Thank you for taking interest in Cfm International Inc part number 856A1107G06, which is listed with the NSN 4920-01-288-2248 and a product description of “Fixture Aircraft Ma.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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| MRC | Criteria | Characteristic |
|---|---|---|
| SR-5 | MANUFACTURERS CODE | 58828 |
| FTLD | FUNCTIONAL DESCRIPTION | USED TO LIFT THE CORE ENGINE MODULE IN THE HORIZONTAL POSITION |
| AGAV | III END ITEM IDENTIFICATION | KC-135R ACFT ENGINE AGE |
| FEAT | SPECIAL FEATURES | MAIN SUPPORT IS A ""T"" SHAPED WELDMENT 36.000 IN. BY 36.000 IN.,CONSTRUCTED OF 2.000 IN. BY 5.000 IN. RECTANGULAR TUBING. 2 STEEL CABLES AND BALL LOCK PINS ARE LOCATED AT THE FWD END OF THE FIXTURE. ON THE BOTTOM SIDE IS A SLOT INTO WHICH THE LIFT EYE IS INSERTED. THE ARM IS ATTACHED BY INSERTING A THIRD BALL LOCK PIN. THE LIFT EYE IS PART OF A VARIABLE CG DOLLY WHICH ROLLS ON TWO ROLLERS ON THE BOTTOM OF THE SUPPORT. POSITION IS CONTROLLED BY A THREADED SHAFT PASSING THROUGH THE DOLLY. A HAND CRANK IS ATTACHED TO EACH END OF THE THREADED ROD AT THE ENDS OF THE LIFT FIXTURE |
| SR-5 | THE MANUFACTURERS DATA | |
| SR-5 | DESIGN CONTROL REFERENCE | 856A1107G06 |
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