Part Number
Definition:
A DEVICE SPECIFICALLY DESIGNED TO DELIVER FUEL TO A JET ENGINE. THE DEVICE MAY BE OF SINGLE/MULTISTAGE AND POSITIVE/NONPOSITIVE DISPLACEMENT DESIGN. IT MOUNTS ON A JET ENGINE ACCESSORY DRIVE CASE OR ON THE FUEL CONTROL AND IS DRIVEN BY THE ENGINE. EXCLUDES ALL PUMPS NOT SPECIFICALLY DESIGNED TO BE USED ON A JET ENGINE.
CAGE Information
| Code | Company |
|---|---|
| 82918 | THE BOEING COMPANY GLOBAL SERVICES & |
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 |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | T62T40LC2 FUEL SYSTEM |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 11.400 INCH LONG;4.600 INCH ID;4 PLACES 0.281 INCH DIA THRU;HARDNESS CRITICAL ITEM HCI |
| FEAT | SPECIAL FEATURES | CONTAINS HARDNESS CRITICAL ITEMS OR PROCESSES;ALL CHANGES TO ITEMS OR WHETHER ANNOTATED OR NOT ON THE DRWGS PICTORIAL OR PARTS LIST MUST BE EVALUATED FOR HARDNESS IMPACT |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |