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Old 5th Feb 2013, 16:34
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Gncy
 
Join Date: Oct 2012
Location: Asia
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Qatar Airways_A320 Line Training Technical Questions - Rev.03

Hey guys,

My personal notes from my line training on A320, all the technical questions, answers and tech references up to date. Quite a few guys didn't make it on this fleet and I don't think they were bad pilots but rather unlucky.
Please feel free to implement the revision number in the title with your own questions and we will get something good.

Hope it helps,



TCAS max rang? Proximity, TA, RA? DSC-34-80-10
THRT, ALL, ABV, BLW? DSC-34-80-20

TCAS TA, PF: “TCAS, I have control”, follow TCAS even with climb orders at max ceiling FCTM SI-060
altitude; disconnect FD after APs to ensure autothrust speed mode; PNF will not try to see
intruders
TCAS TA, maintain safe separation if contact is established OM Part A 8.3.6
If under TCAS RA manoeuvre, ATC request opposite action: “unable TCAS RA”
When clear of conflict: “returning to FL xx or ALT xx”, and then “clear of conflict (assigned
instruction / clearance) resumed”

Turbulence speed:
A320: 250kts, 300kts-0.76M at or above FL200 PRO-SUP-91-10 p5/8
A321: 275kts, 305kts-0.76M at or above FL200 PRO-SUP-91-10 p7/8

Use of EXP CLB up to FL 250, revert from EXP to normal via managed mode preferable PRO-NOR-SRP-FMS-01-40

To cancel “TOGA LK” or “ALPHA FLOOR”, disconnect A/T (leave thrust in CL) and DSC-22-30-90 p9/12
A/T ON again

The value manually displayed on the FCU will vanish in: DSC-22-10-40-20 p2/8
_ 10s for the speed window
_ 45s for the HDG/TRK and V/S windows

Set brake fans:
_ Just before stopping at the gate (disregard the 5 mins, it is a minimum time) SOP 3.03.24 p2
_ If brake temp at 500°C

Tankering will be limited for any last minute increase of the ZFW to: OM Part A 8.1.7.4.2
_ MLW reduced by 500kgs
_ The next rotation of the aircraft

The forward and aft cargo door are hydraulically opened from the yellow hydraulic system DSC-52-10-40 p1/2
and mechanically locked open and closed. The bulk cargo door is only mechanical.

ASR to be submitted to the flight safety office within 12 hours and OM Part A 11.6.1
forwarded within 72 hours to the QCAA OM Part A 11.6.2
List of occurrences OM Part A 11.6.3

TOW between prelim and final loadsheet: +0kg; -500kg: use prelim TO perf SOP 3.03.07 p1a
LMC > +/-500kg: new loadsheet; LMC>+/-250kg: new LIZFW OM Part A 8.1.8.3

Flight instruments tolerance (ADRs, ISIS, magnetic heading speed…) PRO-SUP-34

CG>27%, basic forward CG (25% TO and LDG plus operational margin) PER-LOD-WBA-LTS
LIM-13 p15/22

Service ceiling: A320 and A321 (except ADK): 39800ft, ADK: 39100ft, A319: 41100ft LIM-12
Minimum altitude airfield: -1000ft, maximum OAT 55°C Environmental envelope

NPA with Engine Out LIM-22-10
_ No limit for A319, A320
_ A321: AP not approved for FINAL APP or NAV (V/S or FPA). The FD can be used

How long can we wait at max transient engine oil temperature? 15min LIM-70 (oil)

Take off following SRS should give a speed between V2 and V2+15 with one engine FCTM AO-020 p11/12
and between V2+10 and V2+25 with two engines FCTM NO-050 p5/10
With no FD (after rotation of 12.5° for one engine), the pitch is 15° FCTM NO-180 p2/6

On ground the amber half frame of the OXY pressure indication on the ECAM DOOR/OXY DSC-35-20-20 p5/8
SD page (1000 or 1500psi depending of the A/C) requires to check with the LIM-35.

Pax missing: offload checked baggage, ask PAX to identify their cabin luggage to avoid OM Part A 10.1.14
offloading the wrong ones, fill loadsheet with names, number of baggage

Emergency communication with the cabin crew members:
_ Hijackers: ---censured--- OM Part A 10.1.21.5
Cabin and safety manual
_ Emergency in the cockpit: “CS to the flight deck” 5.5.6
_ Emergency alert on ground: “Attention crew at stations” 5.5.5
_ Abort evacuation after the emergency alert on ground:
"Cabin crew and passengers - keep your seats" 5.5.5
_ Evacuation: "Evacuate, evacuate, evacuate" 5.5.4
_ Turbulence: “Cabin crew, take your seats” 5.1.1
_ Emergency descent : ???
_ End of emergency descent: "We have reached a safe altitude; cabin crew and
passengers may remove their oxygen mask" 5.3.6

ICAO Aerodrome reference code 4C (code element 2, wing span between 24m and 36m, OM Part A 8.1.2.1.1
outer main gear wheel span between 6m and 9m) Jeppesen_Text_Book,
introduction, glossary

Turn Radius minimum pavement for 180° A319-20-21: around 21m-23m-28m DSC-20-20 p6/12
Wing clearance A319-20-21: around 22m, tail A321: 25m

Fuel feed system sequence:
_ First the ACT (fuel transfer to the centre tank) DSC-28-10-30 p10/12
_ Centre tanks, if the fuel used to cool down the IDG overfill the inner tanks (via the DSC-28-10-60
transfer valves of the outer tanks or the spill pipe), then the centre tank pumps are stopped
until 500kg have been used in the inner tanks… and so on until the centre tanks are empty
_ Inner tanks down to 750kg each
_ Outer tanks through the transfer valves via the inner tanks
_ The last 1500kgs are in the inner tanks

Position computation DSC-22-20-20-10
IRS Mix is a point computed from the three IRS (with less credit for the one which is
drifting or one IRS each if only two are serviceable).
The GPIRS is a mixture of each IRS position and one of the two GPS (based of priority and merit).
The vector between the GPIRS (or the radio position if the GPS mode was rejected by the FMS/
deselected by the pilots) and the IRS Mix is called the BIAS. It is permanently updated by each
FMGC (unless loss of GPIRS and radio then it remains constant) and computed from the IRS Mix
to get the FM position.
If the pilots update the FM position, they also update the BIAS calculated from the IRS Mix.

ICAO holding speed limit: Jeppesen_Test_Book
_ 14000ft <= ALT 230kt Air Traffic Control
_ 14000ft < ALT < 20000ft 250kt Flight Procedures
_ 20000ft < ALT < 34000ft 265kt Part IV Holding Procedures
_ 34000ft < ALT 0.83M
ICAO time of outbound leg in the hold (when no DME and distance specified):
_ 1 minute at or below 14000ft
_ 1.5 minute above 14000ft

Pitot heads, Static ports, AOA and TAT Probes/Window Heating comes on: DSC-30-40-10 p1/2
_ Automatically when one engine is running or in flight DSC-30-50-10 p1/2
_ Manually, with the PROBE/WINDOW HEAT pb set to ON
On the ground:
_ Only at low power for the pitot and windshield
_ Not at all for the TAT probes

Contaminated runway: OM Part A 8.3.8.12.1,
_ More than 25% of surface covered with more than 3mm of water,
loose (non compacted?) snow, slush more restrictive than:
_ Covered with compacted snow
_ Ice and wet ice PER-TOF-CTA-20
Wet runway: _ Less than 3 mm of anything but compacted snow, ice, wet ice
_ Damp

Conditions of cancellation for the destination alternate in cruise: OM Part A 8.3.7.1.4
_ Less than 6 hours to destination
_ FOB at touchdown >= final reserve fuel
_ One runway, weather forecast from 30mins before ETA until 1hour after, ceiling >=2000ft or
min circling+500ft (the greater), visibility >= 5000m
_ Two runways, weather forecast from ETA until 1hour after, downgrade to one category
(ILS CAT1: NPA, NPA: MDH+200ft, RVR or VIS +1000m, circling unchanged)

Aircraft critical systems failures requiring an immediate diversion to the nearest suitable OM Part A 8.5.9
airport:
Two of these failures: _ Blue hydraulic circuit or pump PRO-SPO-40-40 p1/2
_ APU or APU GEN
_ IDG 1
_ IDG 2

AWOPS, effect of failed or downgraded equipment (airport and aircraft) OM Part A 8.4.14
The ISIS or the use of FD for instance are not listed therefore not required for CAT2 or 3 QRH OPS.04

Generators priority: DSC-24-20 p5/32
_ GEN 1 and 2
_ External Power
_ APU Generator

Consequence of a double loss of hydraulic circuits for the flight controls: DSC-29-10-30 p2/4
_ Blue and Green: Aircraft harder to fly
_ Green and Yellow: Aircraft harder to land

Cargo fire extinguisher, two for A320 and A321 first bottle discharged in 1min, DSC-26-50-20
second 60min after and during 90min (60min for A321). Only one bottle for the A319.

Daily check validity 36 hours, 48hours at out station OM Part A 8.1.11.1.4
Tech log #16

An Air Crew Notice (ACN) can be reissued not later than after 3 months

Example of flight duty limitation: OM Part A 7.3.7
A cabin crew is in Std by between 0600 and 1800, she is called out from std by at 1600 OM Part A 7.3.8
and report at 1700. She was acclimatised and will fly 2 sectors. OM Part A 7.5
What is the total duty period allowed?
Called after 6 hours, 11 hours of duty plus 12h15m allowed minus 5 hours of std by
exceeding 6 hours equals 19h15 (1 hour more than the pilots)

Exceedance of flight duty time or reduction of rest periods:
_ In flight relief OM Part A 7.4.1
_ Split duty time OM Part A 7.4.2
_ Commander’s discretion to extend/reduce OM Part A 7.4.4
OM Part A 7.4.5
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