NIIN Output Data
Definition:
A CONTROL CONSISTING OF A WIRE, WIRE ROPE, OR A CENTER LOAD RAIL WITH BALL BEARINGS, WITHIN A FLEXIBLE CONDUIT. ONE END MUST HAVE A THREADED SLEEVE FOR MOUNTING TO A WALL, BULKHEAD, OR HANDLE, OR CLEVIS. IT IS USED TO OPERATE OR CONTROL, EITHER MANUALLY OR MECHANICALLY A MECHANICAL DEVICE. IT MAY INCLUDE SUCH ATTACHING DEVICES AS NUT(S), WASHER(S), CLEVIS, BRACKET(S), AND/OR THE LIKE. FOR ITEMS DESIGNED TO TRANSMIT ROTARY MOTION, SEE SHAFT ASSEMBLY, FLEXIBLE.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 749947-103 | 98897 | A | 1 | 2 | 5 | KE | ||
| C80251-2 | 04638 | A | 3 | 2 | 5 | KE |
CAGE Information
| Code | Company |
|---|---|
| 04638 | TRANSDIGM INC AERO CONTROLEX GROUP, |
| 98897 | LOCKHEED MARTIN CORPORATION DBA LOCK |
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 |
|---|---|---|
| CBBL | FEATURES PROVIDED | ADAPTER |
| BCXR | CORE PROCESSED END CONNECTION TYPE | NONADJUSTABLE CONNECTOR AND ADJUSTABLE THREADED ADAPTER |
| BCYK | TRAVEL DISTANCE | 2.500 INCHES NOMINAL |
| ACZR | CORE CONSTRUCTION | WIRE ROPE |
| ZZZV | FSC APPLICATION DATA | FUEL SYSTEM,AIRCRAFT |
| ABNZ | EFFECTIVE LENGTH | 85.250 INCHES MINIMUM AND 85.750 INCHES MAXIMUM |