FSC 2995 Miscellaneous Aircraft Engine Accessories: 2995-00-253-3299, 2995-00-276-1567, 2995-00-276-7497
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2995-00-253-3299 2995002533299 | HL8167-1 | Friction Disc, Stat | General Characteristics Item Description: Cres MIL&S&5059 composition 301 condition 1-4 hard, 0.032 in. thk, 1.130 in. dia of center hole | Rockwell Collins Electromechanical (86831) Dover Diversified DE Inc. (78062) | |
| 2995-00-253-7680 2995002537680 | 11A12265A | Lever Assembly | III End Item Identification: Aircraft model A-3, F-8 | Goodrich Corporation (11599) | |
| 2995-00-257-5937 2995002575937 | 1200483-101 | Cover, Throttle | General Characteristics Item Description: Nylon, irregularly shaped 7.000 in. lg, 1.234 in. W.0.240 in. thk III Fsc Application Data: Throttle control acft engine | Lockheed Martin Corporation (98897) | |
| 2995-00-257-5938 2995002575938 | 1200483-102 | Cover, Throttle | General Characteristics Item Description: Nylon, irregularly shaped 7.000 in. lg, 1.234 in. W, 0.240 in. thk III Fsc Application Data: Throttle control acft engine | Lockheed Martin Corporation (98897) Williams Aerospace & Manufacturing (3P104) | |
| 2995-00-257-8032 2995002578032 | 7-42484-5 C81900-5 C81900-10 68B658000-105 7-42484-10 | Control Assemble, Throttle | III End Item Identification: Model F15 acft General Characteristics Item Description: 0.527 in. min stroke capacity III Fsc Application Data: Control assembly, push & pull, acft engine | Boeing Company, The (76301) Transdigm Inc. (04638) Triumph Controls LLC (78710) | |
| 2995-00-257-8033 2995002578033 | 7-42484-2 C81900-13 68B658000-102 7-42484-13 7-42484-8 | Control Assembly, Throttle | III End Item Identification: Model F15 acft General Characteristics Item Description: 0.527 in. min stroke III Fsc Application Data: Control assembly, push & pull, acft engine | Boeing Company, The (76301) Transdigm Inc. (04638) Triumph Controls LLC (78710, 3CW15) | |
| 2995-00-257-8035 2995002578035 | C81900-3 68B658000-109 68B658000-114 7-42484-14 68B658000-103 | Control Assembly, Throttle | III End Item Identification: Model TF15 acft General Characteristics Item Description: 0.527 in. min stroke III Fsc Application Data: Control assembly, push & pull, acft engine | Triumph Controls LLC (78710) Transdigm Inc. (04638) Boeing Company, The (76301) | |
| 2995-00-257-8044 2995002578044 | 6856511 311D928P02 | Control Assembly, Nozzle | III End Item Identification: Model J79 acft engine General Characteristics Item Description: Lever activated III Fsc Application Data: Control, actuator, jet engine, acft | General Electric Company (07482) Parker-Hannifin Corporation (93835) | |
| 2995-00-257-8050 2995002578050 | 6856517 7013M88P01 | Control, Nozzle Clos | III End Item Identification: Model J79 acft engine General Characteristics Item Description: Lever actuated III Fsc Application Data: Control, actuator, jet engine, acft | General Electric Company (07482) Parker-Hannifin Corporation (93835) | |
| 2995-00-260-1236 2995002601236 | S8324A7-7 58324A7-7 | Plug, Passage Hole | III End Item Identification: 2995008399181 housing, actuator, 2995008916356 pressure regulator. pneumatic engine starter, F111 acft. General Characteristics Item Description: Aluminum alloy QQ&A&200-8 or QQ&A&225-8, iridite or anodize, 0.2143 to 0.2163 in od. | Honeywell International Inc. (70210, 99193, 59364) | |
| 2995-00-262-3207 2995002623207 | A28 36E133-2QB MIL-S-19557 36E133-2A 36E133-2B | Starter, Engine, Air Turbine | Drive Type: Spline Air Inlet Connection Type: Band coupler Drive Rotation Direction: Counterclockwise | Naval Air Systems Command (30003) Military Specifications (81349) Goodrich Corporation (99551) | |
| 2995-00-262-4316 2995002624316 | 565378 | Cover, Bleed Actuator, Aircraft En | III End Item Identification: 29951734005 General Characteristics Item Description: Aluminum alloy AMS4212 obsolete or AMS4281 obsolete, 6 mtg holes 0.276 in. min, 0.286 in. max dia equally spaced on 3.750 in. dia bolt circle III Fsc Application Data: Cover, actuator, jet engine, acft | United Technologies Corporation (52661, 77445) | |
| 2995-00-262-4318 2995002624318 | 565379 | Cover, Bleed Actuator, Aircraft En | III End Item Identification: 29951734005 General Characteristics Item Description: Aluminum alloy AMS4212 obsolete or AMS4281 obsolete, 6 mtg holes 0.276 in. min, 0.286 in. max dia equally spaced on 3.750 in. dia bolt circle III Fsc Application Data: Cover, actuator, jet engine, acft | JET Industries Inc. (59593) United Technologies Corporation (77445) The Birken Manufacturing Company (31340) | |
| 2995-00-270-7089 2995002707089 | 2487163 | Head, Mounting | General Characteristics Item Description: Aluminum alloy casting, 6.640 in. od, 4.121 in. id, 6 mtd holes 0.415 in.dia. equally spaced on 5.000 in. dia bolt circle III Fsc Application Data: Starter, engine, air turbine F14A acft | Goodrich Corporation (99551) Parker-Hannifin Corporation (59211, 3H889) | |
| 2995-00-270-7122 2995002707122 | 1201365-101 | Quadrant Assembly, Throttle Contr | General Characteristics Item Description: 6.807 in. dia, 1.750 in. lg III Fsc Application Data: Flight control system acft | Lockheed Martin Corporation (98897) | |
| 2995-00-270-7125 2995002707125 | 1201367-101 | Quadrant Assembly, Throttle Contr | General Characteristics Item Description: Consist of 2 bearing part no. B538DDFS428, fscm 2135, 1 spacer make from part no. 1202651 & 101, fscm 36659, 1 quadrant part no. 1201367 & 103, fscm 36659 III Fsc Application Data: Throttle control engine aircraft | Lockheed Martin Corporation (98897) | |
| 2995-00-276-1567 2995002761567 | 12P4713-17 | Retainer, Stub Duct | Lockheed Martin Corporation (81755) | ||
| 2995-00-276-4994 2995002764994 | 223895-4 5021T80P04 | Valve, Anti-Icing | General Characteristics Item Description: 28 vdc operation Reference Number Differentiating Characteristics: As differentiated by source control dwg fscm 99207 part no. 5021T80P04 | General Electric Company (99207) Whittaker Controls Inc. (79318) | |
| 2995-00-276-5377 2995002765377 | 1200927-101 | Flange, Torque Tube | General Characteristics Item Description: Flange mtg holes 2.185 in. min, 2.188 in. max C to C, 2 holes 0.250 in min, 0.252 in max dia, flange 0.190 in. thk, body od 1.031 in. min, 1.032 in. max body id 0.750, O/a lg 1.630 in. | Lockheed Martin Corporation (98897) | |
| 2995-00-276-7497 2995002767497 | 14-50852-501 | Lever, Manual Control, Quadrant | III End Item Identification: Quadrant assembly, throttle control, acft engine, part NO.114-50826-503FSCM 76823 III Fsc Application Data: Quadrant control, acft engine | Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) |