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 |
|---|---|
| 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 |
|---|---|---|
| FEAT | SPECIAL FEATURES | FINISH F-8.05;HEAT TREAT T62 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | E-3A |
| ABPX | MATERIAL THICKNESS | 0.040 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 65.000 INCHES NOMINAL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE |
| CZDJ | AIRCRAFT LOCATION | SIDE COWL ENGINE NACELLE PANEL |
| BWJF | SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| ABHP | OVERALL LENGTH | 70.000 INCHES NOMINAL |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |