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Line 4 > Salsa > Flashcards

Salsa Flashcards

1
Q

PROGS im OFP

A

Collection time and time of forecast data

Wx Charts updated 4times a day with 30hours validity

00; 06; 12; 18 utc

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2
Q

At night Instrument approach shall be preferred to visual approach

A

Category c circling minimsa- visual

Mdh 600ft
Minimum vs 2400m

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3
Q

Planning

Takeoff alternate
——-
Destinstion

——
In flight

A

ETA plus minus 1 Hour

Precisuon : RVR only ( min CAT1)
Non precision: vis and ceiling

————————-
Gleiche , wenn darunter muss man 2nd alternate nehmen

—-
Bis 1000 ft Continue, nur RVR entscheidend, bei DA muss man Referenz haben. Wenn nur vis gegebenen, umrechnen in rvr

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4
Q

If a main landing gear tire is damaged during takeoff, it is possible that braking of the main gear wheels during retraction may be affected. A spinning tire with a loose tread must be stopped prior to entering the wheel well or it can cause damage to wheel well components. When a spinning tire with loose tread impacts a fitting in the wheel well ring opening, that gear stops retracting and free falls back to the down position. The affected gear cannot be retracted until the fitting is replaced.

A

-

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5
Q

Speed von 250 direkt auf 180

A

Flap Extension Schedule requires reducing the command speed to ‘Up’ speed before selecting faps. During fap extension, selection of the faps to the next fap position should be made when approaching, and before decelerating below, the manoeuvre speed for the existing fap position. This event is a useful reminder of the importance of awareness by PF when PM’s monitoring is degraded e.g. a verbal update on the command speed reduction may have helped PM spot the oversight.

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6
Q

In accordance with OPS 009-17 Autopilot engagement during a go-around is not recommended until the faps have been retracted (to the planned fap setting) and LVL CHG/VNAV has been selected, or the missed approach altitude is captured. Engaging the autopilot prior to this will result in non-standard AFDS modes which are not in accordance with the NP

A

On selection of TOGA, the FD’s did not appear, causing PF some confusion and distraction. Nevertheless, the required task of pointing the aircraft safely away from the ground with adequate power and along the prescribed track was accomplished. It was not until circa 1,500ft that PM realised that during the approach, they’d indeed turned the FD’s off (rather than recycle them).

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7
Q

Canarias UIR—South of 25N and west of 20W

A

contact Canarias radio on HF and or do a SECAL Check

One Hf is enough since we have Alternative VHF freq. otherwise 2 HF needed

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8
Q

Required communication equipment

A

2 independent systems required —2 HF
MEL says:If not crossing the Atlantic and alternatives are given (VHF) one HF is enough

Special~

in Canarias UIR south of 25N and west of 20W—one HF is required
No HF requirement in SAL Oceanic and routes via
GUNET since they are east of it

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9
Q

Manual takeoff

A

A/T bleibt an. Nur FD sind Off…

Bei über 80 Knoten unter 2000ft dgl. kann man beim drücken von TOGA die FD Commands anzeigen lassen

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10
Q

Dual AP approach, AT

A

AT disconnects automatically after 2s..but this time with no indication

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11
Q

Normal Takeoff…normal thrust reduction is at 3000ft.how can you immediately start the thrust reduction to climb thrust

A

by pressing N1

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12
Q

dual AP landing

A

always with Vref plus 5..even with no HWC

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13
Q

How and when is the AT G/A Mode being armed?

A

below 2000ft with A/T engaged…until 2s after landing

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14
Q

During normal landing with AP and AT disengaged

A

Pressing TOGA you have to advance thrust lever manually….green bug

When flying manually with no FD it is important to have the FD recycled to have the

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15
Q

FD off flight

A

dont forget to recycle FD

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16
Q

Non precision Flight

A

we turn FDs off at the minimas..then recycle FD!

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17
Q

an alternate source of power for autoslat operation is..

A

system A hydraulics through PTU in case of system B pressure loss

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18
Q

standby hydraulic is for

A

LE slats..not autoslats!

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19
Q

Speedbrake Armed…deploy automatically if..

A

Thrust IDLE; Right landing gear/any landing gear, Radio Alt less than 10ft and main landing gear spin up (more than 60knots)…if spin up does not occur it right/any landing gear is enoug

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20
Q

speedbrake not armed during landing!

A

speedbrake automatically operate when main landing gear wheel spin up (more than 60); IDLE and REVERSE THRUST!

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21
Q

TE flaps relief speed

A

F40 bei 163kts, F30 bei 176

22
Q

FMC gets its fuel indication directly from

A

fuel quantiy indication system

23
Q

Kein waypoint sollte weiter als 100nm von der position weg sein…

A

alles unter 100 wird mit dem aktuellen wind gebiased!

Heißt abeams nehmen um nahe Punkte zu haben, da aktuele winde genau sind!

24
Q

DRAG required on FMC

A

10 knots ore more above FMC target speed or within 5 knots of VMO/MMO

25
Q

OVERSPEED DISCONNECT

A

DUring path descend: FMC speed restrictions exceedance by more than 15knots

26
Q

Sonne geht auf

A

In östlicher Richtung

27
Q

Sonne geht unter

A

Westliche Richtung des

28
Q

Medical im Cockpit bzw 40 min zur Notlandung -ditch

A

SCCM to Cockpit (3x)

29
Q

Kommandos zeitliche Reihenfolge Notlandung

A 
40 min-SCCM to Cockpit 
20min-prepare for emerg. Landing-ditching
2min-attention Crew in Station -ditch
30s-brace brave Safety Position -ditch
Passender evac-ditch
30
Q

Crew zum sitzen auffordern bei landing

A

Canon Crew please ne Seated

31
Q

Transit search was eintragen in TAL

A

NIL

32
Q

Was draußen beim SS checken

A 
Aft/fwd Cargo sofern noch nicht Beladung gestartet wurde 
Nose wheel 
Main Wheel well 
Toilet
Water
Pre condionded air 
Power recep
33
Q

Antalya-mun-ham

A

Transit search steht NIL drin…

Hier muss Hamburger Crew SS machen. Cockpit muss letzen beiden leg’s checken und Bescheid geben !

34
Q

FOX wird für Passagiere gebraucht… wichtig für Rückflug

A

Gesetzgeber sieht mindestdruck in FOX von knapp 1500 Psi für Rapid decomp vor… heißt lieber mehrere anfangen und Druck hoch lassen

35
Q

A question from our follower: “What would you do, if you got a TCAS RA climb, climb at FL410?”

Conclusion: As majority of you correctly said, follow the RA. Even at the limits of the operating envelope the airplane has sufficient performance available to follow the RA “Climb”. Check out the FCTM where you can find more details

A

-

36
Q

Approach briefing

A

Master Caution recall
Landebahn beschreiben, Papi
GS alert bei IAN

37
Q

Toperf speeds zu hoch

A

Ging dieses Mal auch mit no improved climb ?

38
Q

Richtung hurghada

A

15 min prior Egypt airspace call Cairo on SET 2

39
Q

De icing remote

A

Anmelden bei ops oder startup freq
Pad Frequenz auf Set 2
Sofort nach Engine Start Anti Ice on
Flaps up hin—nach enteisung f40 und auf to setting sofern nicht unter 0 grad mit preci oder contam
No flight control check — nah enteisung 2 mal
Trotzdem before Start cL
Anmelden mit Flugnummer und Kennung mit benötigte enteisung

40
Q

After landing cooling period engine

A

At least one minute (starting from idle reverse )

Three minutes are recommended

41
Q

Apu start time

A

1 min 15 sec

42
Q

Engine anti ice nach Landung

A

Buch sagt Engine aus und Damm mit Procedure aus machen

Ruben sagt

43
Q

Condotional clearances

A

Conditional line up clearance:
Big Jet 345, behind landing Boeing 757, line up runway 27, behind
Behind landing Boeing 757, line up runway 27, behind, Big Jet 345

44
Q

Wann cont/ wann FLT

A

CONT
- provides ignition to selected igniters when engine is operating and start lever is in IDLE
- inflight, provides ignition to both igniters when N2 is < idle and start lever is in IDLE
- use for operation in heavy rain
FLT
- provides ignition through both igniters when the start lever in IDLE
- the ignition select switch is bypassed when in this position (FLT)
- use for inflight starts (windmill), severe turbulence, flight in moderate to severe icing or volcanic ash

45
Q

Ideally Main gear touchdown with thrust reaching idle

A

-

46
Q

RNP Approach

A

Nps und 2 fmc required

2nm before final, 45 degrees

47
Q 
SPEED 
after Takeoff 
Takeoff with failure at V1
GA
Single engine GA
A

v2+15 bis v2+25— Toga pitch geht auf v2+20

Min V2 bis v2+15—Toga pitch geht auf current speed min V2

V2+15 bis v2+25— Toga geht auf next flap setting, IAS blanks

V2 bis v2 +15– Toga geht auf selected Speed; IAS is open

48
Q

Sobald Höhe genannt wird nach der man turnen kann m.. Climb with max Gradient

A

Engine anti ice conditions- gleich Englne anti ice anmachen nach Start!

49
Q

Recirc procedures

A

Preflight an
Flight an
Nach landing as needed

50
Q

The role of the pilot monitoring to actively monitor and identify airspeed stagnation during the rotation phase to take-off target pitch attitude.
• In gusty conditions, momentarily delay rotation to ensure that the aircraft starts rotation at an average speed above the rotate speed.
• Adherence to the recommended average all-engine take-off rotation rate of 2 to 3° per second.

A

-

Line 4 (11 decks)

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