Part Number
Definition:
A DEVICE FOR MAINTAINING CONTROL OF AN AIRCRAFT ABOUT ITS ROLL AXIS. IT MAY BE OF VARIOUS SHAPES BUT IT MUST HAVE A PIVOT POINT FROM WHICH ROTARY MOTION MAY BE OBTAINED. IT MAY BE INTERCONNECTED TO OTHER COMPONENTS TO ALLOW SIMULTANEOUS CONTROL OF THE AIRCRAFT ABOUT ITS TURN (YAW) AXIS. EXCLUDES WHEELS USED FOR THE OPERATION OF TRIM TABS OR THE LIKE. IT IS A PART OF A CONTROL COLUMN, AIRCRAFT.
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 |
|---|---|---|
| FEAT | SPECIAL FEATURES | ALUMINUM ALLOY,AMS 4135,ALLOY 2014; 2.630 IN.,0.730 C TO C DIST BTWN HOLES,0.250 IN. DIA SMALLER HOLE |
| AGAV | END ITEM IDENTIFICATION | ACFT MODEL B52 |