A sector distance is 450 NM long. The TAS is 460 kt. The wind component is 50 kt tailwind. What is the still air distance?

(For this question use annex 033-3301A or Flight Planning Manual MEP1 Figure 3.1) A flight is to be made from one airport (elevation 3000 ft) to another in a multi engine piston aireroplane (MEP1). The cruising level will be FL 110. The temperature at FL 110 is ISA - 10° C. The temperature at the departure aerodrome is -1° C. Calculate the fuel to climb with mixture rich.

(For this question use annex 033- 11043A or Route Manual STAR charts for PARIS CHARLES DE GAULLE (20-2)) The route distance from CHIEVRES (CIV) to BOURSONNE (BSN) is :

Unless otherwise shown on charts for standard instrument departure the routes are given with:

(For this question use annex 033-3317A or Route Manual chart E(HI)4 CAA-Edition) An aeroplane has to fly from Salzburg (48° 00.2"N 012° 53.6"E) to Klagenfurt (46° 37.5"N 014° 33.8"E). At Salzburg there is stated on the chart D 113.8 SBG. That means :

The still air distance in the climb is 189 Nautical Air Miles (NAM) and time 30 minutes. What ground distance would be covered in a 30 kt head wind?

In the appropriate box of a flight plan, for endurance, one must indicate the time corresponding to:

Given: Maximum allowable take-off mass 64 400 kg. maximum landing mass 56200 kg. maximum zero fuel mass 53 000 kg. dry operating mass 35 500 kg. estimated load 14 500 kg. estimated trip fuel 4 900 kg. minimum take-off fuel 7 400 kg. Find: maximum additional load

(For this question use annex 033-11704A) True Air speed: 170 kt W ind in the area: 270° /40 kt According to the attached the navigation log, an aircraft performs a turn overhead BULEN to re- route to ARD via TGJ. The given wind conditions remaining constant. The fuel consumption during the turn is 20 litres. The total fuel consumption at position overhead ARD will be:

The maximum permissible take-off mass of an aircraft for the L wake turbulence category on a flight plan is:

(For this question use annex 033-3302A or Flight Planning Manual MEP1 Figure 3.6) A flight is to be made to an airport, pressure altitude 3000 ft, in a multi engine piston aireroplane (MEP1). The forecast OAT for the airport is -1° C. The cruising level will be FL 110, where OAT is -10° C. Calculate the still air descent distance for: 145 KIAS Rate of descent 1000 ft/min Gears and flaps up

The cruising speed to write in the appropriate box of a flight plan is:

(For this question use annex 033-3316A or Route Manual chart E(HI)4 CAA-Edition) An aeroplane has to fly from Salzburg (48° 00.2"N 012° 53.6"E) to Klagenfurt (46° 37.5"N 014° 33.8"E). Which statement is correct ?

(For this question use annex 033-9716A or Flight Planning Manual SEP 1 Figure 2.4) Given: Aeroplane mass at start-up 3663 lbs, Aviation gasoline (density 6 lbs/gal)-fuel load 74 gal, Take-off altitude sea level, Headwind 40 kt, Cruising altitude 8000 ft, Power setting full throttle 2300 RPM 20° C lean of peak EGT Calculate the range.

(For this question use annex 033-9715A or Flight Planning Manual SEP 1 Figure 2.1) Given: Take-off mass 3500 lbs, departure aerodrome pressure altitude 2500 ft, OAT +10°C , First cruising level: FL 140, OAT -5°C Find the time, fuel and still air distance to climb.

(For this question use annex 033-9712A and 033-9712 B or Route Manual STAR 10-2 and Instrument approach chart 11-4 ILS/DME Rwy 27R for London (Heathrow)) Planning an IFR-flight from Paris to London (Heathrow). Name the identifier and frequency of the initial approach fix (IAF) of the BIG 2A arrival route.

In the cruise at FL 155 at 260 kt TAS, the pilot plans for a 500 feet/min descent in order to fly overhead MAN VOR at 2 000 feet (QNH 1030). TAS will remain constant during descent, wind is negligible, temperature is standard. The pilot must start the descent at a distance from MAN of:

Given:maximum allowable take-off mass 64 400 kg maximum landing mass 56 200 kg maximum zero fuel mass 53 000 kg dry operating mass 35 500 kg estimated load 14 500 kg estimated trip fuel 4 900kg minimum take- off fuel 7 400 kg Find the maximum allowable take-off fuel:

An aircraft is in cruising flight at FL 095, IAS 155kt. The pilot intends to descend at 500 ft/min to arrive overhead the MAN VOR at 2 000 FT (QNH 1 030hPa). The TAS remains constant in the descent, wind is negligeable, temperature standard. At which distance from MAN should the pilot commence the descent?

In the appropriate box of a flight plan form, corresponding to the estimated time of departure, the time indicated is that at which the aircraft intends to :

When a pilot fills in a flight plan, he must indicate the wake turbulence category. This category is a function of which mass?

You are to determine the maximum fuel load which can be carried in the following conditions : - dry operating mass : 2800 kg - trip fuel : 300 kg - payload : 400 kg - maximum take-off mass : 4200 kg - maximum landing mass : 3700 kg

(For this question use annex 033-4737A or Flight Planning Manual SEP 1 Figure 2.1) Given: FL 75 OAT: +5° C During climb: average head wind component 20 kt Take-off from MSL with the initial mass of 3 650 lbs. Find: Time and fuel to climb.

(For this question use annex 033-4738A or Flight Planning Manual SEP 1 Figure 2.1) Given: FL 75 OAT: +5° C During climb: average head wind component 20 kt Take-off from MSL with the initial mass of 3 650 lbs. Find: Still air distance (NAM) and ground distance (NM) using the graph "time, fuel, distance to climb".

(For this question use annex 033- 11021A or Route Manual chart E(HI)4 CAA-Edition) Aeroplanes intending to use airway UR14 should cross GIBSO intersection (50° 45"N 002° 30"W) at or above:

(For this question use annex 033- 11006A or Route Manual chart E(HI)4 CAA-Edition) The radio navigation aid serving STRASBOURG (48° 30"N 007° 34"E) is a: statements is (are) correct with regard to computer flight plans 1. The computer takes account of bad weather on the route and adds extra fuel. 2. The computer calculates alternate fuel sufficient for a missed approach, climb, cruise, descent and approach and landing at the destination alternate.

(For this question use annex 033-11272A) The flight crew of a turbojet aeroplane prepares a flight using the following data: . Take-off mass: 168 500 kg . Flight leg ground distance: 2 000 NM . Flight level FL 370. "Long Range" flight regime . Tailwind component at this level: 30 kt . Total anti-ice set on "ON" . Fixed taxi fuel: 500 kg. final reserve: 2 000 kg . Ignore alternate fuel. The effects of climb and descent are not corrected for consumption. The prescribed quantity of trip fuel for the flight leg is:

(For this question use annex 033-4736A or Flight Planning Manual SEP 1 Table 2.2.3) Given: FL 75 OAT +10° C Lean mixture 2300 RPM Find: Fuel flow in gallons per hour (GPH) and TAS.

The navigation plan reads: Trip fuel: 100 kg Flight time: 1h35min Taxi fuel: 3 kg Block fuel: 181 kg The endurance on the ICAO flight plan should read:

The navigation plan reads: Trip fuel: 136 kg Flight time: 2h45min Calculated reserve fuel: 30% of trip fuel Fuel in tank is minimum (no extra fuel on board) Taxi fuel: 3 kg The endurance on the ICAO flight plan should read:

(For this question use annex 033- 10994A or Route Manual chart E(LO)6 ) The magnetic course/distance from GROSTENQUIN GTQ 111.25 (49° 00"N 006° 43"E) to LINNA (49° 41"N 006° 15"E) on airway R7 is:

(For this question use annex 033-10989A or Route Manual chart E(HI)4 CAA-Edition) Of the following, the preferred airways routing from FRANKFURT FFM 114.2 (50° 03" N008° 38"E) to KOKSY (51° 06"N 002° 39"E) above FL245, on a W ednesday is :

(For this question use annex 033- 10990A or Route Manual chart E(HI)5 CAA-Edition) Of the following, the preferred airways routing from MARTIGUES MTG 117.3 (43° 23"N 005° 05"E) to ST PREX SPR 113.9 (46° 28"N 006° 27"E) above FL245 is :

(For this question use annex 033-10991A or Route Manual chart E(HI)5 CAA-Edition) Of the following, the preferred airways routing from AMBOISE AMB 113.7 (47° 26"N 001° 04"E) to AGEN AGN (43° 53° "N 000° 52"E) above FL200 is:

(For this question use annex 033- 10993A or Route Manual chart E(HI)4 CAA-Edition) The magnetic course/distance from DINKELSBUHL DKB 117.8 (49° 09"N010° 14"E) to ERLANGEN ERL 114.9 (49° 39"N011° 09"E) on airway UR11 is.

(For this question use annex 033- 10995A or Route Manual chart E(LO)5) The magnetic course/distance from ELBE LBE 115.1 (53° 39"N 009° 36"E) to LUNUD (54° 50"N 009° 19"E) on airway H12 is:

(For this question use annex 033- 10996A or Route Manual chart E(LO)5) The initial magnetic course/distance from EELDE EEL 112.4 (53° 10"N 006° 40"E) to W ELGO (54° 18"N 007° 25"E) on airway A7 is:

(For this question use annex 033- 10997A or Route Manual chart E(LO)2) The magnetic course/distance from CAMBRAI CMB 112.6 (50° 14"N 003° 09"E) to TALUN (49° 33"N 003° 25"E) on airway B3 is:

(For this question use annex 033- 10998A or Route Manual chart E(LO)1) The magnetic course/distance from W ALLASEY WAL 114.1 (53° 23N 003° 28"W° to LIFFY (53° 29"N 005° 30"W) on airway B1 is:

(For this question use annex 033- 10999A or Route Manual chart E(HI)4 CAA-Edition) The magnetic course/distance from TRENT TNT 115.7 (53° 03"N 001° 40"W) to W ALLASEY WAL 114.1 (53° 23"N 003° 08W) on airway VR3 is:

(For this question use annex 033- 11000A or Route Manual chart E(HI)4 CAA-Edition) The magnetic course/distance from TANGO TGO 112.5 (48° 37"N 009° 16"E) to DINKELSBUHL DKB 117.8 (49° 09"N 010° 14E) on airway UR11 is:

(For this question use annex 033- 11001A or Route Manual chart E(HI)4 CAA-Edition) The magnetic course/distance from ST PREX SPR 113.9 (46° 28"N 006° 27"E) to FRIBOURG FRI 115.1 (46° 47"N 007° 14"E) on airway UG60 is:

(For this question use annex 033- 10992A or Route Manual chart E(HI)4 CAA-Edition) Of the following, the preferred airways routing from CLACTON CLN 114.55 (51° 51"N 001° 09"E) to DINARD DIN 114.3 (48° 35"N 002° 05"W) above FL245 is:

If your destination airport has no ICAO indicator, in the appropriate box of your flight plan, you write:

(For this question use annex 033-3906A or Route Manual chart SID PARIS Charles-De- Gaulle (20-3)) Planning a IFR flight from Paris (Charles de Gaulle) to London (Heathrow). Find the elevation of the departure aerodrome.

(For this question use annex 033-3907A or Route Manual chart STAR LONDON Heathrow (10-2)) Planning a IFR flight from Paris (Charles de Gaulle) to London (Heathrow). Find the elevation of the destination aerodrome.

(For this question use annex 033-3908A or Route Manual chart E(HI)4 CAA-Edition) Planning a IFR flight from Paris Charles de Gaulle (N49 00.9 E002 36.9) to London Heathrow (N51 29.2 W000 27.9). Find the average true course from Paris to London.

(For this question use annex 033- 11013A or Route Manual chart E(LO)1) The radio navigation aid at SHANNON (52° 43"N 008° 53"W) is :

(For this question use annex 033-3909A or Route Manual chart E(HI)4 CAA-Edition) Planning a IFR flight from Paris Charles de Gaulle (N49 00.9 E002 36.9) to London Heathrow (N51 29.2 W000 27.9). Determine the preplanning distance by calculating the direct distance plus 10%. The preplanning distance is:

(For this question use annex 033- 11002A or Route Manual chart E(HI)4 CAA-Edition) The magnetic course/distance from SALZBURG SBG 113.8 (48° 00"N 012° 54"E) to STAUB (48° 44"N 012° 38"E) on airway UB5 is:

(For this question use annex 033-4622A or Flight Planning Manual MEP 1 Figure 3.3) A flight has to be made with a multi engine piston aeroplane (MEP 1). For the fuel calculations take 5 US gallons for the taxi, and an additional 13 minutes at cruise condition to account for climb and descent. Calculated time from overhead to overhead is 1h47min. Powersetting is 45%, 2600 RPM. Calculated reserve fuel is 30% of the trip fuel. FL 100. Temperature - 5° C. Find the minimum block fuel.

(For this question use annex 033-4623A or Flight Planning Manual MEP 1 Figure 3.3) A flight has to be made with a multi engine piston aeroplane (MEP 1). For the fuel calculations take 5 US gallons for the taxi, and an additional 13 minutes at cruise condition to account for climb and descent. Calculated time overhead to overhead is 2h37min. Powersetting is 65%, 2500 RPM. Calculated reserve fuel is 30% of the trip fuel. FL 120. Temperature 1° C. Find the minimum block fuel.

Which of the following statements is (are) correct with regard to the operation of flight planning computers ? 1. The computer can file the ATC flight plan. 2. In the event of inflight re-routing the computer produces a new plan.

The fuel burn off 200 kg/h with a relative fuel density of 0,8. If the relative density is 0,75, the fuel burn will be:

Which of the following statements is (are) correct with regard to the advantages of computer flight plans ? 1. The computer can file the ATC flight plan. 2. Wind data used by the computer is always more up-to-date than that available to the pilot.

(For this question use annex 033- 11044A or Route Manual SID chart for LONDON HEATHROW (10-3)) Which of the following is a correct Minimum Safe Altitude (MSA) for the Airport?

(For this question use annex 033- 11014A or Route Manual chart E(LO)5) The VOR and TACAN on airway G9 at OSNABRUCK (52° 12"N 008° 17"E) are:

(For this question use annex 033- 11015A or Route Manual chart E(LO)5) The NDB at DENKO (52° 49"N 015° 50"E) can be identified on:

(For this question use annex 033- 11016A or Route Manual chart E(LO)5) The airway intersection at RONNEBY (56° 18"N 015° 16"E) is marked by:

An airway is marked 3500T 2100 a. This indicates that: 3500 ft

(For this question use annex 033- 11003A or Route Manual chart E(HI)5 CAA-Edition) The magnetic course/distance from ELBA ELB 114.7 (42° 44"N 010° 24"E) to SPEZI (43° 49"N 009° 34"E) on airway UA35 is:

(For this question use annex 033- 11045A or Route Manual STAR chart for MADRID BARAJAS (10-2A,B)) For runway 33 arrivals from the east and south, the Initial Approach Fix (IAF) inbound from airway UR10 is :

(For this question use annex 033- 11046A or Route Manual SID charts for ZURICH (10- 3)) Which is the correct ALBIX departure via AARAU for runway 16?

(For this question use annex 033- 11047A or Route Manual SID chart for AMSTERDAM SCHIPHOL (10-3B)) The route distance from runway 27 to ARNEM is:

(For this question use annex 033- 11048A or Route Manual SID chart for AMSTERDAM SCHIPHOL (10-3)) Which of the following statements is correct for ANDIK departures from runway 19L?

(For this question use annex 033- 11049A or Route Manual STAR charts for MUNICH (10- 2A,B)) The correct arrival route and Initial Approach Fix (IAF) for an arrival from the west via TANGO for runway 08 L/R is:

(For this question use annexes 033-12302A and 033-12302B or Flight Planning Manual MRJT 1 Figure 4.5.2 and 4.5.3.1) Given : Distance C - D : 3200 NM Long Range Cruise at FL 340 Temperature Deviation from ISA : +12° C Tailwind component 50 kt Gross mass at C : 55 000 kg The fuel required from C - D is :

(For this question use annex 033- 11040A or Route Manual STAR charts for ZURICH (10- 2,10-2A,10-2B)) Aeroplane arriving via route BLM 2Z only, should follow the following route to EKRON int:

(For this question use annex 033- 11023A or Route Manual chart E(HI)5 CAA-Edition) The minimum enroute altitude available on airway UR160 from NICE NIZ 112.4 (43° 46"N 007° 15"E) to BASTIA BTA 116.2 (42° 32"N 009° 29"E) is:

Following in-flight depressurisation, a turbine powered aeroplane is forced to divert to an en-route alternate airfield. If actual flight conditions are as forecast, the minimum quantity of fuel remaining on arrival at the airfield will be:

On a flight plan you are required to indicate in the box marked "speed" the planned speed for the first part of the cruise or for the entire cruise. This speed is:

(For this question use annex 033- 11004A or Route Manual chart E(HI)5 CAA-Edition) The magnetic course/distance from LIMOGES LMG 114.5 (45° 49"N 001° 02"E) to CLERMONT FERRAND CMF 117.5 (45° 47"N 003° 11"E) on airway UG22 is:

(For this question use annexes 033-12303A and 033-12303B or Flight Planning Manual MRJT 1 Figure 4.5.2 and 4.5.3.1)) Given : Distance C - D : 680NM Long Range Cruise at FL340 Temperature Deviation from ISA : 0° C Headwind component 60 kt Gross mass at C : 44 700 kg The fuel required from C - D is :

(For this question use annex 033-12304A or Flight Planning Manual MRJT 1 Figure 4.5.1) Given : Brake release mass : 58 000 kg Temperature ISA + The fuel required to climb from an aerodrome at elevation 4000 ft to FL300 is :

(For this question use annex 033- 11029A or Route Manual chart E(LO)5) The minimum enroute altitude that can be maintained continuously on airway B65/H65 from DOXON (55° 27"N 018° 10"E) to RONNE ROE 112.0 (55° 04"N 014° 46"E) is :

An airway is marked 5000 2900a. The notation 5000 is the :

(For this question use annex 033- 11027A or Route Manual chart E(LO)2) The minimum enroute altitude (MEA) that can be maintained continuously on airway G4 from JERSEY JSY 112.2 (49° 13"N 002° 03"W) to LIZAD (49° 35"N 004° 20"W) is :

An airway is marked FL 80 1500 a. This indicates that: (MRA).

(For this question use annex 033- 11025A or Route Manual chart E(LO)1) The minimum enroute altitude that can be maintained continuously on airway G1 from STRUMBLE STU 113.1 (52° 00"N 005° 02"W) to BRECON BCN 117.45 (51° 43"N 003° 16"W) is :

((For this question use annex 033- 11024A or Route Manual chart E(HI)4 CAA-Edition) The minimum enroute altitude that can be maintained continuously on airway UA34 from W ALLASEY WAL 114.1 (53° 23"N 003° 08"W) to MIDHURST MID 114.0 (51° 03"N 000° 37"W) is :

(For this question use annex 033-3313A or Route Manual chart E(HI)4 CAA-Edition) An aeroplane has to fly from Abbeville (50° 08.1"N 001° 51.3"E) to Biggin (51° 19.8"N 000° 00.2"E). What is the distance of this leg ?

(For this question use annex 033-3314A or Route Manual chart E(HI)4 CAA-Edition) An aeroplane has to fly from Abbeville (50° 08.1"N 001° 51.3"E) to Biggin (51° 19.8"N 00° 00.2"E). At Biggin you can find : 141° . This is :

(For this question use annex 033-3315A or Route Manual chart E(HI)4 CAA-Edition) An aeroplane has to fly from Salzburg (48° 00.2"N 012° 53.6"E) to Klagenfurt (46° 37.5"N 014° 33.8"E). Which statement is correct ?

A descent is planned from 7500 ft MSL so as to arrive at 1000 ft MSL 6 NM from a VORTAC. With a GS of 156 kts and a rate of descent of 800 ft/min. The distance from the VORTAC when descent is started is :

(For this question use annex 033-9702A or Route Manual SID chart 20-3 for PARIS Carles-de-Gaulle) Planning an IFR-flight from Paris to London. Determine the distance of the departure route ABB 8A.

(For this question use annexes 033-9710A, 033-9710B and 033- 9710C or Route Manual chart E(HI)4 CAA- Edition, STAR 10-2 and Instrument approach chart 11-4 ILS DME Rwy 27R for London Heathrow ) Planning an IFR-flight from Paris to London (Heathrow). Assume: STAR is BIG 2A, Variation 5° W, en- route TAS 430 kts, W /V 280/40, descent distance 76NM. Determine the magnetic course, ground speed and wind correction angle from ABB 116.6(N50 08.1 E001 51.3) to top of descent.

(For this question use annex 033-9709A or SID chart Paris Charles de Gaulle 20-3 ) Planning an IFR-flight from Paris Charles de Gaulle to London. SID is ABB 8A. Assume Variation 3° W , TAS 430kts, W/V 280/40 and distance to top of climb 50NM Determine the magnetic course, ground speed and wind correction angle from top of climb to ABB 116.6.

(For this question use annexes 033-9707A, 033-9707B or Route Manual chart E(HI)4 CAA-Edition, Instrument approach chart ILS DME Rwy 27R) Planning an IFR-flight from Paris to London (Heathrow) via initial approach fix (IAF) Biggin VOR . Given: distance from top of descent (TOD) to Rwy 27R is 76 NM Determine the distance from ABB 116.6 to TOD.

(For this question use annex 033-9703A or Route Manual SID chart 20-3 for PARIS Charles-de-Gaulle) Planning an IFR-flight from Paris (Charles de Gaulle) RWY 27 to London. Given: Distance from PARIS Charles-de- Gaulle to top of climb 50 NM Determine the distance from the top of climb (TOC) to ABB 116.6.

(For this question use annex 033- 11041A or Route Manual SID chart for MUNICH(10- 3C,10-3D)) Which is the correct departure via KEMPTEN from runway 26L ?

In a flight plan when the destination aerodrome is A and the alternate aerodrome is B, the final reserve fuel for a turbojet engine aeroplane corresponds to:

The Trip Fuel for a jet aeroplane to fly from the departure aerodrome to the destination aerodrome is 5 350 kg. Fuel consumption in holding mode is 6 000 kg/h. The quantity of fuel which is needed to carry out one go-around and land on the alternate airfield is 4 380 kg. The destination aerodrome has a single runway. What is the minimum quantity of fuel which should be on board at take-off?

For turbojet engine driven aeroplane, given: Taxi fuel 600 kg Fuel flow for cruise 10 000 kg/h Fuel flow for holding 8 000 kg/h Alternate fuel 10 200 kg Planned flight time to destination 6 h Forecast visibility at destination 2000 m The minimum ramp fuel required is:

An aeroplane is flying from an airport to another. In cruise, the calibrated airspeed is I50 kt, true airspeed 180 kt, average groundspeed 210 kt, the speed box on the filed flight plan shall be filled as follows:

(For this question use annex 033-12352A Flight Planning Manual MRJT 1 Figure 4.3.1C) For a flight of 2400 ground nautical miles the following apply : Tail wind component 25 kt Temperature ISA -10° C Cruise altitude 31000ft Landing mass 52000kg The (a) trip fuel and (b) trip time respectively are :

(For this question use annex 033-12351A Flight Planning Manual MRJT 1 Figure 4.3.5) For a flight of 2400 ground nautical miles the following apply : Tail wind 25kt Temperature ISA - 10° C Brake release mass 66000kg The (a) trip fuel and (b) trip time respectively are :

(For this question use annex 033-12350A or Flight Planning Manual MRJT 1 Figure 4.3.5) The following apply : Tail wind component 10kt Temperature ISA +10° C Brake release 63000kg Trip fuel available 20000kg What is the maximum possible trip distance ?

(For this question use annex 033- 11011A or Route Manual chart E(HI)4 CAA-Edition) The radio navigation aid on airway UG4 at LUXEUIL (47° 41"N 006° 18"E) is a:

(For this question use annex 033- 11010A or Route Manual chart E(HI)4 CAA-Edition) The radio navigation aid at CHIOGGIA (45° 04"N 012° 17"E) is a:

(For this question use annex 033-12348A or Flight Planning Manual MRJT 1 Figure 4.3.5) The following apply: Temperature ISA +15° C Brake release mass 62000kg Trip time 5hr 20 min What is the trip fuel ?

(For this question use annex 033-12347A Flight Planning Manual MRJT 1 Figure 4.3.5) For a flight of 3500 ground nautical miles, the following apply : Tail wind component 50 kt Temperature ISA +10° C Brake release mass The (a) trip fuel and (b) trip time respectively are :

(For the question use annex 033-12346A Flight Planning Manual MRJT 1 Figure 4.3.1C) For a flight of 2800 ground nautical miles the following apply : Tail wind component 45kt Temperature ISA - 10° C Cruise altitude 29000ft Landing mass 55000kg The (a) trip fuel (b) trip time respectively are :

(For this question use annex 033-12345A or Flight Planning Manual MRJT 1 Figure 4.3.5) Given a trip time of about 9 hours, within the limits of the data given, a temperature decrease of 30° C will affect the trip time by approximately :

(For this question use annex 033-12344A or Flight Planning Manual MRJT 1 Figure 4.3.1C) For a flight of 2000 ground nautical miles, cruising at 30000 ft, within the limits of the data given, a headwind component of 25 kt will affect the trip time by approximately :

(For this question use annex.033-12342A or Flight Planning Manual MRJT 1 Figure 4.3.5) Given the following : Head wind component 50 kt Temperature ISA + 10° C Brake release mass 65000kg Trip fuel available 18000kg What is the maximum possible trip distance ?

Given: Dry operating mass (DOM)= 33510 kg Load= 7600 kg Trip fuel (TF)= 2040 kg Final reserve fuel= 983 kg Alternate fuel= 1100 kg Contingency fuel= 5% of trip fuel Which of the listed estimated masses is correct?

Given: Dry operating mass (DOM)= 33000 kg Load= 8110 kg Final reserve fuel= 983 kg Alternate fuel= 1100 kg Contingency fuel 102 kg The estimated landing mass at alternate should be :

Given: Dry operating mass (DOM)= 33510 kg Load= 7600 kg Final reserve fuel= 983 kg Alternate fuel= 1100 kg Contingency fuel 102 kg The estimated landing mass at alternate should be :

(For this question use annex 033- 11012A or Route Manual chart E(LO)1) The radio navigation aid at BELFAST CITY (54° 37"N 005° 53"W) is :

(For this question use annex 033-12341A or Flight Planning Manual MRJT 1 Figure 4.3.1C) For a flight of 1900 ground nautical miles the following apply : Head wind component 10 kt Temperature ISA -5° C Trip fuel available 15000 kg Landing mass 50000kg What is the minimum cruise level (pressure altitude) which may be planned ?

(For this question use annex 033- 11005A or Route Manual chart E(LO)1 ) The radio navigation aid at TOPCLIFFE (54° 12"N 001° 22"W) is a:

A public transport aeroplane with reciprocating engines,is flying from PARlS to LYON. The final reserve corresponds to:

(For this question use annex 033- 11007A or Route Manual chart E(HI)4 CAA-Edition) The radio navigation aid at ST DIZIER (48° 38N 004° 53"E) is a:

(For this question use annex 033- 11008A or Route Manual chart E(HI)4 CAA-Edition) The radio navigation aid at ZURICH (47° 36"N 008° 49"E) is :

(For this question use annex 033- 11009A or Route Manual chart E(HI)4 CAA-Edition) The radio navigation aid STAD (51° 45"N 004° 15"E) is:

(For this question use annexes 033-12306A and 033-12306B or Flight Planning Manual MRJT 1 Figure 4.5.2 and 4.5.3.3) Given : Distance B - C : Cruise Mach 0.78 at FL300 Temperature - 52° C Headwind component : 50 kt Gross mass at 64 500 kg The fuel required from B - C is :

(For this question use annex 033-12313A or Flight Planning Manual MRJT 1 Figure 4.3.6) Given : Distance to Alternate : 400 NM Landing mass at Alternate : 50 000kg Headwind component : 25 kt The alternate fuel required is :

(For this question use annex 033-12340A or Flight Planning Manual MRJT 1 Figure 4.3.5) For a flight of 2800 ground nautical miles the following apply : Head wind component 20 kt Temperature ISA + 15° C Brake release 64700 kg The (a) trip fuel, and (b) trip time respectively are :

(For this question use annex 033-12311A or Flight Planning Manual MRJT 1 Figure 4.4) - HOLDING PLANNING) The fuel required for 45 minutes holding, in a racetrack pattern, at PA 5000 ft, mean gross mass 47 000 kg, is :

(For this question use annex 033-12343A or Flight Planning Manual MRJT 1 Figure 4.3.1C) Within the limits of the data given, a mean temperature increase of 30° C will affect the trip time by approximately :

(For this question use annexes 033-12309A and 033-12309B or Flight Planning Manual MRJT 1 Figure 4.5.2 and 4.5.3.4) Given : Distance B - C 350 NM Cruise 300 KIAS at FL 210 Temperature - 40° C Tailwind component : 70 kt Gross mass at 53 200 kg The fuel required from B - C is :

(For this question use annexes 033-12307A and 033-12307B or Flight Planning Manual MRJT 1 Figure 4.5.2 and 4.5.3.3) Given : Distance B - C 1200 NM Cruise Mach 0.78 at FL300 Temperature Deviation from ISA : - 14° C Tailwind component 40 kt Gross mass at B : 50 200 kg The fuel required from B - C is :

(For this question use annex 033-12312A or Flight Planning Manual MRJT 1 Figure 4.3.6) Given: Distance to Alternate 450 NM Landing mass at Alternate : 45 000 kg Tailwind component : 50 kt The Alternate fuel required is :

(For this question use annex 033-12305A or Flight Planning Manual MRJT 1 Figure 4.5.1) Given : Brake release mass : 62 000 kg Temperature ISA + 15° C The fuel required for a climb from Sea Level to FL330 is :

(For this question use annex 033- 11042A or Route Manual STAR chart for LONDON HEATHROW (10-2D)) The minimum holding altitude (MHA) and maximum holding speed (IAS) at MHA at OCKHAM OCK 115.3 are:

(For this question use annexes 033-12308A and 033-12308B or Flight Planning Manual MRJT 1 Figure 4.5.2 and 4.5.3.4) Given : Distance C - D 540 NM Cruise 300 KIAS at FL 210 Temperature Deviation from ISA : +20° C Headwind component 50 kt Gross mass at 60 000 kg The fuel required from C to D is :

(For this question use annex 033-12339A Flight Planning Manual MRJT 1 Figure 4.3.1C) For a flight of 2800 ground nautical miles the following apply : Head wind component 15 kt Temperature ISA + 15° C Cruise altitude 35000 ft Landing mass 50000 kg The (a) trip fuel and (b) trip time respectively are :

(For this question use annex 033-12310A or Flight Planning Manual MRJT 1 Figure 4.4) - HOLDING PLANNING The fuel required for 30 minutes holding, in a racetrack pattern, at PA 1500 ft, mean gross mass 45 000 kg, is :