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Question 116-1 : 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.. err a 033 559 ? [ Training professional ]

Fl250.

. /com en/com033 559.jpg..the minimum enroute altitude from nice to bastia is fl250. exemple 216 Fl250.

Question 116-2 : Route manual chart paris charles de gaulle ils rwy 27 21 2.the crossing altitude and descent instruction for a propeller aircraft at coulommiers clm are .. err a 033 566 ?

Cross at fl60 descend to 4000 ft.

. /com en/com033 566.jpg.. exemple 220 Cross at fl60 descend to 4000 ft.

Question 116-3 : Route manual chart munich ndb dme rwy 26l approach 16 3..the frequency and identifier of the ndb for the published approachs are.. err a 033 568 ?

400 msw

.key informations are displayed in big, bold text.. 400 msw is the main beacon to be use on the munich ndb dme rwy 26l approach procedure. exemple 224 400 msw

Question 116-4 : Route manual chart e hi 4 caa edition. the radio navigation aid serving strasbourg 48°30'n 007°34'e is a.. err a 033 571 ?

Vor/tacan, frequency 115.6 mhz

.the distance measurement component of tacan operates with the same specifications as civil dmes..therefore to reduce the number of required stations, tacan stations are frequently co located with vor facilities. these co located stations are known as vortacs. this is a station composed of a vor for civil bearing information and a tacan for military bearing information and military/civil distance measuring information...the ' d ' indicates a distance measuring equipment dme , since we do not have the answer 'vor/ dme , frequency 115.6 mhz', we can only choose 'vor/ tacan , frequency 115.6 mhz'. exemple 228 Vor/tacan, frequency 115.6 mhz

Question 116-5 : Use route manual chart e lo 1.what are the applicable grid moras for a flight from dean cross 115.2 dcs 54°43'n 003°20'w to talla 113.8 tla 55°30'n 003°21'w on airway a2.. err a 033 574 ?

45 and 40.

. /com en/com033 574.jpg.. exemple 232 45 and 40.

Question 116-6 : Use route manual chart e lo 1..what are the magnetic curse and distance when flying on airway b4 from the reporting point shapp n54°30' w002°38' to the reporting point eskdo n55°18' w003°12' .. err a 033 584 ?

343°/52 nm.

. /com en/com033 584.jpg.the question asks for the magnetic course from shapp to eskdo, so 163°+180° = 343°. exemple 236 343°/52 nm.

Question 116-7 : Use route manual chart e hi 2..an aircraft has to fly from alma n55°25' e013°34' to peter n56°50' e013°35'. excluding rvsm, the lowest flight level above fl400 that can be flown on an ifr flight plan, is.. err a 033 585 ?

Fl 430

.on the airway ug55 from point alma to point peter, you have a e> indicates that an even flight level must be used..excluding rvsm, the lowest flight level above fl400 that can be flown, won't be fl420, but fl... 430 it's crazy isn't it.you have to refer to icao semicircular cruising level diagram.. 710..at or above fl290, only odd levels are used in order to allow a minimum separation of 2000 ft between aircrafts. exemple 240 Fl 430

Question 116-8 : Use route manual chart e hi 4 caa edition..an aircraft 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 you can read on the chart d 113.8 sbg. it means.. err a 033 586 ?

Vor/dme, ident sbg, frequency 113.8 mhz, can be used.

exemple 244 Vor/dme, ident sbg, frequency 113.8 mhz, can be used.

Question 116-9 : Use route manual chart e lo 1...the radio navigation aid at st. abbs 55°55'n 002°12'w is.. err a 033 594 ?

A vordme, frequency 112.5 mhz.

exemple 248 A vordme, frequency 112.5 mhz.

Question 116-10 : For this question use route manual chart e hi 2..the radio navigation aid s at 56°17'n 010°47'e is/are.. err a 033 597 ?

Ndb, frequency 374 khz.

9996angel.como he de saber si es de uso temporal o no...an asterisk indicates navaid operation or service not continuous..example. /com en/com033 597.jpg..here, 'tu' means 'tango uniform', this is the navaid name. exemple 252 Ndb, frequency 374 khz.

Question 116-11 : Use route manual chart e hi 1..an aircraft is flying towards gow 55°52'n 004°27w on airway un615 prior to an arrival in the london fir..according to the information on the chart, what is the most relevant frequency to receive the broadcast weather for london fir north .. err a 033 598 ?

126.60 mhz.

.133.67 mhz and 133.67 mh are the frequencies for scottish control..115.4 mhz is the frequency of gow vor..126.60 mhz is the london north weather wx frequency. exemple 256 126.60 mhz.

Question 116-12 : For this question use route manual chart e hi 2..the radio navigation aid s at 55°26' n011°38'e is/are.. err a 033 599 ?

Vordme, frequency 112.8 mhz.

exemple 260 Vordme, frequency 112.8 mhz.

Question 116-13 : Route manual chart e hi 4 caa edition...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 wednesday is .. err a 033 601 ?

Ur10 ntm ub6 bub ats

. /com en/com033 601.jpg.ub69 is not available on wednesday you can read in blue 'available only friday 1800 to monday 0800 lt'. exemple 264 Ur10 ntm ub6 bub ats

Question 116-14 : Use route manual chart e hi 1..what navigation aid s is/are available to civil aircraft at the military airfield of kinloss 57°40'n 003°32'w .. err a 033 602 ?

The range element only of tacan on dme frequency 109.8 mhz.

. /com en/com061 453.jpg.for civil aircrafts, only the range element of a tacan is available. exemple 268 The range element only of tacan on dme frequency 109.8 mhz.

Question 116-15 : On ur14 airway, an aircraft overflying gibso must be at or above. 1496 ?

Fl 250

exemple 272 Fl 250

Question 116-16 : The correct track and corresponding iaf for a western arrival via ridar, for runway 08l/r, is. 1497 ?

Ridar 2m, iaf miq

exemple 276 Ridar 2m, iaf miq

Question 116-17 : Refer to jeppesen manual chart e hi 4 or figure hi 08..the magnetic course and distance from st prex spr 113.9 n4628 e00627 to fribourg fri 115.1 n4647 e00714 on airway ug60, are. 1498 ?

061° / 37 nm

exemple 280 061° / 37 nm

Question 116-18 : Refer to jeppesen student manual london area chart..you are required to hold at bovingdon 51°43,6 n000°33,0 w however, the vor is unserviceable. what procedure.should now follow. 1499 ?

Enter the bovva alternate hold which starts at 32 dme biggin on 141° qdm.

exemple 284 Enter the bovva alternate hold which starts at 32 dme biggin on 141° qdm.

Question 116-19 : Refer to jeppesen manual chart e hi 4...your aircraft registered in the uk is outbound from london towards new york via ug1 and shanwick cta/fir, prior to.crossing w002 what should you have obtained. 1500 ?

Oceanic entry clearance on 127,65 mhz.

exemple 288 Oceanic entry clearance on 127,65 mhz.

Question 116-20 : Refer to jeppesen manual chart e hi 5...flying eastbound between bologna 44°32,2 n 011°17,5 e and ancona 43°35,2 n 013°28,3 e what is the minimum icao ifr cruising level. 1501 ?

Fl 310

exemple 292 Fl 310

Question 116-21 : Refer to jeppesen student manual trm, sabadell area chart 19 1 or figure vfr 12...what is the published frequency for barcelona atis. 1502 ?

118.65 mhz.

exemple 296 118.65 mhz.

Question 116-22 : Planning an ifr flight from paris charles de gaulle to london..sid is abb 8a. assume.variation 3° w.tas 430 kts.w/v 280/40.distance to top of climb 50 nm..determine the magnetic course, ground speed and wind correction angle from top of climb to abb 116.6.. 1503 ?

Mc 349°, gs 414 kts, wca 5°.

exemple 300 Mc 349°, gs 414 kts, wca -5°.

Question 116-23 : Refer to jeppesen student route manual chart e lo 1..the minimum en route altitude mea that can be maintained continuously on airway l602 from talla 113.8 tla 55°30 n 003°21 w to newcastle 114.25 new 55°02 n 001°24w is. 1504 ?

Fl200.

Img1505 exemple 304 Fl200.

Question 116-24 : 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/h. alternate fuel is 4380 kg..contingency should be 5% of trip fuel..what is the minimum required ?

13000 kg.

.warning this question indicates contingency should be 5% of trip fuel...normal rules for contingency the greater of 5% of trip or 5 min holding at 1500 ft..we must assume the operator has an exemption.....minimum quantity of fuel at take off = trip fuel + alternate + contingency 5% of trip fuel + 30 min final reserve jet aircraft...trip fuel = 5350 kg...alternate = 4380 kg...contingency = 5% of trip fuel.5% x 5350 = 267 kg..30 min final reserve = 6000 /2 = 3000 kg...minimum quantity of fuel at take off = 5350 + 4380 + 267 + 3000 = 12997 kg. exemple 308 13000 kg.

Question 116-25 : Using the power setting table, for the single engine aeroplane, determine the manifold pressure and fuel flow lbs/hr with full throttle and cruise lean mixture in the following conditions.oat +13°c.pressure altitude 8000 ft.rpm 2300. 2161 ?

22.4 in.hg and 69.3 lbs/hr.

.first search isa temperature.at 8000 ft oat is +13°c..in standard atmosphere, temperature at 8000 ft is 15°c 2°c x 8 = 1°c..we are in isa +14°c..we need now to interpolate between isa and isa +20°c on the table. 1139.isa fuel flow 71.1 pph and man press 22.4.isa +20°c fuel flow 68.5 pph and man press 22.4.. 71.1 68.5 x 14 / 20 = 1.82. fuel flow = 71.1 1.82 = 69.3 lbs/hr. exemple 312 22.4 in.hg and 69.3 lbs/hr.

Question 116-26 : Given the following.head wind component 50 kt.temperature isa +10°c.brake release mass 65000 kg.trip fuel available 18000 kg.what is the maximum possible trip distance. 2363 ?

2740 nm.

. 1156 exemple 316 2740 nm.

Question 116-27 : The fuel burn off is 200 kg/h with a relative fuel density of 0,8..if the relative density is 0,75, the fuel burn will be ?

200 kg/h.

.volume changes, mass consumption will not change...if they ask for litre/hour instead of kg/h , then fuel burn will be 235 l/h. exemple 320 200 kg/h.

Question 116-28 : 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 ?

13 230 kg.

.minimum quantity of fuel at take off = trip fuel + alternate + contingency + 30 min final reserve jet aircraft...trip fuel = 5350 kg...alternate = 4380 kg...contingency = the greater of 5% of trip or 5 min holding at 1500 ft.5% of trip = 5% x 5350 = 267 kg.5 min holding at 1500 ft = 6000 x 5/60 = 500 kg...30 min final reserve = 6000 /2 = 3000 kg...minimum quantity of fuel at take off = 5350 + 4380 + 500 + 3000 = 13230 kg. exemple 324 13 230 kg.

Question 116-29 : Given.fl 75, oat +10°c, lean mixture, 2300 rpm..find.fuel flow in gallons per hour gph and tas. 2461 ?

11.6 gph, tas 160 kt.

.at fl75, in standard atmosphere, isa is 15°c 2°c x 7.5 = 0°c..oat is +10°c, thus we are at isa +10°c...no need for long interpolations, fuel flow is around 11.4 to 12 gph, and tas between 158 to 160 kt. 1162 exemple 328 11.6 gph, tas: 160 kt.

Question 116-30 : A public transport aeroplane with reciprocating engines, the final reserve should be ?

Fuel to fly for 45 minutes.

Eu ops 1.255 fuel policy..... c an operator shall ensure that the pre flight calculation of usable fuel required for a flight includes..1. taxi fuel and.2. trip fuel and.3. reserve fuel consisting of.. i contingency fuel see eu ops 1.192 and.. ii alternate fuel, if a destination alternate aerodrome is required. this does not preclude selection of the departure aerodrome as the destination alternate aerodrome and.. iii final reserve fuel see appendix 1 to ops 1.255 below and.. iv additional fuel, if required by the type of operation e.g. etops and..4. extra fuel if required by the commander...appendix 1 to eu ops 1.255...... final reserve fuel, which shall be.. a for aeroplanes with reciprocating engines, fuel to fly for 45 minutes or.. b for aeroplanes with turbine engines, fuel to fly for 30 minutes at holding speed at 1 500 ft 450 m above aerodrome elevation in standard conditions, calculated with the estimated mass on arrival at the destination alternate aerodrome or the destination aerodrome, when no destination alternate aerodrome is required. exemple 332 Fuel to fly for 45 minutes.

Question 116-31 : Assuming the following data.ground distance to be covered 1 500 nm.cruise flight level fl 310.cruising speed mach 0.82 true airspeed 470 kt.head wind component 40 kt.planned destination landing mass 140 000 kg.temperature isa +15°c.cg 37%.total anti ice on, pack flow hi..fuel consumption for such a ?

23 500 kg.

.proceed like this.1500 nm / 470kt 40kt = 3.49 h..3.49 x 470 = 1640 nam..on the table, to find the corresponding value for 1640 nam, you have to interpolate between line 1600 and 1700 nam.. 22221 20955 /10 x4 = 506 kg..20955 + 506 = 21461 kg..you must add +1% for pack flow high.and.you have to add +7% for total anti ice on..it means 8% of 21461 = 1717 kg..21461 + 1717 = 23178 kg..we are on isa+15 condition, for each degree above isa temperature apply fuel correction 0.010 x 15 x 1640 = 246 kg..23178 + 246 = 23424 kg. exemple 336 23 500 kg.

Question 116-32 : For a flight of 2400 ground nautical miles the following apply.tail wind 25 kt.temperature isa 10°c.brake release mass 66000 kg.the a trip fuel and b trip time respectively are. 2463 ?

A 14000 kg b 5h 35 min.

. 1169 exemple 340 (a) 14000 kg (b) 5h 35 min.

Question 116-33 : Given.brake release mass 58 000 kg.temperature isa +15.the fuel required to climb from an aerodrome at elevation 4000 ft to fl300 is. 1515 ?

1250 kg.

. 1173.you have to decrease the fuel by 100 kg as prescribe in the fuel adjustment table. exemple 344 1250 kg.

Question 116-34 : The flight crew of a turbojet aeroplane prepares a flight using the following data. flight level fl 370 at 'long range' lr cruise regime. mass at brake release 212 800 kg. flight leg ground distance 2 500 nm. temperatures isa. cg 37%. headwind component 30 kt. 'total anti ice' set on 'on' for the ?

34 430 kg.

.nam = ngm x tas/gs.nam = 2500 x 470/440.nam = 2670 nam....212 800 kg is corresponding to 8083 nam in the table. /com en/com033 99.jpg....8083 2670 = 5413 nam....5413 nam is corresponding to 180 329 kg in the table...fuel = 212 800 180 329 = 32 471 kg....fuel consumption with total anti ice 0n = 32 471 x 1.06 = 34 419 kg... renfernandes i still did not understand what do de values on top of the columns 0.2 .4 in this case.8 mean... i couldn't choose a column unless i knew what they mean....thanks...mass at brake release is 212 800 kg ==> 212 ton + 0.8 ton...if mass at brake release was 213 600 kg ==> 212 ton + 1.6 ton... miguel.would you be so kind to explain why 5413 are exactly 180 329 kg because i'm trying to calculate it via interpolation but i cannot find a successful result. thank you....180400 180200 = 200 kg.5419 5402 = 17 nam..17 nam for 200 kg.1 nam = 11.8 kg..5419 5413 = 6 nam.6 x 11.8 kg = 71 kg..180400 71 = 180329 kg. exemple 348 34 430 kg.

Question 116-35 : The purpose of the decision point procedure is ?

To reduce the minimum required fuel and therefore be able to increase the traffic load.

.reduced contingency fuel rcf procedure decision point procedure.this is a technique for increasing the traffic load by reducing the minimum fuel required. you reduce the contingency figures by using it only from the decision point to the destination...if an operator's fuel policy includes pre flight planning to a destination 1 aerodrome commercial destination with a reduced contingency fuel procedure using a decision point along the route and a destination 2 aerodrome optional refuel destination , the amount of usable fuel, on board for departure, shall be the greater of 2.1. or 2.2. below..2.1. the sum of. a taxi fuel and. b trip fuel to the destination 1 aerodrome, via the decision point and. c contingency fuel equal to not less than 5% of the estimated fuel consumption from the decision point to the destination 1 aerodrome and. d alternate fuel or no alternate fuel if the decision point is at less than six hours from the destination 1 aerodrome are fulfilled and. e final reserve fuel and.. f additional fuel and. g extra fuel if required by the commander...2.2. the sum of.. a taxi fuel and. b trip fuel to the destination 2 aerodrome, via the decision point and.. c contingency fuel from departure aerodrome to the destination 2 aerodrome and. d alternate fuel, if a destination 2 alternate aerodrome is required and. e final reserve fuel and.. f additional fuel and. g extra fuel if required by the commander. exemple 352 To reduce the minimum required fuel and therefore be able to increase the traffic load.

Question 116-36 : At reference or see flight planning manual mrjt 1 figure 4.7.2.for the purpose of planning an extended range flight it is required that with a start of diversion mass of 55000kg a diversion of 600 nautical miles should be achieved in 90 minutes..using the above table, the only listed cruise ?

M/kias.74/330

. /com en/com033 120.jpg.. exemple 356 M/kias .74/330

Question 116-37 : Using the power setting table, for the single engine aeroplane, determine the cruise tas and fuel flow lbs/h with full throttle and cruise lean mixture in the following conditions. oat 3°c. pressure altitude 6000 ft. power 21 in/hg / 2100 rpm.. 2155 ?

134 kt and 55.7 lbs/h.

.first step, search for isa temperature.oat is +3°c, isa at 6000 ft = 15°c 2 x 6 = +3°c.we are in standard condition isa...for standard day isa , ktas is the same 134 kt...step two, search for fuel flow.for standard condition isa , fuel flow is 55.7 pph pound per hour or lbs/h. exemple 360 134 kt and 55.7 lbs/h.

Question 116-38 : 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 ?

77 800 kg.

.fuel flow for cruise 6h x 10000 kg = 60000 kg..contingency fuel 5% x 60000 = 3000 kg..taxi fuel 600 kg..alternate fuel 10200 kg..30 minutes fuel for holding at 8000kg/h = 4000 kg..total = 60000 + 3000 + 600 + 10200 + 4000..total = 77800 kg. exemple 364 77 800 kg.

Question 116-39 : The following apply.temperature isa +15°c.brake release mass 62000 kg.trip time 5h 20 min..what is the trip fuel . 2180 ?

13500 kg.

. 1194.enter the graph at 5.33 5h40. exemple 368 13500 kg.

Question 116-40 : At reference or see 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 .. err a 033 146 ?

A 17600 kg b 6 hr 50 min.

.first, set the red lines on the graph.. /com en/com033 146.jpg..reach the ref lines first, and after join the red lines..above landing mass on the right part of the graph , you have to use the dashed line it is for high pressure alitude flights. exemple 372 (a) 17600 kg (b) 6 hr 50 min.


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