Part Number
Part Number:
NSN:
NIIN:
Item Name:
STIFFENER , AIRCRAFT
Definition:
AN ITEM, GENERALLY A STRIP, DESIGNED TO STRENGTHEN AND RESIST LOADS BY ATTACHMENT TO VARIOUS COMPONENTS SUCH AS SKINS, RIBS, PYLONS, AND THE LIKE.
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 | OUTBOARD AILERON |
| FEAT | SPECIAL FEATURES | T4 TEMP; FINISH F-2.30; DIMENSIONS ARE STOCKSIZE; AND10134-0602; USED ON -9; OPPOSITE -14 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | KC-135 |
| AGAV | END ITEM IDENTIFICATION | KC-135 |
| ABHP | OVERALL LENGTH | 3.500 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | STIFFENER |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| CZEJ | AIRCRAFT STATION NUMBER | WS835.10 |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |