Piper PA 28-181 User Manual

PIPER AIRCRAFT
CORPORATION
PA-28-r8r,
ÄRCHER II
SECTION 2
LIMITATIONS
In full view of the
pilot,
in rhe area of the air
conditioner control
panel
wh€n
the air conditioner is install€dr
"WARNINC
AIR
CONDITIONER
MUST
BE OFF
TO INSURE
NORMAL TAKEOFF
CLIMB PER-
FORMANCE."
Adjacent io upper door
latchi
"ENCAGE
LATCH BEFORE FLIGHT."
On
inside of the baggage companment door.
"BAGGACE
MAXIMUM 2OO LBS."
.UTILITY
CATEGORY OPERATION
-
NO
BAG.
GAGE OR
AFT PASSENGERS ALLOWED.
NOR-
MAL CATEGORY OPERATION. SEE PILOT'S
OPERATING
HANDBOOK
WEIGHT
AND BAL-
ANCE SECTION
FOR
BAGGACE AND AFT PAS,
SENGER
LIMITATIONS."
In full vi€w of the
piloti
"va
=
I
ll KIAS AT
2550ä
(SEE
P.O.H.)"
.DEMO.
X-WIND I7
KTS.'
In full view of the
pilor;
'OIL
COOLER
WINTERIZATIOT-
PLATE TO
BE
REMOVED
WHEN
AMBIENT TEMPERATURE
EX-
CEEDS 50'F."
ISSUf,D:
JULY 2, 1979
REVISED: JULY 21, 1982
Rf,PORT:
VB-1120
2-9

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