Piper CHEROKEE 180 - Performance Specifications

CHEROKEE 180 SECTION
I
SECTION
I
SPECIFICATIONS
PERFORMANCE
Performance figures
are for airplanes equipped for
cross-country
transportation
and flown
at gross weight under standard
conditions
at
sea level or stated altitude.
Any
changes
in
equipment
may
result
in
changes in performance.
Take-off
Ground Run (S.L.
Std.,
maximum effort,
25
°
flap) (ft) 720
Take-off
over
50-ft
Barrier S.L. Std., (maximum effort,
25°flap)
(ft)
1625
Best
Rate
of
Climb Speed
(mph) 85
Rate of Climb
(ft per min)
725
Service
Ceiling
(ft)
14,150
Absolute
Ceiling
(ft) 16,500
Top Speed (mph)
148
Optimum
Cruise Speed
(TAS) (75% power,
optimum
altitude,
leaned
to
best power) (mph)
141
Cruising Range
(75%
power,
optimum
altitude
leaned to best
economy,
no
reserves
or
climb
allowance)
(mi)
686
Optimum
Cruising
Range (55%
power, 10,000 ft,
leaned to best
economy,
no reserves
or
climb
allowance (mi) 706
Stalling
Speed
CAS
(flaps down) (mph)
61
-
Stalling
Speed
CAS
(flaps
up) (mph) 68
Landing
Roll
S.L.
Std., (flaps down)
(ft)
635*
Landing
Roll over
50-ft
Barrier
S.L.
Std.,
(ft)
1185*
*This
value
applies only for
the
conditions indicated on the
landing
distance versus
density
altitude chart.
761
513
1
720615