NIIN Output Data
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.
Reference/Part Number
Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
---|---|---|---|---|---|---|---|---|
9692M44P07 | 07482 | A | 1 | 2 | 2 | MB | ||
02-4891-111 | 99167 | A | 3 | 2 | 2 | ZZ | ||
02489-111 | 99167 | A | 5 | 9 | 5 | MB |
CAGE Information
Code | Company |
---|---|
07482 | GENERAL ELECTRIC COMPANY DBA GE DIV |
99167 | HAMILTON SUNDSTRAND CORPORATION |
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 |
---|---|---|
ZZZV | FSC APPLICATION DATA | ACFT ENGINE FUEL PUMP |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 12.910 IN. MIN,13.030 IN. MAX O/A LG |
AGAV | END ITEM IDENTIFICATION | ENGINE,ACFT,TF39GE1A |