Example: quiz answers

CAP 698 CAA JAR-FCL Examinations

CAP 698 CAA JAR-FCL ExaminationsAeroplane Performance ManualThird Edition July Regulation Group 698 CAA JAR-FCL ExaminationsAeroplane Performance ManualThird Edition July 2006 Safety Regulation GroupCAP 698 CAA JAR-FCL Examinations - Aeroplane Performance Manual Civil Aviation Authority 2006 All rights reserved. Copies of this publication may be reproduced as training material for students, foruse within a company or organisation, or for personal use, but may not otherwise be reproduced forpublication or for commercial use or reference CAA publications for any other purpose, please contact the CAA at the addressbelow for formal 0 11790 653 0 First published August 1999 Second edition June 2001 Third edition July 2006 Third edition (corrected) September 2006 Enquiries regarding the content of this publication should be addressed to.

aeroplane is flown in accordance with the recommended techniques. Outside Air Temperature (OAT or SAT) The free air static (ambient) temperature. Take-Off Mass (TOM) The mass of an aeroplane, including everything and everyone contained within it, at the start of the take-off run. TAS The 'true airspeed' is the speed of the

Tags:

  Examination, Aeroplanes, 698 caa jar fcl examinations

Information

Domain:

Source:

Link to this page:

Please notify us if you found a problem with this document:

Other abuse

Advertisement

Transcription of CAP 698 CAA JAR-FCL Examinations

1 CAP 698 CAA JAR-FCL ExaminationsAeroplane Performance ManualThird Edition July Regulation Group 698 CAA JAR-FCL ExaminationsAeroplane Performance ManualThird Edition July 2006 Safety Regulation GroupCAP 698 CAA JAR-FCL Examinations - Aeroplane Performance Manual Civil Aviation Authority 2006 All rights reserved. Copies of this publication may be reproduced as training material for students, foruse within a company or organisation, or for personal use, but may not otherwise be reproduced forpublication or for commercial use or reference CAA publications for any other purpose, please contact the CAA at the addressbelow for formal 0 11790 653 0 First published August 1999 Second edition June 2001 Third edition July 2006 Third edition (corrected) September 2006 Enquiries regarding the content of this publication should be addressed to.

2 Personnel Licensing Department, Safety Regulation Group, Civil Aviation Authority, Aviation House,Gatwick Airport South, West Sussex, RH6 latest version of this document is available in electronic format at ,where you may also register for e-mail notification of by TSO (The Stationery Office) on behalf of the UK Civil Aviation copy available from: TSO, PO Box 29, Norwich NR3 orders/General enquiries: 0870 600 5522E-mail: orders: 0870 600 5533 Textphone: 0870 240 3701 CAP 698 CAA JAR-FCL Examinations - Aeroplane Performance ManualSectionPageDateSectionPageDate Page iiiiiiJuly 2006 (corr.)ivJuly 2006vJuly 2006viJuly 2006 Revision History1 July 2006 (corr.)Revision History2 July 2006 Section 11 July 2006 Section 12 July 2006 Section 13 July 2006 Section 14 July 2006 Section 21 July 2006 (corr.)

3 Section 22 July 2006 (corr.)Section 23 July 2006 Section 24 July 2006 Section 25 July 2006 Section 26 July 2006 Section 27 July 2006 Section 28 July 2006 Section 29 July 2006 Section 210 July 2006 Section 31 July 2006 Section 32 July 2006 Section 33 July 2006 Section 34 July 2006 Section 35 July 2006 (corr.)Section 36 July 2006 Section 37 July 2006 Section 38 July 2006 (corr.)Section 39 July 2006 Section 310 July 2006 Section 311 July 2006 (corr.)Section 312 July 2006 Section 313 July 2006 (corr.)Section 314 July 2006 Section 315 July 2006 Section 316 July 2006 Section 317 July 2006 Section 318 July 2006 Section 319 July 2006 Section 320 July 2006 Section 321 July 2006 (corr.)Section 322 July 2006 Section 323 July 2006 (corr.)Section 324 July 2006 Section 41 July 2006 Section 42 July 2006 Section 43 July 2006 Section 44 July 2006 (corr.)

4 Section 45 July 2006 Section 46 July 2006 Section 47 July 2006 Section 48 July 2006 Section 49 July 2006 Section 410 July 2006 Section 411 July 2006 Section 412 July 2006 Section 413 July 2006 Section 414 July 2006 Section 415 July 2006 Section 416 July 2006 Section 417 July 2006 Section 418 July 2006 Section 419 July 2006 Section 420 July 2006 Section 421 July 2006 Section 422 July 2006 Section 423 July 2006 Section 424 July 2006 Section 425 July 2006 Section 426 July 2006 Section 427 July 2006 Section 428 July 2006 Section 429 July 2006 Section 430 July 2006 Section 431 July 2006 Section 432 July 2006 Section 433 July 2006 Section 434 July 2006 Section 435 July 2006 Section 436 July 2006 Section 437 July 2006 Section 438 July 2006 Section 439 July 2006 Section 440 July 2006 Section 441 July 2006 (corr.)

5 Section 442 July 2006 (corr.)Section 443 July 2006 (corr.)Section 444 July 2006 (corr.)Section 445 July 2006 Section 446 July 2006 Section 447 July 2006 Section 448 July 2006 Section 449 July 2006 Section 450 July 2006 July 2006 (corr.)List of Effective PagesINTENTIONALLY LEFT BLANKPage ivCAP 698 CAA JAR-FCL Examinations - Aeroplane Performance ManualJuly 2006 CAP 698 CAA JAR-FCL Examinations - Aeroplane Performance Manual Page vList of Effective PagesiiiRevision History1 Section 1 General NotesAircraft Description1 Layout of Data Sheets1 Definitions2 Conversions4 Section 2 Data for Single-Engine Piston Aeroplane (SEP1)General Considerations1 Take-Off1 Take-Off Climb6En-Route8 Landing9 Section 3 Data for Multi-Engine Piston Aeroplane (MEP1)General Considerations1 Take-Off1 Take-Off Climb9En-route17 Landing17 Section 4 Data for Medium-Range Jet Transport (MRJT1)

6 General Considerations1 Take-Off7 Obstacle Clearance35En-route39 Landing45 July 2006 ContentsINTENTIONALLY LEFT BLANKCAP 698 CAA JAR-FCL Examinations - Aeroplane Performance Manual Page viJuly 2006 CAP 698 CAA JAR-FCL Examinations - Aeroplane Performance Manual Revision History Page 1 Revision History1st EditionAugust 1999 CAP 698, CAA JAR-FCL Examinations Performance Manual, was produced to support trainingand Examinations in JAR-FCL Subject 032 - Performance for EditionJune 2001 The manual was reissued to incorporate CAA House Edition July 2006 This edition has been upgraded with digitised graphics. Definitions and conversions have beenrationalised and known errors have been Edition (corrected) September 2006 Since the publication of the third edition, some errors and omissions have been identified.

7 Thecorrections are as follows:The affected pages are identified by the word (corr.) after the page Page(s)Correction2/SEP1 Text of paragraph to Example and Solution at paragraph and associated conditions; 'reaction time'corrected to 'recognition time'.3/MEP11 Fig ROC scale; '800' corrected to '500'.3/MEP13 Fig Associated conditions; 'Inoperative enginefeathered' and 'obstacle speed' corrected to 'barrierspeed'.3/MEP23 Fig speed scale of barrier speed ; '90' changed to'82' and '66' changed to '68'.4/MRJT4 Fig - At base of graph, 'crosswind component' , 42, 43, 44 Figs , , and ; Max continuous thrustlimit box; 'A/C Auto (High)' corrected to 'A/C OFF'.July 2006 (corr.)INTENTIONALLY LEFT BLANKR evision History Page 2 CAP 698 CAA JAR-FCL Examinations - Aeroplane Performance ManualJuly 2006 CAP 698 CAA JAR-FCL Examinations - Aeroplane Performance Manual Section 1 - General Notes Page 1 Section 1 General Notes1 IntroductionImportant data sheets in this manual are produced to support training and Examinations inJAR-FCL Subject 032 - Performance for data contained within these sheets are for training and examination purposesonly.

8 The data must not be used for any other purpose and, specifically, are not tobe used for the purpose of planning activities associated with the operation ofany aeroplane in use now or in the aeroplanes used in these data sheets are of generic types related to the classesof aeroplane on which the appropriate Examinations are must select the correct class of aeroplane for the question beingattempted. same set of generic aeroplanes will be utilised in the following subjects: 031 - Mass and Balance - aeroplanes 032 - Performance - aeroplanes 033 - Flight Planning and Monitoring - Aeroplanes3 Layout of Data set of data sheets will consist of an introduction that will contain some pertinentinformation relating to the aircraft and the subject being examined. This data willinclude (but is not limited to) a list of abbreviations and some conversion will be followed by a selection of graphs and/or tables that will provide coveragesuitable for the syllabus to be examined.

9 A worked example will accompany eachgraph/table and will demonstrate typical AeroplanesSingle-Engine Pistoncertificated under CS 23 (Light aeroplanes )Performance Class BSEP1 Multi-Engine Pistoncertificated under CS 23 (Light aeroplanes )Performance Class BMEP1 Medium-Range Jet Transport certificated under CS 25 (Large aeroplanes )Performance Class AMRJT1 July 2006 CAP 698 CAA JAR-FCL Examinations - Aeroplane Performance Manual Section 1 - General Notes Page 24 DefinitionsDefinitions given in italics are not given in ICAO, or JAA or EASA documentation butare in common altitude shown on the charts is pressure altitude. This is the height in the International Standard Atmosphere at which the prevailing pressure occurs. It may be obtained by setting the sub-scale of a pressure altimeter to 1013 hPa ( inches or 760 mm.)

10 Of mercury).Climb GradientThe ratio, in the same units of measurement, expressed as a percentage, as obtained from the formula:-Gradient = Change in Height x 100% Horizontal Distance ElevationThe vertical distance of an object above mean sea level. This may be given in metres or HeightThe true height attained at any point in the take-off flight path using gross climb performance. Gross height is used for calculating pressure altitudes for purposes of obstacle clearance and the height at which wing flap retraction is PerformanceThe average performance that a fleet of aeroplanes should achieve if satisfactorily maintained and flown in accordance with the techniques described in the vertical distance between the lowest part of the aeroplane and the relevant Standard Atmosphere (ISA)A structure of assumed conditions relating to the change of pressure, temperature and density with height in the airspeed is the reading obtained on a pitot-static airspeed indicator calibrated to reflect standard adiabatic compressible flow at mean sea Structural Landing MassThe maximum permissible total mass of an aeroplane on landing (under normal circumstances).


Related search queries