Materie
Allenamento!
Simulazione d'esame
Esame in PDF!
Partner
Contattaci
iOS & Android »

Flight Planning and Monitoring - ATPL - Airline Transport Pilot license

Test 10 domande Flight Planning and Monitoring, tempo libero

1 - Refer to CAP 697 Section 2 SEP1 Page 3 Figure 2.1 Time, Fuel and Distance to Climb. Given: Take-off mass 3500 lbs, departure aerodrome pressure altitude 2500 ft,OAT +10°C,First cruising level: FL 140, OAT -5°CFind the time, fuel and still air distance to climb.

24 min, 7.7 GAL, 47 NAM 16.5 min, 4.9 GAL, 34.5 NAM 23.5 min, 7.1 GAL, 48.5 NAM 23 min, 7.7 GAL, 50 NAM

2 - For the purposes of Item 9 (Wake turbulence category) of the ATC flight plan, an aircraft with a maximum certificated take-off mass of 62000 kg is:

Heavy 'H' Light 'L' Medium 'M' Unclassified 'U'

3 - Given: true course (TC) 017 W/V 340/30TAS 420 kt Find: wind correction angle (WCA) and ground speed (GS) WCA +2° GS 396 kt WCA -2° GS 426 kt WCA -2° GS 396 kt WCA +2° GS 416 kt

4 - Refer to CAP697 Section 4 - MRJT1 Page 17 Figure 4.4 Holding Fuel Flow - Flaps RetractedThe final reserve fuel taken from the HOLDING PLANNING table for the twin jet aeroplane is based on the following parameters: Pressure altitude, aeroplane mass and flaps up with maximum range speed Pressure altitude, aeroplane mass and flaps down with maximum range speed Pressure altitude, aeroplane mass and flaps down with minimum drag airspeed Pressure altitude, aeroplane mass and flaps up with minimum drag airspeed[see Annex]

5 - The maximum permissible take-off mass of an aircraft for the L wake turbulence category on an ATC flight plan is: 2 700 kg 7 000 kg 10 000 kg 5 700 kg

6 - The planned departure time from the parking area is 1815 UTC The estimated take-off time is 1825 UTCThe flight plan must be filed with ATC at the latest at: 1725 UTC 1745 UTC 1715 UTC 1755 UTC

7 - On an instrument approach chart, a minimum sector altitude (MSA) is defined in relation to a radio navigation facility. Without any particular specification on distance, this altitude is valid to: 20 NM 25 NM 10 NM 15 NM

8 - Refer to CAP697 MRJT1 Figure 4.7.2 (One Engine Inop):An aircraft on an extended range operation is required never to be more than 120 minutes from an alternate, based on 1 engine inoperative LRC conditions in IS Using the above table and a given mass of 40000 kg at the most critical point, the maximum air distance to the relevant alternate is: 810 NM 794 NM 875 NM 735 NM[see Annex]

9 - Refer to CAP697 MRJT1 Figure 4.5.4 (Descent)A descent is planned at .74/250KIAS from 35000ft to 5000ft. How much fuel will be consumed during this descent? 150kg 140kg 278kg 290kg[see Annex]

10 - Planning an IFR-flight from Paris (Charles de Gaulle) to London (Heathrow) for the twin jet aeroplane.Given: Estimated Take-off Mass (TOM) 52000 kg, Airport elevation 387 ft, FL 280, W/V 280°/40 kt, ISA Deviation -10°C, Average True Course 340°Find: Time to the top of climb (TOC) 3 min 11 min 15 min 12 min[see Annex]

Cambia Materia

Iscriviti alla Newsletter:

QuizVds.it - Facebook - Contattaci - Donazione - Cookie Policy - Privacy Policy