Piper PA 28-181 User Manual

SECTION 2
LIMITATIONS
PIPER
AIRCRAFT
CORPORATION
PA-28.I8I.
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CATE(iORY
OPERATION
ONLY
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\o AFT
PASSENGERS At_t_OWED.
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ARE
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TO
THE I OLLOWI\Gi
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pilor:
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S]'ROBE I I'iHI
S
WHEN
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OR HAZE."
On Lachoüreter fa.e:
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5 ltll\: Rhl)l
CE POWER
TO :650
Rp\t
-
SPI\S PROH 1I]I ]ED
S ]FI:P II]R\S
I,\ZY EICIITS
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EN IRY
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]] K IAS
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KIAS
I] K
IAS
ISSt:fD:
JULY 2.
1979
RtrvISED:
JULY
20, 1983
R[ I'0RTr \
B-1120
l- r0

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