PPL checkride oral Canada Cartes | Quizlet

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165 Terms

1
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What makes a Certificate of Airworthiness invalid?

GLEAMS
Gross weight
Limitations
Exported
Airworthiness Directives (AD)
Maintenance

2
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When does the pitot static system needs a check?

Every two years

3
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What do you need to carry on a plane in terms of documents?

AROWJIL
Certificate of Airworthiness
Certificate of Registration
Pilot Operating Handbook
Weight & Balance
Journey Log
Insurance
Licences (Radio operators certificate, Medical, Pilot license of permit)

4
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What makes a Certificate of Registration invalid?

DEADS
Decommissioned
Exported
Address (change within 7 days)
Destroyed
Sold

5
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When do you check a new type ELT?

Refer to the manufacturer, doesn't need to be checked in the first 5 minutes of every UTC hour, as with an old style ELT.

6
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What does the Certificate of Registration tell you?

It gives the:
- nationality and registration mark
- aircraft manufacturer
- model and serial number
- the purpose (private, commercial)
- name and address of the owner
- owner registration date
- certificate issue date;
- and signature for the Minister of Transport.

7
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How long is the Certificate of Registration invalid? What invalidates it?

It remains valid as long as the ownership does not change or the owner's address does not change (and see DEADS = decommissioned, exported, address, destroyed, sold)

8
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For how long is the original Certificate of Airworthiness valid?

Indefinetely, or becomes invalid with GLEAMS (outside gross weight, outside limitations, exported, not complying to AD's and not maintaining the plane) or when in an accident

9
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How often must the Certificate of Airworthiness be re-validated?

Once a year

10
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How is a CoA revalidated?

By submitting an Annual Airworthiness Information Report

11
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Is a CoA issued for amateur-built aircraft?

No, amateur-built aircraft are issued a flight permit

12
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Define Basic Empty Weight

The Basic Empty weight includes:
- Weight of the standard airplane (airframe, engine, standard equipment and unusable fuel)
- All optional equipment
- Full oil

13
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Define maximum takeoff weight

The maximum weight approved for the start of the takeoff run

14
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How does the maximum takeoff weight differ from the maximum ramp weight?

The maximum ramp weight includes the fuel that will be used for start, taxi and run-up. Therefore, maximum takeoff weight will be less than maximum ramp weight.

Note: maximum ramp weight is usually not used for small aircraft

15
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Who prepares the Weight and Balance document that must be carried on board?

The W&B is prepared by the manufacturer

16
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What is the difference between normal and utility categories?

The utility category is solely for the purpose of training pilots in certain flight manoeuvres and, therefore, is usually subject to some restrictions.

In the normal category, maximum gross weight operations are permitted, but certain manoeuvres, such as spins and steep turns, are prohibited.

17
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Is an aircraft considered airworthy if overloaded? Why?

No, compliance with weight limitations is part of the airworthiness validity

18
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How often does an aircraft have to be re-weighed?

Aircraft must be re-weighed and an amended W&B Report produced if a change in weight of more than 2% of the empty weight has occurred, or if the weight change cannot be measured.

If the weight of the aircraft exceeds 12,500 lbs, it must be re-weighed every 5 years.

19
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What information is found on the W&B report that will not be found elsewhere?

The date of manufacture of the aircraft, the actual unusable fuel, the amount of full oil.

20
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Does the Journey Logbook have to be carried on board for each flight?

Yes, unless the pilot does not plan to land and shut down at a location other than the departure base.

21
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What is the difference between air time and flight time?

Air time is wheels up to wheels down (the actual time an aircraft is in the air)

Flight time is the moment an aircraft is moving on its own power.

22
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Are aircraft inspections based on air time or flight time?

Air time

23
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What type of inspection schedule is the aircraft on?

Refer to Journey Log (usually every 100 hours of air time and 50 hour intervals)

24
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If the inspection was due at 1,050 hours, can you fly the aircraft beyond that time? If yes, under what circumstances?

Yes, you can fly the aircraft, by a maximum of 10 hours, if an AME has given written confirmation of an extension in the Journey Logbook.

25
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How do you know that an annual inspections has been carried out?

The appropriate entry has been made in the Journey Logbook and an Annual Airworthiness Information Report has been completed.

26
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If a snag is reported in the Remarks section of the Journey Logbook, can you fly the aircraft? Is it airworthy?

No, unless an AME has checked it and signed it off (deferred)

27
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How do you correct an error in the Journey Logbook?

All errors should be corrected with a single line through them. The correct information should then be entered. Errors must never be erased.

28
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How often must the compass be swung?

Annually

29
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How do you verify that the compass has been swung?

Check the appropriate entry in the Journey Logbook

30
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1.33 When do you require an ELT?

An ELT is required on board at all times, unless the aircraft is operated within 25 NM of the departure aerdrome

31
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How often and by whom must the ELT be certified? Is an entry required in the Journey Logbook?

An ELT must be certified once per year, an entry must be made in the Journey Logbook

32
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For how long is an ELT battery good?

ELT batteries are good for two years from the date of manufacture

33
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At what time can you check if the ELT is operational?

First five minuted for no longer than 5 seconds in every UTC hour (old-style ELT). For new style ELT's, refer to manufacturer

34
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With respect to the Journey Logbook, what should you check before departing on a cross-country?

Check if the aircraft is airworthy, pay special attention to how much time is left on the aircraft until the next inspection and make sure that you will not exceed this time on your flight.

35
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When was the last inspection of the pitot-static system performed? How often should it be done?

It must be certified once every two years if the aircraft flies IFR or VFR in Class B

36
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Once a Journey Logbook has been completely filled, how long must it be retained?

For a period of not less then three years

37
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Using the Journey Logbook, demonstrate that the aircraft is airworthy?

a. Check if the maintenance inspection have been done
b. Check if the last air time entry against the next inspection due air time
c. check if compass was swung in the past year
d. Check if the ELT was certified within the past year
e. Check for snags
f. Check if the pitot-static system has been certified within the past two years

38
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What type of information can be found in the POH?

It has all the pertinent information for the make and model of the aircraft.

39
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How does the W&B information found in the pOH differ from the W&B Report for a particular aircraft?

The weight and balance information found in the POH is usually a generic example of that particular make and model.

40
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Lift the documents any flight crew member must carry on board while operatin an aircraft?

Licence or permit
Valid medical
Radiotelephone operators certificate

41
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What document tells you that a pilot licence is valid?

The medical

42
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What class of medical is required for a private pilot licence and for how long is it valid?

A category 3 medical is required. It is valid for 5 years up to 40 years of age, over 40 years of age it is valid for 2 years.

43
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When does your medical expire?

The medical expires on the first day of the month following the anniversary date. So medical from 3 march 2020 would be expired on 1 april 2025.

44
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What, in general terms, are the interception procedures? Where can you find them?

In the CFS, CARs and in the TC AIM

45
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Does proof of insurance for the aircraft have to be on board for each flight?

Yes, on all flights except for commercial aircraft

46
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Which documents lists the owner and the purpose of the aircraft?

The Certificate of Registration

47
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A fireproof plate bearing the aircraft registration must be affixed to the aircraft? Where is this plate located?

It is attached to the structure of the aircraft in a place where it is visible to a person on the ground

48
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The serial number of the aircraft is attached to the body of the aircraft. Where?

On the floor, under the pilot's seat

49
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Name the four sections of the Technical Logbook

- Airframe Log
- Propeller Log
- Engine Log
- Aircraft Modifications and ADs log

50
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May the Technical Logbook be carried on board the aircraft?

No, it must not be carried on board the aircraft at the same time as the Journey Logbook

51
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How long must Technical Logbooks be kept once they are full?

They must be kept until the aircraft is no longered registered.

52
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Should a Radio Station Licence be carried on board during flight?

No, not required for flights in Canada. However, a valid radio station is issued for international flights.

53
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What is the minimum instrumentation for day VFR flight?

MAATE
Magnetic Compass
Airspeed Indicator
Altimeter
Timepiece
Engine instruments (tachometer, oil pressure, oil temperature, fuel quantity)

Radiocomm when required.

54
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What is the minimum instrumentation for night VFR flight?

In addition to MAATE:
FATDAPPILOV
Fuses (spare)
Attitude Indicator
Turn coordinator
Directional gyro
Sensitive pressure altimeter
Pitot heat
Position lights and anti-collision lights
Instrument lights
Landing light (if carrying passengers)
OAT gauge
Vertical speed indicator

55
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How many minutes does 0.1 equal?

6 minutes

56
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What type of engine does your aircraft have? Describe it.

It is a 4-cylinder, horizontally opposed engine. It has 160 BHP. The engine is air cooled.

57
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What type of fuel and oil does it require?

100 Low lead, blue color.

58
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What is the minimum and maximum oil capacity?

Oil capacity is 6 QTS

59
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What is the total usable and unusable fuel?

40 gallons usable (3 gallons unusable) = 43 in total

60
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Describe (or draw) the fuel system of your aircraft?

The fuel system si gravity fed.

61
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Does the aircraft have a fuel pump?

No, some high wing aircraft do, but not this particular aircraft. All low-wing aircraft do have a fuel pump.

62
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If the fuel vent became blocked, what could happen?

Fuel starvation could occur. With no fuel, the engine will stop.

63
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What are the recommended tire pressures?

Main wheels: 29 psi
Nose wheel: 31 psi

64
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What type of flaps does your aircraft have?

Single-slotted flaps

65
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What type of ailerons does your aircraft have?

Differential ailerons

66
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Is your aircraft equipped with an elevator, or a stabilator?

Elevator

67
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Does the trim tab move in the same direction as the elevator, the stabilator or the anti-servo tab?

No, it does not move in the same direction as the elevator

68
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How does the cockpit heater system work?

A shroud around the exhaust muffler allows the air to be warmed before it is channeled into the cockpit.

69
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Of what does the winterization kit usually found on small aircraft consist? When should it be used?

It normally consists of two plates to partially cover the cowl nose cap opening, insulation for the engine crankcase breather line and a few placards. It should be installed when temperatures are below 7 degrees celsius.

70
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What are the maximum load factors for the test aircraft?

Normal category
Flaps-up: 3.8g, -1.52G
Flaps-down: 3.0g

Utility category
Flaps-up: 4.4g, -1.76g
Flaps down: 3.0g

71
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What does "maximum crosswind component" refer to?

It is the maximum crosswind for which adequate control of the aircraft has been demonstrated during takeoff and landing as part of the certification process.

72
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Determine the following for the flight test aircraft:
a. Voltage of the electrical system
b. Voltage of the battery
c. Ampere strength of the alternator
d. Ampere hours of the battery

Voltage of electrical system: 14V
Voltage of battery: 12 Volt
Ampere strength of alternator: 60amp
Ampere hours of battery: 25 amp hour battery

73
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How does the ammeter work?

The ammeter indicates the flow of current from the alternator to the battery or from the battery to the airplane electrical system.

The alternator is driven by a belt via the crankshaft.

74
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In the event of the ammeter showing a complete deflection to the right (an excessive rate of charge) and the voltage light illuminating, how would you handle this situation in flight?

Master switch -- OFF
Master switch -- ON
Over-voltage light -- OFF
If it illuminates again:
Flight -- TERMINATE

75
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If the ammeter was deflected to the left (an insufficient rate of charge) and the voltage light illuminated, how would you handle this situation in flight?

Alternator -- OFF
Nonessential Electrical Equipment -- OFF
Flight -- TERMINATE ASAP

76
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How can you determine a high/low; or over-voltage situation?

The red voltage light may either indicate an overcharging or undercharging situation. The ammeter will indicate which situation actually exists.

77
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In the event of a total electrical failure, how will it affect the magnetos?

It will not affect the magnetos at all.

78
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Name the pitot/static instruments

Altimeter, VSI, Airspeed indicator (pitot)

79
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Which pitot-static instrument(s) utilize the pitot tube? And which the static port?

Pitot = Airspeed indicator
Static = ASI, VSI, ALT

80
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If the pitot tube gets blocked, which instrument(s) will be affected? What about a static port blockage?

Pitot tube blockage: ASI
Static port blockage: ASI, VSI, ALT

In case the static port becomes blocked, you can use the alternate static source or break the glass case of the VSI.

81
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How will the airspeed indicator react to pitot tube blockage?

In a climb the ASI will over-read and in a descent, it will under-read

82
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How will the airspeed indicator react to static port blockage?

In a climb, the airspeed indicator will under-read and in a descent, over-read.

83
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How will the altimeter and VSI react to a pitot tube blockage? How will they react to a static port blockage?

Pitot tube blockage: not, as they are only connected to the static port

Static port blockage: altimeter will freeze at last reading
vsi will indicate "0" once the static air pressure has equalized.

84
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Name the gyroscopic instruments

Attitude indicator, Heading Indicator, Turn coordinator (or turn and slip indicator

85
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How are they powered?

They can either be powered electrically or powered by a vacuum pump driven off the engine.

86
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How do you know if the information from the gyro instruments is reliable?

Checking if the suction gauge is in the green
Checking that there are no flags on the instruments
Performing an instrument check during taxi

87
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Name the major sources of error on the heading indicator

Bearing friction and the earths rotation are the major sources of error on the HI

88
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How often must you reset the heading indicator? Under what conditions can you set it?

At least once every 15 mins

89
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Does the turn coordinator indicate the amount of bank?

No, the turn coordinator does not indicate the amount of bank. It shows rate of turn and roll.

90
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What is the inclinometer? How does it work?

It is used to measure the attitude of an aircraft relative to the horizontal. The inclinometer works on the principle of gravity.

91
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How do you lean the mixture for best economy cruise? For best power?

RPM at peak = max power
RPM decreasing = best economy (between rpm increasing and max power, peak)

92
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What is the danger of running the engine too lean?

It may cause overheating and detonation.

93
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When you apply carburetor heat, why do you get a decrease in performance?

Hotter - less dense air - is introduced into the mixture. The fuel-to-air ratio becomes richer, too rich for best performance. After carb heat hot, it is good practice to lean the mixture.

94
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How do you determine if carburetor icing is present?

You can determine carb icing by applying carb heat and watching the indications on the tachometer.

95
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In flight, you notice a drop in oil pressure and a rise in oil temperature. What can you expect?

Imminent engine failure

96
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During the engine run-up, you discover that the oil pressure gauge is inoperative. Can you depart anyway?

No, you need your engine instruments (MAATE).

97
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Quote from memory the following speeds: Vx (best angle, Vy (best rate), Vs, Vso, Va, Vg (best glide)

Vx = 60 (55 with flaps 10)
Vy = 70 (65 with flaps 10)
Vs = Lower end of green arc 47
Vso = Lower end of white arc 41
Va = 89 (at 1950), 97 (at gross weight)
Vg = 65

98
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In relation to the best rate of climb (Vy) and the best angle of climb speed (Vx), what is the normal climb speed?

Normal climb between 70 and 80.

Vx = best angle of climb = maximum altitude over given distance
Vy = best rate of climb = most altitude gain in a given period of time

99
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Define Vs

Stalling speed in the clean configuration

100
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What is the designation for the power off stalling speed with flaps up? How is it depicted on the airspeed indicator?

It is Vs and it is shown as the lower limit of the green arc (47 KIAS)