POH / AFM
AQUILA AT01-100A
Section 2
LIMITATIONS
Document Nr.:
Issue:
Supersedes Issue:
Date:
Page:
FM-AT01-1010-101
A.09
A.08 (25.05.2020)
03.03.2021
2 - 9
2.13 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”.
2.14 TEMPERATURE LIMITATIONS
Parts of the aircraft structure that are exposed to direct vertical sunlight must be painted
WHITE.
2.15 OPERATING ALTITUDE
The Aquila AT01-100 has a maximum operating altitude of 14,500 ft.
