Piper PA 28-181 User Manual

SECTION 1
NORMAL PROCEDURES
PIPER
AIRCRAFT
CORPORATION
PA.2t.I6I.
ARCHER II
Performance for
a specific airplane
may vary from
published
figures
dep€nding upon the equipmeni insralled,
rhe condition
of the engine,
airplan€ and eqüipm€nt,
atmospheric conditions
and
piloring
technique.
Best Rate of
Climb Spe€d ...
, .. , .. ... .. .. .. .. .. ..
. ?6 KIAS
Best Angle of
Climb Speed . . . . . .
. .
.
. . . . . . . . . . . . . . .
64 KIAS
Turbulent Air Op€rating
Speed
(S€e
Subsection
2.3),
. , , .. ..
. ..
.. 3 KIAS
Maximum Flap
Speed
. . . ..
102 KIAS
Landins Final Approach
Speed
(naps
a0.)
. .. .. .. .. .66
KIAS
Maximum Demonstrated
Crosswind Velocitv ..,.,....l7
KTS
(b)
tc,
(d)
(0
Rf,PORT: vB-1120
4-2
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