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Piper PA-28-161 User Manual

Piper PA-28-161
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SECTION2
LIMITATIONS
PIPER
AIRCRAFf
CORPORATION
PA-28-161,
WARRIOR
II
2.13
CENTER
OF
GRAVITY
LIMITS
(a) Nonnal Category
2440
Weight
Pounds
Forward Limit Rearward Limit
Inches Aft
of
Datum Inches Aft
of
Datum
88.3
93.0
1950 (and less)
83n
93n
(b) Utility Category
Weight
Pounds
1950
(and less)
2020
Forward Limit
Inches Aft
of
Datum
83.0
83.8
NOTES
Rearward Limit
Inches Aft
of
Datum
93.0
93.0
Straight line variation between points given.
The datum
used
is 78.4 inches
ahead
of
the wing
leading edge at the inboard intersection of the
straight and tapered section.
It is the responsibility of the airplane owner and
the pilot to insure that the airplane is properly
loaded.
See Section 6 (Weight and Balance) for
proper loading instructions.
2.15
MANEUVER
LIMITS
(a)
Normal
Category
- All
acrobatic
maneuvers
including
spins
prohibited.
(b) Utility Category- Approved Maneuvers for bank angles exceeding
6()0:
Steep Turns
Lazy Eights
Chandelles
REPORT: VB-1180
2-4
Entry Speed
111
KIAS
111
KIAS
111
KIAS
ISSUED: AUGUST
13, 1982

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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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