A51K9001-17: LAUNCHER,GUIDED MISSILE,AIRCRAFT.
LAUNCHER,GUIDED MISSILE,AIRCRAFT. Key specifications include mounting_type: PYLON, mounting_location: BOTH WINGS, aircraft_model_number: F14A, missile_launching_method: EJECTED, aircraft_type_for_which_designed: FIXED WING, reference_number_differentiating_characteristics: AS DIFFERENTIATED BY SOURCE CONTROLLING DWG NO.. This part is cataloged in the U.S.
Government catalog under NSN 1440-00-113-6740, 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.
| mounting_type | PYLON |
| mounting_location | BOTH WINGS |
| aircraft_model_number | F14A |
| missile_launching_method | EJECTED |
| aircraft_type_for_which_designed | FIXED WING |
| reference_number_differentiating_characteristics | AS DIFFERENTIATED BY SOURCE CONTROLLING DWG NO. |
| NSN | 1440-00-113-6740 |
| AIRCRAFT MODEL NUMBER | F14A |
| AIRCRAFT TYPE FOR WHICH DESIGNED | FIXED WING |
| MISSILE LAUNCHING METHOD | EJECTED |
| MOUNTING LOCATION | BOTH WINGS |
| SPECIAL FEATURES | FUNCTION FOR WHICH DESIGNED:LAUNCHING;DOCUMENT TYPE:TECHNICAL MANUAL;DOCUMENT IDENTIFICATION:26512;COMPONENT DOCUMENT PAGE NUMBER:A51K9001;INSTALLATION DESIGN:AIRBORNE;JETTISON CAPABILITY:NOT INCLUDED;MISSILE JETTISON CAPABILITY:NOT INCLUDED;MISSILE ACCOMMODATED QTY:1;LAUNCHING POSITION ADJUSTABILITY:NONADJUSTABLE; |
| MOUNTING TYPE | PYLON |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROLLING DWG NO. |