B757 Review Questions. Limitations What is the maximum gear operating/extended speed? 270/.82M.
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Transcript of B757 Review Questions. Limitations What is the maximum gear operating/extended speed? 270/.82M.
![Page 1: B757 Review Questions. Limitations What is the maximum gear operating/extended speed? 270/.82M.](https://reader038.fdocuments.net/reader038/viewer/2022110320/56649c9c5503460f9495a3ef/html5/thumbnails/1.jpg)
B757 Review Questions
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Limitations
• What is the maximum gear operating/extended speed?
• 270/.82M
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Limitations
• What is the maximum alternate gear operating/extended speed?
• 250/.75M
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Limitations
• What is the maximum turbulent air penetration speed?
• 290kts/.78M
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Limitations
• What is the maximum takeoff/landing pressure altitude? 757? 767?
• 757= 9500’
• 767= 8400’
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Limitations
• What is the maximum tailwind component for takeoff an landing?
• 15kts
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Limitations
• What is the maximum crosswind components takeoff/landing on a dry
runway?
• 40/40
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Limitations
• What is the maximum crosswind components takeoff/landing on a wet
runway?
• 25/40
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Limitations
• What is the maximum crosswind components takeoff/landing on a slush
runway?
• 15/20
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Limitations
• What is the maximum crosswind components takeoff/landing on a snow
runway?
• 20/35
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Limitations
• How many knots should the crosswind component be reduced by when utilizing
asymmetric thrust on landing?
• 5 knots
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Limitations
• What is the maximum cabin differential pressure?
• 9.1psi
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Limitations
• What is the maximum differential pressure for takeoff and landing?
• .125psi
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Limitations
• During takeoff do not engage the autopilot until?
• 1000’ AGL
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Limitations
• Max allowable headwind/tailwind/crosswind
for auto land is:
• 25knots / 15knots / 25knots (15knots when RVR is less than 2400 RVR)
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Limitations
• At what pressure altitude is the autopilot use below 100’RA prohibited?
• 8,000’
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Limitations
• What are the minimum use of autopilot on approach: ILS coupled / Non precision
approaches / Auto landings:
• 50’ AGL / 50’ below MDA / touchdown and rollout’
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Limitations
• What flap settings are approved for auto landings?
• 25 and 30 degrees
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Limitations
• What is the minimum oil for dispatch?
• ETOPS 18qts / Domestic 16qts
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Limitations
• Maximum flap extension altitude
• 20,000’
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Limitations
• Minimum altitude for speed brake deployment?
• 800’ or in flight with wing flaps 25 or 30 degrees.
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Limitations
• The maximum allowable in-flight difference between captain and first office altitude displays for RVSM operations is:
• 200’
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Limitations
• Maximum and minimum fuel temperature?
• Max 49C / Minimum at least 3C above the freezing point of the fuel being used or -
45C, whichever is higher.
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Limitations
• With the main tanks less than full, what is the maximum permissible fuel quantity
permitted in the center tank?
• 2000lbs.
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Limitations
• What RNP values are the 757/767 certified?
• .15 RNP
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Limitations
• May Jet B or JP4 fuel be utilized?
• No
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Limitations
• When must the center tank fuel pumps be positioned OFF?
• Less than 5,000lbs in the center tank with the airplane readied for taxi/takeoff, and
when center tank indicates less than 1,000lbs during climb cruise and descent.
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Limitations
• May a fuel circuit breaker be reset?
• No.
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Limitations
• What is the minimum hydraulic quantity prior to takeoff?
• Not below refill mark, RF.
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Limitations
• Maximum tire groundspeed? 757/767
• 195kts / 205kts
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Limitations
• Minimum crew oxygen bottle levels?
• Refer to the chart
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Planning and Performance
• When do you need to compute new V-speeds?
• Weight adjustments exceeding 4440lbs, switching runways, or if the runway
analysis is used
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Planning and Performance
• Is the Flex temp in Fahrenheit or Celsius?
• Celsius
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Planning and Performance
• What is the maximum thrust reduction allowed for takeoff?
• 25%
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Planning and Performance
• Can you use a FLEX reduction if your anti-skid is inoperative , or one brake has been
deactivated?
• No
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Warning Systems
• During what phase of flight are the master warnings inhibited?
• Inhibited for fire only at nose strut extension, and ends at 20 seconds elapsed
time or 400’RA whichever occurs first.
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Warning Systems
• During what phase of flight are the master cautions inhibited?
• Inhibited takeoff roll at 80knots to 20 seconds after nose strut extension or
400’RA whichever occurs first.
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Warning Systems
• When will the EMER LT unarmed light be illuminated?
• Anytime the switch is out of ARMED
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Warning Systems
• Will the EMER lights come on with loss of Normal DC?
• Yes.
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Warning Systems
• What is the required action for STATUS messages prior to departing the gate and
starting engines?
• Contact maintenance for possible corrective action
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Warning Systems
• What does the takeoff configuration warning test?
• Slat/flap takeoff configuration, stabilizer trim out of green band, spoilers armed,
and/or, parking brake set
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Warning Systems
• What is the effect on warnings/caution/advisory/status messages
with the loss of an EICAS screen?
• Status messages will be inhibited, while other information is compacted onto one
screen.
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Warning Systems
• What will cause the activation of the landing configuration warning?
• When below 800’ and the gear not down and the throttles are retarded, or landing
flaps selected.
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Warning Systems
• When are cautions and warnings inhibited on approach?
• Below 200’RA
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Warning Systems
• When are flight attendant calls inhibited?
• Below 800’RA
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Warning Systems
• Can warning messages be removed and recalled with the cancel and recall buttons?
• No.
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Warning Systems
• Can the landing configuration warning be canceled?
• Yes, by pressing the GND PROX/CONFIG OVRD switch.
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Warning Systems
• During flight what causes the slats to automatically extend to the landing configuration?
• A stall warning causes the slats to extend to the landing position if the slats are in the Takeoff
position. When the stall no longer exists the slats automatically retract.
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Warning Systems
• How many stall warning systems are available?
• Two systems are available, both of which are energized in flight and deactivated on
the ground.
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Warning Systems
• When may the ground proximity switches be deactivated?
• Only for approved procedures where the use of flaps at less then normal flap position
or landing gear up is specified.
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Warning Systems
• What are the altitude parameters for the ground proximity system?
• Between 30’ and 2,450’RA
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Warning Systems
• Will the GPWS provide a warning of flight toward vertically sheer terrain or of slow descents into unprepared terrain while in
the landing configuration?
• No.
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Warning Systems
• When is the predictive wind shear alert inhibited?
• Yes, during takeoff at airspeeds above 100kts, until reaching 50’AGL.