National Stock Number (NSN) Output Data
Definition:
A DEVICE DESIGNED TO CONVERT ENERGY, FROM AN EXTERNAL SOURCE, TO A CONTROLLED MECHANICAL FORCE, IN THE FORM OF EITHER LINEAR (STRAIGHT LINE) OR ROTATIONAL MOVEMENT. EXCLUDES HYDRAULIC AND PNEUMATIC CYLINDERS, ACTUATOR, ELECTRICAL-MECHANICAL AND SCREWJACK.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 65-74038-49 | 81205 | A | 3 | 2 | 2 | MF | ||
| 65-74038-47 | 81205 | A | 5 | 2 | 2 | MF |
CAGE Information
| Code | Company |
|---|---|
| 81205 | THE BOEING COMPANY DBA BOEING DIV DE |
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 |
|---|---|---|
| ADAT | BODY WIDTH | 4.060 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | MANUFACTURERS SUGGESTED NAME - MECHANISM ASSY, INBOARD AILERON TAB CONTROL (LEFT HANF) |
| ADAQ | BODY LENGTH | 40.400 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | CONSISTS OF DRUM HOUSING, BRAKE ASSY, BALL JACKSRCREW, AND A SPRING CARTRIDGE ASSY. THE MECHANISM HOUSING CONTAINS THE CABLE DRUM, BRAKE MECHANISM AND SHAFT. THE CABLE DRUM IS CONNECTED DIRECTLY TO THE SHAFT. THE CABLE DRUM RECEIVES ROTARY MOTION FROM THE CONTROL CABLE SYSTEM AND CONVERTS IT TO ALINEAR FORCE WHICH POSITIONS THE INBOARD AILERON TRIM TAB. A FLANGE FLAT, NORMAL TO THE LENGTH OF THE SHAFT, ENGAGES THE BRAKING MECHANISM. THE BRAKING MECHANISM PROVIDES ROTATION IN ONE DIRECTION TO PREVENT LOSS OF AILERON TRIM |
| APGF | DESIGN TYPE | LINEAR |