Electrical Power Up
(Not memorized, read and do)
Do if you get to a dark airplane with one blue light (Ground Power Available) or, if no ground power and you’ll need the APU for electrical.
Can hit lights switch on forward FA panel to turn some lights on so it’s not completely dark.
If RED A/C out-of-service tag is on thrust levers, don’t touch anything and go sit down in first class
Don’t establish hydraulic power if flaps will move unless you cleared the outside area
Not memorized, read and do.
Reference supplemental procedures 5.6.1
VOL 1 / Supplemental Procedures 5.6.1
Preflight Interior Inspection - FO
Detailed
Assumes that the electrical power up has already been done or airplane is on ground power.
Doesn’t technically need to be in order if you get it all done.
Go do the exterior preflight
VOL 1 / 3.4.1
Preflight Interior Inspection - FO
Assumes that the electrical power up has already been done or airplane is on ground power.
Doesn’t technically need to be in order if you get it all done.
Go do the exterior preflight
VOL 1 / 3.4.1
Exterior Inspection - Typically FO
Emphasis on tire wear, airframe or control damage and leaking fluids. Report discrepancies to captain and MX (dispatch ASAP)
VOL 1 / 3.4.2
Preflight Procedure FLOW - PF
IRS Panel - Set
ATIS - Obtain
ACAR - Set
PDC - Obtain
Double check with “Upside Down U”
Visually scan rest of flight deck to confirm PM did it correctly
VOL 1 / 3.4.3
FFOD Preflight Procedure Tests - PM
These checks or tests need to be accomplished prior to the first flight of the day (on that aircraft) as noted in the aircraft logbook.
VOL 1 / 3.4.4
Preflight Procedure FLOW - PM
Detailed
These checks or tests need to be accomplished prior to the first flight of the day (on that aircraft) as noted in the aircraft logbook.
VOL 1 / 3.4.4
Preflight Procedure FLOW - PM
VOL 1 / 3.4.4
Preflight Procedure FLOW - FO
VOL 1 / 3.4.6
Required for Pushback
FOM 14.1.9
Electronic Fuel Service Record (eSVR)
PDC Clearance Verification
“Delta 201, ATL to CLT, Transponder 3404, PHIL3 HRTWL ZELLE JOOLS1, maintain 10,000, FL 270, departure frequency ___”
VOL 1 / 3.3.10
WARTS Briefing
WARTS
W: Weather/Winds
- Takeoff minimums/alternate
- Windshear
- Cold weather ops
- Low vis taxi/ takeoff / SMGCS
A: Abnormal/Aborts
- Captain briefs these at the end
- RTO reason/ plan/ duties
- MEL review
R: Runway Considerations
- Runway length & width
- Surface condition
T: Taxi Plan/ Terrain/ Transition Altitude
- Expected taxi route/ runway departure position
- Hot spots/ crossings
- Abnormalities (NOTAMS, Jeppesen Construction Page, flight plan remark, etc)
- Engine start/ delayed start
- Runway change plan
- Terrain
- Transition altitude
S: SID/ DP/ Company Pages
- Engine out procedures
- SID speeds/ altitude restrictions
- Company pages
- Flight plan remarks/ NOTAMS
THREATS and ERROR MITIGATION
Weight Data Record (WDR)
or pre-pushback message
VOL 1/ 3.4.10
What invalidates a WDR
Pushback FLOW
Pumps, Pumps, Doors, Doors, Transponder
VOL 1/ 3.4.7
Pushback Checklist
Nothing wild on that
VOL 1/ 3.4.7
Pushback
VOL 1/ 3.4.7
Engine Start Procedure
(both engines)
PACKS - OFF, isolation AUTO
ENGINE START SWITCH - GRD
- START VALVE OPEN alter upper DU
Engine start LEVER to IDLE when N2 < 1% in approx 5 seconds (greater than 20% N2)
- SPAR VALVE CLOSED dim then extinguished
Verify FF & EGT within 10 seconds
- white flash box around EGT = ABORT
@56% N2
- ENGINE START SWITCH moves to OFF
- Verify START VALVE OPEN
“STARTER CUTOUT”
Monitor engine instruments
- N1, N2, EGT, FF, oil pressure
- Oil pressure increase by idle, N1 & N2 rotation
- Stabilized idle when EGT red limit line disappears
- Stabilized also 2, 4, 6, 6
20% N1
400˚C EGT
60% N2
.60FF
After right engine start:
- Isolation - OFF
- Right PACK - AUTO
- “Starting engine #1”
- Start clock after 2nd engine start for warm up time
VOL 1/ 3.4.8
AFTER START FLOW
E GPA BARRF
VOL 1/ 3.4.9
Taxi Procedure
VOL 1/ 3.4.10
Taxi Checklist
Flaps …. 1, 1, 1, green
- FLAP lever position
- FMS flap value
- indicated flap position
- green LE FLAPS EXT light illuminates
Takeoff speeds…. 141, 142, 146, Set
- V1 in the FMS
- V2
- VR
- V2 set in IAS/MACH window on MCP
Thrust…. TO1, assume temp 54
- TO, TO1 or TO2 in thrust mode display on CDU
- assumed temp
Stab Trim …. 5.0
- STAB TRIM set to trim value on FMS or WDR. FMS can be used if less than 0.75 difference
Flight controls …. Checked
TAXI CHECKLIST COMPLETE
VOL 1/ 3.4.10
DELAYED START FLOW
(Same as after start)
E GPA BARRF
Start a clock for engine warm up time (2 mins?)
VOL 1/ 3.4.11
NAV Brief
PF will verify and verbalize:
1. Runway - assigned departure runway with FMS runway
2. Departure
3. First fix
4. H: Heading (initial) and/or planned roll mode
5. A: Altitude clearance and transition altitude
6. A: Airspeed restriction (if applicable)
VOL 1/ 3.4.12