POH
AQUILA AT01-200C (N/VFR)
Section 2
LIMITATIONS
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FM-AT01-1010-281
A.02
A.01 (02.03.2020)
03.03.2021
2 - 9
NOTE
For specific operations, additional equipment may be necessary. It is the aircraft operator’s
responsibility to observe the applicable requirements.
2.12 FUEL LIMITATIONS
Left Fuel Tank
Right Fuel Tank
Fuel capacity (total): 15.85 US gal (60.0 l)
15.85 US gal (60.0 l)
Usable fuel (total): 14.48 US gal (54.8 l)
14.48 US gal (54.8 l)
Unusable fuel:
1.37 US gal (5.2 l)
1.37 US gal (5.2 l)
For approved fuel grades, please refer to paragraph 1.8.
CAUTION
To ensure both fuel tanks are emptied evenly, switch to the other tank at least every 60
minutes.
NOTE
The amount of unusable fuel was determined with flap on LDG and V
FE
= 90 kts. It is the worst
case fuel supply configuration within section 4 “NORMAL PROCEDURES”.
NOTE
The fuel quantity, fuel used and fuel remaining functions of the G500 TXi / MVP-50 are advisory
information only and must be verified by the pilot.
2.13 TEMPERATURE LIMITATIONS
Parts of the aircraft structure that are exposed to direct vertical sunlight must be painted
WHITE.
The cooling system of the engine was certified up to ISA +23°C.
For climbing in OAT higher than ISA +23°C an appropriate airspeed of more than v
y
has to be
selected by the pilot.
2.14 OPERATING ALTITUDE
The Aquila AT01-200 has a maximum operating altitude of 16,400 ft.
For flights over FL120 an appropriate oxygen supply for all persons aboard is recommended.
Furthermore national regulations may be considered if applicable.
