AIRCRAFT FLIGHT
MANUAL
BRISTELL B23
Document No.: ADXC-73-001-AFM
Non-approved page
Revision: A2
6-7
Date of Issue: 15.04.2021
Equipment
Req
Opt
In
s
ta
lle
d
= X
,
In
s
ta
l.
d
a
te
M
a
s
s
[
k
g
]
L
o
c
a
tio
n
X
[m
]
In front of instrument panel
AEPS System (complete; if installed)
alternatively AEPS mass balance
1 Req.
X
14.380
12.00
1.080
1015
Garmin engine indication GEA24
1 Req.
X
0.318
1.371
Garmin ADHARS GSU25C
1 Req.
X
0.235
1.504
Overvoltage voltage protection
2 Req.
X
0.145
0.145
1,31 1,38
Encoding altimeter
1 Req.
X
0.180
1.331
Back-Up Battery IBBS 6AH
1 Req.
X
0.967
1.125
Floor area
AP Servo Garmin GSA28
2 Opt.
0.614
0.614
1,858 1,943
Wing
Garmin GAP26 pitot tube / AoA
1 Req.
X
0.177
1.78
NAV/Strobe lights
1R req.
1G Req.
X
X
0.235
0.235
2.551
2.551
Landing light
2 Req.
X
0.183
1.522
L3 Magnetometer MAG-500
1 Req.
X
0.135
1.677
Gear/Brakes
Nose wheel 5.00-
5”
1 Req.
X
4.195
0.603
Main Wheel 5.00-
5”
2 Req.
X
4.205
2.067
Wheel brakes Berringer
2 Req.
X
0.975
2.106
Nose gear suspension damper
1 Req.
X
0.605
0.925
Brake cylinder
4 Req.
X
0.100
1.089
Brake fluid reservoir
1 Req.
X
0.050
0.916
Retrofits/Additions
NOTE:
“Optional” refers to the commercial aspects. Equipment required for a specific
operation mode is defined in Limitation section 2.17