FCAP Flashcards

1
Q

VHF#3 Shall be addressed to Acars-Datalink communications (ACARS or DATA selected). (Airline Policy) Scan mask is defined

A

and selected by Maintenance.

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2
Q

Fuel Planning must not be based only on FMS predictions. If the values provided by the FMGS FUEL PLANNING are considerably different from the OFP fuel requirements,

A

the values shall be crosschecked with the tables “Quick Determination of F-PLN” FCOM / PER-FPL-FLP-QFP-10, according to the instructions provided on it. These tables will be available on EFB ADDOCS, in the file named FUEL DETERMINATION.

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3
Q

During flights operating at Santos Dumont and Congonhas the CM2 should

A

use present weather conditions to calculate and inform the MTOW to dispatcher with ATIS code via ACARS or when not available using VHF on AZUL’s frequency.

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4
Q

Perf Factor: Should be filled with

A

OFP value

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5
Q

PERF PAGE: • Insert the takeoff Acceleration Altitude and Thrust Reduction value from Fly Smart (MINALT) / DIM (minimum is 400 ft AGL), except for Santos Dumont where the Acceleration Altitude

A

is always 1500ft.

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6
Q

FINAL LOADSHEET

CM2: • Insert LOADSHEET

A

ZFW, ZFWCG and THS on FMS; • Update ATOW and T.O CG (basic or extended fwd) on FLYSMART, if necessary; • Validate all data entered on FMS with CM1.

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7
Q

The Pilots may consider a rolling takeoff as long as the conditions below apply:

A

a) Runway longer than 1.800m; b) Taxiway with direct access to the threshold (no back track); c) Select Modify Runway then choose ENTRY ANGLE of 76° (this configuration will reduce runway length in 76 meters); d) Line up following the yellow line.

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8
Q

When not to perform a rolling takeoff:

A

a) When penalize the payload; b) Contaminated runway; c) Heavy rain; d) Low Visibility; e) Technical conditions that may affect braking efficiency; f) SBSP and SBRJ Operations; g) Narrow Runways (less than 45m width).

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9
Q

Last Minute Change: • LOADSHEET

A

335KG

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10
Q

Maximum difference between Operational Flight Plan and Loadsheet (AZFW greater than EZFW) is

A

1300 kg.

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11
Q

If the difference is greater than this value, crew must consider fuel on board,

A

air traffic and weather before requesting additional fuel. It´s not mandatory to request another OFP. Using table below, crew may request additional fuel to account for weight difference

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12
Q

Set ATC to AUTO when

A

clear to start the pushback

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13
Q

A321

Last Minute Change: • LOADSHEET

A

390KG

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14
Q

One engine taxi out

Important Information: a) Taxi is only performed by CM1; b) The start of Engine 2 is performed by CM2;

A

c) Before taxing the Y ELEC PUMP must be turned ON to provide nosewheel steering without using the PTU; d) Before start the Engine 2, the CM2 must turn off the Y ELEC PUMP to enable the PTU automatic test; e) Taxi must be performed in straight line at least 5 sec after selection of the ENG 2 master lever to ON, in order to ensure the PTU automatic test

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15
Q

TAKEOFF RUNWAY

Confirm runway signs/markings.

Confirm visually if

A

PERF Speeds and FLT Plan SID on FMS is for the intended takeoff runway.

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16
Q

After the engine has started, operate at or near idle for at least.

A

3 minutes before selecting high power

17
Q

Flexible takeoff method should be used. However, it is not permitted on

A

contaminated runways. In SBSP Flexible takeoff is not permited with WET runway.

18
Q

For takeoff, all external lights must be on, except

A

for the wing light

19
Q

PM should start the Elapsed Time prior

A

for takeoff in order to monitor the flight time

20
Q

The LAND LIGHTS must be immediately turned off

A

after flaps lever is set to zero

21
Q

In Range Report

The following items must be informed: a) Actual time of departure (ATD)

A

Out of block time; • Out of ground time. b) Estimated Time Arrival (ETA); c) Delay code.

22
Q

The following are part of the PF flight progress check: a) Weather: Destination and alternates weather conditions (ACARS and VOLMET);.

A

b) Step Flight Level: Manage the optimum flight level considering best fuel consumption, wind and turbulence; c) TCAS: Can be selected to BELOW position during cruise at any FL; d) Sec FPL: During cruise, SEC FPL may be used to simulate step climbs, alternate, and contingency routes, such as redispatch route

23
Q

The following are part of the PM flight progress check: a) OFP: Should be filled up by PM and verified by both pilots during flight;

A

b) Wind Data: Wind entries should be made at waypoints when there is a difference of either 30° or 30 kt for the wind data and 5 °C for temperature deviation; c) Flight Monitoring: After the first flight hour ACARS free text message must be sent with the following information to DISPATCH:

Last Waypoint + Time Over + ETA (e.g. REMIG 1000 VCP 1130)

24
Q

Flight Monitoring messages should only be updated in the following situations: • Change in ETA greater than 10 minutes (e.g. NEW ETA 1030);

A

• Unforecast turbulence encounter (e.g. LGT/MOD/SEV TURB FL390 OVER POS); • Weather deviations exceeding 40 Nm of track. (e.g. XW DEV 45NM R/L); • 30 minutes prior to redispatch point with ETO / Estimated fuel on board / CI / FL (e.g. POPMA 18:00 5.5T CI40 FL380); d) Report of failures that occurred during flight a message must be sent to MAINTENANCE (e.g. ELEC AC ESS BUS FAULT).

25
Q

LDG CG configuration must be checked on

A

LOADSHEET (MACLAW) and correctly selected on FlySmart and QRH tables.

26
Q

Conf A

A

RWY DRY; • Informed on Airport Briefing for each RWY. • RWY length/width equal or more than 2.200 x 45 CONF 3 2. REV IDLE 3. AUTOBRAKE LO

27
Q

Conf B

A

RWY DRY; • Informed on Airport Briefing for each RWY. CONF FULL 2. REV IDLE 3. AUTOBRAKE LO

28
Q

Conf C

A

RWY WET; • Informed on Airport Briefing for each RWY. • Required by performance. 1. CONF FULL 2. REV IDLE - RWY DRY 3. REV MAX - RWY WET 4. AUTOBRAKE MED

29
Q

In Range Report a) The following items must be informed: • ETA; • Maintenance status. b) And if necessary:

A

GPU/LPU; • QTA/QTU; • Special requirements for passenger (ex. Wheelchair). c) Obtain parking spot and next schedule flight for aircraft. d) Obtain information if has connecting passengers that will remain on board

30
Q

When LANDING GEAR is selected down,

A

the LAND LIGHTS must be turned on

31
Q

At or below taxi speed, CM1 disarm the spoilers then After Landing Flow should be initiated, including

A

selection of Brake Fan

32
Q

The flight crew must operate the engines at or near idle thrust for a cooling period of

A

3 min before engine shutdown, in order to thermally stabilize the engines.

33
Q

One Engine Taxi is the normal TAXI-IN procedure. It must be disconsidered if any of following situations apply:

A

a) Overweight landing / High gross weight; b) Slippery taxiways; c) Uphill slopes; d) Low visibility conditions; e) Hi workload after landing; f) MEL ITEM related to: • AIR CONDITIONING; • APU; • ELETRICAL POWER; HYDRAULIC POWER; • PNEUMATIC.

34
Q

ENG 2 SHUT DOWN

The flight crew must operate the engines at or near idle thrust for a cooling period of 3 min before engine shutdown, in order to thermally stabilize the engines.

A

Y ELEC PUMP ON

35
Q

Parking

A

Y pump off

36
Q

Since the aircraft system automatically disregard any unavailable satellite, Airbus does not require to

A

deselect the PRN number displayed in NOTAM AZUL.

37
Q

OFP with Reclearance: With any difference (AZFW greater than EZFW)

A

a new Operational Flight Plan can be requested by Captain.

38
Q

When performing a Take-Off, in case of a RTO due to Engine Failure, call:

A

“NO REVERSE ENGINE __”