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Zlin 242L > Flight Manual > Flashcards

Flight Manual Flashcards

1
Q

What’s the Maximum continuous (MCP) engine power - speed - consumption?

A

149 kW or 200 HP - power
2700 RPM - speed
61 l/h - consumption

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2
Q

What’s the Cruising PC (75% MCP) engine power - speed - consumption?

A

112 kW or 150 HP - power
2450 RPM - speed
46,5 l/h - consumption

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3
Q

What’s the Economy EC (65% MCP) engine power - speed - consumption?

A

94 kW or 126 HP - power
2350 RPM - speed
40 l/h - consumption

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4
Q

what’s the Best Economy BE (65% MCP) engine power - speed?

A

86 kW or 115 HP - power
2350 RPM - speed
32 l/h - consumption

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5
Q

What’s the total and usable capacity of fuel?

A

Total - 230 l
Usable - 224 l

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6
Q

What is the recommended inlet oil temperature with outside temperatures of:
-1C to +32C?

A

80C and max 180C

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7
Q

What is the recommended inlet oil temperature with outside temperatures of -18C to +21C?

A

77C and max 170C

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8
Q

What is the recommended inlet oil temperature with outside temperatures of under -12C?

A

71C and max 160C

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9
Q

What are the dimensions of the wingspan of the Zlin 242 L?

A

9.340 m

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10
Q

What is the length of the Zlin 242 L?

A

6.940 m

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11
Q

What is the height of the Zlin 242 L?

A

2.950 m

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12
Q

What is the angle of the flaps during TAKE-OFF?

A

14o±1o

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13
Q

What is the angle of the flaps during LANDING?

A

37o±1o

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14
Q

What is the wing depth of the Zlin 242 L?

A

1.420 m

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15
Q

What is the angle of the ailerons while deflected UP?

A

21o±1o

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16
Q

What is the angle of the ailerons while deflected DOWN?

A

17o±1o

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17
Q

What is the AREA (m2) of the ailerons of the Zlin 242 L?

A

1,408 m2

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17
Q

What is the angle of the Horizontal Tail Unit (HTU) while deflected up?

A

34o

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18
Q

What is the angle of the Horizontal Tail Unit (HTU) or elevator while deflected down?

A

31o ±1o

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19
Q

What is the angle of the Vertical Tail Unit (VTU) or rudder while deflected left or right?

A

30o±2o

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20
Q

What is the cylinder volume of the TEXTRON Lycoming engine?

A

5,92 litres

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21
Q

What’s the Maximum and Minimum Oil Quantity in the Sump for normal (N) operations?

A

7.6 l max. to 3.8 l min.

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22
Q

What’s the maximum take-off and landing mass for the normal (N) category for Zlin 242 L?

A

1090kg take-off and 1050kg landing

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23
Q

What’s the Maximum Permissible Variable Load for the normal (N) category for Zlin 242 L?

A

345kg

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24
Q

What’s the Standard Empty Mass for the normal (N) category for Zlin 242 L?

A

755kg + 2 %

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25
Q

What are the SPECIFIC LOADINGS for the wings (kg/m2) and for the power loading (kg/kW)?

A

78.6 kg/m2 - specific wing loading
7.32kg/kW - specific power loading

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26
Q

What’s the Never Exceed Speed?

A

172 knots or 319 km/h

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27
Q

What’s the Maximal Structural Cruising Speed? (Do not exceed this speed except in smooth air and then only with caution)

A

135 knots or 250 km/h

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28
Q

What is the Design Maneuvering Speed for the Normal (N) category? (Do not make full or abrupt control movements above this speed)

A

121 knots or 224 km/h

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29
Q

What is the Maximum Flaps Extended Speed?

A

99 knots or 184 km/h

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30
Q

What are the AIRSPEED INDICATOR MARKINGS for the “Red radial line” (Limit values)?

A

172 knots or 319 km/h

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31
Q

What are the AIRSPEED INDICATOR MARKINGS for the “Yellow arc” (Caution range)?

A

135 - 172 knots
250 - 319 km/h

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32
Q

What are the AIRSPEED INDICATOR MARKINGS for the “Green arc” (Normal operation range)?

A

60 - 135 knots
111 - 250 km/h

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33
Q

What are the AIRSPEED INDICATOR MARKINGS for the “White arc” (Wing flaps
extended)?

A

50 - 99 knots
93 - 184 km/h

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34
Q

What is regarded as the speed “Operating range” given by the AIRSPEED INDICATOR MARKINGS?

A

The “Green arc” and the “White arc” indications which are for the normal operation range

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35
Q

What is the minimum and maximum oil temperature for the engine of Textron Lycoming limitations?

A

60 C - min
118 C- max

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36
Q

What is the minimum and maximum cylinder head temperature for the engine of Textron Lycoming limitations?

A

93C - min
260C - max

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37
Q

What is the maximim oil pressure in the engine cylinders measured in kPa?

A

172 kPa - min
690 kPa - max

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38
Q

What is the maximim fuel pressure in the engine cylinders measured in kPa?

A

96 kPa - min
310 kPa - max

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39
Q

In what temperature range should you keep the oil temperature at to get the maximum engine service life?

A

Between 75 C - 95 C

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40
Q

In what temperatures is it necessary to warm the engine prior to its starting?

A

In less than -12 C

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41
Q

When does the the power plant instrument marking for the oil temperature indicate the “Red radial line”?

A

When the oil temperature reaches 118 C

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42
Q

When does the the power plant instrument marking for the oil pressure indicate the “Red radial line”?

A

At the minimum of 172 kPa and the maximum of 690 kPa

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43
Q

What are the load factors measured in “g” for the Normal (N) category?

A

+ 3,8
- 1,52

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44
Q

What is the minimum quantity of fuel in litres to have permission for take-off?

A

20 litres

45
Q

What is the maximum operation attitude limit in ft and metres?

A

14 750 ft = 4 500 m

46
Q

Must the flaps be retracted during taxiing?

A

Yes.

47
Q

What is the maximum demonstrated speed for brakes application?

A

54 knots or 100 km/h

48
Q

What is the recommended airspeed for Engine failure after take-off?

A

MIN. 78 knots (145 km/h)

49
Q

What is the recommended airspeed for Engine failure in flight?

A

MIN. 78 knots (145 km/h)

50
Q

What is the recommended airspeed for Emergency landing with engine power?

A

78 - 85 knots (145 - 160 km/h)

51
Q

What is the recommended airspeed for Emergency landing without engine power?

A

78 - 85 knots (145 - 160 km/h)

52
Q

What is the best glide airspeed with flaps retracted for the Normal (N) category?

A

73 knots or 135 km/h

53
Q

Climb airspeed is:

A

81 knots
(150 km/h)

54
Q

Acceleration at lift-off airspeed is:

A

73 knots
(135 km/h)

55
Q

Approach airspeed is (before landing):

A

73 - 76 knots
(135 - 140 km/h)

56
Q

Touch-down airspeed is:

A

62 knots
(115 km/h)

57
Q

At what speed is the stall-warning horn activated?

A

5 knots or 9 km/h above stall speed

58
Q

What is the stall speed when flaps are retracted (0 degrees) regarding CAS?

A

64 knots or 118 km/h

59
Q

What is the stall speed when flaps are on take-off setting (14 degrees) regarding CAS?

A

60 knots or 110 km/h

60
Q

What is the stall speed when flaps are on landing setting (37 degrees) regarding CAS?

A

54 knots or 100 km/h

61
Q

What is the take-off distance?

A

873 ft or 266 m

62
Q

What is the rate of climb regarding the constant 81 knots or 150 km/h?

A

850 ft/min or 4,25 m/s

63
Q

What’s the maximum glide ratio with flaps RETRACTED?

A

73 knots or 135 km/h

64
Q

What’s the minimum descent speed with the flaps RETRACTED?

A

Airspeed of 68 knots (125km/h) and fall of885 ft/min (4,5 m/s)

65
Q

What is the landing run distance for the standard use of brakes?

A

425 m

66
Q

What is the landing run distance for the MAX use of brakes?

A

265 m

67
Q

What cap controls the engine power?

A

Black cap

68
Q

What cap controls the propeller pitch?

A

Blue cap

69
Q

What cap controls the mixture of the fuel?

A

Red cap

70
Q

What’s the MAX quantity of oil in the engine crankcase?

A

7,6 litres

71
Q

The oil temperature, oil pressure, fuel pressure and actual fuel consumption values are displayed on what display of the GARMIN?

A

The engine operating parameters are displayed on the EIS display of the Garmin 500 TXi avionics system.

72
Q

What is the firing order of the cylinders?

A

1-3-4-2

73
Q

What is the name of the fuel injection system in the engine?

A

BENDIX RSA - 5AD1

74
Q

What is the name of the propeller used?

A

MTV-9-B-C/C-188-18 or HARTZELL HC-C3YR-4BF/FC 6890

75
Q

What’s the volume of the main tanks?

A

2 x 60 litres

76
Q

What is the nominal voltage of the network?

A

28 V

77
Q

What is the maximum amperage provided by the generator?

A

60 A

78
Q

Отклонението на носовата стойка при управление чрез педалите е в границите на…(градуси)

A

±15 градуса

79
Q

Носовата стойка е снабдена и с хидравличен демпфер, за да предотварти кой ефект?

A

“Шими” ефекта

80
Q

Какво е “Шими” ефекта?

A

„Шими“ ефекта е нежелано движение на самолета по пистата по време на излитане и кацане

81
Q

При рулиране по земята за сметка на диференциалното спиране на основните колела ъгъла на отклонение на носовата стойка е…(градуси)

A

± 38 градуса

82
Q

Колелата на основната стойка и на носовата са покрити с ………… за намаляване на челното съпротивление в полет.

A

обтекатели

83
Q

Колесника неприбираем ли е в полета?

A

Неприбираем е.

84
Q

Основната стойка на колелата е изработена от …….

A

две пружинни рамена

85
Q

What is the WHEEL BASE and WHEEL TRACK of the landing gear?

A

1,755 m and 2,330 m

86
Q

Предвид начина на закрепване и разположение на двигателя носовата стойка на къде е леко изместена спрямо надлъжната ос на самолета.

A

Леко вляво

87
Q

Основната стойка е снабдена …………. (материал) джанти

A

алуминиеви

88
Q

Относно джантите - в единия им край са оформени канали, в които влиза спирачния диск, който се върти заедно с ……..

A

джантата

89
Q

Спирачката е дискова, хидравлична със самурегулиране на разстоянието между …………………. и диска

A

спирачните цилиндри

90
Q

Чрез колко болта се сглобява носовата джанта и другите две страни на колесника?

A

носова - 3 бр.
другите две - 6 бр.

91
Q

Чрез какво се подава хидравличната течност до спирачните апарати?

A

по гъвкави шлангове

92
Q

Задействането на спирачките става чрез натискане на ……… част на педалите като всеки от тях е свързан с по един цилиндър.

A

горната

93
Q

Задействането на ръчната спирачка става по следните стъпки:

A
  • натискат се спирачките на двата педала;
  • изтегля се ръчката на спирачката и се завърта на 90 градуса
94
Q

Освобождаването на ръчната спирачка става по следните стъпки:

A
  • натискат се педалите;
  • завърта се лостчето на спирачката на 90 градуса и се натиска напред до първоначалното му положение;
  • натискат се и се отпускат спирачките два пъти.
95
Q

Каква вместимост има резервоара на горивото и каква част е използваема?

A

60 литра, използваеми са 55 литра

96
Q

Отсекът за отрицателно претоваране на горивото е с вместимост около:

A

2 литра

97
Q

Електрическата подкачваща помпа за горивото служи за?

A

Тази помпа се използва при запуск и при отказ на главната двигателна горивна помпа.

98
Q

Кои клапи подават сигнал за оставащото в резервоарите гориво към таблото на пилота?

A

поплавковите клапани

99
Q

В краищата на полукрилата вместо горивните резервоари какво може да бъде монтирано?

A

обтекатели

100
Q

Самолета е с ……… разположено крило

A

долно

101
Q

Опишете смесената конструкция на тялото на Zlin 242L.

A

Централната част е фермена конструкция, задната част е от полумонококова конструкция

102
Q

Какъв е ъгълът на V-образност?

A

6 градуса (положителен)

103
Q

Чрез лостът се управлява:

A

хоризонталното кормило (напред, назад) и елероните (наляво, надясно)

104
Q

Управлението. Чрез педали се управлява:

A

Вертикалното кормило и носовата стойка

105
Q

Какво е специалното при левия лост от страна на командирското място?

A

На левия лост за управление има монтиран механизъм за застопоряване на лоста - цялото управление на хоризонталното кормило и елероните (предпазване от вятър при престой на земята)

106
Q

Обяснете особеностите при управлението на хоризонатлното кормило от лявата и от дясната страна.

A

Лявата част на хоризонталното кормило е оборудвана със сервокомпенсатор, а дясната с управляем тример.

107
Q

Стандартни ли са опашните плоскости и от какво се сътоят?

A

Опашните плоскости са стандартни – разположени са в задната част на самолета и се състоят от хоризонтален стабилизатор с хоризонтално кормило и вертикален стабилизатор с вертикално кормило

108
Q

Кормилата балансирани ли са и по какъв начин?

A

Тегловно и аеродинамично баланзирани са.

109
Q

Каква е обшивката на опашните плоскости?

A

Алуминиева сплав.

110
Q

Хоризонталното кормило е снабдено с…

A

тример

111
Q
A

Zlin 242L (1 decks)

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