EFFECTIVITY SIL 004, 005, 017, 018 34-36 TASK 801
D633A103-SIL BOEING PROPRIETARY -Copyright # Unpublished Work -See title page for details Page 202 Jun 15/2010
HCP FAULT CODE
COMBINER DISPLAY
GO TO FIM TASK
HC59 FC59
34-36
TASK
803
HC5A
FC5A
34-36
TASK
803
OHU60
FC60
34-36
TASK
804
OHU61
FC61
34-36
TASK
804
OHU62
FC62
34-36
TASK
804
OHU63
FC63
34-36
TASK
804
OHU64
FC64
34-36
TASK
804
OHU65
FC65
34-36
TASK
804
OHU66
FC66
34-36
TASK
804
OHU67
FC67
34-36
TASK
804
OHU68
FC68
34-36
TASK
804
OHU69
FC69
34-36
TASK
804
OHU70
FC70
34-36
TASK
804
OHU71
FC71
34-36
TASK
804
OHU72
FC72
34-36
TASK
804
OHU73
FC73
34-36
TASK
804
OHU74
FC74
34-36
TASK
804
OHU75
FC75
34-36
TASK
804
OHU76
FC76
34-36
TASK
804
CRITSYM
FC80
34-36
TASK
810
BRTCTL
FC81
34-36
TASK
812
HCP90
FC90
34-36
TASK
806
HCP91
FC91
34-36
TASK
806
HCP92
FC92
34-36
TASK
806
HCP94
FC94
34-36
TASK
806
HCP96
FC96
34-36
TASK
806
HCP97
FC97
34-36
TASK
806
HCA1
A1
34-36
TASK
806
ALIGNHUD
A1
34-36
TASK
811
HAPC1
C1 34-36
TASK
854
-------------------------END OF TASK ---------------------------
EFFECTIVITY SIL 004, 005, 017, 018 34-36 TASK 801
D633A103-SIL BOEING PROPRIETARY -Copyright # Unpublished Work -See title page for details Page 203 Jun 15/2010
LRU/SYSTEM MAINTENANCE MESSAGE GO TO FIM TASK
HUD DEU70 Reference Not Currently Available
HUD DEU74 Reference Not Currently Available
HUD DEU75 Reference Not Currently Available
851. HUD Software Problems -Fault Isolation
A. Description
(1) This task is for fault messages HC01, HC02, HCAC03, or HC04 (combiner display FC01, FC02, FC03, or FC04).
B. Possible Causes
(1)
OPC integrity (HC01), software incompatibility (HC02), or hardware incompatibility (HC04).
(2)
Program pin configuration error (HCAC03).
C. Circuit Breakers
(1) Make sure that these circuit breakers are closed:
CAPT Electrical System Panel, P18-2 Row Col Number Name C 1 C01622 HEAD UP DISPLAY ANNUN DC C 2 C01618 HEAD UP DISPLAY CONT PNL DC C 5 C01619 HEAD UP DISPLAY SYS NORMAL DC C 6 C01620 HEAD UP DISPLAY SYS ALTN DC
D. Related Data
(1)
SSM 34-36.
(2)
WDM 34-36.
E. Initial Evaluation
(1) Do
this
task:
Head
Up
Display
BITE
Procedure,
34-36
TASK
801.
(a)
If fault message HC01, HC02, HCAC03, or HC04 show (combiner display FC01, FC02, FC03, or FC04), do the Fault Isolation Procedure.
(b) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:737-600/700/800/900 FAULT ISOLATION MANUAL 故障隔离手册 导航(129)