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| ( Historical ) |
| NIIN: | 01-133-7820 | Item Name: | INC: | 02909 |
| FSC: | 2835 | Assignment Date: | Jun-21-1982 | CRIT: | N | IIG: | 02909 |
| ISC: | 5 | Date Standardized: | Jun-21-1982 | HMIC: | N | DODIC: |
| NSC: | 5 | Cancellation Date: | Nov-01-1996 | PMIC: | A | FIIG: | T197-B |
| ESD: | Schedule B: | DEMIL: | A | DEMIL INT: |
| TIIC: | L | Originator: | 97 | ADPEC: | RPDMRC: |
| NIIN: | 01-308-3769 | Item Name: |
| FSC: | 2835 | Replacement Date: | Nov-01-1996 | INC: | 50489 |
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The full version of LogiQuest has information related to NSN 2835-01-133-7820 in each of the following databases.
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PROCUREMENT - Procurement History
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D049 - Air Force End Items List
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ILS_INV - ILS Aviation Parts Availability
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WHEREUSED - Where NIIN Used
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CAGE - Commercial And Government Entity
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H6 - Federal Item Name Directory
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FSC - Federal Supply Class
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| Part Number | CAGE | Company | Status | RN CC | RN VC | DAC | RN AAC | RN FC | RN SC | RN JC | SADC | HCC | MSDS |
| 160001-1000 | 99167 | HAMILTON SUNDSTRAND CORPORATION | H | 3 | 3 | 2 | SB | ||||||
| 5902924 | 99167 | HAMILTON SUNDSTRAND CORPORATION | H | 1 | 3 | 2 | SB |
| 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 | FPZ | Y | T | 0 | U | 1 | L | $29,482.71 | EA | SF8---N | Oct-01-1995 | H |
| MOEC | PC | Phrase | QPA | UOM | OOU | JTC |
| DF | F | WHN EXHST USE 2835-01-308-3769 | 000 | |||
| DF | R | REFER TO FAC0002713299 | 000 | |||
| DF | R | REFER TO NET0002448344 | 000 |
| 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 MANIFOLD 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 |
| FEE4 | Aug-23-1993 | 0 | 0 | E | SE | |||
| ZB01 | Apr-01-1991 | ZB | ZB |
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