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1. NAVIGATION SYSTEMS (CONT'D)
C. Standby Instrument
On airplanes 9159 and subsequent:
• Use of the integrated standby instrument localizer display for LOC BC approaches is
prohibited.
D. Mode S Transponder Systems for Enhanced Surveillance
Effectivity:
• Airplane 9169 and subsequent and airplanes incorporating Service Bulletin:
• SB 700−34−039, Air Traffic Control (ATC) Transponder System − Mode S Transponder
to Meet Eurocontrol Enhanced Surveillance Requirements..
• The installed Mode S system satisfies the data requirements of ICAO Doc 7030/4,
Regional Supplementary Procedures for SSR Mode S Enhanced Surveillance in
designated European airspace. The capacity to transmit data parameters is shown in
column 2:
Parameter Available
Magnetic Heading Yes
Indicated Airspeed Yes
Mach Number Yes
Vertical Rate Yes
Roll Angle Yes
Track Angle Rate Yes
True Track Angle Yes
Groundspeed Yes
Selected Altitude Yes
Barometric Pressure Setting Yes
LIMITATIONS
NAVIGATION SYSTEMS
REV 53, Jan 29, 2007 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−09−7
LIMITATIONS
NAVIGATION SYSTEMS
Flight Crew Operating Manual REV 53, Jan 29, 2007
CSP 700−6
Volume 1
02−09−8
THIS PAGE INTENTIONALLY LEFT BLANK
1. CIRCUIT BREAKERS FOR DISABLED SYSTEMS
A. Green Airplanes 9005 thru 9010 not Incorporating Service Bulletin 700−24−045
· The following EMS CDU circuit breakers must be confirmed selected OUT/LOCKED for all
phases of flight:
NOTE
All thermal circuit breakers will be displayed OUT on EMS CDU and
all SSPC’s be displayed LOCKED.
AIR−COND / PRESS SYSTEM Page 2
GALLEY FAN HUMIDIFIER
<SB 70021−001>
AIR−COND / PRESS SYSTEM Page 3
L PACK DUCT HEAT
AIR−COND / PRESS SYSTEM Page 5
R PACK DUCT HEAT TOILET FAN
AIR−COND / PRESS SYSTEM Page 6
TRU BAY FAN TRU BAY FAN CTL
CAIMS SYSTEM Page 1
CKPT PRINTER
<SB 700−23−004>
COMM SYSTEM Page 1
AIRFONE REPEATER
<SB 700−23−003>
AIRFONE SYSTEM
<SB 700−23−003>
COMM SYSTEM Page 2
DATALINK <SB 700−23−005>
COMM SYSTEM Page 3
PASSENGER ADDRESS
COMM SYSTEM Page 4
SATCOM AMP CTLR
<SB 700−23−001>
SATCOM DATA UNIT
<SB 700−23−001>
SATCOM FREQ UNIT
<SB 700−23−001>
COMM SYSTEM Page 5
VHF COM 3
<SB 700−23−002>
ELEC SYSTEM Page 9
EMS CDU ½ PWR D
ELEC SYSTEM Page 12
RAT ACT HTR
LIMITATIONS
ELECTRICAL MANAGEMENT SYSTEM
REV 45, Apr 25, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−10−1
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 02-10-2
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 1 of 4
REASON FOR ISSUE
1. CIRCUIT BREAKERS FOR DISABLED SYSTEMS (CONT'D)
A. Green Airplanes 9005 thru 9010 not Incorporating Service Bulletin 700−24−045 (Cont’d)
FUEL SYSTEM Page 4
L RECIRC SOV 1C L RECIRC SOV 1O L RECIRC SOV 2C L RECIRC SOV 2O
FUEL SYSTEM Page 5
L RECIRC SOV 3C L RECIRC SOV 3O
FUEL SYSTEM Page 6
R RECIRC SOV 1C R RECIRC SOV 1O R RECIRC SOV 2C R RECIRC 2O
L RECIRC SOV 3O
FUEL SYSTEM Page 7
R RECIRC SOV 3O
LIGHTS SYSTEM Page 4
NO SMOKING SIGN
LIGHTS SYSTEM Page 6
SEAT BELTS SIGN
NAV SYSTEM Page 2
FMS 3 <SB 700−34−004> GPS 2 <SB 700−34−005> HUD <SB 700−34−002> HUD CTL PNL
<SB 700−34−002>
NAV SYSTEM Page 4
LIGHTNING SENSOR
<SB 700−34−003>
NAV SYSTEM Page 6
VOR / ILS 3
· on 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
　
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