4 FLIG. PER. EXAM. PREP.

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77 To obtain the maximum possible range when flying into a headwind, the speed should:

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78 If the aircraft's C.G. is moved into a more forward position

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79 For a given aircraft mass, as altitude increases, the minimum total drag will;

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80 The maximum speed that can be achieved in level flight, will occur:

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81 The scheduled landing distance required, is the distance :

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82 The landing distance required will be increased as a result of all of the following';

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83 Which of the following statements relating to hydroplaning is true :

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102 Given that the regulations applied and control requirement is met, the speed at the 50 ft. screen must not be less than :

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103 If the runway is wet, the landing distance required for a dry runway :

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104 The landing distance required must not exceed :

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108 For a grass runway, the landing distance required for a paved runway should be :

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109 In comparison to the true airspeed in still air conditions, the TAS for the best range in a strong tailwind will be:

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110 Consult Fig.4. Refering to this graph, the flight for maximum range in a piston engined aircraft is achieved by flying:

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113 The best rate of climb is achieved.

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114 (Refer to Fig.8). What is the effect of a temperature increase from -4?C to +10°C on the density altitude if the pressure altitude remains at 5,000 feet?

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115 (Refer to Fig.8). What is the effect of a temperature increase from +4?C to -15°C on the density altitude if the pressure altitude remains at 10,000 feet?

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116 (Refer to Fig.8). Determine the pres¬sure altitude with an indicated altitude of 1,380 feet MSL with an altimeter setting of 28.22" at standard temperature.

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117 (Refer to Fig.8). Determine the pres¬sure altitude with an indicated altitude of 1,820 feet MSL with an altimeter setting of 30.58" at standard temperature.

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118 (Refer to Fig.8). Determine the density altitude for these conditions:
Altimeter setting...................................................29.25"
Runway temperature...........................................+27°C
Airport elevation......................................5,250 ft MSL

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119 (Refer to Fig.8). Determine the density altitude for these conditions:
Altimeter setting...................................................30.15"
Runway temperature........................................... -1°C
Airport elevation......................................4,610 ft MSL

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120 (Refer to figure 8.) Determine the pressure altitude at an airport that is 4,563 feet MSL with an altimeter set¬ting of 29.96".

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121 (Refer to figure 8.) What is the effect of a temperature increase from -1?C to 10°C on the density altitude if the pressure altitude remains at 3,000 feet MSL?

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122 (Refer to figure 8.) Determine the pressure altitude at an airport that is 1,386 feet MSL with an altimeter setting of 29.97".

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123 (Refer to figure 8.) Determine the density altitude for these conditions:
Altimeter setting...................................................30.35"
Runway temperature........................................... -4°C
Airport elevation......................................3,894 ft MSL

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124 (Refer to Fig.9) What is the headwind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots?

4 FLIG. PER. EXAM. PREP.

4 FLIG. PER. EXAM. PREP.

77 To obtain the maximum possible range when flying into a headwind, the speed should:

78 If the aircraft's C.G. is moved into a more forward position

79 For a given aircraft mass, as altitude increases, the minimum total drag will;

80 The maximum speed that can be achieved in level flight, will occur:

81 The scheduled landing distance required, is the distance :

82 The landing distance required will be increased as a result of all of the following';

83 Which of the following statements relating to hydroplaning is true :

102 Given that the regulations applied and control requirement is met, the speed at the 50 ft. screen must not be less than :

103 If the runway is wet, the landing distance required for a dry runway :

104 The landing distance required must not exceed :

108 For a grass runway, the landing distance required for a paved runway should be :

109 In comparison to the true airspeed in still air conditions, the TAS for the best range in a strong tailwind will be:

110 Consult Fig.4. Refering to this graph, the flight for maximum range in a piston engined aircraft is achieved by flying:

113 The best rate of climb is achieved.

114 (Refer to Fig.8). What is the effect of a temperature increase from -4?C to +10°C on the density altitude if the pressure altitude remains at 5,000 feet?

115 (Refer to Fig.8). What is the effect of a temperature increase from +4?C to -15°C on the density altitude if the pressure altitude remains at 10,000 feet?

116 (Refer to Fig.8). Determine the pres¬sure altitude with an indicated altitude of 1,380 feet MSL with an altimeter setting of 28.22" at standard temperature.

117 (Refer to Fig.8). Determine the pres¬sure altitude with an indicated altitude of 1,820 feet MSL with an altimeter setting of 30.58" at standard temperature.

118 (Refer to Fig.8). Determine the density altitude for these conditions: Altimeter setting...................................................29.25" Runway temperature...........................................+27°C Airport elevation......................................5,250 ft MSL

119 (Refer to Fig.8). Determine the density altitude for these conditions: Altimeter setting...................................................30.15" Runway temperature........................................... -1°C Airport elevation......................................4,610 ft MSL

118 (Refer to Fig.8). Determine the density altitude for these conditions:
Altimeter setting...................................................29.25"
Runway temperature...........................................+27°C
Airport elevation......................................5,250 ft MSL

119 (Refer to Fig.8). Determine the density altitude for these conditions:
Altimeter setting...................................................30.15"
Runway temperature........................................... -1°C
Airport elevation......................................4,610 ft MSL

123 (Refer to figure 8.) Determine the density altitude for these conditions:
Altimeter setting...................................................30.35"
Runway temperature........................................... -4°C
Airport elevation......................................3,894 ft MSL