.2						2	1	6B	11	2	-	7	112	191.7	118.5	15,095
	Pratt Whitney	PW4077D			-		-										2	1	6B	11	2	-	7	112	191.7	118.5	15,095
	Pratt Whitney	PW4084	777-200	86,760	-		-	2550	34.2	1.68	6.41						2	1	6B	11	2	-	7	112	191.7	118.5	15,095
	Pratt Whitney	PW4084D			-		-										2	1	6B	11	2	-	7	112	191.7	118.5	15,095
	Pratt Whitney	PW4090	777-200/-300	90,200	-		-	2712	38.6	1.7	6.3						2	1	6B	11	2	-	7	112	191.7	118.5	15,584
	Pratt Whitney	PW4090D			-		-										2	1	6B	11	2	-	7	112	191.7	118.5	15,584
	Pratt Whitney	PW4090-3	777-200		-		-										2	1	6B	11	2	-	7	112	191.7	118.5	15,584
	Pratt Whitney	PW4098	777-300	98,000	-		-	2800	42.8	1.75	5.8	14,000	0.581	0.83	35,000		2	1	7B	11	2	-	7	112	194.7	119.5	16,500
	Pratt Whitney	PW4152	A310-324/-324ET/-324F	52,200	-	0.312	-	1705	27.5	1.7	4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4156	A300B4-622/-622R, A310-325/ET	56,000	-	0.32	-	1705	30.2	1.7	4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4156A	A310-325/ET	56,000	-	0.32	-	1705	30.2	1.7	4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4158	A300B4-622R/-622RF, A300F4-622R	58,000	-	0.323	-	1705	30.6		4.75						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4160		60,000	-		-	1934	32	1.75	5.1						2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4164	A330-321, A330-221 (option)	64,500	-		-	1934	32	1.75	5.1						2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4164-1D		64,500	-		-										2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4164C		64,500	-		-										2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4164C-1D		64,500	-		-										2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4164C/B		68,600	-		-										2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4164C/B-1D		68,600	-		-										2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4168	A330-222/-322	68,600	-		-	1934	32	1.75	5.1						2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4168-1D		68,600	-		-										2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4168A	A330-223/-322, KR-860 (not produced)	68,600	-		-	1934	32	1.75	5.1						2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4168A-1D		68,600	-		-										2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4170	A330-223F/-323	70,000	-		-	1934	32	1.75	5.1						2	1	5B	11	2	-	5	99.8	163.1	106.9	12,400
	Pratt Whitney	PW4460	MD-11/-11F/-11F(AF)	60,000	-	0.33	-	1705	31.5		4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4462	MD-11/-11F/-11F(CF)	62,000	-		-		32.3	1.8	4.85						2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW4650	(see military turbojet specification)	51,400	-		-										2	1	4B	11	2	-	4	93.6	132.2	97	9,213
	Pratt Whitney	PW6122	A318-121, Il-214 (candidate engine), A316/A317 (not produced)	22,100	-	0.36	-		27.2								2	1	4B	5	1	-	3	56.5	108.21	62.4	5,400
	Pratt Whitney	PW6124	A318-122	23,800	-	0.37	-		29.6		4.9						2	1	4B	5	1	-	3	56.5	108.21	62.4	5,400
	Pratt Whitney	PW8160	A340-521, A340-621 (proposed)	65,000	-		-										2	1G	3B	5	1	-	3
	Pratt Whitney Canada	JT15D-1	Citation, SN.600 prototype, MH02, SportJet II, JW-1	2,200	-	0.54	-	75			3.3						2	1	-	1C	1	-	2	27.3	57.0	35.3	509
	Pratt Whitney Canada	JT15D-1A	Citation I/ISP	2,200	-	0.54	-	75			3.3						2	1	-	1C	1	-	2	27.3	57.0	35.3	509
	Pratt Whitney Canada	JT15D-1B	Citation I/ISP	2,200	-	0.54	-	75	10	1.5	3.3						2	1	-	1C	1	-	2	27.3	57.0	35.3	509
	Pratt Whitney Canada	JT15D-4	Citation II/IISP, SN.601 Corvette, Diamond I	2,500	-	0.562	-				2.6						2	1	1B	1C	1	-	2	20.8	60.4	35.3	557
	Pratt Whitney Canada	JT15D-4B	Citation S/II	2,500	-	0.562	-				2.6						2	1	1B	1C	1	-	2	20.8	60.4	35.3	557
	Pratt Whitney Canada	JT15D-4C	S211	2,500	-	0.562	-				2.6						2	1	1B	1C	1	-	2	20.8	60.4	35.3	557
	Pratt Whitney Canada	JT15D-4D	Diamond IA	2,500	-	0.562	-				2.6						2	1	1B	1C	1	-	2	20.8	60.4	35.3	557
	Pratt Whitney Canada	JT15D-5	Beechjet 400 (Diamond II)/Hawker 400XP, Beechjet 400A/400T	2,900	-	0.551	-	93	12.6		2						2	1	1B	1C	1	-	2	20.5	63	27	632
	Pratt Whitney Canada	JT15D-5A	Citation V	2,900	-	0.551	-				2						2	1	1B	1C	1	-	2	20.5	63	27	632
	Pratt Whitney Canada	JT15D-5B	(see military turbofan specifications)
	Pratt Whitney Canada	JT15D-5C	S211A	3,190	-	0.551	-				2						2	1	1B	1C	1	-	2	20.5	63	27	665
	Pratt Whitney Canada	JT15D-5D	Citation Ultra, VisionAire Vantage	3,045	-	0.55	-		13.1		2						2	1	1B	1C	1	-	2	20.5	63	27	627
	Pratt Whitney Canada	JT15D-5F		2,900	-		-				2						2	1	1B	1C	1	-	2	20.5	63	27	665
	Pratt Whitney Canada	JT15D-5R		2,900	-		-				2						2	1	1B	1C	1	-	2	20.5	63	27	665
	Pratt Whitney Canada	PW305		4,750	-		-				4.3						2	1	-	4 + 1C	2	-	3	30.7	81.5	36.5	993
	Pratt Whitney Canada	PW305A	Learjet 60/60XR	4,679	-	0.388	-		15.5	1.5	4.3						2	1	-	4 + 1C	2	-	3	30.7	81.5	36.5	993
	Pratt Whitney Canada	PW305B	Hawker 1000	5,266	-	0.391	-	180	15.5		4.3						2	1	-	4 + 1C	2	-	3	30.7	81.5	36.5	993
	Pratt Whitney Canada	PW306A	G200 (Galaxy)	6,040	-	0.394	-		18.3	1.57	4.5						2	1	-	4 + 1C	2	-	3	31.7	75.6		1,043
	Pratt Whitney Canada	PW306B	328JET, Envoy 3	6,050	-		-				4.5						2	1	-	4 + 1C	2	-	3	31.7	75.6		1,043
	Pratt Whitney Canada	PW306C	Citation Sovereign	5,770	-		-				4.5						2	1	-	4 + 1C	2	-	3	31.7	75.6		1,043
	Pratt Whitney Canada	PW306D	Citation Sovereign+	5,907	-		-				4.5						2	1	-	4 + 1C	2	-	3	31.7	75.6		1,043
	Pratt Whitney Canada	PW306D1	Citation Lattitude	5,907	-		-				4.5						2	1	-	4 + 1C	2	-	3	31.7	75.6		1,043
	Pratt Whitney Canada	PW307A	Falcon 7X	6,405	-		-										2	1	-	4 + 1C	2	-	3	31.7	75.6
	Pratt Whitney Canada	PW307B	Learjet 85 (not produced)		-		-										2	1	-	4 + 1C	2	-	3	31.7	75.6
	Pratt Whitney Canada	PW307D	Falcon 8X	6,725	-		-										2	1	-	4 + 1C	2	-	3	31.7	75.6
	Pratt Whitney Canada	PW308A	Hawker 4000	6,904	-		-				4.1						2	1	-	4 + 1C	2	-	3	31.7	75.6
	Pratt Whitney Canada	PW308B	428JET (not produced)	8,089	-		-				4.1						2	1	-	4 + 1C	2	-	3	31.7	75.6
	Pratt Whitney Canada	PW308C	Falcon 2000DX/2000EX/2000LX	7,002	-		-				4.1						2	1	-	4 + 1C	2	-	3	31.7	75.6
	Pratt Whitney Canada	PW530A	Citation Bravo	2,887	-		-		13.3	1.62	3.7						2	1	-	2 + 1C	1	-	2	22.8	60		616
	Pratt Whitney Canada	PW535A	Citation Encore	3,400	-		-				2.6						2	1	1B	2 + 1C	1	-	3
	Pratt Whitney Canada	PW535B	Citation Encore+	3,400	-		-				2.6						2	1	1B	2 + 1C	1	-	3
	Pratt Whitney Canada	PW535E	Phenom 300	3,360	-		-										2	1	1B	2 + 1C	1	-	3
	Pratt Whitney Canada	PW545A	Citation Excel	3,952	-		-		15.7	1.59	4.12						2	1	1B	2 + 1C	1	-	3	27.2	68	32	815
	Pratt Whitney Canada	PW545B	Citation XLS	4,119	-		-		15.7	1.59	4.12						2	1	1B	2 + 1C	1	-	3	27.2	68	32	815
	Pratt Whitney Canada	PW545C	Citation XLS+	4,119	-		-		15.7	1.59	4.12						2	1	1B	2 + 1C	1	-	3	27.2	68	32	815
	Pratt Whitney Canada	PW610F	Eclipse 500, Eclipse 700 (not produced)	1,112	-		-										2	1	-	1 + 1C	1	-	1
	Pratt Whitney Canada	PW610F-A		950	-		-										2	1	-	1 + 1C	1	-	1
	Pratt Whitney Canada	PW615F	Citation Mustang, Eclipse 500, ProJet (candidate engine), NauticAir 450 (not produced)	1,460	-		-										2	1	-	1 + 1C	1	-	1
	Pratt Whitney Canada	PW615F-A		1,460	-		-										2	1	-	1 + 1C	1	-	1
	Pratt Whitney Canada	PW617F	Phenom 100/100E	1,695	-		-										2	1	-	1 + 1C	1	-	1
	Pratt Whitney Canada	PW617F-E	Phenom 100EV	1,820	-		-										2	1	-	1 + 1C	1	-	1
	Pratt Whitney Canada	PW617F1-E		1,891	-		-										2	1	-	1 + 1C	1	-	1
	Pratt Whitney Canada	PW625F	Technology demonstrator	2,500	-		-										2	1	-	1 + 1C	1	-	1
	Pratt Whitney Canada	PW645	Citation CJ3 (candidate engine)		-		-										2	1	4	6	1	-	3
	Pratt Whitney Canada	PW800 (AFTI)	Technology demonstrator	12,500	-		-				7.8						2	1G	-	4 + 1C	2	-	3
	Pratt Whitney Canada	PW800??	Il-214, RRJ, Citation Hemisphere (candidate engine)		-		-										2	1G	-	4 + 1C	2	-	3
	Pratt Whitney Canada	PW810	Citation Columbus (not produced)	8,830	-		-										2	1G	-	4 + 1C	2	-	3
	Pratt Whitney Canada	PW812D	Falcon 6X	13,460	-		-										2	1G	-	4 + 1C	2	-	3
	Pratt Whitney Canada	PW814GA	G500	15,429	-		-										2	1G	2	8	2	-	5		105.71	49.39	3135.7
	Pratt Whitney Canada	PW815GA	G600	16,011	-		-										2	1G	2	8	2	-	5		105.71	49.39	3135.7
	Progress	AI-22	Tu-324		-		-
	Progress	D-36-1	An-74	14,330	-	0.36	-	562	18.7		6.3	3,527	0.65	0.75	26,250		3	1	6	7	1	1	3		136.6	54.1	2,445
	Progress	D-36-1A	An-74		-		-				6.3						3	1	6	7	1	1	3		136.6	54.1	2,445
	Progress	D-36-2A	An-74, An-74D-200		-		-				6.3						3	1	6	7	1	1	3		136.6	54.1	2,445
	Progress	D-36-3A	An-74-200, An-74T-100/-200A, An-74TK-100/200, An-74D-200, An-74VIP		-		-				6.3						3	1	6	7	1	1	3		136.6	54.1	2,445
	Progress	D-36-4A	AN-74T-300, An-74TK-300	14,330	-		-				6.3						3	1	6	7	1	1	3		136.6	54.1	2,445
	Progress	D-36-5A	An-148 (proposed engine)		-		-				6.3						3	1	6	7	1	1	3		136.6	54.1	2,445
	Progress	D-436-148	An-148	15,000	-		-										3	1	6	7	1	1	3
	Progress	D-436K	(see military turbofan specifications)
	Progress	D-436T1	Tu-334-100 (prototype)	16,865	-		-		25.2		4.95						3	1 + 1	6	7	1	1	3	54.1			3,197
	Progress	D-436T1-134	Tu-134M (proposed)		-		-										3	1	6	7	1	1	3	54.1
	Progress	D-436T2	Tu-334-100D, Tu-354 (not produced)	18,078	-		-	584	26.2		4.9						3	1 + 1	6	7	1	1	3	54.1			3,197
	Progress	D-436TM	Yak-42-200 (proposed)	16,865	-		-		25.2		4.95						3	1 + 1	6	7	1	1	3				3,197
	Progress	D-436TP	Be-200	16,500	-		-
	Progress	D-436??	Il-214, RRJ (candidate engine)		-		-										3	1	6	7	1	1	3
	Rolls-Royce	Avon RA.1	Prototype	6,000	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.7 Mk.117	Comet 2R	7,350	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.16	(cancelled)	9,000	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.9 Mk.502	Comet 2X	10,000	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.26 Mk.502	Comet 3	10,000	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.25 Mk.503	Comet 2	6,500	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.25 Mk.504	Comet 2E	6,500	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.25 Mk.505			-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.26 Mk.521	Caravelle prototype	10,000	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.26 Mk.522	Comet 4	10,000	-		-			-	-						1	-	-	16	3	-	-	-	126	47.5	3,328
	Rolls-Royce	Avon RA.29 Mk.522	Caravelle I	10,500	-		-			-	-						1	-	-	16	3	-	-	-	126	47.5	3,328
	Rolls-Royce	Avon RA.29/1 Mk.522	Caravelle I	10,000	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.29 Mk.523	Comet 3	10,500	-		-			-	-						1	-	-	16	3	-	-	-	126	47.5
	Rolls-Royce	Avon RA.26 Mk.524			-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.29 Mk.524			-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.29/1 Mk.524	Comet 2E/4	10,250	-	0.786	-	170	8.8	-	-						1	-	-	16	3	-	-	-	126	47.5
	Rolls-Royce	Avon RA.29/1 Mk.524B		10,250	-		-			-	-						1	-	-	16	3	-	-	-	126	47.5	3,343
	Rolls-Royce	Avon RA.29 Mk.525	Comet 4B/4C	10,250	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.29/1 Mk.525	Comet 4B/4C	10,250	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.29/1 Mk.525B	Comet 4B/4C	10,250	-		-			-	-						1	-	-	16	3	-	-	-	126	47.5	3,383
	Rolls-Royce	Avon RA.29/1 Mk.526	Caravelle 1A	10,500	-	0.786	-	170	8.8	-	-						1	-	-	16	3	-	-	-	126	47.5	3,328
	Rolls-Royce	Avon RA.29 Mk.527	Caravelle III	11,400	-		-			-	-						1	-	-	16	3	-	-	-	126	47.5	3,347
	Rolls-Royce	Avon RA.29/3 Mk.527	Caravelle III	11,400	-		-			-	-						1	-	-	16	3	-	-	-	126	47.5	3,347
	Rolls-Royce	Avon RA.29/3 Mk.527B	Caravelle III	11,400	-	0.853	-			-	-						1	-	-	16	3	-	-	-	126	47.5	3,328
	Rolls-Royce	Avon RA.29/5	(cancelled)	13,300	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.29/6 Mk.530		12,200	-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.29/6 Mk.531	Caravelle VIN	12,200	-		-			-	-						1	-	-	17	3	-	-	-	134	47.5	3,488
	Rolls-Royce	Avon RA.29/6 Mk.531B	Caravelle VIN	12,200	-	0.802	-			-	-						1	-	-	17	3	-	-	-	134	47.5	3,488
	Rolls-Royce	Avon RA.29/6 Mk.532R	Caravelle VIR	12,600	-		-			-	-						1			17	3	-	-	-	134	47.5	3,488
	Rolls-Royce	Avon RA.29/6 Mk.532R-B		12,080	-		-			-	-						1	-	-	17	3	-	-	-	134	47.5	3,478
	Rolls-Royce	Avon RA.29/6 Mk.533R	Caravelle VIR	12,600	-	0.785	-			-	-						1			17	3	-	-	-	134	47.5	3,488
	Rolls-Royce	Avon RA.29/6 Mk.533R-11A		13,000	-		-			-	-						1	-	-	17	3	-	-	-	134	47.5	3,478
	Rolls-Royce	Avon RA.29/6 Mk.535R	Caravelle VIR	12,600	-	0.785	-	185	10.3	-	-						1	-	-	17	3	-	-	-	134	47.5
	Rolls-Royce	Avon RA.30			-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Avon RA.50			-		-			-	-						1	-	-	??	3	-	-	-
	Rolls-Royce	Conway RCo.1			-		-										2	-	4	8	1	-	1
	Rolls-Royce	Conway RCo.2		10,000	-		-										2	-	4	8	1	-	1
	Rolls-Royce	Conway RCo.3			-		-										2	-	4	8	1	-	1
	Rolls-Royce	Conway RCo.5		13,000	-		-										2	-	6	9	1	-	2
	Rolls-Royce	Conway RCo.7	Development engine	15,000	-		-										2	-	4	8	1	-	1
	Rolls-Royce	Conway RCo.8		14,500	-		-										2	-	6	9	1	-	2
	Rolls-Royce	Conway RCo.10 Mk.505	707-420/F	16,500	-		-										2	-	6	9	1	-	2		134.2		4,690
	Rolls-Royce	Conway RCo.10 Mk.507	(cancelled)		-		-										2	-	6	9	1	-	2		134.2		4690
	Rolls-Royce	Conway RCo.12 Mk.507	DC-8-41/42/43/43F	17,500	-		-										2	-	6	9	1	-	2		134.2		4,690
	Rolls-Royce	Conway RCo.12 Mk.508	707-420/F	17,500	-	0.726	-	280	14.1		0.3	4,625	0.822	0.83	36,000		2	-	7	9	1	-	2		134.2		4,690
	Rolls-Royce	Conway RCo.12 Mk.508A	707-420/F	18,000	-		-				0.3	4,625	0.822	0.83	36,000		2	-	7	9	1	-	2		134.2		4,690
	Rolls-Royce	Conway RCo.12 Mk.509	DC-8-41/42/43/43F	17,500	-		-	280	14.1		0.3	4,625	0.822	0.83	36,000		2	-	7	9	1	-	2		134.2		4,690
	Rolls-Royce	Conway RCo.12 Mk.509A	DC-8-41/42/43/43F	18,000	-	0.735	-	285	14		0.3	4,625	0.822	0.83	36,000		2	-	7	9	1	-	2		134.2		4,690
	Rolls-Royce	Conway RCo.14			-		-
	Rolls-Royce	Conway RCo.15 Mk.511			-		-										2	-	6	9	1	-	2		134.2		4690
	Rolls-Royce	Conway RCo.15 Mk.512			-		-										2	-	6	9	1	-	2		134.2		4690
	Rolls-Royce	Conway RCo.15B Mk.5??	DC-8-43	18,500	-		-
	Rolls-Royce	Conway RCo.42/1 Mk.540	VC.10 Type 1101/1102/1103/1109	20,370	-	0.656	-	367	14.8		0.6	5,250	0.84	0.83	36,000		2	-	4 + 3B	9	1	-	2		154	50	5,001
	Rolls-Royce	Conway RCo.42/3 Mk.540	VC.10 Type 1101/1102/1103/1109	20,370	-	0.656	-	367	14.8		0.6	5,250	0.84	0.83	36,000		2	-	4 + 3B	9	1	-	2		154	50	5,001
	Rolls-Royce	Conway RCo.43D Mk.550B	Super VC.10 Type 1151/1154	21,800	-	0.59	-	375	15.8		0.6	5,345	0.819	0.83	36,000		2	-	4 + 3B	9	1	-	2		154	50	5,101
	Rolls-Royce	Derwent 5/17	C-102 Jetliner	3,600	-		-			-	-						1	-	-			-	-	-
	Rolls-Royce	Medway RB.141-3	Trident (candidate engine)		-		-			-	-		2	-	6	11	2	-	2	-	165	42	3,500
	Rolls-Royce	Medway RB.174		17,300	-	0.6	-		16.75	-	-		2	-	6	11	2	-	2	-	165	42	3,500
	Rolls-Royce	Nene RB.41-1	F26 (not produced)	4,600	-	1.049	-	90	4	-	-						1	-	-	1C	1	-	-	-
	Rolls-Royce	Pearl 10X	Falcon 10X	18,000													2			10	2	-	4
	Rolls-Royce	Pearl 15	Global 5500/6500	15,125					43		4.8						2			10	2	-	3	48.5
	Rolls-Royce	Pearl 700	G700	18,250													2			10	2	-	4	51.8
	Rolls-Royce	RB.141-3	HFB 314 (not produced)		-		-
	Rolls-Royce	RB.151		30,000
	Rolls-Royce	RB.158		34,000
	Rolls-Royce	RB.159		16,000
	Rolls-Royce	RB.160		34,000
	Rolls-Royce	RB.162-86	Trident 3B (booster)	5,250	-	1.12	-	86	4.3	-	-						1	-	-	6	1	-	-	-	97.7**		520
	Rolls-Royce	RB.167		20,000
	Rolls-Royce	RB.170		24,000
	Rolls-Royce	RB.171		20,000
	Rolls-Royce	RB.178	HS.132, HS.134, Br.124, SC.5/45 (not produced)	28,500	-		-
	Rolls-Royce	RB.178-14	VC-10 DB265 (not produced)	27,500	-		-				4
	Rolls-Royce	RB.178-51	747-100 (proposed)		-		-				8
	Rolls-Royce	RB.202	Do 231C (lift engines, not produced)	13,100	-		-
	Rolls-Royce	RB.207-3	A300, L1011-1-1 (not produced)	47,500	-	0.54	-	1660	27	2	5						3	1	7	6	1	1	3
	Rolls-Royce	RB.211-22-02	L1011-1	40,600	-		-	1325	27	1.42	4.8						3	1	7	6	1	1	3		128.7		7,189
	Rolls-Royce	RB.211-22B		42,670	-		-										3	1	7	6	1	1	3	84.8	119.4**		9,195
	Rolls-Royce	RB.211-22B-02	L1011-1/1F/50/100/150, L1011-400 (not produced)	41,030	-	0.373	-	1380	24.5	1.42	4.8	9,495	0.628	0.85	35,000		3	1	7	6	1	1	3	84.8	119.4**		10,326
	Rolls-Royce	RB.211-22C-02	L1011-1/50/100/150 (option)	42,000	-		-										3	1	7	6	1	1	3
	Rolls-Royce	RB.211-22CA-02	L1011-1/50/100/150 (option)		-		-										3	1	7	6	1	1	3
	Rolls-Royce	RB.211-23	L1011-1/50/100/150 (option)	38,380	-		-										3	1	7	6	1	1	3
	Rolls-Royce	RB.211-24	(see RB.211-524)		-		-										3	1	7	6	1	1	4
	Rolls-Royce	RB.211-40	BAC 311 (not produced)	43,040	-		-										3	1	7	6	1	1	3
	Rolls-Royce	RB.211-52	A300B (candidate engine)		-		-										3	1	7	6	1	1	4
	Rolls-Royce	RB.211-56	L1011-3, L1011-8.4 (not produced)	52,200	-		-	1370	26	1.59	5.04						3	1	7	6	1	1	4
	Rolls-Royce	RB.211-61	BAC 311 (not produced)	50,000	-		-										3	1	7	6	1	1	3
	Rolls-Royce	RB.211-524	L1011-100/-200, 747-SP (option), L-1011-2/-300 (not produced)	48,000	-		-										3	1	7	6	1	1	3
	Rolls-Royce	RB.211-524B-02	747-SP, L1011-200/-200F/-500/-500F, 747-100 (option), L-1011-600 (not produced)	49,120	-		-	1513	28.4		4.5						3	1	7	6	1	1	3	84.8	119.4**		10,154
	Rolls-Royce	RB.211-524B-B-02		49,120	-		-										3	1	7	6	1	1	3	84.8	119.4**		10,154
	Rolls-Royce	RB.211-524B-D-02	L1011-200/-200F/-500, 747-100 (option)	49,120	-		-	1513	28.4		4.5						3	1	7	6	1	1	3	84.8	119.4**		9,814
	Rolls-Royce	RB.211-524B2-02	L1011-200/-200F/-500, 747-SP/-100 (option)	49,120	-		-	1513	28.4		4.5						3	1	7	6	1	1	3	84.8	119.4**		9,814
	Rolls-Royce	RB.211-524B2-19		49,120	-		-										3	1	7	6	1	1	3				11,154
	Rolls-Royce	RB.211-524B2-B-19		49,120	-		-										3	1	7	6	1	1	3				11,154
	Rolls-Royce	RB.211-524B3-02		49,120	-		-										3	1	7	6	1	1	3				11,000
	Rolls-Royce	RB.211-524B4-02	L1011-200/-200F/-250/-500	49,120	-		-	1500	29		4.4	11,000	0.606	0.85	35,000		3	1	7	6	1	1	3	85.8	122.3**		11,148
	Rolls-Royce	RB.211-524B4-D-02	L1011-200/-500	49,120	-		-	1512	28.6		4.4						3	1	7	6	1	1	3	85.8	122.3**		11,148
	Rolls-Royce	RB.211-524C	747-SP/-100B/-200B/-300	51,500	-		-	1532	28.6		4.5	11,490	0.642	0.85	35,000		3	1	7	6	1	1	3	84.8	119.4**		9,859
	Rolls-Royce	RB.211-524C2	747-SP/-100B/-200B/-300	51,500	-		-	1532	28.6		4.5	11,490	0.642	0.85	35,000		3	1	7	6	1	1	3	84.8	119.4**		9,859
	Rolls-Royce	RB.211-524C2-19		50,600	-		-										3	1	7	6	1	1	3	84.8	119.4**		11,199
	Rolls-Royce	RB.211-524C2-B-19		50,600	-		-										3	1	7	6	1	1	3	84.8	119.4**		11,199
	Rolls-Royce	RB.211-524C4	747-200B, 747-100B/-300 (option)		-		-				4.5						3	1	7	6	1	1	3	84.8	119.4**		9,859
	Rolls-Royce	RB.211-524D4	747-SP/-200B/-200B(M)/-200B(SF)/-200F/-300, L1011-500H&H (not produced)	53,000	-		-	1548	29.3		4.4	11,230	0.617	0.85	35,000		3	1	7	6	1	1	3	85.8	122.3**		9,874
	Rolls-Royce	RB.211-524D4-19		51,980	-		-										3	1	7	6	1	1	3	85.8	122.3**		11,195
	Rolls-Royce	RB.211-524D4-B-19		51,980	-		-										3	1	7	6	1	1	3	85.8	122.3**		11,195
	Rolls-Royce	RB.211-524D4-39		51,980	-		-										3	1	7	6	1	1	3	85.8	122.3**		11,195
	Rolls-Royce	RB.211-524D4-B-39		51,980	-		-										3	1	7	6	1	1	3	85.8	122.3**		11,195
	Rolls-Royce	RB.211-524D4B	747-200/-200F/-300 (option)	52,810	-		-	1548	29.6		4.4	11,230	0.601	0.85	35,000		3	1	7	6	1	1	3	85.8	122.3**		11,195
	Rolls-Royce	RB.211-524D4X-19		52,810	-		-										3	1	7	6	1	1	3	85.8	122.3**		11,195
	Rolls-Royce	RB.211-524D4X-B-19		52,810	-		-										3	1	7	6	1	1	3	85.8	122.3**		11,195
	Rolls-Royce	RB.211-524G	747-400/-400F, 767-300ER (option)	58,000	-		-	1604	32.9		4.3	11,813	0.57	0.85	35,000		3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524G2	747-400/-400F (option)		-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524G3	767-300ER/-300FER (option)		-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524G-T	747-400/-400F, 767-300ER (option)	58,000	-		-	1604	32.9		4.3	11,813	0.57	0.85	35,000		3	1	7	6	1	1	3	86.3	125.0**		9,470
	Rolls-Royce	RB.211-524G-19		56,870	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,470
	Rolls-Royce	RB.211-524G2-T	747-400ER (option)	56,870	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,470
	Rolls-Royce	RB.211-524G-T-19		56,870	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,470
	Rolls-Royce	RB.211-524G3-19		56,870	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,470
	Rolls-Royce	RB.211-524G3-T		56,870	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,470
	Rolls-Royce	RB.211-524G3-T-19		56,870	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,470
	Rolls-Royce	RB.211-524G4-T	767-300ER/-300FER (option)	56,400	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524G/H			-		-				4.3	11,813	0.57	0.85	35,000		3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524G/H-T			-		-				4.3	11,813	0.57	0.85	35,000		3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524H	747-400, 767-300ER, 767-300F/-300FER/-400F (option)	59,450	-		-	1604	34.5		4.1	11,813	0.57	0.85	35,000		3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524H-T	747-400/-400F, 767-300ER, An-124-210 (option)	59,450	-		-	1604	34.5		4.1	11,813	0.57	0.85	35,000		3	1	7	6	1	1	3	86.3	125.0**		9,470
	Rolls-Royce	RB.211-524H-T-36		59,450	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524H2	747-400/-400F	59,450	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524H2-19		59,450	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524H2-T	747-400ER (option)	59,450	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,470
	Rolls-Royce	RB.211-524H2-T19		59,450	-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524H3	767-300ER, 767-300FER (option)		-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-524H4	An-218-200/-300 (proposed)		-		-				4.1						3	1	7	6	1	1	3	86.3	125.0**		9,671
	Rolls-Royce	RB.211-535C-37	757-200/-200(SF)/-200F	36,720	-		-	1142	21.1		4.4	8,453	0.646	0.8	35,000		3	1	6	6	1	1	3	73.2	118.5		7,680
	Rolls-Royce	RB.211-535E4-37	757-200/-200ER/-200ET/-200F, Tu-204-120/-120C/-220/-220C/-222, Tu-224	39,610	-	0.324	-	1151	25.8		4.3	8,700	0.598	0.8	35,000		3	1	6	6	1	1	3	74.1	117.9		7,603
	Rolls-Royce	RB.211-535E4B-37	757-200/-200ET/-300, 757-200ER/-200F (option), Tu-214, Tu-330 (Tu-204-330) (proposed)	42,540	-		-	1151	25.8		4.3						3	1	6	6	1	1	3	74.1	117.9		7,603
	Rolls-Royce	RB.211-535E4B-75	Tu-204-120/-120C/-220/-220C	42,540	-		-				4.3						3	1	6	6	1	1	3	74.1	117.9		7,603
	Rolls-Royce	RB.211-535E4C-37	757-300	42,540	-		-				4.3						3	1	6	6	1	1	3	74.1	117.9		7,603
	Rolls-Royce	RB.220	Do 231C (not produced)	24,000	-		-
	Rolls-Royce	RB.282	Falcon 5X (candidate engine)	10,000	-		-
	Rolls-Royce	RB.432	F29 (not produced)	18,000	-		-				4.8						2	1	-	8	1	-	3
	Rolls-Royce	Spey RSp.1 Mk.505-5	Trident 1/1C	12,550	-		-	203		2.7	0.71	3,070	0.763	0.77	32,000		2	4	-	12	2	-	2		110.0**	37	2,200
	Rolls-Royce	Spey RSp.?? Mk.505-14		10,000	-		-										2	4	-	12	2	-	2		110.0**	37
	Rolls-Royce	Spey RSp.3 Mk.506-2		10,410	-		-			2.7	0.71	3,070	0.764	0.77	32,000		2	4	-	12	2	-	2		110.0**	37
	Rolls-Royce	Spey RSp.3 Mk.506-14	BAC 111-200, Model 2086 (not produced)	10,410	-		-			2.7	0.71	3,070	0.764	0.77	32,000		2	4	-	12	2	-	2		110.0**	37	2,257
	Rolls-Royce	Spey RSp.3 Mk.506-14A	BAC 111-200	10,410	-		-			2.7	0.71	3,070	0.764	0.77	32,000		2	4	-	12	2	-	2		110.0**	37	2,257
	Rolls-Royce	Spey RSp.3 Mk.506-14AW	BAC 111-200	10,410	10,410					2.7	0.71	3,070	0.764	0.77	32,000		2	4	-	12	2	-	2		110.0**	37	2,288
	Rolls-Royce	Spey RSp.3 Mk.506-14D	BAC 111-200	10,410	-		-			2.7	0.71	3,070	0.764	0.77	32,000		2	4	-	12	2	-	2		110.0**	37	2,257
	Rolls-Royce	Spey RSp.4 Mk.510-14	BAC 111-300	11,000	-	0.6	-	206	18.4	2.7	0.71	3,070	0.77	0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,332
	Rolls-Royce	Spey RSp.4 Mk.510-14W	BAC 111-400	11,000	-	0.6	-	206	18.4	2.7	0.71	3,070	0.77	0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,621
	Rolls-Royce	Spey RSp.4 Mk.511-5	Trident 1E/2	11,400	-	0.6	-	206	18.4	2.7	0.71	3,070	0.77	0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,312
	Rolls-Royce	Spey RSp.4 Mk.511-5W	Trident 1E/2	11,400	-	0.6	-	206	18.4	2.7	0.71	3,070	0.77	0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,317
	Rolls-Royce	Spey RSp.4 Mk.511-8	Gulfstream II/II-B/III	11,400	-	0.6	-	197	18.4	2.7	0.64	3,070	0.77	0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,483
	Rolls-Royce	Spey RSp.4 Mk.511-14	BAC 111-300	11,400	-	0.6	-	206	18.4	2.7	0.71	3,070	0.77	0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,483
	Rolls-Royce	Spey RSp.4 Mk.511-14W	BAC 111-400, Liner 40 (not produced)	11,400	-	0.6	-	206	18.4	2.7	0.71	3,070	0.77	0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,621
	Rolls-Royce	Spey RSp.4 Mk.512-5W	Trident 2E/3B	11,930	-	0.6	-	206	20.7	2.6	0.71	3,070		0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,609
	Rolls-Royce	Spey RSp.4 Mk.512-14	BAC 111-475/-500/-510ED, ROMBAC 111-560	12,550	-	0.6	-	206	20.7	2.6	0.71	3,070		0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,609
	Rolls-Royce	Spey RSp.4 Mk.512-14DW	BAC 111-475/-500/-510ED, ROMBAC 111-560	12,550	-	0.6	-	206	20.7	2.6	0.71	3,070		0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,609
	Rolls-Royce	Spey RSp.4 Mk.512-14DWE		12,550	-		-			2.6	0.71	3,070		0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,609
	Rolls-Royce	Spey RSp.4 Mk.512-25	BAC 111-475/-500/-510ED, ROMBAC 111-560	12,550	-	0.6	-	206	20.7	2.6	0.71	3,070		0.77	32,000		2	5	-	12	2	-	2	32.5	109.6	37.1	2,609
	Rolls-Royce	Spey Jr. Mk.555-15	F28 Mk.1000/1000C/2000/3000R/3000RC	9,850	-	0.75	-	199	15.4	2.46	1						2	4	-	12	2	-	2	32.5	97		2,257
	Rolls-Royce	Spey Jr. Mk.555-15H	F28 Mk.3000/4000/6000, F28 Mk.5000/Mk.6600 (not produced)	9,900	-	0.75	-	199	15.4	2.46	1						2	4	-	12	2	-	2	32.5	97		2,257
	Rolls-Royce	Spey Jr. Mk.555-15N	F28 Mk.1000/1000C/2000/3000R/3000RC	9,850	-	0.75	-	199	15.4	2.46	1						2	4	-	12	2	-	2	32.5	97		2,257
	Rolls-Royce	Spey Jr. Mk.555-15P	F28 Mk.1000/1000C/3000	9,900	-	0.75	-	199	15.4	2.46	1						2	4	-	12	2	-	2	32.5	97		2,257
	Rolls-Royce	Tay Mk.610-8	Gulfstream IV	12,420	-												2	1	3B	12	2	-	3	44.8	94.7	70.72	3,255
	Rolls-Royce	Tay Mk.611-8	Gulfstream IV/IV-SP	13,850	-	0.43	-	410	15.8		3.04		0.71	0.8	43,000		2	1	3B	12	2	-	3	44.8	94.7	70.72	3,255
	Rolls-Royce	Tay Mk.611-8B		13,850	-	0.43	-	410	15.8		3.04		0.71	0.8	43,000		2	1	3B	12	2	-	3	44.8	94.7	70.72	3,306
	Rolls-Royce	Tay Mk.611-8C	G350, G450	13,850	-	0.43	-	410	15.8		3.04		0.71	0.8	43,000		2	1	3B	12	2	-	3	44.8	94.7	70.72	3,306
	Rolls-Royce	Tay Mk.620-15	Fokker 70/100	13,850	-	0.43	-	410	15.8		3.04		0.69	0.73	30,000		2	1	3B	12	2	-	3	44.8	94.7	70.72	3,310
	Rolls-Royce	Tay Mk.650-14	BAC 111-475/-500/-560	15,100	-		-	418	16.2		3.06		0.69	0.73	30,000		2	1	3B	12	2	-	3	44.8	94.7	70.72	3,516
	Rolls-Royce	Tay Mk.650-15	Fokker 100	15,100	-		-	418	16.2		3.06		0.69	0.73	30,000		2	1	3B	12	2	-	3	44.8	94.7	70.72	3,516
	Rolls-Royce	Tay Mk.651-54	727-100(QF)/-100C(QF)	15,400	-	0.45	-	426	16.6		3.07		0.69	0.78	35,000		2	1	3B	12	2	-	3	44.8	94.7	70.72	3,590
	Rolls-Royce	Tay Mk.670	727-200RE, DC-9RE, 737-100RE/-200RE, MD-95 (proposed for re-engining)	18,000	-		-	511	19		3.2						2	1	3B	12	2	-	3	50	112		3,750
	Rolls-Royce	Trent RB.203	FH-228 (not produced)	9,730	-		-										3	1	4	5	1	1	2		82.2	38.7	1,751
	Rolls-Royce	Trent 553-61	A340-541, A340-641 (option)	55,780	-		-	1847	35.1		7.7						3	1	8	6	1	1	5	97.4	154		10,930
	Rolls-Royce	Trent 553A2-61	A340-541, A340-641 (option)	55,780	-		-	1847	35.1		7.7						3	1	8	6	1	1	5	97.4	154		10,930
	Rolls-Royce	Trent 556-61	A340-642	58,462	-		-	1892	36.7		7.6						3	1	8	6	1	1	5	97.4	154		10,930
	Rolls-Royce	Trent 556A2-61	A340-542/-642	58,462	-		-	1892	36.7		7.6						3	1	8	6	1	1	5	97.4	154		10,930
	Rolls-Royce	Trent 556B-61		58,462	-		-										3	1	8	6	1	1	5	97.4	154		10,930
	Rolls-Royce	Trent 556B2-61		58,462	-		-										3	1	8	6	1	1	5	97.4	154		10,930
	Rolls-Royce	Trent 560A2-61	A340-643	61,902	-		-										3	1	8	6	1	1	5	97.4	154		10,930
	Rolls-Royce	Trent 560-61		61,902	-		-										3	1	8	6	1	1	5	97.4	154		10,930
	Rolls-Royce	Trent 600	MD-11 (option)	68,000	-		-	2032			4.3						3	1	8	6	1	1	4	97.4	154	102	10,400
	Rolls-Royce	Trent 672	767-400ERX	72,000	-		-		43.2								3	1	8	6	1	1	4	97.4	154	102	11,400
	Rolls-Royce	Trent 6??	747-XQLR (candidate engine), 747-500X/-600X (not produced)		-		-										3	1	8	6	1	1	4	97.4	154	102	11,400
	Rolls-Royce	Trent 758	A330-141	58,000	-		-										3	1	8	6	1	1	4	97.4	154
	Rolls-Royce	Trent 764	MD-12 (not produced)	64,000	-		-										3	1	8	6	1	1	4	97.4	154
	Rolls-Royce	Trent 768-60	A330-341, A330-241 (option)	67,500	-		-	1932	35.2		5.17						3	1	8	6	1	1	4	97.4	154		11,023
	Rolls-Royce	Trent 772-60	A330-342	71,100	-		-	1978	36.8		5.05	11,500	0.565	0.82	35,000		3	1	8	6	1	1	4	97.4	154		11,023
	Rolls-Royce	Trent 772B-60	A330-243/-243F/-343	71,100	-		-	1978	36.8		5.05						3	1	8	6	1	1	4	97.4	154		11,023
	Rolls-Royce	Trent 775-60	A330-244, A330-344 (option)	75,150	-		-	2024	39		4.77						3	1	8	6	1	1	4	97.4	154
	Rolls-Royce	Trent 871-17	777-200	71,000	-		-										3	1	8	6	1	1	5	110	178		13,400
	Rolls-Royce	Trent 875-17	777-200	76,850	-		-	2482	35.9		6.21						3	1	8	6	1	1	5	110	178		13,400
	Rolls-Royce	Trent 877-17	777-200	78,910	-		-	2578	37		6.15						3	1	8	6	1	1	5	110	178		13,400
	Rolls-Royce	Trent 882-17	777-200 (option)	84,700	-		-		38.8								3	1	8	6	1	1	5	110	178		13,400
	Rolls-Royce	Trent 884-17	777-200	85,430	-		-	2661	39.8		5.95						3	1	8	6	1	1	5	110	178		13,400
	Rolls-Royce	Trent 884B-17		85,430	-		-										3	1	8	6	1	1	5	110	178		13,400
	Rolls-Royce	Trent 890-17	777-200/-300, Tu-304 (proposed)	91,300	-		-	2720	42.7		5.74	13,000	0.557	0.83	35,000		3	1	8	6	1	1	5	110	178		13,400
	Rolls-Royce	Trent 892-17	777-200/-300	91,450	-		-	2645	40.8		5.79						3	1	8	6	1	1	5	110	178		13,400
	Rolls-Royce	Trent 892B-17	777-200	91,450	-		-										3	1	8	6	1	1	5	110	178		13,400
	Rolls-Royce	Trent 895-17	777-200, 777-300/-300ER (option)	92,940	-		-	2664	41.6	1.81	5.79						3	1	8	6	1	1	5	110	178		13,400
	Rolls-Royce	Trent 895C-17	777-200, 777-300/-300ER (option)	95,000	-		-	2664	41.6	1.81	5.79						3	1	8	6	1	1	5	110	178		13,400
	Rolls-Royce	Trent 8104	Technology demonstrator	104,000	-		-		45								3	1	8	6	1	1	5	110	178		14,400
	Rolls-Royce	Trent 970-84	A380-841	75,152	-		-										3	1	8	6	1	1	5	110	208.8**	155.2	13,842
	Rolls-Royce	Trent 970B-84	A380-841	78,304	-		-										3	1	8	6	1	1	5	110	208.8**	155.2	13,842
	Rolls-Royce	Trent 972-84	A380-842	76,752	-		-										3	1	8	6	1	1	5	110	208.8**	155.2	13,842
	Rolls-Royce	Trent 972B-84	A380-842	80,213	-		-										3	1	8	6	1	1	5	110	208.8**	155.2	13,842
	Rolls-Royce	Trent 975	747-500X/-600X (not produced)	75,000	-		-	2481	35.8		7.8						3	1	8	6	1	1	5	110	208.8**	155.2	13,842
	Rolls-Royce	Trent 977-84	A380-843F (not produced)	80,781	-		-										3	1	8	6	1	1	5	110	208.8**	155.2	13,842
	Rolls-Royce	Trent 977B-84	A380-843F (not produced)	83,835	-		-										3	1	8	6	1	1	5	110	208.8**	155.2	13,842
	Rolls-Royce	Trent 980-84	A380-941 (not produced)	84,098	-		-										3	1	8	6	1	1	5	110	208.8**	155.2	13,842
	Rolls-Royce	Trent 1000-A	787-8	69,194	-		-										3	1	8	6	1	1	6	112	187.8**		13,300
	Rolls-Royce	Trent 1000-A2	787-8/-9	69,194	-		-										3	1	8	6	1	1	6	112	187.8**		13,111
	Rolls-Royce	Trent 1000-AE		69,194	-		-										3	1	8	6	1	1	6	112	187.8**		13,300
	Rolls-Royce	Trent 1000-AE2		69,194	-		-										3	1	8	6	1	1	6	112	187.8**		13,111
	Rolls-Royce	Trent 1000-AE3	787-8/-9	69,194	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-C	787-8	74,511	-		-										3	1	8	6	1	1	6	112	187.8**		13,300
	Rolls-Royce	Trent 1000-C2	787-8	74,511	-		-										3	1	8	6	1	1	6	112	187.8**		13,111
	Rolls-Royce	Trent 1000-CE		74,511	-		-										3	1	8	6	1	1	6	112	187.8**		13,300
	Rolls-Royce	Trent 1000-CE2		74,511	-		-										3	1	8	6	1	1	6	112	187.8**		13,111
	Rolls-Royce	Trent 1000-CE3	787-8	74,511	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-D	787-8	74,511	-		-										3	1	8	6	1	1	6	112	187.8**		13,300
	Rolls-Royce	Trent 1000-D2	787-8/-9	74,511	-		-										3	1	8	6	1	1	6	112	187.8**		13,111
	Rolls-Royce	Trent 1000-D3	787-8/-9	74,511	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-E	787-8	59,631	-		-										3	1	8	6	1	1	6	112	187.8**		13,300
	Rolls-Royce	Trent 1000-E2		59,631	-		-										3	1	8	6	1	1	6	112	187.8**		13,111
	Rolls-Royce	Trent 1000-G	787-8	72,066	-		-										3	1	8	6	1	1	6	112	187.8**		13,300
	Rolls-Royce	Trent 1000-G2	787-8	72,066	-		-										3	1	8	6	1	1	6	112	187.8**		13,300
	Rolls-Royce	Trent 1000-G3	787-8	72,066	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-H	787-8	63,897	-		-										3	1	8	6	1	1	6	112	187.8**		13,300
	Rolls-Royce	Trent 1000-H2	787-8	63,897	-		-										3	1	8	6	1	1	6	112	187.8**		13,111
	Rolls-Royce	Trent 1000-H3	787-8	63,897	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-J2	787-9	78,129	-		-										3	1	8	6	1	1	6	112	187.8**		13,111
	Rolls-Royce	Trent 1000-J3	787-9/-10	78,129	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-K2	787-9	78,129	-		-										3	1	8	6	1	1	6	112	187.8**		13,111
	Rolls-Royce	Trent 1000-K3	787-9	78,129	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-L2	787-8	74,511	-		-										3	1	8	6	1	1	6	112	187.8**		13,111
	Rolls-Royce	Trent 1000-L3		74,511	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-M3		79,728	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-N3		79,728	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-P3		74,511	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-Q3		78,129	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 1000-R3		81,028	-		-										3	1	8	6	1	1	6	112	187.8**		13,479
	Rolls-Royce	Trent 7000-72	A330-941	72,834	-		-		50		10						3	1	8	6	1	1	6	112	188.0**		14,209
	Rolls-Royce	Trent 7000-72C		72,834	-		-										3	1	8	6	1	1	6	112	188.0**		14,209
	Rolls-Royce	Trent XWB-75	A350-942, A350-8?? (not produced)	74,200	-		-										3	1	8	6	1	2	6	118	176.5		16,043
	Rolls-Royce	Trent XWB-79	A350-8?? (not produced)	78,900	-		-										3	1	8	6	1	2	6	118	176.5		16,043
	Rolls-Royce	Trent XWB-79B	A350-8?? (not produced)	78,900	-		-										3	1	8	6	1	2	6	118	176.5		16,043
	Rolls-Royce	Trent XWB-84	A350-941	84,200	-		-	3166									3	1	8	6	1	2	6	118	176.5		16,043
	Rolls-Royce	Trent XWB-97	A350-1041	97,000	-		-										3	1	8	6	1	2	6	118	176.5		16,643
	Armstrong Siddeley	Viper 11 Mk.22/1	MB.326D	2,500	-		-			-	-						1	-	-	7	1	-	-	-
	Rolls-Royce	Viper Mk.601-22	HS 125-600A/B	3,750	-	0.95	-	58	5.8	-	-						1	-	-	8	2	-	-	-			830
	BMW/Rolls-Royce	BR710A1-10	G550	14,750	-	0.39	-	435	25.7		4.2						2	1	-	10	2	-	2	48	87	52.9	3,520
	BMW/Rolls-Royce	BR710A2-20	Global Express, Global Express XRS, Global 5000/6000	14,750	-	0.39	-	435	25.7		4.2						2	1	-	10	2	-	2	48	87	52.9	3,520
	BMW/Rolls-Royce	BR710C4-11	G550	15,370	-	0.39	-	435	25.7		4.2						2	1	-	10	2	-	2	48	87	52.9	3,520
	BMW/Rolls-Royce	BR710D5-21		15,240	-		-										2	1	3B	10	2	-	4
	BMW/Rolls-Royce	BR710-48	Tu-334-120	16,000	-		-										2	1	-	10	2	-	2	48
	BMW/Rolls-Royce	BR710-??	ARJ 21		-		-										2	1	-	10	2	-	2
	BMW/Rolls-Royce	BR710-??	SL-200/-300 (not produced)		-		-										2	1	-	10	2	-	2
	BMW/Rolls-Royce	BR715A1-30	717-200	18,710	-	0.37	-	614	32.1		4.7						2	1	2B	10	2	-	3	56	93	60.2	4,597
	BMW/Rolls-Royce	BR715B1-30	717-200 (option)	20,160	-		-										2	1	2B	10	2	-	3	56
	BMW/Rolls-Royce	BR715C1-30	717-200 HGW	21,430	-		-	689	32.6		5						2	1	2B	10	2	-	3	56	93	60.2	4,597
	BMW/Rolls-Royce	BR715-55	Tu-354 (not produced)	20,000	-		-										2	1	2B	10	2	-	3	56
	BMW/Rolls-Royce	BR715-??	RRJ, N-2130-100/-200 (candidate engine), A316/A317 (A31X) (not produced)		-		-										2	1	2B	10	2	-	3	56
	BMW/Rolls-Royce	BR725A1-12	G650, G650ER	16,900	-		-										2	1	3B	10	2	-	4
	Rolls-Royce/JAEC	RJ500	(cancelled)	20,000	-		-										2	1		9	3	-	2		101		4116
	Rolls-Royce/Snecma	M45F	Technology demonstrator		-		-										2	1	5B	7	1	-	3
	Rolls-Royce/Snecma	M45H-C	Technology demonstrator	8,245	-		-										2	1	5B	7	1	-	3
	Rolls-Royce/Snecma	M45H-D Mk.501	VFW 614 (not produced)	7,260	-	0.451	-	233	18.8	1.6	2.85	2,745	0.725	0.65	20,000		2	1	5B	7	1	-	3	41.7	116.5	41.8	1,560
	Rolls-Royce/Snecma	M45H-E1	(cancelled)	9,250	-		-										2	1	6B	7	1	-	3
	Rolls-Royce/Snecma	M45H-E2	(cancelled)	9,600	-		-										2	2	6B	7	1	-	3
	Rolls-Royce/Snecma	Olympus 593	Technology demonstrator	20,000	30,610												2	-	7	7	1	-	1
	Rolls-Royce/Snecma	Olympus 593-22R	Concorde prototype	34,650	37,180												2	-	7	7	1	-	1
	Rolls-Royce/Snecma	Olympus 593 Mk.601	Concorde														2	-	7	7	1	-	1
	Rolls-Royce/Snecma	Olympus 593 Mk.610-14-28	Concorde	31,350	37,080	1.39		410	15.5				1.195				2	-	7	7	1	-	1		148.4	47.75	6,510
	PowerJet	SaM146-1S17	SSJ100/95, Il-214 (candidate engine)	15,400													2	1	3	6	1	-	3		141
	PowerJet	SaM146-1S18	SSJ100/95LR	16,100					28		4.4						2	1	3	6	1	-	3		141		4,980
	Shenyang Liming	WP-9	Y-10 (not produced)														2	2	6B	7	1	-	3
	Shenyang Liming	WS-8	Y-10 (not produced)														2	2	6B	7	1	-	3
	Shenyang Liming	WS-13A	ARJ21 (proposed)	22,500
	Shenyang Liming	WS-20	C919, C929 (proposed)	13,800
	Snecma/PWC	SPW14	(cancelled)	14,000	-		-										2	1G	-	4 + 1C	2	-	3
	Snecma	Silvercrest 2C	Citation Hemisphere	12,000					38.5		5.9						2	1	4	4 + 1C	1	-	4	42.5	74		2,290
	Snecma	Silvercrest 2D	Falcon 5X (not produced)	11,450													2	1	4	4 + 1C	1	-	4	42.5	74		2290
	Solovyev	D-20		11,905	-		-										2	3	-	8	1	-	2
	Solovyev	D-20P	Tu-124K/K2/V	11,905	-	0.62	-	249	13.6	2.6	1						2	3	-	8	1	-	2		130	38.3	3,236
	Solovyev	D-30-1	Tu-134/K/LK	14,990	-	0.6	-	280	18.6	2.65	1						2	4	-	10	2	-	2		156.8	41.3	3,417
	Solovyev	D-30-2	Tu-134A/AK/AN/B/B-1	14,990	-		-			2.65	1						2	4	-	10	2	-	2
	Solovyev	D-30-3	Tu-134A-3/B-3/BW	14,990	-	0.608	-	280	17.7	2.65	1						2	5	-	10	2	-	2		156.8	41.3	3,417
	Solovyev	D-30KP	Il-76T	26,460	-	0.481	-	640	18.4		2.42						2	3	-	11	2	-	4
	Solovyev	D-30KP-2	Il-76TD/MDP/LL	26,460	-		-				2.42						2	3	-	11	2	-	4
	Solovyev	D-30KPV	A-40	26,460	-		-										2	3	-	11	2	-	4
	Solovyev (Perm Aviadvigatel)	D-30KU	Il-62M	24,250	-	0.495	-	593	17.4		2.35						2	3	-	11	2	-	2		224	61.4	5,882
	Solovyev (Perm Aviadvigatel)	D-30KU-2	Il-62M	23,850	-		-	593			2.35						2	3	-	11	2	-	2
	Solovyev (Perm Aviadvigatel)	D-30KU-90		26,455	-		-				2.44						2	3	-	11	2	-	2		224.4	61.4	5,291
	Solovyev (Perm Aviadvigatel)	D-30KU-154-2	Tu-154M		-		-										2	3	-	11	2	-	2
	Solovyev (Perm Aviadvigatel)	D-30U-154	Tu-154M	14,990	-	0.6	-	280	18.6	2.65	1						2	4	-	10	2	-	2		156.8	41.3	3,417
	Solovyev	PS-7		17,000	-		-					3,417	0.62	0.8	36,000									47.6			2,976
	Solovyev	PS-9	Il-214-100, Il-214T (candidate engine)	22,000	-		-					4,630	0.59	0.8	36,000									56.5			3,858
	Solovyev	PS-12	MS-21-100/200/300, MS-21K, MS-12KP (candidate engine)	29,762	-			1193	40.2		8.39	5,665	0.549	0.8	36,000									73.6			5,400
	Solovyev	PS-12M		32,740	-		-					6,062	0.553	0.8	36,000									73.6			5,400
	Solovyev (Perm Aviadvigatel)	PS-90A	Il-96-300, Tu-204-100/-100C/-200/-200C, Tu-214, Tu-330, Tu-134D (proposed), Tu-154M2 (not produced)	35,250	-		-				4.8						2	1	2B	13	2	-	4
	Solovyev (Perm Aviadvigatel)	PS-90A-154	Tu-154M-2 (proposed)		-		-										2	1	2B	13	2	-	4
	Solovyev (Perm Aviadvigatel)	PS-90A2	Il-96-300, Il-76TF, Tu-204-500/600 (proposed)		-		-										2	1	2B	13	2	-	4
	Solovyev (Perm Aviadvigatel)	PS-90A10		20,283	-		-	582	23.1		3.76						2	1	-	12	2	-	2	55.1	168.5		4,180
	Solovyev (Perm Aviadvigatel)	PS-90A12	Yak-242	26,455	-		-	816	25.3		5.05						2	1	-	13	2	-	3	65.8	188.2		5,071
	Solovyev (Perm Aviadvigatel)	PS-90AN-76	Il-76TF	35,275	-		-	1036	35.5		4.6						2	1	2B	13	2	-	4	74.8	195.4		6,503
	Solovyev (Perm Aviadvigatel)	PS-90AP	Tu-234		-		-										2	1	-	??	??	-	??
	Solovyev (Perm Aviadvigatel)	PS-90A-??	Il-214, RRJ (candidate engine)		-		-										2	1	2B	13	2	-	4
	Soyuz	R123-300	(cancelled)	3,100	-		-				6						2	1	-	2 + 1C	1	-	1
	Soyuz	R126-300	Tu-324	8,818	-		-										2	1	-	5 + 1C	2	-	3
	Soyuz	R127-300	(cancelled)	1,985	-		-	68									2	1	-	2C	2	-	2
	Turbomeca	Aspin I	DH-11	440	-	0.54	-										1	1G	-	1C	2	-	-			23.8	279
	Turbomeca	Aspin II	A1 (not produced)	792	-	0.52	-	6.6	3.8								1	1G	-	1C	2	-	-			23.8	320
	Turbomeca	Astafan I	(cancelled)	1,365	-		-										1	1	-	2 + 1C	3	-	-
	Turbomeca	Astafan II	(cancelled)	1,570	1685	0.38	-		8.5		1						1	1	-	2 + 1C	3	-	-
	Turbomeca	Astafan IIA	(cancelled)	1,540	-	0.38	-		8.5		1						1	1	-	2 + 1C	3	-	-
	Turbomeca	Astafan IIB4	(cancelled)	1,700	-		-										1	1	-	2 + 1C	3	-	-
	Turbomeca	Astafan IIG	(cancelled)	1,543	-	0.38	-										1	1	-	2 + 1C	3	-	-
	Turbomeca	Astafan III	(cancelled)	1,760	-	1895	-										1	1	-	2 + 1C	3	-	-
	Turbomeca	Astafan IV	(cancelled)		-		-										1	1	-	2 + 1C	4	-	-
	Turbomeca	Astafan IVF6	(cancelled)	2,358	-		-										1	1	-	2 + 1C	4	-	-
	Turbomeca	Marbore IIA	Noratlas N-2502, YT-33	882						-	-						1	-	-	1C	1	-	-	-
	Turbomeca	Marbore VIC	MS.760C (not produced)	1,060	-	1.11	-	21	3.8	-	-						1	-	-	1C	1	-	-	-	55.8		370
	Turbomeca	Marbore VIF	CM.191 (not produced)	1,058	-	1.11	-	21	3.8	-	-						1	-	-	1C	1	-	-	-
	Turbomeca	Palas	Sparrowjet, SB.4	350	-	1.1	-	6.8	4	-	-					1123	1	-	-	1C	1	-	-	-	47	16.1	159
	Turbomeca/Snecma	Larzac 49-01	Falcon 10, Corvette	2,300	-	0.61	-	57	9	2	1.4						2	2	-	4	1	-	1
	Williams	EJ22-1	Eclipse 500 (prototype)	700	-		-										2								41	14.5	85
	Williams	FJ22-1	(see EJ22-1)
	Williams	FJ33-1	FJ-100, Leopard Six (not produced)	1,200	-		-										2	1	3B	1C	1	-	2
	Williams	FJ33-2		1,200	-		-										2	1	3B	1C	1	-	2
	Williams	FJ33-3	The-Jet (not produced)	1,200	-		-										2	1	3B	1C	1	-	2
	Williams	FJ33-4	S-26 Safire (candidate engine)	1,200	-		-										2	1	3B	1C	1	-	2
	Williams	FJ33-4-17M		1,200	-		-										2	1	3B	1C	1	-	2
	Williams	FJ33-4-18M		1,200	-		-										2	1	3B	1C	1	-	2
	Williams	FJ33-4-19J	Javelin MK-10 (not produced)	1,200	-		-										2	1	3B	1C	1	-	2
	Williams	FJ33-4A-11	A700 (not produced)	1,900	-		-										2	1	3B	1C	1	-	2
	Williams	FJ33-4A-15	D-JET (candidate)	1,568	-		-										2	1	3B	1C	1	-	2		47.8	32.7	293
	Williams	FJ33-4A-19	Vision SF50, D-JET, S-33, Sport Jet II (prototype)	1,900	-		-										2	1	3B	1C	1	-	2
	Williams	FJ33-5A	LAR01	1,846	-		-										2	1	3B	1C	1	-	2		42.7	25.1	319
	Williams	FJ33-??	MC-2400 Legend, A700	1,100	-		-										2	1	3B	1C	1	-	2
	Williams	FJ33-??	Citation Mustang, ProJet (candidate engine)	1,350	-		-										2	1	3B	1C	1	-	2
	Williams	FJ33-??	Eclipse 700 (not produced)	1,200	-		-										2	1	3B	1C	1	-	2
	Williams/Rolls-Royce	FJ44-1A	Citation CJ/CJ1, SigmaJet, MagnaJet (not produced)	1,900	-	0.456	-	63	12.8		3.28						2	1	1B	1C	1	-	2		53.4	29.6	460
	Williams/Rolls-Royce	FJ44-1AP	Citation CJ1+	1,965	-		-										2	1	1B	1C	1	-	2		57.9	31.1	468
	Williams/Rolls-Royce	FJ44-1AP-21	Citation M2	1,965	-		-										2	1	1B	1C	1	-	2				460
	Williams/Rolls-Royce	FJ44-1C	SK60	1,500	-	0.46	-	58	10.3		3.4						2	1	1B	1C	1	-	2				447
	Williams/Rolls-Royce	FJ44-2A	Premier I, SJ30-2, SJ30i, Citation Eagle II, NauticAir 450 (candidate engine)	2,300	-		-										2	1	3B	1C	1	-	2		59.8	29.6	530
	Williams/Rolls-Royce	FJ44-2C	Citation CJ2, Spirit Wing Learjet 25D	2,400	-		-										2	1	3B	1C	1	-	2		59.8	29.6	520
	Williams/Rolls-Royce	FJ44-3A	Citation CJ3/CJ3+	2,820	-		-										2	1	3B	1C	1	-	2		62.4	31.1	535
	Williams/Rolls-Royce	FJ44-3A-24	Citation CJ2+	2,490	-		-										2	1	3B	1C	1	-	2		62.4	31.1	535
	Williams/Rolls-Royce	FJ44-3AP		3,052	-		-										2	1	3B	1C	1	-	2		62.4	31.6	516
	Williams/Rolls-Royce	FJ44-3AP-25	Hawker 200, SJ30x, 400XT	2,490	-		-										2	1	3B	1C	1	-	2
	Williams/Rolls-Royce	FJ44-4A	Citation CJ4, PC-24	3,621	-		-										2	1	3B	1C	1	-	2		68.6	32.3	670
	Williams/Rolls-Royce	FJ44-4A-32	Hawker 400XPR	3,230	-		-										2	1	3B	1C	1	-	2		68.6	32.3	670
	Williams/Rolls-Royce	FJ44-4A-QPM		3,616	-		-										2	1	3B	1C	1	-	2		68.6	32.3	670
	Williams/Rolls-Royce	FJ44-4M		3,793	-		-										2	1	3B	1C	1	-	2		65.8	32.3	670
	Williams/Rolls-Royce	FJ44-4M-34		3,421	-		-										2	1	3B	1C	1	-	2		65.8	32.3	670
	Williams	FJX-1	V-Jet II	540	-		-										2
	Williams	FJX-2	V-Jet II	700	-		-										2								41	14.5	85
	B - Booster stage(s)
	C - Centrifugal compressor stage(s)
	R - Radial turbine stage(s)
	G - Geared (fan)
	** - denotes length given from intake flange to turbine exhaust flange
	grey - denotes optional engine selection or no nominal application for engine
	(cancelled) - denotes that the engine program or derivative was cancelled
	(not produced) - denotes the aircraft program or derivative was cancelled
	Notes:
	1. The technical information presented here is to the best of my knowledge.  Any comments, suggestions, questions or
	corrections will be greatly appreciated.
	2. While the designation system used by Boeing for their aircraft consists of a 2-digit customer configuration code, only the
	major series have been indicated here. (eg. 747-4F6 -> 747-400)
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