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National Stock Number(NSN): 2835-01-154-3532 (2835011543532, 011543532)
| NIIN: |
01-154-3532 |
Item Name: |
ENGINE,GAS TURBINE |
INC: |
02909
|
| FSC: |
2835
|
Assignment Date: |
May-24-1983 |
CRIT: |
N |
IIG: |
02909 |
| ISC: |
5 |
Date Standardized: |
May-24-1983 |
HMIC: |
N |
DODIC: |
|
| NSC: |
4 |
Cancellation Date: |
Feb-01-2006 |
PMIC: |
A |
FIIG: |
T197-B |
| ESD: |
|
Schedule B: |
|
DEMIL: |
A |
DEMIL INT: |
|
| TIIC: |
L |
Originator: |
97 |
ADPEC: |
0 |
RPDMRC: |
|
| Part Number |
CAGE |
Company |
Status |
RN CC |
RN VC |
DAC |
RN AAC |
RN FC |
RN SC |
RN JC |
SADC |
HCC |
MSDS |
|
160001-400 |
55820
|
RTX CORPORATION |
H |
5 |
9 |
2 |
MB |
|
B |
|
|
|
|
|
160001-400 |
66195
|
SOLAR TURBINES INCORPORATED |
H |
3 |
3 |
2 |
MB |
|
|
|
|
|
|
|
5901091C |
99167
|
HAMILTON SUNDSTRAND CORPORATION |
H |
1 |
3 |
2 |
MB |
|
|
|
|
|
|
| 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 |
FGZ |
Y |
T |
0 |
U |
1 |
L |
$26,327.02 |
EA |
|
SF8RP-N |
Oct-01-2002 |
H |
Technical Characteristics Information
| MRC |
Requirement Statement |
Reply Statement |
| AAXX |
MOUNTING TYPE |
AIRCRAFT |
| ABHP |
OVERALL LENGTH |
19.500 INCHES NOMINAL |
| ABKW |
OVERALL HEIGHT |
16.500 INCHES NOMINAL |
| ABMK |
OVERALL WIDTH |
16.500 INCHES NOMINAL |
| ACDC |
CURRENT TYPE |
DC |
| AFJH |
FURNISHED ITEMS |
FUEL MAINFOLD ASSY, START FUEL NOZZLE |
| AGAV |
END ITEM IDENTIFICATION |
F-16 ACFT |
| APBQ |
INCLOSURE |
NOT INCLUDED |
| AXKD |
POWER OUTPUT FOR WHICH DESIGNED |
SHAFT |
| AXKE |
SHAFT HORSEPOWER RATING |
210.0 |
| AXKG |
SHAFT HORSEPOWER RATING SPEED IN RPM |
61565.0 |
| AXKT |
ALTITUDE AT WHICH HORSEPOWER IS RATED |
0.0 FEET |
| AXKY |
INLET AIR TEMP AT WHICH HORSEPOWER IS RATED |
59.0 FAHRENHEIT |
| ELEC |
VOLTAGE IN VOLTS |
14.0 |
| ELEC |
VOLTAGE IN VOLTS |
30.0 |
| FEAT |
SPECIAL FEATURES |
MAX ALLOWABLE ENG SPEED 67722.0 RPM; CCW ROTATION; MAX RATED EXHAUST GAS TEMP 1200 DEG F; MAX EXHAUST GAS TEMP DURING START 1385 DEG F; FUEL STD MIL-T-5624, TY JP4/5; SINGLE-STAGE CENTRIFUGAL-FLOW COMPRESSOR; SINGLE-STAGE RADIAL-INFLOW TURBINE; ANNULAR COMBUSTOR; CAPACITOR-DISCHARGE TY IGNITION EXCITER; SURFACE-DISCHARGE TY SPARK PLUG |
| FTLD |
FUNCTIONAL DESCRIPTION |
PROVIDES APPROX 200 SHAFT HP TO THE MAIN ENG FOR STARTING & MAIN ENG MOTORING |
| FUEL |
FUEL TYPE |
JET FUEL |
| PKWT |
UNPACKAGED UNIT WEIGHT |
44.00 POUNDS |
| RDAL |
REFERENCE DATA AND LITERATURE |
AF TO. 2JA3-57-3 |
| ZZZY |
REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS |
AS DIFFERENTIATED BY SOURCE CONTROL DRAWING |
| MOE Rule |
Former MOER |
Effective |
AMC |
AMSC |
IMC |
IMCA |
Collaborators |
Receivers |
| FUU4 |
FEE4 |
Sep-01-2000 |
0 |
0 |
D |
|
TU |
TU |
|