Flows and Profiles *** Flashcards
Exterior Safety Inspection
Exterior Safety Inspection
Check:
• Chocks in place
• Landing gear door position
• Flight control surfaces clear
• APU exhaust area clear (unless APU running)
Warning ! When any gear door is open, check that the respective door
handle release is in the “doors open” position. If the handle
is in the “doors closed” position and the doors are open,
pressurizing hydraulic systems #1 or #4 will close the doors
and can result in personal injury.
ELECTRICAL POWER UP
BATTERY switch………………………………………………………………………………….ON
Verify OFF light is extinguished.
STANDBY POWER selector ………………………. AUTO
Hydraulic demand pump selectors ……………………….OFF
WINDSHIELD WIPER selectors ……………………OFF
ALTERNATE FLAPS selector ……………………..OFF
Landing gear lever ……………………………………..Down
Flap position indication and FLAP lever ………………….. Agree
Electrical power ………………………………….. Establish
BUS TIE switches - AUTO
Preliminary Flight Deck Procedure
IRS mode selectors ………………………. OFF, then NAV
VOICE RECORDER switch……………….ON
EICAS messages …………………………….Check
Engine display …………………………………Check
• Engine oil quantity - Check and not magenta
Status display ……………………………………Check
• Hydraulic quantity - Check and RF not displayed
• Oxygen pressure (psi) - Sufficient for flight
• APU oil quantity - Check and RF not displayed (if APU operating)
NOTE: not status message are allowed, unless dispatch in accordance with DDG
Do the remaining actions after a crew change, maintenance action, or if the aircraft has been left unattended by the flight crew for any period of time.
Note: The following oxygen pressure drop test only needs to be performed at one crewmember or observer station.
Oxygen pressure drop ……………………………………… Test
See “Oxygen Pressure Drop Test” on page SP.1.11
Circuit Breakers …………………………………….Check
4 SMOKE EVACUATION handle……………In
Overhead maintenance panel……………………..Guards closed
The split system breaker OPEN light may be illuminated.
Verify that all other lights are extinguished.
APU START SOURCE switch (if installed)……………… APU BATTERY
Freighter
LOWER LOBE CARGO CONDITIONED AIR FLOW RATE selector ………………………. As required
Cockpit Voice Recorder ………………………………. Test
Flight Deck Emergency Equipment …………………..Check
- Crash axe - Stowed
- Fire fighting gloves - Stowed
- Overhead escape hatch - Closed and locked
- Emergency escape devices - Stowed
- PBE - Checked and stowed
- Verify inspection date is valid and seals are not broken.
- Halon fire extinguisher - Checked and stowed
- Verify wire seal is not broken and bottle pressure in the green band.
- Portable oxygen bottles (if installed) - Checked and stowed
- Ensure all portable oxygen bottles are in working condition by verifying
- the pressure in the green band, all components are present, and the hose is connected to the bottle and the provided mask.
- Flashlights (if installed) - Check
PARKING BRAKE ………………………………………Set
Passenger
FLIGHT DECK ACCESS SYSTEM ……………………………………….. Test
CDU Preflight Procedure - Captain and First Officer
Start the CDU Preflight Procedure anytime after the Preliminary Flight Deck Procedure.
The Initial Data and Navigation Data entries must be complete before the flight instrument check during the Flight Deck Procedure.
The Performance Data entries must be complete before the Before Start Checklist.
Note: Do not enter data in the CRZ CG.
• Failure to enter enroute winds can result in flight plan time and fuel burn errors.
FMC Initial data …………………………………………………… Set
IDENT page
POS INIT page
Navigation data.................................................... Set RTE page DEPARTURES page PROGRESS page: RTE page LEGS page NAV/RAD page
Initial performance data ………………………………………… Set
PERF INIT page
ACARS ………………………………………………………………………….. Enter INIT DATA
Request takeoff performance after receiving the Load Manifest
Note: Load Manifest is the general term for either the Sable
computerized “loadsheet” or manual “W&B Record” (Trim Sheet).
See “Flight Deck Performance - Takeoff” on page SP.20.16 as needed.
When FDP takeoff data is received, both pilots review/verify the following: • WIND, OAT, QNH • CG, GRWT, FUEL, ZFW • REMARKS / CAUTIONS • Runway / intersection • MTOW • Thrust (THR, ATM, and Pack configuration) • Engine Failure Procedure
Note: If using a TLR, see TLR Procedures on page SP.20.37
FDP must be updated when:
• A performance related DDG item is added or removed
• There is a significant change in environmental conditions that
would affect performance (e.g., change of wind direction/speed,
lower altimeter setting, higher temperature, runway surface
conditions/contaminates)
• The departure runway is not shown on the FDP or an intersection takeoff distance shorter than planned.
Final performance data [PF] ……………………………………………………………… Set
Warning ! Do not enter the ZFW into the GR WT boxes. The FMC
will calculate performance data with significant errors.
Note: Selecting VNAV before completing the Performance Data will cause the FMC alert message PERF/VNAV UNAVAILABLE.
Use FDP for entries. If FDP is not available, use Load Manifest and TLR.
PERF INIT page
THRUST LIM page
TAKEOFF REF page:
CDU Departure “T”
1 INIT REF 2 RTE 3 DEP/ARR 4 PROG 5 RTE 6 LEGS 7 NAV/RAD 8 INIT REF
Flight Deck Procedure - Captain / FO
- Captain and FO areas of responsibility
- Final Flight Deck Procedure
- Call “PREFLIGHT checklist” [C]
Before Start Flow
First Officer:
1-CDU display …………………………….Set
2-Flight deck door [F or R] ……………………………… Closed and locked
3-Cabin [F or R] ……………………………………………… Verify cabin secure
4-Exterior Doors [F]…………………………………………….. Verify closed
5-Electrical Power——Verify both APU GENERATOR ON lights and EXT power is removed
6-Start clearance [C, F]…………………………………………….. Obtain
7-Hydraulic panel [F]……………………………………….. Set
Warning ! If the tow bar is connected, do not pressurize the hydraulic systems until the nose gear steering is locked out. Unwanted tow bar movement can occur.
8-Fuel panel [F]………………………………………… Set
9-BEACON light switch [F]…………………………………………. BOTH
10-RECALL [F]…………………………………. Check/Cancel
11-Transponder [F] ………………………….. Verify code, set as needed
12-Do the BEFORE START checklist. [F]
Captain:
1-CDU display
2-Start clearance [C]…………………………………. Obtain
Ensure that both APU GENERATOR ON lights are illuminated .
747-8 - Ensure that external power is disconnected before hydraulic auxiliary pumps 1 or 4 are pressurized.
Obtain a clearance to pressurize hydraulic systems.
Obtain a clearance to start the engines.
3-Verify EICAS messages then state “CANCEL”
4-Trim [C] …………………………. ____Units, zero, zero
Stabilizer trim - ____Units Set the trim for takeoff. Check that the trim is in the greenband.
Aileron trim - 0 units
Rudder trim - 0 units
5-Call “BEFORE START checklist.” [C]
Engine Autostart
Autostart Take corrective steps for
- No EGT rise
- a HOT Start
- a HUNG Start
Do the ABORT ENG START checklist for:
- No N1 Rotation by IDLE N2
- No Normal Oil pressure Indication by IDLLE N2
Capitan
- CALL START ENGINE ( 4-1 / 3-2)
- FUEL CONTROL Switch ————— Run
First officer
-DSP secondary engine Indication ……….. set
PACKS control Selector ………………..Set
GE set Two packs OFF
- ENGINE START SWITCH —————Pull ( after Capitan call for engine start)
Verify
- oil pressure increases *
- N1 Rotation and oil pressure by Idle N2 62-67%
AFTER ENGINE STABILIZED AT IDLE as indicated by the RED EGT start limit li e disappearing, start the other engine as desired
*During cold weather start, initial oil pressure rise may be higher than normal
Before Taxi Flow
Release the ground crew when no longer needed.
Captain:
1-Ground equipment ………………………………………………….. Clear L
2-Call “Flaps ___” as needed for takeoff [C]
3-Flight Controls [C] ……………………Check
4-Verify EICAS messages then state “CANCEL”
5-Call “BEFORE TAXI checklist.” [C]
First Officer:
1-APU selector [F]…………………………………… As needed
2-Hydraulic demand pump selectors [F] ……………. AUTO
3-NACELLE / ENGINE ANTI-ICE [F] …………………. As required
4-AFT CARGO HEAT [F] …………………………… ON
5-PACKS control selectors/switches [F]……………… 4 NORM/8 ON
6-STATUS page / 8 FCTL page [F] ……………. Display for flight control check
7-Ground equipment …………………………. Clear R [F]
8-Flap lever [F] ………………………….. Set takeoff flaps
9-Blank the Lower EICAS/MFD [F]
10-RECALL [F]…………………………………….. Check/Cancel
11-Do the BEFORE TAXI checklist. [F]
TAXI-OUT Procedure
PM and PF verify:
PFD:
- V speeds
- FMA (Blank l TOGA l TOGA; LNAV, VNAV armed)
- HDG and Altitude
ND:
The Captain may initiate the taxi or transfer controls to FO as the PF.
• The pilot taxiing will release the parking brake.
• Lights are the FO’s area of responsibility
ATC Taxi Clearance [F] ……………………………………… Obtain
Salute [C or F] ………………………….Received
PARKING BRAKE [C or PF] ……………….Release
- Active waypoint
- TCAS OFF
EICAS:
- Thrust setting
- Memo messages
- Flaps setting
CDU:-
PF on Takeoff Ref
- PM on Legs
Takeoff Briefing Via CDU
1) RTE pg 1
2) RTE Pg 2
3) LEGS
4) VNAV
5) INIT REF (PERF INIT)
6) TAKEOFF REF pg
7) MCP
Before Takeoff Flow
PF
1-Briefing Update Any changes to the Takeoff briefing as needed
2-WXR or TERR
3-Call “BEFORE TAKEOFF CHECKLIST”
PM
After PF calls for “Before Takeoff Checklist” Pilot Monitoring:
1-Cabin - Notify cabin to prepare for takeoff, verify cabin secure
2-WXR or TERR
3-Trim check if stab blanks or change, delete CG and re-enter CG
4-Transponder TCAS TA/RA
5- Read BEFORE TAKEOFF Checklist
Cleared on to the active departure runway
PM
All, except landing lights Exterior Light
Both
Align airplane with the runway
Verify airplane heading agrees with the assigned runway heading
Cleared for takeoff
PF
Brakes Released
PM
All ON Exterior lights
Takeoff
- Smoothly advance thrust levers to approximately GE 70%N1, GEnx 45%N1,
or PW 1.10 EPR and allow engines to stabilize - Push TO/GA switch to advance the thrust levers to takeoff thrust, or
manually advance the thrust levers to takeoff thrust
-Keep thumb on the autothrottle disconnect switch until 80 knots
80 knts, thrust set, HOLD on FMA:
PM: “80 knts, thrust set”
PF: “Check”
5 knots prior to V1:
PM: “V1”
At Vr:
PM: “Rotate”
Verify a positive rate of climb on the altimeter and call “Positive Rate”.
Verify a positive rate of climb on the altimeter and call “Gear Up”.
Set the landing gear lever to UP.
Appropriate Lift Off Attitude durning to maintain min tail clearance
All engines:
Flaps 10: 10.1º
Flaps 20: 10º
One-engine INOP:
Flaps 10, 20: 10.6º
After Takeoff
PF
After flap retraction is complete
Call
“AFTER TAKEOFF CHECKLIST”
PM
NACELLE anti-ice………………….Auto
Packs………………..Verify operating
Gear lever……………….Off
Read
AFTER TAKEOFF Checklist
Descent Duties
PF
1-ATIS
2-Recall review…… Request
3- Verify EICAS messages then state “CANCEL”
4-Autobrakes Set:
• Select desired brake setting
• Verify AUTOBRAKE ___ memo message
4-CDU Verify: • DEP ARR - arrival & approach procedure • LEGS - speed & altitude constraints • NAV/RAD - Nav. radios • INIT REF – flaps/VREF speed
5-EFIS control panel Set: • Approach minimums on PFD • Preset local altimeter setting • VOR/ADF switches • WXR/TERR
6-Approach briefing Complete
7-call “DESCENT CHECKLIST”
PM
1-Obtain ……ATIS
2-RCL switch
Push:
• Read aloud all alert and memo messages
• If no messages: State “NO ITEMS”
3-CANC switch
If messages present: Push
4-Landing Distance Assessment Obtain: If using Datalink: • Review crew entered data • Verify Runway • Verify Flaps
5-CDU Program & set: • DEP ARR - arrival & approach procedure • LEGS - speed & altitude constraints • NAV/RAD – Nav. radios • INIT REF - flaps/VREF speed
6-EFIS control panel Set: • Approach minimums on PFD • Preset local altimeter setting • VOR/ADF switches • WXR/TERR
7- Read DESCENT Checklist
After Landing Flow
After Pilot Flying calls “Flaps UP After Landing”
Captain:
1) Speedbrakes - DOWN
Pilot Monitoring:
1) APU START, then ON As required
2) NACELLE Anti-ice As required
3) Exterior Lights - Set
4) WXR/TERR switches - OFF
5) AUTOBRAKES - OFF
6) Flaps - UP
7) TransponderAs needed
SHUTDOWN PROCEDURE
PF)
1-Parking Brake Set:
• Verify PARKE BRAKE SET memo message
Capitan: 1-FUEL CONTROL switches CUTOFF 2-F/D switch OFF 3-Parking Brake Release after chocks in place. Remains set if chocks not in place. 4- Call “SHUTDOWN Checklist”
First Officer
1-Electrical power Establish:
• If EXT power EXT 1- Push
• If APU power APU GEN 1-Push
2-Hydraulic demand pumps 4 – AUX ,1, 2, 3 – OFF
Note: 4 OFF after Chocks
3-SEATBELTS selector OFF
4-Fuel pump switches OFF
5-NACELLE anti-ice switches AUTO (OFF – if AUTO n/a)
6-WING anti-ice switch AUTO (OFF – if AUTO n/a)
7-BEACON OFF
8-F/D switch OFF
9-STAT switch Push: Displays STATUS synoptic for Mx write up
10-Transponder STBY
11-Hydraulic demand pump 4 AUX OFF
12-APU selector As needed
13-Read SHUTDOWN Checklist
