Part Details | AIRCRAFT LANDING GEAR JACK
1730-00-571-1140 A lifting device which consists basically of a ram(s) actuated by a hydraulic pump(s). One end of the ram(s) is designed specifically to mate with the jacking points on the landing gear of an aircraft. It may have a wheeled base with a drawbar for mobility. Excludes JACK, DOLLY TYPE, HYDRAULIC and JACK, HYDRAULIC, HAND.
Alternate Parts: 2932010, 2932-010, 2932, F3A, 53D22047, F3A, MILJ8245, 1730-00-571-1140, 00-571-1140, 1730005711140, 005711140
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 17 | JAN 01, 1963 | 00-571-1140 | 26862 ( JACK, AIRCRAFT LANDING GEAR ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1730-00-571-1140
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2932-010 | 02708 | AGE LOGISTICS CORPORATION |
| 2932 | 02708 | AGE LOGISTICS CORPORATION |
| F3A | 80049 | DEPARTMENT OF THE AIR FORCE |
| 53D22047 | 80049 | DEPARTMENT OF THE AIR FORCE |
| F3A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MILJ8245 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 1730-00-571-1140
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | SELF-CONTAINED |
| MOVEMENT TYPE | MOBILE |
| BASE SHAPE | TEE |
| RATED VERTICAL CAPACITY | 50.0 TONS |
| RETRACTED HEIGHT | 16.000 INCHES |
| HYDRAULIC LIFTING DISTANCE | 22.000 INCHES NOMINAL |
| EXTENDED HEIGHT | 36.000 INCHES |
| SCREW EXTENSION | INCLUDED |
| PUMP TYPE AND QUANTITY | 1 HAND |
| POWER OPERATED PUMP MOUNTING PROVISION | NOT PROVIDED |
| PUMP RELATIONSHIP TO LIFTING DEVICE | INTEGRAL |
| WHEEL REMOVAL CRANE | NOT INCLUDED |
| SPECIAL FEATURES | 10000.0 LB OVERLOAD LIFT RANGE; 560.0 LBS; 5.0 GAL HYDRAULIC FLUID CAPACITY; 5.0 IN EXTENSION SCREW LIFT |
| FUNCTIONAL CLASSIFICATION | HH-1.2 |
| FUNCTIONAL DESCRIPTION | USED TO RAISE ACFT AT THE AXLE FOR VARIOUS MAINTENANCE ACTIONS |
| TYPE/MODEL DESIGNATION | F-3A |
| RELATIONSHIP TO SIMILAR EQUIPMENT | JACK;1730006932743 |
| REFERENCE DATA AND LITERATURE | AF T.O. 35A2-2-12-31 |