TB10 POH

The pre-MOD TB10 wing span is?
8,40 meters
9,89 meters
10,64 meters
11,24 meters
Consider the two statements below:
1. Approved fuel grades for the TB10 are 100, 100LL and automotive gasoline.
2. Fuel tank capacity of the TB10 is 53,8 USG (usable).
Both statements are false
Both statements are correct
Statement 1 is correct, 2 is false
Statement 1 is false, 2 is correct
How does a 10kts tailwind affect the take-off run distance in the TB10?
 
At or below 10 kts wind speed the distance is not significantly affected
The take-off run should be expected to be 30% longer
The take-off run should be expected to be 10% longer
Not applicable. Take-off with tailwind is prohibited
After succesful engine start, the starter warning light stay illuminated. What is the first thing you do?
Wait for 30 seconds for the indicator to disappear
Mixture cut-off
Magnetos off
Pull bus 2 circuitbraker
After a successful engine start, a colleague outside the aircraft waves and indicates flames are coming from your engine compartment. What are your first actions?
Mixture idle, continue starting, throttle full open, fuel selector off
Fuel selector off, mixture idle, throttle full open, air conditioning vents fire cut-off
Switch off electrical power and evacuate aircraft immediately
Mixture idle, continue starting, throttle closed, fuel selector off
Upon arrival at your destination aerodrome with the TB10, you discover the flaps are no longer working. Do you make a mayday-call?
Yes, as this is a deviation from a normal landing
Yes, the risk of landing without use of flaps are significant and you want emergency services present
No, this is a non-normal situation but not an emergency
No, a pan pan call should be used for this situation
While at cruising altitude on a VFR flight in VMC, your alternator fails. How long is the battery of the TB10 expected to last, when properly maintained and after switching off non-essential items?
30 minutes
40 minutes
50 minutes
60 minutes
Maintenance should always be contacted after a:
1. Nose wheel landing
2. Suspected tail strike
3. Traversed landing
4. A bounced landing
1,2,3,4
1,2
1,2,4
2
Use of the flaps on the TB10 is subject to the following limitations:
1. Flaps may only be extended below 105 KIAS.
2. With flaps extended, airspeed may be allowed to increase up to maximum 122 KIAS (in smooth air).
Both statements are false
Both statements are correct
Statement 1 is correct, 2 is false
Satement 2 is correct, 1 is false
The blue handle controls the:
Carburettor heat
Mixture control
Throttle
Propeller control
Memory items on a checklist have to be:
Memorised so that the responses can be said on the do items on the checklist
Memorised only for a CPL exam
Checked before every flight
Known by heart
VFE is?
The upper limit of the green arc on the airspeed indicator
Maximum flap operating speed
Maximum flap extended speed
Maximum field elevation speed
The airspeed indicator needs input from?
The static port only
The pitot tube only
The GPS and the pitot tube
The pitot tube and the static port
The lower limit of the green arc on the airspeed indicator is?
V_s0
V_s1
V_NO
V_A
The final speed used for the TB10 for a normal landing (=speed 50ft above the runway)?
Is dependant on the aircraft weight upon landing
Is equal to 1,3 times V_SO
Is equal to V_S
Is a higher speed (exercise shedule) than speed in the POH
Which item is not found in the crashdrill?
Master switch off
Magnetos off
Doors unlatch
Fasten seatbelts
The highest stallspeed of the TB10 occurs:
With the most forward CG
When CG and aerodynamic centre are the same
When CG and CP are the same
With the most rearward CG
The engine doesn't drive the
Startmotor
Vacuuumpump
Alternator
Magneto's
Which statement is correct:
1. When using the alternate static port, open air outlets and set cabin air selector flow lever to open position.
2. The instrument error on the altimeter, when using alternate static air outlets and cabin air selector to open, is not significant.
Both statements are incorrect
Statement 2 is false and 1 is correct
Both statements are correct
Statement 1 is false and 2 is correct
During the initial take off you don't check:
The engine instruments
The advisory panel
The RPM and manifold pressure
The brake pressure
The pitch trim system is
Fully automated
A synchro servo sustem
Electrically actuated
A stabilator anti-tab
The lower limit of the white arc on the airspeed indicator is?
V_S0
V_NO
V_S1
V_A
When the parking brake annunciater light illuminates:
The brakes are used
The parking brake is on
The brake fluid is low
The brake system does not work
Use of external power can be found in?
SOP's
POH
Emergency checklist
TOM
Which of the following actions is part of a spin recovery?
Elevator briskly back
Ailerons opposite to direction of spin
Throttle fully open
None of the answers is true
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