Part Number
Part Number:
NSN:
NIIN:
Item Name:
WEB , STRUCTURAL COMPONENT , AIRCRAF
Definition:
AN ITEM DESIGNED AS A PRINCIPAL MEMBER OF VARIOUS PRIMARY STRUCTURES WITHIN AN AIRCRAFT. IT PROVIDES STRENGTH, RIGIDITY AND THE LIKE WHILE MAINTAINING THE PROPER DIMENSIONAL DISTANCES AS REQUIRED. IT MAY INCLUDE HOLES FOR MOUNTING AND/OR JOINING TO OTHER ITEMS TO FORM AN ASSEMBLY.
CAGE Information
| Code | Company |
|---|---|
| 76301 | BOEING COMPANY THE DBA BOEING |
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 |
|---|---|---|
| CZEJ | AIRCRAFT STATION NUMBER | FS 570.0 TO FS 695.0 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046 MIL SPEC SINGLE MATERIAL RESPONSE |
| AGAV | END ITEM IDENTIFICATION | F/A18-E/F FIGHTER AIRCRAFT |
| CZDJ | AIRCRAFT LOCATION | AFT FUSELAGE |
| ABMK | OVERALL WIDTH | 4.750 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | WEB,STRUCTURAL COMPONENT (INAVY); KEEL WEB, LOWER 591.500 TO 631.250, AFT FUS (DRAWING NAME) |
| ABHP | OVERALL LENGTH | 13.000 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F/A18-E/F |
| ASXK | HOLE QUANTITY | 31 |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| ABPX | MATERIAL THICKNESS | 0.063 INCHES NOMINAL |
| MATT | MATERIAL | TITANIUM ALLOY |