|
National Stock Number(NSN): 2840-00-413-0826 (2840004130826, 004130826)
| NIIN: |
00-413-0826 |
Item Name: |
SUPPORT,TURBINE NOZZLE,AIRCRAFT GAS TURBINE ENGINE |
INC: |
51909
|
| FSC: |
2840
|
Assignment Date: |
Apr-29-1970 |
CRIT: |
Y |
IIG: |
51909 |
| ISC: |
2 |
Date Standardized: |
Dec-01-1974 |
HMIC: |
N |
DODIC: |
|
| NSC: |
8 |
Cancellation Date: |
Nov-20-2002 |
PMIC: |
A |
FIIG: |
A521B0 |
| ESD: |
|
Schedule B: |
|
DEMIL: |
Q |
DEMIL INT: |
|
| TIIC: |
1 |
Originator: |
KE |
ADPEC: |
|
RPDMRC: |
|
| Part Number |
CAGE |
Company |
Status |
RN CC |
RN VC |
DAC |
RN AAC |
RN FC |
RN SC |
RN JC |
SADC |
HCC |
MSDS |
|
699210 |
02403
|
TURBINE ENGINE COMPONENTS TECHNOLOGIES CORPORATION |
H |
5 |
2 |
4 |
MF |
|
|
|
|
|
|
|
699210 |
11449
|
TURBO POWER & MARINE SYSTEM INC SUB OF UNITED TECHNOLOGIES CORP |
H |
3 |
2 |
2 |
MF |
|
|
|
|
|
|
|
699210 |
15014
|
MACHINE PRODUCTS CO INC |
H |
5 |
2 |
4 |
MF |
|
|
|
|
|
|
|
699210 |
33617
|
ELECTRO-METHODS, L.P. |
H |
5 |
2 |
4 |
MF |
|
|
|
|
|
|
|
699210 |
50381
|
MTU AERO ENGINE COMPONENTS INC |
H |
5 |
2 |
4 |
MF |
|
|
|
|
|
|
|
699210 |
50748
|
BOGUE EXECUTIVE ENTERPRISES INC DBA/DEXTER TOOL CO |
H |
5 |
2 |
4 |
MF |
|
|
|
|
|
|
|
699210 |
6D794
|
BARRIDON CORPORATION |
H |
5 |
2 |
4 |
MF |
|
|
|
|
|
|
|
699210 |
77445
|
RTX CORPORATION |
H |
5 |
9 |
2 |
MF |
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 |
| DF |
FHZ |
Y |
T |
0 |
U |
1 |
L |
$1,614.63 |
EA |
|
SF8PQ-V |
Apr-01-1997 |
H |
| MOEC |
PC |
Phrase |
QPA |
UOM |
OOU |
JTC |
| DF |
R |
REFER TO FAC0000149641 |
000 |
|
|
|
| DF |
R |
REFER TO NET0000126964 |
000 |
|
|
|
Technical Characteristics Information
| MRC |
Requirement Statement |
Reply Statement |
| AARX |
INSIDE DIAMETER |
23.265 INCHES MINIMUM AND 23.275 INCHES MAXIMUM |
| ABHP |
OVERALL LENGTH |
1.373 INCHES NOMINAL |
| ABKV |
OUTSIDE DIAMETER |
26.344 INCHES MINIMUM AND 26.346 INCHES MAXIMUM |
| ABTB |
MOUNTING HOLE DIAMETER |
0.216 INCHES MINIMUM AND 0.226 INCHES MAXIMUM |
| ABTJ |
MOUNTING HOLE QUANTITY |
40 |
| AGAV |
END ITEM IDENTIFICATION |
TF-30 AIRCRAFT ENGINE |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
AGAV |
| MATT |
MATERIAL |
NICKEL ALLOY |
| MOE Rule |
Former MOER |
Effective |
AMC |
AMSC |
IMC |
IMCA |
Collaborators |
Receivers |
| FXX4 |
|
Apr-01-1991 |
1 |
H |
X |
SX |
TU |
TU |
|