2
SECTION I
SPECIFICATIONS
PERFORMANCE
Published figures are for standard airplanes flown at gross weight under
standard conditions at sea level, unless otherwise stated. Performance for a
specific airplane may vary from published figures depending upon the
equipment installed, the condition of engine, airplane and equipment,
atmospheric conditions and piloting technique. Each performance figure below
is subject to the same conditions as on the corresponding performance chart
from which it is taken in the Performance Charts Section.
Take-off Run (maximum effort, 25° flap) (ft)
Take
-off over 50-ft barrier (maximum effort, 25° flap) (ft)
Best Rate of Climb Speed (mph)
Rate of Climb (ft per min)
Cruising Speed (75% power,
Sea Level) (mph)
Cruising Range (75% power,
Sea Level) (mi) (hrs)
(75% power, 7000 ft altitude) (mph)
5% power, 7000 ft altitude) (mi)
ange
(55% power, 10,000 ft., std. fuel 7.2 gph)
(mi) (hrs)
Fuel Consumption (75% power) (gph)
Stalling Speed (flaps down) (mph)
Stalling Speed (flaps up) (mph)
Landing Roll (flaps down) (ft)
Landing Roll over 50-ft barrier (ft)
1625
85
750
16,400
19,000
152
134
680 | 5 hrs
143
725 | 5 hrs
845 | 6.8 hrs
10
57
67
600