Maneuver Limits; Flight Load Factors - Piper CHEROKEE WARRIOR II Information Manual

SECTION 2
LIMITATIONS
2.13
CENTER
OF
GRAVITY LThtlTS
(a) Normal Category
Weight
Pounds
2325
195 0 (and less)
(b) Utility Category
Weight
Pounds
195 0 (and less)
2020
Forward Limit
Inches Aft of Datum
87.0
83.0
Forward Limit
Inches Aft of Datum
83.0
83.8
NOTES
Straight line variation between points give~.
PIPER AIRCRAFT CORPORATION
PA-28-161, CHEROKEE WARRIOR II
Rearward Limit
Inches Aft of Datum
93.0
93.0
Rearward Limit
Inches Aft of Datum
93.0
93.0
The datum used is 78.4 inches ahead of the wing leading edge at
the in board intersection of the straight and tapered section.
lt
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 60°:
Steep Tums
Lazy Eights
Chandelles
2.17 FLIGHT
LOAD
FACTORS
Entry Speed
111 KIAS
111 KIAS
111 KIAS
NORMAL
3.8
G
UTILITY
4.4 G (a) Positive Load Factor (Maximum)
(b) Negative Load Factor (Maximum) No inverted maneuvers approved
REPORT: VB-880
24
ISSUED: DECEMBER 16, 1976
REVISED: MAY 30, 1980