Military Turbofan/Turbojet Specifications
Civil Turbofan/Turbojet Specifications
Military Turboshaft/Turboprop Specifications
Civil Turboshaft/Turboprop Specifications

Home




Military Turboshaft/Turboprop Specifications
Military Turboshaft/Turboprop Specifications
(sorted by engine model)
1 2 3 4 5 6 7
Manufacturer Model Application(s) Power SFC Airflow OPR Number LPC HPC HPT IPT LPT Length Width/ Weight Notes Refs
(TO) (TO) (TO) Spools Stgs Stgs Stgs Stgs Stgs Diameter (dry) 1 2 3 4 5 6 7
[shp] [lb/shp hr] [lb/s] [in] [in] [lb]
Allison 250-B17C P68TP, A36, GZ22 420 0.657 4 7.2 1 + FT - 6 + 1C 2 - 2 45.0 22.5 195
Allison 250-B17D RTAF 5, L/M90TP 420 0.657 4 7.2 1 + FT - 6 + 1C 2 - 2
Allison 250-B17F L/M90TP 450 0.657 4 7.9 1 + FT - 4 + 1C 2 - 2 Notes
Allison 250-C18 TH-57A, MD500M 317 0.640 4 7.2 1 + FT - 6 + 1C 2 - 2
Allison 250-C18A OH-58A, MD500M 317 0.640 4 7.2 1 + FT - 6 + 1C 2 - 2
Allison 250-C18C OH-58A, MD500M 317 0.640 4 7.2 1 + FT - 6 + 1C 2 - 2
Allison 250-C20 BO105C/CB 400 0.650 4 7.2 1 + FT - 6 + 1C 2 - 2
Allison 250-C20B OH-58C, MD500MD, A109A, BO105CBS/CBS-4/CBS-5/M/P, Kania 420 0.650 4 7.2 1 + FT - 6 + 1C 2 - 2
MTU 250-MTU-C20B BO105M/P 420 0.650 4 7.2 1 + FT - 6 + 1C 2 - 2 40.7 23.2 158
Allison 250-C20F/2R AS355F2R 450 1 + FT - 6 + 1C 2 - 2 38.8 23.2 161
Allison 250-C20J TH-57B/C, TH-67A 420 0.650 4 7.2 1 + FT - 6 + 1C 2 - 2 38.8 23.2 161
Allison 250-C20R QH-50E 317 4 7.2 1 + FT - 6 + 1C 2 - 2
Allison 250-C20R/1 A109A Mk.2, A190 EOA, A109CM 450 0.608 7.9 1 + FT - 4 + 1C 2 - 2 38.8 23.2 173
Allison 250-C20W RQ-8A 420 0.650 4 7.2 1 + FT - 6 + 1C 2 - 2
Allison 250-C28C BO105LS/LS-A1/LS-A3 500 0.606 4 8.4 1 + FT - 1C 2 - 2 47.3 25.1 230
Allison 250-C30 AH-6J, MH-6J, MD530MG, FT600, S-76A 650 1 + FT - 1C 2 - 2
Allison 250-C30L Bell 406CS 650 0.592 6 8.6 1 + FT - 1C 2 - 2 43.2 25.5 258
Allison 250-C30R AH-58D, OH-58D 650 0.592 6 8.4 1 + FT - 1C 2 - 2 43.2 25.5 258
Allison 250-C30R/1 AH-58D, OH-58D 650 0.592 6 8.4 1 + FT - 1C 2 - 2 43.2 25.5 258
Allison 250-C30R/2 AH-58D, OH-58D 650 0.592 6 8.4 1 + FT - 1C 2 - 2 43.2 25.5 258
Allison 250-C30R/3 AH-58D, OH-58D 650 0.592 6 8.4 1 + FT - 1C 2 - 2 43.2 25.5 258
Allison 250-C30R/3M AH-6??, MH-6?? 650 0.592 6 8.4 1 + FT - 1C 2 - 2 43.2 25.5 258
Allison 250-C30S AUH-76A, S-75, S-76A-2 650 0.592 6 8.4 1 + FT - 1C 2 - 2 43.2 25.5 258
Allison 250-C30U (see T703-AD-700)
Allison AE1107C (see T406-AD-400)
Allison (Rolls-Royce) AE2100D3 C-130J, CC-130J Hercules, Hercules C.4/C.5, C-27J, E-3E (candidate engine) 6,000 0.410 1 + FT - 14 2 - 2
Allison (Rolls-Royce) AE2100H ATL3 1 + FT - 14 2 - 2
Turbomeca Ardiden 1H Dhruv (proposed engine), EC155, A149, KMH (candidate engine) 993 1 + FT 2C 1 - 1
Turbomeca Arriel 1A SA365C 641 0.573 9.0 1 + FT - 1 + 1C 2 - 1 42.9 22.4 265
Turbomeca Arriel 1A1 SA365C1 641 0.573 9.0 1 + FT - 1 + 1C 2 - 1 42.9 22.4 265
Turbomeca Arriel 1A2 SA365C2 641 0.573 9.0 1 + FT - 1 + 1C 2 - 1 42.9 22.4 265
Turbomeca Arriel 1B AS350B/BA 641 0.573 9.0 1 + FT - 1 + 1C 2 - 1 42.9 22.4 265
Turbomeca Arriel 1C AS365N 660 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1C1 AS365N1, S-76A+ 700 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1C2 AS365N2 700 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1D AS350B1/L1 684 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1D1 AS350B2, AS550, KA128 732 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1E BK117C1 708 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1E2 BK117C1/C2, EC145 738 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1K A109K/KN 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1K1 A109KM 738 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1M AS365MA/SA 691 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1M1 SA365K, AS565AA/CA/UA 783 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1S S-76A+ 700 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 1S1 S-76A++/C 723 1 + FT - 1 + 1C 2 - 1 60.6 31.0
Turbomeca Arriel 2B AS550C3 848 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 2B1 EC130B4 848 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 2B1A Z11 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 2C AS365N3, AS563AB/SB/UB, H410A 839 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 2C1 EC155B 839 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 2C2 EC155B1 944 1 + FT - 1 + 1C 2 - 1 39.9 22.7
Turbomeca Arriel 2S1 S-76C+ 856 1 + FT - 1 + 1C 2 - 1
Turbomeca Arriel 2S2 S-76C+ 1 + FT - 1 + 1C 2 - 1
Turbomeca Arrius 1A1 AS555AN/MN/SN/UN 480 1 + FT - 1C 1 - 1
Turbomeca Arrius 2B1 EC635T1 1 + FT - 1C 1 - 1
Turbomeca Arrius 2B1A EC635T1 1 + FT - 1C 1 - 1
Turbomeca Arrius 2B1A1 EC635T1 1 + FT - 1C 1 - 1
Turbomeca Arrius 2B2 EC635T2 1 + FT - 1C 1 - 1
Turbomeca Arrius 2F EC120B 1 + FT - 1C 1 - 1
Turbomeca Arrius 2K1 1 + FT - 1C 1 - 1
Turbomeca Arrius 2K2 1 + FT - 1C 1 - 1
Turbomeca Artouste I SE313B 360 1 - 1 + 1C 3 - -
Turbomeca Artouste IIC5 SE313B 360 7 3.9 1 - 1 + 1C 3 - -
Turbomeca Artouste IIC6 SE313B 360 7 3.9 1 - 1 + 1C 3 - -
Turbomeca Artouste IIIB SA315B, SA316B 570 0.760 10 5.2 1 - 1 + 1C 3 - -
Turbomeca Artouste IIID SA316C 1 - 1 + 1C 3 - -
Turbomeca Astazou II Skyvan 1A 495 1 - 1 + 1C 3 - - 50.0 18.0
Turbomeca Astazou IIIA SA318C 523 0.623 1 - 1 + 1C 3 - -
Turbomeca Astazou IIIA SA341 590 0.650 1 - 1 + 1C 3 - -
Turbomeca Astazou IIIB SA341H 1 - 1 + 1C 3 - -
Turbomeca Astazou IIIC SA341F 1 - 1 + 1C 3 - -
Turbomeca Astazou IIIC2 SA341F 1 - 1 + 1C 3 - -
Turbomeca Astazou IIIN SA341B/C/D/E 590 0.650 1 - 1 + 1C 3 - -
Turbomeca Astazou IIIN2 SA341B/C/D/E 590 0.650 1 - 1 + 1C 3 - -
Turbomeca Astazou XII Skyvan 2 690 1 - 2 + 1C 3 - -
Turbomeca Astazou XIV SA342L 858 1 - 2 + 1C 3 - -
Turbomeca Astazou XIVA 600 0.530 7 7.6 1 - 2 + 1C 3 - -
Turbomeca Astazou XIVB SA319F 573 0.624 1 - 2 + 1C 3 - - 56.3 366
Turbomeca Astazou XIVF SA319C/F 591 0.624 1 - 2 + 1C 3 - -
Turbomeca Astazou XIVH SA342K 1 - 2 + 1C 3 - -
Turbomeca Astazou XIVM SA342M 1 - 2 + 1C 3 - -
Turbomeca Astazou XVID Jetstream T.1/T.2 940 0.500 7 8.2 1 - 2 + 1C 3 - -
Turbomeca Astazou XVIG IA 58A 978 1 - 2 + 1C 3 - -
Turbomeca Astazou XX SA361 1,005 0.508 1 - 3 + 1C 4 - - 60.2 28.4 430
Turbomeca Astazou XXB SA361H 1,400 1 - 3 + 1C 4 - - 60.2 28.4
Rolls-Royce/Turbomeca Astazou 111N Gazelle AH-1 800
Turbomeca Bastan 6A IA 60 Guarani III 930 1 - 1 + 1C 3 - -
GE CT7-2A EH101 prototypes 1,625 0.473 1 + FT - 5 + 1C 2 - 2 47.0 26.0 442
GE CT7-6A1 CH-148 Petrel, CH-149 Chimo (not produced) 2,145 0.445 19.0 1 + FT - 5 + 1C 2 - 2 48.2 25.0 493
GE CT7-8A H-92A, S-92 2,740 1 + FT - 5 + 1C 2 - 2
IHI CT58-IHI-110-1 KV107/II-3/II-4/II-5 1,400 2 - 10 2 - 2 20.7 63.3 440
IHI CT58-IHI-110-2 1,400 2 - 10 2 - 2 20.7 63.3 440
IHI CT58-IHI-140-1 KV107/IIA-3/IIA-4/IIA-5/IIA-SM-1/IIA-SM-2/IIA-SM-3/IIA-SM-4/IIA-SM-17 1,400 2 - 10 2 - 2
IHI CT58-IHI-140-1 1,400 2 - 10 2 - 2
GE CT64-820-1 CC-115 Buffalo, DHC-5A 2,825 2 - 14 2 - 2
GE CT64-820-2 (see T64-GE-P4D)
GE CT64-820-3 CC-115 Buffalo, DHC-5A 3,060 2 - 14 2 - 2
GE CT64-820-4 CC-115D Buffalo, DHC-5D 3,133 2 - 14 2 - 2
LHTEC CTS800-2 A129 1,360 0.448 14.1 1 + FT - 2C 2 - 2 41.2 27.5 383
LHTEC CTS800-4N UH-1H, Super Lynx 300 1,360 0.448 14.1 1 + FT - 2C 2 - 2 41.2 27.5 383
Progress D-136 Mi-26 'Halo', Mi-26MS/T/TZ 11,400 0.456 562 18.7 2 + FT 6 7 1 1 2 146.3 55.2 2,315
Rolls-Royce Dart RDa.6 Mk.510 Turbo Mustang III 1,660 1 - 2C 3 - -
Rolls-Royce Dart RDa.6 Mk.514-7 F27 Mk.300M 1,715 1 - 2C 3 - -
Rolls-Royce Dart RDa.7 Mk.21 Br.1050 Alize, Br.1050M Alize-M 2,100 1 - 2C 3 - -
Rolls-Royce Dart RDa.7 Mk.528-7E F27 Mk.400M 2,000 1 - 2C 3 - -
Rolls-Royce Dart RDa.7 Mk.529-8 TC-4C 2,016 1 - 2C 3 - -
Rolls-Royce Dart RDa.7 Mk.532-7 F27 Mk.400M 2,150 1 - 2C 3 - -
Rolls-Royce Dart RDa.7 Mk.536-7R F27 Mk.500M 2,210 1 - 2C 3 - -
Rolls-Royce Dart RDa.8 Mk.101 A.W.660 Argosy C.1 2,582 1 - 2C 3 - -
Rolls-Royce Dart RDa.8 Mk.102 A.W.660 Argosy C.1 2,582 1 - 2C 3 - -
Rolls-Royce Dart RDa.8 Mk.150 Andover CC.1 2,016 1 - 2C 3 - -
Rolls-Royce Dart RDa.8 Mk.151 Andover CC.2 2,016 1 - 2C 3 - -
Rolls-Royce Dart RDa.12 Mk.201 Andover C.1, DHC-5C (not produced) 3,115 1 - 2C 3 - -
Napier Eland NEl.6 Mk.504A CC-109 (CL-66) Cosmopolitan 3,500
Napier Eland NEl.7 Rotodyne 2,800
GE GE12 Demonstrator for US Army 1,500 0.400 2 - 5 + 1C 2 - 2
Napier Gazelle NGa.2 Mk.101 Belvedere HC.1 1,465 0.740 16 6.3 1 + FT - 11 2 - 1 75.0 42.5 928 Notes
Napier Gazelle NGa.13 Mk.161 Wessex HAS.1 1,450 0.740 16 5.9 1 + FT - 11 2 - 1 75.0 42.5 940
Napier Gazelle NGa.13/2 Mk.162 Wessex HAS.31 1,540 0.750 16 6.1 1 + FT - 11 2 - 1 75.0 42.5 940
Napier Gazelle NGa.22 Mk.165 Wessex HAS.3 1,600 0.690 17 5.9 1 + FT - 11 2 - 1 75.0 42.5 884
Napier Gazelle NGa.22 Mk.165C Wessex HAS.31B 1,600 0.690 17 5.9 1 + FT - 11 2 - 1 75.0 42.5 884
Rolls-Royce Gem ?? Mk.??? Lynx HAS.5/HAS.7/HAS.8(Super Lynx)/AH.9(Battlefield Lynx)/Mk.27 3 4 1C 1 1 2
Rolls-Royce Gem ?? Mk.??? Lynx Mk.81/Mk.86/Mk.87/Mk.88/Mk.89/Mk.90, Lynx Mk.82/Mk.83/Mk.84/Mk.85 (not produced) 3 4 1C 1 1 2
Rolls-Royce Gem ?? Mk.??? Super Lynx Mk.95/Mk.99 3 4 1C 1 1 2
Rolls-Royce Gem 2 Mk.1001 Lynx AH.1/HAS.2/HAS.3(FN)/Mk.21/Mk.23/Mk.25/Mk.80, Lynx Mk.22/Mk.24/Mk.26 (not produced) 825 0.520 12 3 4 1C 1 1 2 43.4 23.5 393
Piaggio Gem 2 Mk.1004D A129 825 0.520 3 4 1C 1 1 2 360
Rolls-Royce Gem 41 Mk.101 1,000 3 4 1C 1 1 2 404
Rolls-Royce Gem 41 Mk.202 1,000 3 4 1C 1 1 2 404
Rolls-Royce Gem 42-1 Mk.204 Lynx HAS.3/HAS.3S/HAS.3ICE/HAS.3GM/HAS.4(FN) 1,000 0.490 13 3 4 1C 1 1 2 43.2 23.5 404
Rolls-Royce Gem 42-1 Mk.205 Lynx HAS.3/HAS.3S/HAS.3ICE/HAS.3GM/HAS.4(FN) 1,000 0.490 13 3 4 1C 1 1 2 43.2 23.5 404
Rolls-Royce Gem 42 Mk.1017 1,000 0.490 13 3 4 1C 1 1 2 43.2 23.5 404
Rolls-Royce Gem 43 Mk.1020 1,000 0.490 3 4 1C 1 1 2
Rolls-Royce Gem 47-1 Mk.??? Lynx AH.28 3 4 1C 1 1 2
de Havilland Gnome H.1000 Mk.101 Whirlwind HAR.9/HAR.10 1,050 1 + FT - 10 2 - 1
de Havilland Gnome H.1000 Mk.110 Wessex HC.2/HC.4/HU.5/Mk.52/Mk.53/Mk.54 1,350
de Havilland Gnome H.1000 Mk.111 Wessex HC.2/HU.5 1,350
de Havilland (Bristol Siddeley) Gnome H.1200 HKP-4A/B/D 1,200
de Havilland (Bristol Siddeley) Gnome H.1400 Sea King HAS.1, Whirlwind HCC.12, HKP-4C 1,400 0.620 8.4 1 + FT - 10 2 - 1 54.8 22.7 326
de Havilland (Bristol Siddeley) Gnome H.1400-1 Sea King HAS.2/HAR.3/HC.4/HAS.5/HAS.6/ASW.6, A 101G 1,660 0.620 14 8.5 1 + FT - 10 2 - 1 54.8 22.7 326
de Havilland (Bristol Siddeley) Gnome H.1800 1,750 15 9.9 1 + FT - 11 2 - 2
Glushenkov (OMKB) GTD-3BM Ka-25 'Hormone' 990 Notes
Glushenkov (OMKB) GTD-3F Ka-25 'Hormone' 900
Glushenkov (OMKB) GTD-350 Mi-2RM/URN/URP/US 'Hoplite' 394 0.840 5 6.1 1 + FT - 7 + 1C 1 - 2 54.4 24.8 307 Notes
PZL Rzeszów GTD-350W 414 0.840 5 6.1 1 + FT - 7 + 1C 1 - 2
Soyuz GTE-400 Ka-118 400
Honeywell HTS900 407 ARH 925 0.540 1 + FT - 1 + 1C 1 - 1 1
Pratt Whitney JFTD12A-4A CH-54A 4,500 2 - 9 2 - 2
Pratt Whitney JFTD12A-5A CH-54B 4,800 0.690 51 6.8 2 - 9 2 - 2
Avco Lycoming LTC 1K-4C CL-84 1,500 1 + FT - 7 + 1C 2 - 2
Avco Lycoming LTP 101-600A-1A P.166-DL3 615 0.544 8.5 1 + FT - 1 + 1C 1 - 1 37.4 23.3 325
Avco Lycoming LTP 101-700A-1A P.166-DLR-MAR 700 0.544 1 + FT - 1 + 1C 1 - 1 37.4 23.3 325
Avco Lycoming LTS 101-750B-2 HH-65A/B/C 742 0.570 8.8 1 + FT - 1 + 1C 1 - 1 32.4 24.7 268
Motorlet M601D PZL-130TM 750
Motorlet M601E PZL-130TB 750
Turbomeca Makila 1A1 AS532AC/AL/SC/UC/UL 1,877 0.481 1 + FT - 3 + 1C 2 - 2 54.9 20.3 535
Turbomeca Makila 1A2 AS532A2/U2 2,100 1 + FT - 3 + 1C 2 - 2 54.9 20.3 535
Turbomeca Makila 1A4 EC775 2,400 1 + FT - 3 + 1C 2 - 2 54.9 20.3 535
Turbomeca Makila 2A EC775 1 + FT - 3 + 1C 2 - 2
Armstrong Siddeley Mamba A.S.Ma.1 Br.960-1 Vultur prototype 980
Armstrong Siddeley Mamba A.S.Ma.3 Br.960-2 Vultur prototype 1,320
Armstrong Siddeley Mamba A.S.Ma.?? Seamew Mk.2 1,590
Armstrong Siddeley Double Mamba Mk.??? B-88 2,700
Armstrong Siddeley Double Mamba Mk.100 Gannet AS.1/T.2, Fairey 17 prototype, YB.1 prototype 2,950
Armstrong Siddeley Double Mamba Mk.101 Gannet AS.1/T.2/AS.4/COD.4/T.5/ECM.6 3,035
Armstrong Siddeley Double Mamba Mk.102 Gannet AEW.3 3,875
Snecma M138 A400M (candidate engine)
Mitsubishi MG6-10 Drones 70 0.430 4.5 1 - 1 1 - - 10.0 8.0
MTU/Rolls-Royce MTR 390 Tiger PAH/HAC, HAP, UHT 1,556 0.460 7 14.0 1 + FT - 2C 1 - 2 42.4 26.9 373
Napier Double Naiad YA.5 prototype (engine cancelled)
Bristol Nimbus 103 Wasp HAS.1 710 0.720 11 5.9 1 + FT - 2 + 1C 2 - 2
Bristol Nimbus 105 Scout AH.1 685 1 + FT - 2 + 1C 2 - 2
Kuznetsov NK-12M Tu-95M 'Bear-A' 14,795 0.360 143 13.0 1 - 14 5 - - 236.2 45.3 5,181
Kuznetsov NK-12MK A-90 'Casp-B' 1 - 14 5 - -
Pratt Whitney Canada PT6A-20 (see T74-CP-700)
Pratt Whitney Canada PT6A-25 T-34C 715 0.630 1 + FT - 3 + 1C 2 - 1 62.0 19.0 353
Pratt Whitney Canada PT6A-25A PC-7, PZL-130T/TE 650 0.630 1 + FT - 3 + 1C 2 - 1 62.0 19.0 343
Pratt Whitney Canada PT6A-25C EMB-312 Tucano, PZL-103TD 750 0.595 1 + FT - 3 + 1C 2 - 1 62.0 19.0 335
Pratt Whitney Canada PT6A-27 UV-18A/B, CC-138 Twin Otter, G-21G Turbo-Goose 620 0.602 7 6.7 1 + FT - 3 + 1C 2 - 1 62.0 19.0 328
Pratt Whitney Canada PT6A-29 (see T74-CP-702)
Pratt Whitney Canada PT6A-34 EMB-111, IAI 201/202 750 0.595 1 + FT - 3 + 1C 2 - 1 62.0 19.0 331
Pratt Whitney Canada PT6A-34B T-44A 750 0.595 1 + FT - 3 + 1C 2 - 1 62.0 19.0 344
Pratt Whitney Canada PT6A-38 C-12A 750 1 + FT - 3 + 1C 2 - 1 62.0 19.0
Pratt Whitney Canada PT6A-41 C-12C/D/L, RC-12D/G/H, TC-12B, UC-12B/D 850 0.591 1 + FT - 3 + 1C 2 - 2 67.0 19.0 403
Pratt Whitney Canada PT6A-42 C-12E/F/R/T/U, RC-12F/M, UC-12F/M 850
Pratt Whitney Canada PT6A-45R (see T101-CP-100)
Pratt Whitney Canada PT6A-50 C-7B, RC-7B 1 + FT - 3 + 1C 2 - 2
Pratt Whitney Canada PT6A-60A C-12S 1,050 0.548 1 + FT - 3 + 1C 2 - 2 72.0 19.0 475 Notes
Pratt Whitney Canada PT6A-62 PC-9A/B/Mk.2, PZL-130TC/TP 1,150 0.567 1 + FT - 3 + 1C 2 - 2 70.0 19.0 454
Pratt Whitney Canada PT6A-65AR C-23B 1,425
Pratt Whitney Canada PT6A-65B C-12J, UC-12J 1,100 0.536 10 10.0 1 + FT - 4 + 1C 2 - 2 74.0 19.0 481
Pratt Whitney Canada PT6A-66 Saras (prototype) 850 0.620 1 + FT - 4 + 1C 2 - 2 70.0 19.0 470
Pratt Whitney Canada PT6A-67D RC-12K/N/P/Q, Saras 1,220 0.530 1 + FT - 4 + 1C 2 - 2
Pratt Whitney Canada PT6A-68 JPATS PC-9 Mk.II, CT-156 Harvard II, EMB-312H 1,250 0.540 1 + FT - 4 + 1C 2 - 2 70.0 19.0 551
Pratt Whitney Canada PT6B-36 S-76B 981 0.594 1 + FT - 4 + 1C 2 - 2 59.2 19.5 372
Pratt Whitney Canada PT6B-37/1 A119 1 + FT - 4 + 1C 2 - 2
Pratt Whitney Canada PT6T-3B-1 CH-146 Griffon 1,800 0.596 1 + FT - 4 + 1C 2 - 2 67.0 44.0 660
Bristol Proteus 755 Britannia C.1/C.2 3,925
Pratt Whitney Canada PW120A CT-142 Dash 8, E-9A 2,000 0.485 2 + FT 1C 1C 1 1 2 84.0 31.0 933
Pratt Whitney Canada PW150?? USMC HLR (proposed engine) 2 + FT 1C 1C 1 1 2 84.0 33.0 1,060
Pratt Whitney Canada PW180 A400M (candidate engine)
Pratt Whitney Canada PW206B EC635P1 710 0.548 1 + FT - 1C 1 - 1
Pratt Whitney Canada PW206B2 EC635P2 1 + FT - 1C 1 - 1
Pratt Whitney Canada PW206C MH-68A, A109E 732 1 + FT - 1C 1 - 1
Pratt Whitney Canada PW209T Bell 400/440 (not produced) 1,000
Rolls-Royce RS.360-07 WG-13 900 0.500 7 12.2 2 + FT 4 1C 1 1 2
Rolls-Royce/Turbomeca RTM 321 Technology demonstrator 1 + FT - 3 + 1C 2 - 2
Rolls-Royce/Turbomeca RTM 322-01 S-70C (test aircraft) 2,100 1 + FT - 3 + 1C 2 - 2 46.1 25.9
Rolls-Royce/Turbomeca RTM 322-01/8 Merlin HM.1 (EH101 Mk.111), EH101 Mk.512/Mk.514/Mk.515/Mk.516, US101 (candidate engine) 2,200 0.450 14.0 1 + FT - 3 + 1C 2 - 2 46.1 25.9 539
Rolls-Royce/Turbomeca RTM 322-02/8 Merlin HC.3 (EH101 Mk.411), CH-149 Cormorant (candidate engine) 2,200 0.450 14.0 1 + FT - 3 + 1C 2 - 2 46.1 25.9 539
Rolls-Royce/Turbomeca RTM 322-01/9 NH90 NFH/TTH, HKP-14 (option) 2,430 0.420 16.0 1 + FT - 3 + 1C 2 - 2 46.1 25.9 499 4
Rolls-Royce/Turbomeca RTM 322-01/12 WAH-64 0.450 1 + FT - 3 + 1C 2 - 2 46.1 25.9 539
Westinghouse T30-W (engine cancelled)
GE XT31-GE-1 XP-81 1,700 0.870 6.1 1 - 14 1 - - 116.0 36.0 1,905
GE XT31-GE-2 XF2R-1 1,700 0.870 6.1 1 - 14 1 - - 116.0 36.0 1,905
GE XT31-GE-3 (engine cancelled) 1,700 0.870 6.1 1 - 14 1 - - 116.0 36.0 1,905
Pratt Whitney T32-P (engine cancelled)
Fredrich Flader XT33-FF-1 (engine cancelled) 5,900 0.590 4.7 1 - 11 2 - - 154.9 51.4 4,805
Pratt Whitney YT34-P-1 YC-124B, YKC-124B
Pratt Whitney T34-P-2 5,700
Pratt Whitney T34-P-3 C-133A 6,000
Pratt Whitney T34-P-5 YC-97J
Pratt Whitney T34-P-6 YC-121F
Pratt Whitney T34-P-7W C-133A, B-377SG 6,500
Pratt Whitney T34-P-7WA C-133A 6,500
Pratt Whitney T34-P-9W C-133B 7,500
Pratt Whitney YT34-P-12A (engine cancelled)
Wright XT35-W-1 XB-52 (early candidate engine, engine cancelled) 5,500 0.740 4.3 1 - 2C 2 - - 152.0 59.0 4,450
Chrysler T36-D (engine cancelled)
Turbodyne XT37-NA-1 MX-562 7,500 6.0 1 - 14 3 - - 167.0 44.2 5,050
Turbodyne XT37-NA-3 YB-35A 10,000 0.670 6.0 1 - 14 2 - - 167.0 46.0 6,000
Allison XT38-A-5 XF-84H, XF-88B, T-29E
Allison YT38-A-10 YH-16A
Allison XT39-A-1 (engine cancelled) 9,000 0.530 6.2 1 - 16 4 - - 176.0 39.0 3,700
Allison XT40-A-2 XA2D-1 5,100 17
Allison XT40-A-4 XP5Y-1 19
Allison YT40-A-6 XA2D-1, XA2J-1, XFV-1 5,500 19
Allison YT40-A-10 R3Y-1/-2 5,850
Allison YT40-A-14 XFV-1, XFY-1, X-18 7,100
GE XT41-GE-1 (engine cancelled) 2,700 1 - 14 2 - - 89.9 40.0 2,400
De Laval T42-DL (engine cancelled)
Wright XT43-W-1 (engine cancelled) 10,000 1 - 14 3 - - 163.6 45.0 6,400
Allison T44-A (engine cancelled)
Pratt Whitney XT45-P-1 XB-52 (early candidate engine, engine cancelled) 10,000 0.596 1 - 13 3 - - 183.0 54.0
Fairchild T46-F (engine cancelled)
Wright T47-W (engine cancelled)
Pratt Whitney T48-P (engine cancelled)
Wright YT49-W-1 XB-47D 9,600
Boeing XT50-BO-1 XL-19B
Boeing T50-BO-4
Boeing T50-BO-8A QH-50C 300
Boeing T50-BO-12 QH-50D
Continental XT51-T-1 XL-19C
Continental XT51-T-3 XH-13F
Pratt Whitney T52-P (engine cancelled)
Avco Lycoming T53-L-1 XH-40 (UH-1 prototype) 700 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-1A UH-1A, YH-40 (UH-1 pre-production) 770 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-1B HH-43A/B 825 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-2 1 + FT - 5 + 1C 1 - 1 Notes
Avco Lycoming T53-L-3 OA1A 960 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-3A OA1A/B/C, JOA1A 960 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-5 UH-1B 960 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-7 OA1A/B 1,005 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-9A UH-1D 1,100 1 + FT - 5 + 1C 1 - 1 Notes
Avco Lycoming T53-L-11 AH-1A, TH-1E, UH-1B/C/D/E/L, AB205A 1,100 0.700 11 6.1 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-11A HH-43F, QH-43G 1,100 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-11B 1,100 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-11C 1,100 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-11D UH-1B/C/D 1,100 1 + FT - 5 + 1C 1 - 1
Avco Lycoming T53-L-13 AH-1G/Q, EH-1H, HH-1H/K, TH-1L, UH-1H/L/M/V, CH-118 Iroquois, AB205A-1 1,400 0.580 13 7.4 1 + FT - 5 + 1C 2 - 2
Avco Lycoming T53-L-13A 1,400 0.580 13 7.4 1 + FT - 5 + 1C 2 - 2
Avco Lycoming T53-L-13B EH-1H, HH-1H, UH-1H/M/V 1,400 0.580 7.4 1 + FT - 5 + 1C 2 - 2 47.6 23.0 545
KHI T53-K-13B2 HH-1H 1,400 0.580 7.4 1 + FT - 5 + 1C 2 - 2 47.6 23.0 540
Avco Lycoming T53-L-15 OA1B/C, JOA1C, RV-1C 1,150 1 + FT - 5 + 1C 2 - 2
Avco Lycoming T53-L-17A Kaman K-Max 1,500 0.590 13 7.4 1 + FT - 5 + 1C 2 - 2 47.6 23.0 545
Avco Lycoming T53-L-701 OV-1D, TCH-1A 1,400 0.580 13 7.4 1 + FT - 5 + 1C 2 - 2
Avco Lycoming T53-L-701A OV-1D, RV-1D, TCH-1A, XC-2 1,400 0.590 7.4 1 + FT - 5 + 1C 2 - 2 58.4 23.0 693
Avco Lycoming T53-L-703 AH-1E/F/P/S, UH-1HP, TAH-1F/S 1,800 0.568 8.0 1 + FT - 7 + 1C 2 - 2 47.6 23.0 545
KHI T53-K-703 AH-1E, UH-1J 1,800 0.568 8.0 1 + FT - 7 + 1C 2 - 2 47.6 23.0 545
Allison T54-A-2
Allison T54-A-3 XFV-2 (not produced)
Allison T54-A-16 FV-2 (not produced)
Avco Lycoming T55-L-5 CH-47A, ACH-47A 2,200 1 + FT - 7 + 1C 2 - 2 Notes
Avco Lycoming T55-L-7 CH-47A, XC-143A 2,650 1 + FT - 7 + 1C 2 - 2 Notes
Avco Lycoming T55-L-7C CH-47B, YAH-63A 2,850 1 + FT - 7 + 1C 2 - 2 44.0 24.2 590 Notes
Avco Lycoming YT55-L-9 Piper Enforcer 2,500 0.608 1 + FT - 7 + 1C 2 - 2 62.2 24.2 799
Avco Lycoming T55-L-11A CH-47C, CH-147 Chinook 3,500 0.550 25 8.0 1 + FT - 7 + 1C 2 - 2 Notes
Avco Lycoming T55-L-11C CH-47C, CH-147 Chinook 3,500 0.550 25 8.0 1 + FT - 7 + 1C 2 - 2 Notes
Avco Lycoming T55-L-11E Chinook HC.1/HC.1B 3,750 0.550 8.0 1 + FT - 7 + 1C 2 - 2 Notes
Avco Lycoming T55-L-712 CH-47D, MH-47D, Chinook HC.1/HC.1B 3,750 0.520 8.2 1 + FT - 7 + 1C 2 - 2 48.5 28.7 760 Notes
Avco Lycoming T55-L-712E CH-47C+ 3,750 0.520 8.2 1 + FT - 7 + 1C 2 - 2 48.5 28.7 760 Notes
Avco Lycoming T55-L-712F Chinook HC.2/HC.2A 3,750 0.520 8.2 1 + FT - 7 + 1C 2 - 2 48.5 28.7 760 Notes
KHI T55-K-712 CH-47-414 3,750 0.520 7.4 1 + FT - 7 + 1C 2 - 2 48.5 28.7 540
Avco Lycoming (Textron Lycoming) T55-L-714 CH-47D, MH-47E 4,867 0.503 29 9.3 1 + FT - 7 + 1C 2 - 2 48.5 28.7 800
Avco Lycoming (Textron Lycoming) T55-L-714A CH-47F, MH-47G 4,867 0.500 9.3 1 + FT - 7 + 1C 2 - 2 48.5 28.7 832
Avco Lycoming (Honeywell) T55-GA-715B USMC HLR (proposed engine) 6,000 1 + FT - 7 + 1C 2 - 2
Allison T56-A-1 YC-130A 3,250 1 - 14 4 - -
Allison T56-A-3 YC-131C 1 - 14 4 - -
Allison T56-A-4 C-131H, VC-131H 1 - 14 4 - -
Allison T56-A-5 YH-16B 2,100 1 - 14 4 - -
Allison T56-A-7 C-130A, CC-130E/NT Hercules 3,750 1 - 14 4 - -
Allison T56-A-7A C-130B/E/F/G, CC-130E/NT Hercules 3,750 32 1 - 14 4 - -
Allison T56-A-8A C-2A, E-2A 4,100 1 - 14 4 - -
Allison T56-A-8B C-2A, E-2A 4,100 1 - 14 4 - -
Allison T56-A-9 C-130A/D 3,750 1 - 14 4 - -
Allison T56-A-10W P-3A 4,200 0.520 32 9.3 1 - 14 4 - -
Allison T56-A-11 C-130A 4,050 1 - 14 4 - -
Allison T56-A-14 P-3B/C, CP-140 Aurora 4,591 0.540 32 9.6 1 - 14 4 - - 146.3 49.0 1,885
IHI T56-IHI-14 P-3C 4,591 0.595 32 9.5 1 - 14 4 - - 146.3 49.0 1,885
Allison T56-A-15 C-130H/K, EC-130E, HC-130H/N/P, TC-130H, Hercules C.1/C.3, CC-130H Hercules 4,591 0.540 32 9.6 1 - 14 4 - - 146.3 44.6 1,848
Allison T56-A-16 EC-130Q, LC-130R 4,591 32 9.3 1 - 14 4 - - 146.3 44.6 1,841
Allison T56-A-17 C-130E 4,050 1 - 14 4 - -
Allison T56-A-18 Demonstrator for US Navy 5,000 32 9.7 1 - 14 4 - - 146.3 44.6 1,841
Allison T56-A-422 C-2A, E-2C 4,910 1 - 14 4 - - 146.3 44.6 1,841
Allison T56-A-423 EC-130Q 4,591 32 9.3 1 - 14 4 - - 146.3 44.6 1,841
Allison T56-A-425 C-2A, E-2C 4,591 32 9.7 1 - 14 4 - - 146.3 44.6 1,899
Allison T56-A-427 E-2C+ 5,250 0.470 12.0 1 - 14 4 - - 146.1 48.3 1,940
Pratt Whitney T57-P-1 XC-132A 15,000
GE T58-GE-1 CH-3B/C, SH-3A, S-61A 1,290 2 - 10 2 - 1 59.0 20.9 315
GE T58-GE-2 AB204AS 1,325 2 - 10 2 - 1 59.0 20.9 315
GE T58-GE-3 TH-1F, UH-1F/P 1,290 2 - 10 2 - 1 59.0 20.9 309
GE T58-GE-5 CH-3E, HH-3E/F, SH-3E/F 1,500 0.600 8.4 2 - 10 2 - 1 59.0 20.9 335
GE T58-GE-6 CH-46A 1,250 8.2 2 - 10 2 - 1 59.0 20.9 305 Notes
GE T58-GE-8B SH-2F, SH-3G, UH-2A/B/C, CH-113A Labrador 1,250 8.2 2 - 10 2 - 1 59.0 20.9 305
GE YT58-GE-8D X-22 1,250 8.2 2 - 10 2 - 1 59.0 20.9 305
GE T58-GE-8F SH-2F, SH-3G, UH-2C, CH-124A/B Sea King 1,350 0.600 8.2 2 - 10 2 - 1 59.0 20.2 305
GE T58-GE-10 CH-46D/F, UH-46D/F, HH-2D, HH-3F, SH-3D/G/H, ASH-3A/D/TS, AS-61R 1,400 0.620 14 8.4 2 - 10 2 - 1 59.0 20.2 350 Notes
GE T58-GE-16 CH-46E 1,870 0.530 14 8.4 2 - 10 2 - 2 63.3 24.2 440
GE T58-GE-100 ASH-3H, CH-124A/B Sea King 1,500 2 - 10 2 - 1 59.0 20.9 335
GE T58-GE-402 CH-46D/E, SH-3H, UH-3H 1,500 2 - 10 2 - 1 59.0 20.9 335
T59 (engine cancelled)
Boeing T60-BO (engine cancelled)
Allison T61-A (engine cancelled)
Solar T62-S (APU)
Allison T63-A-1 KD-10 (not produced) 4 2 - 6 + 1C 2 - 2
Allison T63-A-5A OH-6A, AH-6B, EH-6B, MH-6B, QH-50E, QH-50F (not produced) 252 4 7.2 2 - 6 + 1C 2 - 2
Allison T63-A-100 O-2T 317 4 7.2 2 - 6 + 1C 2 - 2
Allison T63-A-700 OH-58A, CH-158 317 4 7.2 2 - 6 + 1C 2 - 2
Allison T63-A-720 OH-58C, TH-57 418 0.690 4 7.3 2 - 6 + 1C 2 - 2 40.8 23.2 158
GE T64-GE-1 CH-53A 3,080 1 + FT - 14 2 - 2
GE T64-GE-3 HH-53B 3,080 1 + FT - 14 2 - 2
GE YT64-GE-4 YCV-7A 2,850 1 + FT - 14 2 - 2
GE T64-GE-5 XC-142A 3,080 1 + FT - 14 2 - 2
GE T64-GE-6 CH-53A, TH-53A 2,850 1 + FT - 14 2 - 2
GE T64-GE-6B CH-53A, TH-53A 3,080 1 + FT - 14 2 - 2
GE T64-GE-7 CH-53C, HH-53B/C/H 3,925 1 + FT - 14 2 - 2
MTU T64-MTU-7 CH-53G 3,925 0.480 13.0 1 + FT - 14 2 - 2 79.0 20.1 712
GE T64-GE-7A CH-53C, HH-53C 3,936 0.470 14.1 1 + FT - 14 2 - 2 79.0 20.1 720
GE T64-GE-10 CV-7A, C-8A, DHC-5, PJ2 2,736 1 + FT - 14 2 - 2
IHI T64-IHI-10 PS-1 2,736 1 + FT - 14 2 - 2
IHI T64-IHI-10J US-1A, YS-11E 2,736 12.5 1 + FT - 14 2 - 2 79.0 21.1 1,240
GE T64-GE-16A CH-53A, YAH-56A 3,485 0.480 27 13.0 1 + FT - 14 2 - 2 79.0 24.2 720
GE T64-GE-100 MH-53J, TH-53A, S-65A 4,330 0.480 29 14.9 1 + FT - 14 2 - 2 79.0 24.2 720 Notes
GE T64-GE-412 CH-53D, Ya’sur 2000 (not produced) 3,695 1 + FT - 14 2 - 2 79.0 24.2 720
GE T64-GE-413 CH-53D, RH-53A, VH-53D 3,925 0.470 29 14.1 1 + FT - 14 2 - 2 79.0 24.2 720
GE T64-GE-413A CH-53D, RH-53D, VH-53D 3,925 0.470 29 14.1 1 + FT - 14 2 - 2 79.0 24.2 720
GE T64-GE-415 RH-53D/E, MH-53J/M, TH-53B 4,380 0.470 29 14.8 1 + FT - 14 2 - 2 79.0 24.2 720
GE T64-GE-416 CH-53E, MH-53E 4,380 1 + FT - 14 2 - 2 79.0 24.2 720
GE T64-GE-416A CH-53E, MH-53E 4,380 1 + FT - 14 2 - 2 79.0 24.2 720
GE T64-GE-419 MH-53E, USMC HLR (proposed engine) 4,750 14.9 1 + FT - 14 2 - 2 79.0 24.2 755
GE T64-GE-716 3,925 1 + FT - 14 2 - 2 79.0 24.2 720
GE T64-GE-P4C DHC-5B (not produced) 1 + FT - 14 2 - 2 110.0 20.1
Fiat T64-GE-P4D G222, G222RM/VS 2,938 1 + FT - 14 2 - 2 110.0 20.1 1,188
GE T64-GE-P4D-1 C-27A 3,400 0.480 27 13.2 1 + FT - 14 2 - 2 110.0 20.1 1,188
GE T64-GE-S4D-1 S-64B 3,780 1 + FT - 14 2 - 2
GE T64-GE-T4C-2 4,330 1 + FT - 14 2 - 2 79.0 20.1 720 Notes
Continental T65-T (engine cancelled) 335 0.710 3 6.0 1 + FT - 1 + 1C 2 - 1
Solar T66-S (engine cancelled)
Continental XT67-T-1 UH-1D flight test 1,700 0.570 7 7.9 1 + FT - 2 + 1C 2 - 1
Rolls Royce T68-RR (engine cancelled)
Continental T69-T (engine cancelled)
Westinghouse T70-W (engine cancelled)
Allison T71-A (engine cancelled)
Continental T72-T (see XT67-T-1)
Pratt Whitney T73-P-1 CH-54A 4,500 0.690 1 + FT - 9 2 - 2 34.0 920 Notes
Pratt Whitney T73-P-700 CH-54B 4,800 0.688 1 + FT - 9 2 - 2 34.0 935 Notes
Pratt Whitney Canada T74-CP-700 U-21A, RU-21A/D, VC-6A/B 550 1 + FT - 3 + 1C 2 - 1 62.0 19.0 Notes
Pratt Whitney Canada T74-CP-702 RU-21B/C/E 620 1 + FT - 3 + 1C 2 - 1 62.0 19.0 Notes
Garrett T76-G-10 OV-10A 1,040 0.600 8.6 1 - 2 3 - - 43.0 27.0 341
Garrett T76-G-416 OV-10A 1,433 1 - 2 3 - - 43.0 27.0
Garrett T76-G-417 OV-10A 1,433 1 - 2 3 - - 43.0 27.0
Allison XT78-A-2 (engine cancelled) 4,800
Allison T80-A (engine cancelled)
Pratt Whitney Canada T101-CP-100 C-23A/B 850 0.553 1 + FT - 3 + 1C 2 - 2 72.0 19.0 448 Notes
Pratt Whitney Canada T400-CP-400 AH-1J/Q, UH-1N, VH-1N, YAH-63A, CH-135 Huey, Bell 412+ (not produced) 1,530
Pratt Whitney Canada T400-WV-402 AH-1T 1,450
T401 (engine cancelled)
T402 (engine cancelled)
T403 (engine cancelled)
T404 (engine cancelled)
Avco Lycoming T405 (engine cancelled)
Allison (Rolls-Royce) T406-AD-400 CV-22A/B, HV-22A/B, MV-22A/B, USMC HLR (proposed) 6,150 0.426 36 16.7 1 + FT - 14 2 - 2 77.1 34.2 971 Notes
GE T407-GE-?? P-7A (not produced) 6,000 1 + FT - 5 + 1C 2 - 3
GE T407-GE-?? P-9A (not produced) 1 + FT - 5 + 1C 2 - 3
GE T408 (engine cancelled)
GE T700-GE-401 AH-1W/Z, SH-2G, TAH-1W, HH-60D, SH-60B, AH-1T+ prototype 1,720 0.464 17.0 1 + FT - 5 + 1C 2 - 2 46.0 25.0 441
GE T700-GE-401C UH-1Y, HH-60H/J, MH-60S, SH-60B/F/H, S-70B/C, AH-1Z (proposed) 1,800 0.459 18.0 1 + FT - 5 + 1C 2 - 2 46.0 25.0 458
IHI T700-IHI-401C UH-60J/JA, S-70J/K 1,800 0.459 18.0 1 + FT - 5 + 1C 2 - 2 46.0 25.0 458
GE T700-GE-700 EH-60A/C, HH-60G, MH-60A/D/G, UH-60A/P/Q, VH-60N, S-70A, YUH-61A, AH-1T+ prototype, HH-60A/E (not produced) 1,622 0.465 10 17.0 1 + FT - 5 + 1C 2 - 2 46.0 25.0 437
GE T700-GE-701 AH-1Z, AH-64A 1,720 0.464 17.0 1 + FT - 5 + 1C 2 - 2 46.0 25.0 438
GE T700-GE-701A S-70C 1,720 0.465 17.0 1 + FT - 5 + 1C 2 - 2 46.0 25.0 438
GE T700-GE-701C EH-60L, HH-60G/L/M, MH-60G/K/L, NSH-60R, UH-60L, S-70A/C, S-70A-9, AH-64A/D, AH-1Z 1,890 0.462 18.0 1 + FT - 5 + 1C 2 - 2 46.0 25.0 456
GE T700-GE-701D AH-64D, UH-60M 1,944 0.465 18.0 1 + FT - 5 + 1C 2 - 2 46.0 25.0 456
GE T700-GE-T6A EH101 Mk.110/112/410, US101 (candidate engine) 2,000 0.450 18.0 1 + FT - 5 + 1C 2 - 2 48.2 25.0 485
GE T700-GE-T6A-1 CH-149 Cormorant (EH101 Mk.511) 2,145 0.445 19.0 1 + FT - 5 + 1C 2 - 2 48.2 25.0 493
GE T700-GE-T6C 2,040 1 + FT - 5 + 1C 2 - 2 48.2 25.0
GE T700-GE-T6E NH90 NFH/TTH, HKP-14 (option) 2,270 0.434 19.0 1 + FT - 5 + 1C 2 - 2 48.2 25.0 531
GE T700-GE-T6E-1 NH90 NFH/TTH, HKP-14 (option) 2,270 0.434 19.0 1 + FT - 5 + 1C 2 - 2 48.2 25.0 537
Allison T701-A-401 XCH-62A (not produced) 8,080
Allison T701-A-401X S-92M (not produced)
Avco Lycoming T702-LD-400 (see LTS-101-750B-2)
Allison T703-AD-700 OH-58D, Combat Scout 406 (proposed) 650 0.580 8.6 1 + FT - 1C 2 - 2 43.2 25.1 225
LHTEC T800-LHT-800 RAH-66A (not produced) 1,400 0.448 14.1 1 + FT - 2C 2 - 2 33.2 26.1 315
LHTEC T800-LHT-801 RAH-66A, Battlefield Lynx 800 (not produced) 1,560 0.460 14.1 1 + FT - 2C 2 - 2
LHTEC T800-LHT-802 RAH-66A (not produced) 1,608 0.460 14.1 1 + FT - 2C 2 - 2
Turbomeca/Agusta TAA230 A106 260
Turbomeca TM333-1A AS565UB (candidate engine) 1 + FT - 2 + 1C 1 - 1
Turbomeca TM333-2B2 Dhruv 1,105 0.529 1 + FT - 2 + 1C 1 - 1 41.1 28.0 345 1
Turbomeca TM333-2M2 Cheetal, Chetan (proposed) 1,105 0.529 1 + FT - 2 + 1C 1 - 1 41.1 28.0 345 1
Europrop TP400-D6 A400M 10,000 22.0 2 + FT 5 1 3 137.8 4,035
Garrett TPE331-1-101F AU-23A 705 1 - 2C 3 - - 26.0 336
Garrett TPE331-2-201A Skyvan 3M/3M-200 715 0.556 8.3 1 - 2C 3 - - 26.0 336
Garrett TPE331-2-201C C-212A/AV/B/C/E 715 0.556 8.3 1 - 2C 3 - - 26.0 336
Garrett TPE331-3A-301W C-10A (not produced) 840 0.548 10.3 1 - 2C 3 - - 43.0 26.0 355
Garrett TPE331-3UW-304G Merlin IVA 904 0.548 10.3 1 - 2C 3 - - 43.0 26.0 355
Garrett TPE331-5-251C C-211-100 840 0.577 10.3 1 - 2C 3 - - 43.0 26.0 355
Garrett TPE331-5-251K Turbo Commander 690/690A/680B 840 0.577 10.3 1 - 2C 3 - - 43.0 26.0 355
Garrett TPE331-5-252C C-212-100 840 0.577 10.3 1 - 2C 3 - - 43.0 26.0 355
Garrett TPE331-5-252D Do 228-101/-202 840 0.577 10.3 1 - 2C 3 - - 43.0 26.0 355
Garrett TPE331-5-252K Turbo Commander 690A/690B 840 0.577 10.3 1 - 2C 3 - - 43.0 26.0 355
Garrett TPE331-5-254K Jetprop Commander 690C/690D 840 0.577 10.3 1 - 2C 3 - - 43.0 26.0 355
Garrett TPE331-5-255K Turbo Commander 690/690A/690B, Jetprop Commander 690C/690D 840 0.577 10.3 1 - 2C 3 - - 43.0 26.0 355
Garrett TPE331-10 C-212-10, Altair, Mariner 984 0.550 10.8 1 - 2C 3 - - 26.0 380
Garrett TPE331-10-501K Commander 980/1000 984 0.550 10.8 1 - 2C 3 - - 46.0 26.0 380
Garrett TPE331-10R C-41A 984 0.550 10.8 1 - 2C 3 - - 26.0 380
Garrett TPE331-10T YMQ-9A (Predator B) 984 0.550 10.8 1 - 2C 3 - - 26.0 380
Garrett TPE331-10T-516K Turbo Commander 690A/690B, Commander 840/900 984 0.550 10.8 1 - 2C 3 - - 46.0 26.0 380
Garrett TPE331-10UF Jetstream T.3 984 0.550 10.8 1 - 2C 3 - - 46.0 26.0 380
Garrett TPE331-11-601W IA 66 prototype 1,000 0.530 10.8 1 - 2C 3 - - 46.0 26.0 400
Garrett TPE331-11U-601G C-26A 1,000 0.530 10.8 1 - 2C 3 - - 46.0 26.0 400
Garrett TPE331-11U-611G C-26A 1,000 0.530 10.8 1 - 2C 3 - - 46.0 26.0 400
Garrett TPE331-11U-612G C-26A 1,000 0.530 10.8 1 - 2C 3 - -
Pratt Whitney Canada TPE331-12B Tucano T.1 1,151 0.530 10.8 1 - 2C 3 - -
Garrett TPE331-12UA-701G C-26B 1,151 0.522 10.8 1 - 2C 3 - - 46.0 26.0 400
Garrett TPE331-12UAR-701G C-26B 1,151 0.522 10.8 1 - 2C 3 - - 46.0 26.0 400
Garrett TPE331-12UHR-701G UC-26C 1,151 0.522 10.8 1 - 2C 3 - -
Garrett (Allied-Signal) TPE331-14F-801L G520, G520T 0.515 11.0 1 - 2C 3 - - 53.0 32.0 620
Garrett (Allied-Signal) TPE331-14GR-801E An-38-100 0.510 11.4 1 - 2C 3 - - 53.0 36.0 620
Garrett (Allied-Signal) TPE331-14HR-801E An-38-100 0.510 11.4 1 - 2C 3 - - 53.0 36.0 620
Garrett (Allied-Signal) TPE331-15A S-2/AT/ET/E(UP)/T 1,712 0.510 11.0 1 - 2C 3 - -
Mitsubishi TS1-10 OH-1 800
Turbomeca Turmo IIIC SA321A 1,480 0.603 13 5.9 1 + FT - 1 + 1C 2 - 1
Turbomeca Turmo IIIC3 SA321B/D/G 1,480 0.603 13 5.9 1 + FT - 1 + 1C 2 - 1
Turbomeca Turmo IIIC4 SA330B 1,384 0.632 13 5.8 1 + FT - 1 + 1C 2 - 1
Turbomeca Turmo IIIC5 1,500 0.632 1 + FT - 1 + 1C 2 - 1
Turbomeca Turmo IIIC6 SA321F/G/H/J/Ja/K/L/M 1,550 0.632 1 + FT - 1 + 1C 2 - 1
Turbomeca Turmo IIIC7 1,610 0.632 1 + FT - 1 + 1C 2 - 1
Turbomeca Turmo IIID Br.941 1,200 1 + FT - 1 + 1C 2 - 2 Notes
Turbomeca Turmo IIID3 Br.941S 1,480 0.616 13 5.9 1 + FT - 1 + 1C 2 - 2
Turbomeca Turmo IIIE SA321H 1,480 0.603 1 + FT - 1 + 1C 2 - 2
Turbomeca Turmo IIIE6 1,584 0.603 1 + FT - 1 + 1C 2 - 2
Turbomeca Turmo IVA SA330F/H 1,417 0.629 1 + FT - 1 + 1C 2 - ??
Turbomeca Turmo IVB SA330F/G 1,417 0.629 1 + FT - 1 + 1C 2 - ??
Turbomeca Turmo IVC SA330J/L/M 1,417 0.629 1 + FT - 1 + 1C 2 - ??
Isotov (Klimov) TV2-117A Mi-8 'Hip', Mi-9 'Hip-G', Mi-14GP 'Haze' 1,670 0.600 18 6.6 1 + FT - 10 2 - 2 111.5 29.3 745 Notes
Isotov (Klimov) TV2-117TG Mi-8TG, Mi-38 1 + FT - 10 2 - 2
Isotov (Klimov) TV3-117B Ka-32 'Helix-C' 1 + FT - 10 2 - 2
Isotov (Klimov) TV3-117BK 2,170 1 + FT - 10 2 - 2
Isotov (Klimov) TV3-117KM Ka-27 'Helix-A' 1 + FT - 10 2 - 2
Isotov (Klimov) TV3-117M Mi-14 'Haze' 1,900 1 + FT - 10 2 - 2
Isotov (Klimov) TV3-117MT Mi-17 'Hip-H', Mi-17P 'Hip-K', Mi-24 'Hind-A' 1,900 1 + FT - 10 2 - 2 82.1 28.5 628
Isotov (Klimov) TV3-117V Mi-24 'Hind', Mi-25 (export Mi-24D), Mi-35 (export Mi-24V), Mi-35P (export Mi-24P) 2,100 0.463 9.0 1 + FT - 10 2 - 2 Notes
Isotov (Klimov) TV3-117VK Ka-28 'Helix-A', Ka-29TB 'Helix-B' 2,200 1 + FT - 10 2 - 2 Notes
Isotov (Klimov) TV3-117VM Mi-17 'Hip-H', Mi-38 (proposed) 2,000 1 + FT - 10 2 - 2 Notes
Isotov (Klimov) TV3-117VM-02 Mi-17 'Hip-H' 2,000 1 + FT - 10 2 - 2 Notes
Isotov (Klimov) TV3-117VMA Mi-24 'Hind-A', Mi-28A 'Havoc-A', Ka-31 (Ka-29RLD) 'Helix-E', Ka-32T 'Helix-C', Ka-32S 'Helix-D', Ka-50/-50Sh/-50K 'Hokum-A', Ka-52/-52K 'Hokum-B' 2,200 1 + FT - 10 2 - 2 Notes
Isotov (Klimov) TV3-117VMA-02 Ka-32T 'Helix-C', Ka-32S 'Helix-D' 2,200 1 + FT - 10 2 - 2 Notes
Isotov (Klimov) TV3-117VMA-03 Mi-28N 'Havoc-N' (proposed) 2,200 1 + FT - 10 2 - 2
Isotov (Klimov) TV3-117VMA-F Ka-32T 'Helix-C', Ka-32S 'Helix-D', Ka-50/-50Sh/-50K 'Hokum-A', Ka-52/-52K 'Hokum-B', Mi-28N 'Havoc-N' (proposed) 2,200 1 + FT - 10 2 - 2
Klimov TV7-117VK Ka-50/-50Sh/-50K 'Hokum-A', Ka-52/-52K 'Hokum-B' 1 + FT - 5 + 1C 2 - 2
Baranov (OMSK) TVD-20-03 An-38-200 1,380 0.506 1 + FT - 7 + 1C 2 - 2 69.7 33.5 628
PZL Rzeszów TWD-10W W-3L/RM/U 888 0.600 10 7.4 1 + FT - 6 + 1A 2 - 1 73.8 30.1 310 Notes
Rolls-Royce Tyne RTy.12 Mk.101 Belfast C.1 5,460 0.450 13.5 2 6 9 1 - 3 109.0 43.2 2,219
Rolls-Royce Tyne RTy.12 Mk.515/10 CC-106 Yukon 5,730 13.5 2 6 9 1 - 3 109.0 43.2 2,219
Rolls-Royce Tyne RTy.20 Mk.21 Atlantic ATL2 (Br.1150) 5,856 0.470 47 14.0 2 6 9 1 - 3 109.0 43.2 2,203
Rolls-Royce Tyne RTy.20 Mk.22 C-160A/D/F/G/H/NG/R/P/T/Z, C-160AAA/ASF/S/SE (not produced) 6,100 0.470 14.0 2 6 9 1 - 3 109.0 43.2 2,203
Rolls-Royce Tyne RTy.20 Mk.801 G222T 5,480 0.453 14.0 2 6 9 1 - 3 109.0 43.2 2,187
Klimov VK-2500 Mi-17 (Mi-8MT) 'Hip-H', Mi-14 'Haze', Mi-24 'Hind', Mi-25 (Mi-24D) 'Hind-D', Mi-35 (Mi-24V) 'Hind-E', Mi-28 'Havoc-A', Mi-28N 'Havoc-B', Ka-27/-28 'Helix-A', Ka-29 'Helix-B', Ka-31 'Helix-E', Ka-32T 'Helix-C', Ka-32S 'Helix-D', Ka-32A/A1/A2, Ka-50/-50Sh/-50K 'Hokum-A', Ka-52/-52K 'Hokum-B' (proposed)
B - Booster stage(s)
C - Centrifugal compressor stage(s)
R - Radial turbine stage(s)
** - 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.



To top of page



Last updated: 21 Mar 2005

Nathan Meier   nate@jet-engine.net
Copyright © 2000-2005 Nathan Meier