NIIN Output Data
Definition:
AN ASSEMBLY OF GEARS, SHAFT AND BEARINGS WITHIN A HOUSING. IT MAY OR MAY NOT BE DESIGNED TO CHANGE DIRECTION OR ROTARY MOTION OR HAVE A TORQUE DIFFERENTIAL FROM INPUT OR OUTPUT. MAY INCLUDE A HYDRAULIC MOTOR, BRAKE AND THE LIKE. EXCLUDES GEARBOXES THAT ARE TURBINE ENGINE DRIVEN.
Reference/Part Number
Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
---|---|---|---|---|---|---|---|---|
5901-108D | 98752 | A | 1 | 3 | 5 | ZZ | ||
4C95016-108D | 98897 | A | 5 | 9 | 2 | SE | ||
5901-108D | 5H860 | A | 3 | 3 | 5 | ZZ | ||
5901-108D | 78567 | H | 5 | 9 | 5 | ZZ |
CAGE Information
Code | Company |
---|---|
5H860 | THOMAS INSTRUMENT & MACHINE CO. INC. |
98752 | WARNER ROBINS AIR LOGISTICS CENTER |
98897 | LOCKHEED MARTIN CORPORATION DBA LOCK |
78567 | SPECO CORP |
Federal Supply Class
Title
MISCELLANEOUS AIRCRAFT ACCESSORI
Inclusions:
INCLUDES CONTROL ASSEMBLIES, PUSH-PULL; BRACE, POSITIONING CARGO RAMP STOWED ON BOARD; COCKPIT MOUNTED CONTROL QUADRANTS; ACTUATORS, ELECTRO-MECHANICAL AND MECHANICAL; VENTILATORS; RELIEF TUBES; MAP HOLDERS; AERIAL GLIDER TOWING ACCESSORIES ATTACHED TO AIRCRAFT; BELTS, SAFETY AND LAP; HARNESS, SHOULDER AND SAFETY; LITTER ATTACHING SUPPORTS;ELECTRIC WINDSHIELD WIPERS;AIRCRAFT ONBOARD INERT GAS GENERATORS;AIRCRAFT FURNITURE;AIRCRAFT MOUNTED WINCHES AND HOISTS;IN-FLIGHT REFUELING SYSTEM COMPONENTS, INCLUDING FUEL COMPONENTS;AIRCRAFT CURTAINS;CABLE TENSION REGULATORS;SUN VISORS;REAR-VIEW MIRRORS;MECHANICAL TRANSMISSIONS, GEARBOXES AND CONSTANT SPEED DRIVES SPECIALLY DESIGNED FOR AIRCRAFT.
Exclusions:
EXCLUDES ENGINE MOUNTED CONTROL ASSEMBLIES; FITTED COVERS, AIRCRAFT PYLONS; HELICOPTER ROTER BRAKE SYSTEM COMPONENTS; HELICOPTER AUTOMATIC STABILIZATION EQUIPMENT.
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS (NON-CORE) | LOCKHEED SOURCE CONTROL DWG NO. 4C95016-108D |
ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS (NON-CORE) | LOCKHEED SOURCE CONTROL DWG NO. 4C95016-108D |
CZDJ | AIRCRAFT LOCATION | TRAILING EDGE FLAP |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
FEAT | SPECIAL FEATURES | FLAP/SLAT ACTUATOR CRITICAL TO OPERATION OF AIRCRAFT. |