Center Of Gravity Limits; Maneuver Limits - Piper PA-28-161 Pilot Operating Handbook

SECTION2
LIMITATIONS
PIPER AIRCRAFf CORPORATION
PA-28-161, WARRIOR II
2.13 CENTER OF GRAVITY LIMITS
(a) Nonnal Category
2440
Weight
Pounds
Forward Limit Rearward Limit
Inches Aft of Datum Inches Aft of Datum
88.3 93.0
1950 (and less)
83n 93n
(b) Utility Category
Weight
Pounds
1950 (and less)
2020
Forward Limit
Inches Aft of Datum
83.0
83.8
NOTES
Rearward Limit
Inches Aft of Datum
93.0
93.0
Straight line variation between points given.
The datum used is 78.4 inches ahead of the wing
leading edge at the inboard intersection of the
straight and tapered section.
It is the responsibility of the airplane owner and
the pilot to insure that the airplane is properly
loaded. See Section 6 (Weight and Balance) for
proper loading instructions.
2.15 MANEUVER LIMITS
(a) Normal Category - All acrobatic maneuvers including spins
prohibited.
(b) Utility Category- Approved Maneuvers for bank angles exceeding
6()0:
Steep Turns
Lazy Eights
Chandelles
REPORT: VB-1180
2-4
Entry Speed
111 KIAS
111 KIAS
111 KIAS
ISSUED: AUGUST 13, 1982