NIIN Output Data
Definition:
A STREAMLINED ITEM DESIGNED TO PRODUCE A SMOOTH OUTLINE AND TO REDUCE DRAG OR AIR RESISTANCE. IT IS SHAPED TO RISE VERTICALLY ALONG THE BODY OF A GUIDED MISSILE OR ROCKET. DO NOT USE IF A MORE SPECIFIC NAME APPLIES. EXCLUDES FAIRING, ROCKET MOTOR; FAIRING, ROCKET ENGINE, GUIDED MISSILE; AND FAIRING, GUIDED MISSILE TUNNEL SECTION. SEE ALSO COVER, ACCESS, GUIDED MISSILE.
Reference/Part Number
Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
---|---|---|---|---|---|---|---|---|
232-31279-32 | 81205 | A | 3 | 2 | 1 | MF | ||
232-31279-4 | 81205 | A | 5 | 2 | 2 | MF |
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 | FOR FORWARD RIGHT HAND ELEVON |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CONSISTS OF 1 FAIRING,RH,MADE FROM AL 6061 PER QQ-A-250/11,HEAT TREAT TO T62 PER BAC5602; CONTAINS NUCLEAR HARDNESS CRITICAL ITEMS |
AGAV | END ITEM IDENTIFICATION | AGM-86B MISSILE |
CRTL | CRITICALITY CODE JUSTIFICATION | TEXT |