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| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | J85-GE-21 ENGINE NOZZLE ACTUATOR SYSTEM HYDRAULIC POWER UNIT SERIES 34E94-11 |
| FTLD | III FUNCTIONAL DESCRIPTION | USED TO HOLD THE PISTON AND SHOE SEPARATELY DURING AN 80 LB. TEST PULL OF THE VEN PUMP DURING OVERHAUL |
| RDAL | III REFERENCE DATA AND LITERATURE | TO 6J3-8-13-4 |
| SUPP | III SUPPLEMENTARY FEATURES | COMPANY NAME-ADAPTER, PULL TEST |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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