Part Number
Definition:
A FIXTURE DESIGNED TO HOLD AIRCRAFT ENGINE OR AUXILIARY POWER UNIT INDIVIDUAL PARTS, SUBASSEMBLIES, OR ASSEMBLIES IN POSITION FOR MACHINING TO DESIGN TOLERANCES DURING MODIFICATION OR REPAIR.
CAGE Information
Code | Company |
---|---|
77445 | UNITED TECHNOLOGIES CORPORATION DBA |
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 |
---|---|---|
CZDH | NOMINAL OVERALL DIAMETER | 21.000 INCHES |
CYAG | NOMINAL OVERALL HEIGHT | 2.500 INCHES |
AGAV | END ITEM IDENTIFICATION | F100-PW-229 ENGINE |
RDAL | REFERENCE DATA AND LITERATURE | SERD 9304 |
FTLD | FUNCTIONAL DESCRIPTION | REQUIRED FOR PLASMA SPRAY REPAIR OF 2ND STAGE TURBINE RETAINING PLATE AT A WORN INNER SNAP DIAMETER AND AFT FACE THAT CONTACT TURBINE BLADE RETAINIG PLATE AT ENGINE ASSEMBLY. LOCATES AND CLAMPS OUTER DIAMETER FLANGE OF RETAINING PLATE DURING MACHINING OF INNER DIAMETER REPAIR AREAS |
PKWT | UNPACKAGED UNIT WEIGHT | 40.000 POUNDS |