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Limitations DHC-6-400

Beschreibung

It is vital to know the limitations of the aircraft that you are flying. How well do you know your Twin Otter limitations? Take the quiz to find out.
Rieul Gendron
Quiz von Rieul Gendron, aktualisiert more than 1 year ago
Rieul Gendron
Erstellt von Rieul Gendron vor fast 9 Jahre
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Zusammenfassung der Ressource

Frage 1

Frage
The minimum control speed in air (VMCA), flaps 10, is [blank_start]64[blank_end] KIAS, while the minimum control speed on ground (VMCG), flaps 10, is [blank_start]50[blank_end] KIAS.
Antworten
  • 64
  • 50

Frage 2

Frage
The best angle of climb speed (VX), flaps 0, is [blank_start]87[blank_end] KIAS. The best rate of climb speed (VY), flaps 0, is [blank_start]100[blank_end] KIAS. The best single-engine rate of climb speed (VYSE), flaps 10, is [blank_start]80[blank_end] KIAS.
Antworten
  • 87
  • 100
  • 80

Frage 3

Frage
The maximum flaps extended speed (VFE) for flaps 10 is [blank_start]103[blank_end] KIAS, whereas for greater than flaps 10, it is [blank_start]93[blank_end] KIAS.
Antworten
  • 103
  • 93

Frage 4

Frage
State the maximum operating speed (VMO) for the following altitudes: Sea level to 6,700 feet: [blank_start]166[blank_end] KIAS 10,000 feet: [blank_start]156[blank_end] KIAS 15,000 feet: [blank_start]141[blank_end] KIAS 20,000 feet: [blank_start]126[blank_end] KIAS 25,000 feet: [blank_start]112[blank_end] KIAS
Antworten
  • 166
  • 156
  • 141
  • 126
  • 112

Frage 5

Frage
The maneuvering speed (VA) between sea level and 18,000 feet is [blank_start]132[blank_end] KIAS and the gust penetration speed (VB) between sea level and 18,000 feet is [blank_start]132[blank_end] KIAS.
Antworten
  • 132
  • 132

Frage 6

Frage
On the airspeed indicator, there is a red horizontal line. This represents the [blank_start]minimum control speed in air[blank_end]. On the airspeed indicator, there is also a blue horizontal line. This represents the [blank_start]best rate of climb speed, single engine[blank_end].
Antworten
  • minimum control speed in air
  • minimum control speed on ground
  • maximum operating speed
  • maximum flaps extended speed
  • best rate of climb speed, single engine
  • best rate of climb speed, two engines
  • minimum control speed in air
  • minimum control speed on ground

Frage 7

Frage
On the airspeed indicator, the barber pole represents the [blank_start]maximum operating speed[blank_end]. On the other hand, the bottom of the red vertical tape represents the [blank_start]maximum flaps extended speed[blank_end].
Antworten
  • maximum operating speed
  • stall speed in the clean configuration
  • stall speed in the landing configuration
  • maximum flaps extended speed
  • maximum flaps extended speed
  • minimum flaps extended speed
  • stall speed in the landing configuration
  • stall speed in the clean configuration

Frage 8

Frage
On the airspeed indicator, the top of the thermometer tape represents the [blank_start]stall speed in the landing configuration[blank_end].
Antworten
  • stall speed in the landing configuration
  • stall speed in the clean configuration
  • landing reference speed
  • approach speed

Frage 9

Frage
Select the correct limits for the following table.
Image:
Limitations Blank (binary/octet-stream)
Antworten
  • 45
  • 48.5
  • 50
  • 68.4
  • 52
  • 740
  • 765
  • 790
  • 795
  • 1090
  • 685
  • 740
  • 765
  • 790
  • 1090

Frage 10

Frage
Select the correct limits for the following table.
Image:
Limitations Blank (binary/octet-stream)
Antworten
  • 660
  • 685
  • 740
  • 765
  • 101.6
  • 102.6
  • 91
  • 110
  • 91
  • 96
  • 110
  • 101.6

Frage 11

Frage
Select the correct limits for the following table.
Image:
Limitations Blank (binary/octet-stream)
Antworten
  • 740
  • 765
  • 790
  • 685
  • 740
  • 765
  • 790
  • 1090
  • 90 to 92
  • 94 to 96
  • 98 to 100

Frage 12

Frage
Select the correct limits for the following table.
Image:
Limitations Blank (binary/octet-stream)
Antworten
  • 40 MIN
  • -40 to 99
  • 0 to 99
  • 10 to 99
  • 85 to 105
  • 40 MIN
  • -40 to 99
  • -40 MIN
  • 0 to 40
  • -40 MIN
  • 40 MIN
  • 0 to 99
  • 10 to 99
  • -40 to 99
  • 0 to 99
  • 10 to 99
  • 40 to 99
  • -40 MIN
  • 40 MIN
  • 0 to 99
  • 10 to 99

Frage 13

Frage
Unintentional, momentary pilot errors that result in torque settings between 50 and 61 PSI torque during two engine operations are harmful to the engine.
Antworten
  • True
  • False

Frage 14

Frage
At idle, if the T5 temperature approaches the 685 degrees Celsius idle limit, either [blank_start]increase[blank_end] NG or [blank_start]reduce[blank_end] engine loads to stay below the idle temperature limit.
Antworten
  • increase
  • decrease
  • reduce
  • increase

Frage 15

Frage
How long is reverse power operation limited to?
Antworten
  • 2 seconds
  • 25 seconds
  • 60 seconds
  • 120 seconds

Frage 16

Frage
Select all those that apply when the following conditions are met: Ground running of engines (except during maneuvering or taxiing) in ambient temperatures of 32 degrees Celsius and above.
Antworten
  • Aircraft must be headed into wind
  • Operation in other than forward thrust must be kept to a minimum
  • Operation in other than forward thrust must not exceed one minute
  • Operation in other than forward thrust must not exceed two minutes
  • Aircraft must be headed perpendicular to wind
  • Operation of the power levers aft of the idle stop is forbidden

Frage 17

Frage
In-flight operation of the power lever aft of idle is prohibited.
Antworten
  • True
  • False

Frage 18

Frage
Starting temperatures above [blank_start]850[blank_end] degrees Celsius are undesirable and should be reported and investigated for cause.
Antworten
  • 850

Frage 19

Frage
For engine start, temperatures between 980 and 1090 degrees Celsius are acceptable provided the temperature decreases to below 980 degrees Celsius within [blank_start]2[blank_end] second(s).
Antworten
  • 2
  • 1
  • 4
  • 10
  • 25

Frage 20

Frage
Propellers must be set to MAX RPM for every takeoff and every landing.
Antworten
  • True
  • False

Frage 21

Frage
Propeller levers must be set to the MAX RPM position no later than [blank_start]500[blank_end] feet above [blank_start]ground level[blank_end] for visual approaches. Propeller levers must be set to the MAX RPM position no later than [blank_start]500[blank_end] feet above [blank_start]minimum descent altitude (MDA)[blank_end] for instrument approaches.
Antworten
  • 500
  • 1000
  • 200
  • ground level
  • sea level
  • minimum descent altitude (MDA)
  • 500
  • 1000
  • 2000
  • 200
  • minimum descent altitude (MDA)
  • ground level
  • sea level
  • airfield elevation

Frage 22

Frage
In an emergency when jet fuel is not available, any grade of AVGAS may be used, but only at specific mixture ratios.
Antworten
  • True
  • False

Frage 23

Frage
What is the maximum fuel temperature and maximum ambient temperature for takeoff when using AVGAS?
Antworten
  • 20 degrees Celsius
  • 25 degrees Celsius
  • 30 degrees Celsius
  • 35 degrees Celsius

Frage 24

Frage
What is the maximum operating altitude when using AVGAS?
Antworten
  • 8,000 feet
  • 10,000 feet
  • 12,000 feet
  • 15,000 feet

Frage 25

Frage
At least one boost pump per tank must be serviceable at all times when AVGAS is being used.
Antworten
  • True
  • False

Frage 26

Frage
Text sometimes appears outboard of the torque indicators on the primary flight display during various phases of flight. Select the correct indication for each phase by completing the table.
Image:
Indication Table (binary/octet-stream)
Antworten
  • T/O (white)
  • T/O (green)
  • No indication is shown
  • T/O (white)
  • T/O (green)
  • No indication is shown
  • CLMB (white)
  • S/E (white)
  • S/E (green)
  • T/O (white)
  • IDL (white)
  • IDL (green)
  • No indication is shown
  • START (white)
  • START (green)
  • IDL (white)
  • IDL (green)
  • OFF (white)
  • OFF (green)
  • IDL (white)

Frage 27

Frage
If a blue colour appears on the engine parameters NP display, what is this telling the pilot?
Antworten
  • The propeller operation is locked in beta range (abnormal)
  • The propeller operation is in beta range (advisory)
  • The NP value is out of the normal range for this phase of flight (abnormal)
  • The prop lever is not in the minimum governing position

Frage 28

Frage
When a generator is capacity-limited, the maximum load reading is
Antworten
  • 50 amps
  • 100 amps
  • 160 amps
  • 200 amps

Frage 29

Frage
What is suggested to prolong generator life?
Antworten
  • Engine RPM below 59% NG should be avoided, especially at high OAT (>15 degrees Celsius) and high current generator loads (>100 Amps).
  • Engine RPM above 55% NG should be avoided, especially at high OAT (>32 degrees Celsius) and high current generator loads (>100 Amps).
  • Engine RPM below 59% NG should be avoided, especially at high OAT (>15 degrees Celsius) and low current generator loads (<100 Amps).
  • Engine RPM below 55% NG should be avoided, especially at high OAT (>30 degrees Celsius) and high current generator loads (>200 Amps).

Frage 30

Frage
If extended engine operation at low RPM is necessary under high current loads, what is suggested be done? Select ALL possible suggested actions.
Antworten
  • Shed unnecessary electrical loads
  • Switch off one generator
  • Switch off both generators
  • Feather one propeller
  • Feather both propellers
  • Set power levers to idle

Frage 31

Frage
What is meant by cross-generator starting?
Antworten
  • Starting one engine while the generator of the other running engine is online and producing power.
  • Starting an engine while its generator is online.
  • Starting one engine while the generators of both engines are online.
  • Starting one engine while the generator of the other running engine is offline.

Frage 32

Frage
Cross generator starting is forbidden under all circumstances.
Antworten
  • True
  • False

Frage 33

Frage
What action must be taken following a cross generator start?
Antworten
  • The cross generator start must be recorded in the aircraft logs.
  • No action needs to be taken.
  • Switch off the generator of the engine that was initially running, and then switch it back on after 5 seconds.
  • Reduce the power on the engine that was initially running.

Frage 34

Frage
The starter duty cycle limitations are: [blank_start]25[blank_end] second(s) ON, [blank_start]1[blank_end] minute(s) OFF, then [blank_start]25[blank_end] second(s) ON, [blank_start]1[blank_end] minute(s) OFF, then [blank_start]25[blank_end] second(s) ON, followed by a [blank_start]30[blank_end] minute(s) cooling period.
Antworten
  • 25
  • 10
  • 15
  • 30
  • 1
  • 10
  • 25
  • 30
  • 25
  • 10
  • 15
  • 30
  • 1
  • 2
  • 25
  • 30
  • 25
  • 10
  • 50
  • 30
  • 30
  • 1
  • 5
  • 25

Frage 35

Frage
What is the maximum operating altitude of the DHC-6-400 according to the POH?
Antworten
  • 10,000 feet
  • 15,000 feet
  • 20,000 feet
  • 25,000 feet
  • 27,500 feet

Frage 36

Frage
Fill in the blanks using numbers only; do not use spaces or commas. The maximum takeoff weight is [blank_start]12500[blank_end] lbs. The maximum ramp and taxi weight is [blank_start]12600[blank_end] lbs. The maximum landing weight is [blank_start]12300[blank_end] lbs. The maximum zero fuel weight is [blank_start]12300[blank_end] lbs.
Antworten
  • 12500
  • 12600
  • 12300
  • 12300

Frage 37

Frage
Fill in the blanks using numbers only; do not use spaces or commas. The maximum permissible baggage compartment load for the forward baggage compartment is [blank_start]285[blank_end] lbs. The maximum permissible baggage compartment load for the aft baggage compartment is [blank_start]500[blank_end] lbs, which includes the [blank_start]150[blank_end] lbs limit on the extension shelf.
Antworten
  • 285
  • 500
  • 150

Frage 38

Frage
The maximum permissible baggage compartment load for the lower portion of the aft baggage compartment (i.e., the area NOT on the shelf) is 350 lbs.
Antworten
  • True
  • False

Frage 39

Frage
Fill in the blanks using numbers only; do not use spaces or commas. The maximum permissible floor loading value for the forward and rear baggage compartments is [blank_start]100[blank_end] pounds per square foot, whereas for the cabin it is [blank_start]200[blank_end] pounds per square foot.
Antworten
  • 100
  • 200

Frage 40

Frage
Select all that apply. The approved flap takeoff setting(s) is/are:
Antworten
  • 0
  • 10
  • 20
  • 37

Frage 41

Frage
Select all that apply. For normal operations, the approved flap landing setting(s) is/are:
Antworten
  • 0
  • 10
  • 20
  • 37

Frage 42

Frage
Choose the correct answer. At a gross weight of 12,500 lbs and flaps RETRACTED, the flight load factors to which the DHC-6 airplane has been designed are (normal category):
Antworten
  • +3.17g to -1.5g
  • +2.0g to -1.5g
  • +1.5g to -3.17g
  • +1.5g to -2.0g

Frage 43

Frage
Choose the correct answer. At a gross weight of 12,500 lbs and flaps EXTENDED, the flight load factors to which the DHC-6 airplane has been designed are (normal category):
Antworten
  • +2.0g to -1.5g
  • +3.17g to -1.5g
  • +1.5g to -3.17g
  • +3.17g to -2.0g

Frage 44

Frage
Select ALL that apply. The Twin Otter is certified in the Normal Category. Accordingly, the following are NOT approved:
Antworten
  • Spins
  • Lazy eights
  • Chandelles
  • Turns with an angle of bank exceeding 45 degrees
  • Turns with an angle of bank exceeding 60 degrees
  • Stalls

Frage 45

Frage
Take-off is always prohibited with any red or amber CAS message present.
Antworten
  • True
  • False

Frage 46

Frage
Engine start is prohibited if the Hydraulic Power Fail CAS message is present.
Antworten
  • True
  • False

Frage 47

Frage
Regarding TCAS I, The flight crew must NOT use a TA on the PFD traffic display to initiate evasive maneuvering as it lacks the resolution necessary for use in evasive maneuvering.
Antworten
  • True
  • False

Frage 48

Frage
Pilots are authorized to deviate from an ATC clearance when responding to terrain or obstacle alerts generated by the TAWS.
Antworten
  • True
  • False

Frage 49

Frage
It is acceptable to navigate based on TAWS terrain data on the Primary Flight Displays.
Antworten
  • True
  • False

Frage 50

Frage
Select all that apply. The following limitations apply when the weather radar system is operated while the aircraft is on the ground:
Antworten
  • Do not operate the weather radar system during aircraft refuelling.
  • Do not operate the weather radar system when any refuelling operations are being carried out within 100 feet (30 m).
  • Do not operate the weather radar system when personnel are standing forward of the wings within 30 feet (10 m) of the aircraft.
  • Do not operate the weather radar system when personnel are standing behind the wings within 30 feet (10 m) of the aircraft.

Frage 51

Frage
Dispatch of the aircraft with any equipment inoperative is only permitted in accordance with:
Antworten
  • the guidance provided in an operator-specific Minimum Equipment List (MEL) that is derived from the MMEL (Master Minimum Equipment List).
  • the guidance provided in the MMEL (Master Minimum Equipment List) that is derived from an operator-specific Minimum Equipment List (MEL).
  • the guidance provided in an operator-specific Minimum Equipment List (MEL) or the MMEL (Master Minimum Equipment List).

Frage 52

Frage
A Minimum Equipment List (MEL) may be more restrictive than the Master Minimum Equipment List (MMEL).
Antworten
  • True
  • False
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