k
EXTERNAL
B737
700/800/
900
FLIGHT DECK SAFETY
POWER UP
PREPARATION
GROUND
RUN -UP
CHECKLIST
BEFORE ENGINE START
CFM56-7
ENGINE START
STARTING LIMITS
AFTER ENGINE START
ENGINE SHUTDOWN
POWER DOWN
CROSS BLEED START
ENGINE START FAILURES
NON-NORMAL ENGINE CONDITIONS
Compiled by:
SPL/GK
FIRE CONDITIONS
EVACUATION (Backside)
Issued by:
SPL/CC
Name:
Issue date 01-Jan-2017
INCAPACITATION (Backside)
05-92-02 Rev:5
page1
k
CFM56-7
73NG ENGINE RUN NORMAL CHECKLIST
Cover Button
Log of Effective Pages (LEP)
NORMAL CHECKLIST
Pg
COVERPAGE
LEP
EXTERNAL
FLIGHT DECK SAFETY
FLIGHT DECK SAFETY (cont’d)
POWER UP
PREPARATION
BEFORE ENGINE START
STARTING LIMITS
ENGINE START
AFTER ENGINE START
ENGINE SHUTDOWN
POWER DOWN
CROSS BLEED START
Date
1
01 Jan 2017
R
2
3
4
5
6
7
8
9
10
11
12
13
14
01 Jan 2017
01 Jan 2017
01 Jan 2017
R
R
R
R
R
R
R
R
R
R
R
R
R
01 Jan 2017
01 Jan 2017
01 Jan 2017
01 Jan 2017
01 Jan 2017
01 Jan 2017
01 Jan 2017
01 Jan 2017
01 Jan 2017
01 Jan 2017
EMERGENCY CHECKLIST
STARTER VALVE FAILS TO CLOSE
ABORTED ENGINE START
ENGINE STALL, ENGINE FAILURE
FLAMEOUT
TAIL PIPE FIRE, APU FIRE
ENGINE FIRE
EVACUATION PROCEDURE,
INCAPACITATION
15
16
17
18
19
20
01 Jan 2017
01 Jan 2017
01 Jan 2017
01 Jan 2017
01 Jan 2017
01 Jan 2017
R
R
R
R
R
R
R = Revised, N = New, D = Deleted
Revision nr. 5
2
05-92-02 Rev: 5
01 Jan 2017
k
ENGINE RUN
NORMAL CHECKLIST
B737- 7/8/900
EXTERNAL
Cover Button
CAUTION: BEFORE ENGINE TEST-RUN, IT’S NECESSARY
TO INSERT DATA IN PERMIT
Walk around inspection ....................
COMPLETED
Engine Operation Area ....................
CLEAR / CLEAN
Wheel chocks ..................................
IN PLACE*
• Chock distance 6-12 inch in front of wheels and short after.
Nose wheel ......................................
FWD DIRECTION
Tow bar ............................................
REMOVED
Bypass pin .......................................
REMOVED
Steering depress. Valve ..................
NORMAL
Landing gear pins ............................
INSTALLED
Engine ..............................................
CHECKED
Fire extinguisher .............................
IN PLACE
Heading ...........................................
CHECKED
If applicable:
Ground coverings ............................
REMOVED
Wind Limitations
01Jan 2017
05-92-02 rev: 5
3
k
ENGINE RUN
NORMAL CHECKLIST
B737- 7/8/900
FLIGHT DECK SAFETY
Cover Button
(Before applying AC electrical power)
Aircraft Technical Status ................................... CHECKED
Circuit breakers ................................................. IN
Flight recorder test switch ................................. NORMAL
EEC selector p/b’s ............................................ ON
Passenger oxygen switch ................................. NORMAL
IRS switches ..................................................... OFF
Dome white switch ............................................ OFF
Service interphone switch ................................. OFF
Fuel cross feed selector ................................... CLOSED
Fuel pump switches .......................................... OFF
Galley power switch (if installed) ...................... OFF
CAB/UTIL and IFE/Pass seat switches ............ OFF
(if installed)
Standby power switch ....................................... AUTO
Emer. Exit lights switch ..................................... OFF
Wiper selectors ................................................. PARK
Window heat switches ...................................... OFF
Probe heat switches ......................................... OFF or AUTO
Wing anti-ice switch .......................................... OFF
Eng anti-ice switches ........................................ OFF
Eng hydr. Pump switches ................................. ON
Elec hydr. pump switches ................................. OFF
Pack switches ................................................... OFF
Isolation valve switch ........................................ OPEN
Engine bleed switches ...................................... ON
APU bleed switch ............................................. OFF
4
05-92-02 rev: 5
01 Jan 2017
k
ENGINE RUN
NORMAL CHECKLIST
B737- 7/8/900
FLIGHT DECK SAFETY
Cover Button
(continued)
Pressurization mode selector ........................... AUTO
Engine start switches ........................................ OFF
IGN select switch .............................................. IGN R
APU switch ....................................................... OFF
Exterior light switches ....................................... OFF
Main panel DU’s selectors ................................ NORM
Auto brake select switch ................................... OFF
Landing gear lever ............................................ DOWN
Speed brake lever ............................................ DOWN
DETENT
Flap lever .......................................................... SET
Thrust levers ..................................................... IDLE
Eng start levers ................................................. CUTOFF
Engine & APU fire handles ............................... DOWN &
LOCKED
01 Jan 2017
05-92-02 rev: 5
5
ENGINE RUN
NORMAL CHECKLIST
k
B737- 7/8/900
POWER UP
Cover Button
CB’s .................................................................. PULLED
- Weather radar RT CB
- Aural warning CB
DC meter selector ............................................. BAT
BAT power ........................................................ SET
APU GEN switches ........................................... ON
VHF1 (Apron-traffic control freq.) ...................... SET
Fire test ............................................................. PERFORMED
Fire handles........................................................ CHECKED
ACP L&R ............................................................ SET
Emergency procedures (APU/ EVAC)................ REVIEWED
• IF EXTERNAL POWER IS AVAILABLE
AC meter selector ................................... GRD PWR
GRD PWR switch ................................... ON
Fuel pump 1 aft switch ............................ ON
APU switch ............................................. START
APU freq/ volt .......................................... CHECK
APU GEN switches ................................. ON
APU freq/ volt .......................................... CHECK
• WITH BATTERY POWER ONLY
APU switch ............................................. START
AC meter selector ................................... APU GEN
APU freq/ volt .......................................... CHECK
APU GEN switches ................................. ON
APU freq/ volt .......................................... CHECK
Fuel pump 1 aft switch ............................ ON
01 Jan 2017
05-92-02 Rev: 5
6
k
ENGINE RUN
NORMAL CHECKLIST
B737- 7/8/900
PREPARATION
Cover Button
Testrun forms .............................................
PREPARED
Aircraft gross weight ..................................
CHECKED /
NOTED
700 : 38.810 kg
800 : 41.460 kg
900 : 42.400 kg
Master lights test & dim switch ..................
CHECKED
Display source panel .................................
SET
Fuel panel ..................................................
SET
Probe heat switches ..................................
ON or AUTO
Door warning lights ....................................
OFF
Flap lever ...................................................
UP POSITION
Elec hyd pump switches ............................
ON
Hydraulic pressure.......................................
CHECKED
Rudder pedals L&R ....................................
ADJUST
Parking brake .............................................
SET/ LIGHT ON
Wing/ body OVHT test ...............................
CHECKED
APU bleed switch ......................................
ON
Dual bleed light ............................................
CHECKED
Pressurization mode selector ....................
MANUAL
Position lights .............................................
ON
Eng oil QTY ...............................................
CHECKED
FMS (FLT NO -3333)..................................
SET
Apron control .............................................
INFORM or
REQUEST
01 Jan 2017
05-92-02 Rev: 5
7
k
ENGINE RUN
NORMAL CHECKLIST
B737- 7/8/900
BEFORE ENGINE START
Cover Button
Crew Task Assignment....................................... BRIEFED
Emergency procedures. ................................... BRIEFED
Start up area ..................................................... CLEAR
Master Caution recall ........................................ CHECKED
Ground crew ..................................................... CONFIRM
Seat belt L&R..................................................... FASTENED
Permit Start time ................................................ NOTED
L&R display select panel .................................. SET
Anti-collision lights ............................................ ON
01 Jan 2017
05-92-02 rev:5
8
k
ENGINE RUN
NORMAL CHECKLIST
B737- 7/8/900
STARTING LIMITS
Cover Button
a) EGT ........................................
725°C max
b) Fuel flow ................................
300 – 330 kg/h
c) Light up ..................................
within 10 sec.
d)
< 30% N2 permitted
< 0% N2 recommended
Starter re-engagement ............
e) Starter air pressure .................. 25 – 55 psi
(Using ext. pneumatic or cross bleed)
f)
9
Stable to IDLE ......................... . 120 sec.
05-92-02 Rev: 5
01 Jan 2017
k
ENGINE RUN
NORMAL CHECKLIST
B737- 7/8/900
ENGINE START
Cover Button
Engine start switch .......................................... GRD
Left Seat
Right Seat
- Starter valve open light ON:
Call ............“STARTER VLV
OPEN”
- Monitor secondary engine
parameters
- At N2 indication:
Call ……………..……….“N2”
- At N1 indication:
Call ……………….……..“N1”
- At positive Oil pressure
Call ……“OIL PRESSURE”
- At 25%N2 or max. motoring:
START LEVER.IDLE
Call ………..…….."FUEL ON”
- At FF indication
Call………….. “FUEL FLOW”
- At EGT rise:
Call …...……......"LIGHT UP"
- At N2 55% indication: Engine start switch OFF ”
- Starter valve open light OFF:
Call ……….”STARTER VLV
CLOSED”
- EGT stabilized and EGT MAX
Start ind. removed:
Call .…………"ENGINE
STABILIZED"
- Monitor secondary engine
parameters
Elapse time .................................................... RUN
After Engine Start checklist ............................. PERFORM
01 Jan 2017
05-92-02 Rev: 5
10
ENGINE RUN
NORMAL CHECKLIST
k
B737- 7/8/900
AFTER ENGINE START
Engine idle parameters .............................
•
•
•
•
•
•
•
N1 approx.
EGT
N2 approx.
FF approx
Oil press
Oli temp
Vibration
Cover Button
CHECK
: 20%
: 320 - 520°C
: 59%
: 300 kg/h
: > 13 psi
: < 140°C
: < 4 units
Oil filter bypass light ..................................
OFF
Eng valve closed light ...............................
OFF
Spar valve closed light ..............................
OFF
Fuel filter bypass light ................................
OFF
Generator drive light ..................................
OFF
Eng anti-ice ...............................................
AS REQUIRED
Hyd pump low press lights ........................
OFF
APU Bleed / External bleed .......................
OFF
Ground crew ..............................................
INFORM
Shoulder Harness
- Test above Idle thrust setting L&R........
FASTENED
01 Jan 2017
05-92-02 Rev: 5
11
k
ENGINE RUN
NORMAL CHECKLIST
B737- 7/8/900
ENGINE SHUTDOWN
Cover Button
Thrust levers ..................................................... IDLE
Ground crew ..................................................... INFORM
APU gen or GRD PWR ..................................... ON
Eng start levers .................................................. CUTOFF
Engine parameters ............................................ CHECK
Anti collision light .............................................. OFF
Elapse time ......................................................... NOTED
Permit Stop time ............................................... NOTED
Fuel pump switches .......................................... SET
Probe heat switches ......................................... OFF or AUTO
Eng anti-ice ....................................................... OFF
Hyd system ....................................................... NORMAL
Bleed system .................................................... NORMAL
Pressurization mode selector ........................... AUTO
Position light ..................................................... OFF
Platform traffic control ....................................... INFORM
Engine oil QTY .................................................. CHECKED
Fuel used .......................................................... NOTED
Hydraulic oil QTY .............................................. CHECKED
L&R display panel selectors ............................. NORM
Circuit breakers ................................................. IN
01 Jan 2017
05-92-02 Rev: 5
12
k
ENGINE RUN
NORMAL CHECKLIST
B737- 7/8/900
POWER DOWN
Cover Button
External power ..............................................
AS REQUIRED
APU switch ...................................................
OFF
Fuel pump 1 aft switch ..................................
OFF
Cockpit lights/ panel lights ............................
OFF
GRD power switch ........................................
OFF
DC meters selector .......................................
BAT
BAT switch ....................................................
OFF
01 Jan 2017
05-92-02 Rev: 5
13
k
ENGINE RUN
NORMAL CHECKLIST
B737- 7/8/900
Cover Button
CROSS BLEED START
Operating engine .............................................. IDLE
Pack switches ................................................... OFF
Isolation valve switch ........................................ OPEN
Bleed switches .................................................. ON
Thrust lever ....................................................... ADVANCE
Engine start ..................................................... CHECKLIST
Thrust lever ....................................................... IDLE
After engine start checklist ............................... PERFORM
01 Jan 2017
05-92-02 Rev: 5
14
k
ENGINE RUN
EMERGENCY CHECKLIST
B737- 7/8/900
ENGINE START FAILURES
STARTER VALVE FAILS TO CLOSE
► Engine Start Switch ...................................
OFF
► All air sources ............................................
OFF
► Engine start lever ......................................
CUTOFF
Ground crew .................................................. INFORM
15
05-92-02 Rev: 5
01 Jan 2017
Cover Button
ENGINE RUN
EMERGENCY CHECKLIST
k
B737- 7/8/900
Cover Button
ENGINE START FAILURES
ABORTED ENGINE START
(Hot, Hung, no light up)
► Engine Start levers ..................................
CUTOFF
► EGT/ N2/ FF .............................................
MONITOR
► Dry Motor the Engine ...............................
60 sec.
● If starter was already disengaged wait till N2 is below
30% to select the Engine Start switch to GND again
Ground crew .................................................
INFORM
► Engine Start switch ..................................
OFF
NOTE:
● Engine start limit not exceeded.
- ENG CONTROL light maybe illuminated,
maintenance action required.
● Engine start limit exceeded.
- Maintenance action required
01 Jan 2017
05-92-02 rev: 5
16
ENGINE RUN
EMERGENCY CHECKLIST
k
B737- 7/8/900
NON NORMAL ENGINE CONDITIONS
Cover Button
ENGINE STALL
► Thrust levers. .............................................
IDLE
- Check for normal EGT, N2 parameters and vibration level
- Advance thrust lever slowly to find if stall will occur again
● No further STALL observed
- Eng indication normal, continue engine operation
● STALL recur
- Record operational engine conditions at time of stall
- Operate Engine in idle .........................
3 minutes.
- Engine Start lever ................................
CUTOFF
Engine inspection required
ENGINE FAILURE or FLAME OUT
Thrust levers ...............................................
IDLE
Eng Start levers ..........................................
CUTOFF
If conditions permit
Dry Motor the Engine ..............................
60 sec.
● If N1/ N2 show rotation
● If starter was already disengaged wait till N2 is below
30% to select the Eng Start switch to GND again
Eng Start switch ..........................................
01 Jan 2017
05-92-02 rev: 5
OFF
17
k
ENGINE RUN
EMERGENCY CHECKLIST
B737- 7/8/900
FIRE CONDITIONS
TAIL PIPE FIRE
Cover Button
► Thrust levers ......................................... IDLE
► Eng Start lever ........................................ CUTOFF
► Bleed source ........................................... ON
► Dry Motor the Engine until fire is extinguished
● If starter was already disengaged wait till N2 is below 30%
to select the Eng Start switch to GND again
Apron Control ...................................... INFORM*
Ground crew ......................................... INFORM
If fire is out
Eng Start switch .................................... OFF
* Communication Apron control see page 19
NOTE:
- Do not obey the starter time limits.
- If the fire continues, use a fire extinguishing agent to put
out the fire, consider Evacuation procedure.
APU FIRE
► Bell ........................................................ CUTOUT
► Thrust levers ......................................... IDLE
► APU fire handle ..................................... PULL & ROTATE
► APU switch ............................................ OFF
► APU bleed switch .................................. OFF
Apron Control ......................................... INFORM*
Ground crew .......................................... INFORM
* Communication Apron control see page 19
NOTE :
With APU access door open, request ground crew to fight
the fire.
APU fire continues
Evacuation procedure ............................. PERFORM
18
05-92-02 Rev: 4
01 Oct 2013
k
ENGINE RUN
EMERGENCY CHECKLIST
B737- 7/8/900
FIRE CONDITIONS
Cover Button
ENGINE FIRE
► Bell ........................................................ CUTOUT
► Thrust levers ......................................... IDLE
► Eng start levers ..................................... CUTOFF
► Eng fire handle ......................................PULL & ROTATE
NOTE:
If bottle discharge light not on, operate other bottle.
Fuel pump switches ................................OFF
Apron Control ..........................................INFORM *
Ground crew ........................................... INFORM
* Communication Apron control see below
After 30 sec.:
● Eng fire warning light still ON
► Remaining bottle ..................................... DISCHARGE
If fire persists:
Evacuation procedure...............................PERFORM
*Communication Apron control “ Koepel”.
• A/C
Koepel hier PH - ● ● ● BRANDMELDING
• Koepel
P ● ● hier koepel, brandmelding,
gaat uw gang
• A/C
P ● ● , op positie “---” ,
brand op motor “---” , APU fire or Tail pipe fire
verzoek assistentie brandweer
• Koepel
P ● ● , op positie “---” ,
brand op motor “---” (of APU),
wij sturen de brandweer
• A/C
P ● ● , dat is begrepen
NOTE :
- If fire brigade is at the spot for inspection,
Anti-collision switch OFF
01 Jan 2017
05-92-02 Rev: 5
19
k
ENGINE RUN
EMERGENCY CHECKLIST
B737- 7/8/900
EVACUATION PROCEDURE
Cover Button
Thrust levers .............................................. IDLE
Eng start levers............................................ CUTOFF
Eng fire handles .......................................... PULL
APU fire handle ........................................... PULL
Ground crew ............................................... INFORM
Apron-Traffic Control ................................... INFORM*
GRD PWR switch ...................................... OFF
BAT switch ................................................. OFF
Crew ........................................................... EVACUATE
AIRCRAFT
*Communication Apron control “ Koepel”.
• A/C
Koepel hier PH - ● ● ● , EVACUATIE
• Koepel
P ● ● hier koepel, evacuatie, gaat uw gang
• A/C
P ● ● , evacuatie met “---“ personen wegens
aanhoudende APU/ Engine brand op positie “---“,
verzoek assistentie hulpdiensten
• Koepel
P ● ● , evacuatie met “---“ personen wegens
aanhoudende APU/ Engine brand,
wij sturen de hulpdiensten naar positie “---“
• A/C
P ● ● , dat is begrepen
INCAPACITATION
Start switch ................................................. CHECKED/OFF
Thrust levers .............................................. IDLE
Apron Control............................................... INFORM
Ground crew ............................................... INFORM
Elec. Ext. Power/ APU available ................ CONNECT
NOTE :
If conditions permit, allow the engine to cool down for
3 minutes
Eng start levers............................................ CUTOFF
Anti-collision light ........................................ OFF
20
05-92-02 Rev: 5
01 Jan 2017