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 |
|---|---|
| 98748 | AIR FORCE UNITED STATES DEPARTMENT O |
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 |
|---|---|---|
| CZDJ | AIRCRAFT LOCATION | DOOR ASSY,WHEEL WELL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-52 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| AGAV | END ITEM IDENTIFICATION | B-52 ACFT |
| FEAT | SPECIAL FEATURES | FABRICATE ITEM BY TRIMMING 24-1517-3,SIZE 31.0 X 2.0 X .090; U/O -10, -30, -50 |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | UPPER CHORD |