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15 Cards in this Set
- Front
- Back
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Manoeuvring Limit Load Factors?
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Flaps/Slats retracted is
+2.5g to -1.0g Flaps/Slats extended is +2.0 to 0.0g Flaps retracted/Slats extended is +2.0 to 0.0g |
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Runway slope for Takeoff or Landing
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+1.7% to -2.0%
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Limiting tailwind component for takeoff and landing?
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10 knots
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Engine takeoff wind limitations
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Limiting crosswind component is
40 knots For crosswind components greater than 40 knots or tailwind components greater than 10 knots, only taxi and ground handling is allowed, with engine N1 limited to 50% |
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Vmo/Mmo?
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Vmo 340KIAS from sea level to 26,000 feet
Mmo is .82 Mach above 26,000 feet. |
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Flaps/Slats maximum speeds?
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Maximum mach no .57
Slats only = 280 KIAS Flaps 0 to 10 = 280 KIAS Flaps 10.1 to 20 = 240 KIAS Flaps 20.1 to 25 = 220 KIAS Flaps 25.1 to 40 = 200 KIAS |
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Gear down speeds?
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Maximum mach no. = .70
Retraction = 250 KIAS Extension = 300 KIAS Extended = 300 KIAS |
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Maximum certified altitude
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37,000 feet
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Kinds of Operation?
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Transport Category
VFR day and night IFR Icing conditions Backing with reverse thrust |
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Reduced thrust operations?
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Must establish a means to verify availability of takeoff thrust to ensure that engine deterioration does not exceed authorised limits
Permitted on wet runways when using wet runway takeoff performance Not authorised on runways contaminated with standing water, loose snow, slush, compacted snow or wet ice. Not permitted where items affecting performance cause a significant increase in crew workload. |
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Evacuation system?
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FLOW switch must be in NORM for takeoff
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Cabin pressurisation?
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Max cabin differential pressure is
7.86 psi Max emergency relief pressure is 8.27 psi If operating in manual mode, takeoff and land unpressurised |
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Autoland maximum wind components?
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Headwind to 25 knots
Tailwind to 10 knots Crosswind to 15 knots |
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Do not conduct autoland operations if...
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ALIGN mode is not annunciated on the FMA by 100 feet RADALT
Any unusual control position or other abnormal conditions exist in the flight control system "RUDDER PWR OFF" alert is displayed Airport field elevation exceeds 8,000 MSL Runway slope for landing exceeds +0.8% to -0.8% |
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Autopilot?
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During takeoff, do not engage the autopilot below 200' AGL
Do not conduct an auto coupled (ILS or autoland) approach if "STAB OUT OF TRIM" alert illuminates for longer than 3 seconds after airplane is stabilized and tracking glideslope For non-precision approaches, the autopilot must be disengaged no lower than the applicable minimums minus 50 feet. |
