Aircraft and Missile Prime Movers Engine Fuel System Components: 868522-7, 868C349P18, 86946
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 868522-7 8685227 | 2915-01-151-0832 | Fuel Control, Main, Turbine Engine | III End Item Identification: Engine model T76-G-10, T76-G-12, T76-G-12 a/F Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Edison Machine Co. (99169) | |
| 868560-2 8685602 | 2915-00-013-6877 | Regulator, Fuel Flow, Turbo-Prop E | Honeywell International Inc. (99193) | ||
| 868560-4 8685604 | 2915-00-248-9248 | Regulator, Fuel Flow, Turbo-Prop E | General Characteristics Item Description: Regulates fuel output to engine, 1 outlet to start, 1 outlet to run, 1 outlet to fuel heater, 1 high pressure inlet, 1 metered fuel inlet, 6.735 in. lg, 5.030 in. W, 1.980 in. H O/a dim. III Fsc Application Data: Acft engine fuel system | Honeywell International Inc. (99193) | |
| 868561-4 8685614 | 2915-00-248-9248 | Regulator, Fuel Flow, Turbo-Prop E | General Characteristics Item Description: Regulates fuel output to engine, 1 outlet to start, 1 outlet to run, 1 outlet to fuel heater, 1 high pressure inlet, 1 metered fuel inlet, 6.735 in. lg, 5.030 in. W, 1.980 in. H O/a dim. III Fsc Application Data: Acft engine fuel system | Honeywell International Inc. (99193) | |
| 868752-1 8687521 | 2915-00-894-3164 | Nozzle, Fuel Control | III End Item Identification: Turboprop aircraft engine P/ns 868740-42 and 868740-44 General Characteristics Item Description: Cres, 0.395 in. min, 0.405 in. max lg, 0.307 in. min, 0.313 in. max dia across hex, 0.100 in. min, 0.115 in. max dia other end, 1/4-32 UNEF-2A thd | Honeywell International Inc. (99193) | |
| 868905-1 8689051 | 2915-01-419-6631 | Nozzle, Fuel Injection | Honeywell International Inc. (99193) | ||
| 868906-1 8689061 | 2915-00-894-3154 | Nozzle, Fuel | III End Item Identification: Turboprop aircraft engine P/ns 868740-42 and 868740-44 | Honeywell International Inc. (99193) | |
| 868914-1 8689141 | 2915-00-894-3127 | Nozzle and Manifold | Honeywell International Inc. (99193) | ||
| 868970-1 8689701 | 2915-00-894-3127 | Nozzle and Manifold | Honeywell International Inc. (99193) | ||
| 868C349P15 | 2915-00-064-5662 | Valve, Fuel Pressure | III End Item Identification: Ab fuel control for J79-GE-15, -17 aircraft engine General Characteristics Item Description: Cres; 8.565 in. lg, 1.855 in. H O/a; 2 mtg holes 0.266 in. dia thru, 3.34 in. apart and 1.655 in. dist to endinlet port; 2 inlet ports, 1.3125-12UN-3A thd, 3.25 in. cen-to-cen; one ea primary, secondary annulus ports and primary, secondary core ports, 0.750-16UNF-3A thd | General Electric Co. (24446) General Electric Company (07482) | |
| 868C349P17 | 2915-00-064-5662 | Valve, Fuel Pressure | III End Item Identification: Ab fuel control for J79-GE-15, -17 aircraft engine General Characteristics Item Description: Cres; 8.565 in. lg, 1.855 in. H O/a; 2 mtg holes 0.266 in. dia thru, 3.34 in. apart and 1.655 in. dist to endinlet port; 2 inlet ports, 1.3125-12UN-3A thd, 3.25 in. cen-to-cen; one ea primary, secondary annulus ports and primary, secondary core ports, 0.750-16UNF-3A thd | General Electric Company (07482) | |
| 868C349P18 | 2915-00-927-4538 | Valve, Fuel Pressurizing and Drai | III End Item Identification: Jet engines J79 Special Features: This fuel pressure valve has a critical tolerance, fit restriction, and application III Part Name Assigned By Controlling Agency: Valve, fuel, pressurizing | General Electric Company (07482) | |
| 868C729P2 | 2915-00-962-1274 | Cover, Valve, Fuel Pressurizing | III End Item Identification: Valve, pressurising and drain, fuel P/N 868C842G2 | General Electric Co. (24446) General Electric Company (07482) | |
| 868C842G2 | 2915-00-446-2817 | Valve, Fuel Pressurizing and Drai | III End Item Identification: Engine, aircraft, model J79-8, J79-8A, J79-15 | General Electric Co. (24446) General Electric Company (07482) | |
| 868C996P1 | 2915-00-573-0920 | Filter, Fluid | III Fsc Application Data: Engine fuel system components, acft Special Features: This filter has a critical tolerance, fit restriction, and application Material: Steel corrosion resisting filtering medium aluminum alloy sediment bowl | General Electric Company (07482) | |
| 868C996P2 | 2915-00-573-0920 | Filter, Fluid | III Fsc Application Data: Engine fuel system components, acft Special Features: This filter has a critical tolerance, fit restriction, and application Material: Steel corrosion resisting filtering medium aluminum alloy sediment bowl | General Electric Company (07482) | |
| 869005-1 8690051 | 2915-00-894-3170 | Manifold Assembly, Fuel | III End Item Identification: T76-101-12 turboprop aircraft engine General Characteristics Item Description: CRES | Honeywell International Inc. (99193) | |
| 869021-3 8690213 | 2915-01-284-3677 | Manifold | Honeywell International Inc. (99193) | ||
| 869022-1 8690221 | 2915-00-894-3170 | Manifold Assembly, Fuel | III End Item Identification: T76-101-12 turboprop aircraft engine General Characteristics Item Description: CRES | Honeywell International Inc. (99193) | |
| 86946 | 2915-00-024-5989 | Cover, Retaining, Coarse | General Characteristics Item Description: Aluminum alloy ams 4135, 2.60 in. dia, 0.78 in. thk | Hamilton Sundstrand Corporation (73030) |