How much useable fuel should on board at start-up given the following planning information:

APU fuel flow    ----------- 150 kg/h

Taxi fuel flow    ------------ 11 kg/minute

APU time            ----------  38 minutes

Taxi                      ----------- 13 minutes

Trip fuel (including contingency) ------------ 4250 kg

Alternate and Final Reserve fuel -------------3730 kg

Which one of the statements below regarding the distance from departure to the Point of Equal Time (PET) is correct?

Flying from Manchester to Alicante, using the GSPRM Manuals ALICANTA 10-2B.

Locate the best STAR that would take you through VILNA?

Assuming the following data:

Ground distance to be covered 2000 NM

Cruise flight level FL330

Cruising speed M 0.82 (TAS 470 kts)

Headwind component 30 kts

Planned destination Landing Mass 160 000 kg

Temperature ISA 

CG 37%

Total anti-ice ON

Pack flow Hi

Fuel needed to carry out such a flight is?

Given the following information for a Commercial Air Transport flight: 

Missed Approach at destination: 6 min 

Climb to cruise level: 7 min 

Cruise distance: 85 NM 

Cruise TAS: 165 kt 

Tailwind component: 10 kt 

Anticipated hold at alternate: 10 min 

Descent to alternate: 6 min Approach to alternate: 7 min.

What is the time (in minutes) needed from the destination to the alternate aerodrome?

Given:

Distance from departure to destination 1100 NM

True track 280°

W/V 100/80

TAS 440 kts

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

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 hr 30 min and the fuel flow will be 600 kg/h. Final Reserve Fuel remains unchanged.

What will be the estimated landing mass at the alternate airport?

Given the following information for a Commercial Air Transport operation, calculate the maximum possible Extra Fuel, including any fuel penalty, that can be uplifted?

MTOM: 875000 lb

MLM: 652000 lb

MZFM: 555100 lbs

DOM: 394100 lbs

Traffic Load: 109350 lbs

Trip Fuel: 289750 lbs

Planned T/O Fuel: 315315 lbs

Taxi Fuel: 1600 lbs

Fuel burn correction per 1000lb of Extra Fuel based upon: TOM: +470lb and LDM: + 887lb

Tank capacity: 377750 lbs

Given the following information, what is the total fuel required for an IFR Commercial Air Transport flight from A to B with alternate with a turbine-engine aircraft?

Taxi Fuel 250 kg

Trip Fuel 4520 kg

Alternate Fuel 236 kg

Fuel flow for Final Reserve Fuel 2510 kg/h

During the pre-flight planning procedure of a Commercial Air Transport flight, the pilot reviews the serviceability of the GNSS via NOTAMs. What is the optimum decision, if, according to a NOTAM, fluctuations of the signal reception will take place during the RNP approach at the destination aerodrome at the time of arrival?

If 567 kg of fuel at Specific Gravity 0.812 are on board an aircraft, the amount of fuel in US gallons is?

For an IFR flight from the departure aerodrome A to the destination aerodrome B, the decision point procedure has to be applied, considering a Decision Point DP and an optional refuel destination C. Given the following information, how much Trip Fuel is required?

Distance from A to B: 2100 NM

Distance from A to C: 1150 NM

Distance from A to DP: 980 NM

TAS: 410 kt

Fuel flow: 2800 kg/h

Tailwind Component: 12 kt

Greece Directory 7-3. Refer to Jeppesen Student Manual - Greece Aerodrome Directory (7-3) or figure VFR-9

What is the local time (LT) in Greece in ________ Winter and _______ Summer?

For the medium range transport aeroplane, from the Loading Manual.

Determine the maximum total volume of fuel which can be loaded into the main wing tanks?

Fuel density value 078 (Note for conversion use formula 1 US gallon = 3.785 liters) 

Refer to ALICANTE - charts 19-1, 19-2 and 19-3 from Jeppesen GSPRM 2017.

What is the maximum altitude following the Tabarca route?

A twin-jet aeroplane is being operated for a Commercial Air Transport flight. The Reduced Contingency Fuel (RCF) procedure is being applied. Given the following information, find the sum of the required Trip Fuel and Contingency Fuel?

TAS: 400 kt

Wind DEP-DP-DEST: 50 kt tailwind

Wind DP-A: 20 kt tailwind

Fuel consumption: 1500 kg/h

Alternate Fuel for DEST: 1000 kg

Alternate Fuel for A: 900 kg

Additional Fuel for DEST: not required

Additional Fuel for A: 900 kg

Extra Fuel: not required

The quantity of fuel which is calculated to be necessary for a jet aeroplane to fly IFR from departure aerodrome to the destination aerodrome is 5352 kg.

Fuel consumption in holding mode is 6000 kg/hr

Alternate fuel is 4380 kg

Contingency should be 5% of Trip Fuel

What is the minimum required quantity of fuel which should be on board at take-off?

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

You must fly IFR on an airway orientated 135° magnetic with a MSA at 7800 ft. Knowing the QNH is 1 025 hPa and the temperature is ISA +10°, the minimum flight level you must fly at is?

Refer to ALICANTE - chart 10-2G from Jeppesen GSPRM.

Which approach is possible on Runway 28?

A flight from aerodrome H to aerodrome G is planned using the Reduced Contingency Fuel (RCF) procedure aiming to increase the traffic load. The decision point along the route is DP and aerodrome R is the optional refueling destination.

Given the following data, calculate the minimum fuel required for from H to G?

Taxi fuel at aerodrome H: 160 kg

Final Reserve Fuel: 1200 kg

Trip fuel from H to G via DP: 7800 kg

Trip fuel from H to R via DP: 7250 kg

Trip fuel from DP to G: 3050 kg

Alternate fuel and Extra Fuel is NOT required and an En-Route Alternate aerodrome (ERA) for the optional refuel station is NOT available.

Given:

Distance from departure to destination 2000 NM

Safe Endurance 5 hrs

TAS 500 kts

Ground speed out 480 kts

Ground speed home 520 kts

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

Refer to figure.

For this question use VFR chart ED-4 from the Jeppesen GSPRM 2017.

The track between Regensburg Oberhub aerodrome (EDNR) (N49° 09', E012º 05) and Strunkovice aerodrome (LKSR) (N49° 05, E014° 05') is 092° (T). 

What is the magnetic track?

Given

Cruising FL75

Mixture lean

Full throttle 2300 RPM

Take-off fuel 444 lbs.

Take-off from MSL

Find endurance in hours?

Given the following information about a Commercial Air Transport flight with a jet aircraft, determine the minimum fuel required?

Trip Fuel 72340 kg

Fuel to alternate 4589 kg

Fuel flow at 1500 feet above destination aerodrome 5592 kg per hour

Taxi Fuel 345 kg

Refer to figure.

What is the highest obstacle within 4 NM of the road A9, proceeding south from MIKE NDB (N48°34', E 011'36') to where it crosses the railway line north-east of OBERSCHLEISSHEIM aerodrome (EDNX) (N 48°14', E011°34')?