XtremeAir GmbH, Harzstr.2, D-39444 Hecklingen
Doc. Nr.:________
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POA-Nr.: DE.21G.0227
Compass compensation
Form FO-P-07, Rev. 1 Dated 09.12.2013
Aircraft Type:
Registration:
Aircraft S/N:
Compass type:
Compass S/N:
Compass manufacturer:
Reason for compensation:
New Aircraft
Maintenance
Compass instrument panel Pilot (rear)
Compass instrument panel Passenger (front)
Deviation
in Degrees:
+
14
12
10
8
6
4
2
0
2
4
6
8
10
12
14
Deg
000
030
060
090
120
150
180
210
240
270
300
330
360
Calculation of the deviation coefficients:
A =
4
)
(
)
(
)
(
)
(
W
S
O
N
B =
2
)
(
)
(
W
O
C =
2
)
(
)
(
S
N
A =
4
)
(
)
(
)
(
)
(
B =
2
)
(
)
(
C =
2
)
(
)
(
A =
°
B =
°
C =
°
Verification of the compass compensation:
Target heading
N
030°
060°
O
120°
150°
S
210°
240°
W
300°
330°
Real heading
No observations
Observations
Electrical equipment was on during the test
Place, Date
Stamp
Signature CS
Summary of Contents for XA41
Page 281: ...Maintenance Manual XA41 XA42 AMM XA42 0040 001 C 00 Page 18 Page date Appendix 24 09 2018 ...
Page 282: ...Maintenance Manual XA41 XA42 AMM XA42 0040 001 C 00 Page date Page 19 24 09 2018 Appendix ...
Page 283: ...Maintenance Manual XA41 XA42 AMM XA42 0040 001 C 00 Page 20 Page date Appendix 24 09 2018 ...
Page 284: ...Maintenance Manual XA41 XA42 AMM XA42 0040 001 C 00 Page date Page 21 24 09 2018 Appendix ...