Weight Limits; Center Of Gravity Limits; Maneuver Limits; Flight Load Factors - Piper SEMINOLE 2013 Pilot Operating Handbook

PA-44-180, SEMINOLE

2.11 WEIGhT LIMITS

(a) Maximum Ramp Weight
(b) Maximum Takeoff Weight
(c) Maximum Landing Weight
(d) Maximum Weight in Baggage
Compartment
Refer to Section 5 (Performance) for maximum
weight as limited by performance.

2.13 cENTER Of GRAVITy LIMITS

Weight
Pounds
2800
3400
3800
Straight line variation between points given.
The datum used is 78.4 inches ahead of the wing
leading edge at wing station 106.
It is the responsibility of the airplane owner and
the pilot to ensure that the airplane is properly
loaded. See Section 6 (Weight and Balance) for
proper loading instructions.

2.15 MANEUVER LIMITS

All intentional acrobatic maneuvers (including spins) are prohibited. Avoid
abrupt maneuvers.

2.17 fLIGhT LOAD fAcTORS

(a) Positive Load Factor (Maximum)
(1) Flaps Up
(2) Flaps Down
(b) Negative Load Factor (Maximum)
No inverted maneuvers approved.
ISSUED: June 5, 2013
NOTE
Forward Limit
Inches Aft of Datum
84.0
85.0
89.0
NOTES
SECTION 2
LIMITATIONS
Rearward Limit
Inches Aft of Datum
93.0
93.0
93.0
REPORT: VB-2307
3816 lb
3800 lb
3800 lb
200 lb
3.8 G
2.0 G
-1.5 G
2-5