Part Details | AIRCRAFT AIR CONDITIONING-HEATING DUCT ASSEMBLY
1660-01-334-1411 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: F20G8041050507, F20G8041050-507, 1660-01-334-1411, 01-334-1411, 1660013341411, 013341411
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | FEB 16, 1991 | 01-334-1411 | 32351 ( DUCT ASSEMBLY, AIR CONDITIONING-HEATING, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1660-01-334-1411
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| F20G8041050-507 | 56852 | DASSAULT FALCON JET CORP.DIV DASSAULT FALCON JET - WILMINGTON |
Technical Data | NSN 1660-01-334-1411
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL CORROSION RESISTING |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-6721 MIL SPEC SINGLE MATERIAL RESPONSE |
| AIRCRAFT LOCATION | FUSELAGE STATION |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | HU-25A |
| OVERALL LENGTH | 8.375 INCHES NOMINAL |
| OVERALL WIDTH | 4.737 INCHES NOMINAL |
| HEIGHT | 4.321 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.032 INCHES NOMINAL |
| SPECIAL FEATURES | DUCT HOLE I/D 4.314 IN.;O/D 4.532 IN.;FLANGE END INCLUDES STAINLESS STEEL SQUARE WIRE MESH,SZ.0.032 WITH 0.250 IN.OPENING;MESH LENGTH 6.875 IN.;3.216 IN.DIA.;FLANGE DIA.0.750 IN.;TH.0.050 IN.;DISTANCE FROM DUCT HOLE TO MESH 4.125 IN.;ACFT MODEL HU25A AIR-INLET ALTERNATOR 5KVA,APU |