ab6 (beforedescent-parking) expand normal checklist

8/8/2019 AB6 (BeforeDescent-Parking) Expand Normal Checklist

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By chatvi AP45

AB6 EXPAND NORMAL CHECKLIST from Before Descent-Parking AIRCRAFT OPERATIONS MANUAL AOM 3.2/2 Page 10

***BEFORE DESCENT To be read by PNF ***

1.Air-conditioning .... NORMAL FLOW..PNF

See Overhead Co-pilot side

2. ECAM .............. CHECKED .................PNF – Check STATUS on MEMO page. Review if required.

Check they’re depressed

Check STATUS

Landing elevation + set Vapp on Stby ASI



By chatvi AP45

3. Landing elevation ............ SET..........PNF – Set landing field elevation on the window.

Front panel gear indicator

4. Landing weight & data .......................... CHECKED............ P – Check that landing weight will be within limits for actual landing runway and condition. – Check landing data for actual landing weight. – Set VAPP on standby ASI bug.

5. Loose objects ............ CHECKED.......... PChecklist completed

Predicted landing

weight

Set speed bug



By chatvi AP45

***APPROACH To be read by PNF***

1. Seatbelt sign ................ ON................. LP

600R 2. Trim tank ............. CHECKED...........PNF ****(600R)******

– If flight is performed not above FL200 , check fuel quantity in trim tank (ECAM FUEL page). If trim tank containsfuel more than 2000 kg, manually transfer the fuel forward by selecting TRIM TK MODE p/b to FWD position.

3. Bank limiter ............... SET.................. PF – Check that bank angle limiter is in NORM or as required.

fuel trim tank

fuel

Check FCU

At 20,000'Seatbelt sign on + rwy turn off+wing lt on



By chatvi AP45

4. Altimeters .............. __/__FT ................... P – Both pilots compare actual QNH with forecast value and set LH, RH and standby altimeters to actual QNH asapplicable at transition level. The change of altimeter setting from 1013.2 hPa to local QNH can be made at thetime a descent clearance is issued to altitude below transition level , provided that after the descent hascommenced, level flight above the transition level is not indicated or anticipated.

– Both pilots cross-check readings of the three altimeters for possible differences by calling out the mb settingand the indicated altitude.

– If local regulations issue altitude clearance based on meter, set meter altimeter to QNH/QFE.

Altitude tolerance limitation AOM Vol 1 chapter 13 instrument and recorders 2.13/3 p1

I2AON.Ip1SR3eT/rD3aRtAUoiTMnAEINTSSTRAUNMDERNETCSORDERS

1.1. AIR DATA INSTRUMENT TOLERANCE – ALTI 1 or ALTI 2 at ground check .......................... ft ± 30 – STBY ALTI at ground check .................................. ft ± 80

1.2. DIFFERENCE BETWEEN AIR DATAINSTRUMENT INDICATIONS

ALTI 1 and ALTI 2 – At ground check .................................................... ft 50 – FL 50/250 KIAS ..................................................... ft 55 – FL 100/250 KIAS ................................................... ft 65 – FL 200/300 KIAS ................................................... ft 90 – FL 300/M0.78 ± 0.02 ............................................. ft 135 – FL 400/M0.78 ± 0.02 ............................................. ft 170

STBY ALTI to any ALTI 1 or ALTI 2For HS-TAA to -TAF

– At ground check .................................................... ft 70 – FL 50/250 KIAS ..................................................... ft 100 – FL 100/250 KIAS ................................................... ft 140 – FL 200/300 KIAS ................................................... ft 210 – FL 300/M0.78 ± 0.02 ............................................. ft 275 – FL 400/M0.78 ± 0.02 ............................................. ft 330

Set Baro



By chatvi AP45

STBY ALTI to any ALTI 1 or ALTI 2For HS-TAG to -TAZ

– At ground check .................................................... ft 100 – FL 50/250 KIAS ..................................................... ft 125 – FL 100/250 KIAS ................................................... ft 170 – FL 200/300 KIAS ................................................... ft 250 – FL 300/M0.78 ± 0.02 ............................................. ft 310 – FL 400/M0.78 ± 0.02 ............................................. ft 390

NOTE: For aircraft with STBY ALTI vibration not supplied on ground (VIB flag displayed on ground), STBY ALTI tolerance at ground check is ±300 ft and STBY ALTI should not be compared to ALTI 1 or ALTI 2 at ground check.

5. External lights ............. SET................ LP

6. NAVAIDS ............ SET & CHECKED ....... P – Check that ADF, VOR/DME, ILS are tuned correctly to proper stations for landing RWY and airport. Availablenavaids should be used at every approach and landing irrespective of weather conditions, experience and knowledgeof the area and landing airport.

– Check that navaids readings correspond to the expected position in the approach to the runway . This isnecessary in order to maintain proper terrain clearance and to prevent landing on wrong runway or airport.

( FCU) ( centre pedestral)

Below 10,000

At 3000’Clear forapproach

Clear to Land

When Cleared for APPR from ATC,Turn On Nose Taxi and LDG Lt.



By chatvi AP45

7. Cabin crew ............. NOTIFIED............ LP – As soon as passing through 2500 ft RH, LP notifies cabin crew by switching SEAT BELT switch to OFF thenON.

Checklist to landing gear PF calls out "Gear down, complete checklist".

8. Gear ............. DOWN & CHECKED......... P

– Check the 3 green downlock lights on.

9. Ignition ....... OFF/CONT RELIGHT.....PNFGE GE – Set the ignition to CONT RELIGHT if heavy rain, icing conditions or heavy turbulence is expected duringapproach or go-around.

PW – Set the ignition to CONT RELIGHT

( Overhead Panel)

(PW)

(GE)

Check green

light

green light front panel

check overhead panel

"Autobrake low or med" +arm spoiler



By chatvi AP45

10.Spoilers ................ ARMED.................. LP

11.Anti/skid ............. CHECKED .............PNF – Check 8 brake release indications on ECAM system display.

12.Autobrake ............ OFF/LO/MED ............ P – Select autobrake mode on order by LP . – Normally, LO mode is recommended due to very high deceleration rate of MED mode.

Retract

Normally “LO”



By chatvi AP45

13.Landing clearance ....... RECEIVED....... PChecklist completed

After a go-around directly followed by an approach without flight above transition altitude

14.NAVAIDS .......... SET & CHECKED......... P15.Spoilers ............. DISARMED............... LPChecklist to landing gear

***AFTER LANDING To be read by RP***

1. Transponder & RADAR ........ SET ........RP – Set Transponder mode selector as required by localregulation.

– Set TCAS mode selector to STBY. – Set RADAR to OFF.

2. Ice protection ............ OFF/ON............RP – Engine anti-ice as required. – Set WING ANTI-ICE SUPPLY p/b switch to OFF.

Set Auto when mode S

required on ground TCAS to STBY

Set WXR to off

As Re uired

SET OFF

STROBE lt to AUTO+LDG Lt OFF +Nose Taxi lt+LDG lt extend off +

Disarm spoiler.



By chatvi AP45

3. Ignition ................... OFF .....................RP – Set ignition rotary selector to OFF.

4. External lights ............... SET.............. LP – Set STROBE light switch to AUTO. – Set all other external lights as required.

5. Spoilers ...... RETRACTED & DISARMED .................. LP – Push spoiler handle down to disarm position. – Confirm spoilers retraction from ECAM.

Strobe lightAUTO

Landing lightRETRACT+OFF

Nose to TAXI

Push to disarm

Check Spoiler

position 2



By chatvi AP45

6. Stabilizer .............. SET .......................RP – Set the stabilizer by using pitch trim switch to 1° NU .

7. Slats & Flaps ............ SET ...................RP – Retract the flaps to 0°. – For terminating stop, retract the slats .

8. APU ............ OFF/STARTED..................RP – Start APU as required.

Set to 1°up

Normally, retract

FLAP to 0Terminated,

retract SLAT to 0

12



By chatvi AP45

9. Brake temp & fan .......... __°/SET .........RP – Brake fan selection should be delayed for a minimum of about 5 minutes or just before stopping at the gate(whichever occurs first), to allow thermal equalization and stabilization and thus avoid oxidation of brake surface hotspots. However, when turnaround time is short, or brake temperatures are likely to exceed 500°C , use the brakefans disregarding possible oxidation phenomenon.

NOTE: The arc displayed on the ECAM WHEEL page, suggesting the selection of brake fans at taxi-out, should beignored at taxi-in. The ECAM BRAKE HOT warning after landing should not lead to the immediate selection of brake fans as long as 500°C is not likely to be reached; wait for 5 minutes after gate arrival.

Checklist completed

***PARKING To be read by RP ***

1. Parking brake ................ SET.............. LP

– Set parking brake and check brake pressure.

Bra e Fan ON; one o t ese con itions.

-5 mins after landing

- gate

-Short connection, short turnaround

-Approaching 500°C

LOCK

Check Brake

Pressure

Set

Before turning to parking bayturn off Rwy turn off lt + LDG lt off



By chatvi AP45

2. APU bleed ................ OFF/ON..............RP – Selecting APU bleed to on before shutting down the engines to avoids cycling of the packs.

3. FUEL levers ................. OFF ................ LP – Set both fuel levers to OFF and check engine parameters to decrease. – Record fuel used.NOTE: If APU is not available, shut down engine 1 first, wait until the external power is ready to supply to aircraft thenshut down engine 2.

4. Seatbelt sign ................ OFF............... LP

On, On

ENG

APU,

ENG1

EXT Pwr

ENG2



By chatvi AP45

5. Door slides ............ DISARMED ...........RP – Check SLIDE white indications are not displayed on ECAM.

6. Fuel pumps ................... OFF...............RP – Set all fuel pumps to OFF except L inner tank pump 2 if fuel remains in inner tank and APU is running. – Check TRIM TK MODE p/b at AUTO.

7. Beacon ................... OFF ..................... LP

Auto show on parkingor press it to show

On pump

APU running

fuel tank

Check auto(light out)



By chatvi AP45

8. Window & probe heat ......... OFF ........RP

(Over head panel Co-Pilot)

9. IRS...................... SET ............................ P – Check radial error rate according to AOM 2.15/9 as required. – Select IRS 1 to OFF ................................... LP – Select IRS 2 & 3 to OFF .............................RP

From AOM Vol1 2.15/9 p22 After Parking

1. PROG key………………………………………………………….PUSH2. Ramp position…………………………………………………..WRITE 3. LLSK opp present position…………………………………PUSH

- UPDATE* prompt appears on the same line key.4. RLSK opp UPDATE*…………………………………………..PUSH

- UPDATE* prompt disappears and the system is update to the ramp position.5. IRS 1/2/3 position from ISDU…………………………….WRITE 6. RLSK opp BRG/DIST……………………………………………PUSH

- Bearing and distance of IRS 1/2/3 to the ramp position is displayed (radial errors).

- Compute radial error rates (radial error per block hour in nm/hr) and compare the errors with theRADIAL ERROR CHART. If the rate exceeds 2.4 nm/hr, enter in A/C Log.

LP set OFF

RP set OFF



By chatvi AP45

10.External lights ................. SET ........... LP – Set external lights as required.

11.CRT’s. ....................... SET ..................... P – Set EFIS, FMS and ECAM CRTs to DIM. Select OFF if aircraft is not flying again within 2 hours.Note“EFIS SGU 3 fault" will come on ECAM if all EFIS CRT are selected off within 5 minutes after engines shutdown.

12.Wheels & brakes ....... CHOCKED & RELEASED...... LP – Check wheel chocks in place and release parking brake when N2 indications are close to zero.

13.Brake temp & fan ........ __°/OFF/ON .....RP – Check brake temperature on SYSTEM display:• If below 100°C with brake fan operating, select BRK FAN OFF.• If above 100°C, leave brake fan on.

– If time delay for next takeoff is 2 hrs or more, select BRK FAN OFF regardless of temperature.

When flight is terminated

14.Crew oxygen ............... OFF.................RP – Set crew oxygen LO PR SUPPLY p/b to OFF.

Check N2

close to 0

Release

Confirm

Chock ON



By chatvi AP45

15.Instrument lights ............ OFF............... P

16.APU ........................ OFF/ON ................RP – Set L INR TK PUMP 2 off if not require.

17.Emergency lights ........... DISARM.......RP

18.Batteries .................... SET..................RP – Set battery switches to OFF provided APU is shut down.

Checklist completed

Disarm light

SET OFF, then APU

will shut down

ab6 (beforedescent-parking) expand normal checklist

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