Before Departure
Preflight Inspection
- Open checklist in QRH to preflight
- AUX pump on to charge brake accumulator and THEN pull parking brake
- Pressure will drop but make sure it stays above 1200 psi
- Hydraulic service panel
- Only "FULL" light
Before Starting Engines (AFM 2-9)
- Step 5b. EMER BATT -- EMER
- Wait 5-8 seconds after turning on main batteries to turn on EMER BATT
- When DU2 powers up and everything stops flashing then can turn on EMER BATT
- Otherwise will deploy PAX oxygen masks (rubber jungle)
- Wait 5-8 seconds after turning on main batteries to turn on EMER BATT
- Step 5c. L & R AV MSTR -- ON
- Turn FMS on at same time as turning avionics
- Otherwise will have to wait a while
- Press "ON / OFF DIM" button
- Turn FMS on at same time as turning avionics
- Step 10. Flight Controls
- Just box for freedom of movement
- Step 12. DU and REVERSION panels -- NORM
- 2 DU knobs
- 4 reversion knobs
- Step 13. EICAS
- Oil temp above -28 °C
- This from Operations Reference Manual 1-47
- Pilot Training Guide 19-30 says above -40 °C or -40 °F
- Oil temp above -28 °C
- Step 18. Environmental Control
- 11 o'clock is good starting point
- Step 20. SYSTEM TEST Panel -- Test
- Need to memorize the procedures for all these tests
- All of these are in the Pilot Training Guide starting on 20-16
- Step 21. Master CAUT -- Inhibit
- Press and hold on one side and look at the other side
- Step 22. Trim system -- Check
- Commit to memory because after transitioning from AFM to QRH the QRH doesn't say WHAT to test
- Step 26. Standby Instruments -- Uncaged & Checked
- Cage standby attitude indicator
- Pull out and turn
- Left to uncage
- Right to cage
- Step 27. FMS -- Set
- Always start with Fuel page
- (pink I's in top = independent)
- FOB -- hit "BACK" (next to 0)
- Hit enter (this pulls from fuel computer how much fuel is on board)
- Flight Plan Page
- Menu
- Notes:
- "First to reverse, last to pass"
- Also the one with asterisk is the hold???
- Step 28. Takeoff Data -- Computed & Speeds Set
- MFD press "MFD button" and go to "SPDS" page
- Note: press the VSPEED button on the far right until three magenta dashes before inputting speeds
- V1 = 110
- VR = 115
- V2 = 124
- (Set speed bug 149 -> V2 + 25)
- Now upside down "U" check
- Verify source
- e.g. GPS-based departure -- FMS source (starts bottom left of PFD)
- Puts us into white needles
- Check V-speeds are posted
- Airspeed shows zero
- Speed bug set
- Top left is speed reference
- Verify V2 + 25 -- flap retraction speed
- Arrow pointing towards whoever flying (XFR button on flight guidance controller)
- Hit go-around button
- Mode (and Source?)
- Flight guidance controller -- heading or nav Mode -- since departure fly NAV
- Set top altitude using ASEL knob on flight guidance controller
- Altimeters set
- Indicated alt within 75 feet of field elevation
- VSI zero
- Set heading bug to runway heading
- Verify source
- MFD press "MFD button" and go to "SPDS" page
Trim System Check (Step 22)
- a. PITCH TRIM Switch -- Select SEC.
- b. SEC Switch -- Trim NDN or NUP.
- c. Copilot’s Control Wheel Master Switch (MSW) -- Check cutout of SEC trim.
- d. PITCH TRIM Switch -- Select OFF.
- e. Pilot’s or Copilot’s Control Wheel Trim Switch -- Trim NDN or NUP. No trim should occur.
- f. PITCH TRIM Switch -- Select PRI.
- g. Copilot’s Control Wheel Trim Switch -- Trim NDN or NUP.
- h. Pilot’s Control Wheel Trim Switch -- Trim NDN or NUP.
- i. Pilot’s Control Wheel Master Switch (MSW) -- Check cut-out of PRI trim.
- j. Pilot’s Control Wheel Trim Switch -- Trim LWD or RWD.
- Note: go two units and see box around trim value, than back to 0 (only need to check either left or right)
- k. RUDDER TRIM Switch -- Reset to zero (0).
- Note: go two units and see box around trim value, than back to 0 (only need to check either left or right)
Rotary System Test Panel
Fire Detection
- Before starting the test
- Select APU master ON
- Put the RMU on "engine" page
- Press test to clear test results if needed
- Hold the test for minimum 15 seconds
- Just long enough to hear the APU fire horn sounding from the nose
- If you hold for 30 seconds it will shut the APU down -- so don't hold more than 30 seconds
- Press and hold fire test button = 21 indications, go top to bottom
- Master warning switch indicators (2)
- EICAS ITT FIRE annunciated (2)
- Red CAS messages (3)
APU FIRELR BLEED AIR LEAKWING/STAB LEAK
- Crew warning panel (3)
WING/STAB LEAKL BLEED AIR LEAKR BLEED AIR LEAK
- RMU select PGE -- right side -- engine (4)
- 2 indications on each engine
- Bottom of pedestal get all red switches illuminated (7)
- For each engine
- FIRE PUSH
- ARMED (EXTINGUISHER #1)
- ARMED (EXTINGUISHER #2)
- APU FIRE
- For each engine
- Listen for APU fire horn coming from nose
- After completing test
- APU Master OFF
- RMU page -> Radio
- Pilot Training Guide page 8-7
Gear
- 10 indications, go top to bottom
- 2 master WARN
- 1 GEAR CAS
- 1 GEAR CWP
- 3 green down lights
- 3 in transit lights
- 1 aural alert: "Gear"
Flaps
- 6 indications
- 2 master CAUT
- 2 CAS
FLAPS FAILAmber CASFLAPS FAULTAmber CAS
- 1 Amber box around flap setting on EICAS
- 1 aural tone
- (no CWP)
ADC
- "Overspeed" aural alert
- Red
ADC TESTon both primary flight displays (PFDs) - Airspeed = 330 kt (red)
- Mach = 0.81 (red)
- Altitude = 1000 ft
- Altitude trend = +1500 fpm
- Vertical speed = +5000 fpm
- Overspeed cue = 330 kt and above
- TAS (MFD) = 466 kt
- SAT (MFD) = – 45°C
- Altimeter indicates 29.92
Stall
- This whole process runs through on left and then right side
- Red LSA (low-speed awareness band) moves up
- AOA needle sweeps
(L/R) AOA HT FAILamber CAS- Master CAUT tone and light
- Stick shaker activation
- "Stall" voice
Anti-Ice
WG/STAB HT OKwhite CASWING OVHTred CAS andSTAB OVHTred CWP- Master WARN tone and light
EGPWS
- As soon as you see
TERR TESTpop up in MFD let go of the button- Less than 2 seconds press
GPWS SYS FAILwhite CAS message is displayed momentarilyGND PROX FAILwhite CAS andWINDSHEAR FAILwhite CAS messages may also appear momentarilyGPWS FAILannunciators on the upper, outboard corner of the pilot and copilot instrument panels are also displayed momentarily- Either
- This
- "Glideslope" aural alert will be enunciated
- Amber
GND PROXis momentarily displayed in the ADI sphere on both PFDs GPWS G/S INHBwhite CAS message is momentarily posted
- Or this
- "Glideslope Inop" aural alert will be enunciated
- This
TCAS
- Rotate rotary knob to empty spot
- This is just procedural / a reminder -- it doesn't do anything
- Select any 4 lines in TCAS DSPY window on RMU, press buttons
- If do this, don't need to select TCAS on MFD
- Press and hold test button on RMU
- Aural "TCAS test" => "TCAS test pass"
- Want to see four indications in TCAS windows and ... ?
Off
- Once done all tests, move the rotary switch to "OFF"
Starting Engines
- Step 1. Cabin Door -- Closed and latched
- Two handles forward, no
ENTRY DOORred CAS
- Two handles forward, no
- Step 2. L & R AV MSTR -- OFF (If desired)
- Just leave them on
- Step 7. Engine -- Start
- Co-pilot start timer when engine starts
- Pilot keep hand on thrust lever during start
- Hot start is rapidly increased ITT past the 6 o'clock position
- No checklist for hot or hung start -- CUTOFF, shutdown and call MX
- Note max ITT attained
- N2 nice continuous acceleration up to about 55 percent
- Engine takes about 25 seconds to start, more than that is probably hung start
- Step 13. EX PWR Switch -- AVAIL and disconnect
- Set to available FIRST ... then once you SEE it's AVAIL then call for disconnect
- Step 15. Anti-Ice system
- See below
- Step 18. Bleed Air System
- See below
- Step 20. EMER PRESS -- check
- Check -- turn on -- check
L R EMER PRESS ONamber CAS message -- back off
- Check -- turn on -- check
Anti-Ice System Check
- Note: starts with both bleeds ON (think of this as 8 button pushes)
- a. L BLEED Switch -- OFF.
- b. WING/STAB Switch -- ON. Check both ITTs rise.
- c. R BLEED Switch -- OFF. Check both ITTs reduce.
- d. L BLEED Switch -- On. Check both ITTs rise.
- e. R BLEED Switch -- On.
- f. WING/STAB Switch -- As required.
- Just turn it off since it needs to be off in next step
- g. L and R NAC Switches -- ON (NAC green EI), then as required.
- Engine idle will increase and N1 bugs will shift.
- Just turn NAC OFF when done
Bleed Air System Check
- a. WING/STAB Switch -- OFF
- b. L BLEED Switch -- OFF. Verify normal cockpit airflow.
- c. L BLEED Switch -- On
- d. R BLEED Switch -- OFF. Verify normal cockpit airflow.
- e. R BLEED Switch -- On
- f. WING/STAB Switch -- As required.
- On if below 10 °C and visible moisture
Before Taxi
- Step 3. Manual Mode Governor -- Checked
- See below
- Step 5. Spoilers
- Bring up "FLT" system page on EICAS
- Step 6. Flaps
- We always do flaps 8 takeoffs!
- Don't set flaps until lineup if in snowy conditions!
- Step 7. Flight controls
- Checking spoilerons
- Step 14. Emergency / Parking Brake -- Release
- Note: skip down to non-movement "taxi and before takeoff" checks step 4 and do those before removing parking brake and moving
Manual Mode Governor Check
Test each engine separately, keep hands there in case engine runs away, problem with manual mode governor
- a. L ENG CMPTR Switch — MAN. (MAN white EI)
- b. Gradually advance left thrust lever until an increase in N1 is observed.
- Go to about 35% or so
- c. Retard thrust lever and note decrease in N1.
- d. L ENG CMPTR Switch — ON.
- e. Repeat steps a thru d using R ENG CMPTR Switch and Right Thrust Lever.
Taxi and Before Takeoff
First start with item 4 and below -- the non-movement items. Then release parking break and do steps 1, 2, and 3
- Step 8. Trims
- Aileron rudder 0 trim, pitch set by weight and balance
- Recommend waiting until lineup checks to set pitch trim
- Otherwise control yoke moves towards pilots and is a bit less comfortable
- Step 9. TO Brief
- Below 80 KIAS abort for anything
- Between 80 KIAS and V1 abort for 4 things
- Fire
- Engine failure
- Loss of directional control
- Thrust reverser deployment
- Anything other than these 4 is in-flight emergency
- Brief MSA
- Don't need to spew off memory items
- Step 11, Radar -- As required
- Set it to STBY
After completing the latter part of this checklist, release parking brake and go back to the first 3 items of "Taxi and Before Takeoff" check.
Turn on Taxi and Recog lights
- Step 1. Brake and nose-wheel steering check
- Throttle up to about 35% N1
- Step 2. Flight instruments -- checked
- TBD
- Step 3.
- Deploy TRs, don't add thrust, just deploy
- Then push them back down
- Keep palm of hand on thrust lever and just use fingers for TRs
Runway Lineup
Now back to runway lineup checks
Done by PM
FLOW
Transponder TA/RA mode -- line select key (will get out of standby)
Step 6. -- APR is always desired to ARM if it is working
MAKE SURE TO SET PITCH TRIM HERE!!
Before takeoff (3-2-1)
- EICAS (3)
- REV
- APR armed
- REV
- Buttons illuminated on hydraulic panel (2)
- NOSE STEER ON
- AUX HYD ON
- CAS Messages (1)
AUTOSPLR ARMEDwhite CAS
- EICAS (3)
Then
- No boxes
- No colors
- No dashes
Also
- Flaps handle set to 8° and indicating 8°
- Runway number callout and identified