Part Number
Part Number:
NSN:
NIIN:
Item Name:
PLATE , STRUCTURAL , AIRCRAFT
Definition:
A FLAT OR PREFORMED ITEM OF METALLIC OR NONMETALLIC MATERIAL. IT MAY VARY IN SHAPE AND ITS SURFACE MAY BE SMOOTH AND/OR SERRATED. ITS THICKNESS IS SMALL IN COMPARISON TO BOTH ITS LENGTH AND WIDTH. IT IS DESIGNED TO BE MOUNTED UPON A SURFACE OR BETWEEN TWO SURFACES. ITS PRIMARY FUNCTION IS TO STRENGTHEN, JOIN, OR SEPARATE AIRCRAFT STRUCTURAL PARTS. EXCLUDES PLATE, MENDING; SHIM; AND SPACER, PLATE.
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 |
|---|---|---|
| ABHP | OVERALL LENGTH | 5.470 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.850 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | SUPPORT NO. 1 & 2 SPOILER, WING PANEL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
| ABMK | OVERALL WIDTH | 4.810 INCHES NOMINAL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| FEAT | SPECIAL FEATURES | NHA L1600042 SUITABLE FOR B-1B 83-0065 THRU 86-0140 (ACFT 2 THRU 100); HEAT TREAT T7351; ALUM PLATE; DIM. ARE STOCKSIZE |
| AGAV | END ITEM IDENTIFICATION | B-1B |