NSN 1620-00-127-5785
Part Details | LANDING GEAR CYLINDER AND PISTON ASSEMBLY
1620-00-127-5785 The main shock absorption portion of an aircraft landing gear, consisting of the main cylinder and piston and other associated parts. May be with or without axle(s). Excludes LANDING GEAR, FIXED and LANDING GEAR, RETRACTABLE.
Alternate Parts: 144160733, 14-41607-33, 144160733, 14-41607-33, 14416073, 14-41607-3, 14416073, 14-41607-3, 144160733, 14-41607-33, 144160733, 14-41607-33, 144160733, 14-41607-33, 1620-00-127-5785, 00-127-5785, 1620001275785, 001275785
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | JAN 06, 1973 | 00-127-5785 | 61579 ( CYLINDER AND PISTON ASSEMBLY, LANDING GEAR ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1620-00-127-5785
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 14-41607-33 | 24398 | EAGLE TOOL & MACHINE CO. INC. |
| 14-41607-33 | 4N727 | INTEGRAL AEROSPACE, LLC |
| 14-41607-3 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 14-41607-3 | 0JRC1 | NORTHROP GRUMMAN TECHNICAL SERVICES,INC. |
| 14-41607-33 | 91379 | PEACOCK AEROSPACE INC |
| 14-41607-33 | 33068 | TRIUMPH ACTUATION SYSTEMS -CONNECTICUT, LLC |
| 14-41607-33 | 6D161 | TRIUMPH STRUCTURES-LOS ANGELES, INC. |
Technical Data | NSN 1620-00-127-5785
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | U/A:CYLINDER, PISTON ASSEMBLY, NOSE LANDING GEAR; MATL: STEEL NAI-1274 HY-TUF, 21.562IN O/A LG, 3.625IN. MIN O/A DIA, 1.875IN. DIA BORE THRU, 1 END COUNTER BORED 2.243IN. MIN TO 2.245IN. MAX DIA 2.090IN. DEEP, 1 END COUNTER BORED 2.648IN. MIN TO 2.650IN. MAX DIA 19.250IN. DEEP, 1 END 2.625-16 UN-3A THD 0.500IN. LG. 1 END 2.845-16 UN-3B THD 0.562IN. LG, AS NOTED MACHINED SURFACES 16.0 32.0 63.0 AND 125.0 MICROINCH FINISH, HEAT TREAT 220000 TO 245000 PSI, SHOT PEEN ALL EXTERNAL SURFACES EXCEP THREADS |
| END ITEM IDENTIFICATION | F-5 AIRCRAFT |