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| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | III END ITEM IDENTIFICATION | F110-GE-129 ENGINE AGE |
| SR-5 | MANUFACTURERS CODE | 66464 |
| FEAT | SPECIAL FEATURES | C/0 WYE SHAPED PLATE WITH ITS LEGS SPACED 120.0 DEG APART AND OF EQUAL LENGTH; CLEVIS MOUNTING BLOCK AT THE CENTER OF THE PLATE ON ONE SIDE AND THREE EQUALLY SPACED SUPPORT BLOCKS ON THE OPPOSITE SIDE OF THE CLEVIS MOUNTING BLOCK |
| SR-5 | THE MANUFACTURERS DATA | |
| RDAL | REFERENCE DATA AND LITERATURE | SERD NO. 1832 |
| FTLD | FUNCTIONAL DESCRIPTION | USED TO INSTALL/REMOVE THE COMPRESSOR ROTOR STAGE 1 AND 2 SPOOL WITH THE COMPRESSOR ROTOR SHAFT IN POSITION AND TO TURN THE COMPRESSOR ROTOR STAGE 1 AND 2 SPOOL FROM THE HORIZONTAL TO THE VERTICAL PLANE |
| SR-5 | DESIGN CONTROL REFERENCE | 3C4206G01 |
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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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