(O) Except for ER operations, aeroplane may be dispatched in the pressurized configuration with one Bleed Air System inoperative provided
(GV-SP):
Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows:
1. Affected Bleed Air Valve is selected OFF
2. Affected R BLEED AIR CONT:
REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
Aeroplane is operated in accordance with AFM Limitations.
NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN.
GV-SP pressurized configuration:
Flight crew will CLOSE inoperative Bleed Control Valve and electrically deactivate affected system.
If failure occurs with
1) Right Bleed Air Control Valve: Select Right Bleed Air Valve OFF utilizing R Eng Bleed Air Switch and pull R BLEED AIR CONT REER E-9 and R WING ANTI-ICE REER D-13 circuit breaker.
2) Left Bleed Air Control Valve: Select Left Bleed Air Valve OFF utilizing L Eng Bleed Air Switch and pull L BLEED AIR CONT: LEER E-10 and L WING ANTI-ICE: LEER, D-4 circuit breaker.
In addition, opposite Engine Bleed Air System will be verified operative and Isolation Valve will be selected OPEN.
BAS Fail, L-R
(Amber – Caution)
(GV-SP/GIV-X) (cont’d)
(continued)
B
(O) Except for ER operations, aeroplane may be dispatched in the pressurized configuration with one Bleed Air System inoperative provided
(GIV-X):
Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows:
1. Affected Bleed Air Valve is selected OFF
2. Affected R BLEED AIR CONT:
REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
Isolation Valve is verified to be operative and selected OPEN,
Aeroplane is not operated in forecast or known icing conditions, and
Aeroplane is operated in accordance with AFM Limitations.
NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN.
GIV-X pressurized configuration:
Flight crew will CLOSE associated Bleed Control Valve and electrically deactivate affected system and pull and collar R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers.
In addition, opposite Engine Bleed Air System and Isolation Valve will be verified operative and Isolation Valve selected OPEN
BAS Fail, L-R
(Amber – Caution)
(GV-SP/GIV-X) (cont’d)
(continued)
B
(O) Except for ER operations, aeroplane may be dispatched in the unpressurized configuration with both Bleed Air Systems inoperative provided
(GV-SP):
Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows:
1. Affected Bleed Air Valve is selected OFF
2. Affected R BLEED AIR CONT:
REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
Manual pressurization control is selected,
Outflow valve is slewed to the full OPEN position,
RAM Air is selected ON,
Cabin differential pressure is monitored to be nominally zero psid during the flight,
Aeroplane is not operated in known or forecast icing conditions, and
Aeroplane is operated in accordance with AFM Limitations.
For GV-SP unpressurized configuration:
Flight crew will ensure inoperative Bleed Control Valve is CLOSED and deactivated electrically and pull and collar R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers.
To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight.
BAS Fail, L-R
(Amber – Caution)
(GV-SP/GIV-X) (cont’d)
B
(O) Except for ER operations, aeroplane may be dispatched in the unpressurized configuration with both Bleed Air Systems inoperative provided
GIV-X):
Affected Valve(s) are verified CLOSED,
Manual pressurization control is selected,
Outflow valve is slewed to the full OPEN position,
RAM Air is selected ON,
Cabin differential pressure is monitored to be nominally zero psid during the flight,
Aeroplane is not operated in forecast or known icing conditions, and
Aeroplane is operated in accordance with AFM Limitations.
For GIV-X unpressurized configuration:
Flight crew will ensure all affected Valve(s) are verified CLOSED.
To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight.
BAS FAIL, L-R
(Amber – Caution)
(GV)
(continued)
B
(O) Except for ER operations, aeroplane may be dispatched in the pressurized configuration with one Bleed Air System inoperative provided
(GV):
Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows:
1. Affected Bleed Air Valve is selected OFF
2. Affected R BLEED AIR CONT:
REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
Opposite Engine Bleed Air System is operative,
Isolation Valve is verified to be operative and selected OPEN, and
Aeroplane is operated in accordance with AFM Limitations.
NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN.
GV pressurized configuration:
Flight crew will CLOSE inoperative Bleed Control Valve and electrically deactivate affected system.
If failure occurs with
1) Right Bleed Air Control Valve: Select Right Bleed Air Valve OFF utilizing R Eng Bleed Air Switch and Pull R Bleed CONT REER, E-9 and R WING ANTI-ICE: REER, D-13 circuit breakers.
2) Left Bleed Air Control Valve: Select Left Bleed Air Valve OFF utilizing L Eng Bleed Air Switch and Pull Left Bleed CONT LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers.
In addition, opposite Engine Bleed Air System will be verified operative and Isolation Valve will be selected OPEN.
BAS FAIL, L-R
(Amber – Caution)
(GV)
B
(O) Except for ER operations, aeroplane may be dispatched in the unpressurized configuration with both Bleed Air Systems inoperative provided
(GV):
Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows:
1. Affected Bleed Air Valve is selected OFF
2. Affected R BLEED AIR CONT:
REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
Manual pressurization control is selected,
Outflow valve is slewed to the full OPEN position,
RAM Air is selected ON,
Cabin differential pressure is monitored to be nominally zero psid during the flight,
Aeroplane is not operated in known or forecast icing conditions, and
Aeroplane is operated in accordance with AFM Limitations.
For GV unpressurized configuration:
Flight crew will ensure both Bleed Air Valves are CLOSED and deactivated electrically and pull and collar R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers.
To operate the airplane unpressurized, select manual pressurization and slew the outflow valve to the full open position with RAM air selected ON. Monitor cabin differential pressure to be nominally zero psid during the flight.
(O) Aeroplane may be dispatched with one inoperative battery charger provided:
Both Engine Generators are operative,
APU Generator is operative,
Associated L BATT CHGR: Left PDB, Left Main AC section or R BATT CHGR: Right PDB, Right Main AC section circuit breaker on the Power Distribution Box is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
Standby Electrical System is operative,
Affected Battery is selected OFF, and
Repairs are made within two (2) flight days.
Flight crew will pull and collar associated “BATT CHGR” circuit breakers:
Left PDB, Left Main AC section or R BATT CHGR: Right PDB, Right Main AC section circuit breaker on the Power Distribution Box.
Battery Charger Fail, L-R
(Amber – Caution)
(GV-SP/GIV-X)
A
(O) Aeroplane may be dispatched with one inoperative battery charger provided:
Both Engine Generators are operative,
APU Generator is operative,
Associated L BATT CHGR: Left PDB, Left Main AC section or R BATT CHGR: Right PDB, Right Main AC section circuit breaker on the Power Distribution Box is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
Standby Electrical System is operative,
Affected Battery is selected OFF, and
Repairs are made within two (2) flight days.
Flight crew will ensure that associated L BATT CHGR: Left PDB, Left Main AC section or R BATT CHGR: Right PDB, Right Main AC section circuit breaker on the Power Distribution Box is pulled and collared.
Brake Maintenance Reqd
(Blue – Advisory)
(GV-SP/GIV-X)
C
Aeroplane may be dispatched.
None required.
BRAKE MAINT REQD
(Blue – Advisory)
(GV)
C
Aeroplane may be dispatched.
None required.
CAB PRESS SEMIAUTO
(Blue – Advisory)
(GV)
C
Aeroplane may be dispatched provided aeroplane is operated in accordance with AFM Limitations.
None required.
Cabin Pressure Semi-auto
(Blue – Advisory)
(GV-SP/GIV-X)
C
Aeroplane may be dispatched provided aeroplane is operated in accordance with AFM Limitations.
None required.
CCD 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
B
(O) Aeroplane may be dispatched provided:
Both Display Controllers, Weather Radar Controllers, and 2 MCDU’s are operative, and
Current terminal charts for the origin, destination and alternate airports are carried onboard the aeroplane and available to the flight crew.
Flight crew will ensure:
Both Display Controllers, Weather Radar Controllers and two MCDUs are operative, and
Current terminal charts for the origin, destination and alternate airports are carried, or EFB’s are carried, onboard the airplane and available to the flight crew.
CDU 1-2-3 FAIL
(Blue – Advisory)
(GV)
A
Except where en route operations or approach minimums require its use, aeroplane may be dispatched provided:
Affected system is not required for IRS alignment,
Long Range Navigation is not dependent on its use,
Procedures do not require its use,
Both RFMUs are operative, and
Repairs are made within two (2) flight days.
NOTE: Two (2) systems are required for dispatch into MNPS or RNP-10 airspace. One (1) system is required in PRNAV, BRNAV, RNAV 1 and RNAV 2 airspace.
None required.
CHECKLIST MISMATCH
(Blue – Advisory)
(GV)
B
(O) Aeroplane may be dispatched provided:
The checklist module in Fault Warning Computer (FWC) 1 is operative, and
Current paper checklists are utilized.
Flight crew will ensure:
The checklist module in Fault Warning Computer (FWC) 1 is operative, and
Utilize current paper checklists.
CKPT TEMP FAN FAIL
(Blue – Advisory)
(GV)
C
(O) Aeroplane may be dispatched provided:
a) None of the following CAS messages are also posted:
Aft Cabin Temp Fan Fail;
Forward Cabin Temp Fan Fail;
b) Cockpit Temperature Manual mode is operative,
c) Associated temperature indicator is operative,
d) CKPT SENSOR FAN, REER D-10, is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and
e) Flight crew monitor cockpit temperature and cockpit duct temperature.
Flight crew will ensure:
None of the following CAS messages are also posted:
Aft Cabin Temp Fan Fail; Forward Cabin Temp Fan Fail,
Cockpit Temperature Manual mode is operative,
Associated temperature indicator is operative,
CKPT SENSOR FAN circuit breaker: REER D-10 is pulled and collared, and
Cockpit temperature and cockpit duct temperature are monitored.
CMC Fail
(Blue – Advisory)
(GV-SP/GIV-X)
B
Aeroplane may be dispatched provided all faults are recorded after each flight.
Aeroplane does not exceed 8 further consecutive flights with cockpit voice recorder unserviceable, and
Any flight data recorder required to be carried is operative.
None required.
Cowl Valve Fail Open, L-R
(Amber – Caution)
(GV-SP/GIV-X)
B
(O) Aeroplane may be dispatched with one (1) valve inoperative provided:
a) Affected Valve is verified OPEN,
b) All components of both HP Bleed Air Systems are operative,
c) Both Environmental Control Systems (ECS) Packs are operative,
d) Affected Cowl Anti-Ice switch is ON,
e) Affected L COWL ANTI-ICE: LEER, D-3 or R COWL ANTI-ICE: REER, D-14 valve circuit breaker is pulled or in the OPEN position. Flight crew may accomplish this task if properly qualified and authorized,
f) Performance Computer is initialized with COWL ANTI ICE selected ON for either takeoff or landing when COWL ANTI-ICE valve is pressurized, and
g) Aeroplane is operated in accordance with AFM Limitations and Performance.
Flight crew will ensure:
BOTH HP Bleed Air Systems and BOTH Environmental Control System (ECS) Packs are operative,
Select the affected Cowl Anti-Ice switch ON and ensure that the affected valve circuit breaker is pulled or in the OPEN position, and
Flight crew verifies that fact by viewing the ECS synoptic page to see that Cowl Anti-ice pressure is indicated. There will also be an A/I icon in the TGT instrument
