7120-22-220-7102: STRINGER,AIRCRAFT.
The STRINGER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, aircraft_station_number: WL261.20 AND WL256.70, end_item_identification: MH60, aircraft_mission_design_series: MH60, material_document_and_classification: AMS-QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE, part_name_assigned_by_controlling_agency: (INAVY)STRINGER INSTALLATIOON, SIDE FUSELAGE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-564-4342, 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 |
| aircraft_station_number | WL261.20 AND WL256.70 |
| end_item_identification | MH60 |
| aircraft_mission_design_series | MH60 |
| material_document_and_classification | AMS-QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | (INAVY)STRINGER INSTALLATIOON, SIDE FUSELAGE |
| NSN | 1560-01-564-4342 |
| AIRCRAFT STATION NUMBER | WL261.20 AND WL256.70 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE |
| SPECIAL FEATURES | J SHAPED STRINGER HAVING 89 DEGREE ANGLE ON LARGER SIDE CONNECTION AND 91 DEGREE ANGLE ON SHORTER SIDE CONNECTION; HAVING TWO THRU HOLES LOCATED AT 5.000 AND 15.970 INCHES FROM LEFT END; ALSO HAVING TWO ADDITIONAL THRU HOLES LOCATED BETWEEN LEFT END AND THE 5.000 INCH HOLE; LARGER SIDE PORTION HAS 21 THRU HOLES EVENLY SPACED BETWEEN THE BENDS IN THE STRINGER IN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | (INAVY)STRINGER INSTALLATIOON, SIDE FUSELAGE |
| END ITEM IDENTIFICATION | MH60 |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | MH60 |
No substitute or cross-reference records for this part.