Center Of Gravity Limits - Piper PA 28-181 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