European aviation safety agency

(Blue – Advisory)

(GV-SP/GIV-X)

1. 
   Aeroplane does not exceed 8 further consecutive flights with flight data recorder unserviceable,
   
2. 
   Not more than 72 hours have elapsed since flight data recorder was found to be unserviceable, and
   
3. 
   Any cockpit voice recorder required to be carried is operative.
   

a) Loss of flight recording function is evident to flight crew during pre-flight check e.g. by means of a system status monitor,

b) Need for maintenance has been identified by system monitors, where available, with setting of an indicator and cause of that setting has not been determined, or

c) Analysis of recorded data or maintenance actions have shown that more than 5% of the total number of individual parameters (variable and discrete), required to be recorded for the particular aircraft, are not being recorded properly.

NOTE 2: Where improper recording affects 5% of the parameters or less, timely corrective action will need to be taken by aeroplane operator in accordance with approved maintenance procedures.

(Amber – Caution)

(GV)

NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations.

(Amber – Caution)

(GV-SP/GIV-X)

(Amber – Caution)

(GV)

(Blue – Advisory)

(GV-SP)

(Blue – Advisory)

(GIV-X)

(Blue – Advisory)

(GV-SP)

1. 
   Electric Pitch Trim System is operative,
   
1. 
   Alternate control is verified to be operative before each departure, and
   
2. 
   Repairs are made within two (2) flight days.
   

(Blue – Advisory)

(GV)

(Blue – Advisory)

(GV)

1. 
   Electric Pitch Trim System is operative,
   
1. 
   Alternate control is verified to be operative before each departure, and
   
2. 
   Repairs are made within two (2) flight days.
   

(Blue – Advisory)

(GV-SP/GIV-X)

a) FMS position is checked against available sensors, and

b) If errors encountered, affected GPS is de-selected as a position sensor and FMS position is updated.

(Blue – Advisory)

(GV-SP/GIV-X)

1. 
   Affected system is not required for IRS alignment,
   
2. 
   Long Range Navigation is not dependent on its use,
   
3. 
   Procedures do not require its use,
   
4. 
   Both RFMU’s are operative (GV), and
   
5. 
   Repairs are made within two (2) flight days.
   

(Blue – Advisory)

(GV)

1. 
   Affected system is not required for IRS alignment,
   
2. 
   Long Range Navigation is not dependent on its use,
   
3. 
   Procedures do not require its use,
   
4. 
   Both RFMU’s are operative (GV), and
   
5. 
   Repairs are made within two (2) flight days.
   

(Blue – Advisory)

(GV-SP/GIV-X)

a) None of the following CAS messages are also posted:

Aft Cabin Temp Fan Fail;

Cockpit Temp Fan Fail;

b) Forward Temperature Manual mode is operative,

c) Associated temperature indicator is operative,

d) FWD CABIN SENSOR FAN, LEER D-9, is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and

e) Flight crew monitor forward cabin temperature and forward cabin duct temperature.

1. 
   None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Cockpit Temp Fan Fail,
   
2. 
   Forward Cabin Temperature Manual mode is operative,
   
3. 
   Associated temperature indicator is operative,
   
4. 
   FWD CABIN SENSOR FAN circuit breaker: LEER D-9 is pulled and collared, and
   
5. 
   Forward cabin temperature and Forward cabin duct temperature are monitored.
   

(Blue – Advisory)

(GV-SP/GIV-X)

(Blue – Advisory)

(GV)

(Blue – Advisory)

(GV-SP/GIV-X)

(continued)

1. 
   Both tanks are completely filled using overwing refueling in accordance with the Aircraft Operating Manual, Section 09-02-00,
   
2. 
   Both Fuel Flow Indicating Systems are operative,
   
3. 
   After takeoff, power is set by matching fuel flow indications on both engines, and
   
4. 
   Flight crew maintains a log of fuel burned.
   

NOTE: Total Fuel indications will be INVALID with inoperative indicator.

NOTE: Do not pull Fuel Qty circuit breaker as this disables Fuel Level Low caution message.

Flight crew will ensure:

1. 
   Both Fuel Flow Indicating Systems are operative.
   
2. 
   After takeoff, power is set by matching Fuel Flow indications on both engines.
   
3. 
   A log of fuel burned is maintained.
   

(Blue – Advisory)

(GV-SP/GIV-X) (cont’d)

1. 
   Affected tank is defueled before each refueling in accordance with the Aircraft Operating Manual, Section 09-02-00,
   
2. 
   Affected tank is fueled with a known quantity of fuel,
   
3. 
   Both fuel flow meters are operative,
   
4. 
   After takeoff, power is set by matching fuel flow indications on both engines, and
   
5. 
   Flight crew maintains a log of fuel burned.
   

Flight crew will ensure:

1. 
   Both fuel flow meters are operative.
   
2. 
   After takeoff, power is set by matching Fuel Flow indications on both engines.
   
3. 
   A log of fuel burned is maintained.
   

(Blue – Advisory)

(GV)

(continued)

1. 
   Both tanks are completely filled using overwing refueling in accordance with the Aircraft Operating Manual, Section 09-02-00,
   
2. 
   Both Fuel Flow Indicating Systems are operative,
   
3. 
   After takeoff, power is set by matching fuel flow indications on both engines, and
   
4. 
   Flight crew maintains a log of fuel burned.
   

NOTE: Do not pull Fuel Qty circuit breaker as this disables Fuel Level Low caution message.

Flight crew will ensure:

1. 
   Both Fuel Flow Indicating Systems are operative.
   
2. 
   After takeoff, power is set by matching Fuel Flow indications on both engines.
   
3. 
   A log of fuel burned is maintained.
   

(Blue – Advisory)

(GV) (cont’d)

1. 
   Affected tank is defueled before each refueling in accordance with the Aircraft Operating Manual, Section 09-02-00,
   
2. 
   Affected tank is fueled with a known quantity of fuel,
   
3. 
   Both fuel flow meters are operative,
   
4. 
   After takeoff, power is set by matching fuel flow indications on both engines, and
   
5. 
   Flight crew maintains a log of fuel burned.
   

Flight crew will ensure:

1. 
   Both fuel flow meters are operative.
   
2. 
   After takeoff, power is set by matching Fuel Flow indications on both engines.
   
3. 
   A log of fuel burned is maintained.
   

(Amber – Caution)

(GV-SP/GIV-X)

1. 
   Aeroplane is not operated in known or forecast icing conditions, and
   
2. 
   Both side window heat systems are operative.
   

(Blue – Advisory)

(GV-SP/GIV-X)

(Amber – Caution)

(GV-SP/GIV-X)

1. 
   All Fuel Boost Pumps are operative,
   
2. 
   Fuel Intertank Valve is operative,
   
3. 
   Fuel Quantity Indicating System is operative,
   
4. 
   Fuel Tank Temperature System is operative, and
   
5. 
   Aeroplane is operated in accordance with AFM Limitations.
   

1. 
   All Fuel boost Pumps are operative,
   
2. 
   Fuel Intertank Valve is operative,
   
3. 
   Fuel Quantity Indicating System is operative,
   
4. 
   Fuel tank temperature system is operative.
   

(Blue – Advisory)

(GV-SP)

a) Flight crew monitors fuel tank temperature, and

b) Aeroplane is operated in accordance with AFM Limitations.

(Blue – Advisory)

(GV)

a) Flight crew monitors fuel tank temperature, and

b) Aeroplane is operated in accordance with AFM Limitations.

(Blue – Advisory)

(GV)

a) None of the following CAS messages are also posted:

Aft Cabin Temp Fan Fail;

Cockpit Temp Fan Fail;

b) Forward Temperature Manual mode is operative,

c) Associated temperature indicator is operative,

d) FWD CABIN SENSOR FAN, LEER D-9, is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and

e) Flight crew monitor forward cabin temperature and forward cabin duct temperature.

1. 
   None of the following CAS messages are also posted: Aft Cabin Temp Fan Fail; Cockpit Temp Fan Fail,
   
2. 
   Forward Cabin Temperature Manual mode is operative,
   
3. 
   Associated temperature indicator is operative,
   
4. 
   FWD CABIN SENSOR FAN circuit breaker: LEER D-9 is pulled and collared, and
   
5. 
   Forward cabin temperature and Forward cabin duct temperature are monitored.
   

(Amber – Caution)

(GV)

1. 
   Aeroplane is not operated in known or forecast icing conditions, and
   
2. 
   Both side window heat systems are operative.
   

(Blue – Advisory)

(GV-SP/GIV-X)

1. 
   APU Generator is used for all phases of flight,
   
1. 
   Aeroplane is operated at or below FL450,
   
2. 
   Standby Electrical System is operative, and
   
3. 
   Repairs are made within two (2) flight days.
   

(Blue – Advisory)

(GV)

1. 
   APU Generator is used for all phases of flight,
   
2. 
   Aeroplane is operated at or below FL450,
   
3. 
   Standby Electrical System is operative, and
   
4. 
   Repairs are made within two (2) flight days.
   

(Blue – Advisory)

(GV-SP/GIV-X)

1. 
   Opposite Generator and GCU is operative,
   
2. 
   APU Generator is used for all phases of flight,
   
3. 
   Aeroplane is operated at or below FL450,
   
4. 
   Standby Electrical System is operative, and
   
5. 
   Repairs are made within two (2) flight days.