717 Flashcards
Maximum operating altitude
37,000 feet
Maximum takeoff and landing tailwind
10 knots or as permitted by company pages
Crosswind limit
38 knots including gusts
Severe turbulence penetration speed
275 indicated/.75 mach
During takeoff do not engage the autopilot below
200 ft AGL
Maximum allowable wind component for autoland operations:
HW
CW
TW
HW: 25kts
CW: 15kts
TW: 10kts
APU air switch off for
takeoff and inflight operations
Aborted start
Fuel switch: off
Ignition switch: auto
Cabin altitude or rapid decompression
Oxygen masks: on/establish 100 percent
crew communications: establish
Complete loss of AC power or Gen ALL off
Emer power selector: on
Engine fire or severe engine demage/seperation
Autothrottles: off
throttle affected engine confirm and : idle
Two engine flameout
Ignition switch: on
Start pump switch: on
Runaway stabilizer
Autopilot, if engaged: disconnect
If stabilizer runaway continues, control wheel trim switches: trim opposite direction of runaway as necessary
Unreliable airspeed
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
Pushback Flow
Exterior doors - verify closed on EAD
* Verify CABIN IS READY FOR
PUSHBACK advisory has been
received.
Beacon on parking brake off when clearance received
Before takeoff flow
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
After takeoff flow
- 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
Descent flow
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.