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### 107 Cards in this Set

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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 MMO M .89 at 30,267 ft to M 842 @ 51,000 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