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| MRC | Criteria | Characteristic |
|---|---|---|
| FEAT | SPECIAL FEATURES | TESTS THE PROPELLER IN BOTH THE HORIZONTAL AND VERTICAL POSITIONS; THE FIXTURE POST ASSEMBLY ALLOWS THE PROPELLER TO BE MANUALLY ROTATED AND LOCKED IN SIX INDEXED POSITIONS IN ORDER TO TEST BLADE ANGLE |
| AGAV | III END ITEM IDENTIFICATION | OV-10 ACFT |
| CWFR | NOMINAL OVERALL LENGTH | 51.500 INCHES |
| CXRQ | NOMINAL OVERALL WIDTH | 36.000 INCHES |
| CYAG | NOMINAL OVERALL HEIGHT | 40.000 INCHES |
| FTLD | FUNCTIONAL DESCRIPTION | THE FIXTURE IS DESIGNED TO HOLD HAMILTON STANDARD MODEL 33 LF-337/338 PROPELLER ASSEMBLY DURING TESTING OF BLADE ANGLE AND PRESSURE TESTING OF UNITS UNDER TEST |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 33D2-11-78-1 |
| ALXZ | SPECIFIC USAGE DESIGN | ENABLES TESTING/MAINTENANCE/ASSEMBLY/DISASSEMBLY OF PROPELLERS |
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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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