NIIN Output Data
Definition:
A SELF-CONTAINED POWER TRANSMITTING DEVICE DESIGNED TO CONVERT ROTARY MOTION TO LINEAR (STRAIGHT LINE) MECHANICAL MOVEMENT. MUST BE COMPRISED OF A BALL NUT, PILLOW BLOCK(S), SCREW SHAFT AND SUCH ACCESSORIES AS REQUIRED FOR THE SPECIFIC MOVING AND POSITIONING OF OTHER COMPONENTS.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 4C95016-127E | 98897 | A | 1 | 3 | 5 | MB | ||
| 5901-127E | 78567 | H | 5 | 9 | 5 | MB | ||
| 5901-127E | 98752 | A | 3 | 3 | 5 | ZZ |
CAGE Information
| Code | Company |
|---|---|
| 78567 | SPECO CORP |
| 98897 | LOCKHEED MARTIN CORPORATION DBA LOCK |
| 98752 | WARNER ROBINS AIR LOGISTICS CENTER |
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 |
|---|---|---|
| FEAT | SPECIAL FEATURES | T.O. 16A1-13-18-3; USED ON FLAP ACTUATION SYSTEM, WING P/N 4C65005-101A; OVERALL DIA 5.75 IN.; BALL SCREW DIA1.50 IN.; OVERALL LENGTH 94.449 IN.; NOMINAL TRAVEL 83.0 IN.; LEAD 0.3125 IN. |
| FEAT | SPECIAL FEATURES | T.O. 16A1-13-18-3; USED ON FLAP ACTUATION SYSTEM, WING P/N 4C65005-101A; OVERALL DIA 5.75 IN.; BALL SCREW DIA1.50 IN.; OVERALL LENGTH 94.449 IN.; NOMINAL TRAVEL 83.0 IN.; LEAD 0.3125 IN. |
| CRTL | CRITICALITY CODE JUSTIFICATION | SUPP |
| SUPP | SUPPLEMENTARY FEATURES | FLAP/SLAT ACTUATION CRITICAL TO SAFE OPERATION OF ACFT |
| ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY LOCKHEED SOURCE CONTROL DWG NO. 4C95016-127E |