FLIGHT PERFORMANCE AND PLANNING (P) - PPL Slovenia - PART 2

Generate an image of a light aircraft flying over a scenic landscape with a focus on flight performance metrics and planning charts, depicting clear skies and floating clouds.

Flight Performance and Planning Quiz

Test your knowledge on flight performance and planning with this comprehensive quiz designed for aviation enthusiasts and aspiring pilots.

  • 32 challenging questions
  • Covers various topics related to performance and planning
  • Ideal for PPL candidates
32 Questions8 MinutesCreated by FlyingFalcon32
510ft
550ft
565ft
585ft
920ft
950ft
1030ft
1180ft
510ft
765ft
1110ft
1850ft
510ft
520ft
530ft
545ft
565ft
850ft
935ft
1120ft
590ft
660ft
685ft
855ft
1265ft
1360ft
1850ft
1900ft
1125ft
1210ft
1970ft
2100ft
1385ft
1350ft
1320ft
1280ft
965ft
1140ft
1205ft
1445ft
1350ft
1555ft
1565ft
2945ft
104kts
110kts
115kts
120kts
19.7 USA gal.
16.0 USA gal.
15.1 USA gal.
12.0 USA gal.
14.9 USA gal.
15.3 USA gal.
18.6 USA gal.
22.7 USA gal.
2500 RPM
2400 RPM
2300 RPM
2200 RPM
5.7 USA gal/h
6.2 USA gal/h
5.8 USA gal/h
6.8 USA gal/h
Which forward speed is normally maintained, following an engine failure in flight in a light airplane or in a powered hang glider?
Best endurance speed.
Best glide speed.
Minimum rate of descend speed.
Minimum speed.
The forward speed for minimum rate of descent of an aircraft, compared with its best glide speed, is
Always higher.
Often higher
Always lower
Always lower
What should be done first, following an aircraft's engine failure in flight?
Carburetor heat must be applied
Move the mixture lever to position FULL RICH
Select a suitable field for forced landing.
Select the gliding attitude with best glide speed
An aircraft without an engine will fly the longest distance from a given altitude at the angle of attack at which
S parasite drag the least
Are induced drag and parasite drag equal.
Is parasite drag equal to lift coefficient.
Frost on the wings of an airplane may
Cause the airplane to become airborne with a lower angle of attack and at a lower indicated airspeed.
Make it difficult or impossible to become airborne.
Present no problem since frost will blow off when the aircraft starts moving during takeoff.
Change the camber (curvature of the wing) thereby increasing lift during takeoff.
What is the main danger arising out of even a slight amount of frost or snow on the wings and controls of an aircraft?
Decrease lift due to irregular airflow over the wings
Increased weight due to ice will increase stall speed
Ice and snow will jam control surfaces.
What is the headwind component for a landing on Runway 18 if the tower reports the wind as 220°/30 kts? (See figure12)
19kts
23kts
30kts
34kts
What is the crosswind component for a landing on Runway 18 if the tower reports the wind as 220°/30 kts?
19kts
23kts
30kts
34kts
06
14
24
32
06
14
24
32
15.5 kts headwind and 8 kts crosswind
15.5 kts headwind and 15 kts crosswind.
13.5 kts headwind and 24 kts crosswind.
7.5 kts headwind and 13 kts crosswind
18kts
25kts
29kts
35kts
20kts
18kts
15kts
12kts
13kts
16kts
18kts
20kts
5 kts headwind and 8 kts crosswind
10 kts headwind and 8 kts crosswind.
8 kts headwind and 4 kts crosswind.
8 kts headwind and 8 kts crosswind.
15 kts headwind and 10 kts crosswind
Zero headwind component; crosswind component 20 kts.
10 kts headwind and 15 kts crosswind.
20 kts headwind; zero crosswind componen
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