Part Details | GAS TURBINE ENGINE POWER UNIT
2835-01-390-1807
Alternate Parts: 945465410, 9454654-10, 945465410, 9454654-10, 945465410, 9454654-10, 84460001, 8446000-1, LASS, AM32A95, A/M32A-95, 945465410, 9454654-10, 84460001, 8446000-1, LASS, AM32A95, A/M32A-95, 2835-01-390-1807, 01-390-1807, 2835013901807, 013901807
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 13, 1994 | 01-390-1807 | 02910 ( POWER UNIT, GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-390-1807
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9454654-10 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 9454654-10 | 36024 | LIBBY POWER SYSTEMS LLC |
| 9454654-10 | 98750 | SAN ANTONIO AIR LOGISTICS CENTER |
| 8446000-1 | 98750 | SAN ANTONIO AIR LOGISTICS CENTER |
| LASS | 98750 | SAN ANTONIO AIR LOGISTICS CENTER |
| A/M32A-95 | 98750 | SAN ANTONIO AIR LOGISTICS CENTER |
| 9454654-10 | 98752 | WARNER ROBINS AIR LOGISTICS CENTER |
| 8446000-1 | 98752 | WARNER ROBINS AIR LOGISTICS CENTER |
| LASS | 98752 | WARNER ROBINS AIR LOGISTICS CENTER |
| A/M32A-95 | 98752 | WARNER ROBINS AIR LOGISTICS CENTER |
Technical Data | NSN 2835-01-390-1807
| Characteristic | Specifications |
|---|---|
| POWER OUTPUT FOR WHICH DESIGNED | PNEUMATIC |
| AIR FLOW RATE | 150.0 POUNDS PER MINUTE |
| DISCHARGE PRESSURE RATING | 49.0 POUNDS PER SQUARE INCH |
| FUEL TYPE | JET FUEL |
| CURRENT TYPE | DC |
| VOLTAGE IN VOLTS | 24.0 |
| FURNISHED ITEMS | ENCLOSURE ASSY, TURBINE ENG ASSY, FUEL SYS, LUBE SYS, FRAME & RUNNNING GEAR, AIR DELIVERY SYS, 30-FOOT BLEED-AIR HOSE |
| INCLOSURE | INCLUDED |
| MOUNTING TYPE | V ANY ACCEPTABLE |
| OVERALL LENGTH | 114.000 INCHES NOMINAL |
| OVERALL HEIGHT | 72.000 INCHES NOMINAL |
| OVERALL WIDTH | 62.000 INCHES NOMINAL |
| SPECIAL FEATURES | DISCHARGE PRESSURE RATING PSIA; FUEL TYPES INCLUDE MIL-T-5624, GRADE JP-4 OR JP-5 & MIL-T-83133, GRADE JP-8 & VV-F-800 GRADES DF-1, DF-2, DFA |
| SUPPLEMENTARY FEATURES | DOES NOT MEET THE THE GENERAL SPECIFICATION FOR STARTING THE F119 ENGINE (F-22 ACFT) FROM -40 TO -15 AND +105 TO +120 DEGREES F AT SEA LEVEL OR FROM -40 TO +120 DEGREES F AT AN ALTITUDE OF 7000 FEET |
| FUNCTIONAL DESCRIPTION | 4-WHEELED TOWABLE VEHICLE USED TO FURNISH PNEUMATIC POWER FOR GROUND SUPPORT OF ACFT SYSTEMS, ESPECIALLY TO START ACFT ENGINES FOR A VARIETY OF ACFT |
| TYPE/MODEL DESIGNATION | A/M32A-95 |
| REFERENCE DATA AND LITERATURE | AF TO. 35D12-2-14-1 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | AIR START CART, TURBINE ENGINE -- TYPE A/M32A-95 |