GsPilot

1/30

Question ID: 104065

Using GSPRM Allicante 13-2-Approaching LEAL, due to a tailwind last minute you cannot land and must carry out a missed approach. What must you do?

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A

Continue the approach anyway

B

Declare a mayday

C

Fly to the south of the aerodrome and land on runway 28

D

Fly to the north of the aerodrome and land on runway 28

2/30

Question ID: 118117

Given the following data:
Cruise TAS: 120 kt.
Fuel flow in cruise: 22 USG/h.
Cruise distance: 150 NM.
Once the climb is completed, there is 20 kt of headwind.

What is the cruise fuel?

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A

33 USG

B

25 USG

C

27 USG

D

35 USG

3/30

Question ID: 104033

GSPRM Using the Alicante VFR chart 19-1. What is the maximum height in Tabarca route?

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A

2000FT

B

1500FT

C

1000FT

D

2500FT

4/30

Question ID: 104772

An aircraft operating as Commercial Air Transport is flying from Paris to Barcelona. Using the following information, determine the Contingency Fuel required?
Trip Fuel: 4560 kg
Fuel flow at 1500 feet above destination aerodrome: 2304 kg/h
Fuel penalty when flying 2000 feet lower than optimum altitude: 232 kg
Answer in KG

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A

258

B

238

C

248

D

228

5/30

Question ID: 103866

ED 4, VFR flight from LOLK to LOLF. Which of the following nav aids would be a suitable radio navigation aid for the flight?

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A

N46°26'; E015'08'

B

N48°26'; E014°08'

C

N48°26'; E011°08'

D

N45°26'; E014°08'

6/30

Question ID: 104701

Given Planning data as shown in the Flight Log excerpt (Fuel Planning Section)
After a balked landing at the destination airport, you have to divert to the alternate airport with the gear extended. The re-calculated flight time to the alternate due to the reduced speed is 1 h 20 min and the fuel flow will be 720 kg/h. Final Reserve Fuel remains unchanged. What will be the estimated landing mass at the alternate airport?

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A

6749 kg

B

5320 kg

C

5669 kg

D

6175 kg

7/30

Question ID: 104198

Which of the following statements regarding filing a flight plan is correct?

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A

Any flight plan should be filed at least 10 minutes before departure

B

In case of ATFM (Air Traffic Flow Management) the flight plan should be filed at least three hours in advance of the EOBT

C

A flight plan should be filed when a national FIR boundary will be crossed

D

A flying college can file repetitive flight plan for VFR flights

8/30

Question ID: 104476

Given
Maximum structural take-off mass 7400 kg
Maximum structural landing mass 7400 kg
Zero Fuel Mass 5990 kg
Taxi Fuel 15 kg
Contingency Fuel 110 kg
Alternate Fuel 275 kg
Final Reserve Fuel 250 kg Trip Fuel 760 kg
The expected Landing Mass (LM) at destination will be?

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A

6625 kg

B

7135 kg

C

7385 kg

D

7400 kg

9/30

Question ID: 104462

Conversion of fuel volume to mass?

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A

Must be done by using standard fuel density values as specified in EASA AIR OPS

B

Must be done using fuel density values of 0.79 for JP 1 and 0.76 for JP 4 as specified in EASA AIR OPS

C

Must be done by using actual measured fuel density values

D

May be done by using standard fuel density values as specified by the Operations Manual, if the actual fuel density is not known

10/30

Question ID: 118205

Which of the following is (are) Type B approach(es)?
1. ILS DH = 230ft
2. VOR DH = 250ft
3. VOR DH = 270ft

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A

1 only

B

1 and 3 only

C

2 and 3 only

D

1 and 2 only

11/30

Question ID: 103922

ELO 2. You are at TULIP heading North on P1 route. You accidentally hit the frequency and changed it. What frequency do you reset to?

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A

Amsterdam 123.705

B

Lisse 124.705

C

Amsterdam 125.75

D

Munich 127.05

12/30

Question ID: 104792

Given: True Airspeed: 100 kt Fuel flow: 9.6 US gal Remaining fuel: 50 US gal Wind component: 15 kt (tailwind) Calculate the remaining total flight time and distance?

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A

5 hours 20 minutes and 599 NM

B

5 hours 13 minutes and 599 NM

C

5 hours 20 minutes and 443 NM

D

5 hours 13 minutes and 521 NM

13/30

Question ID: 103852

What is a possible entry for ITEM 15 CRUISING SPEED for the following flight? Flight rules VFR Cruise level FL80 Temperature is Cruise speed 90 kt IAS Wind component-12 kt Holding speed 62 kt IAS

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A

N0090

B

K0090

C

N0100

D

K0150

14/30

Question ID: 104553

Given
Cruise FL300/M 0.78
Distance B-C 800 NM
Temperature -55°C
Headwind component 50 kts
Gross mass at B 64500 kg
The fuel required from B-C is?

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A

4975 kg

B

6000 kg

C

6150 kg

D

5050 kg

15/30

Question ID: 104285

A flight is to be made in a multi engine piston aeroplane:
The cruising level will be 11000 ft
The outside air temperature at FL is -15°C
The usable fuel is 123 US gallons
The power is set to economy cruise

Find the range in NM with 45 min reserve fuel?

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A

852 NM

B

752 NM

C

610 NM

D

602 NM

16/30

Question ID: 104613

Given the following information, find the minimum required Additional Fuel for a Commercial Air Transport flight with a twin-jet aeroplane to an isolated aerodrome
Fuel consumption enroute 2100 kg/h
Fuel consumption in holding 1200 kg/h
No enroute alternate exists?

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A

300 kg

B

2400 kg

C

4200 kg

D

600 kg

17/30

Question ID: 104339

Given:
Distance A to B 1973 NM
Ground speed OUT 430 kts
Ground speed BACK 385 kts

The time from A to the point of equal time (PET) between A and B is?

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A

145 min

B

181 min

C

162 min

D

130 min

18/30

Question ID: 118133

Which one of the following cases require the submission of an ATC flight plan?
1. Commercial Air Transport flight
2. IFR flight
3. Any flight carried out in regions are designated to ease the provision of the Alerting Service or the operations of Search and Rescue
4. Cross-border flights
5. Overwater flight

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A

1, 5

B

1, 2, 3

C

3, 4, 5

D

2, 4

19/30

Question ID: 104265

Given the following Commercial Air Transport operation, calculate the maximum possible Extra Fuel, including any fuel penalty, that can be uplifted.
MZFM:51,300 kg
MTOM:62,800 kg
MLM: 57,900 kg
Planned ZFM:48,200 kg
Fuel tank capacity: 17,000 kg
Planned T/O Fuel: 8,484kg
Planned trip fuel: 6100 kg
Fuel burn correction per 1000 kg of Extra Fuel based upon: TOM: +135 kg and LDM: + 156 kg
Answer in KG

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A

6136

B

6116

C

6126

D

6146

20/30

Question ID: 104328

An aircraft has a TAS of 300 kts and a safe endurance of 10 hrs. If the wind component on the outbound leg is 50 kts head.
What is the distance to the point of safe return?

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A

1622 NM

B

1500 NM

C

1458 NM

D

1544 NM

21/30

Question ID: 119804

A mountain 6 011 ft AMSL will be crossed. What is the lowest VFR ICAO level the aircraft must fly to obtain a clearance of 2000 ft?
Given:
Variation: 10°W
Aircraft's Track: 356° T
Aircraft's HDG: 355° M
QNH: 990 hPa
Assume 1 hPa = 30 ft

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A

FL115

B

FL085

C

FL090

D

FL095

22/30

Question ID: 104099

Refer to NANTES - Charts 19-1, 19-2, 19-3 from Jeppesen GSPRM 2017.

What is the distance between reporting points E1 and E2? Answer in NM (1NM tolerance each-way given)

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A

6

B

9

C

7

D

8

23/30

Question ID: 104780

Calculate the maximum possible extra fuel, based on the flight and aircraft data given below?
MTOM: 476100 lb
MLM: 387350 lb
MZFM: 362700 lb
Planned ZFM: 323450 lb
Trip fuel: 72460 lb
Take-off fuel:124830 lb
Fuel penalty:630 lb/1 000 lb
Answer in LBS

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A

18493

B

18693

C

18593

D

18793

24/30

Question ID: 103897

What is the Minimum Descent Altitude for a Cat A aircraft completing an LNAV approach to runway 32R at Toulouse Blagnac (LFBO)?

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A

430 ft

B

428 ft

C

930 ft

D

1500 ft

25/30

Question ID: 119741

Refer to ALICANTE - charts 19-1, 19-2 and 19-3 from Jeppesen GSPRM 2017.
What is the elevation of the highest obstacle on the chart?

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A

1821 ft AMSL

B

FL75

C

4252 ft AMSL

D

5000 ft AGL

26/30

Question ID: 104272

An aircraft has a MTOM of 7500kgs, but on a given day has a takeoff mass of 5,000KG What letter should you insert into item 9 of the flight plan?

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A

H

B

L

C

M/L

D

M

27/30

Question ID: 118198

Refer to Aberdeen (Dyce) chart 19-1 from the Jeppesen GSPRM 2017.

Which ATIS frequency(ies) is/are available when still on the ground?

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A

114.300 MHz only

B

121.850 MHz only

C

121.700 MHz only

D

114.300 MHz and 121.850 MHz

28/30

Question ID: 114224

If the actual in-flight wind produces a greater headwind than the forecast wind input into the FMC, what should be expected?

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A

The optimum level will be lowered

B

Earlier ETAs will be generated by the FMC

C

A new cruise level will be generated by the FMC

D

Speeds will be increased to maintain ETAs

29/30

Question ID: 104385

Given:
Distance from departure to destination 950 NM
Safe Endurance 3.5h
TAS 360 kt
Ground Speed Out 320 kt
Ground Speed Home 400 kt

What is the distance and time of the PSR from the departure point?

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A

Distance: 311 NM Time: 52 min

B

Distance: 622 NM Time: 117 min

C

Distance: 528 NM Time: 79 min

D

Distance: 328 NM Time: 62 min

30/30

Question ID: 104490

Refer to CAP FIGURE 3.1
A flight is to be made from one airport (elevation 3000 ft) to another in a multi engine piston aeroplane:
The cruising level will be FL110
The temperature at FL110 is ISA-10°C
The temperature at the departure aerodrome is -1°C
Calculate the fuel to climb with mixture rich?

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A

3 US gallons

B

10 US gallons

C

6 US gallons

D

12 US gallons

Question ID: 104065

Using GSPRM Allicante 13-2-Approaching LEAL, due to a tailwind last minute you cannot land and must carry out a missed approach. What must you do?

A

B

C

D

Question ID: 118117

Given the following data:Cruise TAS: 120 kt.Fuel flow in cruise: 22 USG/h.Cruise distance: 150 NM.Once the climb is completed, there is 20 kt of headwind.What is the cruise fuel?

A

B

C

D

Question ID: 104033

GSPRM Using the Alicante VFR chart 19-1. What is the maximum height in Tabarca route?

A

B

C

D

Question ID: 104772

A

B

C

D

Question ID: 103866

ED 4, VFR flight from LOLK to LOLF. Which of the following nav aids would be a suitable radio navigation aid for the flight?

A

B

C

D

Question ID: 104701

A

B

C

D

Question ID: 104198

Which of the following statements regarding filing a flight plan is correct?

A

B

C

D

Question ID: 104476

Given Maximum structural take-off mass 7400 kg Maximum structural landing mass 7400 kg Zero Fuel Mass 5990 kg Taxi Fuel 15 kg Contingency Fuel 110 kg Alternate Fuel 275 kg Final Reserve Fuel 250 kg Trip Fuel 760 kg The expected Landing Mass (LM) at destination will be?

A

B

C

D

Question ID: 104462

Conversion of fuel volume to mass?

A

B

C

D

Question ID: 118205

Which of the following is (are) Type B approach(es)?1. ILS DH = 230ft2. VOR DH = 250ft3. VOR DH = 270ft

A

B

C

D

Question ID: 103922

ELO 2. You are at TULIP heading North on P1 route. You accidentally hit the frequency and changed it. What frequency do you reset to?

A

B

C

D

Question ID: 104792

Given: True Airspeed: 100 kt Fuel flow: 9.6 US gal Remaining fuel: 50 US gal Wind component: 15 kt (tailwind) Calculate the remaining total flight time and distance?

A

B

C

D

Question ID: 103852

What is a possible entry for ITEM 15 CRUISING SPEED for the following flight? Flight rules VFR Cruise level FL80 Temperature is Cruise speed 90 kt IAS Wind component-12 kt Holding speed 62 kt IAS

A

B

C

D

Question ID: 104553

GivenCruise FL300/M 0.78Distance B-C 800 NMTemperature -55°CHeadwind component 50 ktsGross mass at B 64500 kgThe fuel required from B-C is?

A

B

Given the following data:
Cruise TAS: 120 kt.
Fuel flow in cruise: 22 USG/h.
Cruise distance: 150 NM.
Once the climb is completed, there is 20 kt of headwind.

What is the cruise fuel?

Given
Maximum structural take-off mass 7400 kg
Maximum structural landing mass 7400 kg
Zero Fuel Mass 5990 kg
Taxi Fuel 15 kg
Contingency Fuel 110 kg
Alternate Fuel 275 kg
Final Reserve Fuel 250 kg Trip Fuel 760 kg
The expected Landing Mass (LM) at destination will be?

Which of the following is (are) Type B approach(es)?
1. ILS DH = 230ft
2. VOR DH = 250ft
3. VOR DH = 270ft

Given
Cruise FL300/M 0.78
Distance B-C 800 NM
Temperature -55°C
Headwind component 50 kts
Gross mass at B 64500 kg
The fuel required from B-C is?

A flight is to be made in a multi engine piston aeroplane:
The cruising level will be 11000 ft
The outside air temperature at FL is -15°C
The usable fuel is 123 US gallons
The power is set to economy cruise

Find the range in NM with 45 min reserve fuel?

Given the following information, find the minimum required Additional Fuel for a Commercial Air Transport flight with a twin-jet aeroplane to an isolated aerodrome
Fuel consumption enroute 2100 kg/h
Fuel consumption in holding 1200 kg/h
No enroute alternate exists?

Given:
Distance A to B 1973 NM
Ground speed OUT 430 kts
Ground speed BACK 385 kts

The time from A to the point of equal time (PET) between A and B is?

An aircraft has a TAS of 300 kts and a safe endurance of 10 hrs. If the wind component on the outbound leg is 50 kts head.
What is the distance to the point of safe return?

A mountain 6 011 ft AMSL will be crossed. What is the lowest VFR ICAO level the aircraft must fly to obtain a clearance of 2000 ft?
Given:
Variation: 10°W
Aircraft's Track: 356° T
Aircraft's HDG: 355° M
QNH: 990 hPa
Assume 1 hPa = 30 ft

Refer to NANTES - Charts 19-1, 19-2, 19-3 from Jeppesen GSPRM 2017.

What is the distance between reporting points E1 and E2? Answer in NM (1NM tolerance each-way given)