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747 Memory Lists > Memory lists > Flashcards

Memory lists Flashcards

1
Q

Pulling Engine Fire Switches

A
  • closes the related engine and spar fuel valves
  • closes the related engine bleed air valve
  • trips off the related engine generator
  • shuts off hydraulic fluid to the related engine-driven hydraulic pump
  • depressurizes the related engine-driven hydraulic pump
  • arms both related engine fire extinguishers
    Rotate to A or B - discharges selected fire extinguisher into the engine nacelle.
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2
Q

FUEL CONTROL Switches
RUN to CUTOFF

A
  • closes fuel valves
  • removes igniter power
  • commands respective hydraulic demand pump to operate when Demand
    Pump selector in AUTO
  • unlocks Engine Fire switch
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3
Q

APU Fire Switch out

A
  • arms APU fire extinguisher bottle
  • closes APU fuel valve
  • closes APU bleed air valve
  • closes APU air inlet door
  • trips APU generator field and generator breaker
  • shuts down APU (if automatic shutdown does not occur)
    Rotate - discharges APU fire extinguisher into APU compartment.
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4
Q

Engine Fire switch is released when

A
  1. Fire detected
  2. Fuel Control Switch moved to cutoff
  3. Mechanical unlock button
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5
Q

Max doors wind limit

A

40 kt to operate
65 kt to leave open
Entry and cargo

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6
Q

APU altitude limits

A

Operates to 20,000
Electric and start on the ground only.
1 pack to 15,000

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7
Q

When will the speedbrakes go UP with lever in ARM?

A
  1. Ground sensed
    2.Thrust levers 1 and 3 near idle.
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8
Q

When will the speedbrakes go UP with lever in DN

A
  1. Ground sensed
  2. Thrust levers 1 and 3 near idle
  3. 2 & 4 in idle reverse
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9
Q

When will the Autobrakes operate with the switch in RTO

A
  1. Over 85 KTs GS
  2. All Thrust levers are closed
  3. Ground senses
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10
Q

Autobrakes on landing

A
  1. Ground sensed
  2. Thrust lever closed
  3. Wheels have spun up.
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11
Q

Wings span

A

64.9 M

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12
Q

Minimum width for 180 degrees turn

A

46.3 M

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13
Q

Minimum runway width

A

150 ft

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14
Q

Wheels span

A

12.6 M

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15
Q

Flaps 10 vs 20 T/O

A

10 - Higher T/O WT, less noise, wear and tear, less thrust required, Tail strik hazard
20 - FCTM default

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16
Q

Flaps 25 vs 30

A

25 - Less noise, wear and tear, speed margin
30 - Slower landing speed, shorter landing distance.

17
Q

Minimum T/O fuel

A
  1. 25,000
  2. 22,500 on PIC descretion on transit stop but no less the Required fuel
18
Q

Minimum landing Fuel/ Final Reserve

A

Greater of:
1. 3600 Kgs
2. 30 minutes holding fuel.

19
Q

Contingency Fuel

A
  1. 5% trip Fuel
  2. 3% with enroute alternate
  3. Maximum of 20 minutes cruise Fuel.
    or
    5 Holding fuel at 1500 ft
20
Q

When is Alternate required

A

Any time the destination is not ALM

21
Q

Disptach without alternate

A

1.Flight time less than 6 hours.
2. 2 seperate runways.
3. Ceilng minima + 1500 ft or 2000 ft
Visibility +3000 m or 5000 m

22
Q

When is enrout alternate required

A

The distance between departure and destination airports, or any of their alternates is such that
from any point on the planned route, the aircraft will be unable to reach one of these:
– While flying at altitude for depressurized flight, with critical fuel remaining; or
– The route includes a point further away from an adequate aerodrome at 60 minutes zero
wind flying time with all-engines operating LRC speed
2. It is required by Chapter 8.1.1.1 through Chapter 8.1.1.3 in order to meet one or two engine out
performance requirements.

23
Q

Minimum fuel VS mayday Fuel

A

Single aerodrome option to land with MLF VS landing with less than MLF

24
Q

Scan policy

A

Auto-flight - PF outside, PM instruments
Manual - PF intruments PM outside

25
Q

Stabilized approach

A
  1. The aircraft is on the correct flight path;
  2. Only small changes in heading/pitch are required to maintain the correct flight path;
  3. The aircraft speed is not more than target speed +20 kts indicated airspeed and not less than
    Vref;
  4. The aircraft is in the correct landing configuration;
  5. Power setting is appropriate for the aircraft configuration and is not below the minimum power
    for approach as defined in the respective OM Part B;
  6. All briefings and checklists have been conducted;
  7. ILS approaches must be flown within one dot of glide slope and localizer;
  8. Touchdown must be made within the touchdown zone.
    NOTE: Unique approach procedures or abnormal conditions requiring a deviation from the
    above elements of a stabilized approach require a special briefing.
    When the approach becomes unstabilized below 1,000 ft above airport elevation in IMC or below
    500 ft above airport elevation in VMC an immediate Go-Around is mandatory.
26
Q

Wind shear criteria

A

– Airspeed change of +/- 15 kts;
– Vertical speed change of 500 ft/min;
– Pitch change of more than 5°;
– Glideslope displacement of more than 1 dot;
– Abnormal power lever position for a significant period of time.

27
Q

When are the pack in high flow?

A
  1. Position of LLCCAFR
  2. Phase of flight
  3. Number of operating packs
    The system reconfigures automatically when one pack shutdown or fail
28
Q

Fuel System Management cards

A
  1. Closes x-feed 2&3 when flaps are extended for T/O on the ground.
  2. Opens X-feed 2&3 when flaps are out of range 10&20 settings.
  3. Opens reserve transfer valves when main tank 2 OR 3 fuel quantity approx 18,200 KG.
  4. With no fuel in the center wing tanks, activates override/Jettison pumps 2&3.
29
Q

Equipment Cooling Normal

A

Fan supplies cool cabin air to electrical equipment.
E&E exhaust routing depends on:
1. Ambient temp
2. LLCCAFR congif
3. FWD cargo compartment temp selector.

30
Q

Equipment Cooling EICAS

A

System is not configured for flight. Can be resolved by switching selector to STBY.

31
Q

Equipment Cooling STBY

A
  1. Ground exhaust valve closed
  2. Automatic control bypassed to configure system for flight; inboard
    exhaust valve open
  3. with a single internal fault, equipment inboard exhaust valve closes and
    cooling system reconfigures to allow internal closed loop recirculation
    of cooling air
32
Q

Equipment Cooling in Override

A
  • inboard exhaust valve closed
  • ground exhaust valve closed
  • equipment supply valve closed; cooling air supplied through flight
    panels
  • smoke/override valve open; differential pressure exhausts cooling air
    overboard

747 Memory Lists (3 decks)

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