5.2.10 Maximum Endurance
Notice:
Fuel quantity:
usable fuel 28.9 US gal (109,6 l)
A not properly maintained engine
The calculation of the endurance includes:
and aircraft may considerably
1. Fuel for engine start-up and taxiing: 0.8 US gal (3 l).
reduce the endurance.
2. Fuel for take-off and climb to cruise altitude with max.
continuous power as well as fuel for the descent.
3. Reserve for 30 min of holding at 55% = 2.11 US gal (8 l).
Example:
Pressure Altitude: 9500 ft
Density Altitude: 10000 ft
Power Setting : 75%
Endurance: 4,31 h = 4 h 19'
Outside Air Temperature: 32°F (0°C)
FM-AT01-1010-106
A.01
-
02.03.2020
5 - 12
POH
AQUILA AT01-200C
Section 5
PERFORMANCE
Document Nr.:
Issue:
Supersedes Issue:
Date:
Page:
3,0
3,5
4,0
4,5
5,0
5,5
6,0
6,5
Endurance [h]
55%
65%
75%
Perform.:
85%
MCP
n=2260
-22
-4
14
32
50
68
86
104
0
2000
4000
6000
8000
10000
12000
14000
16000
-30
-20
-10
0
10
20
30
40
Outside Air Temperature [°F]
Density
A
ltitude
[ft]
Outside Air Temperature [
°
C]
Pressure Altitude
Conditions:
Power Setting: according to page 5-11
Flaps: UP
