2 ATTENT. FLIG. PER. EXAM. PREP.

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Question 1 of 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?

Select one of the following:

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

Explanation

Question 2 of 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

Select one of the following:

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

Explanation

Question 3 of 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

Select one of the following:

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.

Explanation

Question 4 of 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

Select one of the following:

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

Explanation

Question 5 of 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.

Select one of the following:

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

Explanation

Question 6 of 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/

Select one of the following:

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.]

Explanation

Question 7 of 30

61 The Service Ceiling is the pressure altitude where :

Select one of the following:

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.

Explanation

Question 8 of 30

67 For a given aircraft mass, the climb gradient:

Select one of the following:

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.

Explanation

Question 9 of 30

74 When an aircraft reaches its service ceiling :

Select one of the following:

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.

Explanation

Question 10 of 30

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

Select one of the following:

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.

Explanation

Question 11 of 30

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

Select one of the following:

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

Explanation

Question 12 of 30

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

Select one of the following:

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.

Explanation

Question 13 of 30

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

Select one of the following:

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

Explanation

Question 14 of 30

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

Select one of the following:

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.

Explanation

Question 15 of 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?

Select one of the following:

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

Explanation

Question 16 of 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?

Select one of the following:

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

Explanation

Question 17 of 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.

Select one of the following:

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

Explanation

Question 18 of 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.

Select one of the following:

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

Explanation

Question 19 of 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

Select one of the following:

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

Explanation

Question 20 of 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

Select one of the following:

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

Explanation

Question 21 of 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".

Select one of the following:

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

Explanation

Question 22 of 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?

Select one of the following:

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

Explanation

Question 23 of 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".

Select one of the following:

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

Explanation

Question 24 of 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

Select one of the following:

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

Explanation

Question 25 of 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?

Select one of the following:

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

Explanation

Question 26 of 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.

Select one of the following:

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

Explanation

Question 27 of 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.

Select one of the following:

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

Explanation

Question 28 of 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?

Select one of the following:

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

Explanation

Question 29 of 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?

Select one of the following:

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

Explanation

Question 30 of 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?

Select one of the following:

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

Explanation

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