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Command > SOP's > Flashcards

SOP's Flashcards

0
Q

The recommended procedure for flight in severe turbulence is?

A
  • Target airspeed is 280 knots or .76 MACH whichever is lower, do not chase the airspeed
  • if autopilot is engaged use CWS, do not use ALT HOLD
  • auto throttle disengage
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1
Q

When should gear be taken on an ILS?

A

At 4nm, but not later than 3.5nm, call “GEAR DOWN”, “FLAPS 15.” Arm speed brake and check green light illuminated. Call “LANDING CHECKLIST DOWN TO FLAPS.”

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2
Q

What are the maximum and recommended speeds at which you can exit a Rapid Exit Taxiway?

A

Maximum speed 60 knots

Recommended speed 45 knots

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3
Q

If moderate to heavy rain, hail or sleet is encountered…

A

Start switches should be positioned to CONT, Autothrottle disconnected, thrust levers adjusted slowly. A slower IAS/Mach used and consideration given to starting the APU

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4
Q

What warnings signify predictive windshear?

A

‘Windshear Ahead’
‘Go Around Windshear Ahead’
‘Monitor Radar Display’

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5
Q

When should a commander declare a Mayday for fuel?

A

When calculated usable fuel on landing at the nearest suitable aerodrome where a safe landing can be performed is less than final reserve fuel.

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6
Q

In flight fuel checks should be performed and recorded on the plot at…

A

At TOC or nearest equivalent abeam waypoint and regular intervals in the cruise. Time interval in the cruise is 30 mins or next waypoint thereafter. Fuel shall be recorded at TOD

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7
Q

The minimum pressure for the Brake accumulator gauge (HYD’s pressurised). on the walk around is?

A

2800 psi

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8
Q

Maximum taxi speed on the apron is

A

15 knots

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9
Q

It is policy to conduct a low drag approach once the met and visibility is above?

A

1000ft

5000m

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10
Q

An ‘Emergency Turn’ (Engine failure on take off) must be flown at?

A

V2 with a 15’ angle of bank

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11
Q

At what stage are we no longer constrained by MEL?

A

Once pushback has commenced, the aircraft is no longer constrained by the MEL

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12
Q

How long does the rectangle around each mode annunciation remain active after each engagement.

A

10 seconds

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13
Q

Whenever the APU is operating and AC electrical power is on the airplane busses, operate at least one fuel boost pump to supply fuel under pressure to the APU to extend the service life of the APU fuel control unit.

A

Correct

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14
Q

For aircraft with the old centre pumps installed (placarded) the centre pumps should not be switched on for T/O with less than ?

A

2,300kgs of fuel in the centre tank.

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15
Q

Prior to switching on the A system pump switches, we should ensure?

A

Ground personnel are clear of the tow bar or the bypass pin is installed

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16
Q

Oil quantity for dispatch is?

A

12 quarts

17
Q

When we test and hold the oxygen for 5 secs what are we checking for?

A

Verify that the crew oxygen pressure does not decrease more than 100 psig.

18
Q

Assumed temperature thrust reduction shall be used with the exception of the following:

A
  • contaminated or slippery runway
  • windshear is suspected
  • anti-skid inop
  • thrust reverser inop
  • TOW is within 500 kgs of the RTOW (1000kgs when obstacle limited)
  • EEC in alternate mode
  • landing gear extended flight
  • bleeds off takeoff
  • when prohibited by airfield brief
  • crosswind exceeding 10 knots.

Note: When crosswind in excess of ten knots exists and no assumed temperature reduction off a given derate is possible, then the next highest derate shall be selected, i.e., 22k derate, no assumed temp possible, select 24k for this takeoff. This is a tailstrike prevention policy.

19
Q

FMC speeds may be used if they differ from the calculated RTOW speed by no more than ?

A

1 knot

20
Q

Quick method for checkin accuracy of loadsheet

A
  • Subtract the actual load from the allowed load
  • Add the resulting figure to the T/O weight

This should give you the max allowable T/O weight

21
Q

Position engine start lever to IDLE detent when:

A
  • N1 rotation is observed and
  • N2 RPM reaches 25% or (if 25% N2 is not achievable)
  • At max motoring and a minimum of 20% N2.

Max motoring occurs when N2 acceleration is less than 1% in approximately 5 seconds.

22
Q

After engine start engine EGT may vary between?

A

Idle EGT may vary from 320°C – 520°C depending on OAT, bleed configuration, and engine conditions

23
Q

A minimum of how long is required between engine start attempts?

A

10 seconds

24
Q

Accomplish the ABORTED ENGINE START checklist for one or more of the following conditions:

A
  • No N1 rotation before the engine start lever is raised to IDLE.
  • No oil pressure indication by the time the engine is stabilized at idle.
  • No increase in EGT within 10 seconds of raising the engine start lever to IDLE.
  • No increase in, or a very slow increase in N1 or N2 after EGT indication.
  • EGT rapidly approaching or exceeding the start limit.
25
Q

At what speed should the Autothrottle annunciation change to THR HLD?

A

By 84 knots

26
Q

More than how many units of control wheel deflection will cause the Spoilers to deflect which in turn affects take- off performance

A

1.5 units (10 degrees aileron)

27
Q

To increase tail clearance during strong crosswind conditions, consider using what if takeoff performance permits

A

A higher Vr

28
Q

At FL100 pressurization panel should read?

A

12:20pm

FL 200 should read 1:40pm

29
Q

If there is a level off on a SID at or below 3000 feet when should you bug up?

A

ALT ACQ

30
Q

Vertical Speed should not be used until when?

A

Flaps are up

31
Q

What height must you be above before setting STD

A

3000 feet

32
Q

When is standby altimeter set?

A

Above the MSA

33
Q

If there is a difference of more than 200 feet between capt and FO’s altimeter what should you do?

A

Split the difference

Use ALT HOLD

34
Q

Safety harnesses should be worn when?

A

Below FL100 and in turbulence

35
Q

Do we need to get encounters weather when weather is good?

A

No

36
Q

When should seats for landing be given?

A

6 miles to touchdown

37
Q

Requirements for a stabilized approach

A
  • correct speed or correcting if less than Vref or greater than Vref+20
  • vertical speed not more than 1000fpm
  • on profile and in landing configuration
  • N1 at an appropriate setting
38
Q

Calculating Fly Speed for landing use half headwind plus?

A

The entire gust

39
Q

To calculate crosswind use entire crosswind plus?

A

Half the gust

40
Q

Max Approach speed should not exceed?

A

Vref +20 knots
Or
Landing Flap placard speed minus 5 knots whichever is lower

41
Q

Second detent reverse thrust is approx?

Max reverse thrust is approx?

A

75% N1

82% N1

Command (12 decks)

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