Anti-skid off braking procedures, AFM Section 3, Abnormal Procedures, Anti-Skid Failure are followed,
No WOW Power Faults exist,
If Auto mode of the AUX Hydraulic Pump is inoperative, AUX pump is selected ON for takeoff and landing, and
Aeroplane is operated in accordance with AFM Limitations.
NOTE: Anti-Skid inoperative AFM performance penalties must be applied. Refer to AFM, Section 5, Performance, Reference Accelerate-Stop Distance.
Flight crew will ensure airplane is operated in accordance with AFM, Limitations. Flight crew will select ANTI-SKID “OFF” and follow Anti-Skid Off Braking Procedures. AFM, Section 3, Abnormal Procedures, Anti-Skid Failure. NOTE: May be inoperative provided AFM performance penalties are applied. Refer to AFM, Section 5, Performance, Reference Accelerate-Stop Distance.
AP 1-2 Fail
(Amber – Caution)
(GV-SP/GIV-X)
B
(O) Except for ER operations or where en route operations or approach minimums require its use, Aeroplane may be dispatched with one (1) Autopilot inoperative provided the aeroplane is operated in accordance with AFM Limitations in the event operative FGC fails and Yaw Damper is inoperative.
NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations.
Flight crew will operate the airplane in accordance AFM limitations in the event the operative FGC fails and the Yaw Damper is inoperative
AP 1-2 Power Fail
(Blue – Advisory)
(GV-SP/GIV-X)
B
(O) Except for ER operations or where en route operations or approach minimums require its use, Aeroplane may be dispatched with one (1) inoperative provided aeroplane is operated in accordance with AFM Limitations in the event operative FGC fails and Yaw Damper is inoperative.
NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations.
Flight crew will operate airplane in accordance with AFM limitations in the event the FGC fails and the Yaw Damper is inoperative.
AP/Trim Fail
(Blue – Advisory)
(GV-SP/GIV-X)
B
(O) Aeroplane may be dispatched with one (1) elevator trim servo inoperative provided the inoperative trim servo circuit breaker(s) is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized.
GV-SP: Flight crew will ensure inoperative PITCH TRIM SERVO #1: POP, E-2 or PITCH TRIM SERVO #2: CPOP, E-1 servo circuit breaker is pulled and collared.
GIV-X: Flight crew will ensure inoperative PITCH TRIM SERVO #1: POP, E-2 or PITCH TRIM SERVO #2: CPOP, E-1 servo circuit breaker is pulled and collared.
APM 1-2-3-4 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
B
Aeroplane may be dispatched with one (1) APM inoperative.
None required.
APU Fail
(Amber – Caution)
(GV-SP/GIV-X)
B
(O) Except for ER operations, aeroplane may be dispatched provided:
Both Engine Driven generators are operative, and
Standby Electrical System is operative.
Flight crew will ensure:
BOTH Engine Driven Generators are operative, and
Standby Electrical system is operative.
APU FAIL
(Amber – Caution)
(GV)
B
(O) Except for ER operations, aeroplane may be dispatched provided:
BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and
Standby Electrical System is operative.
APU GCU FAIL
(Blue – Advisory)
(GV)
A
(O) Except for ER operations, aeroplane may be dispatched provided:
APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS,
Standby Electrical System is operative, and
Repairs are made within two (2) flight days.
Flight crew will ensure:
APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared,
BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and
Standby Electrical System is operative.
APU Generator Fail
(Blue – Advisory)
(GV-SP/GIV-X)
A
(O) Except for ER operations, aeroplane may be dispatched provided:
APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS,
Standby Electrical System is operative, and
Repairs are made within two (2) flight days.
Flight crew will ensure:
APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared,
BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and
Standby Electrical System is operative
APU Generator Maint Reqd
(Blue – Advisory)
(GV-SP/GIV-X)
C
Aeroplane may be dispatched.
None required.
APU GEN FAIL
(Blue – Advisory)
(GV)
A
(O) Except for ER operations, aeroplane may be dispatched provided:
APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS,
Standby Electrical System is operative, and
Repairs are made within two (2) flight days.
Flight crew will ensure:
APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared,
BOTH Engine Driven Generators are operative by reference to the AC synoptic and the absence of failure message on CAS, and
Standby Electrical System is operative.
APU GEN MAINT REQD
(Blue – Advisory)
(GV)
C
Aeroplane may be dispatched.
None required.
APU Maintenance Required
(Blue – Advisory)
(GV-SP/GIV-X)
C
Aeroplane may be dispatched.
None required.
APU MAINT REQD
(Blue – Advisory)
(GV)
C
Aeroplane may be dispatched.
None required.
APU Shutoff Valve Fail
(Amber – Caution)
(GV-SP/GIV-X)
B
(O) Except for ER operations, may be inoperative provided:
Both Engine Driven generators are operative,
Standby Electrical System is operative,
APU CONT #1 LEER C-13 and APU CONT # 2 REER C-11 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and
APU is not used.
Flight crew will ensure:
BOTH Engine Driven Generators are operative,
Standby Electrical system is operative, and
Pull and collar the APU CONT #1 LEER C-13 and APU CONT # 2 REER C-11 circuit breakers to ensure that the APU cannot be used in flight
ATC 1-2 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
C
Aeroplane may be dispatched with either transponder failed in excess of those required by Operating Requirements.
NOTE 1: Flight Director, Autopilot, and Transponder must use the same Air Data source for flight into RVSM airspace.
NOTE 2: Transponder and altitude reporting capability must be operative for flight into RVSM airspace.
None required.
BAROSET 1 Fail
(Blue – Advisory)
(GV-SP/GIV-X)
C
(O) Aeroplane may be dispatched provided:
None of the following CAS messages are also posted:
ADS 2 Fail
ADS 3 Fail
BAROSET 2 Fail
BAROSET 3 Fail
b) Manual Pressurization Control System is operative,
c) Cabin Altitude and Differential Pressure Indicators are operative,
d) Cabin Rate of Climb Indicator is operative,
e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure,
f) Autopilot is operative, and
g) Aeroplane is operated in accordance with AFM Limitations.
NOTE 1: Two systems are required for operation in RVSM airspace.
NOTE 2: Transponder and Flight Director/Autopilot must use same ADC data for RVSM.
Flight crew will ensure:
None of the following CAS messages are also posted:
ADS 2 Fail
ADS 3 Fail
BAROSET 2 FAIL
BAROSET 3 FAIL
Manual Pressurization Control System is operative,
Cabin Altitude and Differential Pressure Indicators are operative,
Cabin Rate of Climb Indicator is operative,
Flight crew select ADS sources that are independent and not associated with the BAROSET failure,
