Part Number
Definition:
A FIXTURE DESIGNED TO HOLD/POSITION AIRCRAFT ENGINE/ENGINE COMPONENTS TO FACILITATE INSPECTION, MAINTENANCE, REPAIR, TESTING AND/OR REPLACEMENT OF COMPONENTS.
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 |
---|---|---|
FEAT | SPECIAL FEATURES | DRAWING NAME=FIXTURE,HEAT TREAT-INNER FAIRING, INTERMEDIATE CASE |
PKWT | UNPACKAGED UNIT WEIGHT | 277.000 POUNDS |
FTLD | FUNCTIONAL DESCRIPTION | FIXTURE IS REQUIRED TO CONSTRAIN THE PROXIMATE SPLITTER INNER FAIRING P/N 4054220 DURING A HEAT TREAT CYCLE AFTER PLUG WELDING OF DAMAGED MOUNTING HOLE THREADS. CIP TASK 311-80 |
RDAL | REFERENCE DATA AND LITERATURE | F33657-97-C-0017 SERD 8627 |
AGAV | END ITEM IDENTIFICATION | F100-PW-100-200-220-220E |
CYAG | NOMINAL OVERALL HEIGHT | 7.000 INCHES |
CZDH | NOMINAL OVERALL DIAMETER | 30.000 INCHES |