European aviation safety agency

(Blue – Advisory)

(GV)

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.
   

(Blue – Advisory)

(GV-SP/GIV-X)

(Blue – Advisory)

(GV)

(Blue – Advisory)

(GV-SP/GIV-X)

1. 
   Alternate procedures are established and used,
   
2. 
   Pilot-Not-Flying (PNF) monitors flight progress with reference to radio altimeter data and situational awareness,
   
3. 
   PNF advises Pilot-Flying (PF) of adverse situations,
   
4. 
   Aeroplane is operated in accordance with AFM Limitations, and
   
5. 
   Repairs or replacements are carried out within 6 further flights or 25 flying hours or 2 calendar days, whichever occurs first.
   

(Blue – Advisory)

(GV)

1. 
   Alternate procedures are established and used,
   
2. 
   Pilot-Not-Flying (PNF) monitors flight progress with reference to radio altimeter data and situational awareness,
   
3. 
   PNF advises Pilot-Flying (PF) of adverse situations,
   
4. 
   Aeroplane is operated in accordance with AFM Limitations, and
   
5. 
   Repairs or replacements are carried out within 6 further flights or 25 flying hours or 2 calendar days, whichever occurs first.
   

(Blue – Advisory)

(GV-SP/GIV-X)

(Blue – Advisory)

(GV-SP/GIV-X)

a) Extended ground operations are avoided, and

b) Pilot selected HUD brightness is reduced.

(Blue – Advisory)

(GV-SP/GIV-X)

NOTE: Accuracy of hydraulic quantity indication will be degraded during long flights in cold soak conditions. If Right Hydraulic System (R SYS) sensor has failed in flight, there is no protection against overheating R SYS pumps during Power Transfer Unit (PTU) operation. In flight, with either or both sensors failed, there is no warning of hot hydraulic system temperatures.

(Blue – Advisory)

(GV)

NOTE: Accuracy of hydraulic quantity indication will be degraded during long flights in cold soak conditions. If Right Hydraulic System (R SYS) sensor has failed in flight, there is no protection against overheating R SYS pumps during Power Transfer Unit (PTU) operation. In flight, with either or both sensors failed, there is no warning of hot hydraulic system temperatures.

(Amber – Caution)

(GV-SP/GIV-X)

a) Aeroplane is operated in accordance with alternate AFM procedures,

b) Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and SAT is +10 deg C or less, and

c) Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges.

NOTE: With Ice Detection Systems inoperative, automatic anti-ice is not available.

(Amber – Caution)

(GV)

a) Aeroplane is operated in accordance with alternate AFM procedures,

b) Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and SAT is +10 deg C or less, and

c) Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges.

NOTE: With Ice Detection Systems inoperative, automatic anti-ice is not available.

(Blue – Advisory)

(GV-SP/GIV-X)

1. 
   Both PFD attitude indicating systems operate independently,
   
2. 
   Flight crew ensure same IRS is NOT used as attitude source for both pilots,
   

3. 
   Standby Attitude Indicator is operative, and
   
4. 
   Repairs are made within two (2) flight days.
   

(Blue – Advisory)

(GV)

1. 
   Both PFD attitude indicating systems operate independently,
   
2. 
   Flight crew ensure same IRS is NOT used as attitude source for both pilots,
   
3. 
   Standby Attitude Indicator is operative, and
   
4. 
   Repairs are made within two (2) flight days.
   

(Blue – Advisory)

(GV)

(Blue – Advisory)

(GV-SP/GIV-X)

(Blue – Advisory)

(GV-SP/GIV-X)

a) The affected battery is located in the #2 or #3 IRU back up battery position, and

b) Repairs are made within one (1) flight day.

1. 
   Aeroplane is operated in day VMC conditions, and
   
2. 
   Repairs are made within one (1) flight day.
   

1. 
   All other components of the Electrical Power system are operative, and
   
2. 
   Repairs are made within one (1) flight day.
   

(Blue – Advisory)

(GV)

(Blue – Advisory)

(GV-SP/GIV-X)

1. 
   Ambient Temperature is 95 degrees F (35 degrees C) or cooler,
   
2. 
   TRU electrical loads are 50% or less,
   
3. 
   Right main TRU is operative,
   
4. 
   Both Environmental Control System (ECS) Packs are operative,
   
5. 
   Flight crew minimize ground operation time, and
   
6. 
   For ground operations longer than 15 minutes, flight crew ensure main and baggage doors are closed, APU air is selected “ON” and outflow valve is fully OPEN.
   

1. 
   Minimize ground operation time, espescially during hot weather.
   
2. 
   During Ground operation, monitor TRU load – limit load to 50%.
   

For ground operation longer than 15 minutes ensure main and baggage doors are closed. APU air is selected “ON” and outflow valve is fully OPEN.

(Blue – Advisory)

(GV-SP/GIV-X)

(Blue – Advisory)

(GV-SP/GIV-X)

(Blue – Advisory)

(GV)

1. 
   Manual Pressurization Control System is operative,
   
2. 
   Cabin Altitude and Differential Pressure Indicators are operative,
   
3. 
   Cabin Rate of Climb Indicator is operative,
   
4. 
   Autopilot is operative,
   
5. 
   Aeroplane is operated in accordance with AFM limitations,
   
6. 
   MADC 1: POP A-9, MADC 2: CPOP A-9, and MADC 3: POP A-10 circuit breakers associated with the failed Micro Air Data Computer (MADC) are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and
   
7. 
   Flight crew selects operative and different MADC sources prior to departure.
   

NOTE 2: For MADC 1 FAIL, expect the L Engine Backup Air Data advisory and associated Engine Maintenance message to post.

NOTE 3: For MADC 2 FAIL, expect the R Engine Backup Air Data advisory and associated Engine Maintenance message to post.

Flight crew will operationally check and assure that the items called out in provisos a) thru d) are operative.

Flight crew will comply with all AFM limitations in section 1-03-30, 1-03-40, and 1-21-10.

(Blue – Advisory)

(GV)

1. 
   Aeroplane is not operated in visible moisture or known or forecast icing conditions,
   
2. 
   L LWR PITOT HTR: POP A-5 and R LWR PITOT HTR: CPOP A-5 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
   
3. 
   Flight crew select MADC sources that are different and not associated with failed pitot heater element,
   
4. 
   Dispatch is not authorized in conjunction with MADC 2-SBY PROBE FL, and
   
5. 
   Repairs are made within two (2) flight days.
   

(Blue – Advisory)

(GV)

1. 
   Aeroplane is not operated in visible moisture or known or forecast icing conditions,
   
2. 
   L UPR PITOT HTR: POP A-6 and R UPR PITOT HTR: CPOP A-4 circuit breakers are pulled and collared. Flight crew may accomplish this task if properly qualified and authorized,
   
3. 
   Flight crew select MADC sources that are different and not associated with failed pitot heater element, and
   
4. 
   Dispatch is not authorized in conjunction with MADC 1-2 PROBE FL, and
   
5. 
   Repairs are made within two (2) flight days.
   

(Amber – Caution)

(GV-SP/GIV-X)

1. 
   Fuel Crossflow Valve is operative,
   
2. 
   Fuel Intertank Valve is operative,
   
3. 
   Both Fuel Low Quantity Warning Systems are operative,
   
4. 
   Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure,
   
5. 
   Dispatch is not authorized in conjunction with Alternate Pump Fail, L-R or with Alt FuelPump Fail, L-R, and
   
6. 
   Aeroplane is operated in accordance with AFM Limitations.
   

1. 
   Fuel Crossflow Valve and Intertank Valve are operative,
   
2. 
   BOTH Fuel Low Quantity Warning Systems are operative,
   
3. 
   Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure.
   

(Amber – Caution)

(GV)

1. 
   Fuel Crossflow Valve is operative,
   
2. 
   Fuel Intertank Valve is operative,
   
3. 
   Both Fuel Low Quantity Warning Systems are operative,
   
4. 
   Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure,
   
5. 
   Dispatch is not authorized in conjunction with ALT PUMP FAIL, L-R, and
   
6. 
   Aeroplane is operated in accordance with AFM Limitations.
   

1. 
   Fuel Crossflow Valve and Intertank Valve are operative,
   
2. 
   BOTH Fuel Low Quantity Warning Systems are operative,
   
3. 
   Verify compliance with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure.
   

(Blue – Advisory)

(GV)

(Amber – Caution)

(GV-SP/GIV-X)

a) Both Generators are operative,

b) Both essential TRU’s are operative,

c) Auxiliary TRU is operative,

d) APU Generator is operative,

e) Both Battery chargers are operative,

f) Both Main Aeroplane Batteries are operative,

g) Inoperative L MAIN TRU: LPDB, Left Main AC section or R MAIN TRU: RPDB, Right Main AC section TRU circuit breaker on the Power Distribution Box is pulled and collared. Flight crew may accomplish this task if properly qualified and authorized, and

h) Repairs are made within two (2) flight days.

Flight crew will ensure AUX TRU is operative and both essential TRUs are operative.

(Blue – Advisory)

(GV-SP/GIV-X)

1. 
   With one (1) failed fan provided performance of items affected by the indicated MAU are monitored during the flight,
   
2. 
   Flight crew references the appropriate matrix in AFM Section 03-16-80, and
   
3. 
   Repairs are made within two (2) flight days.