1000121-3: RETRACTOR ASSEMBLY,WEAPON CRADLE.
RETRACTOR ASSEMBLY,WEAPON CRADLE. Key specifications include end_item_identification: AH-1W ADVANCE ATTACK HELICOPTER W, reference_data_and_literature: T.O.6J3-4-102-4, part_name_assigned_by_controlling_agency: CONTROL,ENGINE ELECTRONIC, reference_number_differentiating_characteristics: AS DIFFERENTIATED BY SOURCE CONTROL DWG NO. 4060642.
This part is cataloged in the U.S. Government catalog under NSN 1740-01-140-7583, 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.
| functional_description | RECEIVES ENGINE OPERATING DATA AND PILOT-INITIATED SIGNALS AND TRANSMITS COMMAND SIGNALS FOR USE BY FUEL METERING CONTROL |
| end_item_identification | AH-1W ADVANCE ATTACK HELICOPTER W |
| reference_data_and_literature | T.O.6J3-4-102-4 |
| general_characteristics_item_description | STEEL ALLOY; CADMIUM PLATE QQ-P-416,TYPE 2,CLASS 1; 4.090 IN. MIN AND 4.150 IN. MAX LG,3.500 IN. DIA,ULTIMATE STRENGTH OF ASSEMBLY SHALL BE 2500 LB MIN LBS |
| part_name_assigned_by_controlling_agency | CONTROL,ENGINE ELECTRONIC |
| reference_number_differentiating_characteristics | AS DIFFERENTIATED BY SOURCE CONTROL DWG NO. 4060642 |
| NSN | 1740-01-140-7583 |
| GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL ALLOY; CADMIUM PLATE QQ-P-416,TYPE 2,CLASS 1; 4.090 IN. MIN AND 4.150 IN. MAX LG,3.500 IN. DIA,ULTIMATE STRENGTH OF ASSEMBLY SHALL BE 2500 LB MIN LBS |
| END ITEM IDENTIFICATION | AH-1W ADVANCE ATTACK HELICOPTER W |