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You are here: home->amp->R05->R.8.9.6.1.A.1
8961
Longitudinal (fore and aft) clearance of constant speed propeller blades or cuffs must be at least 1/2 inch (12.7 mm) between propeller parts and stationary parts of the aircraft. This clearance is with the propeller blades
| | A) at takeoff pitch (maximum thrust) angle. |
| | B) at the lowest pitch angle. |
| | C) feathered or in the most critical pitch configuration. |
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