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91 Cards in this Set
- Front
- Back
Minimum battery voltage for an APU start
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21 Volts
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Maximum operating altitude
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41,000 ft
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Maximum altitude takeoff & landing
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8,000 ft
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Minimum altitude takeoff & landing
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-1,000 ft
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Load Factor: Flaps UP
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+2.5g to -1.0g
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Load Factor: Flaps DOWN
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+2g to 0g
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Maximum runway slope
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+/- 2%
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Approved runway surface
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Paved
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Maximum tailwind takeoff and landing
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10kts
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Maximum crosswind for takeoff and landing: Dry
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28 kts sustained, with gusts to 38 kts
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Maximum crosswind for takeoff and landing: Wet
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28 kts
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Maximum crosswind for takeoff and landing: Compacted Snow
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20kts
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Maximum crosswind for takeoff and landing: Standing water/slush/wet snow/dry snow
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18 kts
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Maximum crosswind for takeoff and landing: With Ice (no melting)
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12 kts
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Maximum wind limits for a CAT II approach: Headwind
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25 kts
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Maximum crosswind for a CAT II approach: Tailwind
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10 kts
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Maximum crosswind for a CAT II approach: Crosswind
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12 kts
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Maximum temp for takeoff and landing
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ISA +35
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Minimum temp for takeoff
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-40
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Maximum taxi speed for straight DRY or WET
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30 kts
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Maximum taxi speed for straight CONTAMINATED
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15 kts
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TRUE/FALSE The airplane may never be operated below the green dot speed
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TRUE
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VMO
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320 KIAS
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MMO
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.82 Mach
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Maximum turbulent air penetration speed: Less than 10,000' MSL
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250 KIAS
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Maximum turbulent air penetration speed: Greater than or equal to 10,000' MSL
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270 KIAS/.76 Mach (whichever is less)
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Minimum RAT speed
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130 KIAS
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Oxygen Quantity Color: Green
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Normal range (minimum for dispatch with three crewmembers on the flight deck)
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Oxygen Quantity Color: Cyan
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Normal range (minimum for dispatch with two crewmembers on the flight deck)
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Oxygen Quantity Color: Amber
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Cautionary range (dispatch is not allowed)
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Cabin Pressurization: Up to 37,000 ft
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7.8 psi
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Cabin Pressurization: Above 37,000 ft
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8.3 psi
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Cabin Pressurization: Max differential overpressure
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8.7 psi
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Cabin Pressurization: Max differential negative pressure
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-0.5 psi
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Cabin Pressurization: Max differential pressure for TO/LNDG
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0.2 psi
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Maximum altitude for single pack operation
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FL310
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Autopilot: Min height to engage on takeoff
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Acceleration altitude
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Autopilot: Min height to engage on go-around
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400' AGL
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Autopilot: Min en route height
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500' AGL
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Autopilot: Min height for non-precision approach
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MDA
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Autopilot: Min height for a precision approach
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70' AGL
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Autopilot: Special instrument approach
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As specified in the procedure
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Maintenance is required if the battery voltage is less than
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21 Volts
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Minimum battery temp for an APU start
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-20C
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When airplane is stopped, taxi and landing lights must be
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OFF
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For takeoff and in flight, the taxi nose light must be
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OFF
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How long must you wait after power from GPU or APU is transferred before shutting down engines?
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10 seconds
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Maximum altitude for flap extension
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20,000 ft
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Flap speed limits: Flaps 1
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230 KIAS
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Flap speed limits: Flaps 2
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215 KIAS
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Flap speed limits: Flaps 3
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200 KIAS
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Flap speed limits: Flaps 4
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180 KIAS
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Flap speed limits: Flaps 5
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180 KIAS
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Flap speed limits: Flaps Full
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165 KIAS
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Maximum useable fuel
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20,785 lbs
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Maximum fuel imbalance in flight
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794 lbs
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Minimum fuel tank temp
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-40C
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During takeoff and landing the crossfeed selector knob must be
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OFF
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A hydraulic system warm-up must be accomplished before starting the engines if the reservoir temps are below
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-18C
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How do you determine if you are in SLD
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If abnormal ice formation is observed on areas of the airplane that do not usually accrete ice. You must exit SLD.
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The MCDU TO DATASET MENU must be set to ENG when SAT is 5C to 10C and:
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1. Visible moisture will be encountered up to 1700 ft AFE or, 2. Operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines nacelles, or engine sensor probes.
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The MCDU TO DATASET MENU must be set to ALL when SAT is less than 5C and:
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1. Visible moisture will be encountered up to 1700 ft AFE or, 2. Operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines nacelles, or engine sensor probes.
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Icing Conditions definition:
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Icing conditions exist in flight whenever the SAT on the ground or for takeoff, or TAT in flight, is 10C or below and in visible moisture
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If either one or both ice detectors fail, the crew must set the mode selector to ON when:
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icing conditions exist or are anticipated below 10C TAT with visible moisture
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Maximum speed to operate the windshield wipers
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250 KIAS
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VLO (landing gear extension)
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250 KIAS
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VLO (landing gear retraction)
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250 KIAS
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VLE
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250 KIAS
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Maximum ground speed (tire speed)
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195 KIAS
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Minimum runway/taxiway width for a 180 deg. Turn (E170)
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54' 8”
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Minimum runway/taxiway width for a 180 deg. Turn (E175)
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59' 2”
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What altimeter setting must be used for CAT I approach?
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Baro
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The VOR flight director mode is prohibited
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...nothing more to say about that.
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Back course approaches using the IESS are prohibited
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...nothing more to say about that.
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Minimum Air Temp for APU start
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-54C
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Maximum altitude for APU start
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30,000 ft
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Maximum altitude for APU GEN
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33,000 ft
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Maximum altitude for Bleed Air
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15,000 ft
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Maximum altitude for APU-assisted Engine Start
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21,000 ft
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APU starter duty cycle limitations:
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1 & 2: ON for 60, OFF for 60. 3: ON for 60, OFF for 5
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How long must the engines be stabilized before stopping the APU?
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5 seconds or power transfer confirmed on the synoptic page
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What N2 % must the engines be after shutdown, and before starting the APU?
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30% N2
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Maximum temp during engine start
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815C
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For takeoffs, the ATTCS must be
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ON
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Engine warm-up and cool down period
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2 minutes
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Starter Limits: Dry Motoring
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1st attempt – 90 seconds on, 5 minutes off. 2nd through 5th attempt – 30 seconds on, 5 minutes off
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Starter Limits: With Fuel Added
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1st and 2nd attempt – 90 seconds on the ground, or 120 seconds in the air, followed by 10 seconds off. 3rd through 5th attempts – 90 seconds on the ground, or 120 seconds in flight, followed by 5 minutes off
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Powerback Operations
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PROHIBITED
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Thrust Reverser: Engines must be idle by
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60 KIAS
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Thrust Reverser: Engines must be out of reverse by
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30 KIAS
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No FLEX if: (5 items)
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1. Runway is contaminated 2. The antiskid is inop 3. T/O performance section does not include FLEX T/O data 4. 10-7 pages prohibit FLEX 5. The PIC determines that FLEX is unsafe.
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