CPL/IFR Oral Flashcards
Seperation
Class C IFR Seperated from IFR and VFR
Class D IFR Seperated from IFR
Night VFR minima
Below 3000ft surface in sight clear of cloud
Minimum ceiling 1500ft
In mountainous areas 2000ft above highest obstical within 8km
1000ft above the highest obstical within 8km
Flight plan filed if leaving the vicinity of the aerodrome
2 way radio
Cav ok
Cloud base 5000ft or more, or no cloud below the MSA.
Visibility 10km or more
No siginificant weather
No CB or TCU
Special VFR
Ceiling above 600ft Vis greater than 1.5km Speed less than 140kt Day time only Clear of cloud When cleared by atc
ESB (engine start battery)
To prevent electrical surges to the avionics.
Charged from the left generator
Noise abaitment
Noise abaitment 1 800ft reduce thrust Keep flaps Climb vx 3000ft Retract flaps Increase thrust
Noise abatement 2
Retract flaps at 800ft
climb to 3000ft vy
Increase thrust and climb away
Critical engine
The Engines on the P2006 both rotate clockwise then been viewed from behind.
Due to the asymmetric blade effect (P-factor), the right-hand engine typically develops its resultant thrust vector at a greater lateral distance from the aircraft’s C.G. than the left-hand engine.
Therefore the left engine is the criticle one.
The downgoing blade is at a higher angle of attack than the upgoing blade.