Part Number
Part Number:
NSN:
NIIN:
Item Name:
BRACKET , STRUCTURAL COMPONENT , AIR
Definition:
AN ITEM OF VARIOUS CONFIGURATION THAT IS AN INTEGRAL MEMBER OF THE AIRFRAME STRUCTURE. IT IS SPECIFICALLY DESIGNED FOR THE PURPOSE OF MAINTAINING, POSITIONING, JOINING, AND STRENGTHENING THE AIRCRAFT STRUCTURE. IT MAY INCLUDE HOLES FOR MOUNTING PURPOSES OR TO FORM AN ASSEMBLY.
CAGE Information
Code | Company |
---|---|
81205 | THE BOEING COMPANY DBA BOEING DIV DE |
Federal Supply Class
Title
AIRFRAME STRUCTURAL COMPONENTS
Inclusions:
INCLUDES FLIGHT CONTROL SURFACES; INTERNAL AND EXTERNAL AUXILIARY FUEL TANKS; EXHAUST SYSTEMS; PYLONS, TRIM TABS; AIRCRAFT.
Exclusions:
EXCLUDES FITTED COVERS; HELICOPTER ROTOR BRAKE SYSTEM COMPONENTS; AIRCRAFT LOOSE EQUIPMENT AND ALTERNATE MISSION CONFIGURATION EQUIPMENT STORED ON BOARD THE AIRCRAFT.
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
ABPX | MATERIAL THICKNESS | 0.750 INCHES NOMINAL |
CZDJ | AIRCRAFT LOCATION | LEADING EDGE, WING BOX |
AGAV | END ITEM IDENTIFICATION | F-22 RAPTOR |
ABMK | OVERALL WIDTH | 2.500 INCHES NOMINAL |
FEAT | SPECIAL FEATURES | OVERALL WIDTH & MATERIAL THICKNESS DIM. ARE STOCK MATERIAL; M/O 7050-T7451 ALUM PLATE, HT ALUM ALLOY PER AMS2770 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4050 ASSN STD SINGLE MATERIAL RESPONSE |
CZEK | AIRCRAFT MISSION DESIGN SERIES | OPPOSITE -101; OVERALL WIDTH & MATERIAL THICKNESS DIM. ARE STOCK MATERIAL; M/O 7050-T7451 ALUM PLATE, HT ALUM ALLOY PER AMS2770 |
ABHP | OVERALL LENGTH | 4.000 INCHES NOMINAL |
MATT | MATERIAL | ALUMINUM ALLOY 7050 |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | BRACKET |