1
Q
Fire in flight
A
Mixture ø Fuel ø Master ø Cabin Heat/Air ø Airspeed 100 Emergency Landing
2
Q
Electrical fire in flight
A
Master ø
All switches ø
Vents Air/Heat ø
Fire Extinguisher
After discharging Master ON Circuit CHECK Avionics ON Radio/Electrical ON Vents Air/Heat ON
3
Q
Fire in Cabin
A
Master ø
Vents Air/Heat ø
Fire Extinguisher
After discharging
Ventilate
Land ASAP
4
Q
Wing fire
A
Navigation Light ø Pitot heat ø Strobe light ø Sideslip Land ASAP
5
Q
Icing
A
"Pitot Heat ON Turn back/Altitude Cabin Heat FULL Throttle FULL Carb Heat AS REQ
Land
(nearest airport/ASAP)
6
Q
Balked Landing
A
Throttle FULL Carb Heat ø Flaps 20 Level until 55kt Flaps 10 Flaps ø @ 60
7
Q
Début vent arrière
A
Primer LOCKED Master ON Magnetos BOTH Carb Heat ON Mixture RICH Fuel BOTH Brake CHECK 2200 RPM
8
Q
Fin vent arrière
A
˜1800 RPM
Vi 70kts
Flaps 10
9
Q
Landing after icing
A
Stall Speed!! Wing Flaps ø Left Window OPEN Airspeed 65-75 Land Level
10
Q
Rule of thumb for Gusts and Approach speed
A
Add half of gust factor to approach speed.
e.g 10G30kt
Gust factor = 30/2 = 15
Approach speed + 15kt
11
Q
What is the Lift formula?
A
L = CL (1/2 ρV²) S
L = Resultant lift CL = Coefficient of Lift (determined by AoA and design of airfoil) ρ = Air density V = TAS S = Surface Area of the wing (modified by flaps)
12
Q
explain each parameter of
L = CL (1/2 ρV²) S
A
L = Resultant lift CL = Coefficient of Lift (determined by AoA and design of airfoil) ρ = Air density V = TAS S = Surface Area of the wing (modified by flaps)
13
Q
Does temperature affect TAS?
A
High temperature will increase TAS → higher roll for climb
PPL Canada
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