Part Number
Definition:
A PREFORMED ITEM WHICH MAY BE ANY SHAPE, HAVING A SANDWICH OR HONEYCOMB CORE BONDED TO A METALLIC OR NONMETALLIC FACING MATERIAL. IT IS USED TO ENCLOSE ANY PORTION OF THE FUSELAGE OR TO FABRICATE PARTITIONS OR COMPARTMENTS WITHIN A WING, EMPENNAGE, FUSELAGE OR NACELLE. IT MAY HAVE HOLES DRILLED OR CUT TO ACCOMMODATE ITEMS, BUT WILL HAVE NO ITEMS MOUNTED ON IT, EXCEPT BRACKET(S) OR OTHER FACILITIES FOR ITS OWN MOUNTING OR SUPPORT. IT MAY BE MOUNTED BY FASTENERS, BONDING, OR WELDING. EXCLUDES COVER, ACCESS; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL; COVER, ACCESS, GUIDED MISSILE; PANEL, STRUCTURAL, AIRCRAFT.
CAGE Information
| Code | Company |
|---|---|
| 81205 | THE BOEING COMPANY DBA BOEING DIV DE |
Federal Supply Class
Title
GUIDED MISSILE COMPONENTS
Inclusions:
INCLUDES STRUCTURAL COMPONENTS; COMPONENTS AND ACCESSORIES SPECIALLY DESIGNED FOR USE ON OR WITH GUIDED MISSILES, INCLUDING COMPLETE GYRO MECHANISMS, HYDRAULIC PUMPS, AUTOMATIC PILOT MECHANISMS AND SPECIALLY DESIGNED ASSEMBLIES, AND ELECTRONIC GUIDANCE EQUIPMENT INSTALLED IN MISSILES.
Exclusions:
EXCLUDES ELECTRONIC REMOTE GUIDANCE EQUIPMENT USED TO GUIDE MISSILES; SOLID AND LIQUID PROPELLANT UNITS; COMPONENTS OF GYRO MECHANISMS.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| FTLD | FUNCTIONAL DESCRIPTION | COVERS PAYLOAD BAY SECTION 43 |
| RDAL | REFERENCE DATA AND LITERATURE | T.O.21M-AGM86-4-1 |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | OVERALL LENGTH 12.650 IN.; CONTAINS HARDNESS CRITICAL ITEMS OR PROCESSES |
| CRTL | CRITICALITY CODE JUSTIFICATION | TEXT |
| AGAV | END ITEM IDENTIFICATION | AGM-86A MISSILE |