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107 Cards in this Set
- Front
- Back
Maximum Ramp Weight
|
98,250 lbs
|
|
Maximum T/O Weight
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98,000 lbs
|
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Maximum Landing Weight
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78,600 lbs
|
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Maximum Zero Fuel Weight
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56,000 lbs
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Minimum Operating Empty Weight
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45,000 lbs
|
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VMO
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300 KIAS SL to 8,000 ft
340 KIAS 8,000 to 30,267 ft |
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MMO
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M .89 at 30,267 ft to M 842 @ 51,000
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VMCG
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80 KIAS
|
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VMCA
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86 KIAS
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VLO
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200 KIAS
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Turb Penetration
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300 KIAS or M .80 whichever is lower
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Max Tire Speed
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183
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VLE
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250
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MLE
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M .70
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VFE Slats
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225 KIAS
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VFE Flaps 6
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210 KIAS
|
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VFE Flaps 16
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210 KIAS
|
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VFE Flaps 30
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185 KIAS
|
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The maximum speed that it is safe to extend and retract the gear
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200 KIAS
|
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Maximum speed at which the airplane may be flown with the gear down is
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250 KIAS
|
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What is the maximum altitude that you can fly with the gear down?
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20,000 ft
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Maximum airport pressure altitude is for take off and landing is
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10,000 ft
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Maximum Operating Altitude is
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51,000 ft
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Maximum ambient air temperature approved for take off and landing is
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+50 deg C
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Minimum ambient temperature approved for take off is
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-30 or -40 deg C ???
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During takeoff, use of cowl anti-ice in ______ is prohibited
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AUTO MODE
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When must the cowl anti-ice be selected on for takeoff
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OAT is 10 deg C or less with visible moisture or a contaminated runway
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Icing conditions exist in flight when?
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The TAT is 10 deg C or below and visible moisture except when the SAT is -40 deg C
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During takeoff, the use of wing anti-ice in ______ is prohibited
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AUTO MODE
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When must the wing anti-ice be selected on for takeoff
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When the OAT is 5 deg C or less in visible moisture or contaminated runway
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The maximum runway slopes approved for takeoff and landing is
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+2% uphill
-2% downhill |
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The maximum tailwind component approved for takeoff and landing is
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10 Kts
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Engine starts are not permitted when the tailwind componentexceeds
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20 kts
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Total fuel left main tank
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15,050 lbs
|
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Total fuel right main tank
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15,050 lbs
|
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Total fuel center tank
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11,150 lbs
|
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Total aft tank
|
2,300 lbs
|
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Total fuel
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43,550 lbs
|
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When the wing tanks have more than 20,250 lbs the on ground, max imbalance is
|
600 lbs
|
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Max fuel imbalance in flight is
|
1100 lbs
|
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The engine starter must not be used for start if the indicated RPM exceeds
|
42% N2
|
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What is the minimum fuel quantity for a go around per wing
|
600 lbs
|
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When using wide cut fuels operation is limited to ______ ft until the bulk fuel temp is below ______deg C
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13,000 ft, 15 deg C
|
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Minimum Bulk Fuel for take-off
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-30 deg C
|
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Maximum Bulk Fuel for take-off
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54 deg C
|
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Bulk Fuel Freezing Point
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-40 deg C
|
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Minimum Engine Fuel Temperature for take-off
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5 deg C
|
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Fuel Recirc must be _____ for take-off and initial climb to altitude
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Off
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Fuel Recirc must be off below?
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34,000 ft
|
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It is recommended that the Fuel Recirc be turned on when the bulk fuel temp reaches ______
|
-25 deg C
|
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What is the maximum oil consumption per engine?
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0.2 litre per hour
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Minimum Oil Temp for start is
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-40 deg C
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Minimum Oil Temp before the engine can be accelerated above idle is
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+20 deg C
|
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Maximum Permissible Oil Temp is
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+160 deg C
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It is prohibited to replenish the engine oil when the OAT is
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less then -12 deg C
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The autothrottle must be engaged and take-off thrust verified prior to ______ for autothrottle engaged take-off
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60 KIAS
|
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Maximum APU RPM is
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106%
|
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Maximum APU EGT for start is
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675 deg C to 1038 deg C
|
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APU EGT for Normal Operations is
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613 deg C to 732 deg C
|
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Maximum Operating Altitude for the APU is
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45,000 ft
|
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Minimum ambient temp for starting a cold soaked APU is
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-40 deg C
|
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The max number of start attempts per hour for the APU is
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3
|
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Maximum altitude to start the APU is
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37,000 ft
|
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Maximum altitude to extract Bleed Air is
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30,000 ft
|
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It is prohibited to extract Bleed Air for air conditioning if the OAT is above
|
45 deg C
|
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Manueuveing Load Limit Factors
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Slats/Flaps Retracted -1 to +2.5 G
Slats/Flaps Extended 0.0 to +2.0 G |
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Pack Discharge Temps during manual mode temp control must be kept between
|
5 deg C and 60 deg C
|
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If you are in manual pressurization control what must you do with the packs
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Turn one off
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The maximum relief differential pressure is
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10.73 psi
|
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The maximum negative relief differential pressure is
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-0.5 psi
|
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At touchdown on landing the pressure diff must not exceed
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1.0
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AUX PRESS system operations are prohibited at altitudes above
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41,000 ft
|
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Maximum altitude for flight with the yaw damper disengaged is
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41,000 ft
|
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The minimum autopilot engage height is
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400 ft AGL
|
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The minimum autopilot use height for a precision appr is
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50 ft AGL
|
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The minimum autopilot use height for a non-precision appr is
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400 ft AGL
|
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USE of FLC with the speed bug above M .85 is
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Prohibited
|
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The APU Generator load limit is
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40 KVA
|
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For operations above ______ if the APU generator is powering a bus the associated _______ must be selected off
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37,000, hydraulic
|
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Flight Spoilers must be retracted below
|
300 ft
|
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Flight with flaps/slats extended at altitudes above _______ is prohibited
|
18,000 ft
|
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During QFE operations with no GPS sensors available the EGPWS system must be inhibited by selecting the TERRAIN switch to OFF
|
N/A
|
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The TERR switch must be selected off nwhen within ____ nm of an airport not in the database
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15
|
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The terrain database does not account for man-made obstructions except for asll known man-made obstructions in Canada, The US and Mexico
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N/A
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The FMS must not be used as a navigation source it is receiving suitable navigation information from what sources?
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One VOR/DME, or
Two DME's, or One IRS |
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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
|
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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?
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2
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The use of GPS is approved for supplemental means of enroute and terminal operations.
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N/A
|
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Are GPS only approaches approved?
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Yes
|
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Are RNP 5 operations approved
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Yes
|
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RNP 10 is approved. How long can you fly in NAV with out the IRS's updating
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6.2 hours, Unlimited with a second GPS installed
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The use of VNAV is prohibited when the baro altitude is set to landing field elevation in QFE Ops
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N/A
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What is the maximum operating airspeed in RVSM airspace
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M .86
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What is the maximum altimeter difference to remain in RVSM airspace
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200 ft between the coupled altimeter and either of the other primary sources
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To be legal in RVSM ops the autopilot must be coupled to the same active ADC as the active ______
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Transponder
|
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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 |
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If operating with the RAT deployed are RVSM requirements met?
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No
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FMS TOLD informations is advisory only
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N/A
|
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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 |
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When is the use of the FMS TOLD function prohibited
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When the OAT is below -30 deg C or above +45 deg C
|
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The use of FMS 3 for TOLD calculations is prohibited
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N/A
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The FMS TOLD function is prohibited during QFE ops
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N/A
|
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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
|
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For tailwind operations you must increase the FMS TOLD take-off field length by _____ and the landing field length by _______.
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65 ft and 110 ft
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For take-offs with one TR inop use the 0 TR operative distance
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N/A
|
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Is the use of the FLEX mode on the FMS for take-off approved
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No
|
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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 |