Users Manual Part 3

Table 6-1. L1, L2 and L3 Codes (Cont)
Repair actionLog type
L3L2L1
DescriptionCode
Descrip-
tion
Code
Descrip-
tion
Code
Check A429 signal
from source
Critical FaultsSSM FT2
Pitch Angle
Label
1
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Check A429 signal
from source
Critical FaultsSSM FT2
Roll Angle
Label
2
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Check A429 signal
from source
Critical FaultsSSM FT2
Pitch Rate
Label
3
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Check A429 signal
from source
Critical FaultsSSM FT2
Roll Rate
Label
4
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Check A429 signal
from source
Critical FaultsSSM FT2
Yaw Rate
Label
5
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Check A429 signal
from source
Critical FaultsSSM FT2
Body
Longitudinal
Acceleration
6
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Check A429 signal
from source
Critical FaultsSSM FT2
Body
Vertical
Acceleration
7
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Check A429 signal
from source
Critical FaultsSSM FT2
True
Heading
Label
8
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Page 6-58
23-15-84
EFFECTIVITY
ALL
11 Nov 2020
© Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
JetWave™ MCS-8562 Terminal