曝光台 注意防骗
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is still present.
When the TEST-RECALL switch is set to TEST, all legends on the 10-channel and
8-channel system annunciator panels and the master caution lights come on.
The BRT-DIM switch on the 10-channel system annunciator panel controls the
brightness of both system annunciator panel legends, the two master caution
lights and all individual system lights.
Four test switches allow all warning lights to be tested. The switches are
located as follows:
TEST/RECALL on 10-channel system annunciator panel
- WARN LTS TEST on pilot's facia panel
- WARNING LT TEST on centre pedestal
WARN LTS TEST on copilotfs facia panel
Figure 8 shows the locations of the warning lights tested by each switch,
SECTION 3
Page 3
Oct 03/83
canadair
chanenQer
OPERATING MANUAL
An electronic circuit breaker unit completes the system. The unit contains 40
protected 28-volt dc power supplies for the master caution and warning system
and other flight compartment warning lights. Each power supply is fed from
three separate sources:
- BATT BUS, CBP-B
- 28V DC ESS BUS, CPD-D
- 28V DC BUS 2, CBP-B
Each output is automatically scanned to detect any possible overload,
indicating a fault in one of the channels. When a fault is detected the AUTO
CB CHAN FAIL annunciator comes on.
The unit operates individually or simultaneously from the three power sources.
SECTION 3
Page 4
Oct 03/83
cacnhaaanaeirn per
OPERATING MANUAL
r
LH ENG
FIREDET
APU
FIRE DET
RH ENG
FIREDET
AIR DATA
COMP
LDG GEAR
CONT UNIT
VERTNAV
COMP/CONT
FLAP
1 CONT UNIT
1 HORIZ
STAB
J UNIT
1 THROTTLE
CONT
J UNIT
1 SPOILER
PROX
SWITCHES
d
1 %
ENG. FIRE J
9 — •• j
STALL V
i
4
1 A
OVERSPEED 1
LND GEAR NOT
DOWN AND LOCKED
\
^
r^V
f '
i
1
ALT ALERT
klRSPEED/FLAP
TO HIGH
AURAL WAR!
28VDC X.
ESS BUS — O
AURAL V\
> = .
BATTERY- °
BUS-RIGHT
RELAY BOX JB2
M 1
(
1 1
t 1
| 1
•MM* m* im—mm
r-+
TONE
TEST
|
•si
^ |
»SJ
^
^J
k
BELL
WARBLER
CLACKER
HORN
CHORD !
WAILER
m «i mm
A A J
PRESS I
Ml ITC ' '
m m
TONE
SUMMER
X
t INCOR
•TAKF-f
INTERMIT
HORN
RECT
"IFF
i
""J
VOLUME
CONTROL
1
^ V \
pA ^ L^n
1
\ \ i
1? \
i | Ur\>-^ AUDIO
AMP N>
\y
1 CONFIGURATION
1
>,
/ARN 2
w
L POWER
T - SUPPLY
3 h
AURAL WARNING •
TEST PANEL •
1i
PILOT -1
COPILOT
TO FLIGHT
COMPARTMEN"
SPEAKERS
PILOT
1
1 COPILOT
L_ .... ... y
TO INTERCOM
1
Aural Warning System - Block Diagram
Figure 2
SECTION 3
Page 5
Oct 03/33
cacnhaadnaeinr cjer
OPERATING MANUAL
MASTER
CAUTION
PRESS TO
RESET
MASTER CAUTION LIGHTS
O
WARN
LTS
TEST
( S ) OFF
LAMP TEST SWITCH
©
E I MLGBAYW
QVHT FAIL ||| RECALL DIM!
MLG BAY
QVHT FAIL
EFFECTIVITY: A/C 1004 TO 1035
I SPARE Iff
RECALL DIM
EFFECTIVITY: A/C 1036 & SUBS
10-CHANNEL SYSTEM ANNUNCIATOR PANEL
EMER LGT
FLTREC t
EFFECTIVITY: A/C 1004 TO 1035
a-CHANNEL SYSTEM ANNUNCIATOR PANEL e
LAMP TEST SWITCH
FIRE FAULT
{ FLTCONTJI
1 EMER LTG I
1 FLTREC Jl
EFFECTIVITY: A/C 1036 & SUBS
Master Caution and Warning Lights
Figure 3
SECTION 3
Page 6
Oct 03/83
cacnhaadnaeinr per
OPERATING MANUAL
ANTI-ICE
Comes on to indicate a fault from
any of the following systems:
ADS HEATER CONTROL
ANTI ICE
WINDSHIELD TEMPERATURE
WOW
Comes on to indicate a fault from
the landing gear control unit.
EMERGENCY LIGHTING
Comes on when emergency
lights are off.
FIRE FAULT
Comes on to indicate a fault from any of the
following systems:
ENGINE FIRE DETECTION AND WARNING
APU FIRE DETECTION AND WARNING
ENGINE FIRE EXTINGUISHING
ENGINE
Comes on to indicate a fault from any of
the following systems:
THRUST REVERSERS
ENGINE VIBRATION MONITORING
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