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 |
|---|---|
| 43999 | BOEING COMPANY THE 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 |
|---|---|---|
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12, AL ALY BARE PLATE ALLOY 7075-T7351 FED SPEC SINGLE MATERIAL RESPONSE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SPAR |
| ABMK | OVERALL WIDTH | 3.000 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 2.000 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | SPAR, REAR---SPOILER NO. 2 |
| ABHP | OVERALL LENGTH | 67.700 INCHES NOMINAL |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| FEAT | SPECIAL FEATURES | -004 OPP -003 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B1-B ACFT |