Performance Flashcards
The tailwind correction under the Runway Limits column of the Airport Analysis is “N/A.” This means that ____.
takeoff with a tailwind is not authorized on that runway
Your Dispatcher can provide you with automated contaminated runway corrections. Concerning these corrections, ____.
This system is outside of the TPS and cannot update data on the TPS printout.
When calculating new V-speeds from the Performance Manual, you notice V1 and rotation speeds are in the shaded area of the table. Before using these speeds, you should ____.
compare to VMCG and Minimum VR
Which of the following requires takeoff thrust at TO Max?
Improved Performance
TO1 and TO2 may not be used for takeoff above _____ feet pressure altitude.
6,000
When computing Runway Limited Maximum Landing Weight, a runway is considered wet when visibility is less than ___ mile.
3/4
The tailwind correction under the Runway Limits column of the Airport Analysis is “0.” This means that ____.
the maximum tailwind component is authorized with no weight adjustment required
Authorized flap settings for takeoff with TO thrust are ____ for a 777-200ER.
5, 15, 20
When operating on contaminated runways, in order to minimize takeoff V-speeds, use of Flaps ____ is recommended for 200ER.
15
A runway should be considered contaminated when more than __% of the required field length within the width being used is covered by standing water, slush, or wet snow more than __ inch deep.
25, 1/8
The V-speeds (V1, VR, V2) for TO2 given: PA 600 ft, 35°C, dry runway, Flaps 15, GWT 540.0, and winds L/V are ______________ on a 777-200ER.
146, 148, 152
Takeoff from a contaminated runway WILL NOT be accomplished ______________.
using improved performance
with a tailwind
with TO1 thrust
Climb limited landing weight must be reduced for ice accretion if moderate to severe icing will be encountered for at least 30 minutes duration, within the hour of flight prior to arrival, and the temperature at the arrival airport is _____ or colder.
10°C
Landing heavier than Maximum Quick Turn-Around Weight does not require a waiting period to determine if thermal plugs have not melted if the BRAKE TEMP advisory message is not displayed on EICAS ____ minutes after parking.
10 to 15
Charts to determine the Advisory Landing Distance in the event of an in flight failure of the antiskid system can be found in the ______________ .
QRH - Performance Inflight
After takeoff from Zurich in a cold clear morning, 0°C, and PA 3000’, an emergency requires an immediate return. For the 777-200ER, the Climb Limited Maximum Landing Weight is_____.
627.4
Operating in icing conditions, you have selected wing and engine A/I ON. Your forecasted landing temp is 0°C in moderate snow with PA 2000 ft. You anticipate 30 minutes holding in the weather in reported moderate icing. Based on this, for the 777-300ER, your Climb Limited Maximum Landing Weight is ____.
728.2
Improved performance uses a faster ____ which increases the climb capability of the aircraft and therefore increases the climb limited weight.
V2
The use of improved performance is not authorized on a contaminated runway.
True
At 500,000 lbs. gross weight and near the Equal Time Point on an ETOPS flight, one engine flames out and cannot be restarted. After offset and driftdown, what is your best 320 knot cruise altitude on a standard day on a 777-200ER?
FL 210
Near the Equal Time Point on an ETOPS flight, one engine flames out and cannot be restarted. After offset and driftdown and at a weight of 400,000 lbs. gross weight, the best 320 knot cruise altitude on a standard day is FL ____ on a 777-200ER.
230
At 540,000 lbs. gross weight and near the Equal Time Point on an ETOPS flight, one engine flames out and cannot be restarted. After offset and driftdown, the best 320 knot cruise altitude on a standard day is FL ____on a 777-300ER.
220
After driftdown, what altitude and airspeed could be maintained with one engine inop and the remaining engine at maximum continuous thrust with a gross weight of 500.0 and a temperature deviation of -5°C? (777-200ER)
25,600 ft/246 KIAS
After driftdown, what altitude and airspeed could be maintained with one engine inop and the remaining engine at maximum continuous thrust with a gross weight of 600.0 and a temperature deviation of -10°C on a 777-300ER?
25,600 feet/260 KIAS
