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จำ Flashcards

1
Q

Brake temp condition that require maintenance action

A
  • temp different between 2 brakes of a gear >150celcuis & 1 brake >=600c
  • temp different between 2 brakes of a gear >150celcuis & 1 brake <=60c
  • Different average temp between 2 gear brakes >= 200c
  • temp of 1 brake exceeds 900c (800celcuis for 321)
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2
Q

Emergency Equipment

A
  • Life vest หลังเก้าอี้ / ใต้ Jump Seat
  • Axe ข้าง Jump Seat
  • Oxygen mask ขวาหลัง FO เช็ค pressure
  • PBE / Smoke hood ด้านขวาหลัง FO / humanity indicator not pink
  • BCF / Fire extinguisher ใต้ oxygen mask / Pressure Gauge needle in green zone
  • Flash light ใต้ไมค์ red light flash every 3-7sec
  • Rope บนหัว
  • Fireproof Glove 2 อัน ข้าง Jump Seat
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3
Q

Thrust Reduction , Acceleration Altitude , NADP

A

follow NADP & SID first then
400’/400’/ENG OUT ACC เสมอ
***Engine fail -> TOGA to gain SRS Go-around (because below EOACC altitude)
on course track >75degree from runway track & reach specific Altitude before turn
use Greendot Speed until turn 45 from track Opticlimb , 250 below MSA
EOACC Alt default 800’ AAL / Miss Approach ACC Alt default 1500’ AAL

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4
Q

Pack

A
  • OAT < 20celcius / APU Bleed OFF , Pack OFF
    20celcius <= Cabin Temp <= 26celcius / APU Bleed ON , 1 PACK ON
    26celcius < Cabin Temp / APU Bleed ON , 2 PACK ON
  • OAT <20c , Cabin temp >=24c APU Bleed ON , 1 PACK ON
  • LO when number of occupants below 141 (320) , 168 (321)
    HI when abnormal hot & humid conditions
  • range temp 24 +/- 6celcius
  • should switch Pack on each flight to prevent excessive wear of 1 pack
  • during OETD OETA pack 2 should be OFF
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5
Q

Green dot Speed

A
  • type 320 = 2*GW/1000 + 85
  • type 321 = 1.5*GW/1000 + 110
  • Green dot speed by Fly smart & FMGS difference of 2kt or more indicate discrepancy exists
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6
Q

Taxi Speed

A

Taxi Speed Dry/Wet/Contaminated
- Taxi Speed 30/20/10
- Vacate Runway , Backtrack 45/20/10
- 90degree Turn 15/10/5

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7
Q

Choosing Auto Brake & Flap

A

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<LDA)
if(Flap 3 Autobrake MED FLD <= LDA) use Flap 3 Autobrake MED
if(Flap Full Autobrake MED FLD <= LDA) use Flap Full Autobrake MED
if(Flap Full Manual Brake FLD <= LDA) use Flap Full Autobrake MED(Maximum Brake after touchdown)
else Landing Not Permit
The Company recommends using CONF 3 REV IDLE for all normal landings
- For all landings FLD (1.15 LD) of the selected landing configuration must be equal or less than full runway landing distance available
- LD < LDA
- Tailwind <= 10kt CEO , <= 15kt NEO
- Runway not contaminated

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8
Q

Company Standard EOP

A

Climb runway centerline to EOACC retract flap/slat turn L/R to lowest MSA follow ATC

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9
Q

Stabilized Approach

A

1000’AAL (500’AAL Visual , Circling)
1. correct lateral/vertical flight path
2. only small change in heading/pitch
3. correct landing configuration with Speed Brake retract & spoiler armed
4. thrust appropriate to maintain VAPP
(with A/THR thrust idle is acceptable but Engine spool up must be achieved by 500’AAL)
5. all briefing & applicable checklist complete
6. Speed not more than VAPP “bug” speed + 15kt and not less than VLS
7. Sink rate no greater than 1000ft/min or special briefing shall be conducted
8. not detect any excessive flight parameter deviation
- ILS -> 1 dot LOC/GS
- RNP -> XTK < 0.3nm / VDEV below path 3/4dot
- NPA -> less than 5degree deviation
- Visual -> align runway in 500’AAL
- Circling -> align runway in 300’AAL
*“Destable” after 1000’AAL “Stabilize” thereafter if external condition push aircraft beyond the stabilized parameter , the approach shall be re-stabilized at latest 500’AAL (without config change)
**Landing flaps selection should be initiated by 1,500’AAL for instruments approach , Crew may change landing flap to full & complete landing checklist by 1000’AAL

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10
Q

Runway Visual Reference “See to Land”

A
  • Element of Approach light
  • Threshold
  • Threshold marking
  • Threshold light
  • TDZ , TDZ marking
  • TDZ light
  • Runway edge light
  • Runway end(Threshold) identification light
  • Visual glide slope indicator
  • Other visual reference accepted by the authority
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11
Q

นักบินน้อย ชม

A
  • นักบิน ชม <=200hr บินด้วยกันไม่ได้
  • กับตัน ชม <=100hr ห้าม LVO
  • กัปตัน ชม <=200hr ต้อง RVR +100m / Circling +200’ , 800’ which is higher
  • กับตัน ชม <=250hr และยังไม่ LANDEE check ห้ามให้ FO แลน
  • กับตัน ชม <=250hr ห้ามบิน CAT C aerodrome
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12
Q

FO T/O L/D limitation

A

F/O T/O Ceiling/Visibility more than 200’/600m
F/O L/D Ceiling/Vis Straight in app with 500’/1600m
F/O L/D Ceiling/Vis Circling app with 800’/4800m
X-wind not exceed 20kt gust include
Runway is not Contaminated , Slippery
Aerodrome not CAT C

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13
Q

OMA 8.1.2 Criteria for determining the Usability of Aerodromes

A
  • RFF 320 required 6 minimum 5 / 321 required 7 minimum 6 / Adequate alternate 4
  • Takeoff Alternate required when Departure Aerodrome minima < Landing minima
  • only Departure / Destination minima ที่ไม่ต้องคิดบวกอากาศ 1 ขั้น
  • Planning minima for Non precision APP apply +200’/1000m
  • Destination Alternate Aerodrome within 50nm apply ceiling/visibility -> 2000’/5000m
  • 2 Destination Alternate require when destination aerodrome < planning minima / no meteorological information
  • Emergency Airport = Airport not adequate aerodrome , not list in OMC , use only in dire emergency
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14
Q

OMA 8.1.7 Determination of the Quantities of Fuel and Oil to be Carried

A
  • Contingency fuel เอาค่ามากระหว่าง
    5% trip fuel
    5min holding Speed 1500’AAL at Destination ISA
  • Contingency fuel ใช้ได้ทันทีหลังถอด fuel browser
  • Alternate fuel คิดตั้งแต่ a Miss APP / CI = 0
  • Final reserve คิด 30 min holding Speed 1500’ at Destination Alternate ISA
  • Additional Fuel เช่น ETOP fuel , Company Fuel
  • No Economic Tankering fuel in Contaminated Runway
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15
Q

OMA 8.2.1 Fuelling Procedure

A
  • A screen capture of fuel order is presented to engineer each time refueling to be made
  • Refueling when Embark/Disembark required at least 1 Cockpit Crew / half of Cabin Crew
  • D2R D4R not be Armed unless Emergency & Crew remain
  • Defueling / Mix fueling when passenger on board , embark , disembark is strictly prohibit
  • Refueling with 1 Engine running is only permitted at airports with no pneumatic & no APU
  • in exceptional circumstances other fuels in AFM maybe uplifted when JETA1 is not available
  • Jet B -> wide-cut fuel (naphtha-kerosene/kerosene30% , gasoline70% / low freezing point)
  • MOC authorize required for fuel mixing other than JETA & JETA1
  • Freezing point of mixture with JETA more than 10% is considered as JETA
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16
Q

In-flight Fuel Management

A
  • ประหยัดน้ำมัน ลด CI / optimum Alt / closet Alternate / ขอ Direct
  • Continue without alternate fuel -> 1hr before Destination / establish VHF / Estimate Arrival Time , Max delay known / 2 independent runways & suitable for landing / ceiling 1500’ visibility 5000m / Final reserve 30min
  • “Minimum Fuel” -> committed to land at specific aerodrome & any change in the existing clearance may result in landing with less than planned final reserve fuel (EFOB=final reserve)
  • “Maydayx3 Fuel” -> calculated fuel on landing at nearest aerodrome landing will be less than planned final reserve fuel (EFOB<final reserve)
  • flight crew responsibility to ensure that the fuel remaining at touchdown is not less than planned final reserve
17
Q

PAN PAN MAYDAY

A
  • MAYCAY call -> Aircraft or its occupants are in grave and imminent requiring immediate assistance
  • PAN PAN call -> compel it to land without requiring immediate assistance
18
Q

OMA 14 Crew Regulations

A
  • Documentation Validity not later than 7days before expiry & update along with Staff number
  • Logbook are mandatory & record particulars of each flight within 24hr after the end of the flight
  • must be available to be contacted by OCC 12hr prior to reporting time
  • Passport must notify 24hr before report time
  • Tolerances of 5min only will be allowed on the reporting time
  • Cabin crew avoid entering cockpit until 10min after SIGN OFF & SIGN ON twice consecutively 15min before L/D
  • entering bar , liquor store while wearing any part of uniform is strictly prohibited
  • Non-uniform items of clothing must not be visible when worn with uniform
    Visible Piercing & Tattoo are not allowed
    wearing sunglasses is not permitted in the cabin while greeting & bidding farewell
    Backpack , Sling bag is not allowed
    other jacket , Pilot Bag must be black
19
Q

Code วันลา

A
  • CL = Casual Sick Leave without certified by doctor but Verified by Flight Ops -> must report to OCC minimum period 3hr from reporting time
  • submit medical leave into eMC within 48hr even doesn’t have MC (medical certification) -> CSL
  • X = no certified by doctor / 1 = verified by Flight Operation / L = late (Report <3hr)
  • AWOL(Absence without Approved Leave) = CSL no certified by doctor & no Verified by Flight Op
  • MIA (Missing in action) = ติดต่อไม่ได้ ไม่ไปบินตาม schedule (ใส่เหตุผลได้)
  • EL = ขอ AL ในกรณีที่ roster ออกมาแล้ว
    CLVE = ลามีคนในครอบครัวตาย ครั้งละไม่เกิน 3 วัน
    BL คือการลาไปทำธุระสำคัญที่คนอื่นไปทำแทนไม่ได้ และต้องได้รับอนุญาตก่อนถึงนับว่าเป็นการลา
    รวมกันไม่เกิน 5 วัน
20
Q

Memory Item Speed

A

V1 > Vef , Vmcg
VR >= 1.05Vmca , V1
Vlof >= 1.05Vmu(n-1) , 1.08Vmu(n)
V2 >= 1.1Vmca , 1.13Vs1g
Approach climb gradient speed >= 1.23Vs1g , VMCL / <= 1.41Vs1g
Landing climb gradient speed >= 1.13Vs1g , VMCL / <= 1.23Vs1g
Vls , Vat -> IAS at threshold = 1.23Vs1g

21
Q

T/O Segment

A
  • First Segment 35’ or Vlof -> gear up
    Second Segment gear up -> ACC alt / Gradient 2.4%
    Third Segment ACC alt(min 400’) -> clean config
    Final Segment Gradient 1.2%
  • Gradient panelty 0.8%
  • minimum SID Gradient 3.3%
  • Net flight Path Cruise gradient 1.6%
  • Runway Slope T/O Certificated +/- 2%
22
Q

T/O Speed

A
  • Vef -> Engine Failure Speed , CAS at which engine assume to fail
  • V1 -> Decision Speed , Vef + recognition time 1sec
  • VR -> Rotation Speed , speed at which pilot initiate rotate 3degree/sec
  • Vlof -> Lift off Speed , CAS at which plane first airborne
  • V2 -> minimum speed that must be reach at height of 35’ above runway with 1 engine
  • Maximum Tire Speed 195kt (Ground Speed)
23
Q

Approach phase Call out

A
  • “SPEED” -> VAPP > -5/+10
  • “SINK RATE” -> V/S > 1000’/min
  • “PITCH” -> Pitch <(-2.5)degree , >10degree (320) / >7.5degree (321)
  • “BANK” -> >7degree
  • “LOC” “GLIDE”-> 1/2 dot
  • “V/DEV” -> >1/2 dot
  • “CROSS TRACK” -> >0.1nm
  • “COURSE” VOR > 1/2dot , 2.5degree / NDB >5degree
  • altitude check point -> __ft high or low
    Landing phase Call out
  • “Pitch Pitch” -> reach (-2.5)degree , 10degree (320) / 7.5degree (321)
  • “Bank Bank” -> reach 7degree
    Go around phase Call out
  • “PITCH” pitch <10 , >20
  • “SINK RATE” no climb rate
    “Passing (Fix name) ___ft” -> FDP
    order FCU “MANAGE” = push button / only FL said before order -> “FL190 MANAGE”
    “Speed Check” check speed tape “Flap XXX” check lever position on ECAM Upper display
24
Q

Extend Duty Period

A
  • Extend Duty Period not more than 2hr (3hr with augment crew)
  • if allowed increase FDP is exceeded because of unforeseen after T/O flight crew may continue to planned destination or alternate
    Rest period following FDP maybe reduce but never be less than 8hr
  • Divert ไม่นับ Sector แล้ว (รู้ Maximum FDP ตั้งแต่แรก)
25
Q

OMA 8.3.12 Admission to Flight Deck

A
  • Admission to Flight Deck
    Crew perform duty
    Authorized officer under law of state
    person required accordance to OM
    person who authority of CAAT
  • “Code of the day” if no CDSS
  • Jumpseat -> CAAT inspector / Engineer / Flight Crew / Cabin Crew / Staff on duty travel
    maximum occupants allowed into the flight deck is limited to the available number of Jumpseat
  • อนุญาตคนนอกเข้า Cockpit หรือนั่ง Jump Seat ให้ขอจาก HFO
26
Q

Overweight Landing / Hard Landing

A

Overweight Landing
- at DMK, flight crew shall contact MOC to determine whether overweight landing can be performed
- malfunction affect Airworthiness
- expeditions landing would reduce the exposure to a degrading safety level
- 1 Engine inoperative
- serious illness required medical attention
Hard Landing (sink rate >=600 ft/min)
- shall be recorded in Aircraft Technical Log , MOR , ASR
- when ever LOAD15 generated after L/D , PIC must annotate in MR1 “Suspect Hard Landing”

27
Q

OMA 8.3.1 VFR/IFR Policy

A
  • AP should be engaged for normal flight >10000’ AAL
  • AP , A/THR shall be engage for approach in IMC if 300’/1600m above DH/visibility
  • Minimum height for turn 400’ AGL day , VMC / EOACC altitude night , IMC unless EOSID required
  • Visual pattern 1500’
  • Approach Ban -> if the reported RVR/VIS is less than minimum approach shall not continue
    below 1000’ AAL / final segment if DA> 1000’ AAL
    if pass 1000’ AAL approach may continue to DA
  • Touchdown point exceed 1000m for LDA > 2400m or
    exceed Touchdown zone marking for LDA < 2400m Go around must be initiated
28
Q

OMA 8.1.3 Methods for Determination and Use of Aerodrome Operating Minima

A
  • X-Wind T/O 30/20kt gust included - CP/FO
  • X-Wind L/D 30/25/20kt gust included - dry/wet/heavy rain
  • VAT = indicated airspeed at threshold -> aeroplanes categories classification
    1.3 VS / 1.23 VS1G(fly by wire) -> category C = 121 - 140kt
  • ICAO Miss Approach Climb Gradient 2.5%
  • เลือก Lower Minima เสมอถ้า ACG ไม่ถึงให้เลือก Miss App อื่นเช่น Company Engine Out
  • Circling APP minima 600’/2400m
  • Visual APP condition 1500’/5000m
  • intent for Visual Approach must be request & approved by ATC & briefing don prior to 5000’AAL
  • CMV ห้ามใช้คิด LVO , T/O minima , VIS <800m
29
Q

C/B Reset

A
  • Fuel pump C/B once tripped shall not be reset
  • in flight only 1 reset attempt should be made
  • Under no circumstances shall a tripped C/B be held in place in “set” position
  • Deliberate tripping C/B shall only be with requirements detailed in abnormal/emergency checklist
  • green CB monitor by ECAM after pull 1min
  • Wing Tip Brake CB have red cap to prevent reset in flight
30
Q

OM ETC*

A
  • ILS glide path 10nm +/- 8degree from centerline & 2degree above 1.5degree below
  • T/O & L/D is not allow when the report Braking action “Poor” (RWYCC 1)
    braking friction coefficient <= 0.25 (RCAM)
  • หลัง Control Rest ต้องจด Name , Time , Period ลง VR
    20 min prior to TOD
    maximum time <40min
    SCC contact every 20min
  • ATC flight plan valid 6hr & must be file at least 1hr before ETD
  • All ASRs are summitted to Safety Department within 24hr of incident being reported
31
Q

SOP ETC*

A
  • 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
  • to avoid TCAS RA on last 2000’ climb or descent limit V/S to 1500’ especially in busy airspace
  • Minimum Pavement for 180degree turn 30m for A320
  • ENG page oil quantity >=15qt or 9.5 + 0.5 qt/h (CEO), 8.9 + 0.45 qt/h (NEO&321)
  • AIRCRAFT ACCEPTANCE must be complete at the end of Cockpit Preparation
  • After reset rudder trim flight crew may observe indication up to 0.3degree (L or R)
  • OETD Yellow Electric pump ON providing nosewheel without using PTU
  • Wheel Speed 130kt connection between nosewheel steering & rudder pedal is removed
  • if GPS PRIMARY LOST & ACCURACY LOW
    check accuracy (position error <= 3nm is reliable) , if not reliable -> raw data
  • OAT > 30celcius , no refuelling is required -> keeping CONF1 to prevent AIR WING LEAK on hot weather condition
32
Q

FCOM limitation Speed*

A
  • Pitch 320 Gear Not Compress / Compress -> 13.5ceo 13.7neo / 11.7
  • Pitch 321 Gear Not Compress / Compress -> 11.2 / 9.7
  • MED brake 2sec after spoiler deploy 3m/s^2
  • LO brake 4sec after spoiler deploy 1.7m/s^2 (เครื่องใหม่ๆ เป็น 2sec 2m/s^2)
  • NWS on rudder pedals 6degree 40kt to 130kt
  • NWS from hand wheel 75degree 20kt to 80kt
  • Maximum Tire Speed 195kt (Ground Speed)
  • 320 Flap VMO Speed 230/215/200/185/177
  • 321 Flap VMO Speed 243/225/215/195/186
  • Minimum Rat Speed 140kt
  • APU
    FL250 Start by BATT
    FL225 Supply Bleed (single pack)
    FL200 Assist ENG start
    FL150 Supply Bleed (dual pack)
33
Q

FCOM limitation Speed 2*

A
  • VMO/MMO 350/0.82 , EXP DES Mach 340/0.8
  • Cockpit Window Maximum Speed 200kt
    Wiper Maximum Speed 230kt
  • Runway witdth 45m (required authorize if operate below)
  • Maximum Xwind 38kt (35kt for T/O NEO , 321)
    Maximum Tailwind 15kt (10kt for L/D CBL)
  • Tailwind L/D >10kt CEO Flap full ONLY / NEO , 321 Flap full Recommend
  • Maximum wind Passenger door operation 65kt
    Maximum wind Cargo door operation 40kt (50kt in leeward side) close before exceed 65kt
  • Taxi speed 20kt if T/O weight >76T
34
Q

ECAM SD page CRUISE check

A
  • ENG -> Oil pressure & temp
  • BLEED -> Parameter
  • ELEC -> Parameter & GEN load
  • HYD -> Slight decrease in quantity is normal / Fluid contraction during cold soak can be expected / Green system is lower than on ground following landing gear retraction
  • FUEL -> Fuel distribution
  • COND -> Duct temp compare with zone temp avoid large different for passenger comfort
  • F/CTR -> not any unusual control surface
  • DOOR -> Oxygen pressure
35
Q

OMA 8.9 EFB

A
  • Class 2 Type B EFB for TAA
  • mounting model: RAM-B-189-TAB3U
  • tolerance 2cm from designated location (17.5cm ขอบข้าง ,2.5cm ขอบล่าง)
  • FO responsibility for company IPAD (bear full cost base on market price)
  • 50% Battery charge EFB at duty time
  • EFB charging on ground while aircraft door open / >10000’ (Sterile Cockpit)
    charge until 80% / 2 hour
  • EFB Mount defect shall log in MR1
  • after loss of IPAD crew shall inform EFB manager to deactivated applications
    (maximum loan30 days)
  • In case dispatch with 2 IPAD
    Both IPAD belong to pilot -> PM will utilize his personal IPAD as company IPAD for Mission+
    1 Company IPAD -> PM handle company IPAD , PF use another IPAD
  • Base & Hub required 3 EFB / ต่างเบส required 2 EFB
36
Q

Medical Condition Unscheduled Landing

A

Unconsciousness
Severe Shock
Heart Attack
Stop pulse & breath
Uncontrol bleeding
Internal bleeding
Epileptic fits
Retained Placenta

37
Q

Refueling with 1 Engine Running

A
  • Applied in the event of unserviceable APU & no externel ground pneumatic power
  • Airport authorize is obtain & fire fighting at aircarft
  • Safety Cone of Rope shall be position
  • parking brake ON
  • 1 flight crew monitor form cockpit & Communication establish entire operation
  • Once​ refueling​ is finished,​ the ​PIC ​shall​ ​give​ ​permission​ for embarkation
  • PIC shall signal ramp staff to insert chock & Beacon ON
  • PIC permission is required for embark/disembark
  • Eng 1 running Eng 2 Shutdown “Cabin crew disarm all door & crosscheck”
  • D1R disembark/Catering
  • D2R D4R Armed & man by SCC
  • In event of Evacuation all star board sided used (port sided after Engine 1 shutdown)
  • Overwing fueling is not permit

E Captain (11 decks)

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