Part Details | AIRCRAFT AIR CONDITIONING-HEATING DUCT ASSEMBLY
1660-01-380-1431 A hollow body used to transport air to various parts of the aircraft for the purpose of heating, cooling, pressurizing, de-icing, and the like. It may include flange(s), bracket(s), and the like for mounting purposes. Excludes pipes used in aircraft exhaust systems and pipes used in non-aircraft applications. Excludes PIPE, EXHAUST and PIPE, AIR CONDITIONING-HEATING.
Alternate Parts: 17P6N10121, 17P6N1012-1, 1660-01-380-1431, 01-380-1431, 1660013801431, 013801431
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | SEP 15, 1993 | 01-380-1431 | 32351 ( DUCT ASSEMBLY, AIR CONDITIONING-HEATING, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1660-01-380-1431
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 17P6N1012-1 | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 1660-01-380-1431
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM |
| MATERIAL DOCUMENT AND CLASSIFICATION | DMS 1872 MFR REF SINGLE MATERIAL RESPONSE |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-S-5002 MIL SPEC SINGLE TREATMENT RESPONSE |
| AIRCRAFT LOCATION | WING, LEADING EDGE |
| SIDE FOR WHICH DESIGNED | BOTH SIDES |
| AIRCRAFT MISSION DESIGN SERIES | C-17A |
| OVERALL LENGTH | 38.920 INCHES NOMINAL |
| OVERALL WIDTH | 3.000 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.016 INCHES MINIMUM |
| SPECIAL FEATURES | DUCT ASSY, ANTI-ICING, INNER; LEADING EDGE OTBD; C/O -5 WELD ASSY, 4 SQ FT -7 SILICONE BINDER GLASS FIBER BATTING, 2 SQ FT -9 SILICONE COATED GLASS CLOTH, 2 FT X 1" -11 PRESSURE SENSITIVE ADHESIVE GLASS FABRIC TAPE; -5 WELD ASSY C/O -3 & -15 DUCTS, -17 ADAPTER, 14713-3-11 LINER & 7D0072-300MST FLANGE |
| SPECIAL TEST FEATURES | PROOF & LEAK TEST AT 240 PSIG |
| SUPPLEMENTARY FEATURES | MAX OPERATING PRESSURE 48 PSIG; MAX OPERATING TEMPERATURE 450 DEG F |