Piper PA 28-181 User Manual

sDcrtoN 2
LIMITATIONS
PIPER ATRCRAFT
CORPORATION
PA.28.ItI.
ARCHER II
2.15 MANEUVER
LIMITS
(a)
(b)
Normal
Category
-
All acrobatic
maneuvers
including
spins
prohibited.
Utility
Cstcgory
-
Approvcd
maneuvers for
bank anglcs €xcceding
60".
Steep Turns
Lazy Eights
Chandelles
Entry
Speed
I I3
KIAS
I I3 KIAS
I 13 KIAS
2,19 TYPES
OF OPERATION
The
airplan€ is approved
for the following
operations
when
equipped in
accordance
with FAR 9l or
FAR 135.
(a)
Day V.F.R.
(b)
Night V.F.R.
(c)
Day I.F.R.
(d)
Nighr I.F.R.
(e)
Non lcinS
2.I7 FLIGIIT
LOAD FACTORS
(a)
Positive Load Factor
(Maximum)
(b)
Negative
Load Factor
(Maximum)
2.2I FUEL
LIMITATIONS
(a)
Total Capacity
(b)
Unusable Fu€l
The unusable
fuel for ihis
airplane
has
been determined
as 1.0
gallon
in
each
wing in crirical
flight attirudes.
(c)
Usable
Fuel
The
usablcfu€l in this
airplane
hasbeen
determined
ar 24.0
gllons
in each
wing.
REPORT:
V&1120
Normal
Utility
3.8 G 4.4
G
No inverted
maneuvers
apProved
U,S.
CAL,
U,S. GAL.
48
U.S. CAL.
50
2
ISSUED:
JULY 2,
l9?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