b737 First Officer Note

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B737-900ER FIRST OFFICER’S NOTE

1. NORMAL PROCEDURES

1.1 GENERAL

1.2 PROCEDURES

2. LIMITATIONS

3. MEMORY ITEMS

3.1 ABORT ENGINE START

3.2 AIRSPEED UNRELIABLE

3.3 APU FIRE

3.4 CABIN ALTITUDE WARNING

3.5 EMERGENCY DESCENT

3.6 ENGINE FIRE

3.7 ENGINE LIMITS OR SERGE OR STALL

3.8 ENGINE OVERHEAT

3.9 ENGINE SEVERE DAMAGE OR SEPARATION

3.10 ENGINE TAIL PIPE FIRE

3.11 EVACUATION

3.12 LANDING CONFIGURATION

3.13 LOSS OF THRUST ON BOTH ENGINES

3.14 RAPID DEPRESSURIZATION

3.15 RUNAWAY STABILIZER

3.16 SMOKE, FIRE OR FUMES

3.17 TAKE OFF CONFIGURATION

3.18 WARNING HORN

3.19 WARNING LIGHTS( CABIN ALTITUDE OR TAKE OFF CONFIGURATION)

4. ON BOARD REQUIRED DOCUMENT CHECKLIST

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1. NORMAL PROCEDURES

1.1 GENERAL

PHILOSOPHY AND ASSUMPTIONS

Normal procedures verify for each phase of flight that:

• The airplane condition is satisfactory

• The flight deck configuration is correct.

Normal procedures are done on each flight. Refer to the Supplementary Procedures (SP) chapter for

procedures that are done as needed, for example the adverse weather procedures.

Normal procedures are written for a trained flight crew and assume:

• All systems operate normally

• The full use of all automated features (LNAV, VNAV, autoland, autopilot, and autothrottle). This

does not preclude the possibility of manual flight for pilot proficiency where allowed

Normal procedures also assume coordination with the ground crew before:

• Hydraulic system pressurization, or

• Flight control surface movement, or

• Airplane movement.

Normal procedures do not include steps for flight deck lighting and crew comfort items.

Normal procedures are done by memory and scan flow. The panel illustration in this section shows the

scan flow. The scan flow sequence may be changed as needed.

CONFIGURATION CHECK

It is the crew member’s responsibility to verify correct system response. Before engine start, use system

lights to verify each system's condition or configuration.

After engine start, the master caution system alerts the crew to warnings or cautions away from the

normal field of view.

If there is an incorrect configuration or response:

• Verify that the system controls are set correctly

• Check the respective circuit breaker as needed. Maintenance must first determine that it is safe

to reset a tripped circuit breaker on the ground

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Before engine start, use individual system lights to verify the system status. If an individual system light

indicates an improper condition:

• Check the Dispatch Deviations Guide (DDG) or the operator equivalent to decide if the condition

has a dispatch effect

• Decide if maintenance is needed

If, during or after engine start, a red warning or amber caution light illuminates:

• Do the respective non-normal checklist (NNC)

• On the ground, check the DDG or the operator equivalent

If, during recall, an amber caution illuminates and then extinguishes after a master caution reset:

• Check the DDG or the operator equivalent

• The respective non-normal checklist is not needed

CREW DUTIES

Preflight and post flight crew duties are divided between the captain and first officer. Phase of flight

duties are divided between the Pilot Flying (PF) and the Pilot Monitoring (PM.)

Each crewmember is responsible for moving the controls and switches in their area of responsibility:

• The phase of flight areas of responsibility for both normal and non-normal procedures is shown

in the Area of Responsibility illustrations in this section. Typical panel locations are shown

• The preflight and post flight areas of responsibility are defined by the “Preflight Procedure -

Captain” and “Preflight Procedure – First Officer.”

The captain may direct actions outside of the crewmember’s area of responsibility The general PF phase

of flight responsibilities are:

• taxiing

• flight path and airspeed control

• airplane configuration

• navigation.

The general PM phase of flight responsibilities are:

• checklist reading

• communications

• tasks asked for by the PF

• monitoring taxiing, flight path, airspeed, airplane configuration and navigation.

PF and PM duties may change during a flight. For example, the captain could be the PF during taxi but be

the PM during takeoff through landing.

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Normal procedures show who does a step by crew position (C, F/O, PF, or PM):

• in the procedure title, or

• in the far right column, or

• in the column heading of a table

The mode control panel is the PF’s responsibility. When flying manually, the PF directs the PM to make

the changes on the mode control panel.

The captain is the final authority for all tasks directed and done.

SCAN FLOW/ AREA OF RESPONSIBILITY

The scan flow and areas of responsibility diagrams shown below are representative and may not match

the configuration(s) of your airplanes.

The scan flow diagram provides general guidance on the order each flight crew member should follow

when doing the preflight and post flight procedures.

Specific guidance on the items to be checked are detailed in the amplified Normal Procedures. For

example, preflight procedure details are in the Preflight Procedure - Captain and Preflight Procedure -

First Officer.

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AREA OF RESPONSIBILITY CAPTAIN IS PF

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1.2 PROCEDURES

1.2.1 ELECTRICAL POWER UP PROCEDURES

The following procedure is accomplished to permit safe application of electrical power.

1. BATTERY switch ... Guard closed

2. STANDBY POWER switch ... Guard closed 3. ALTERNATE FLAPS master switch ... Guard closed 4. Windshield WIPER selector(s) ... PARK 5. ELECTRIC HYDRAULIC PUMPS switches... OFF 6. LANDING GEAR lever ... DN 7. Fires Test……….Perform

• Verify that the engine No. 1, APU and No. 2 fire switches are in. • OVERHEAT DETECTOR switches – NORMAL

• TEST switch – Hold to FAULT/INOP

o Verify that the MASTER CAUTION lights are illuminated. o Verify that the OVHT/DET annunciator is illuminated. o Verify that the FAULT light is illuminated.

o Verify that the APU DET INOP light is illuminated. • TEST switch – Hold to OVHT/FIRE

o Verify that the fire warning bell sounds.

o Verify that the master FIRE WARN lights are illuminated. o Verify that the MASTER CAUTION lights are illuminated. o Verify that the OVHT/DET annunciator is illuminated. • Master FIRE WARN light – Push

o Verify that the master FIRE WARN lights are extinguished. o Verify that the fire warning bell cancels.

o Verify that the engine No. 1, APU and No. 2 fire switches stay illuminated. o Verify that the ENG 1 OVERHEAT and ENG 2 OVERHEAT lights stay illuminated. 8. EXTINGUISHER TEST switch………..…..Check

• TEST Switch - Position to 1 and hold

o Verify that the three green extinguisher test lights are illuminated. • TEST Switch - Release

o Verify that the three green extinguisher test lights are extinguished. • Repeat for test position 2.

9. APU………..start 10. Lights ……….set

• Circuit breaker and panel lights (overhead) • Position and wheel well lights

• Main panel and DU (Captain and F/O rudder panel) • Flood and panel lights (pedestal panel)

11. APU GENERATOR bus switch………on 12. Wheel well fire warning system………..……..test

• Test switch – Hold to OVHT/FIRE

o Verify fire warning bell sounds, master FIRE WARN lights, MASTER CAUTION lights and OVHT/DET annunciator illuminate.

• Fire warning BELL CUTOUT switch – Push

o Verify that the master FIRE WARN lights extinguish. o Verify that the fire warning bell cancels.

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ELECTRICAL POWER UP PROCEDURES

1 2 3 4 5 6 7 8 9 11 12 10 light on

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1.2.2 PRELIMINARY PREFLIGHT PROCEDURES

The Preliminary Preflight Procedure assumes that the Electrical Power Up supplementary procedure is

complete.

1. IRS mode selectors ...OFF, then NAV • Verify that the ON DC lights illuminate then extinguish. • Verify that the ALIGN lights are illuminated.

2. Verify that the following are sufficient for flight: • oxygen pressure

• hydraulic quantity • engine oil quantity

3. on board library………Check (see item 4.1) 4. Maintenance documents ... Check

5. FLIGHT DECK ACCESS SYSTEM switch ... Guard closed 6. Emergency equipment ... Check

• F/O escape rope • F/O life vest • F/O goggle • 3 gear pins • Fire extinguisher

• Observer goggle and mask • PBE

• Flash light • Crash axe • Captain life vest • Asbestos gloves • Captain goggle • Captain escape rope

7. ELT switch... Guard closed • Verify that the ELT light is extinguished.

8. PSEU light ...Verify extinguished 9. ILS panel ...Check

• Display selector at heading status • System display…… L

10. GPS light ...Verify extinguished 11. SERVICE INTERPHONE switch... OFF 12. ENGINE panel ... Set

• Verify that the REVERSER lights are extinguished. • Verify that the ENGINE CONTROL lights are extinguished. 13. EEC switches – ON

14. Oxygen panel ... Set

• PASSENGER OXYGEN switch………Guard closed • Verify that the PASS OXY ON light is extinguished.

15. Secondary Landing gear indicator lights ... Verify illuminated 16. Flight recorder switch ... Guard closed 17. STALL WARNING TEST switches... Push and hold, one at a time

• Verify that each control column vibrates when the respective switch is pushed. 18. Circuit breakers (P6 panel) ... Check

19. Circuit breaker at pedestal and rudder panel……….……Check 20. Manual gear extension access door ...Closed 21. Circuit breakers (control stand, P18 panel) ... Check 22. Parking brake... As needed

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1.2.3 CDU PREFLIGHT PROCEDURES

1. IDENT PAGE 2.POSITION INIT PAGE 3. ROUTE PAGE

• Select aircraft model

• Select NAV aid database update • Select POS INIT • Go to page 2

• Select position from GPS L • Put in the box

• If aircraft parking in bay, cross check with coordination in Jepp.

• For flight plan VTBD to VTCC • Originating point get from GPS,

put in 1L box (VTBD)

• Put destination VTCC in 1R box • Departing runway in 3L box • Flight number in 2R box

4. DEP/ARR PAGE 5. ROUTE PAGE 6. LEGS PAGE

• Select departing aerodrome • Select departing runway • Select SID transition

• Repeat for arriving aerodrome

• Start from page 2 to build flight plan

• Left side is airway (via) • Right side is waypoint

• After finishing route page, EXEC • Go to leg page, cross check all

way points in flight plan • Select PERF INIT 6R to proceed

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7. PERF INIT PAGE 8. N1 LIMIT PAGE 9. TAKE OFF REF PAGE • Select PERF INIT PAGE

• Fill up the empty boxes • Select N1 LIMT PAGE to

proceed

• Input assumed temperature (----)/ OAT (box)on 1L • Select derated climb as

required

• Find take off speed in RAM • Go to page 2 correct

acceleration altitude and thrust reduction altitude as required

10. CLIMB PAGE 11. CRUISE PAGE 12. DESCENT PAGE

• Check speed restriction below

10,000 feet • Check cruising altitude • Check speed restriction below 10,000 feet • Select FORECAST to put

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1.2.3 CDU PREFLIGHT PROCEDURES (CONTINUED)

13. FIX PAGE 14. PROGRESS PAGE • Go to FIX PAGE 1

• Set MSA as per approach chart • Go to page 2

• Set reference point in case of returning to land

• Check total distance

• Check fuel (ramp fuel, landing fuel and trip fuel)

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1.2.4 PREFLIGHT PROCEDURES

1. Flight Control Panel... Check • FLIGHT CONTROL switches – Guards closed

• Verify that the flight control LOW PRESSURE lights are illuminated. 2. Flight SPOILER switches………..Guards closed 3. YAW DAMPER switch………..ON • Verify that the YAW DAMPER light is extinguished.

• Verify that the standby hydraulic LOW QUANTITY light is extinguished. • Verify that the standby hydraulic LOW PRESSURE light is extinguished. • Verify that the STBY RUD ON light is extinguished.

4. ALTERNATE FLAPS master switch……… Guard closed 5. ALTERNATE FLAPS position switch……….……. OFF

• Verify that the FEEL DIFF PRESS light is extinguished. • Verify that the SPEED TRIM FAIL light is extinguished. • Verify that the MACH TRIM FAIL light is extinguished. • Verify that the AUTO SLAT FAIL light is extinguished.

6. NAVIGATION panel... Set • VHF NAV transfer switch – NORMAL

• IRS transfer switch – NORMAL • FMC transfer switch – NORMAL

7. DISPLAYS panel... Set • SOURCE selector – AUTO

• CONTROL PANEL select switch – NORMAL

8. FUEL panel... Set • Verify that the ENG VALVE CLOSED lights are illuminated dim. • Verify that the SPAR VALVE CLOSED lights are illuminated dim. • Verify that FI LTER BYPASS lights are extinguished.

9. CROSSFEED selector………..………. Closed • Verify that the VALVE OPEN light is extinguished.

10. FUEL PUMP switches……….OFF

• Verify that the center tank fuel pump LOW PRESSURE lights are extinguished. • Verify that the main tank fuel pump LOW PRESSURE lights are illuminated. 11. ELECTRICAL panel... Set

• BATTERY switch – Guard closed • CAB/UTIL power switch – ON • IFE/PASS SEAT power switch – ON • STANDBY POWER switch – Guard closed

o Verify that the STANDBY PWR OFF light is extinguished. o Verify that the BAT DISCHARGE light is extinguished. o Verify that the TR UNIT light is extinguished.

o Verify that the ELEC light is extinguished.

12. GENERATOR DRIVE DISCONNECT switches………Guards closed • Verify that the DRIVE lights are illuminated.

13. BUS TRANSFER switch……….Guard closed • Verify that the TRANSFER BUS OFF lights are extinguished. • Verify that the SOURCE OFF lights are extinguished. 14. Verify that the GEN OFF BUS lights are illuminated.

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1.2.4 PREFLIGHT PROCEDURES (CONTINUED)

15. OVERHEAT AND FIRE PROTECTION panel... Check

Do these check if the flight crew did not do the Electrical Power Up supplementary procedures. This check is needed once per flight day or following a flight crew change.

• Verify that the engine No. 1, APU, and engine No. 2 fire switches are in. Alert ground personnel before the following test are accomplished:

15.1 OVERHEAT DETECTOR switches………..NORMAL 15.2 TEST switch……….Hold to FAULT/INOP

• Verify that the MASTER CAUTION lights are illuminated. • Verify that the OVHT/DET annunciator is illuminated. • Verify that the FAULT light is illuminated.

• If the FAULT light fails to illuminate, the fault monitoring system is inoperative. • Verify that the APU DET INOP light is illuminated.

Do not run the APU if the APU DET INOP light does not illuminate.

15.3 TEST switch………..….Hold to OVHT/FIRE • Verify that the fire warning bell sounds.

• Verify that the master FIRE WARN lights are illuminated. • Verify that the MASTER CAUTION lights are illuminated. • Verify that the OVHT/DET annunciator is illuminated.

15.4 Master FIRE WARN light………Push • Verify that the master FIRE WARN lights are extinguished.

• Verify that the fire warning bell cancels.

• Verify that the engine No. 1, APU and engine No. 2 fire switches stay illuminated. • Verify that the ENG 1 OVERHEAT and ENG 2 OVERHEAT lights stay illuminated. • Verify that the WHEEL WELL light stays illuminated.

16. EXTINGUISHER TEST switch ………Check 16.1 TEST switch – Position to 1 and hold.

• Verify that the three green extinguisher test lights are illuminated. 16.2 TEST switch – Release

• Verify that the three green extinguisher test lights are extinguished. 16.3 Repeat for test position 2.

17. APU switch (as needed)... START

CAUTION: Center tank fuel pump switches should be positioned ON only if the fuel quantity in the center tank exceeds 453 kgs.

CAUTION: do not operate the center tank fuel pumps with the flight deck unattended.

18. APU GENERATOR bus switches – ON

• Verify that the SOURCE OFF lights are extinguished. • Verify that the TRANSFER BUS OFF lights are extinguished.

19. EQUIPMENT COOLING switches... NORM • Verify that the OFF lights are extinguished.

20. EMERGENCY EXIT LIGHTS switch... Guard closed • Verify that the NOT ARMED light is extinguished.

21. Passenger signs... Set • NO SMOKING switch – ON

• FASTEN BELTS switch –(verify refueling completed) ON

22. Windshield WIPER selectors... PARK • Verify that the windshield wipers are stowed.

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1.2.4 PREFLIGHT PROCEDURES (CONTINUED)

23. WINDOW HEAT switches... ON • Position switches ON at least 10 minutes before takeoff.

• Verify that the OVERHEAT lights are extinguished. • Verify that the ON lights are extinguished.

24. PROBE HEAT switches... OFF/AUTO • Verify that all lights are illuminated.

25. WING ANTI–ICE switch... OFF • Verify that the VALVE OPEN lights are extinguished.

26. ENGINE ANTI–ICE switches... OFF • Verify that the COWL ANTI–ICE lights are extinguished.

• Verify that the COWL VALVE OPEN lights are extinguished.

27. Hydraulic panel... Set 27.1 ENGINE HYDRAULIC PUMPS switches – ON

• Verify that the LOW PRESSURE lights are illuminated. 27.2 ELECTRIC HYDRAULIC PUMPS switches – OFF

• Verify that the OVERHEAT lights are extinguished. • Verify that the LOW PRESSURE lights are illuminated.

28. Air conditioning panel... Set 28.1 AIR TEMPERATURE source selector ………..As needed 28.2 TRIM AIR switch ……….ON

• Verify that the ZONE TEMP lights are extinguished.

28.3 Temperature selectors ………..As needed • Verify that RAM DOOR FULL OPEN lights are illuminated.

28.4 RECIRCULATION FAN switches ………auto 28.5 Air conditioning PACK switches ……….AUTO or HIGH 28.6 ISOLATION VALVE switch ………..………..OPEN 28.7 Engine BLEED air switches ……….ON 28.8 APU BLEED air switch……….ON

• Verify that the DUAL BLEED light is illuminated. • Verify that the PACK lights are extinguished.

• Verify that the wing body overheat lights are extinguished. • Verify that the bleed trip off lights are extinguished

29. Cabin pressurization panel... Set • Verify that the AUTO FAIL light is extinguished.

• Verify that the OFF SCHED DESCENT light is extinguished.

30. FLIGHT ALTITUDE indicator………..Cruise altitude. 31. LANDING ALTITUDE indicator……….………….Destination field elevation 32. Pressurization mode selector ………AUTO

• Verify that the ALTN light is extinguished. • Verify that the MANUAL light is extinguished.

33. Lighting panel... Set • See Lighting Management on GENERAL section for details.

34. Ignition select switch... IGN L or R • First flight of the day or following a flight crew change - select IGN R • Alternate the ignition select switch position on subsequent starts. 35. ENGINE START switches... OFF 36. Lighting pane... Set

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1.2.4 PREFLIGHT PROCEDURES (CONTINUED)

37. Mode control panel... Set • COURSE(S) – Set

• FLIGHT DIRECTOR switch – ON

38. EFIS control pane... Set • MINIMUMS reference selector – RADIO or BARO

• MINIMUMS selector – Set engine out acceleration altitude as reference • FLIGHT PATH VECTOR switch – As needed

• METERS switch – As needed

• BAROMETRIC reference selector – IN or HPA • BAROMETRIC selector – Set local altimeter setting • VOR/ADF switches – As needed

• Mode selector – MAP • CENTER switch – As needed

• Range selector – PF: 10 - 40nm / PM one range higher • TRAFFIC switch – As needed

• WEATHER RADAR – Off

• Verify that the weather radar indications are not shown on the MAP. • Map switches – As needed.

39. Oxygen... Test and set • Crew oxygen pressure – Check

• Verify that the pressure is sufficient for dispatch. • Oxygen mask – Stowed and doors closed • RESET/TEST switch – Push and hold

• Verify that the yellow cross shows momentarily in the flow indicator. • EMERGENCY/TEST selector – Push and hold

• Continue to hold the RESET/TEST switch down and push the EMERGENCY/TEST selector for 5 seconds.

• Verify that the yellow cross shows continuously in the flow indicator. • Verify that the crew oxygen pressure does not decrease more than 100 psig. • If the oxygen cylinder valve is not in the full open position, pressure can:

o decrease rapidly, or

o decrease more than 100 psig, or o increase slowly back to normal.

• Release the RESET/TEST switch and the EMERGENCY/TEST selector. • Verify that the yellow does not show in the flow indicator.

• Normal/100% selector – 100%

40. Clock... Set • TIME/DATE pushbutton - UTC time

41. Display select panel... Set • MAIN PANEL DISPLAY UNITS selector – NORM

• LOWER DISPLAY UNIT selector – NORM

42. Disengage light TEST switch... Hold to 1 • Verify that the A/P light is illuminated steady amber.

• Verify that the A/T light is illuminated steady amber. • Verify that the FMC light is illuminated steady amber.

43. Disengage light TEST switch... Hold to 2 • Verify that the A/P light is illuminated steady red.

• Verify that the A/T light is illuminated steady red. • Verify that the FMC light is illuminated steady amber. Do the Initial Data and Navigation Data steps from the CDU Preflight

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1.2.4 PREFLIGHT PROCEDURES (CONTINUED)

42. Flight instruments... Check • Verify that the flight instrument indications are correct.

• Verify that only these flags are shown: o TCAS OFF

o NO VSPD until V–speeds are selected o expected RMI flags

• Verify that the flight mode annunciations are correct: o auto throttle mode is blank

o roll mode is blank o pitch mode is blank o AFDS status is FD • Select the map mode.

43. GROUND PROXIMITY panel... Check • FLAP INHIBIT switch – Guard closed

• GEAR INHIBIT switch – Guard closed • TERRAIN INHIBIT switch – Guard closed

• Verify that the GROUND PROXIMITY INOP light is extinguished. 44. Landing gear panel... Set

• Landing gear lever – DN

• Verify that the green landing gear indicator lights are illuminated. • Verify that the red landing gear indicator lights are extinguished. 45. AUTO BRAKE selector... RTO

• Verify that the AUTO BRAKE DISARM light is extinguished

46. ANTISKID INOP light... Verify extinguished 47. Engine display control panel... Set

• N1 SET selector - AUTO

• SPEED REFERENCE selector – AUTO • FUEL FLOW switch – RATE

• Move switch to RESET, then RATE.

48. Engine instruments... Check

• Verify that the primary and secondary engine indications show existing conditions. • Verify that no exceedance is shown.

• Verify that the hydraulic quantity indications do not show RF. 49. CARGO FIRE panel... Check This check is needed once per flight day or following a flight crew change. 49.1 DETECTOR SELECT switches – NORM

49.2 TEST switch – Push

• Verify that the fire warning bell sounds.

• Verify that the master FIRE WARN lights are illuminated. 49.3 Master FIRE WARN light – Push

• Verify that the master FIRE WARN lights are extinguished. • Verify that the fire warning bell cancels.

• Verify that the FWD and AFT lights stay illuminated. • Verify that the DETECTOR FAULT light stays extinguished. • Verify that the green EXTINGUISHER test lights stay illuminated. • Verify that the DISCH light stays illuminated.

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1.2.4 PREFLIGHT PROCEDURES (CONTINUED)

50. Radio tuning panel... Set • WARNING: Do not key HF radio while airplane is being fueled. • Injury to personnel or fire may result.

• Verify that the OFF light is extinguished.

50.1 VHF NAVIGATION radios... Set for departure 50.2 Audio control panel... .Set 50.3 ADF radios... Set 50.4 WEATHER RADAR panel... Set 50.5 Transponder panel... Set 50.6 STABILIZER TRIM override switch. ... Guard closed

51. Seat... Adjust

• Use the handhold above the forward window for assistance when pulling the seat forward. Do not use the glare shield as damage can occur.

• Adjust the seat for optimum eye reference. • Verify a positive horizontal (fore and aft) seat lock.

52. Rudder pedals... Adjust

• Adjust the rudder pedals to allow full rudder pedal and brake pedal movement. 53. Seat belt and shoulder harness... Adjust

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1.2.5 BEFORE START PROCEDURES

BEFORE START PROCURE FUEL PUMPS……….on HYDRAULIC PUMPS……….on ANTI COLLISION LIGHT………..on LOWER DU……..check hydraulic pressure

1

2

3

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1.2.6 BEFORE TAXI PROCEDURES

AFTER START/BEFORE TAXI PROCURE 1. ECTRIC POWER GEN 1 AND 2...on 2. PROBE HEAT………..….on 3. PACKS……….……auto 4. ISOLATION SWITCH………...….auto 5. APU BLEED……….………off 6. APU……….………off 7. ENGINE START………….…..continuous 8. RECALL……….……….check 9. LOWER DU………check blank

1 2 3 4 5 6 7 8 9

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1.2.7 BEFORE TAKE OFF PROCEDURES

BEFORE TAKE OFF PROCURES 1. STROBE LIGHTS……….on 2. TRANSPONDER………..…..TA/RA

LIGHTG MANAGEMET BEFORE TAXI

1. WHEEL WELL LIGHT………..off 2. TAXI LIGHT………..…auto BEFORE LINE UP

1. STROBE LIGHTS………..on BEFORE TAKE OFF

1. TAXI LIGHTS……….off 2. FIXED LANDING GEAR………..on

1

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1.2.8 CLIMB AND CRUISE PROCEDURES

CLIMB AND CRUIS PROCURES 1. PACKS………check 2. ENGINE START………..…..CONT/ FLT 3. AUTO BRAKE……….…….off 4. LANDING GEAR……….off 5. BANK LIMIT……….25°*

* Recommendation from sim instructor

1

2

3

4 5

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1.2.9 DESCENT PROCEDURES

DESCENT PROCURES 1. LANDING ALTITUDE………..set 2. MINIMUM………..calculate 3. RECALL………..…..check 4. V ref………..………..set 5. AUTO BRAKE……….….set 6. NAV AIDS………..……..set 1 2 3 4 5 6

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1.2.10 APPROACH PROCEDURES

APPROACH PROCURES 1. TRANSITION LEVEL………QNH set 2. PASSENGER SIGN………on 3. 10,000 feet light management FIXED LANDING LIGHTS………..………on STROBE LIGHTS………on (stdy)

1 3

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1.2.11 APPROACH TO LAND PROCEDURES

PHASE OF FLIGHT PRECISION APPROACH NON PRECISION APPROACH 1. If turn to intercept the final

approach course

At 10 nm. Before final approach

course Arm APP Arm VOR/LOC

2. If straight in approach

At 10 nm. Before intermediate fix Arm APP Arm VOR/LOC 3. reduce speed to extend the flaps, check with ND for deceleration point

• If speed window open, or in LVL CH mode, set clean up speed • If speed window closes, or in VNAV mode, speed reduced by itself.

• At clean up speed ( magenta arrow on PFD) or 10 knots above, whichever comes first, select flap 1 • At flap 1 speed, select flap 5

4. localizer capture • Set MCP heading to final approach course. • Set heading bank limit to 15°

5. Glide slope alive

(for precision Approach only) • Gear down • Flap 15 • Arm speed brake • Set ENG START to CONT 6. At 2.2 nm. to final approach fix

(for non-precision approach only)

* SOP uses 2.0, but sim instructor recommends 2.2 nm.

• Gear down • Flap 15

• Arm speed brake • Set ENG START to CONT 7. Glide slope captured

(for precision approach only) • Set landing flap • Set Missed approach altitude

8. At 1.1 nm. to final approach fix (for non-precision approach only)

* SOP uses 1.0, but sim instructor recommends 1.1 nm.

• Set landing flap • Set Missed approach

altitude 300 feet above MDA

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12.2.12 AFTER LANDING PROCEDURES

AFTER LANDING PROCURES (Use captain setting speed brake down as the signal to proceed to procedures) 1. APU………..start 2. PROBE HEAT………..………off 3. LIGHT MANAGEMENT……….….set TAXI LIGHT………...auto POSITION/STROBE………….off 4. ENGINE START………....off/auto 5. WEATHER RADAR………..off 6. AUTO BRAKE……….off 7. TRANSPONDER………..set 8. FLAP……….up 9. TRIM………..…4.0 units 1 2 3 4 5 6 7 8 9

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1.2.12 SHUT DOWN PROCEDURES

ENGINE SHUT DOWN PROCURES 1. ENGINE GEN……….on 2. SEAT BELT SIGN……….……off 3. ANTI COLISION LIGHT………..……off 4. FUEL PUMPS……….………..off 5. CAB/UTIL SWITCH………..…set 6. IFE SWITCH………..set 7. WINDOW HEAT……….…off 8. HYDRAULIC PUMPS………..………set 9. RECIRCULATING………….……..……..auto 10. PACKS……….………..auto 11. ISOLATION……….……….……open 12. ENG BLEED……….…on 13. APU BLEED………..….off 14. APU……….…..as required 15. F/D……….……….off 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15

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1.2.13 SECURE PROCEDURES

PRELIMINARY PREFLIGHT PROCURE 1. IRS………..off 2. EMERGENCY EXIT LIGHT……….off

3. PACKS………..…off 1

2

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2. LIMITATIONS

3. MEMORY ITEMS

3.1 ABORT ENGINE START

1 Engine start lever (affected engine) . . . . CUTOFF

3.2 AIRSPEED UNRELIABLE

1 Autopilot (if engaged) . . . .Disengage

2 Auto throttle (if engaged). . . .Disengage

3 F/D switches (both) . . . ….. . . OFF

4 Set the following gear up pitch attitude and thrust:

Flaps extended . . . 10° and 80% N1

Flaps up . . . 4° and 75% N1

3.3 APU FIRE

1 APU fire switch. . . Confirm . . . .Pull, rotate to the stop, and hold for 1 second

2 APU switch . . . OFF

3.4 CABIN ALTITUDE WARNING

1 Don oxygen masks and set regulators to 100%.

2 Establish crew communications.

3 Pressurization mode selector . . . MAN

4 Outflow VALVE switch . . . Hold in CLOSE until the outflow VALVE indication

shows fully closed

5 If cabin altitude is uncontrollable:

Passenger signs . . . ON

PASS OXYGEN switch . . . ON

Go to the Emergency Descent checklist

3.5 EMERGENCY DESCENT

1 Announce the emergency descent. The pilot flying will advise the cabin crew, on the

PA system, of impending rapid descent. The pilot monitoring will advise ATC and

obtain the area altimeter setting.

2 Passenger signs . . . ON

3 Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is

higher.

4 ENGINE START switches (both) . . . CONT

5 Thrust levers (both) . . . Reduce thrust to minimum or as needed for anti-ice

6 Speed brake . . . FLIGHT DETENT

If structural integrity is in doubt, limit speed as much as possible and avoid high

maneuvering loads.

(30)

3.6 ENGINE FIRE

1 Auto throttle (if engaged) . . . .Disengage

2 Thrust lever (affected engine) . . . Confirm . . . Close

3Engine start lever (affected engine) . . . Confirm . . . CUTOFF

4 Engine fire switch (affected engine) . . . Confirm . . . Pull

To manually unlock the engine fire switch, press the override and pull.

5 If the engine fire switch or ENG OVERHEAT light is illuminated:

Engine fire switch . . . Rotate to the stop and hold for 1 second

If after 30 seconds the engine fire switch or ENG OVERHEAT light stays illuminated:

Engine fire switch. . . .Rotate to the other stop and hold for 1 second

3.7 ENGINE LIMITS OR SERGE OR STALL

1 Auto throttle (if engaged) . . . .Disengage

2 Thrust lever (affected engine) . . . . Confirm. . . . .Retard until engine indications

stay within limits or the thrust lever is closed

3.8 ENGINE OVERHEAT

1 Auto throttle (if engaged). . . .Disengage

2 Thrust lever (affected engine) . . . Confirm . . . Close

3 If the ENG OVERHEAT light stays illuminated:

Go to the ENGINE FIRE or Engine Severe Damage or Separation checklist

3.9 ENGINE SEVERE DAMAGE OR SEPARATION

1 Auto throttle (if engaged) . . . .Disengage

2 Thrust lever (affected engine) . . . Confirm . . . Close

3Engine start lever (affected engine) . . . Confirm . . . CUTOFF

4 Engine fire switch (affected engine) . . . Confirm . . . Pull

To manually unlock the engine fire switch, press the override and pull.

5 If the engine fire switch or ENG OVERHEAT light is illuminated:

Engine fire switch . . . Rotate to the stop and hold for 1 second

If after 30 seconds the engine fire switch or ENG OVERHEAT light stays illuminated:

Engine fire switch. . . .Rotate to the other stop and hold for 1 second

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3.10 ENGINE TAIL PIPE FIRE

1Engine start lever (affected engine) . . . CUTOFF

2 Advise the cabin.

3 Choose one:

3.1 Bleed air is available: Go to step 4

3.2 Bleed air is not available: Advise the tower.

4 PACK switches (both) . . . OFF

5ISOLATION VALVE switch. . . AUTO

6 Engine BLEED air switches (both) . . . ON

7 Choose one:

7.1 APU is running: APU BLEED air switch . . . ON and Go to step 8

7.2 APU is not running: Go to step 8

8 Choose one:

8.1 Affected ENGINE START switch is in GRD: and Go to step 9

8.2 Affected ENGINE START switch is not in GRD: Allow the affected N2 to decrease

below 20%.

ENGINE START switch (affected engine) . . . GRD and Go to step 9

9 Advise the tower.

10 When the tailpipe fire is extinguished:

ENGINE START switch(affected engine) . . . OFF

3.11 EVACUATION

1 PARKING BRAKE. . . Set C

2 Speed brake lever . . . DOWN C

3 FLAP lever . . . 40 F/O

4 Pressurization mode selector . . . MAN F/O

5 Outflow VALVE switch . . . Hold in OPEN until the outflow VALVE

indication shows fully open to depressurize the airplane F/O

6 If time allows, verify that the flaps are 40 before the engine start levers are moved to

CUTOFF. C

7Engine start levers (both) . . . CUTOFF C

8 Advise the cabin to evacuate. C

9 Advise the tower. F/O

10 Engine and APU fire switches (all) . . . . Override and pull F/O

11 If an engine or APU fire warning occurs:

Illuminated fire switch . . . Rotate to the stop and hold for 1 second F/O

3.12 LANDING CONFIGURATION

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3.13 LOSS OF THRUST ON BOTH ENGINES

1 ENGINE START switches (both) . . . FLT

2 Engine start levers (both) . . . CUTOFF

3 When EGT decreases:

Engine start levers (both) . . . IDLE detent

4 If EGT reaches 950°C or there is no increase in EGT within 30 seconds:

Engine start lever (affected engine) . . . . Confirm . . . CUTOFF,

then IDLE detent

If EGT again reaches 950°C or there is no increase in EGT within 30 seconds, repeat as

needed.

3.14 RAPID DEPRESSURIZATION

1 Don oxygen masks and set regulators to 100%.

2 Establish crew communications.

3 Pressurization mode selector . . . MAN

4 Outflow VALVE switch . . . Hold in CLOSE until the outflow VALVE indication

shows fully closed

5 If cabin altitude is uncontrollable:

Passenger signs . . . ON

PASS OXYGEN switch . . . ON

Go to the Emergency Descent checklist

3.15 RUNAWAY STABILIZER

1 Control column. . . Hold firmly

2 Autopilot (if engaged) . . . .Disengage

Do not re-engage the autopilot.

Control airplane pitch attitude manually with control column and main electric trim as

needed.

3 Auto throttle (if engaged). . . .Disengage

Do not re-engage the auto throttle.

4 If the runaway stops after the autopilot is disengaged: (checklist completed)

5 If the runaway continues after the autopilot is disengaged:

STAB TRIM CUTOUT switches (both) . . . CUTOUT

If the runaway continues:

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3.16 SMOKE, FIRE OR FUMES

1 Diversion may be needed.

2 Don oxygen masks and set regulators to 100%, as needed.

3 Don smoke goggles, as needed.

4 Establish crew and cabin communications.

5 BUS TRANSFER switch . . . OFF

6 Advise the cabin crew that the cabin lighting will be extinguished, but passenger

reading lights will continue to work.

7 CAB/UTIL switch. . . OFF

8 IFE/PASS SEAT switch . . . OFF

9 RECIRC FAN switches (both) . . . OFF

10 APU BLEED air switch . . . OFF

11 Anytime the smoke or fumes become the greatest threat:

Go to the Smoke or Fumes Removal checklist

12 Choose one:

12.1 Source of the smoke, fire or fumes is obvious and can be extinguished quickly:

Isolate and extinguish the source.

If possible, remove power from the affected equipment by switch or circuit breaker in

the flight deck or cabin.

Go to step 13

12.2 Source of the smoke, fire or fumes is not obvious or cannot be extinguished

quickly:

Go to step 14

13 Choose one:

13.1 Source is visually confirmed to be extinguished and the smoke or fumes are

decreasing:

Continue the flight at the captain’s discretion.

Restore unpowered items at the captain’s discretion.

Go to the Smoke or Fumes Removal checklist needed (checklist completed)

13.2 Source is not visually confirmed to be extinguished or smoke or fumes are not

decreasing:

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3.16 SMOKE, FIRE OR FUMES (CONTINUED)

14 EQUIP COOLING SUPPLY and EXHAUST switches (both) . . . ALTN

15 Instruct the cabin crew to:

Turn on cabin reading lights.

Turn on galley attendants work lights.

Turn off cabin fluorescent light switches.

16 Divert to the nearest suitable airport while continuing the checklist.

17 Consider an immediate landing if the smoke, fire or fumes situation becomes

uncontrollable.

18 Do not delay landing in an attempt to complete all of the following steps.

19 ISOLATION VALVE switch. . . CLOSE

20 R PACK switch . . . OFF

21 Wait 2 minutes unless the smoke or fumes are increasing. This allows time for the

smoke or fumes to clear.

22 Choose one:

22.1 Smoke or fumes are decreasing:

Go to the Smoke or Fumes Removal checklist on page 8.18, if needed

22.2 Smoke or fumes continue or are increasing:

R PACK switch . . . AUTO

L PACK switch . . . OFF

Go to step 23

23 Wait 2 minutes unless the smoke or fumes are increasing. This allows time for the

smoke or fumes to clear.

24 Choose one:

24.1 Smoke or fumes are decreasing:

Go to the Smoke or Fumes Removal checklist on page 8.18, if needed

24.2 Smoke or fumes continue or are increasing:

L PACK switch . . . AUTO

Consider an immediate landing.

Go to the Smoke or Fumes Removal checklist on page 8.18, if needed

3.17 TAKE OFF CONFIGURATION

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3.18 WARNING HORN

1 If the intermittent warning horn sounds or a CABIN ALTITUDE light (if installed and

operative) illuminates in flight at an airplane flight altitude above 10,000 feet MSL:

Don the oxygen masks and set the regulators to 100%.

Establish crew communications.

Go to the CABIN ALTITUDE WARNING or Rapid Depressurization checklist

2 If the intermittent warning horn sounds or a TAKEOFF CONFIG light (if installed and

operative) illuminates on the ground when advancing the thrust levers to takeoff

thrust:

Assure correct airplane takeoff configuration.

3.19 WARNING LIGHTS ( CABIN ALTITUDE OR TAKE OFF CONFIGURATION)

1 If the intermittent warning horn sounds or a CABIN ALTITUDE light (if installed and

operative) illuminates in flight at an airplane flight altitude above 10,000 feet MSL:

Don the oxygen masks and set the regulators to 100%.

Establish crew communications.

Go to the CABIN ALTITUDE WARNING or Rapid Depressurization checklist

2 If the intermittent warning horn sounds or a TAKEOFF CONFIG light (if installed and

operative) illuminates on the ground when advancing the thrust levers to takeoff

thrust:

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