Part Number
Part Number:
NSN:
NIIN:
Item Name:
SPAR , AIRCRAFT
Definition:
A PRINCIPAL SPANWISE MEMBER OF THE STRUCTURAL FRAMEWORK OF A WING, STABILIZER, OTHER AIRFOIL, AND THE LIKE. IT IS DESIGNED TO ABSORB BENDING LOADS APPLIED TO THE AIRFOIL.
CAGE Information
| Code | Company |
|---|---|
| 82918 | THE BOEING COMPANY GLOBAL SERVICES & |
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 | SPAR |
| AGAV | END ITEM IDENTIFICATION | KC-135 ACFT |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | KC-135 ACFT |
| CZDJ | AIRCRAFT LOCATION | INBOARD AILERON |
| FEAT | SPECIAL FEATURES | T6 EXTR; T6 TEMP; FINISH F2.30; BAC1518-222 X 30.5; USED ON 586074; DIM. ARE STOCKSIZE MATL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-277 FED SPEC SINGLE MATERIAL RESPONSE |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 AND ALUMINUM ALLOY 7075 |
| ABHP | OVERALL LENGTH | 30.500 INCHES NOMINAL |