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 |
|---|---|---|---|---|---|---|---|---|
| 74J658016-205 | 76301 | A | 5 | 2 | 1 | KE | ||
| 7-45281-8 | 78710 | A | 3 | 2 | 5 | KE |
CAGE Information
| Code | Company |
|---|---|
| 76301 | BOEING COMPANY THE DBA BOEING |
| 78710 | TRIUMPH CONTROLS LLC DBA TRIUMPH CON |
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 |
|---|---|---|
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| FEAT | SPECIAL FEATURES | PART OF 2 PIECE FLEX CABLE CONN UPLATCH TO CONTRL HANDLE |
| AGAV | END ITEM IDENTIFICATION | F-18 E/F |
| ABNZ | EFFECTIVE LENGTH | 312.300 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | CONTROL ASSEMBLY, PUSH-PULL-ARRESTING HOOK UPLATCH |