74A314377-2005: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 17.000 INCHES NOMINAL IN, overall_length: 22.000 INCHES NOMINAL IN, special_features: CONSISTS OF 1 FORMER,3 BEARINGS;3.0 IN THICK IN, aircraft_location: NLG FWD FUSELAGE DOOR MACHANISM, aircraft_station_number: Y230.20. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-600-2170, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | ALUMINUM ALLOY 7075 |
| overall_width | 17.000 INCHES NOMINAL IN |
| overall_length | 22.000 INCHES NOMINAL IN |
| special_features | CONSISTS OF 1 FORMER,3 BEARINGS;3.0 IN THICK IN |
| aircraft_location | NLG FWD FUSELAGE DOOR MACHANISM |
| aircraft_station_number | Y230.20 |
| side_for_which_designed | RIGHT SIDE |
| aircraft_mission_design_series | F/A18A |
| material_document_and_classification | MMS-159 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-600-2170 |
| AIRCRAFT STATION NUMBER | Y230.20 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MMS-159 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 22.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 17.000 INCHES NOMINAL IN |
| SPECIAL FEATURES | CONSISTS OF 1 FORMER,3 BEARINGS;3.0 IN THICK IN |
| AIRCRAFT LOCATION | NLG FWD FUSELAGE DOOR MACHANISM |
| MATERIAL | ALUMINUM ALLOY 7075 |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F/A18A |
No substitute or cross-reference records for this part.