NSN 4710-01-462-2199
Part Details | METAL TUBE ASSEMBLY
4710-01-462-2199 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: 17G4612201, 17G461220-1, 4710-01-462-2199, 01-462-2199, 4710014622199, 014622199
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 47 | JAN 26, 1999 | 01-462-2199 | 21989 ( TUBE ASSEMBLY, METAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 4710-01-462-2199
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 17G461220-1 | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 4710-01-462-2199
| Characteristic | Specifications |
|---|---|
| TUBING MATERIAL | STEEL, AMS 5566 |
| TUBE OUTSIDE DIAMETER | 1.000 INCHES NOMINAL |
| WALL THICKNESS | 0.035 INCHES NOMINAL |
| DESIGN FORM | STRAIGHT |
| END CONNECTION SPEC/STD | DPS (DOUGLAS PROCESS STD) 3.80-5 (FABRICATE PER) |
| OVERALL LENGTH | 19.110 INCHES NOMINAL |
| END ITEM IDENTIFICATION | SUPPORT EQUIPMENT, C-17A AIRCRAFT |
| SPECIAL FEATURES | PROOF PRESSURE TEST AT 200 PSIG PER 3.80-5; REPLACEMENT TUBE ASSY SHALL BE PROOF TESTED PRIOR TO INSTALLATION INTO A PRODUCTION FUEL TANK LEAK TEST CART |
| SPECIFICATION/STANDARD DATA | 88277-MIL-D-9898 GOVERNMENT SPECIFICATION |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | TUBE ASSEMBLY, PRESSURE REGULATOR-OUTLET |