Global Express
Terms
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- Maximum Ramp Weight
- 98,250 lbs
- Maximum T/O Weight
- 98,000 lbs
- Maximum Landing Weight
- 78,600 lbs
- Maximum Zero Fuel Weight
- 56,000 lbs
- Minimum Operating Empty Weight
- 45,000 lbs
- VMO
-
300 KIAS SL to 8,000 ft
340 KIAS 8,000 to 30,267 ft - VMCG
- 80 KIAS
- VMCA
- 86 KIAS
- VLO
- 200 KIAS
- Turb Penetration
- 300 KIAS or M .80 whichever is lower
- Max Tire Speed
- 183
- VLE
- 250
- MLE
- M .70
- VFE Slats
- 225 KIAS
- VFE Flaps 6
- 210 KIAS
- VFE Flaps 16
- 210 KIAS
- VFE Flaps 30
- 185 KIAS
- The maximum speed that it is safe to extend and retract the gear
- 200 KIAS
- Maximum speed at which the airplane may be flown with the gear down is
- 250 KIAS
- What is the maximum altitude that you can fly with the gear down?
- 20,000 ft
- Maximum airport pressure altitude is for take off and landing is
- 10,000 ft
- Maximum Operating Altitude is
- 51,000 ft
- Maximum ambient air temperature approved for take off and landing is
- +50 deg C
- Minimum ambient temperature approved for take off is
- -30 or -40 deg C ???
- During takeoff, use of cowl anti-ice in ______ is prohibited
- AUTO MODE
- When must the cowl anti-ice be selected on for takeoff
- OAT is 10 deg C or less with visible moisture or a contaminated runway
- Icing conditions exist in flight when?
- The TAT is 10 deg C or below and visible moisture except when the SAT is -40 deg C
- During takeoff, the use of wing anti-ice in ______ is prohibited
- AUTO MODE
- When must the wing anti-ice be selected on for takeoff
- When the OAT is 5 deg C or less in visible moisture or contaminated runway
- The maximum runway slopes approved for takeoff and landing is
-
+2% uphill
-2% downhill - The maximum tailwind component approved for takeoff and landing is
- 10 Kts
- Engine starts are not permitted when the tailwind componentexceeds
- 20 kts
- Total fuel left main tank
- 15,050 lbs
- Total fuel right main tank
- 15,050 lbs
- Total fuel center tank
- 11,150 lbs
- Total aft tank
- 2,300 lbs
- Total fuel
- 43,550 lbs
- When the wing tanks have more than 20,250 lbs the on ground, max imbalance is
- 600 lbs
- Max fuel imbalance in flight is
- 1100 lbs
- The engine starter must not be used for start if the indicated RPM exceeds
- 42% N2
- What is the minimum fuel quantity for a go around per wing
- 600 lbs
- When using wide cut fuels operation is limited to ______ ft until the bulk fuel temp is below ______deg C
- 13,000 ft, 15 deg C
- Minimum Bulk Fuel for take-off
- -30 deg C
- Maximum Bulk Fuel for take-off
- 54 deg C
- Bulk Fuel Freezing Point
- -40 deg C
- Minimum Engine Fuel Temperature for take-off
- 5 deg C
- Fuel Recirc must be _____ for take-off and initial climb to altitude
- Off
- Fuel Recirc must be off below?
- 34,000 ft
- It is recommended that the Fuel Recirc be turned on when the bulk fuel temp reaches ______
- -25 deg C
- What is the maximum oil consumption per engine?
- 0.2 litre per hour
- Minimum Oil Temp for start is
- -40 deg C
- Minimum Oil Temp before the engine can be accelerated above idle is
- +20 deg C
- Maximum Permissible Oil Temp is
- +160 deg C
- It is prohibited to replenish the engine oil when the OAT is
- less then -12 deg C
- The autothrottle must be engaged and take-off thrust verified prior to ______ for autothrottle engaged take-off
- 60 KIAS
- Maximum APU RPM is
- 106%
- Maximum APU EGT for start is
- 675 deg C to 1038 deg C
- APU EGT for Normal Operations is
- 613 deg C to 732 deg C
- Maximum Operating Altitude for the APU is
- 45,000 ft
- Minimum ambient temp for starting a cold soaked APU is
- -40 deg C
- The max number of start attempts per hour for the APU is
- 3
- Maximum altitude to start the APU is
- 37,000 ft
- Maximum altitude to extract Bleed Air is
- 30,000 ft
- It is prohibited to extract Bleed Air for air conditioning if the OAT is above
- 45 deg C
- Manueuveing Load Limit Factors
-
Slats/Flaps Retracted -1 to +2.5 G
Slats/Flaps Extended 0.0 to +2.0 G - Pack Discharge Temps during manual mode temp control must be kept between
- 5 deg C and 60 deg C
- If you are in manual pressurization control what must you do with the packs
- Turn one off
- The maximum relief differential pressure is
- 10.73 psi
- The maximum negative relief differential pressure is
- -0.5 psi
- At touchdown on landing the pressure diff must not exceed
- 1.0
- AUX PRESS system operations are prohibited at altitudes above
- 41,000 ft
- Maximum altitude for flight with the yaw damper disengaged is
- 41,000 ft
- The minimum autopilot engage height is
- 400 ft AGL
- The minimum autopilot use height for a precision appr is
- 50 ft AGL
- The minimum autopilot use height for a non-precision appr is
- 400 ft AGL
- USE of FLC with the speed bug above M .85 is
- Prohibited
- The APU Generator load limit is
- 40 KVA
- For operations above ______ if the APU generator is powering a bus the associated _______ must be selected off
- 37,000, hydraulic
- Flight Spoilers must be retracted below
- 300 ft
- Flight with flaps/slats extended at altitudes above _______ is prohibited
- 18,000 ft
- During QFE operations with no GPS sensors available the EGPWS system must be inhibited by selecting the TERRAIN switch to OFF
- N/A
- The TERR switch must be selected off nwhen within ____ nm of an airport not in the database
- 15
- The terrain database does not account for man-made obstructions except for asll known man-made obstructions in Canada, The US and Mexico
- N/A
- The FMS must not be used as a navigation source it is receiving suitable navigation information from what sources?
-
One VOR/DME, or
Two DME's, or
One IRS - Use of FMS as a sole NAV source for inst apprs past the final appr fix is prohibited unless _____ is displayed on the PFD
- APP
- How many FMS's must be installed and operating and receiving information from at least two inertial ref systems to operate legally into MNPS airspace?
- 2
- The use of GPS is approved for supplemental means of enroute and terminal operations.
- N/A
- Are GPS only approaches approved?
- Yes
- Are RNP 5 operations approved
- Yes
- RNP 10 is approved. How long can you fly in NAV with out the IRS's updating
- 6.2 hours, Unlimited with a second GPS installed
- The use of VNAV is prohibited when the baro altitude is set to landing field elevation in QFE Ops
- N/A
- What is the maximum operating airspeed in RVSM airspace
- M .86
- What is the maximum altimeter difference to remain in RVSM airspace
- 200 ft between the coupled altimeter and either of the other primary sources
- To be legal in RVSM ops the autopilot must be coupled to the same active ADC as the active ______
- Transponder
- What required equipment must you have and how many of each item must be operational to operate in RVSM airspace
-
Autopilot(2) 1 Operational
Altitude Alert Sys (2) 1 Oper
ATC Transponder (2) 1 Oper
Micro ADC (3) 2 Oper
Pitot Probe Heat (4) 2 Oper - If operating with the RAT deployed are RVSM requirements met?
- No
- FMS TOLD informations is advisory only
- N/A
- When the x wind component exceeds 20 kts the RWY REQ must be increased by
-
1700 ft for flap 6 and
1500 ft for flap 16 - When is the use of the FMS TOLD function prohibited
- When the OAT is below -30 deg C or above +45 deg C
- The use of FMS 3 for TOLD calculations is prohibited
- N/A
- The FMS TOLD function is prohibited during QFE ops
- N/A
- When operating single engine the "cowl anti-ice on" must be selected on on the FMS regardless of the whether it is actually on or not
- N/A
- For tailwind operations you must increase the FMS TOLD take-off field length by _____ and the landing field length by _______.
- 65 ft and 110 ft
- For take-offs with one TR inop use the 0 TR operative distance
- N/A
- Is the use of the FLEX mode on the FMS for take-off approved
- No
- When is the use of the FMS TOLD functions prohibited
-
WING ANTI-ICE FAIL message
BRAKE TEMP message
Contaminated Rwys
Airport Elev above 10,000 ft
QFE Ops