For a long-distance flight at FL 390, 'Long Range' regime, divided into four flight legs with the following characteristics segment AB?

Ground distance 2000 NM, head wind component 50 kt

segment BC?

Ground distance 1000 NM, head wind component 30 kt

segment CD?

Ground distance 500 NM, tail wind component 100 kt

segment DE?

Ground distance 1000 NM, head wind component 70 kt

The air distance of the entire?

An aircraft is flying a route from position A to B, a distance of 57 Nautical Ground Miles (NGM). Given the following information: True Airspeed (TAS): 145 kt Forecast wind: 240°/30 kt Course: 205° (M) Variation: 15°.

 What is the distance covered in Nautical Air Miles (NAM)?

What is the difference between an RNAV STAR and RNAV STAR overlay?

Given the following information, at what distance should the pilot commence the descent in order to arrive overhead the airfield at 2000 ft?

Cruise level: FL95

GS: 155 kt

TAS: constant

Wind component: negligible

Temperature: ISA

QNH: 1030 hPa

Rate of descent: 500 ft/min

In Commercial Air Transport operations, the purpose of Contingency Fuel is to?

When completing an ATC flight plan for a flight commencing under IFR but possibly changing to VFR, the letters entered in Item 8 (FLIGHT RULES) would be?

An aeroplane with reciprocating engines is planning to depart for an isolated destination aerodrome, as a Commercial Air Transport operation. Calculate the minimum amount of fuel required when overhead the isolated aerodrome, considering the following details?

Flight time: 2 hours and 45 minutes

Top of climb to top of descent time: 2 hours

Normal fuel consumption at cruise: 600 kg per hour

Use the following information to calculate the total amount of fuel required for a Commercial Air Transport flight in a Medium Range Jet Transport MRJT aeroplane, with no destination alternate?

APU fuel flow: 115 kg/h

Taxi Fuel: 11 kg per minute

Planned APU usage at the parking position: 15 minutes

Planned taxi time: 15 minutes at both departure and destination aerodromes

Total trip distance: 315 NM

Average fuel flow: 2878 kg/h

TAS: 440 kt

Average headwind component: 16 kt

Contingency Fuel: 5 minutes Holding Fuel Holding fuel flow: 2200 kg/h

Answer in KG

Determine the Take-off Mass (TOM) for the following single engine aeroplane.

Given Basic Empty Mass 1764 lbs Optional Equipment 35 lbs Pilot + Front seat passenger 300 lbs Cargo Mass 350 lbs Take-off Fuel 60 Gal Trip Fuel 35 Gal Fuel density 6 lbs/Gal

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?

An aircraft flies a planned heading of 040* according to the forecast wind of 160° T40 kt.

If the aircraft finally experiences in-flight a wind of 100*(T40 kt, which of the following statements is correct?

The engines always feed from each individual inner tank (left engine from left tank and right engine from right tank).

The trim tank transfer all content to the inner tanks when the inner tanks have less than 4000kg.

The outer tanks transfer all content to the inner tanks when the inner tanks have less than 3500 kg.

The fuel state of the aeroplane is as follows:

Trim tank: Full.

Outer tanks: Full.

During the flight, the trim tank transfer pump fail when the total fuel on board is 18620 kg. What is the Remaining endurance if the aeroplane fuel consumption is 96 kg/min?

The maximum wind velocity (*/kts) immediately north of TUNIS (36° N 010" E) is?

Refer to GSPRM-VFR Chart ED-4.

Find the magnetic course for a flight from Germany to Czech Republic?

Departure airfield is REGENSBURG (EDNR, N49° 08.52' E012 04.92') and destination airfield is STRUNKOVICE (LKSR, N49*4.95’E14*4.55').

The engines always feed from each individual inner tank (left engine from left tank and right engine from right tank)?

When the inner tanks have 4000 kg fuel in them the trim tack transfer all its content evenly between the two inner tanks.

When the inner tanks have less than 3500 kg the outer tanks transfer all their content into their respective inner tank via transfer valves.

During flight when the fuel quantity reaches 12730 kg the left-hand transfer valve between the left outer and inner tanks fail to open.

What is the remaining endurance for the right engine if the fuel flow is 5420 kg/h?

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

A VFR flight intends to land at Alicante Aerodrome (LEAL). The aircraft is currently overhead VFR report point SE, following the Tabarca route to intercept the South Route. The pilot expects delays, as the airport is busy with IFR arrivals and departures.

Where might the pilot be expected to hold?

Given the following information, what will be the Estimated Time of Overflight (ETO) and estimated remaining fuel at waypoint C?

Refer to GSPRM Jeppesen VFR Plates ALICANTE 19-1 and 19-3.

You are approaching from the SW, VFR along the coast to recover to land;

What is the latest time you contact Alicante TWR?

Refer to E LO 1

An aircraft is following the route Y906, approaching overhead position RIMOL (N57,33, w004*,03). Using the below, what WCA is needed to follow the route N560 southbound towards Glasgow VOR(GOW)?

MH 118

W/V 338"/45kts

Tas 200 kt

What will be the approximate change in air distance available from 1000 kg of fuel for the following situation if the tailwind component increases from 45 kt to 65 kt? 

Aircraft mass at start of cruise leg 50000 kg 

Cruise level FL370 

Cruise speed Mach 0.74

The aeroplane uses fuel in the following order:

Each engine feeds from the inner tank of the wing (Left engine feeds from Left Inner Tank; Right Engine from Right Inner Tank) When the inner tanks have 4000 Kg then the Trim Tank transfers all its contents equally to the Inner Tanks. When the Inner Tanks have 3500 Kg then the Outer tanks transfer their contents to the Inner Tanks via Transfer Valves.

Fuel state: Outer Tanks FULL Trim Tank FULL

During the flight the Trim Tank transfer pump fails when the total fuel on board is 18620 Kg

What is the Aeroplanes Total Endurance if the fuel consumption is 96 Kg/Min?

Given the following information, calculate the distance from position A to the Point of Safe Return (PSR):

Distance from A to B: 2900 NM 

True airspeed: 470 kt 

Average wind component "out": +55 kt 

Average wind component "back": -75 kt 

Safe Endurance: 9 h 30 min

For which flights are Flight Plans required?

1) IFR flights.

2) IFR and VFR flights.

3) Flights crossing national boundaries.

4) Flights over water.

5) Public transport flights.