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 |
|---|---|
| 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 |
|---|---|---|
| ABPX | MATERIAL THICKNESS | 0.025 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | DIM. ARE STOCKSIZE MATL; WIDTH IS 4.63 AT ONE END, OTHER END 10.02 |
| AGAV | END ITEM IDENTIFICATION | KC-135 ACFT |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | KC-135 ACFT |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| CZDJ | AIRCRAFT LOCATION | FUSELAGE |
| ABHP | OVERALL LENGTH | 112.110 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | REAR SPAR, RIGHT |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |