NSN 4710-01-489-5897
Part Details | METAL TUBE ASSEMBLY
4710-01-489-5897 A length of tubing, straight, or prebent to a predetermined angle, with added component(s) that forms an end connection on one or both ends. For flexible tube assemblies, see HOSE ASSEMBLY (as modified). For items having perforations in the tubing or attachments, see TUBE ASSEMBLY, FIRE EXTINGUISHING SYSTEM. Excludes items having integral preformed or plain ends, TUBE, BENT (as modified), and items which are branched or forked.
Alternate Parts: 5HJ71105317, 5HJ71105-317, 4710-01-489-5897, 01-489-5897, 4710014895897, 014895897
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 47 | SEP 17, 2001 | 01-489-5897 | 21989 ( TUBE ASSEMBLY, METAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 4710-01-489-5897
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5HJ71105-317 | 81205 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 4710-01-489-5897
| Characteristic | Specifications |
|---|---|
| TUBING MATERIAL | ALUMINUM ALLOY, WW-T-700/6, ALLOY 6061, T4, TYPE 1 |
| TUBE OUTSIDE DIAMETER | 2.000 INCHES NOMINAL |
| WALL THICKNESS | 0.035 INCHES NOMINAL |
| OVERALL LENGTH | 32.000 INCHES NOMINAL |
| END ITEM IDENTIFICATION | F-22 RAPTOR |
| SPECIAL FEATURES | ASSEMBLY CONSISTS OF INLET P/N 5HJ71205-201 1EA; INLET SCREEN P/N 5HJ71206-301 1EA; TUBE P/N 5HJ71105-417 1EA; BOLT P/N LK105E08-1 3EA; INSERT P/N MS21209C0820L 3EA; WASHER P/N NAS1149EN816R 3EA; FLANGE P/N 21F02-32D 1EA. |
| PROPRIETARY CHARACTERISTICS | NPAC |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | TUBE ASSY- FUEL PUMP INLETS |