FSC 2995 Miscellaneous Aircraft Engine Accessories: 2995-00-125-4431, 2995-00-127-4128, 2995-00-127-7487
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2995-00-125-4431 2995001254431 | LD586757 BUWEPSLD586757 | Control Assembly, Push-Pull | BAE Systems Land & Armaments L.P. (44114) Navair and Navsea Managed (10001) | ||
| 2995-00-125-8914 2995001258914 | 206-001-118-3 | Control arm, Throttle | General Characteristics Item Description: Shaft 1.687 lg; 0.4997 in. min 0.5002 in. max dia; shaft tongue 0.1868 in. min 0.1873 in. max W after plating by 0.550 in. lg; one 0.094 in. min 0.097 in. max dia thru hole in shaft; right angle clevis, rod end, 1.409 in. lg; 0.628 in. w; 0.1896 in. min 0.1901 in. max dia inline holes in ea clevis arm spaced 1.910 in. center to center W/shaft, 63.0 microin surf finish in hole; clevis offset 0.480 in. | Bell Helicopter Textron Inc. (97499) | |
| 2995-00-125-8915 2995001258915 | 206-062-711-1 | Retainer, Boot Contr | Bell Helicopter Textron Inc. (97499) | ||
| 2995-00-126-0888 2995001260888 | 362562-2 | Chamber Assembly, Cartridge | III End Item Identification: 2995001153532 383934-1-1 starter General Characteristics Item Description: Steel chamber, 6.530 to 6.540 in. id, W/handle and hdwe III Fsc Application Data: Starter, engine, gas, acft | Honeywell International Inc. (59364, 99193) | |
| 2995-00-126-0889 2995001260889 | 364020-1 364020-4 | Plenum Assembly, Starter | III End Item Identification: Starter, engine, gas turbine P/N 383934-1-2;USAF type STU-20/A34;J79-GE-15 acft eng General Characteristics Item Description: Components shell, support, inner segment, outer segment, plate, holder, flange;matl steel, welded;od turbine wheel assy opening 9.070 to 9.100 in.;chamber assy opening 8.360 to 8.420 in. | Honeywell International Inc. (99193) | |
| 2995-00-126-0890 2995001260890 | 364021-1 | Chamber, Cartridge Starter | III End Item Identification: Starter, engine, gas turbine P/N 383242-1-8, 383934-1-2;USAF type STU-20/A34;U/O J79-15 acft eng General Characteristics Item Description: O/a dia 7.225 to 7.229 in.;id 6.530 to 6.540 in.;wall thk 0.090 to 0.135 in.;o/a chamber lg 7.583 to 7.613 in.;boss lg 0.575 to 0.585 in.;boss stock dia 0.875 in.;matl cres III Fsc Application Data: Starter, engine, gas, acft | Honeywell International Inc. (59364, 99193) | |
| 2995-00-126-0891 2995001260891 | 364034-1 | Lever Assembly, Splined | III End Item Identification: Starter, engine, gas turbine P/N 383934-1-2, usaf type STU-20/A34 General Characteristics Item Description: Matl cres 17-4PH, ams 5355;ROCKWELL hardness rc 35.0 to 42.0;SPLINED shank 2.510 to 2.530 in. lg, spline quantity 36, major dia 0.3110 in., minor dia 0.2910 in.;lever end thk 0.590 to 0.610 in.;distance between shank and lever end hole 1.584 in.;incl insert MS21209F1-15 | Honeywell International Inc. (59364, 99193) | |
| 2995-00-126-0896 2995001260896 | 364036-1 | Lever Assembly, Actuating | III End Item Identification: Starter, engine, gas turbine P/N 383242-1-8, 383934-1-2;USAF type STU-20/A34;U/O J79-GE-15 acft eng General Characteristics Item Description: Matl cres ams 5643, ams 5355;O/A W 0.680 to 0.700 in. | Honeywell International Inc. (59364, 99193) | |
| 2995-00-126-0898 2995001260898 | 364039-1 | Lever, Actuating | III End Item Identification: Starter, engine, gas, turbine P/N 383242-1-8, 383934-1-2;USAF type STU-20/A34;J79-GE-15 acft eng General Characteristics Item Description: O/a lg 2.435 to 2.490 in.;o/a W 0.790 to 0.820 in.;pivot hole dia 0.2008 to 0.2013 in.;pivot end od 0.910 to 0.940 in.;pivot end O/a W 0.420 to 0.440 in.;matl cres ams 5355 or 5643;HEAT treat rockwell C 35.0 to 42.0 | Honeywell International Inc. (99193, 59364) | |
| 2995-00-126-6088 2995001266088 | 364067-1 | Spring Assembly, cam | III End Item Identification: Starter, engine, gas turbine P/N 383934-1-2;USAF type STU-20/A34;J79-GE-15 acft eng General Characteristics Item Description: Components rivet, blind P/N MK321BS, fscm 07707;PLATE, reinforcing P/N 364050-1;SPRING, leaf P/N 364032-1;CAM, control P/N 364033-1 | Honeywell International Inc. (59364, 99193) | |
| 2995-00-126-6090 2995001266090 | 364075-1 | Cover, Governor | Honeywell International Inc. (99193, 59364) | ||
| 2995-00-126-6091 2995001266091 | 364078-1 | Wheel Assembly, Turbine | III End Item Identification: Starter, engine, gas turbine P/N 383242-1-8, 383934-1-2;USAF type STU-20/A34;J79-15 acft eng | Honeywell International Inc. (99193, 59364) | |
| 2995-00-126-6092 2995001266092 | C4P10595-5 | Arm Assembly, Throttle | III End Item Identification: Control assy, engine, overhead console, P/N C4P10160-5, C7A General Characteristics Item Description: Lh;prop reversing;matl steel plate, 0.063 in. thk, MIL-S-18729 III Fsc Application Data: Quadrant control | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| 2995-00-126-6093 2995001266093 | C4P10595-6 | Arm Assembly, Throttle | III End Item Identification: Control assy, engine, overhead console, P/N C4P10160-5, C-7A General Characteristics Item Description: Rh;prop reversing;matl steel plate 0.063 in. thk, MIL-S-18729, cond N III Fsc Application Data: Quadrant control | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| 2995-00-126-6107 2995001266107 | C4P10607-5 | Arm Assembly, Throttle | General Characteristics Item Description: Lh, steel, prop reversing III Fsc Application Data: Control quadrant, overhead console, P-N C4P10160-5, C7A acft engine accessory | Bombardier Aerospace Aerospace Div. (71867) | |
| 2995-00-126-6108 2995001266108 | C4P10607-6 | Arm Assembly, Throttle, Prop Rever | III End Item Identification: C-7A acft General Characteristics Item Description: Arm matl steel MIL-S-18729;O/A thk 0.063 in.;slot W 0.440 IN.;2 rivet holes for 0.188 in. dia rivet, holes spaced 1.000 in. C to c;fulcrum hole 0.7875 to 0.7885 in. III Fsc Application Data: Controls assy, engine, overhead console P/N C4P10160-5 | DE Havilland Inc. (0HWZ3) Bombardier Aerospace Aerospace Div. (71867) | |
| 2995-00-126-6109 2995001266109 | C4P10617-7 | Lever Assembly, Throttle | III End Item Identification: C-7A acft General Characteristics Item Description: Consists of lever P/N C4P10606-3;2 washers P/N C4P10609-5;SIDE plate P/N C4P10611-3;PLATE support P/N C4P10682-1, P/N C4P10682-3;1 roll pin MS16562-36;SPRING MS24586-95;7 screws AN507-440-8;3 rivet AN507-440-14;3 screws AN507-440-20;6 washers an 960PD41;6 nut NAS679A04 III Fsc Application Data: Control assy, engine C4P10160-5 | Bombardier Aerospace Aerospace Div. (71867) Monterey Peninsula Engineering (0HZW3) | |
| 2995-00-126-6110 2995001266110 | C4P10617-8 | Lever Assembly, Throttle | III End Item Identification: C-7A acft General Characteristics Item Description: Consists of lever P/NC4P10606-4;2 washer P/N C4P10609-5;SIDE plate P/N C4P10611-3;PLATE support P/N C4P10682-1, C4P10682-3;ROLL pin MS16562-36;SPRING MS24586-95;7 screw AN507-440-8;3 rivet AN507-440-14;3 screw an 507-440-20;6 washer AN960PD41;6 nut NAS679A04 III Fsc Application Data: Control assy, engine P/N C4P10160-5 | Bombardier Aerospace Aerospace Div. (71867) DE Havilland Inc. (0HWZ3) | |
| 2995-00-127-4128 2995001274128 | LM-307-SA9 | Parts kit, Mount, Fie | Lord Corporation (76005) | ||
| 2995-00-127-7487 2995001277487 | C297892 | Control Assembly | III End Item Identification: Aircraft model AV-8C | British Aerospace Military (K0289) BAE Systems Operations LTD (U9143) |