Part Number
Definition:
A MECHANICAL DEVICE DESIGNED TO BE SECURED TO AN INTERNAL COMBUSTION ENGINE AND USED TO TRANSMIT THE ROTARY MOTION OF THE CRANKSHAFT TO AUXILIARY EQUIPMENT, SUCH AS GENERATORS, CRANES, PUMPS, COMPRESSORS, MIXERS, AND THE LIKE. INCLUDES A POWER OUTPUT SHAFT AND A CLUTCH WHICH MAY BE CONTROLLED BY A HAND LEVER OR A HYDRAULIC OR AIR CYLINDER. MAY INCLUDE PULLEY(S), FLANGE, YOKE OR REDUCTION GEAR UNIT. EXCLUDES VEHICULAR CLUTCHES AND POWER TAKEOFF, TRANSMISSION.
CAGE Information
Code | Company |
---|---|
99207 | GENERAL ELECTRIC COMPANY DBA GE DIV |
Federal Supply Class
Title
MISCELLANEOUS ENGINE ACCESSORIES
Inclusions:
INCLUDES ENGINE DYNAFOCAL SUSPENSION MOUNTS; ENGINE COWLING MOUNTS; ENGINE MOUNTED CONTROL ASSEMBLIES; PNEUMATIC STARTERS; PUSH-PULL CONTROL ASSEMBLIES;SPECIALLY DESIGNED JET ENGINE AIR, OIL, ANTI-ICING AND HYDRAULIC REGULATORS; VALVES AND PUMPS; STARTING UNITS.
Exclusions:
EXCLUDES EXHAUST SYSTEM; (FSC 1560); JET ENGINE HYDRAULIC RESERVOIRS (FSC 2840); JET ENGINE OIL TANKS (FSC 2840); ELECTRICAL STARTERS (FSC 2925); COCKPIT MOUNTED CONTROL QUADRANTS (FSC 1680); AIRCRAFT ENGINE COVERS (FSC 1730).
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
FEAT | SPECIAL FEATURES | TUSED AS COMPRESSOR SECTION COMPONENTS; SEE ALSO, 2J-J85-94, FIG 10, IND 1 |
AGAV | END ITEM IDENTIFICATION | J85-5/7/13/17/17A/21 AIRCRAFT GAS TURBINE ENGINE |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-J85-94, FIG 3, IND 24 |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT AND AGAV |