Part Details | AIRCRAFT AIR CONDITIONING-HEATING DUCT ASSEMBLY
1660-01-380-6008 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: 17P6N1013503, 17P6N1013-503, 1660-01-380-6008, 01-380-6008, 1660013806008, 013806008
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | SEP 22, 1993 | 01-380-6008 | 32351 ( DUCT ASSEMBLY, AIR CONDITIONING-HEATING, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1660-01-380-6008
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 17P6N1013-503 | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 1660-01-380-6008
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL CORROSION RESISTING |
| MATERIAL DOCUMENT AND CLASSIFICATION | DMS1872 MFR REF SINGLE MATERIAL RESPONSE |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-S-5002 MIL SPEC SINGLE TREATMENT RESPONSE |
| AIRCRAFT LOCATION | WING, LEADING EDGE |
| AIRCRAFT STATION NUMBER | STA 818.838 TO 853.632 |
| SIDE FOR WHICH DESIGNED | BOTH SIDES |
| AIRCRAFT MISSION DESIGN SERIES | C-17A |
| OVERALL LENGTH | 35.790 INCHES NOMINAL |
| OVERALL WIDTH | 3.000 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.016 INCHES NOMINAL |
| SPECIAL FEATURES | DUCT ASSY, ANTI-ICING, OTBD WING LEADING EDGE SLAT; C/O -7 DUCT ASSY, 4 SQ FT -15 SILICONE BOUND FIBERGLASS BATTING, 2 SQ FT -17 SILICONE COATED GLASS CLOTH, 2 FT X 1" -21 GLASS FABRIC PRESSURE SENSITIVE TAPE, 1 EA 14713-3-1 SEAL & 14713-3-11 LINER; NHA17N6N0691 |
| SPECIAL TEST FEATURES | PROOF & LEAK TEST AT 240 PSIG |
| SUPPLEMENTARY FEATURES | MAX OPERATING PRESSURE 48 PSIG; MAX OPERATING TEMPERATURE 450 DEG F |