2 ATTENT. FLIG. PER. EXAM. PREP.

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Questão 1 de 30

52 If an aircraft is overloaded by 90 lbs (48 kgs),how much fuel has to be removed so that the aircraft loading will be within limits?

Selecione uma das seguintes:

O '15 USG.
O '12 USG.
O '6 USG.
O '9 USG.

Explicação

Questão 2 de 30

53 What is the maximum baggage weight that can be loaded on the aeroplane so that the center of gravity remains within limits?(Fig FPP07)
Empty Weight = 1350 lb moment(/1000) = 51,5., Pilot and front passengers = 250 lb, Rear Passengers =400lbs, Fuel = (30

Selecione uma das seguintes:

O '105 Ib.
O '120 Ib.
O '90 Ib.
O '751b.

Explicação

Questão 3 de 30

54 calculate the moment/1.000 of the following aircraft and check if it is loaded within the CG envelope limits.(Fig FPP07)], Βάρος κενό/Empty Weight = 1350 lb ροπή/moment(/1000) = 51,5. Πιλότος και επιβάτης εμπρός/Pilot and front passengers = 310 lb. Επιβάτ

Selecione uma das seguintes:

O '83.0 within limits.
O '78.2. out of the CG envelope.
O '88.3. within limits.
O '80,2. out of the CG envelope.

Explicação

Questão 4 de 30

55 What is the maximum amount of fuel which can be loaded on the aeroplane before take off, so that the total moment remains within the envelope limits? (Fig FPP07)]. Βάρος κενό/ Empty Weight = 1350 lb ροπή/moment(/1000) = 51,5. Πιλότος και επιβάτης εμπρός/P

Selecione uma das seguintes:

O '40 USG.
O '34 USG.
O '24 USG.
O '46 USG.

Explicação

Questão 5 de 30

56 Calculate the total moment and check if it is within the envelope limits. (Fig FPP07)]. Βάρος κενό/Empty Weight = 1350 lb ροπή/moment(/1000) = 51,5. Πιλότος και επιβάτης εμπρός/Pilot and front passengers = 340 lb. Επιβάτες πίσω/Rear Passengers = 310lbs.

Selecione uma das seguintes:

O '77,7 Ib-inches.
O '69,9 Ib-inches.
O '73,9Ib-inches.
O '38,7Ib-inches.

Explicação

Questão 6 de 30

57 Calculate the CG position and check if it is located within the envelope limits.(Fig FPP07)]. Βάρος κενό/Empty Weight = 1350 lb ροπή/moment(/1000) = 51,5. Πιλότος και επιβάτης εμπρός/Pilot and front passengers = 380 lb. Αποσκευές/Baggage = 45 lb. Καύσιμο/

Selecione uma das seguintes:

O within limits, normal category.
O within limits, utility category.
O out of the CG envelope, to the left of the diagram.
O out of the CG envelope ,to the right of the diagram.]

Explicação

Questão 7 de 30

61 The Service Ceiling is the pressure altitude where :

Selecione uma das seguintes:

O the rate of climb reaches a specified value,
O the rate of climb is zero
O the rate of climb is 100fpm.
O the a/c flies more efficient.

Explicação

Questão 8 de 30

67 For a given aircraft mass, the climb gradient:

Selecione uma das seguintes:

O decreases if flap angle increases, and if temperature increases.
O increases if flap angle increases, and if temperature decreases.
O decreases if flap angle increases, and if temperature decreases.
O increases if flap angle increases, and if temperature increases.

Explicação

Questão 9 de 30

74 When an aircraft reaches its service ceiling :

Selecione uma das seguintes:

O it will have a small positive rate of climb
O the excess power will be zero
O the rate of climb will be zero
O power required will decrease.

Explicação

Questão 10 de 30

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

Selecione uma das seguintes:

O remain the same and the Vmd will remain the same .
O decrease, and the Vmd will decrease
O increase, and the Vmd will increase
O remain the same and the Vmd will be diminished.

Explicação

Questão 11 de 30

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

Selecione uma das seguintes:

O when the drag is equal to the maximum thrust available,
O when the drag is a minimum
O when CL / CD is a minimum
O when CD is a minimum

Explicação

Questão 12 de 30

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

Selecione uma das seguintes:

O 30% above the stalling speed with landing flap.
O 20% above the stalling speed with landing flap
O 30% above the stalling speed with flaps up
O stall speed.

Explicação

Questão 13 de 30

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

Selecione uma das seguintes:

O slightlyO the same.
lower.
O the same.
O slightly higher.
O significantly lower, proportional to the tailwind component.

Explicação

Questão 14 de 30

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

Selecione uma das seguintes:

O at that speed which provides the minimum power/ airspeed ratio.
O significantly higher than the minimum drag speed (Vmd).
O at the lowest density altitude environment that is safely possible.
O at the same speed which provides the maximum power/airspeed ratio.

Explicação

Questão 15 de 30

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?

Selecione uma das seguintes:

O 1,650-foot increase.
O 1,000-foot increase.
O 1,300-foot increase.
O 1950-foot increase.

Explicação

Questão 16 de 30

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?

Selecione uma das seguintes:

O 2,100-foot decrease.
O 1,800-foot increase.
O 1,500-foot decrease.
O 1,000-foot increase.

Explicação

Questão 17 de 30

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.

Selecione uma das seguintes:

O 3,010 feet MSL.
O 1,250 feet MSL.
O 1,373 feet MSL.
O 2500 feet MSL.

Explicação

Questão 18 de 30

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.

Selecione uma das seguintes:

O 1,200 feet MSL.
O 2,440 feet MSL.
O 2000 feet MSL.
O none of them.

Explicação

Questão 19 de 30

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

Selecione uma das seguintes:

O 8,500 feet MSL.
O 4,600 feet MSL.
O 5,877 feet MSL.
O 6000 feet MSL.

Explicação

Questão 20 de 30

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

Selecione uma das seguintes:

O 3,500 feet MSL.
O 4,900 feet MSL.
O 4,000 feet MSL.
O 3,000 feet MSL.

Explicação

Questão 21 de 30

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".

Selecione uma das seguintes:

O 4,527 feet MSL.
O 4,236 feet MSL.
O 3,640 feet MSL.
O 4,600 feet MSL.

Explicação

Questão 22 de 30

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?

Selecione uma das seguintes:

O 1,300-foot increase.
O 900-foot increase.
O 1,100-foot decrease.
O 1300-foot decrease.

Explicação

Questão 23 de 30

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".

Selecione uma das seguintes:

O 1,341 feet MSL.
O 1,451 feet MSL.
O 1,562 feet MSL.
O 1,212 feet MSL.

Explicação

Questão 24 de 30

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

Selecione uma das seguintes:

O 2,000 feet MSL,
O 1,500 feet MSL
O 2,900 feet MSL,
O 3,500 feet MSL

Explicação

Questão 25 de 30

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?

Selecione uma das seguintes:

O 23knots.
O 19 knots.
O 30 knots.
O 34 knots.

Explicação

Questão 26 de 30

125 (Refer to Fig.9) Determine the maxi¬mum wind velocity for a 45° crosswind if the maxi¬mum crosswind component for the airplane is 25 knots.

Selecione uma das seguintes:

O 35 knots.
O 18 knots.
O 25 knots.
O 29 knots.

Explicação

Questão 27 de 30

126 (Refer to Fig.9) Determine the maxi¬mum wind velocity for a 50° crosswind if the maxi¬mum crosswind component for the airplane is 23 knots.

Selecione uma das seguintes:

O 20 knots.
O 28 knots.
O 30 knots.
O 32 knots.

Explicação

Questão 28 de 30

127 (Refer to Fig.9) What is the maximum wind velocity for a 30? crosswind if the maximum crosswind component for the airplane is 12 knots?

Selecione uma das seguintes:

O 23 knots.
O 16 knots.
O 20 knots.
O 25 knots.

Explicação

Questão 29 de 30

128 (Refer to Fig.9) What is the maximum wind velocity for a 35 ? crosswind if the maximum crosswind component for the airplane is 17 knots?

Selecione uma das seguintes:

O 25 knots.
O 20 knots.
O 15 knots.
O 17 knots.

Explicação

Questão 30 de 30

129 (Refer to Fig.9) With a reported wind of north at 20 knots, which runway (6, 29, or 32) is acceptable for use for an airplane with a 13-knot maxi¬mum crosswind component?

Selecione uma das seguintes:

O Runway 32.
O Runway 6.
O Runway 29.
O Out of limits.

Explicação

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