FLOWS AND PROFILES Flashcards
ORIGINATING FLOW
Airworthiness acceptance - Complete
DCP - Checked
Glareshield lights - Set
ADS probe heaters - As req.
Reversionary panel - Set
PFD - No flags
MFD - Set
O2 and ACP - Checked and set
Alt. Gear Extension - Checked
BEFORE START “TO THE LINE” TASKS PF
Verify the navigation database will be current for the duration of the flight
Enter route
Enter ADSB designation from the dispatch release into the ACT RTE Flight ID in the FMS
Set Transponder Code
Begin PERF INIT (up to, but not including ZFW)
Set/Verify DEP Limit page i.e. standard/non-standard speeds and acceleration altitude
Select anticipated runway conditions in ACARS
Set Guidance Panel: Runway heading, Altitude, Source, Course, and SPEED knob to FMS
Complete EFB set up (2)
Departure WANT Briefing: (1) • Brief Autobrake setting
BEFORE START “TO THE LINE” TASKS PM
Initialize ACARS
FFOD Inquiry
Obtain ATIS
Obtain clearance (PDC)
Verify route
Verify PERF INIT
Verify GP set up
Complete EFB set up (2)
Set communications frequencies
Verify Departure Limit speeds and altitudes
BEFORE START “TO THE LINE” FLOWS
Crew O2 - Check
PFD - Check
MFD - Set
BEFORE START “ BELOW THE LINE” TASKS
CP:
Verify accuracy of passenger and baggage/cargo count on completed manifest
Enter ZFW in PERF INIT Enter TO CG
Complete Takeoff Data pages
• TO-X, Temp, ATTCS, A/I, Flex temp
Verify flap settings
Enter takeoff V-speeds
Press TOGA after V-speeds are entered Copy flight plan
FO:
Complete Manifest (ACARS or FliteView Manifest)
Read takeoff data to Captain
“ZERO FUEL WEIGHT (_____) LBS, TAKEOFF CG (__). FOR PLANNED RUNWAY TO-(__), ATTCS (__), ECS (__), A/I (__). OUTSIDE AIR TEMP (__) C, FLEX TEMP (__). FLAPS (__), SPEEDS (__), (__), (__), (__).”
Set pitch trim for takeoff
BEFORE START “ BELOW THE LINE” FLOW
Seatbelts/ shoulder harness - ON
Beacon - ON
ACMP 3A and 1 - ON
Doors/ windows - Closed & locked
XPDR - ON
FO task during Pushback
Set flaps
Engine Start Sequence
“STARTING ENGINE 1 (2)”
Turn the START / STOP selector to START momentarily (2 sec) and back to RUN, keeping the hand on the START / STOP selector to abort the engine start, when necessary
Start Clock
Monitor IGN A (B) at 7% N2, fuel flow at approximately 20% N2
Ensure N2 and N1 accelerate normally and positive oil pressure is indicated
Verify the annunciation IGN A (B) goes out at approximately 50% N2 ENGINE START SEQUENCE “START ENGINE 1 (2)”
Verify the engine stabilizes at idle and at the correct N1 target (1)(2)
“NORMAL START”
CROSSBLEED START FLOW PROCEDURE
Rear of Aircraft - CLEAR
Thrust Lever (Operating Engine) - Advance
Duct Pressure - 40 - 45 PSI
START/STOP Selector - Start, then RUN
-after start-
Thrust Levers - IDLE
N1 Target - Verify
“NORMAL START”
After Start Checklist Flow
Captain “Flaps(), APU(), flight control check”
Flaps - SET
APU - as required
ACMP 1 - AUTO
ADS probe heaters - Pushed Out
Flight controls - Checked on CP MFD
Electronic Devices - Airplane Mode
Normal Callouts prior to moving aircraft
CP “Clear left”
FO “Clear right”
FO - turns on taxi lights
Before Takeoff Flow
PA - Cabin Announcement
CAB - Cabin Secured
Status Page - Brake Temp Checked
CCD - Select MAP
T/O Config - “OK”
Takeoff Call outs
PF - “Check Thrust”
PM - “Thrust Checked”
PM - “Eighty Knots”
PF - “Checked”
PM - “V1 , Rotate”
PM - “Positive Rate”
PF - “Gear UP”
PM - “Gear UP”
-400’ AGL-
PF - “HDG()”
PM - “HDG()”
PM - “Gear UP”
-Acceleration altitude-
PF - “Climb Sequence, after takeoff checklist”
PM - “After takeoff checklist complete”
Close in Turns Takeoff profile
During turn - Maintain FD bank limits and V2+ 10 knots
ACCEL altitude - VNAV
When Turn complete - Climb Sequence, flap retraction
Bank angle limits Engine failure at or after V1
15° at V2
20° at V2 + 5kt
25° at V2 + 10kt
