Part Number
Definition:
A DEVICE OF VARIOUS SHAPES TO BE PERMANENTLY ATTACHED TO THE STRUCTURE OF AN AIRCRAFT. IT IS DESIGNED TO PERMANENTLY MOUNT AND/OR SUPPORT AN INTEGRAL MEMBER, OR GROUP OF MEMBERS OF THE AIRFRAME IN A PROPER POSITION AND BEAR THE STRESS IMPOSED BY THE COMPONENTS BEING SUPPORTED. IT MAY HAVE MOUNTING PROVISIONS, SUCH AS SLOTS, HOLES, AND/OR ATTACHMENTS TO FACILITATE INSTALLATION. EXCLUDES ITEMS WHICH ARE PRIMARILY DESIGNED FOR DAMPENING SHOCK AND/OR VIBRATION. EXCLUDES BRACKET, ANGLE; BRACKET, DOUBLE ANGLE; BRACKET, SHELF; BRACKET, MOUNTING; AND BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT.
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 |
---|---|---|
FEAT | SPECIAL FEATURES | HEAT TREAT T42;FINISH F-2.115; NHA 65-1349 |
ABPX | MATERIAL THICKNESS | 0.050 INCHES NOMINAL |
CZDJ | AIRCRAFT LOCATION | AFT ENTRY DOOR LINING ATTACHMENT ANGLE |
CZEK | AIRCRAFT MISSION DESIGN SERIES | E-3A |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE |
ABMK | OVERALL WIDTH | 2.300 INCHES NOMINAL |
ABHP | OVERALL LENGTH | 30.000 INCHES NOMINAL |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |