717 Flashcards

1
Q

Maximum operating altitude

A

37,000 feet

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2
Q

Maximum takeoff and landing tailwind

A

10 knots or as permitted by company pages

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3
Q

Crosswind limit

A

38 knots including gusts

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4
Q

Severe turbulence penetration speed

A

275 indicated/.75 mach

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5
Q

During takeoff do not engage the autopilot below

A

200 ft AGL

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6
Q

Maximum allowable wind component for autoland operations:
HW
CW
TW

A

HW: 25kts
CW: 15kts
TW: 10kts

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7
Q

APU air switch off for

A

takeoff and inflight operations

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8
Q

Aborted start

A

Fuel switch: off
Ignition switch: auto

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9
Q

Cabin altitude or rapid decompression

A

Oxygen masks: on/establish 100 percent

crew communications: establish

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10
Q

Complete loss of AC power or Gen ALL off

A

Emer power selector: on

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11
Q

Engine fire or severe engine demage/seperation

A

Autothrottles: off
throttle affected engine confirm and : idle

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12
Q

Two engine flameout

A

Ignition switch: on
Start pump switch: on

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13
Q

Runaway stabilizer

A

Autopilot, if engaged: disconnect
If stabilizer runaway continues, control wheel trim switches: trim opposite direction of runaway as necessary

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14
Q

Unreliable airspeed

A

AFS Overide switches: off
If necessary to stablilize the aircraft or climb to a safe altitude set the following pitch and thrust:

AC clean: 4 degrees and 80 percent N1

All other configs: 10 degrees and 80 percent N1

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15
Q

Pushback Flow

A

Exterior doors - verify closed on EAD
* Verify CABIN IS READY FOR
PUSHBACK advisory has been
received.

Beacon on parking brake off when clearance received

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16
Q

Before takeoff flow

A

Proximity to takeoff runway

  • EAD - Check
    ◦ Verify green box or white box around “SPOILERS” message if Auto Ground Spoiler
    System inoperative
    ◦ Check alert and status messages
  • Fuel - Check
    ◦ Fuel quantity is equal to or greater than MIN FUEL FOR T/O
17
Q

After takeoff flow

A
  • GASPER BOOSTER FAN - OFF
  • HYDRAULICS panel - Set
    ◦ TRANS and AUX pumps OFF
  • APU panel - Set
    ◦ Verify APU AIR and MASTER
    switch OFF
    ◦ Verify APU data block not
    displayed on SD
  • FLAP T.O. SEL - 5
  • Spoilers - Disarm
    ◦ Push SPEED BRAKE handle
    down
  • EAD - Check
  • Check for alert and status messages
18
Q

Descent flow

A

TOD or 20 minutes prior to landing:

  • HYDRAULICS panel - Set.
    ◦ TRANS and AUX pumps ON
  • WINDSHIELD ANTI-FOG switch - As
    required
    ◦ ON for descent into high humidity
    conditions when flight has been
    conducted above FL250.