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Questão 1 de 32

175 An aeroplane operating from a flat runway in the same wind conditions as when operating from an up-sloping runway will require a ....(i).... take-off distance and a ....(ii).... landing distance.

Selecione uma das seguintes:

O (i) shorter (ii) longer
O (i) longer (ii) longer
O (i) longer (ii) shorter
O (i) shorter (ii) shorter

Explicação

Questão 2 de 32

179 Pressure altitude is frequently employed as the datum for measuring aircraft performance. Given an aerodrome elevation as 1010ft amsl and a QFE of 990hPa.
What is the aerodrome pressure altitude? [1mb = 30ft]

Selecione uma das seguintes:

O 1700ft
O 1500ft
O 1244ft
O 1623ft.

Explicação

Questão 3 de 32

181 Flight for maximum range in a piston engined normally aspirated aircraft is achieved by flying:

Selecione uma das seguintes:

O at just above the minimum drag speed.
O at the lowest density altitude that is safely possible.
O just below that speed which provides the maximum power/airspeed ratio.
O at the same speed, where minimum difference between power required and power available exist.

Explicação

Questão 4 de 32

183 The remaining fuel weight available for computing mass and balance, is 285 Kgs AVGAS of specific gravity 0.70. Determine how many litres the pump will indicate to be within limits.

Selecione uma das seguintes:

O 407 lts.
O 1995 lts.
O 355 lts.
O 500 lts.

Explicação

Questão 5 de 32

184 In a constant IAS climb in the troposphere?

Selecione uma das seguintes:

O TAS increases.
O TAS decreases.
O TAS increases, then remains constant.
O TAS decreases, then remains constant.

Explicação

Questão 6 de 32

186 The relationship between Vx and Vy?

Selecione uma das seguintes:

O Vx is always less than or equal to Vy.
O Vx is always less than Vy.
O Vx is always greater than Vy,
O There's no between them.

Explicação

Questão 7 de 32

188 Loading icreases, then……………………

Selecione uma das seguintes:

O Vx and Vy increase.
O Vx increases and Vy decreases.
O Vx decreases and Vy increases.
O both Vx and Vy decrease.

Explicação

Questão 8 de 32

199 If the aeroplane in Fig. 27 quits engine at 8.000 ft, the distance will cover in still air conditions, is:

Selecione uma das seguintes:

O 12 nm
O 10 nm
O 14 nm
O 13 nm.

Explicação

Questão 9 de 32

200 An aircraft with full tanks has 500 litres on board. Given that the fuel specific gravity is 0.750, the weight of the fuel will be:

Selecione uma das seguintes:

O 825 lbs or 375 Kgrs.
O 800 lbs. or 362 Kgrs
O 820 lbs or 372 Kgrs.
O 900 lbs or 407 Kgrs.

Explicação

Questão 10 de 32

203 What effect has a centre of gravity close to the forward limit?

Selecione uma das seguintes:

O A reduce rate of climb
O A better rate of climb capability
O A reduction in the specific fuel consumption
O A decreased induced drag

Explicação

Questão 11 de 32

206 Consult Fig.30 that's in accordance with CAP 696
Where is the reference datum?

Selecione uma das seguintes:

O 39 inches forward of the firewall
O 74 inches aft of the fwd CG position
O 80.4 inches aft of the rear CG position
O 87.7 inches aft of the rear CG position

Explicação

Questão 12 de 32

207 Consult Fig.30 that's in accordance with CAP 696
What are the CG limits?

Selecione uma das seguintes:

O fwd limit = 74 inches to 80.4 inches and aft limit = 87.7 inches
O fwd limit = 74 inches to 80.4 inches
O fwd limit = 74 inches, aft limit = 80.4 inches
O fwd limit = 74 inches, aft limit = 87.7 inches

Explicação

Questão 13 de 32

208 Consult Fig.30 that's in accordance with CAP 696
What is the CG at the BEM?

Selecione uma das seguintes:

O 77.7 inches
O 77 inches
O 87 inches
O 77.7 centimetres

Explicação

Questão 14 de 32

209 Consult Fig.30 that's in accordance with CAP 696
What is the distance of the main undercarriage from the firewall?

Selecione uma das seguintes:

O 58 inches
O 97 inches
O 87.7 inches
O 39 inches

Explicação

Questão 15 de 32

210 Consult Fig.30 that's in accordance with CAP 696
The aircraft has six seats. Assuming no other cargo or baggage, what is the maximum fuel (in 74USG capacity version), that can be carried if all six seats are occupied and the mass of each occupant is 180 lb?

Selecione uma das seguintes:

O 155 lbs but the CG would be dangerously out of limits
O 296 lbs but the CG would be dangerously out of limits
O 444 lbs and the CG would be dangerously out of limits
O 1551bs and the CG would be in limits since tank fuel capacity is 74USG.

Explicação

Questão 16 de 32

211 Consult Fig.30 that's in accordance with CAP 696
If the landing mass is 3075 lb and the trip fuel was 40 USG, what was the ZFM if the fuel tanks held 60 gallons of fuel prior to take-off?

Selecione uma das seguintes:

O 3000 lb
O 3035lb
O 3590 lb
O 3055lb

Explicação

Questão 17 de 32

212 Fig.30 that's in accordance with CAP 696
What is the maximum ramp mass (MRM), out of hangar?

Selecione uma das seguintes:

O 3663 lbs
O 3650 lbs
O 3780 lbs
O 3880 lbs

Explicação

Questão 18 de 32

213 Consult Fig.30 that's in accordance with CAP 696
How far is the main wheel from the aft CG limit?

Selecione uma das seguintes:

O 9.3 inches aft of the rear datum
O 0.7 inches behind the rear datum
O 0.7 inches forward of the rear datum
O 6.6 inches forward of the rear datum

Explicação

Questão 19 de 32

216 The Take-off mass is:

Selecione uma das seguintes:

O the mass of the aeroplane including everyone and everything contained within it at the start of the take-off run.
O the maximum permissible total aeroplane mass on completion of the refuelling
operation.
O the maximum permissible total aeroplane mass for take-off but excluding fuel.
O the maximum permissible total aeroplane mass at the start of the take-off run.

Explicação

Questão 20 de 32

218 If an aeroplane is at elevation of 660ft and QFE is 1003 hPa, the approximate Pressure Altitude is:

Selecione uma das seguintes:

O 300ft
O 660ft
O 350ft
O 365ft

Explicação

Questão 21 de 32

219 The Basic Empty Mass is the:

Selecione uma das seguintes:

O Operating mass minus the crew and fuel load
O MZFM minus both traffic load and the fuel load
O Take-off mass minus the traffic load and the fuel load
O Landing mass less traffic load

Explicação

Questão 22 de 32

220 (Refer to Fig.7) What is the maxi¬mum amount of baggage that may be loaded aboard the airplane for the CG to remain within the moment envelope?
MASS (LB) MOM/1000
Basic Empty Mass 1,350 51.5
Pilot and front passenger 250 -
Rear passengers 400 -
Baggage - -
Fuel, 27 USG _ _
Oil, 8qt - -0.2

Selecione uma das seguintes:

O 165 pounds.
O 110 pounds.
O 120 pounds.
O 150 pounds

Explicação

Questão 23 de 32

221 (Refer to Fig.7) Calculate the moment of the airplane and determine which category is applicable.
MASS (LB) MOM/1000
Basic Empty Mass 1,350 51.5
Pilot and front pass 380 -
Rear passengers 96 -
Fuel, 38 gal - _
Oil, 8 qt - -0.2

Selecione uma das seguintes:

O 80.3 (lb-in), utility category.
O 69.2 (lb-in), utility category.
O 81.2 (lb-in), normal category
O 83.0 (lb-in) normal category

Explicação

Questão 24 de 32

222 (Refer to Fig.7) What is the maxi¬mum amount of fuel that may be aboard the airplane on takeoff if loaded as follows?
MASS (LB) MOM/1000
Basic Empty Mass 1,350 51.5
Pilot and front passenger 340 -
Rear passengers 310 _
Baggage 45 _
Oil, 8 qt _ _

Selecione uma das seguintes:

O 150 litres.
O 90 litres.
O 120 litres.
O 200 litres.

Explicação

Questão 25 de 32

223 18 (Refer to Fig.7) Determine the moment/1000 with the following data:
MASS (LB) MOM/1000
Basic Empty Mass 1,350 51.5
Pilot and front passenger 340 -
Fuel (std. tanks) Capacity -
Oil, 8 qt - -

Selecione uma das seguintes:

O 74.9 pound-inches.
O 69.9 pound-inches.
O 77.6 pound-inches.
O 81.0 pound-inches.

Explicação

Questão 26 de 32

224 (Refer to figure 7). Determine the aircraft loaded moment /1000 and the aircraft category.
MASS (LB) MOM/1000
Basic Empty mass 1,350 51.5.
Pilot and front pass 345 -
Fuel 48 gal. 288 -
Oil, 8 qt - -

Selecione uma das seguintes:

O 80.0 utility category.
O 78.2, normal category.
O 79.2, normal category.
O 80.4, utility category.

Explicação

Questão 27 de 32

225 Refer to the graph in Fig. 32. Which combination of aircraft gross weight in pounds and C of G position in inches aft of the datum results in safe configuration?

Selecione uma das seguintes:

O 2700 lbs and 35.0 inches.
O 3040 lbs and 50.4 inches.
O 3620 lbs and 45.0 inches.
O 2800 lbs and 50.0 inches.

Explicação

Questão 28 de 32

226 Refer to the graph in Fig. 32. Which combination of aircraft gross weight in pounds and C of G position in inches aft of the datum results in safe configuration?

Selecione uma das seguintes:

O 2540 lbs and 33.5 inches.
O 3600 lbs and 42.0 inches.
O 3650 lbs and 45.0 inches.
O 2750 lbs and 49.8 inches.

Explicação

Questão 29 de 32

227 Refer to the graph in Fig. 31. What's the maximum amount of fuel with long range tanks that may be aboard the aeroplane on take off, if loaded as follows:
MASS MOM/1000
BEM 1800 lb 63.3
Pilot 290 lb 12.6
2nd row seat 260 lb 25.2
Fuels _ _
Bagg. Compartment 100 lb 11.6
Aft Bagg. Area _ 1.6

Selecione uma das seguintes:

O 450 lt or 75 USG.
O 500 lt or 83 USG.
O 336 lt or 56 USG.
O 336 lt or 50 USG.

Explicação

Questão 30 de 32

228 Refer to the graph in Fig. 31. Fill her up with std tanks and determine, if the total moments are within envelope.
MASS MOM/1000
BEM 1800 lb 63.3
1st row seat 340 lb 12.6
2nd row seat 340 lb 25.2
Fuels Full capacity _
Bagg. Compartment 104 lb 10.5

Selecione uma das seguintes:

O 127.7 lb-in and 43.7 inches aft of datum.
O 111.6 lb-in and 38.2 inches aft of datum.
O 127.7 lb-in and 38.2 inches aft of datum.
O 116.6 lb-in and 43.7 inches fore of datum.

Explicação

Questão 31 de 32

229 Use the C of G envelope graph in Fig.2 in order to answer the following question.
The combination of weight "mass" and moment arm shown, which is acceptable for flight in the Utility Category is:

Selecione uma das seguintes:

O 2000lb 80.0
O 2100lb 75.3
O 2115lb 100.2
O 2117lb 100.2

Explicação

Questão 32 de 32

230 Pressure Altitude is?

Selecione uma das seguintes:

O The altimeter indication when 1013.25 hPa, is set on the sub-scale.
O The altitude above sea level.
O The altimeter indication when QFE, is set on the sub-scale.
O The altimeter indication when QNH, is set on the sub-scale.

Explicação

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