KTAS RPM Fuel Flow % Power
167 2675 9.5 GPH 75%
157 2600 8.4 GPH 65%
151 2500 7.3 GPH 55%
ENGINE: Lycoming ??????????????????.. O-360-A1A
PROPELLER: Senisentch ??????????????. ??. 72FM859-1-85
Percent of Power Chart by Altitude
Altitude RPM Percent of H. P
2500 2550 75%
3500 2575 75%
4500 2600 75%
5500 2625 75%
6500 2650 75%
7500 2675 75%

__________________
(This post by: Christopher Checca
EAA Lifetime Member #799388)
Allen Checca (father)
Christopher Checca (son)
RV-6A - N468AC
ENGINE: Lycoming 180 HP O-360-A1A
PROPELLER: Senisentch 72FM859-1-85
WEIGHT: Empty Aircraft 1152 lbs
BASED: KC09 - Morris, IL.
Flying since June 6, 2005
N468AC Web Site