Piper CHEROKEE TURBO ARROW III 1976 Pilot Operating Handbook page 99

PIPER AIRCRAFT CORPORATION
SECTION 5
PA-28R-201T,
CHEROKEE
TURBO
ARROW III
PERFORMANCE
P A-28 R-201T
P©Wо
-
PEUT©¾¾AUCE
C
OSE
GEAK
UP, FLAPS UP,2900 LBS GROSS WEIGHT
MIXTURE
LEANED
TO
100°F
R CE 0 E PENK ECT(1650°F MIX. ALLOWABLE
I I
-51 -25
O 25 50 75 100
°F 110 1 O 1 O 140 150 180 170 180
-40 -20
20 0
°C
TRUE AIRSPEED
-
KNOTS
OUTSIDE AIR TEMP.
Example:
Cruise pressure altitude:
8500 ft.
Cruise OAT:
10°C
Power: 75%
True airspeed: 154
knots
SPEED POWER
-
PERFORMANCE
CRUISE
Figure 5-21
ISSUED:
DECEMBER 20, 1976
REPORT: VB-800
5-23