• Author / Uploaded
• vasilisnikon

Citation preview

A318/A319/A320 NORMAL CHECKLIST BEFORE START

APPROACH (BELOW FL 180)

Log Book/Security Check. . . . . . . . . Checked/Entered Departure Brief . . . . . . . . . . . . . . . . . . . . . . Completed Cockpit Prep . . . . . . . . . . . . . . . . . . . . . . . . Completed Cabin Signs . . . . . . . . . . . . . . . . . . . .On, Auto & Armed ADIRS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Nav Fuel . . . . . . . . . . . . . . . Rlsd With __ , __ Lbs On Board Baro Ref. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___Set Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On

(CR) (CR) (CR) (C) (C) (C) (CR) (C)

Takeoff Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set Beacon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On NW Strg Disc . . . . . . . . . . . . . . . . . . . . . . . . . . Checked Windows, Doors & Slides . . . . . . . . . . Closed & Armed Cockpit Door . . . . . . . . . . . . . . . . . . . Closed & Locked

(CR) (C) (C) (CR) (F)

AFTER START Anti-ice. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On / Off Pitch Trim. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___Set Rudder Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Zero ECAM Status (two-engine start only) . . . . . . . Checked Yellow Electric Pump . . . . . . . . . . . . . . . . . . . . . . . On Engine 2 Generator . . . . . . . . . . . . . . . . . . . . . . . . Off

(C) (CR) (F) (CR) (F) (F)

SECOND ENGINE START Yellow Electric Pump . . . . . . . . . . . . . . . . . . . . . . . Off Engine 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Start Anti-ice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On / Off Challenge . . . . . . . . . “Off the Steering and Brakes” Engine 2 Generator . . . . . . . . . . . . . . . . . . . . . . . . On APU Bleed/APU Master. . . . . . . . . . . . . . . . . . On/Off ECAM Status. . . . . . . . . . . . . . . . . . . . . . . . . Checked

(F) (F) (F) (F) (F) (F) (CR)

BEFORE TAKEOFF Takeoff Brief . . . . . . . . . . . . . . . . . . . . . . . . Completed Flight Controls . . . . . . . . . . . . . . . . . . . . . . . . . Checked Flight Instruments . . . . . . . . . . . . . . . . . . . . . Checked Flaps . . . . . . . . . . . . . . . . . . . . . . . ___Planned ___Set ECAM Memo . . . . . . . . . . . . . . . . . . . . . . . T.O. No Blue

(CR) (CR) (CR) (CR) (CR)

Cabin Signal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Given TCAS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TA/RA Packs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off

(F) (F) (F)

AFTER TAKEOFF (SILENT) Ldg Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Up Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Retracted Packs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On ECAM Memo . . . . . . . . . . . . . . . . . . . . . . . . . . Checked

(CR) (CR) (CR) (PNF) (PNF)

LANDING Cabin Signal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Given A/Thr . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Speed / Off Landing Gear . . . . . . . . . . . . . . . Down & Three Green ECAM Memo . . . . . . . . . . . . . . . . . . . . . . . .Ldg No Blue

(PNF) (PF) (CR) (CR)

AFTER LANDING (SILENT) Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Retracted Landing Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Spoilers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Disarmed Radar & Predictive W/S. . . . . . . . . . . . . . . . . . . . . . Off TCAS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Stby APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On / Off

(F) (F) (F) (F) (F) (F)

SINGLE ENGINE TAXI IN APU (if required at gate) . . . . . . . . . . . . . . . . . . . Start (F) Ensure APU AVAIL light on prior to shutting down #2 engine. Yellow Electric Pump. . . . . . . . . . . . . . . . . . . . . . . . On (F) Challenge . . . . . . . . . “Off the Steering and Brakes” (F) Engine 2 Master . . . . . . . . . . . . . . . . . . . . . . . . . . .Off (F) SINGLE ENGINE APU START If the APU is required after Engine 2 is shutdown APU Generator . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Off (F) APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Start (F) When APU AVAIL light is illuminated: Challenge . . . . . . . . . “Off the Steering and Brakes” (F) APU Generator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On (F)

PARKING Park Brk & Chocks . . . . . . . . . . . . . . . . . . . . . . .On & In Engine(s). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Beacon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Seat Belt Signs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Emerg Exit Lights . . . . . . . . . . . . . . . . . . . . . Armed/Off Yellow Electric Pump . . . . . . . . . . . . . . . . . . . . . . . . Off Fuel Pumps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off

(C) (C) (C) (C) (C) (C) (C)

SECURING (PNF) (PNF) (PNF) (PNF)

NOTE: Checklist items presented in BOLD type represent Single Engine Taxi procedures and are “Read and Do” items.

676011 Rev. 12

Approach Brief . . . . . . . . . . . . . . . . . . . . . . . Completed ECAM Status. . . . . . . . . . . . . . . . . . . . . . . . . . .Checked Baro & MDA/DH . . . . . . . . . . . . . . . . . . . . . . . . .___ Set Seat Belt Signs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On Autobrake . . . . . . . . . . . . . . . . . . . . . . Low / Med / Off

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADIRS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Oxygen . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Exterior Lights. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cabin Signs & Emerg Exit Lights . . . . . . . . . . . . . . . APU & BAT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

On Off Off Off Off Off

(F/C) (F/C) (F/C) (F/C) (F/C) (F/C)

FAA Approved 04/17/06

A318/A319/A320 SUPPLEMENTAL CHECKLIST Refer to FOM Volume II, Chapter 5.10 for expanded information. NOTE: In the following procedures, the F/O should read and the captain should execute the actions.

MANUAL ENGINE START Thr Levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Idle Eng Mode Selector . . . . . . . . . . . . . . . . . . . . . . . Norm then Ign Eng Man Start . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .On When N2 reaches max motoring speed (min 20%) Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .On ECAM Displays . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check When N2 reaches 50% ECAM Displays . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check Eng Idle Parameters . . . . . . . . . . . . . . . . . . . . . . Check Normal Man Start . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Eng Mode Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Norm In the event of a start malfunction Man Start (affected) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Eng Master (affected). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off – Mode Sel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Crank – Man Start (affected) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .On

Crossbleed Engine Start Adjust thrust of supplying engine to obtain 30 PSI at start valve prior to (and at least 25 PSI during) crossbleed start. If Starting Prior to Taxi Before Start Checklist . . . . . . . . . . . . . . . . . . . . . . . . Complete APU Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Eng Bleed (running engine) . . . . . . . . . . . . . . . . . . . . . . . . . . On Eng Bleed (receiving engine). . . . . . . . . . . . . . . . . . . . . . . . . Off X Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Open If Starting After Single Engine Taxi: Yellow Electric Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off APU Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Eng Bleed (running engine) . . . . . . . . . . . . . . . . . . . . . . . . . . On Eng Bleed (receiving engine). . . . . . . . . . . . . . . . . . . . . . . . . Off X Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Open After start Thrust Lever (supplying engine) . . . . . . . . . . . . . . . . . . . . . Idle X Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Auto Eng Bleed (receiving engine). . . . . . . . . . . . . . . . . . . . . . . . . On Packs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check On After Start Checklist. . . . . . . . . . . . . . . . . . . . . . . . .Accomplish

Crosswind Component

NOTE: The last two lines are not displayed on the ECAM. Dry crank the engine for 30 seconds. The start valve automatically reopens when N2 is below 20%. The pilot must decide whether to attempt a new start, or to report the no start condition for appropriate maintenance action.

Start Valve Manual Operation Audio Control Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cab When ground crew member is ready, order “START 1(2)” Eng Mode Sel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ign Eng Master . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .On Start Valve . . . . . . . . . . . . . . . . . Order “Open and Keep Open” When N2 at 50% Start Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Order “Close”

Engine Start w/Ext Pneumatic Power Before connecting external pneumatic power Packs 1 and 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Before start APU Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Eng Bleed (both engines) . . . . . . . . . . . . . . . . . . . . . . . . . . . Off X Bleed (if starting engine 2) . . . . . . . . . . . . . . . . . . . . . . Open Cleared to start Brake Accum Press. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check Engine 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Start Normal Engine Start Procedures . . . . . . . . . . . . . . . . . . . Apply NOTE: Consider using manual engine start procedure in case of low air pressure. See FOM II, Chapter 5.10. After Engine 1 (2) is started External Power . . . . . . . . . . . . . . . . . . . . . . . . . . .Off/Removed Packs 1 and 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .On Eng Bleed (running engine) . . . . . . . . . . . . . . . . . . . . . . . . . .On

676011 Rev. 12

Enter the graph by following the “Wind Direction Relative to Runway” radial line until it intersects the windspeed. From the point of intersection, determine the headwind/tailwind component by moving horizontally to the left, and the crosswind component by moving vertically down.

FAA Approved 04/17/06

A318/A319/A320 LANDING DATA

Per

Runway Condition

A318 LANDING DISTANCE (WITHOUT AUTOBRAKE) – CONF FULL (FEET) WEIGHT (1000 LB) Dry Wet 1/4 in Water 1/2 in Water 1/4 in Slush 1/2 in Slush Compact Snow Ice

80 2180 2820 3870 3700 3780 3640 3750 7860

90 2180 2850 3950 3790 3850 3720 3790 7940

100 2170 2860 4010 3860 3920 3790 3830 8040

110 2260 3040 4290 4120 4180 4050 4050 8410

120 2370 3260 4640 4450 4490 4340 4300 8860

130 2480 3480 5010 4790 4780 4620 4540 9280

140 2620 3710 5400 5150 5110 4930 4800 9760

A318 CORRECTIONS ON ACTUAL LANDING DISTANCE – CONF FULL 1/4 in 1/2 in 1/4 in 1/2 in Compact Rwy Condition Dry Wet Water Water Slush Slush Snow 1000 ft above SL + 3% + 3% + 4% + 3% + 4% + 4% + 3% 10 kt headwind No correction for headwind due to wind correction on approach speed 10 kt tailwind + 19% + 23% + 25% + 23% + 23% + 21% + 19% 5 kt speed increment (and no failure) add 8% (all runways)

150 2810 3950 5800 5510 5480 5280 5060 10230

Ice + 3% + 38%

Runway Condition

A319 LANDING DISTANCE (WITHOUT AUTOBRAKE) – CONF FULL (FEET) WEIGHT (1000 LB) Dry Wet 1/4 in Water 1/2 in Water 1/4 in Slush 1/2 in Slush Compact Snow Ice

Rwy Condition

Per

1000 ft above SL 10 kt headwind 10 kt tailwind

90 2280 2980 4040 3870 3950 3800 3890 8200

100 2270 2990 4110 3940 4010 3870 3920 8290

110 2330 3140 4330 4150 4230 4080 4090 8610

120 2440 3360 4670 4470 4520 4360 4330 9030

130 2540 3540 5000 4770 4770 4600 4530 9380

140 2650 3750 5330 5080 5040 4860 4740 9770

150 2800 3990 5730 5440 5400 5190 4990 10240

160 3110 4240 6130 5780 5780 5550 5240 10730

CORRECTIONS ON ACTUAL LANDING DISTANCE – CONF FULL 1/4 in 1/2 in 1/4 in 1/2 in Compact Dry Wet Water Water Slush Slush Snow + 3% + 3% + 4% + 4% + 5% + 4% + 3% No correction for headwind due to wind correction on approach speed + 20% + 23% + 25% + 23% + 24% + 21% + 19% Per 5 kt speed increment (and no failure) add 8% (all runways)

170 3380 4410 6390 6060 6030 5780 5380 11010

Ice + 3% + 35%

Runway Condition

A320 LANDING DISTANCE (WITHOUT AUTOBRAKE) – CONF FULL (FEET) WEIGHT (1000 LB) Dry Wet 1/4 in Water 1/2 in Water 1/4 in Slush 1/2 in Slush Compact Snow Ice

Per

Rwy Condition 1000 ft above SL 10 kt headwind 10 kt tailwind

676011 Rev. 12

100 TBD TBD TBD TBD TBD TBD TBD TBD

110 TBD TBD TBD TBD TBD TBD TBD TBD

120 TBD TBD TBD TBD TBD TBD TBD TBD

130 TBD TBD TBD TBD TBD TBD TBD TBD

140 TBD TBD TBD TBD TBD TBD TBD TBD

150 TBD TBD TBD TBD TBD TBD TBD TBD

160 TBD TBD TBD TBD TBD TBD TBD TBD

170 TBD TBD TBD TBD TBD TBD TBD TBD

CORRECTIONS ON ACTUAL LANDING DISTANCE – CONF FULL 1/4 in 1/2 in 1/4 in 1/2 in Compact Dry Wet Water Water Slush Slush Snow TBD TBD TBD TBD TBD TBD TBD No correction for headwind due to wind correction on approach speed TBD TBD TBD TBD TBD TBD TBD Per 5 kt speed increment (and no failure) TBD

180 TBD TBD TBD TBD TBD TBD TBD TBD

Ice TBD TBD

°C

°F

-40 -39 -38 -37 -36 -35 -34 -33 -32 -31 -30 -29 -28 -27 -26 -25 -24 -23 -22 -21 -25 -20 -19 -18 -17 -16 -15 -14 -13 -12 -11 -10 -9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49

-40 -38 -36 -35 -33 -31 -29 -27 -26 -24 -22 -20 -18 -17 -15 -13 -11 -9 -8 -6 -13 -4 -2 0 1 3 5 7 9 10 12 14 16 18 19 21 23 25 27 28 30 32 34 36 37 39 41 43 45 46 48 50 52 54 55 57 59 61 63 64 66 68 70 72 73 75 77 79 81 82 84 86 88 90 91 93 95 97 99 100 102 104 106 108 109 111 113 115 117 118 120

FAA Approved 04/17/06

A318/A319/A320 EMERGENCY QUICK REFERENCE CHECKLIST ENGINE TAILPIPE FIRE CAUTION External fire agents can cause severe corrosive damage and therefore should only be considered after having applied the following procedure. – MAN START . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – ENG MASTER (affected). . . . . . . . . . . . . . . . . . . . . . . . . .OFF – AIR BLEED PRESS . . . . . . . . . . . . . . . . . . . . . . . . ESTABLISH – ENG MODE SEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CRANK – MAN START . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON • When burning stopped: – MAN START . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – ENG MODE SEL . . . . . . . . . . . . . . . . . . . . . . . . . . . .NORM End of Procedure

SMOKE/FUMES IF PERCEPTIBLE SMOKE APPLY IMMEDIATELY: – OXYGEN MASKS. . . . . . . . . . . . . . . . ON / 100% / EMERG – CREW COMMUNICATION . . . . . . . . . . . . . . . . .ESTABLISH – LAND ASAP – CAB FANS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – BLOWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OVRD – EXTRACT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OVRD – GALLEY & CAB . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – CABIN SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON – CABIN COMMUNICATION . . . . . . . . . . . . . . . . . . . ESTABLISH – FAULT EQUIP (if identified). . . . . . . . . . . . . . . . . . . . ISOLATE IF DENSE SMOKE, at any time of the procedure: – EMER EXIT LIGHTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON – SMOKE/TOXIC FUMES REMOVAL . . . . . . . . . . . . . . . . APPLY – EMER ELEC CONFIG. . . . . . . . . . . . . . . . . . . . . . . CONSIDER Refer to FOM Volume II, Chapter 4.10

UNRELIABLE SPEED INDICATION Unreliable speed indication may be caused by radome destruction or frozen pitots. CAUTION If the failure is due to radome destruction, the drag will increase and therefore N1 must be increased 5%. Fuel flow will increase by about 27%. – CROSSCHECK INSTRUMENTS • If unable to establish reliable source, perform the following action items: – THRUST/PITCH – Below THR RED ALT . . . . . . . . . . . . . . . . . . . . 15°/TOGA – Above THR RED ALT and Below FL 100 . . . . . . . . 10°/CL – Above THR RED ALT and Above FL 100 . . . . . . . . . 5°/CL – AP/FD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – FLAPS . . . . . . . . . . . . . . . . . . . MAINTAIN CURRENT CONFIG – SPEEDBRAKES. . . . . . . . . . . . . . . . . . . . . . CHECK RETRACT If failure is detected while in CONF FULL and go-around is initiated, select CONF 3. – LANDING GEAR . . . . . . . . . . . . . . . . . UP WHEN AIRBORNE Refer to FOM Volume II, Chapter 4.10

ENGINE FAIL AT CRUISE STRATEGY – – – – – –

ECAM ACTIONS / MCT (Simultaneously) . . . . . INITIATE / SET AUTOTHRUST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF CRUISE FL (PROG Page) . . . . . . . . . . . . . . . . . . DETERMINE ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTIFY SPEED ON FCU . . . . . M.78, 300 KT / GREEN DOT – PULL ALTITUDE ON FCU . . . . . . . . . . . . CRUISE FL – SET & PULL Refer to FOM II, Chapter 9 – Additional Procedural Techniques

EMERGENCY DESCENT – OXYGEN MASKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON – CREW COMMUNICATION . . . . . . . . . . . . . . . . . ESTABLISH NOTE: Set the oxygen diluter selector to the N position. With the oxygen diluter selector left at 100%, oxygen quantity may be insufficient to cover the entire emergency descent profile. The recommendation is to descend with the AP engaged: – Turn the ALT selector knob and pull. – Turn the HDG selector knob and pull. – Adjust the target SPD/MACH. – Use of the autopilot is also permitted in EXPEDITE mode. – THRUST LEVERS (If A/THR not engaged). . . . . . . . . . . IDLE – SPD BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL – Extension of the speedbrakes will significantly increase VLS. – In order to avoid AP disconnection and automatic retraction of speedbrakes due to possible activation of angle of attack protection, allow the speed to increase before starting to use speedbrakes – SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . MAX APPROPRIATE Refer to FOM Volume II, Chapter 4.10

LOSS OF BRAKING • IF AUTOBRAKE IS SELECTED: – BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . . . . .PRESS • IF NO BRAKING AVAILABLE: – REV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .MAX – BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . .RELEASE – A /SKID & NW STRG . . . . . . . . . . . . . . . . . . . . . . . . . OFF – BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS – MAX BRAKE PRESS . . . . . . . . . . . . . . . . . . . . . 1000 PSI • IF STILL NO BRAKING: – PARKING BRAKE . . . . . . . . . . SHORT AND SUCCESSIVE APPLICATIONS End of Procedure

ON GROUND EMERGENCY / EVACUATION – AIRCRAFT / PARKING BRK . . . . . . . . . . . . . . . . . STOP / ON – ATC (VHF) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTIFY – P . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK ZERO If not zero, MODE SEL on MAN, V/S CTL FULL UP. – ENGINE MASTER 1 AND 2 . . . . . . . . . . . . . . . . . . . . . . . OFF – NOTIFY CABIN CREW . . . . . . . . . . . . (PA) “REMAIN SEATED” – FIRE P/Bs (ENG and APU). . . . . . . . . . . . . . . . . . . . . . PUSH – AGENTS (ENG and APU) . . . . . . . . . . . . . . . . . . . . .AS RQRD – EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE End of Procedure

NOTE: Shaded checklist items (presented in BOLD ITALIC type) represent memory items. These should be accomplished from memory prior to consulting this Emergency QRC.

676011 Rev. 12

FAA Approved 04/17/06