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Piper PA-28-161 User Manual

Piper PA-28-161
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PIPER
AIRCRAFT
CORPORATION
PA-28-161,
WARRIOR
II
SECTION
2
LIMITATIONS
2.1
GENERAL
SECTION
2
LIMITATIONS
This section provides the
"FAA
Approved" operating limitations,
instrument markings, color coding
and
basic placards necessary for
operation of the airplane
and
its systems. ·
This airplane must be operated as a normal
or
utility category airplane
in
compliance with the operating limitations stated in the form
of
placards
and markings
and
those given in this section
and
handbook. ·
Limitations associated with those optional systems and equipment
which require
handbook
supplements can be found in Section 9 (Supple-
ments).
2.3
AIRSPEED
LIMITATIONS
SPEED
Never Exceed Speed (VNE) -
Do
not
exceed this speed in any operation.
Maximum
Structural
Cruising Speed
(VNo) -
Do
not exceed this speed
except
in
smooth
air
and then only
with caution.
Maximum Flaps Extended
Speed
(VFE) -
Do
not exceed this speed
w1th
the tlaps extended.
ISSUED:
AUGUST
13, 1982
KIAS
KCAS
160
153
126
122
103
100
REPORT:
VB-1180
2-1

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Piper PA-28-161 Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelPA-28-161 Warrior II
EngineLycoming O-320-D3G
Horsepower160 hp
Seating Capacity4
Wingspan35 ft (10.7 m)
Length24 ft 0 in
Maximum Speed127 knots
Cruise Speed122 knots
Maximum Takeoff Weight2, 325 lb (1, 055 kg)
Fuel Capacity48 US gallons (182 L)

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