Un compte Premium offert sur le site FCL.055 ! Rendez-vous sur www.fcl055-exam.fr puis créez un compte avec le même email que celui...   [Lire la suite]


Question 216-1 : North atlantic high level airspace nat hla .a check on the operation of the selcal equipment during a transatlantic flight using the ots organised track system must be done ? [ Preparation civilian ]

At or prior entering the oceanic airspace

exemple 316 At or prior entering the oceanic airspace.

Question 216-2 : North atlantic high level airspace nat hla .if a flight is planned to operate along the whole length of one of the organised tracks in the mnps airspace the intended organised track should be defined in items of the flight plan by ?

The abbreviation 'nat' followed by the code letter assigned to the track

exemple 320 The abbreviation 'nat' followed by the code letter assigned to the track.

Question 216-3 : North atlantic high level airspace nat hla .in the event of a contingency which required an en route diversion to an alternate aerodrome across the direction of the prevailing 'nat' traffic flow and if prior atc clearance cannot be obtained an aircraft able to maintain its assigned flight level ?

If above fl410 climb or descend 1000 ft while turning towards the alternate aerodrome

Mnpsa manual .12 3 special procedures.12 3 1 the general concept of these oceanic in flight contingency procedures is whenever operationally feasible to offset from the assigned route by 15 nm and climb or descend to a level which differs from those normally used by 500 ft if below fl410 or by 1000 ft if above fl410 exemple 324 If above fl410, climb or descend 1000 ft, while turning towards the alternate aerodrome.

Question 216-4 : Extended range operations with two engined aeroplanes etops .an aircraft leaves point p 60°n 030°w on a true heading equal to 090° while the gyro compass which is assumed to be operating perfecly and without an ho y rate corrector unit indicates 000° the aircraft arrives at point q 62°n 010°w ?

328°

We need to calculate transport precession and earth rate astronomic precession ..earth rate astronomic precession .15 x sin 61 x 1 5 = 20.15 sin lat x flight time = 20°..transport precession .degrees of longitude travelled x sin lat.20 x sin 61 = 17°..we start on a true heading of 090° and a gyro heading of 000° we arrives on a true heading of 095° and a gyro heading which gyro compass is assumed to be operating perfectly a gyro heading of 005° .005° 37° = 328° exemple 328 328°.

Question 216-5 : Extended range operations with two engined aeroplanes etops .you plan to fly from point a 60°n 010°e to point b 60°n 020°e . the north of the directional gyro with no rate correction device is aligned with the true north of point a .the constant gyro heading to be followed when starting from ?

076°

First earth rate astronomic precession .15 x sin lm x flight time lm mean latitude .15 x sin60 x 1 5 = 20°.second transport precession .g xsin lm g the longitude difference .10 x sin 60 = 8°.total error 28° minus because in northern hemisphere astronomic precession and transport precession are negative .we start with a 090° gyro heading we will arrive at b with a 062° gyro heading the constant gyro heading the average heading to be followed is equal to 090+062 /2 = 076° exemple 332 076°.

Question 216-6 : Extended range operations with two engined aeroplanes etops .the chart type is polar stereographic with the grid parallel to the zero meridian and grid north in the direction of the north geographic pole the gyro is not fitted with a rate correction device . the gyro magnetic compass of an aircraft ?

32 5°

We do not need to correct mechanical precession .we do not need to correct apparent wander we stay at the stand .the only error calculation we need is earth rate ..earth rate error = 15 x sin lm x time.earth rate error = 15 x 0 87 x 2 5 = 32 5°..in northern hemisphere earth rate is 'minus' so it's 32 5° exemple 336 -32.5°.

Question 216-7 : Extended range operations with two engined aeroplanes etops .the pilot uses a south polar stereographic chart with grid parallel with the zero meridian and grid north in the direction of geographic north along this meridian . the aircraft position is 80°s 130°e its true route is 110° the grid ?

240°

Img /com en/com070 24 jpg.grid track = true track + convergency.grid track = 110° + 130° = 240° exemple 340 240°.

Question 216-8 : Extended range operations with two engined aeroplanes etops .the mnps airspace extends from ?

27° north to 90° north

Mnpsa manual chaper 16 .16 1 general..16 1 1 the north atlantic region is essentially divided into two distinct areas for flight operation i e mnps airspace and non mnps airspace operations within mnps airspace require the user to adhere to very specific operating protocols the vertical dimension of mnps airspace is between fl285 and fl420 i e in terms of normally used cruising levels from fl290 to fl410 inclusive ..16 1 2 the lateral dimensions include the following areas .a those portions of the new york oceanic north of 27°n but excluding the area west of 60°w and south of 38°30'n .b and all of the reykjavik shanwick gander and santa maria oceanic control areas ctas . /com fr/com070 21 jpg..please download the guidance concerning air navigation in and above the north atlantic mnps airspace edition 2010 .pdf675 exemple 344 27° north to 90° north.

Question 216-9 : Extended range operations with two engined aeroplanes etops .the mnps airspace extends vertically between flight levels ?

285 and 420

Mnpsa manual chaper 16 .16 1 general..16 1 1 the north atlantic region is essentially divided into two distinct areas for flight operation i e mnps airspace and non mnps airspace operations within mnps airspace require the user to adhere to very specific operating protocols the vertical dimension of mnps airspace is between fl285 and fl420 i e in terms of normally used cruising levels from fl290 to fl410 inclusive ..16 1 2 the lateral dimensions include the following areas .a those portions of the new york oceanic north of 27°n but excluding the area west of 60°w and south of 38°30'n .b and all of the reykjavik shanwick gander and santa maria oceanic control areas ctas . /com fr/com070 21 jpg..please download the guidance concerning air navigation in and above the north atlantic mnps airspace edition 2010 .pdf675 exemple 348 285 and 420.

Question 216-10 : When refuelling is being performed while passengers are boarding or disembarking the aircraft one of the requirements is ?

The ground area beneath the exits intended for emergency evacuation and slide deployment areas must be kept clear

exemple 352 The ground area beneath the exits intended for emergency evacuation and slide deployment areas must be kept clear.

Question 216-11 : The regulatory green navigation light is located on the starboard side with a coverage angle of ?

110°

Admin . 1463 exemple 356 110°.

Question 216-12 : North atlantic high level airspace nat hla .the validity period of a night time organised track system in mnps minimum navigation performance specification airspace is normally at 30°w between ?

01h00 utc to 08h00 utc

Jorgepardo .in nordian's book this question shoud be different because they say that the night time is between 1 30 and 8 00 utc..please download the guidance concerning air navigation in and above the north atlantic mnps airspace edition 2010 .pdf675.chapter 2 .2 1 1 as a result of passenger demand time zone differences and airport noise restrictions much of the north atlantic nat air traffic contributes to two major alternating flows a westbound flow departing europe in the morning and an eastbound flow departing north america in the evening the effect of these flows is to concentrate most of the traffic unidirectionally with peak westbound traffic crossing the 30w longitude between 1130 utc and 1900 utc and peak eastbound traffic crossing the 30w longitude between 0100 utc and 0800 utc . . page 11 .the hours of validity of the two organised track systems ots are normally as follows .day time ots 1130 utc to 1900 utc at 30°w .night time ots 0100 utc to 0800 utc at 30°w exemple 360 01h00 utc to 08h00 utc

Question 216-13 : North atlantic high level airspace nat hla .the validity period of a day time organised track system in mnps minimum navigation performance specification airspace is normally at 30°w between ?

11h30 utc to 19h00 utc

Please download the guidance concerning air navigation in and above the north atlantic mnps airspace edition 2010 .pdf675.chapter 2 .2 1 1 as a result of passenger demand time zone differences and airport noise restrictions much of the north atlantic nat air traffic contributes to two major alternating flows a westbound flow departing europe in the morning and an eastbound flow departing north america in the evening the effect of these flows is to concentrate most of the traffic unidirectionally with peak westbound traffic crossing the 30w longitude between 1130 utc and 1900 utc and peak eastbound traffic crossing the 30w longitude between 0100 utc and 0800 utc . . page 11 .the hours of validity of the two organised track systems ots are normally as follows .day time ots 1130 utc to 1900 utc at 30°w .night time ots 0100 utc to 0800 utc at 30°w exemple 364 11h30 utc to 19h00 utc.

Question 216-14 : North atlantic high level airspace nat hla .during a flight to europe planned in mnps minimum navigation performance specification airspace you expect to cross the 30°w meridian at 00h30 utc .you will then normally be ?

Out of the validity period of organised flight track system

Please download the guidance concerning air navigation in and above the north atlantic mnps airspace edition 2010 .pdf675.chapter 2 .2 1 1 as a result of passenger demand time zone differences and airport noise restrictions much of the north atlantic nat air traffic contributes to two major alternating flows a westbound flow departing europe in the morning and an eastbound flow departing north america in the evening the effect of these flows is to concentrate most of the traffic unidirectionally with peak westbound traffic crossing the 30w longitude between 1130 utc and 1900 utc and peak eastbound traffic crossing the 30w longitude between 0100 utc and 0800 utc . . page 11 .the hours of validity of the two organised track systems ots are normally as follows .day time ots 1130 utc to 1900 utc at 30°w .night time ots 0100 utc to 0800 utc at 30°w exemple 368 Out of the validity period of organised flight track system.

Question 216-15 : North atlantic high level airspace nat hla .the minimum navigation equipment required for an aircraft flying without restriction in mnps airspace can be at the very least ?

Two inertial navigation systems

Mnpsa manual .chapter 10 procedures in the event of navigation system degradation or failure.10 1 2 for unrestricted operation in mnps airspace an approved aircraft must be equipped with a minimum of two fully serviceable lrnss exemple 372 Two inertial navigation systems.

Question 216-16 : North atlantic high level airspace nat hla .the minimum longitudinal separation of two aircraft flying in mnps airspace at the same flight level on the same track and with the same mach number is ?

10 minutes

Longitudinal separations between subsequent aircraft following the same track in trail and between aircraft on intersecting tracks in the nat mnps airspace are assessed in terms of differences in atas/etas at common waypoints the longitudinal separation minima currently used in the nat mnps airspace are thus expressed in clock minutes .doc 7030 nat regional supplementary procedures.6 2 2 1 minimum longitudinal separation between turbo jet aircraft shall be .a 15 minutes or.b 10 minutes provided the mach number technique is applied whether in level climbing or descending flight and the aircraft concerned have reported over a common point to follow continuously diverging tracks until some other form of separation is provided and .1 at least 10 minutes longitudinal separation exists at the point where the tracks diverge and.2 at least 5 minutes longitudinal separation exists where lateral separation is achieved and.3 lateral separation will be achieved at or before the next significant point normally ten degrees of longitude along track s or if not within 90 minutes of the time the second aircraft passes the common point or within 1 112 km 600 nm of the common point whichever is estimated to occur first .6 2 2 2 minimum longitudinal separation between non turbo jet aircraft shall be .a 30 minutes and.b 20 minutes in the west atlantic route system watrs area exemple 376 10 minutes.

Question 216-17 : North atlantic high level airspace nat hla .during the flight of two aircraft in mnps airspace with a leading aircraft flying at higher speed the longitudinal separation must not be below ?

5 minutes

Longitudinal separations between subsequent aircraft following the same track in trail and between aircraft on intersecting tracks in the nat mnps airspace are assessed in terms of differences in atas/etas at common waypoints the longitudinal separation minima currently used in the nat mnps airspace are thus expressed in clock minutes .doc 7030 nat regional supplementary procedures.6 2 2 1 minimum longitudinal separation between turbo jet aircraft shall be .a 15 minutes or.b 10 minutes provided the mach number technique is applied whether in level climbing or descending flight and the aircraft concerned have reported over a common point to follow continuously diverging tracks until some other form of separation is provided and .1 at least 10 minutes longitudinal separation exists at the point where the tracks diverge and.2 at least 5 minutes longitudinal separation exists where lateral separation is achieved and.3 lateral separation will be achieved at or before the next significant point normally ten degrees of longitude along track s or if not within 90 minutes of the time the second aircraft passes the common point or within 1 112 km 600 nm of the common point whichever is estimated to occur first .6 2 2 2 minimum longitudinal separation between non turbo jet aircraft shall be .a 30 minutes and.b 20 minutes in the west atlantic route system watrs area exemple 380 5 minutes.

Question 216-18 : The term decision height dh is used for ?

A precision approach

Admin .at landing two types of procedures exist . non precision approach rnav/lnav ndb ndb/dme vor vor/dme llz llz/dme vdf sra .and. precision approach ils gls mls par . .for a non precision approach we use the word mdh a minimum descent height altitude .for a precision approach we use the word dh a decision height altitude .at mdh a you are able to level your aircraft at the minimum descent height until reaching a specific point wich can be based on time or distance from a facility offering you opportunity to established visual contact with the runway to perform a landing .at dh a you must initiate a go around procedure . .minimum descent height mdh .for an ils approach without the glidepath localizer only 250 ft .for a for a vor/dme approach 250 ft .for a vor approach 300 ft .for a ndb approach 350 ft .for a rnav/lnav approach 300 ft .decision height dh .for ils cat ii 100 ft .for ils cat i 200 ft .for a gls gnss landing system similar to traditional category i approaches exemple 384 A precision approach.

Question 216-19 : Ops regulation.according to air ops a life jacket is mandatory for each person on board a land aeroplane when flying over water at a distance from the shore of more than ?

50 nm

. easa air ops .cat ide a 285 flight over water . a the following aeroplanes shall be equipped with a life jacket for each person on board or equivalent flotation device for each person on board younger than 24 months stowed in a position that is readily accessible from the seat or berth of the person for whose use it is provided . 1 landplanes operated over water at a distance of more than 50 nm from the shore or taking off or landing at an aerodrome where the take off or approach path is so disposed over water that there would be a likelihood of a ditching and. 2 seaplanes operated over water exemple 388 50 nm.

Question 216-20 : Ops regulation.on overwater flights an operator shall not operate an aeroplane at a distance away from land which is suitable for making a emergency landing greater than that corresponding to ?

400 nm or 120 minutes at cruising speed

. easa air ops .cat ide a 285 flight over water .on overwater flights an operator shall not operate an aeroplane at a distance away from land which is suitable for making an emergency landing greater than that corresponding to ..1 120 minutes at cruising speed or 400 nautical miles whichever is the lesser for aeroplanes capable of continuing the flight to an aerodrome with the critical power unit s becoming inoperative at any point along the route or.planned diversions or.2 30 minutes at cruising speed or 100 nautical miles whichever is the lesser for all other aeroplanes exemple 392 400 nm or 120 minutes at cruising speed.

Question 216-21 : Amc4 spa lvo 100 ecqb2022 v4 .a category ii precision approach cat ii is an approach with ?

A decision height of at least 100 ft

Admin .at landing two types of procedures exist . non precision approach rnav/lnav ndb ndb/dme vor vor/dme llz llz/dme vdf sra .and. precision approach ils gls mls par . .for a non precision approach we use the word mdh a minimum descent height altitude .for a precision approach we use the word dh a decision height altitude .at mdh a you are able to level your aircraft at the minimum descent height until reaching a specific point wich can be based on time or distance from a facility offering you opportunity to established visual contact with the runway to perform a landing .at dh a you must initiate a go around procedure . .minimum descent height mdh .for an ils approach without the glidepath localizer only 250 ft .for a for a vor/dme approach 250 ft .for a vor approach 300 ft .for a ndb approach 350 ft .for a rnav/lnav approach 300 ft .decision height dh .for ils cat ii 100 ft .for ils cat i 200 ft .for a gls gnss landing system similar to traditional category i approaches exemple 396 A decision height of at least 100 ft

Question 216-22 : A category i precision approach cat i is an approach which may be carried out with a runway visual range of at least ?

550 m

Admin .category i cat i approach operation means a precision instrument approach and landing using an instrument landing system ils microwave landing system mls gls ground based augmented global navigation satellite system gnss/gbas landing system precision approach radar par or gnss using a satellite based augmentation system sbas with a decision height dh not lower than 200 ft and with a runway visual range rvr not less than 550 m exemple 400 550 m.

Question 216-23 : With the control display unit cdu of an inertial navigation system ins you can read the following information desired track dtk = 100° track tk = 120° .you can conclude that the ?

Track error angle tke is right r

Dalton .we are diverging too also isn't it ..as you can see the answer aircraft is diverging from its ideal course is not the right answer .maybe the aircraft is diverging maybe the aircraft is converging maybe we are flying parallel to the desired track from the given informations we are unable to conclude on this . marcusorjehag .info from cdu would be 'tke right' and not divergent after all they are asking for the cdu presentation of the info exemple 404 Track error angle (tke) is right (r).

Question 216-24 : The abbreviation mnps means ?

Minimum navigation performance specification

exemple 408 Minimum navigation performance specification

Question 216-25 : For aeroplanes certified before the 1 april 1998 cockpit voice recorder cvr when required must keep the conversations and sound alarms recorded during the last ?

30 minutes of operation

Admin .easa air ops.cat ide a 185 . a an operator shall not operate any aeroplane with a maximum certificated take off mass over 5 700 kg first issued with an individual certificate of airworthiness before 1 april 1998 unless it is equipped with a cockpit voice recorder which records . 1 voice communications transmitted from or received on the flight deck by radio . 2 the aural environment of the flight deck . 3 voice communications of flight crew members on the flight deck using the aeroplane's interphone system . 4 voice or audio signals identifying navigation or approach aids introduced into a headset or speaker and. 5 voice communications of flight crew members on the flight deck using the public address system if installed . b the cockpit voice recorder shall be capable of retaining information recorded during at least the last 30 minutes of its operation . c the cockpit voice recorder must start to record prior to the aeroplane moving under its own power and continue to record until the termination of the flight when the aeroplane is no longer capable of moving under its own power . d the cockpit voice recorder must have a.device to assist in locating that recorder in water exemple 412 30 minutes of operation.

Question 216-26 : On board a non pressurised aircraft 10% of the passengers shall be supplied with oxygen throughout the entire flight time after 30 minutes at pressure altitude greater than ?

10 000 ft and 13 000 ft

Admin .supplemental oxygen for non pressurised aeroplanes. 2624 exemple 416 10 000 ft and 13 000 ft.

Question 216-27 : On board a pressurized aircraft a flight shall be undertaken only if the aircraft is provided with an oxygen reserve enabling all the crew members and part of the passengers to be supplied with oxygen in the event of a cabin depressurization throughout the flight period during which the pressure ?

13 000 ft

Admin oxygen minimum requirements for supplemental oxygen for pressurised aeroplanes. 2625 exemple 420 13 000 ft.

Question 216-28 : For the flight crew members quick donning type of oxygen masks are compulsory on board any pressurised aeroplane operating at a pressure altitude above ?

25 000 ft

Supplemental oxygen pressurised aeroplanes.a . .b . . iv oxygen masks for use by flight crew members in pressurised aeroplanes operating at pressure altitudes above 25 000 ft shall be a quick donning type of mask exemple 424 25 000 ft.

Question 216-29 : All aeroplanes must be fitted with a flight data recorder fdr when their maximum certificated take off mass is greater than ?

5700 kg

Admin .cat ide a 190 flight data recorder.the following aeroplanes shall be equipped with a flight data recorder fdr that uses a digital method of recording and storing data and for which a method of readily retrieving that data from the storage medium is available .1 aeroplanes with an mctom of more than 5 700 kg and first issued with an individual cofa on or after 1 june 1990 .2 turbine engined aeroplanes with an mctom of more than 5 700 kg and first issued with an individual cofa before 1 june 1990 and .3 multi engined turbine powered aeroplanes with an mctom of 5 700 kg or less with an mopsc of more than nine and first issued with an individual cofa on or after 1 april 1998 exemple 428 5700 kg.

Question 216-30 : The minimum lateral separation in the nat region is ?

60 nm between aircraft meeting minimum navigation performance specifications

Please download the guidance concerning air navigation in and above the north atlantic mnps airspace edition 2010 .pdf675.16 3 route planning.lateral separation minima & resulting route definition conventions.16 3 1 in the north atlantic mnps airspace the lateral separation standard is 60 nm since 60 nm is equivalent to one degree of latitude along any meridian and given that the vast majority of flights through this airspace are generally eastbound or westbound this standard is deemed to be met by tracks separated by one degree of latitude at common meridians exemple 432 60 nm between aircraft meeting minimum navigation performance specifications.

Question 216-31 : Which separation will be provided if reduced vertical separation minimum rvsm is used when operating in mnps airspace ?

60 nm lateral and 1000 ft vertical

Doc 9574 manual on implementation of a 300 m 1000 ft vertical separation minimum between fl 290 and fl 410 inclusive .rvsm refers to a vertical.separation minimum of 300 m 1000 ft between fl 290 and fl 410 inclusive .mnpsa manual .in the mnps airspace the lateral separation standard is 60 nm exemple 436 60 nm lateral and 1000 ft vertical.

Question 216-32 : Following an explosive decompression the maximum altitude without oxygen supply at which flight crew efficiency is not impaired is ?

8000 ft

exemple 440 8000 ft.

Question 216-33 : The coverage angle of the regulatory white navigation / position lights located to the rear of the aircraft is ?

140°

Admin . 1463.same for helicopters exemple 444 140°.

Question 216-34 : During a night flight an observer located in the cockpit seeing an aircraft coming from front right on approximate opposite parallel track will first see the ?

Green light

Admin . 1463.this aircraft coming in front of us from the right will not cut our path he will stay on our right in the opposite direction . 1464 exemple 448 Green light.

Question 216-35 : During a night flight an observer located in the cockpit seeing an aircraft coming from front left on approximate opposite parallel track will first see the ?

Red steady light

Admin . 1463.take care this aircraft coming in front of us from the left will not cut our path he will stay on our left in the opposite direction . 1662 exemple 452 Red steady light.

Question 216-36 : The coverage angle of the red navigation/position light is ?

110°

Admin . 1463 exemple 456 110°.

Question 216-37 : Astronomic precession ?

Causes the gyro axis to spin to the right in the northern hemisphere

Admin .astronomic precession is 'earth rate' the gyro drift due to earth rotation 15° / h x sin lm .it is the angular velocity or rate of the earth's rotation .it causes the gyro axis to spin to the right in the northern hemisphere .it causes the gyro axis to spin to the left in the southern hemisphere exemple 460 Causes the gyro axis to spin to the right in the northern hemisphere.

Question 216-38 : The lowest minima to be used by an operator for circling with a category d aeroplane is a meteorological visibility of ?

3600 m

Admin .lowest minima for circling .category a 1500 m .category b 1600 m .category c 2400 m .category d 3600 m exemple 464 3600 m

Question 216-39 : The lowest minima to be used by an operator for circling with a category c aeroplane is a meteorological visibility of ?

2400 m

Admin .lowest minima for circling .category a 1500 m .category b 1600 m .category c 2400 m .category d 3600 m

Question 216-40 : The lowest minima to be used by an operator for circling with a category b aeroplane is a meteorological visibility of ?

1600 m

Admin .lowest minima for circling .category a 1500 m .category b 1600 m .category c 2400 m .category d 3600 m exemple 472 1600 m.


~

Exclusive rights reserved. Reproduction prohibited under penalty of prosecution.

8599 Free Training Exam