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 |
|---|---|---|
| CZDJ | AIRCRAFT LOCATION | DRAG SHEAR LUG-COWL PANEL ASSEMBLY ENGINE NACELLE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | E-3 |
| ABHP | OVERALL LENGTH | 2.500 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | NEXT HIGHER ASSEMBLY,204-70045;MACHINE FROM CRES BAR,15-5PH PER AMS 5659;HEAT TREAT TO 180-200KSI,PER BAC 5619;PENETRANT INSPECT PER BAC 5423;FINISH F-8.07 + SRF 12.205 |
| MATT | MATERIAL | STEEL CORROSION RESISTING |
| ABMK | OVERALL WIDTH | 2.000 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 1.000 INCHES NOMINAL |