Pre-solo test

34 important questions on Pre-solo test

Tailwind and crosswind limitations for SOLO

  • Tailwind: 5 kts
  • Crosswind 10 kts
  • Max wind 25kts including gusts

Tailwind and crosswind limitations for DUAL

  • Tailwind: 5 kts
  • Crosswind: 25 kts
  • Max wind 35 kts including gusts

Green light signal

  • Cleared for take-off
  • Cleared to land
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Red light signal

  • Give way to other traffic and keep circling
  • Stop taxiing

Red flashing signal

  • AD unsafe do not land
  • Taxi clear of landing area in use

VFR planning minima

  • Min cloud base ceiling 2000ft
  • Min visibility 5km
  • Min flight altitude 1000ft AGL
  • No clouds below 500ft
  • 1000ft vertical and 1500m horizontal distance from cloud
  • No thunderstorms or icing conditions

Aft CG TB-10

Self correction minder effectief
Stalling speed decreased
Minimum (or no) nose down effect

Ice build-up on wing during flight

Land ASAP, maintain higher airspeed and make flapless landing

Approved fuel grades

  • 100LL Grade Aviation Fuel (Blue)
  • 100 Grade Aviation Fuel (Green)
  • UL91

High performance aircraft

>200HP

On what tank do you take-off

Take-off on tank used for run-up

VFR flight shall not be flown

  • Over congested areas of cities, towns or settlements or over an open air assembly of persons at a height less than 300m (1000ft) above the highest obstacle within a radius of 600m of the aircraft
  • Elsewhere than as specified above at a height less than 150m (500ft) above the ground or water

Pitot heat on ground limitation

3 minutes

Starter motor time limits

10 seconds on / 1 minute OFF
10 seconds on / 1 minute OFF
10 seconds on / 15 minutes OFF

Fuel tank draining

First flight of day and after tanking

First action after EFATE

Nose down

What do you check when you select take-off power during take-off

RPM en Manifold Air Pressure

What happens on solo flight

Faster towards Vr, higher rate of climb and more floating

What airspace classes in NL

ABCDEFG

Uphill or downhill terrain before the runway

  • Uphill slope creates illusion of being too high possibly inducing correction placing aircraft too low
  • Downhill slope creates illusion of being too low possibly inducing correction placing aircraft too high

Wide and short runway

Illusion of being too low

Integrated flight concept

Control aircraft by use of outside references supported by control instruments in order to maintain desired flight path. The flight path is checked on the performance instruments

Descent rate, angle and airspeed

Descent rate and angle are controlled by attitude.
Descent airspeed is controlled by engine power

Compass turns NH

Never see the North always see the South

Wake turbulence categories

Super heavy MTOW > 560000 kg
Heavy MTOW > 136000 kg
Medium MTOW >7000 <136000 kg
Light MTOW <7000 kg

Gyro vaccuum green sector

4,5 - 5,4 inch

Low fuel annunciation

Fuel lower than 6.6 USG

On final you see a red flare

Do not land, go-around and leave the circuit

Min visibility to fly circuit at Eelde

5km

Max flight level Amsterdam FIR for VFR

FL195

What do we set when flying in the circuit and VFR area

QNH

Loss of oil pressure

Propeller goes to fine pitch

Total electrical failure be aware off

Flaps unavailable
Radio unavailable
No lights

Hoogeveen circuit height

740ft AMSL 700ft AAL
Minimum approach altitude 1040ft AMSL (1000ft AAL)

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