OM B Chapter 2 Normal Procedures Flashcards

Question

What are the TREF(flat temperature, lowest temp you can use as flex for takeoff.) for A319, A320, A321 ?

Answer 1

``` A319 = ISA +30°C A320 = ISA +29°C A321= ISA +15°C ```

Answer 2

when a TOGA takeoff shall be performed due to takeoff performance limitation. (RWY/OBS)

Answer 3

*At 130 kt (wheel speed), the connection between nosewheel steering and the rudder pedals is removed.*

Answer 4

It provide the Aircraft with a buffet margin of 0,3g. Pilot may enter a higher FL as long as it allow a margin of 0,2g

Answer 5

VLS+15kts in case of gusty or crosswind greater than 20kts

Answer 6

The checklist has to be completed by 500ft.

Answer 7

Aircraft shall be stable at 1000ft and must be at 500ft (400ft on circling) * A/C in landing config * On correct lateral and vertical flight path * Target final approach speed +10/-5 * Bank angle max 15° (for circling +-30° from final track) note : PAPI visual slope indications and FMS Baro VNAV path indications may not be aligned when OAT differs from ISA. When OAT is significantly above ISA, PAPI indications may indicate “4 whites” while following FMS vertical path. In this condition, the approach can be continued provided the FMS vertical guidance is followed.

Answer 8

1 FMS must be GPS Primary

Answer 9

At least 2NM before the final descent point

Answer 10

Yes as long as you use the other side AP/FD where GPS Primary is still active

Answer 11

* GPS Primary lost on both NDs * XTK \> 0.3NM * NAV FM/GPS POS Disagree on ECAM * NAV Accuracy downgrade on both FMGS * For LNAV/VNAV when deviation below vertical path of more than ¾ dot (75ft)

Answer 12

Yes you can continue but FINAL APP cannot be use, you need to use NAV FPA (with LNAV minima) For RNP AR you can't continue this approach, another approach must be selected Corrected, thanks Jascha

Answer 13

In the QRH **Aircraft Configuration Summary in Operational Data**

Answer 14

Both GPS and FMS must be available

Answer 15

LDEV \> ½ dot (1 dot is 0,1NM) VDEV \> ½ dot ( 1 dot is 100ft)

Answer 16

LDEV reach 1RNP (value on the ND not lateral scale) VDEV reach ¾ dot below profile (75ft)

Answer 17

Discontinue the approach and refer to the RNP AR equipment requirement

Answer 18

In case of **single** Failure of : * GPS Primary lost on one ND (use remaining AP/FD) * Nav accuracy downgrade on one FMGS (use the remaining AP/FD) * GPS (MMR) * FMGS * EFIS DU * MCDU * AP (use the remaining one)

Answer 19

* Final APP doesn't engage * Loss of GPWS terrain * FM/GPS position disagree * FMS1/FMS2 Pos Diff * GPS primary loss on both ND * Dual nav accuracy downgrade * Dual loss of FMGC or dual loss of Final APP mode * Dual AP failure if RNP \< 0.3NM

Answer 20

* One FMGC * One GPS * One MCDU * One FD * One PFD on the PF side * **Two** NDs * **Two** FCU channel * **Two** IRS

Answer 21

1 FMS 1 GPS or 2 DME to update FM Position Additional requirement if indicated on approach chart

Answer 22

⅓ of the runway or 1000m whichever is less

Answer 23

The ground spoiler have to be deployed

Answer 24

upon landing when rev is set, they will still deploy even if not armed

Answer 25

You have to go around before REV are deployed. As soon as the REV Have been deployed it must be a full stop landing

Answer 26

Set to toga then Flex/MCT

Answer 27

Captain says “I HAVE CONTROL” and press and hold takeover push button Annonce TOGA Adjust pitch to climb away from the ground Do not change config until captain says Go around flaps Note: it may trigger Config Flaps not in TO position =\> disregard

Answer 28

If temp diff between two brakes of the same gear are more than 150°C and one of these is above 600°C If temp diff between two brakes of the same gear are more than 150°C and one of these is below 60°C If temp diff between left and right gear is more than 200°C Brakes temp more than 900°C

Answer 29

* “SPEED” if the speed decreases below the speed target -5 kt or increases above the speed target +10 kt. * “SINK RATE” when V/S is greater than -1000 ft/min. * “BANK” when bank angle becomes greater than 7°. * “PITCH” when pitch attitude becomes lower than -2.5° or higher than +10° (A319/A320)/+7.5° (A321). * “LOC” or “GLIDE” when either localizer or glide slope deviation is 1/2 dot for LOC or GS. * “CROSSTRACK” when greater than 0.1nm deviation from inbound track in FINAL APP mode. * “V-DEV” when greater than half dot deviation from approach path in FINAL APP mode. * “COURSE” when greater than 1/2 dot (VOR) or 5 degrees (ADF). * “\_\_FT HIGH/LOW” at altitude checks points.

Answer 30

* “LAT-DEV” when L/DEV reaches ½ dot * “VDEV” when ½ dot deviation above or below path * “SINK RATE” when the descent rate exceeds 1000 ft/min * “BANK” when the bank angle goes above 30°.

Answer 31

During landing, the PM announces: “PITCH PITCH”, if the pitch attitude approaches the tail strike pitch limit indicator or reaches +10° (A319/A320)/+7.5° (A321). “BANK BANK”, if the bank angle reaches 7°.

Answer 32

During a go-around, the PM announces: “BANK”: If the bank angle becomes greater than 7°, “PITCH”: If the pitch attitude becomes greater than 20° up or less than 10° up, “SINK RATE”: If there is no climb rate.

Answer 33

**TRAMPLING OF CABLES IN A RIGGED/UP STATE** **General Information** The take off run should be started after any RIGGED/UP cable or from a point such that the speed is \<40 kt as the aircraft crosses the cable. During the take off roll there should be no operational concern for crossing a RIGGED/UP cable provided the aircraft does not exceed the 40 kt limitation at the point of crossing the cable. Trampling a RIGGED/UP cable at greater than 40 kt is not recommended: In the event that a cable is trampled in excess of 40 kt, contact MOC for an inspection procedure. In the case of a high speed abort and subsequent crossing of a departure end RIGGED/UP cable at speed, then a check is to be done of the undercarriage to confirm no damage: refer to MOC. **TRAMPLING OF CABLES IN A RIGGED/DOWN STATE** There are no restrictions on operations on runways where the cables are in the RIGGED/DOWN position. **Operational Caution Notes:** Check with the local Airport Authorities that they have not published any specific operating restrictions. Landing beyond the cables reduces the possibility of damage. If landing beyond the cables is not feasible, inspect the aircraft in order to check that there is no damage. If the cable is raised taxi slowly, with a maximum transit speed of 40 kt. For cable laid to the runway surface, there is no technical objection to cross the cable at a speed \> 40 kt. Do not cross the cables at maximum reverse thrust. Take into account the above recommendations for the performance computation. Carefully monitor the tyre pressure of your aircraft to avoid rolling over the cables with less that recommended tyre pressure. Inspect the landing gear to detect any damage caused by the arresting device in the case of trampling a RIGGED/UP cable \>40 kt.

Answer 34

TREF is the flat rating temperature, meaning the lowest temp you can use as flex for takeoff. It is used for takeoff as the TFLEX has to be above the TREF FCOM EFB TOF 20 20 20 A319 = ISA+30 A320 = ISA +29 A321 = ISA +15

Answer 35

**Shear Pin Failure** In the event of a shear pin failure during pushback: * if push stop immediately after failure then no inspection is required * nose gear must be inspected when there is separation and overrun of the towbar by A/C, Push-turn operations, when the towbar arm touches the tractor after a failure of the turning towbar shear pin only.

Answer 36

Steeper is when angle more than 3,5° and 4,5° No autoland No CAT III/II Decelerated approach can be done up to 3,5°, if greater then fully stabilised approach is required OMB 2.4.26

Answer 37

* Press RCL more than 3s to see cleared or canceled ECAM * ECAM pages (OXY, HYD, ENG (oil)) * Tech log * Aircraft configuration summary * OEB

Answer 38

The computation of DISPATCH LDG PERFORMANCE is not required if the flight crew can ensure that RLDW is limited by maximum structural landing weight, this is only applicable when DRY or WET runway surface conditions are expected.

Answer 39

It is flown by the commander It is a go around initiated near the ground (during landing from flare until thrust reverser selection)

Answer 40

if any of the following occurs at any time during landing: * An emergency * Deceleration not as expected * Failure affecting landing perf * Long flare or long touchdown * Unexpected tailwind OMB 2.3.19.1

OM B Chapter 2 Normal Procedures Flashcards

(66 cards)