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GIVEN:
pressure alt- 6,000ft
temperature- +3C
power- 2,200RMP -22" MP
usable fuel available- 465 lb
what is the maximum available flight time under the giventerm-36 conditions? - ✔✔6
hours 39 minutes
The performance tables of an aircraft for takeoff and climb are based on -
✔✔pressure/density altitude
density altitude is the vertical distance above mean sea level in the standard
atmosphere which - ✔✔a given atmospheric density is to be found
To determine pressure altitude prior to takeoff, the altimeter should be set to - ✔✔29.92
HG and the altimeter indication noted
at higher elevation airports the pilot should know that indicated airspeed - ✔✔will be
unchanged but groundspeed will be faster
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,as air temperature increases, density altitude will - ✔✔increase
GIVEN:
pressure altitude-12,000ft
true air temperature- +50F
from the conditions given, the approximate density altitude is - ✔✔14,130ft
GIVEN:
pressure altitude-5,000ft
true air temperature- +30C
from the conditions given, the approximate density altitude is - ✔✔7,800ft
GIVEN:
pressure altitude-6,000ft
true air temperature- +30F
from the conditions given, the approximate density altitude is - ✔✔5,500ft
GIVEN:
pressure altitude-12,000ft
true air temperature- +15F
from the conditions given, the approximate density altitude is - ✔✔11,900ft
GIVEN:
pressure altitude-7,000ft
true air temperature- +15C
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, from the conditions given, the approximate density altitude is - ✔✔8,500ft
what effect does an uphill runway slope have on takeoff performance - ✔✔increase
takeoff distance
GIVEN:
temp- 30F
pressure alt- 6,000ft
weight- 3,300lb
headwind- 20kts
what is the total takeoff distance over a 50-foot obstacle - ✔✔1,500ft
GIVEN:
temp- 100F
pressure alt- 4,000ft
weight- 3,200lb
headwind- calm
what is the ground roll required for takeoff over a 50-foot obstacle - ✔✔1,350ft
GIVEN:
temp- 50F
pressure alt- 2,000ft
weight- 2,700lb
headwind- calm
what is the total takeoff distance over a 50-foot obstacle - ✔✔800ft
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