I?m getting close to the certification of my RV8A.
My DAR has asked if I can correlate the engine and propeller combination (vans parts) with any kind of production aircraft.
This would allow him by similarities to only require a 25 hour test requirement instead of the 40 hours.
Have any of you run across this before?
Do you have a solution that I can offer to the DAR to only require the 25 hour flight test?
Below are the engine and propeller combination that I purchased from Vans.
Experimental O-360 180HP
LYC XO-360-A1A
Compact hub Constant-speed prop for (I)O-360 (180/200hp) 74"
PROP C2YR-1BFP/F7497
thanks
My DAR has asked if I can correlate the engine and propeller combination (vans parts) with any kind of production aircraft.
This would allow him by similarities to only require a 25 hour test requirement instead of the 40 hours.
Have any of you run across this before?
Do you have a solution that I can offer to the DAR to only require the 25 hour flight test?
Below are the engine and propeller combination that I purchased from Vans.
Experimental O-360 180HP
LYC XO-360-A1A
Compact hub Constant-speed prop for (I)O-360 (180/200hp) 74"
PROP C2YR-1BFP/F7497
thanks