Weight Limits; Center Of Gravity Limits; Maneuver Limits - Piper PA-44-180 Seminole 1979 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

PIPER AIRCRAFT CORPORATION
PA-44-180, SEMINOLE
(e) Cylinder Head Temperature
Green Arc (Normal Range)
Red Line (Maximum)
2.11 WEIGHT LIMITS
(a) Maximum Takeoff Weight
(b) Maximum Ramp Weight
(c) Maximum Landing Weight
(d) Maximum Weight in Baggage
Compartment
2.13 CENTER OF GRAVITY LIMITS
Weight
Pounds
2800
3400
3800
Forward Limit
Inches Aft of Datum
84.0
85.0
89.0
NOTES
SECTION 2
LIMITATIONS
200° to 435° F
500°F
3800 lbs.
3816 lbs.
3800 lbs.
200 lbs.
Rearward Limit
Inches Aft of Datum
93.0
93.0
93.0
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 insure 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.
ISSUED: MARCH 23, 1978
REVISED: JANUARY 22, 1982
REPORT: VB-860
2-5