Part Number
Part Number:
NSN:
NIIN:
Item Name:
WEB , STRUCTURAL COMPONENT , AIRCRAF
Definition:
AN ITEM DESIGNED AS A PRINCIPAL MEMBER OF VARIOUS PRIMARY STRUCTURES WITHIN AN AIRCRAFT. IT PROVIDES STRENGTH, RIGIDITY AND THE LIKE WHILE MAINTAINING THE PROPER DIMENSIONAL DISTANCES AS REQUIRED. IT MAY INCLUDE HOLES FOR MOUNTING AND/OR JOINING TO OTHER ITEMS 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 |
|---|---|---|
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | WEB ASSY |
| ABMK | OVERALL WIDTH | 4.600 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | C/O -16, -17; CLAD 2024 SH; T3 TEMP; USED ON -9, -10; DIMENSIONS ARE STOCKSIZE; FINISH F-2.10 |
| CZDJ | AIRCRAFT LOCATION | OUTBOARD AILERON |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | KC-135 |
| AGAV | END ITEM IDENTIFICATION | KC-135 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| ABHP | OVERALL LENGTH | 17.200 INCHES NOMINAL |
| CZEJ | AIRCRAFT STATION NUMBER | WS835.10 |
| ABPX | MATERIAL THICKNESS | 0.016 INCHES NOMINAL |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |