SOP Flashcards

Question

Brake

Answer 1

- Avoid excessive Manual Brake > 100kt it can result in Thermal Oxidation , disengage should be approaching 45kt - DECEL light appear when the actual deceleration 80% of selected rate - Brake temp limit 300c before T/O (150c with brake fan) ensure that in case hydraulic leakage will not ignited - during Taxi out if an arc is displayed on WHEEL SD page set ON BRAKE FAN - Brake Fan should not be used during T/O to avoid FOD to fans & brakes - Before 20kt DISENGAGE Auto Brake to avoid brake jerk at low speed - PF announces "MANUAL BRAKING" if pedal brake used PM announces "AUTOBRAKE OFF" if Autobrake disengages , no "MANUAL BRAKE" call out - for 321 "Spoiler Reverse Green Brake Low Decel" due to BRK LO on FMA - Autobrake Activated when wheel speed >40 kt & spoiler extension (wheel speed >72 kt) - If brake temp >500c (350c with brake fan) avoid apply parking brake unless necessary - brake fan using if brake temp >500c, 5min after L/D, approaching gate(vacate runway for neo) Use Brake Fan before Aircraft reach gate to prevent blowing carbon brake dust to ground person - PARK BRK handle OFF if brake hot -> prevent critical structures from being exposed to high temp

Answer 2

Reverser - If ground spoilers are not armed -> extend at reverser thrust selection - if no spoiler extend -> check thrust lever set to IDLE / set both thrust lever to MAX REV & fully press brake pedals - 70kt REV IDLE (unless required due to emergency) to prevent gases reentering the compressor by distortion of airflow cause engine stall result in excessive EGT - On snow the reverser should be stowed when aircraft speed reach 25kt Select REV IDLE on WET runways - FLD (1.15 LD) must be equal or less than full runway LDA regardless of autobrake & runway condition - landing distance has been made with -> MEDIUM TO POOR landing performance / no reverser credit

Answer 3

Choosing Auto Brake & Flap 1. For all landings FLD (1.15 LD) of the selected landing configuration must be equal or less than runway length 2. However to avoid unduly high autobrake (MED) , FLD may exceed LDA as long as all following satisfied - RWYCC 5,6 - Autobrake LOW LD < LDA - Manual brake FLD < LDA if(Flap 3 Autobrake LOW FLD <= LDA) use Flap 3 Autobrake OFF (Manual Brake only required <100kt) if(Flap 3 Autobrake LOW LD <= LDA) use Flap 3 Autobrake LOW (RWYCC 5,6/Manual Brake FLD

Answer 4

- First exterior inspections check WHEEL CHOCKS / LANDING GEAR DOOR / APU AREA - Dont pressurize hydraulic until ground clearance obtain - APU auto shutdown & discharge fire extinguisher if APU fire test > 3sec - when electric supplied by Battery, only right dome light is on - RESERVOIR FLUID LEVEL Check within normal range - OXY FCOM check when half amber box (<800) OXYGEN page Ref temp = (OAT + Cockpit Temp)/2 - ENG page oil quantity >=15qt or 9.5 + 0.5 qt/h (CEO), 8.9 + 0.45 qt/h (NEO&321) - never use rain repellent to wash windshield & on dry windshield - AIRCRAFT ACCEPTANCE must be complete at the end of Cockpit Preparation

Answer 5

- All White Light OFF except GEN FAULT LIGHT & maintenance panel - Dont transmit on HF during refueling operations - ถ้าไม่บิน RVSM , ATC SYS 1 only (only SYS 1 in emergency electric configuration) - Conservative used in wind variable FMGS set (ให้ใส่ tail wind ที่มากที่สุดเสมอ) THR RED / ACC ALT สามารถใส่ได้เลยนอกนั้น CM2 CALLOUT CM1 INSERT insert T/O shift value - Barometer maximum difference 20' both PFD / 100' ISIS & PFD / 300' Standby altimeter & PFD (75' diff กับ CHART) - LDG ELEV AUTO & STS & RCL check - Disconnect External power while EXT PWR ON may cause injury to engineer - WINDOWS & DOORS check red ring / cockpit door / ECAM DOOR page - CM1 amend LTS with LMC LMC 500kg

Answer 6

- if ECAM not display NW STRG DISC memo, but ground crew confirm tow pin in position dont start Engine during pushback to avoid damage to nose landing gear upon Y HYD pressurization - Dont use brake during pushback unless emergency - "Cabin Crew be seated for T/O" as soon as practical after receiving the cabin ready signal - After reset rudder trim flight crew may observe indication up to 0.3degree (L or R) - OETD maintain taxi in straight line during at least 5sec after EMG2 Master lever ON to ensure PTU auto test complete - OETD Yellow Electric pump ON providing nosewheel without using PTU - ENG IGN (T/O do only CEO) -> standing water runway / heavy rain / severe turbulence expected

Answer 7

- To counter the nose up effect of setting engine T/O Thrust, apply full forward sidestick until speed 80kt. Release sidestick gradually to reach 100kt - Wheel Speed 130kt connection between nosewheel steering & rudder pedal is removed - initiate the rotation with rate 3degree/sec to pitch altitude 15degree (12.5degree 1 Engine fail) - if tailstrike occurs avoid flying at an altitude requiring a pressurized cabin and return to origin airport for damage assessment - "positive climb" when V/S is positive & radio altimeter has increased - selecting pack on before reducing T/O thrust would result in an EGT increase - When Climbing <10000' AAL(OM เขียน MSL) pilot may accelerate to ECON CLB Speed above MSA - MAX REC FL give the aircraft 0.3g buffet (may enter FL above provided that it does not exceed 0.2g buffet otherwise "CRZ ABOVE MAX FL") - Enter new wind & temp each WPT where wind differs by >30degree , 10kt , temp 3degree - if GPS PRIMARY LOST & ACCURACY LOW check accuracy (position error <= 3nm is reliable) , if not reliable -> raw data

Answer 8

- Speed limit 250kt must not be exceeded below 5000' AAL - LDG ELEV AUTO check - If NAV ACCURACY LOW dont use TERR ON ND - no call out is required if GPS PRIMARY is available - EARLY STABILIZED APPROACH enter VAPP at FDP (selected guidance, high glide path, low alt IF) - when aircraft below FCU alt , flight crew must apply GO AROUND (cant discontinued approach) - On WET runways with RWYCC not reported , landing performance MEDIUM - On WET runways in heavy rain with RWYCC not reported , landing performance MEDIUM TO POOR - At least 1 triangle on each landing gear strut on WHEEL page is sufficient to indicate that gear is lockdown - if residual pressure indicated on triple indicator -> RESIDUAL BRAKING PROC on QRH (แค่ CEO) - 15nm from touchdown activated APPR phase if not in NAV mode - FLAPS 1 should be selected more than 3nm before FDP - GS 10nm +/- 8degree from centerline & 1.75nominal angle above 0.3nominal angle below - Decelerate Approach FLAPS 1 & S speed >= 2000' on final descent Flap 2 at 1 dot below flight path - for FINAL APP 1nm before FDP FPA Set , 0.3nm FPA Pull - for FINAL APP at minimum -50' if AP engage "DISCONNECT AP FOR LDG" will remind that Autoland is not available - เครื่องเก่าๆติด AP ทำ one Engine NPA "FINAL APP" ไม่ได้ ใช้ได้แต่ FD - RNAV with LNAV/VNAV cannot NAV FPA , TRK FPA RNAV with LNAV can NAV FPA (cross-reference table)

Answer 9

- To minimize flaps wear , extend flaps at VFE NEXT -15kt , Recommend Gear extension VLO -10kt - Ground Spoiler extension inhibit if thrust lever remain above IDLE detent - CHRONO should be started once the aircraft has touched down if REV MAX using CHRONO should be started when REV IDLE - 350' Autoland "LAND MODE" if ILS course pointer & runway track diff >5degree perform go around or visual landing - 10' Autoland "RETARD" callout trigger - DECEL callout confirmed by the speed trend on the PFD - OAT > 30celcius , no refuelling is required -> keeping CONF1 to prevent AIR WING LEAK on hot weather condition - In case ACCU PRESS not in green band, chock are required before Engine 1 shutdown - operate the engines idle for cooling period of 3min before shutdown in order to thermally stabilize - for NIGHT operation a pair of lighted torch is MANDATORY - Turn off beacon light when all ENG spooled down N1<10% - after shutdown ADIRS wait 10sec before shutdown electric to ensure ADIRS memorize recent data - before BATT OFF wait until APU flap fully close (2min after APU AVAIL light out) ETC

Answer 10

- First T/O of the day crew should carry out full Emergency briefing to cover a reject T/O For a subsequent flight on the same day with the same crew "Standard Reject Briefing" - Sterile Cockpit when aircraft <10000' AAL - Preliminary & Securing Checklist are READ & DO procedure carried out by CM2 - both TERR ON ND when operating in mountainous area <10000' AAL,MSA / PF should deselect if Weather Radar required (แต่ใน procedure เขียนว่า radar on PF / TERR ON ND on PM) - The PF will have 1 hand on the Thrust lever form a minimum of 1500' AAL - if Aircraft below profile V/S -1000' - to avoid TCAS RA on last 2000' climb or descent limit V/S to 1500' especially in busy airspace - transfer duty read FMA + FL "you have control" - Minimum Pavement for 180degree turn 30m for A320 / 32m for A321 - get ground crew clearance before using the electric pump - 320 Gear Not Compress / Compress -> 13.7 / 11.7 321 Gear Not Compress / Compress -> 11.2 / 9.7

Answer 11

- In case electrical power supply interrupt during start sequence (loss of ECAM DU) abort start then perform 30sec dry crank (FADEC limit N2 to 30%) - Parameter call out is not mandatory - The Engine may not start at first attempt flight crew should not abort the start while FADEC automatically manage a second attempt - After Start to avoid thermal shock pilot should operate engine at idle 2min (3min for neo,321) (5min if OAT -29c) before advancing thrust lever to high power - fuel leak from engine drain mast -> idle 5 min ,if leak still present -> shutdown & maintenance - PTU Fault is trigger if last engine start within 40sec following the end of cargo doors operation

SOP Flashcards

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