8 FLIG. PER. EXAM. PREP.

Question 1 of 25

1

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?

Select one of the following:

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

Explanation

Question 2 of 25

1

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

Select one of the following:

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

Explanation

Question 3 of 25

1

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

Select one of the following:

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

Explanation

Question 4 of 25

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

Select one of the following:

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.

Explanation

Question 5 of 25

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215 The Maximum Structural Take-off Mass is:

Select one of the following:

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,

Explanation

Question 6 of 25

1

216 The Take-off mass is:

Select one of the following:

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.

Explanation

Question 7 of 25

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

Select one of the following:

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.

Explanation

Question 8 of 25

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

Select one of the following:

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

Explanation

Question 9 of 25

1

219 The Basic Empty Mass is the:

Select one of the following:

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

Explanation

Question 10 of 25

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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

Select one of the following:

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

Explanation

Question 11 of 25

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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

Select one of the following:

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

Explanation

Question 12 of 25

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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 _ _

Select one of the following:

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

Explanation

Question 13 of 25

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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 - -

Select one of the following:

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

Explanation

Question 14 of 25

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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 - -

Select one of the following:

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

Explanation

Question 15 of 25

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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?

Select one of the following:

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.

Explanation

Question 16 of 25

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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?

Select one of the following:

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.

Explanation

Question 17 of 25

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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

Select one of the following:

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

Explanation

Question 18 of 25

1

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

Select one of the following:

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.

Explanation

Question 19 of 25

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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:

Select one of the following:

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

Explanation

Question 20 of 25

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230 Pressure Altitude is?

Select one of the following:

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.

Explanation

Question 21 of 25

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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

Select one of the following:

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.

Explanation

Question 22 of 25

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

Select one of the following:

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.

Explanation

Question 23 of 25

1

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)?

Select one of the following:

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.

Explanation

Question 24 of 25

1

	Created by tsampikos pompou over 8 years ago

	Copied by tsampikos pompou over 8 years ago

8 FLIG. PER. EXAM. PREP.

8 FLIG. PER. EXAM. PREP.

Question 1 of 25

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?

Select one of the following:

Explanation

Question 2 of 25

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

Select one of the following:

Explanation

Question 3 of 25

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

Select one of the following:

Explanation

Question 4 of 25

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

Select one of the following:

Explanation

Question 5 of 25

215 The Maximum Structural Take-off Mass is:

Select one of the following:

Explanation

Question 6 of 25

216 The Take-off mass is:

Select one of the following:

Explanation

Question 7 of 25

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

Select one of the following:

Explanation

Question 8 of 25

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

Select one of the following:

Explanation

Question 9 of 25

219 The Basic Empty Mass is the:

Select one of the following:

Explanation

Question 10 of 25

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

Select one of the following:

Explanation

Question 11 of 25

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

Select one of the following:

Explanation

Question 12 of 25

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 _ _

Select one of the following:

Explanation

Question 13 of 25

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 - -

Select one of the following:

Explanation

Question 14 of 25

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 - -

Select one of the following:

Explanation

Question 15 of 25

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?

Select one of the following:

Explanation

Question 16 of 25

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?

Select one of the following:

Explanation

Question 17 of 25

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

Select one of the following:

Explanation

Question 18 of 25

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

Select one of the following:

Explanation

Question 19 of 25

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:

Select one of the following:

Explanation

Question 20 of 25

230 Pressure Altitude is?

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?

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

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

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

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

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 _ _

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 - -

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 - -

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

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

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: