PERFORMANCE Flashcards

1
Q

What is the MACTOW CG to use Alternate CG on the OPT for pax and freighter?

A
  • Pax - 26%
  • Freighter - 28%
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2
Q

When is the Assumed Temperature not authorized?

A
  • Alternate EEC mode operation;
  • Contaminated Runways;
  • Potential Windshear conditions exist;
  • At pilots discretion full thrust can be used.
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3
Q

The Commander may request a new OFP if the ZFW changes by…

A

2.0 tons or more.

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4
Q

All weights including fuel may be amended (LMC). The LMC limit for an individual LMC or total LMC shall be:

A

500 kg

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5
Q

After a LMC it is mandatory to check the following:

A
  1. ZFW, TOW and LW limits are not exceeded (Structural and Performance);
  2. Take-off performance calculations are validated using the revised TOW and TOWOCG;
  3. Loading limitations are not exceeded.
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6
Q

What should be done if the LMC is greater than 500 kg?

A
  • New ACARS or computer loadsheet required;
  • In case of a manual loadsheet, ament loadsheet figures and issue a new trim sheet.
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7
Q

Taxi fuel consumption:

A

2400 kgs/hr (rule of thumb)

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8
Q

Maximum taxi speed

A
  • 30 kts
  • 10 kts - for slippery surface

Crew may exceed these limits when backtracking on an active runway.

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9
Q

Minimum width of runway

A

45 meters.

Unless a specific airport risk assessment has been carried out and reflected in either the CCI page or a briefing package, where applicable.

For contaminated runways: 30 meters

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10
Q

Aircraft ICAO and FAA codes for Taxi limitations

A
  • ICAO: E
  • FAA: V
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11
Q

Best Rate of Climb Speed

A
  • Flaps UP maneuver speed + 60 knots until intercepting M .82; or
  • Vref 30 + 140 knots
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12
Q

Best Angle of Climb Speed

A

On VNAV CLIMB page of the FMC

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13
Q

Aircraft Approach Categories

A

777-200 - C (D for circling)

777-300ER & 777-F - D

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14
Q

Standby Fuel

A

3 tons below flight plan fuel

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15
Q

APU Fuel Burn

A
  • Ground Consumption - 240 kg/hour;
  • In-flight Consumption - +2.5% for the APU Door being open and 90 kg/hour.
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16
Q

Fuel Uplift Check

A
  • Actual Uplift - Calculated Uplift = Uplift Difference (Tolerence +2.000kg, -1.000kg)
  • Uplift Difference : Calculated Uplift = % Difference Tolerance ±5%
17
Q

Jettison Rates

A
  • Center Tank Fuel - 2,500 kg/min
  • No Center Tank Fuel - 1,400 kg/min
  • 2/3 of Jettison Fuel = Time in minutes (Rule of Thumb)
18
Q

Maximum Tire Speed

A

Takeoff - 204 knots

Landing - 226 knots

Ref.: B777 AFM