|
National Stock Number(NSN): 1440-00-164-6248 (1440001646248, 001646248)
| NIIN: |
00-164-6248 |
Item Name: |
LAUNCHER,GUIDED MISSILE,AIRCRAFT |
INC: |
23401
|
| FSC: |
1440
|
Assignment Date: |
Nov-06-1971 |
CRIT: |
N |
IIG: |
23401 |
| ISC: |
C |
Date Standardized: |
Dec-01-1974 |
HMIC: |
N |
DODIC: |
|
| NSC: |
5 |
Cancellation Date: |
Jul-01-2001 |
PMIC: |
A |
FIIG: |
A503L0 |
| ESD: |
|
Schedule B: |
|
DEMIL: |
F |
DEMIL INT: |
|
| TIIC: |
4 |
Originator: |
TU |
ADPEC: |
0 |
RPDMRC: |
3 |
| NIIN: |
01-012-3294 |
Item Name: |
LAUNCHER,GUIDED MISSILE,AIRCRAFT |
| FSC: |
1440 |
Replacement Date: |
Jul-01-2001 |
|
INC: |
23401 |
| Part Number |
CAGE |
Company |
Status |
RN CC |
RN VC |
DAC |
RN AAC |
RN FC |
RN SC |
RN JC |
SADC |
HCC |
MSDS |
|
421740-1 |
3B150
|
RAYTHEON COMPANY |
H |
3 |
2 |
5 |
KE |
|
|
|
|
|
|
|
421740-1 |
49956
|
RAYTHEON COMPANY |
H |
5 |
9 |
5 |
KE |
3 |
D |
|
|
|
|
|
575600-1 |
3B150
|
RAYTHEON COMPANY |
H |
3 |
2 |
3 |
KE |
|
|
|
|
|
|
|
575600-1 |
49956
|
RAYTHEON COMPANY |
H |
5 |
9 |
3 |
KE |
1 |
B |
|
|
|
|
|
575725-1 |
3B150
|
RAYTHEON COMPANY |
H |
3 |
2 |
5 |
KE |
|
|
|
|
|
|
|
575725-1 |
49956
|
RAYTHEON COMPANY |
H |
5 |
9 |
5 |
KE |
3 |
D |
|
|
|
|
|
A51K9006-1 |
26512
|
NORTHROP GRUMMAN SYSTEMS CORPORATION |
H |
5 |
9 |
5 |
KE |
3 |
D |
|
|
|
|
|
A51K9006-1 |
61174
|
NORTHROP GRUMMAN SYSTEMS CORPORATION |
H |
5 |
2 |
5 |
KE |
|
|
|
|
|
|
|
A51K9006-91 |
26512
|
NORTHROP GRUMMAN SYSTEMS CORPORATION |
H |
5 |
9 |
5 |
KE |
1 |
B |
|
|
|
|
|
A51K9006-91 |
61174
|
NORTHROP GRUMMAN SYSTEMS CORPORATION |
H |
5 |
2 |
5 |
KE |
|
|
|
|
|
|
|
A51K9006-93 |
26512
|
NORTHROP GRUMMAN SYSTEMS CORPORATION |
H |
5 |
9 |
5 |
KE |
3 |
B |
|
|
|
|
|
A51K9006-93 |
61174
|
NORTHROP GRUMMAN SYSTEMS CORPORATION |
H |
5 |
2 |
5 |
KE |
|
|
|
|
|
|
|
LAU92A |
23669
|
AERONAUTICAL AND AERONAUTICAL SUPPORT EQUIPMENT TYPE DESIGNATION SYSTEM/MIL STD 875/ |
H |
5 |
2 |
6 |
KE |
3 |
D |
|
|
|
|
| MOEC |
SOS |
A A C |
R C |
S L C |
CIIC |
U P Q |
U S C |
Unit Price |
UI |
UICF |
MCD |
Action Date |
C/H |
| DN |
N32 |
V |
H |
0 |
7 |
1 |
L |
$19,280.00 |
EA |
|
4ZPFAR9 |
Sep-01-1998 |
H |
| MOEC |
PC |
Phrase |
QPA |
UOM |
OOU |
JTC |
| DN |
F |
WHN EXHST USE 1440-01-012-3294 |
000 |
|
|
|
Technical Characteristics Information
| MRC |
Requirement Statement |
Reply Statement |
| AAXX |
MOUNTING TYPE |
WING |
| AYQM |
MOUNTING LOCATION |
BOTH WINGS |
| BCQY |
AIRCRAFT TYPE FOR WHICH DESIGNED |
FIXED WING |
| BCRB |
MISSILE LAUNCHING METHOD |
RELEASED |
| CYEP |
AIRCRAFT MODEL NUMBER |
F-14A |
| FEAT |
SPECIAL FEATURES |
FUNCTION FOR WHICH DESIGNED:LAUNCHING;INSTALLATION DESIGN:AIRBORNE;DOCUMENT CONTROLLING AGENCY:NAVY;JETTISON CAPABILITY:NOT INCLUDED;MISSILE JETTISON CAPABILITY:INCLUDED;MISSILE ACCOMMODATED QTY:1; |
| MOE Rule |
Former MOER |
Effective |
AMC |
AMSC |
IMC |
IMCA |
Collaborators |
Receivers |
| N2R4 |
|
Apr-01-1991 |
0 |
0 |
E |
KE |
KE |
KE |
|