Part Number
Definition:
AN AIRFOIL DESIGNED TO MAINTAIN A GUIDED MISSILE IN A NOSE-FIRST FLIGHT ATTITUDE WHEN INSTALLED IN A FIXED POSITION. IT IS NOT CAPABLE OF MOVEMENT(S) TO ALTER FLIGHT PATH. IT MAY BE CANTED TO IMPART SPIN STABILIZATION. FOR MOVABLE ITEMS, SEE FIN, GUIDED MISSLE. FOR FIXED ITEMS HAVING A MOVABLE PORTION ATTACHED, SEE CONTROL SURFACE ASSEMBLY, GUIDED MISSILE. EXCLUDES FIN, ROCKET MOTOR; STABILIZER, HORIZONTAL; STABILIZER, VERTICAL; AND RUDDER, INITIAL CONTROL, GUIDED MISSILE.
CAGE Information
Code | Company |
---|---|
98748 | AIR FORCE UNITED STATES DEPARTMENT O |
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 |
---|---|---|
AGAV | END ITEM IDENTIFICATION | B-52 SE |
FEAT | SPECIAL FEATURES | POWER DRIVE UNIT CONTROLLER;PART OF POWER DRIVE UNIT,P/N 99167;USED ON SUSPENDED FRAME,P/N 82918 |