Weight Limits; Center Of Gravity Limits; Maneuver Limits - Arrow PA-28R-201 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

PIPER AIRCRAFT CORPORATION
PA.28R.201, ARROW
SECTION 2
LIMITATIONS
2.11 WEIGHT LIMITS
(a) Maximum Weight
(b) Maximum Baggage
NOTE
Refer to Section 5 (Performance) for maximum
weight as limited by performance.
2.13 CENTER OF GRAVITY LIMITS
2750 LBS.
200LBS.
Weight
Pounds
Forward Limit
Inches Aft of Datum
Rearward Limit
Inches Aft of Datum
2750
2375 and
Below
88.9
82.0
NOTES
Straight line variation between points given.
91.5
91.5
The datum used is 78.4 inches ahead of the
wing leading edge at the 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
No acrobatic maneuvers including spins.
Approved maneuvers which do not exceed 60° of bank and 30° of pitch:
Steep Turns
Lazy Eights
Chandelles
ISSUED: SEPTEMBER 15, 1988
REVISED: SEPTEMBER 12, 2005
REPORT: VB·1365
2·5