Part Number
Definition:
A FIXTURE DESIGNED TO HOLD/POSITION AIRCRAFT COMPONENTS TO FACILITATE INSPECTION, REPAIR, TESTING AND/OR REPLACEMENT OF COMPONENTS. D0 NOT USE IF A MORE SPECIFIC NAME APPLIES. SEE FIXTURE (1) (AS MODIFIED).
CAGE Information
| Code | Company |
|---|---|
| 07482 | GENERAL ELECTRIC COMPANY DBA GE DIV |
Federal Supply Class
Title
AIRCRAFT MAINTENANCE AND REPAIR
Inclusions:
INCLUDES MAINTENANCE STANDS DESIGNED FOR SUPPORT OF AIRCRAFT ASSEMBLIES DURING REPAIR OR OVERHAUL; TEST STANDS AND TEST EQUIPMENT SPECIALLY DESIGNED FOR MAINTENANCE AND REPAIR OF AIRCRAFT COMPONENTS SUCH AS: ENGINES, GENERATORS, HYDRAULIC SYSTEMS, ARMAMENT, AUTOMATIC PILOT, FIRE CONTROL, FLIGHT CONTROL, AND NAVIGATIONAL SYSTEMS.
Exclusions:
EXCLUDES HAND TOOLS; AIRFIELD MAINTENANCE PLATFORMS; BASIC TYPES OF ELECTRICAL AND ELECTRONIC TEST INSTRUMENTS, INCLUDING THOSE SPECIALLY DESIGNED, SUCH AS AMMETERS, VOLTMETERS OHMMETERS, MULTIMETERS, AND SIMILAR INSTRUMENTS, AS SHOWN IN THE INDEXES TO THE FSC; TEST APPARATUS USED FOR BOTH COMMUNICATIONS AND OTHER ELECTRICAL AND ELECTRONIC EQUIPMENT.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| RDAL | REFERENCE DATA AND LITERATURE | TO 2J-J85-94 |
| AGAV | END ITEM IDENTIFICATION | J85-GE-21/-21A TURBOJET ENGINE |
| FEAT | SPECIAL FEATURES | NC/O STEEL Y SHAPED PLATE W/SUB ASSY FASTENED TO EACH ARM. ONE SUB-ASSY IS A FIXTURE TO HOLD THE STAGE 1 TURBINE BLADE,THE SECOND FIXTURE IS THE STAGE 2 TURBINE BLADE AND THE THIRD IS A GRINDING WHEEL DRESSING UNIT |