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Browse Cradle Guided Missile Section products in Aviation.
Manufacturer's List for Cradle Guided Missile Section
Displaying Page 1 of 1
| Part No. | Description | Manufacturer | RFQ | |
|---|---|---|---|---|
| 2560370 | Cradle Guided Missile Section | Standard Manufacturing Co Inc | ||
| 2560370 | Cradle Guided Missile Section | Standard Manufacturing Co Inc | ||
| 25a43161-101-13 | END ITEM IDENTIFICATION: AGM 69A SRAM GENERAL CHARACTERISTICS ITEM DESCRIPTION: INCLUDES 1 CRADLE ASSY,2 BRAKE SHOES (1 INBD 1 OUTBD),2 ARM CLAMPS (1 INBD 1 OUTBD),6 CAM FOLLOWERS,1 FRAME,AND HARDWARE;USED ON P/N 2A14158A 101 15 HANDLING FIXTURE;USED DURING UPLOAD/DOWNLOAD TO THE CARRIER AIRCRAFT AND FOR ROLL POSITIONING MISSILE TO MEET ACFT/MSLE INTERFACE REQUIREMENTS REFERENCE DATA AND LITERATURE: T.O. 11N H5028 2 | The Boeing Company | ||
| 25a43161-101-13 | END ITEM IDENTIFICATION: AGM 69A SRAM GENERAL CHARACTERISTICS ITEM DESCRIPTION: INCLUDES 1 CRADLE ASSY,2 BRAKE SHOES (1 INBD 1 OUTBD),2 ARM CLAMPS (1 INBD 1 OUTBD),6 CAM FOLLOWERS,1 FRAME,AND HARDWARE;USED ON P/N 2A14158A 101 15 HANDLING FIXTURE;USED DURING UPLOAD/DOWNLOAD TO THE CARRIER AIRCRAFT AND FOR ROLL POSITIONING MISSILE TO MEET ACFT/MSLE INTERFACE REQUIREMENTS REFERENCE DATA AND LITERATURE: T.O. 11N H5028 2 | The Boeing Company | ||
| 25a43161-101-14 | END ITEM IDENTIFICATION: AGM 69A SRAM GENERAL CHARACTERISTICS ITEM DESCRIPTION: INCLUDES 1 CRADLE ASSY,2 BRAKE SHOES (1 INBD 1 OUTBD),2 ARM CLAMPS (1 INBD 1 OUTBD),6 CAM FOLLOWERS,1 FRAME,AND HARDWARE;USED ON P/N 2A14158A 101 15 HANDLING FIXTURE;USED DURING UPLOAD/DOWNLOAD TO THE CARRIER AIRCRAFT AND FOR ROLL POSITIONING MISSILE TO MEET ACFT/MSLE INTERFACE REQUIREMENTS REFERENCE DATA AND LITERATURE: T.O. 11N H5028 2 | The Boeing Company | ||
| 25a43161-101-14 | END ITEM IDENTIFICATION: AGM 69A SRAM GENERAL CHARACTERISTICS ITEM DESCRIPTION: INCLUDES 1 CRADLE ASSY,2 BRAKE SHOES (1 INBD 1 OUTBD),2 ARM CLAMPS (1 INBD 1 OUTBD),6 CAM FOLLOWERS,1 FRAME,AND HARDWARE;USED ON P/N 2A14158A 101 15 HANDLING FIXTURE;USED DURING UPLOAD/DOWNLOAD TO THE CARRIER AIRCRAFT AND FOR ROLL POSITIONING MISSILE TO MEET ACFT/MSLE INTERFACE REQUIREMENTS REFERENCE DATA AND LITERATURE: T.O. 11N H5028 2 | The Boeing Company | ||
| 71360-10 | Cradle Guided Missile Section | Precision Engineering Inc | ||
| 71360-10 | Cradle Guided Missile Section | Precision Engineering Inc |
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