Piper PA 28-181 User Manual

SECTION 2
LI}IITATIONS
PIPER
AIRCRAFT
CORPORATION
PA-2&1ü,
ARCHER II
SPEED
Design
Maneuv€ring Speed
(VA)
-
Do not
make full or
abrupt control movcments
KIAS
KCAS
above this speed.
At 2550 lbs.
G.w.
At 1634 lbs. G.W.
I
13
89
CAUTION
Maneuvering spe€d
decrcases
at lighter wcight
as
the effccts of aerodynamic
fotces
become
more
pronounced.
Lin€ar interpolation
may
b€
used for intermcdiate
g:oss
weights.
Maneuver-
ing sp€€d
should not
be exc€eded while
opera-
ting in rough
air.
Maximum
Flaps Extended
Speed
(VFE)
-
Do not
exceed this speed *ith
the llaps
€xtended.
102
2.5 AIRSPEED
INDICATOR
MARKINGS
MARKING
Red Radial
Line
(Never
Exceed)
Yellow Arc
(Caution
Range
-
Smooth
Air
Only)
Green Arc
(Normal
Operating
Range)
White Arc
(Flap
Down)
REPORT:
VlU20
lll
89
100
IAS
I54 KTS
125 KTS to
154 KTS
55 KTS to
I25
KTS
49 KTS to
IO2
KTS
ISSUED
JULY
2, 1979

Piper PA 28-181 Specifications

General

Manufacturer	Piper Aircraft
Engine	Lycoming O-360-A4M
Horsepower	180 hp
Wingspan	35 ft 6 in (10.82 m)
Height	7 ft 3 in (2.21 m)
Maximum Takeoff Weight	2, 550 lb (1, 157 kg)
Seating	4
Service Ceiling	14, 100 ft
Fuel Capacity	50 US gal (190 L)
Propeller	Fixed Pitch