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| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | III END ITEM IDENTIFICATION | F/A-18E/F AIRCRAFT |
| FEAT | SPECIAL FEATURES | SOCKET WALL IS KNURLED; ASSY IS DRIVEN BY A 0.500 INCH STANDARD RATCHET/TORQUE WRENCH WHICH INTERFACES WITH THE BAR; ASSY IS INSERTED INTO SOCKET BY A 1.000 INCH WIDE BY 0.6200 INCH DEEP RECEIVING SLOT IN THE SOCKET; SPECIFIC MATERIAL IS VISCOUNT 44; ASSY USED TO REMOVE OR INSTALL HYDRAULIC CYLINDER TO AND FROM THE MANIFOLD OF A LEX SPOILER SUBASSEMBLY |
| MATT | MATERIAL | STEEL CORROSION RESISTING |
| SFTT | SURFACE TREATMENT | OXIDE |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | SOCKET-BAR ASSEMBLY |
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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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