Piper PA 28-181 User Manual

sEcTtoN
2
LIMITATIONS
PIPER
AIRCRAFT
CORPORATION
PA-2&161,
aRcHER
II
2.25
PLACARDS
ln full
view of th€
pilot:
-IHIS
AIRPLANE
MUST
BEOPERATED
AS
A NOR.
MAL
OR UTILITY
CATEGORY
AIRPLANE
IN
COM.PLIANCE
WITH
THE
OPERATING
LIMITATIONS
STATED
IN
THE
FORM
OF
PLACARDS,
MARK-INGS
AND
MANUALS.
ALL
MARKINGS
AND
PLACARDS
ON THIS AIR.
PLANE
APPLY TO
ITS
OPERATION
AS A
UTILITY
CATECORY
AIRPLANE.
FOR NORMAL
AND
UTILITY
CATECORY
OPERATION
REFER
TOTHE
PILOT'S
OPERATING
HANDBOOK,
NO ACROBATIC
MANEUVERS
ARE
APPROVED
FOR NORMAL
CATEGORY
OPERATIONS,
SPINS
ARE
PROHIBITED
FOR
NORMAL
AND
UTILITY
CATEGORY.'
In full
view of the
pilot:
TAKEOFF
CHECK
LIST
Fuel on
pro!'er
tank
Electric
fuel
pump
on
Engine
gauges
checked
Flap!
-
s€t
Carb. heat
off
Mixture
s€t
Primer
locked
Fuel
on
proper
tank
Mixture
rich
Electric fuel
pump
on
Seat backs
erect
Seal
backs erect
Fasten
belts/harn€ss
Trim
ub
-
set
controls- free
Door
-
larched
Air
Conditioner
off
LANDING
CHECK
LIST
Flaps
-
set
Fasten
belts/ harness
Air Conditioner
off
The
"AlR
COND
OFF" item
in the
above takeoff
and
landioc
check
lists
is mandarory
for
air conditioned
aircraft
onlv.
REPORT:
VFU20
Lt
ISSUED:
JULY 2,
1979

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