Part Number
Definition:
AN ITEM DESIGNED TO INCLOSE, SUPPORT OR PROTECT THE INTERNAL PARTS OF A FUEL PUMP. IT MAY BE FABRICATED FROM A SINGLE CASTING OR COMPOSED OF TWO OR MORE SEPARATE PARTS. USUALLY CONTAINS ACCESS HOLES TO FACILITATE INSTALLATION OF COMPONENT PARTS. MAY INCLUDE ACCESS COVERS, BUSINGS, DOWELL PLUGS- AND THE LIKE. EXCLUDES: HOUSING, LIQUID PUMP.
CAGE Information
| Code | Company |
|---|---|
| 81982 | HYDRO-AIRE INC. |
Federal Supply Class
Title
ENGINE FUEL SYSTEM COMPONENTS, A
Inclusions:
INCLUDES CARBURETORS; FUEL PUMPS; ENGINE FUEL FILTERS; FUEL CONTROLS, JET ENGINE; FUEL PRIMERS; WATER INJECTION CONTROLS AND VALVES; FUEL VALVES FUEL FLOW REGULATORS; COMPONENTS OF SMOKE ABATEMENT SYSTEMS.
Exclusions:
EXCLUDES AIRCRAFT FUEL TANKS (FSC 1560); IN-FLIGHT REFUELING SYSTEM FUEL COMPONENTS (FSC 1680). FUEL SYSTEM COMPONENTS NOT SPECIFICALLY DESIGNED FOR USE WITH AIRCRAFT ENGINES OR MISSILE PRIME-MOVERS.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| MEDA | MEDIA FOR WHICH DESIGNED | FUEL, JET |
| CYDT | ENGINE MODEL NUMBER FOR WHICH DESIGNED | C-130 |
| AGAV | END ITEM IDENTIFICATION | C-130 |
| CYDS | ENGINE DESIGN CONTROL ACTIVITY | 98897 |
| FEAT | SPECIAL FEATURES | T.O.6J10-3-101-4;C/O INSERT P/N R908SB10,LOCK RING P/N RL38SB9,HOUSING ANODIZED P/N 60-36910-11 |
| CYDV | PUMP DESIGN CONTROL ACTIVITY | 81982 |
| CQRG | BODY MATERIAL | ALUMINUM ALLOY |
| ALBY | USAGE DESIGN | AIRCRAFT ENGINE ACCESSORY |