Part Number
Definition:
A CABINETLIKE ITEM USUALLY WITH A FRONT WORK AREA AND CONSISTING OF THE NECESSARY INSTRUMENTATION, MECHANICAL AND ELECTRICAL FACILITIES FOR COMPONENT MOUNTING. DESIGNED TO TEST EFFICIENCY OF PACKAGED HYDRAULIC AND PNEUMATIC PRESSURE AND ELECTRIC POWER GENERATING EQUIPMENT. COMPONENT UNDER TEST IS EQUIPPED WITH SELF CONTAINED POWER SOURCE. EXCLUDES TEST STAND, HYDRAULIC SYSTEM COMPONENT; TEST STAND, ELECTRIC; AND HYDRAULIC SYSTEM COMPONENTS.
CAGE Information
Code | Company |
---|---|
05172 | AAI CORPORATION DIV MISSISSIPPI OPER |
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 |
---|---|---|
FTLD | FUNCTIONAL DESCRIPTION | USED TO TEST MANY HYDRAULIC SERVOCYLINDER COMPONENTS OF THE SPOILER PANELS, HORIZONTAL STABILIZER, BENDING OSCILLATING CONTROLS, RUDDERS, STABILITYAND CONTROL AUGMENTATION SUBSYSTEMS, WEAPONS BAY DOOR POWER DRIVE UNIT, AND FLAP/SLAT POWER CONTROL UNIT |
FEAT | SPECIAL FEATURES | C/O:CRT, CONTROL PANEL, PLOTTER, ELECTRIC INTERFACE PORTS, POWER SUPPLY, HYDRAULIC INTERFACE PORTS, UNIVERSALSERVOVALVE TEST MANIFOLD |
AGAV | END ITEM IDENTIFICATION | FLIGHT CONTROL SYSTEM |