General CPL Questions Flashcards

1
Q

What specification of aircraft fly in accordance of Subpart H (Performance Class B)?

A
  • Propeller driven aircraft - Maximum approved passenger seating arrangement of 9 or less - Maximum take-off weight of 5700kg or less
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2
Q

What are the requirements for an aircraft to be dispatched?

A

A) The landing mass at the estimated time of landing allows a full stop landing, from 50ft above the threshold, within 70% of LDA B1) It must also be assumed that the aeroplane will land on the most favourable R/W in still air AND B2) The aeroplane will land on the R/W most likely to be assigned considering probable wind direction and speed as well as the ground handling characteristics of the AC and the available nav aids and terrain - If the operator is unable to comply with B2 for the destination aerodrome then it may only be dispatched if an alternate aerodrome is designated which permits A through B2

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3
Q

What is the definition of a Clearway?

A
  • An area which may be provided at the end of the TORA (in the direction of take off) which is free of any obstacles that could cause a hazard to aeroplanes in flight - It extends 75m either side of the R/W centre line - It extends out to the first non-frangible object to a maximum of 50% of the TORA
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4
Q

What is the definition of a Stopway?

A
  • An obstacle free rectangular area at the end of a runway - At least as wide as the R/W - Must be prepared such that an AC can roll over it without hazard to itself or its occupants
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5
Q

When do you need a T/O alternate?

A

Take off alternate :- Required if it would not be possible to return to the aerodrome of departure for performance or meteorological reasons. Alternate requirements:- Two engined a/c – must be within one hours flight time at one engine cruising speed. Planning minima :- Weather reports or forecasts for a period of one hour before and after estimated time of arrival at take off alternate must be at or above the applicable landing minima. If the only available approaches are non-precision the ceiling shall be taken into account.

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6
Q

When do you need destination alternate

A

a)When weather reports or forecasts one hour before and after the expected arrival time at destination are below applicable planning minima, or, b)No meteorological information is available for destination

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7
Q

If there are no performance TO factors in the AFM, what factors do you use for TO and LDG?

A

Additional Factors

  • Take off (if no information in AFM)
    • Short Dry Grass1.2 x TODR
    • Short Wet Grass1.3 x TODR
    • SOFT Ground - 1.25+ x TODR
  • Landing - (if no information in AFM)
    • Short Dry Grass1.15 x LDR
    • Short Wet Grass1.35 x LDR
    • SOFT Ground - 1.25+ x LDR
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8
Q

Portuguese night definition (for night flight)?

A

Sunset plus 25 minutes and Sunrise minus 25 minutes

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9
Q

What is Vs1

A

Stalling Speed, or the minimum continuous speed at which the airplane is still
controllable with flaps and landing gear retracted.

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10
Q

What is Vs0

A

Stalling Speed, or the minimum continuous speed at which the airplane is still
controllable in the landing configuration.

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11
Q

What is Vs

A

Stalling Speed, or the minimum continuous speed at which the airplane is still
controllable in the given configuration.

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12
Q

Vsse

A

Minimum Control Speed for Schooling. Minimum speed necessary in case of
one engine intentionally inoperative / idle (training purposes).

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13
Q

Definition of empty mass

A

The mass of the airplane including unusable fuel, all operating fluids and
the maximum quantity of oil.

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14
Q

Maximum landing mass definition according to DA42 AFM?

A

The highest mass for landing conditions at the maximum descent velocity.
This velocity was used in the strength calculations to determine the
landing gear loads during a particularly hard landing.

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15
Q

Definition of useful load

A

The difference between take-off mass and empty mass.

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16
Q

CPL Requirements: Age? Medical? Hours?

A

18 yrs

Class 1 Medical

150 hrs intergrated

Pass CPL test

Pass 14 ATPL exams

17
Q

With a CPL the pilot may act as:

A
  1. PIC or co-pilot in any ops except air transport
  2. PIC of single pilot commercial ops
  3. Co-pilot in commercial air transport ops
18
Q

Recent experience to maintain CPL: Day? Night?

A

Day: 3 T/O, app. and landing in same type or class in preceding 90 days

Night: 1 T/O, app. and landing at night and hold IR rating

19
Q

Steady Green in AIR

A

Cleared to land

20
Q

Steady green on GROUND

A

Cleared take off

21
Q

Steady red in AIR

A

Give way to other aircraft

22
Q

Steady red on GROUND

23
Q

Green flashes in AIR

A

Return for landing, clearance to land given in due course

24
Q

Green flashes on GROUND

A

Cleared taxi

25
Red flashes in AIR
Aerodrome unsafe don’t land
26
Red flashes on GROUND
Taxi clear of landing area
27
White flashes in AIR
Land at this aerodrome after receiving clearance and taxi to apron
28
White flashes on GROUND
Return to starting point on airfield
29
Red and green flashes in AIR & on GROUND
Danger be on alert
30
Red pyrotechnics (AIR only)
Regardless of previous instructions do not land until advised
31
Describe the TEM model
* structured method of dealing with potential hazards * all about identifying threats and errors, and managing them to ensure a safe outcome to the flight. **Threat** * any situation, which occurs outside your influence as the pilot, which might pose a hazard to the flight **Error** * An error is any situation, which occurs due to an action or in-action by you as the pilot **Managing** * **Avoid** * **Trap** * **Mitigate**
32
What is the definition of Vmc?
As for Vmca, but * Actual conditions of the day * Any other weight & CG position * STRENGTH & SKILL OF PILOT!
33
What is ACA?
Asymmetric Committal Altitude (ACA): the lowest altitude from which a light multi-engine aircraft can make a successful go-around when asymmetric, whether IMC or VMC.
34
What is EOA?
Engine Out Allowance (EOA): the height needed for the transition from descending to climbing flight when asymmetric. The engine out allowance is added to the decision altitude on a precision approach when asymmetric and should be considered when determining when to initiate go-around when carrying out a non-precision approach using a notional glidepath technique
35
EASA EU OPS (Air-OPS). What are the requirements for Perf Class B - MEP for the Take off climb?
(a) Take-off climb * **AEO** * **at least 4 %** with: * take-off power on each engine; * the landing gear extended, except that if the landing gear can be retracted in not more than seven seconds, it may be assumed to be retracted; * flaps in the take-off position(s) * climb speed not less than the greater of 1,1 VMC (minimum control speed on or near ground) and 1,2 VS1 (stall speed or minimum steady flight speed in the landing configuration). * **OEI** * at an altitude of **400 ft above the take-off surface** shall be **measurably positive** with: * the critical engine inoperative and its propeller in the minimum drag position; * the remaining engine at take-off power; * the landing gear retracted; * the wing flaps in the take-off position(s); and * a climb speed equal to that achieved at 50 ft. * shall be **not less than 0,75 % at an altitude of 1 500 ft** above the take-off surface with: * the critical engine inoperative and its propeller in the minimum drag position; * the remaining engine at not more than maximum continuous power; * the landing gear retracted; * the wing flaps retracted; and * a climb speed not less than 1,2 VS1.
36
EASA EU OPS (Air-OPS). What are the requirements for Perf Class B - MEP for the Landing climb?
* AEO * at least 2,5 % with: * not more than the power or thrust that is available eight seconds after initiation of movement of the power controls from the minimum flight idle position; * the landing gear extended; * the wing flaps in the landing position; and * a climb speed equal to VREF (reference landing speed). * OEI * not less than 0,75 % at an altitude of 1 500 ft above the landing surface with: * the critical engine inoperative and its propeller in the minimum drag position; * the remaining engine at not more than maximum continuous power; * the landing gear retracted; * the wing flaps retracted; and * a climb speed not less than 1,2 VS1.