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COMM SYSTEM Page 5
VHF COM 3
<SB 700−23−002>
AUDIO PANEL 3A AUDIO PANEL 3B
DC BUS 1, SPDA 3 Page 3
WING INSPECT LTS
[9127 and subsequent]
DC BUS 1, SPDA 4 Page 3
WING INSPECT LTS
[9002 thru 9126]
LIMITATIONS
ELECTRICAL MANAGEMENT SYSTEM
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−10−7
ACTION
Add the following note to the list of circuit breakers for the disabled systems:
· On airplanes 9002 thru 9139 incorporating SB 700−24−056, the AV BATT HEAT and
APU BATT HEAT circuit breakers must be confirmed OUT for all phases of flight.
TEMPORARY REVISION BD 700/35-1
INSERT IN LIMITATIONS
FACING PAGE 02-10-8
Temporary revision to advise the flight crew that the battery heaters are no longer required.
Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
Page 4 of 4
REASON FOR ISSUE
1. CIRCUIT BREAKERS FOR DISABLED SYSTEMS (CONT'D)
D. Green Airplanes 9123 and Subsequent and Airplanes Incorporating SB 700−24−045
(Cont’d)
ELEC SYSTEM Page 1
AC 1 CABIN FEED AC 2 CABIN FEED AC 3 CABIN FEED AC 4 CABIN FEED
ELEC SYSTEM Page 5
DC 1 CABIN FEED DC 2 CABIN FEED 1
ELEC SYSTEM Page 6
DC 2 CABIN FEED 2 DC 2 CABIN FEED 3 DC 2 CABIN FEED 4
FUEL SYSTEM Page 7
R/D PANEL COCKPIT
<SB 700−28−002>
[9002 to 9110]
<SB 700−28−034>
LIGHTS SYSTEM Page 3
L LOGO LT
<SB 700−33−001>
LIGHTS SYSTEM Page 4
NO SMOKING SIGN
LIGHTS SYSTEM Page 6
R LOGO LT
<SB 700−33−001>
SEAT BELTS SIGN
NAV SYSTEM Page 2
FMS 3 CDU
<SB 700−34−004>
GPS 2 <SB 700−34−005> HUD <SB 700−34−002>
NAV SYSTEM Page 4
LIGHTNING SENSOR
<SB 700−34−003>
NAV SYSTEM Page 6
VOR / ILS 3
OIL SYSTEM Page 1
OIL TANK PROBE
<SB 700−79−005>
· on airplanes 9105 and subsequent and airplanes incorporating SB 700−34−022, STBY
ADI circuit breaker must be confirmed selected OUT for all phases of flight.
· on airplanes 9002 thru 9139 incorporating SB 700−31−012 and airplanes 9140 and
subsequent, STBY CLOCK BACKUP circuit breaker must be confirmed selected OUT for
all phases of flight.
< > circuit breaker limitation applies on airplanes [ ] not incorporating the referenced Service
Bulletin (i.e.,<SB 700xxx−xxx>).
LIMITATIONS
ELECTRICAL MANAGEMENT SYSTEM
Flight Crew Operating Manual REV 45, Apr 25, 2005
CSP 700−6
Volume 1
02−10−8
2. EMS CDU SWITCH CONTROL PAGE SETTINGS
A. Green Airplanes 9005 and Subsequent
Selections on the EMS SWITCH CONTROL page must be as follows for all phases of flight.
SWITCH CONTROL Page 1
STALL WARN ADVANCE ................. NORM SLAT / FLAP RESET ............................OFF
LEFT FOOTWARMER ............................ON RIGHT FOOTWARMER..........................ON
HUMIDIFIER <SB 700−21−001> ..........OFF
SWITCH CONTROL Page 2
AC 1 CABIN PWR .................................OFF AC 2 CABIN PWR .................................OFF
AC 3 CABIN PWR .................................OFF AC 4 CABIN PWR .................................OFF
SWITCH CONTROL Page 3
DC 1 CABIN PWR.................................OFF DC 2 CABIN PWR 1..............................OFF
DC 2 CABIN PWR 2..............................OFF DC 2 CABIN PWR 3..............................OFF
< > switch position limitation applies on airplanes not incorporating the referenced Service
Bulletin (i.e.,<SB 700xxx−xxx>).
LIMITATIONS
ELECTRICAL MANAGEMENT SYSTEM
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−10−9
LIMITATIONS
ELECTRICAL MANAGEMENT SYSTEM
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 1
02−10−10
THIS PAGE INTENTIONALLY LEFT BLANK
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