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SECTION 5 - PERFORMANCE
GROSS PRESSURE RATE-OF-CLIMB WITH ONE ENGINE
INOPERATIVE
The gross pressure rate-of-climb, with one engine inoperative, may be obtained
from the GROSS PRESSURE RATE-OF-CLIMB - ONE ENGINE INOPERATIVE
chart for varying weight, altitude and air temperature. The performance sched-
uled is “gross” data, and is the expected performance of an average airplane of
its type and no margins have been subtracted. The rates of climb are “pressure”
rates and may be directly compared with performance measured by the air-
plane’s altimeter set to 1013.2 millibars.
Stall speeds have been scheduled for a center of gravity location of 185 inches
(19.56% MAC) for use in airworthiness test flights.
Approved Performance Data
Issued: November, 2005
P/N 101-590010-471 5 of 8
