8 FLIG. PER. EXAM. PREP.

Question 1

Question

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?

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fd0d841e-1e10-4e2f-8b58-8f22b13299bd (image/jpeg)

Answer

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

Question 2

Question

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

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57850827-ef17-4124-b3f2-fcf807b6f8a3 (image/jpeg)

Answer

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

Question 3

Question

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

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c642f018-d5a9-49b4-bd20-010cddb976c3 (image/jpeg)

Answer

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

Question 4

Question

214 The Maximum Zero Fuel Mass is the maximum permissible mass of the aeroplane:

Answer

O with no useable fuel unless the Aeroplane Flight Manual Limitations explicitly include it.
O with no useable fuel
O including the fuel taken up for take-off
O including all useable fuel unless the Aeroplane Flight Operations Manual explicitly excludes it.

Question 5

Question

215 The Maximum Structural Take-off Mass is:

Answer

O the maximum permissible total aeroplane mass 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 subject to the limiting conditions at the departure airfield.
O the maximum permissible total aeroplane mass for take-off but excluding fuel,

Question 6

Question

216 The Take-off mass is:

Answer

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.

Question 7

Question

217 The Basic Empty Mass is the mass of the aeroplane:

Answer

O plus standard items such as unusable fluids, fire extinguishers, emergency oxygen equipment, supplementary electronics etc.
O plus non-standard items such as lubricating oil, fire extinguishers, emergency oxygen equipment etc.
O minus non-standard items such as lubricating oil, fire extinguishers, emergency oxygen equipment etc.
O minus non-standard items such as unusable fluids, fire extinguishers, emergency oxygen and supplementary electronic equipment etc.

Question 8

Question

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

Answer

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

Question 9

Question

219 The Basic Empty Mass is the:

Answer

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

Question 10

Question

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

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Answer

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

Question 11

Question

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

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Answer

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

Question 12

Question

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 _ _

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803593c0-5f21-4438-8c15-31e22f9ba38b (image/jpeg)

Answer

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

Question 13

Question

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 - -

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b37d6d2e-e6db-44bd-9a93-bbd18ae5e973 (image/jpeg)

Answer

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

Question 14

Question

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 - -

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942a1d1e-7409-44b2-b775-adea69cd9f4a (image/jpeg)

Answer

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

Question 15

Question

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?

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dd5cd94d-665c-40ff-99cd-9ebef4a7fcda (image/jpeg)

Answer

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.

Question 16

Question

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?

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34273ca9-f34b-4bf5-8e57-d75967943cea (image/jpeg)

Answer

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.

Question 17

Question

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

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ad8dc7a0-c19a-47d3-aa59-fe44f1733081 (image/jpeg)

Answer

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

Question 18

Question

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

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4a3093c5-6d40-49eb-9d4d-2b10d38a187e (image/jpeg)

Answer

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.

Question 19

Question

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:

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1cbca423-5fec-4791-9849-0a252e7602cb (image/jpeg)

Answer

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

Question 20

Question

230 Pressure Altitude is?

Answer

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.

Question 21

Question

231 Calculate the Centre of Gravity and total weight "mass", given the following conditions. MASS LEVER ARM MOM/1000 BEM 2122 lb 35.76 _ Pilot & Copilot 340 lb 37.0 12.6 Centre row seat _ lb 70.0 23.8 Aft row seat 340 lb _ 34.0 Bagg. Compartment 104 lb 126.9 _ Aft Bagg. Area _ _ _ Fuels (55USG) _ 48.0 17.0

Answer

O 3600 lb and 49.0 inches aft of datum.
O 2906 lb and 29.6 inches aft of datum.
O 3246 lb and 42.1 inches aft of datum.
O 3600 lb and 24.2 inches aft of datum.

Question 22

Question

232 Four on board. Investigate using tables in Fig. 33, the total moments (/100) and if within limits?

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10498ceb-eef4-4a43-a339-feaac5287f3a (image/jpeg)

Answer

O 156.769 cmkp and within limits.
O 159.868 cmkp and out of limits.
O 176.681 cmkp and out of limits.
O 134.583 cmkp and within limits.

Question 23

Question

233 After new equipment installed on aeroplane, as in technical certificate shown in Fig. 34, what's the Basic Empty Mass and total moments(/100)?

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662184ad-743a-4b8e-94e2-d8e77603680b (image/jpeg)

Answer

O 977,9 Kg and 93155 cmkp.
O 968,0 Kg and 92751 cmkp
O 975,0 Kg and 93045 cmkp.
O None of them becomes true, since BEM is not affected by adding or removing any basic equipment from cockpit.

Question 24

Question

234 With reference to airplanes, what is that plane from which the centers of gravities of all masses are referenced?

Answer

O The Datum
O The Centre of Gravity
O The Normal or Vertical Axis
O The Centre of Pressure

Question 25

Question

235 If air density is reduced, full throttle take-off distance will be:

Answer

O Increased
O Reduced
O The same because increased thrust is balanced by increased drag
O The same because the aircraft will accelerate quicker due to decrease drag.

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8 FLIG. PER. EXAM. PREP.

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Question 2

Question 3

Question 4

Question 5

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Question 11

Question 12

Question 13

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