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Piper PA 28-181 User Manual

Piper PA 28-181
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PIPER AIRCRAFT CORPORATION
PA-2t.ItI. ARCHER II
sEcTtoN
3
EMERGENCY PROCEDURES
If roughness
persists, prepar€
for a
precautionary
landing
at
pilot's
discretion.
NOTE
Partial carburelor heat may be worse than no
heat at all.
rince
ir may melt
parr
of
rhe
ice
\{hich
$ill rcfreeze in the intake syslem. When
u'ingcarbur€tor hear, there[ore.alwa]s
use full
hear,
and
when ice
is remo\ed relurn rhe
control
to
the
full
cold
position.
ISSUEDT JANUARY U,
l9tl
REPORT: v&
201

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Piper PA 28-181 Specifications

General IconGeneral
ManufacturerPiper Aircraft
EngineLycoming O-360-A4M
Horsepower180 hp
Wingspan35 ft 6 in (10.82 m)
Height7 ft 3 in (2.21 m)
Maximum Takeoff Weight2, 550 lb (1, 157 kg)
Seating4
Service Ceiling14, 100 ft
Fuel Capacity50 US gal (190 L)
PropellerFixed Pitch

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