Piper PA 28-181 User Manual

PIPER ATRCRAFT
CORPORATION
PA.2&TTT, ARCHER
II
SECTION 2
LIMITATIONS
2.I3 CENTER OF GRAYITY LIMITS
(a)
Normal Category
Weight
Pounds
Forward Limit
Inches Aft of Datum
Rearward Limit
Inches Aft of Datum
2550
2050
(and
lcss)
88.6
82.0
93.0
93.0
(b)
Utility Category
Wcight
Pounds
Forward Limit
Inches Aft of Datum
Rearward Limit
Inches Aft of Datum
2130
2050
(and
83.0
82.0
93.0
93.0
NOTES
Straight
line variation bctween
poinrs gi\en.
The dalum used
is
78.4
inches ahead ofthc
winS
leading
edge at the
inboard
inrcrscction of rh€
straight and tapered
section.
It is the responsibility oftheairplane own€r and
the
pilot
1o
insure
that the airplan€ is
properly
loaded.
Se€ Section 6
(
Weight and Balanc€) for
proper
loading instructions.
REPORT: VFtl20
2-5
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