POH / AFM
AQUILA AT01-100A
Section 2
LIMITATIONS
Document Nr.:
Issue:
Supersedes Issue:
Date:
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FM-AT01-1010-101
A.09
A.08 (25.05.2020)
03.03.2021
2 - 6
2.7 WEIGHT LIMITS
Maximum Takeoff Weight
1653 lb
(750 kg)
Maximum Landing Weight
1653 lb
(750 kg)
Max. Weight in Baggage Compartment
88.2 lb
( 40 kg)
WARNING
Exceeding the weight limits can overload the aircraft and is prohibited. In addition, aircraft
performance and handling characteristics may be detrimentally affected. The stall speed will
increase, so that the instrument markings are no longer accurate.
2.8 CENTER OF GRAVITY LIMITS
The reference datum is located at the wing leading edge, at the fuselage-wing junction.
With the aircraft leveled, the reference datum and the vertical fall in a plane.
The center of gravity must be within the following limits:
Forward Limit:
16.8 in.
(0.427 m)
aft of Datum
Rearward Limit:
20.6 in.
(0.523 m)
aft of Datum
WARNING
Exceeding the center of gravity limits is prohibited. Exceeding the limits reduces the
controllability and stability of the aircraft.
The procedure to determine the center of gravity location for flight is provided in Section 6 of
this handbook.
2.9 MANEUVER LIMITS
The aircraft is certificated in accordance to the JAR-VLA. That certification includes the
following maneuvers:
a)
All normal, non acrobatic maneuvers.
b)
Stalls:
Wings level stall
c)
Steep Turns:
Angle of Bank
≤ 60°
d)
Chandelle:
Entry Speed 120 kts
e)
Lazy Eight:
Entry Speed 110 kts
NOTE
All acrobatic maneuvers as well as maneuvers with a bank angle exceeding 60° are prohibited.
