CAP 747 Mandatory Requirements for Airworthiness

Section 2 Part 1, DHC-1 2 30 November 2009 Section 2 Part 1, DHC-1 3 30 November 2009 Section 2 Part 1, DHC-1 4 30 November 2009 Section 2 Part 1, DHC-1 5 30 November 2009 Section 2 Part 1, DHC-1 6 30 November 2009 Section 2 Part 1, DHC-1 7 29 June 2012 Section 2 Part 1, DHC-1 8 29 June 2012 List of Effective Pages CAP 747 Mandatory Requirements for Airworthiness 24 March 2020 Page iv Part Chapter Page Date Part Chapter Page Date Section 2 Part 1, DHC-1 9 28 February 2014 Section 2 Part 1, DHC-1 10 28 February 2014 Section 2 Part 1, DH 60-94 1 30 November 2009 Section 2 Part 1, DH 60-94 2 29 January 2010 Section 2 Part 1, DH 60-94 3 29 January 2010 Section 2 Part 1, DH 60-94 4 25 November 2014 Section 2 Part 1, DH 60-94 5 25 November 2014 Section 2 Part 1, DH 60-94 6 25 November 2014 Section 2 Part 1, DH 60-94 6 25 November 2014 Section 2 Part 1, DH 60-94 7 25 November 2014 Section 2 Part 1, DH 60-94 8 25 November 2014 Section 2 Part 1, DH 60-94 9 25 November 2014 Section 2 Part 1, DH 60-94 10 25 November 2014 Section 2 Part 1, DH 60-94 11 25 November 2014 Section 2 Part 1, DH 60-94 12 25 November 2014 Section 2 Part 1, DH104 1 30 November 2009 Section 2 Part 1, DH104 2 30 November 2009 Section 2 Part 1, DH104 3 30 November 2009 Section 2 Part 1, DH104 4 30 November 2009 Section 2 Part 1, DH104 5 30 November 2009 Section 2 Part 1, DH104 6 30 November 2009 Section 2 Part 1, DH104 7 30 November 2009 Section 2 Part 1, DH104 8 30 November 2009 Section 2 Part 1, DH104 9 30 November 2009 Section 2 Part 1, DH104 10 30 November 2009 Section 2 Part 1, DH104 11 30 November 2009 Section 2 Part 1, DH104 12 30 November 2009 Section 2 Part 1, DH104 13 30 November 2009 Section 2 Part 1, DH104 14 30 November 2009 Section 2 Part 1, DH104 15 30 November 2009 Section 2 Part 1, DH104 16 30 November 2009 Section 2 Part 1, DH104 17 30 November 2009 Section 2 Part 1, DH104 18 30 November 2009 Section 2 Part 1, DH114 1 30 November 2009 Section 2 Part 1, DH114 2 30 November 2009 Section 2 Part 1, DH114 3 30 November 2009 Section 2 Part 1, DH114 4 30 November 2009 Section 2 Part 1, DH114 5 30 November 2009 Section 2 Part 1, DH114 6 30 November 2009 Section 2 Part 1, DH114 7 30 November 2009 Section 2 Part 1, DH114 8 30 November 2009 Section 2 Part 1, DH114 9 30 November 2009 Section 2 Part 1, DH114 10 30 November 2009 Section 2 Part 1, DH114 11 30 November 2009 Section 2 Part 1, DH114 12 30 November 2009 Section 2 Part 1, DH114 13 30 November 2009 Section 2 Part 1, Dornier 1 30 November 2009 Section 2 Part 1, Douglas 1 29 January 2010 Section 2 Part 1, Douglas 2 29 January 2010 Section 2 Part 1, Douglas 3 21 February 2011 Section 2 Part 1, Douglas 4 21 February 2011 Section 2 Part 1, Douglas 5 21 February 2011 Section 2 Part 1, Douglas 6 21 February 2011 Section 2 Part 1, Jodel 1 30 November 2009 Section 2 Part 1, Learjet 1 30 November 2009 Section 2 Part 1, Lockheed 1 30 November 2009 Section 2 Part 1, Luscombe 1 30 November 2009 Section 2 Part 1, Miles M14A 1 30 November 2009 Section 2 Part 1, Miles M14A 2 30 November 2009 Section 2 Part 1, Miles M38 1 30 November 2009 Section 2 Part 1, Miles M38 2 30 November 2009 Section 2 Part 1, Miles M38 3 30 November 2009 Section 2 Part 1, Miles M38 4 30 November 2009 Section 2 Part 1, Miles M38 5 30 November 2009 Section 2 Part 1, Miles M65 1 30 November 2009 Section 2 Part 1, Miles M65 2 30 November 2009 Section 2 Part 1, Miles M65 3 30 November 2009 Section 2 Part 1, Miles M65 4 30 November 2009 Section 2 Part 1, Miles M65 5 30 November 2009 Section 2 Part 1, Perc. Prentice 1 30 November 2009 Section 2 Part 1, Perc. Proctor 1 30 November 2009 Section 2 Part 1, Perc. Proctor 2 30 November 2009 Section 2 Part 1, Perc. Proctor 3 30 November 2009 Section 2 Part 1, Perc. Proctor 4 30 November 2009 Section 2 Part 1, Perc. Proctor 5 30 November 2009 Section 2 Part 1, Rollason 1 30 November 2009 Section 2 Part 1, Scheibe 1 30 November 2009 Section 2 Part 1, Scheibe 2 30 November 2009 Section 2 Part 1, Scott. Aviation 1 30 November 2009 Section 2 Part 1, Scott. Aviation 2 30 November 2009 Section 2 Part 1, Scott. Aviation 3 30 November 2009 Section 2 Part 1, Scott. Aviation 4 30 November 2009 Section 2 Part 1, Scott. Aviation 5 30 November 2009 Section 2 Part 1, Scott. Aviation 6 30 November 2009 Section 2 Part 1, Scott. Aviation 7 30 November 2009 Section 2 Part 1, Scott. Aviation 8 30 November 2009 Section 2 Part 1, Scott. Aviation 9 30 November 2009 Section 2 Part 1, Scott. Aviation 10 30 November 2009 Section 2 Part 1, Scott. Aviation 11 30 November 2009 Section 2 Part 1, Scott. Aviation 12 30 November 2009 Section 2 Part 1, Sikorsky 1 30 November 2009 Section 2 Part 1, Slingsby T61 1 24 March 2020 Section 2 Part 1, Slingsby T61 2 24 March 2020 Section 2 Part 1, Stampe 1 30 November 2009 Section 2 Part 1, Trago Mills 1 30 November 2009 Section 2 Part 1, Westland 1 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness 24 March 2020 Page v Part Chapter Page Date Part Chapter Page Date Section 2 Part 1, Westland 2 30 November 2009 Section 2 Part 1, Alvis 1 30 November 2009 Section 2 Part 1, RRCheetah 1 30 November 2009 Section 2 Part 1, RRCheetah 2 30 November 2009 Section 2 Part 1, RR Cirrus 1 30 November 2009 Section 2 Part 1, RR Cirrus 2 30 November 2009 Section 2 Part 1, RR Cirrus 3 30 November 2009 Section 2 Part 1, RR Cirrus 4 30 November 2009 Section 2 Part 1, RR Cirrus 5 30 November 2009 Section 2 Part 1, RR Cirrus 6 30 November 2009 Section 2 Part 1, RR Continental 1 30 November 2009 Section 2 Part 1, RR Continental 2 30 November 2009 Section 2 Part 1, RR Continental 3 30 November 2009 Section 2 Part 1, RR Gem 1 30 November 2009 Section 2 Part 1, RR Gipsy 1 30 November 2009 Section 2 Part 1, RR Gipsy 2 30 November 2009 Section 2 Part 1, RR Gipsy 3 30 November 2009 Section 2 Part 1, RR Gnome 1 30 November 2009 Section 2 Part 1, RR Gnome 2 30 November 2009 Section 2 Part 1, RR Gnome 3 30 November 2009 Section 2 Part 1, RR Tyne 1 30 November 2009 Section 2 Part 1, RR Tyne 2 30 November 2009 Section 2 Part 1, RR Tyne 3 30 November 2009 Section 2 Part 1, RR Viper 1 30 November 2009 Section 2 Part 1, RR Viper 2 30 November 2009 Section 2 Part 1, RR Viper 3 30 November 2009 Section 2 Part 1, RR Viper 4 30 November 2009 Section 2 Part 1, RR Viper 5 30 November 2009 Section 2 Part 1, RR Viper 6 30 November 2009 Section 2 Part 1, RR Viper 7 30 November 2009 Section 2 Part 1, BAe Dynamics 1 29 January 2010 Section 2 Part 1, BAe Dynamics 2 29 January 2010 Section 2 Part 1, BAe Dynamics 3 29 January 2010 Section 2 Part 1, BAe Dynamics 4 29 January 2010 Section 2 Part 1, BAe Dynamics 5 29 January 2010 Section 2 Part 1, BAe Dynamics 6 29 January 2010 Section 2 Part 1, BAe Dynamics 7 29 January 2010 Section 2 Part 1, BAe Dynamics 8 29 January 2010 Section 2 Part 1, BAe Dynamics 9 29 January 2010 Section 2 Part 1, BAe Dynamics 10 29 January 2010 Section 2 Part 1, BAe Dynamics 11 29 January 2010 Section 2 Part 1, BAe Dynamics 12 29 January 2010 Section 2 Part 1, BAe Dynamics 13 29 January 2010 Section 2 Part 1, BAe Dynamics 14 29 February 2012 Section 2 Part 1, Dowty Aerosp 1 30 November 2009 Section 2 Part 1, Dowty Aerosp 2 30 November 2009 Section 2 Part 1, Dowty Aerosp 3 30 November 2009 Section 2 Part 1, Dowty Aerosp 4 30 November 2009 Section 2 Part 1, Dowty Aerosp 5 30 November 2009 Section 2 Part 1, Dowty Aerosp 6 30 November 2009 Section 2 Part 1, Dowty Aerosp 7 30 November 2009 Section 2 Part 1, Dowty Aerosp 8 30 November 2009 Section 2 Part 1, Dowty Aerosp 9 30 November 2009 Section 2 Part 1, Dowty Aerosp 10 30 November 2009 Section 2 Part 1, Dowty Aerosp 11 30 November 2009 Section 2 Part 1, Dowty Aerosp 12 30 November 2009 Section 2 Part 1, Dowty Aerosp 13 30 November 2009 Section 2 Part 1, Dowty Aerosp 14 30 November 2009 Section 2 Part 1, Dowty Aerosp 15 30 November 2009 Section 2 Part 1, Dowty Aerosp 16 30 November 2009 Section 2 Part 1, Dowty Aerosp 17 30 November 2009 Section 2 Part 1, Dowty Aerosp 18 30 November 2009 Section 2 Part 1, Dowty Aerosp 19 29 January 2010 Section 2 Part 1, Dowty Aerosp 20 29 January 2010 Section 2 Part 1, Dowty Aerosp 21 30 November 2009 Section 2 Part 1, Fairey Reed 1 30 November 2009 Section 2 Part 1, Permali 1 30 November 2009 Section 2 Part 1, Equipment 1 30 November 2009 Section 2 Part 1, Equipment 2 30 November 2009 Section 2 Part 1, Equipment 3 30 July 2016 Section 2 Part 1, Equipment 4 30 July 2016 Section 2 Part 1, Equipment 5 30 July 2016 Section 2 Part 1, Equipment 6 30 July 2016 Section 2 Part 1, Equipment 7 30 July 2016 Section 2 Part 1, Equipment 8 30 July 2016 Section 2 Part 1, Equipment 9 30 July 2016 Section 2 Part 1, Equipment 10 30 July 2016 Section 2 Part 1, Equipment 11 30 July 2016 Section 2 Part 2 1 24 March 2020 Section 2 Part 2 2 29 January 2010 Section 2 Part 3 1 24 March 2020 Section 2, Part 3, GR No. 4 1 30 November 2009 Section 2, Part 3, GR No. 4 2 30 November 2009 Section 2, Part 3, GR No. 4 3 30 November 2009 Section 2, Part 3, GR No. 6 1 30 November 2009 Section 2, Part 3, GR No. 6 2 16 November 2012 Section 2, Part 3, GR No. 8 1 16 November 2012 Section 2, Part 3, GR No. 8 2 16 November 2012 Section 2, Part 3, GR No. 8 3 16 November 2012 Section 2, Part 3, GR No. 9 1 16 November 2012 Section 2, Part 3, GR No. 9 2 16 November 2012 Section 2, Part 3, GR No. 10 1 21 July 2017 Section 2, Part 3, GR No. 10 2 24 March 2020 Section 2, Part 3, GR No. 10 3 21 July 2017 Section 2, Part 3, GR No. 10 4 21 July 2017 Section 2, Part 3, GR No. 11 1 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness 24 March 2020 Page vi Part Chapter Page Date Part Chapter Page Date Section 2, Part 3, GR No. 11 2 30 November 2009 Section 2, Part 3, GR No. 15 1 24 March 2020 Section 2, Part 3, GR No. 15 2 16 November 2012 Section 2, Part 3, GR No. 16 1 30 November 2009 Section 2, Part 3, GR No. 16 2 30 November 2009 Section 2, Part 3, GR No. 17 1 24 March 2020 Section 2, Part 3, GR No. 17 2 24 March 2020 Section 2, Part 3, GR No. 17 3 30 July 2016 Section 2, Part 3, GR No. 17 4 30 November 2009 Section 2, Part 3, GR No. 18 1 30 November 2009 Section 2, Part 3, GR No. 18 2 30 November 2009 Section 2, Part 3, GR No. 19 1 30 November 2009 Section 2, Part 3, GR No. 19 2 30 November 2009 Section 2, Part 3, GR No. 19 3 30 November 2009 Section 2, Part 3, GR No. 23 1 25 November 2014 Section 2, Part 3, GR No. 23 2 25 November 2014 Section 2, Part 3, GR No. 23 3 25 November 2014 Section 2, Part 3, GR No. 23 4 25 November 2014 Section 2, Part 3, GR No. 23 5 25 November 2014 Section 2, Part 3, GR No. 23 6 25 November 2014 Section 2, Part 3, GR No. 24 1 24 March 2020 Section 2, Part 3, GR No. 24 2 24 March 2020 Section 2, Part 3, GR No. 24 3 24 March 2020 Section 2, Part 3, GR No. 24 4 24 March 2020 Section 2, Part 3, GR No. 24 5 24 March 2020 Section 2, Part 3, GR No. 24 6 21 December 2012 Section 2, Part 3, GR No. 24 7 21 December 2012 Section 2, Part 3, GR No. 24 8 21 December 2012 Section 2, Part 3, GR No. 24 9 21 December 2012 Section 2, Part 3, GR No. 25 1 24 March 2020 Section 2, Part 3, GR No. 25 2 29 February 2012 Section 2, Part 4, GC No. 1 1 24 March 2020 Section 2, Part 4, GC No. 1 2 30 November 2009 Section 2, Part 4, GC No. 1 3 30 November 2009 Section 2, Part 4, GC No. 1 4 30 November 2009 Section 2, Part 4, GC No. 6 1 24 March 2020 Section 2, Part 4, GC No. 6 2 24 March 2020 Section 2, Part 4, GC No. 6 3 24 March 2020 Section 2, Part 4, GC No. 6 4 24 March 2020 Section 2, Part 4, GC No. 6 5 24 March 2020 Section 2, Part 4, GC No. 6 6 31 May 2012 Section 2, Part 4, GC No. 6 7 31 May 2012 Section 2, Part 4, GC No. 6 8 31 May 2012 Section 2, Part 4, GC No. 6 9 24 March 2020 Section 2, Part 4, GC No. 6 10 24 March 2020 Section 2, Part 4, GC No. 7 1 24 March 2020 Section 2, Part 4, GC No. 7 2 24 March 2020 Section 2, Part 4, GC No. 7 3 16 November 2012 Section 2, Part 4, GC No. 7 4 16 November 2012 Section 2, Part 4, GC No. 7 5 16 November 2012 Appendix 1 1 30 November 2009 Appendix 1 2 30 November 2009 Appendix 1 3 30 November 2010 Appendix 1 4 21 February 2011 Appendix 1 5 21 February 2011 Appendix 1 6 21 February 2011 Appendix 1 7 21 February 2011 Appendix 1 8 30 November 2009 Appendix 1 9 29 February 2012 Appendix 1 10 25 November 2014 Appendix 1 11 25 November 2014 CAP 747 Mandatory Requirements for Airworthiness 24 March 2 0 2 0 Page 1 List of Effective Pages Foreword Revision History Section 1 General Information Part 1 Introduction and Guide to Use Part 2 Lists of Non-EASA Products, their Classification, and States of Design Part 3 Sources of Data Section 2 Mandatory Information Introduction Section 2, Contents Part 1 Airworthiness Directives and Mandatory Information Issued by the CAA Aircraft Engines Propellers Equipment Part 2 Requirements applicable to State/public service aircraft Part 3 Generic Requirements (GRs) Part 4 Generic Concessions (GCs) Appendix 1 Requirements Removed CAA Airworthiness Directives and Mandatory Requirements removed from CAP 747 Contents INTENTIONALLY LEFT BLANK CAP 747 Mandatory Requirements for Airworthiness Page 1 Foreword 1 Introduction This CAP 747 is the means by which airworthiness requirements made mandatory by the CAA are notified; (pursuant to Article 39 of the Air Navigation Order 2016 as amended). This publication also identifies the sources for other requirements made mandatory for UK-registered aircraft subject to European legislation. 2 ICAO Compliance Statement to CAP 747 Mandatory Requirements for Airworthiness 2.1 The Civil Aviation Authority (Chicago Convention) Directions 2007, issued by the Department for Transport (DfT), require the Civil Aviation Authority (CAA) to ensure that it acts consistently with the obligations placed on the UK under the Convention on International Civil Aviation (Chicago Convention) of December 1944. 2.2 This document is published in support of the CAA’s discretionary powers contained in the Air Navigation Order and includes requirements based on certain International Standards and Recommended Practices (SARPs) contained in Annexes to the Chicago Convention. 2.3 It is the policy of the CAA to have reference to this document when exercising the discretionary powers referred to above and, in particular, it will exercise those powers to ensure the effective implementation of any such requirements based on SARPs. 3 Classification of Products 3.1 Each aircraft type is categorised as either: • an “EASA aircraft”; (an aircraft that is included in the scope of Regulation (EU) 2018/1139; or • a “Non-EASA aircraft”; (an aircraft that is subject to national regulations). 3.2 Aircraft that fall within the categories set out in Annex 1 to Regulation (EU) 2018/1139 are “non-EASA aircraft” types. In addition, individual aircraft that are operated for certain State or public service purposes as set out in Article 2 of Regulation (EU) 2018/1139 are subject to national regulations; (e.g. military, customs, police, search and rescue, firefighting, border control, coastguard aircraft). All other aircraft are “EASA aircraft” regardless of their State of Design or State of Manufacture. 3.3 For both EASA and non-EASA aircraft, CAA and EASA requirements, and requirements notified by the State of Design of the aircraft, (and its engines, propellers and equipment as applicable) may be mandatory. Section 1, Part 3 of this CAP 747 identifies the sources of these mandatory requirements. 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Page 2 4 Status 4.1 This CAP 747 is the means by which airworthiness requirements made mandatory by the CAA are notified. 4.2 Some requirements previously made mandatory for UK-registered aircraft were withdrawn on 28 September 2003, when European regulations came into force. Aircraft owners and operators should ensure that: a) any retained modifications installed in order to comply with previous additional UK requirements continue to be maintained in accordance with all applicable approved data and service information; b) any de-modification of an aircraft is performed by approved organisations or licensed aircraft engineers in accordance with approved airworthiness documentation. Following de-modification, a review and re-issue of the continued airworthiness instructions must be carried out and a Certificate of Release to Service obtained; c) any data from the Type Certificate Holder that has previously been made mandatory by the CAA, but is no longer mandatory, should still be considered for inclusion in the maintenance programme. Failure to do so could expose the aircraft to safety hazards and may invalidate the Certificate of Airworthiness. 5 Generic Concessions 5.1 A number of concessions are set out in Section 2, Part 4 of this CAP 747.These may be used by UK-registered aircraft subject to the limitations and conditions specified. 6 Interpretation 6.1 The Requirements, with or without explanatory material, should not be regarded as constituting text book material. The interpretation of the Requirements against a background of current aeronautical knowledge is essential. 6.2 Mandatory clauses are denoted by the use of “shall” or “must”; “should” or “may” are used in the text to introduce permissive or recommended clauses. 6.3 Imperatives such as “ensure”, “prevent” and “shall be designed”, imply that all steps deemed necessary will be taken, on the basis of the knowledge and techniques available at the time. 6.4 It is implicit in requirements expressed qualitatively (e.g. “readily visible”, “adequately tested”, etc.) that the CAA will adjudicate in cases where doubt exists. 6.5 An Airworthiness Directive is a document issued or adopted by the Authority of the State of Registry of an aircraft which mandates the actions to be performed to restore an acceptable level of safety to an aircraft when an unsafe condition has been identified. 6.6 Words purporting the masculine gender include the feminine. 7 Notification of Requirements 7.1 Aircraft on the UK Register are required by law to comply with applicable Airworthiness Directives (ADs) issued by the UK CAA, EASA, and the National Aviation Authority (NAA) of the State of Design. See Guide to Identifying the Applicable Requirements, in Section 1, Part 1. 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Page 3 7.2 Non-Emergency ADs 7.2.1 EASA is responsible for distributing EASA ADs for aircraft subject to European regulations, to ICAO Contracting States.These ADs are available from the EASA website at www.easa. eu. You may register for e-mail notification at: http://ad.easa.europa.eu/. 7.2.2 The CAA is responsible for notifying other ICAO Contracting States of CAA ADs for UK Products not subject to European regulations.These are available from the CAA website at: https://www.caa.co.uk/Commercial-Industry/Aircraft/Airworthiness/Continuing- airworthiness/Airworthiness-Directives/. 7.2.3 CAA ADs are published in CAP 747; other ADs may be obtained from EASA or the originating NAA as applicable. 7.3 Emergency ADs 7.3.1 Where urgency dictates that a short timescale is required to address an unsafe condition, the CAA, EASA or NAA will issue an Emergency Airworthiness Directive (EAD). 7.3.2 All EADs for affected UK-registered aircraft are published by the CAA on its website at http://publicapps.caa.co.uk/modalapplication.aspx?appid=11&mode=list&type=sercat&id=54. 7.3.3 To receive notification when a new EAD is published owners/ operators/ maintenance organisations etc. should register with the CAA’s free publications subscription service at www.caa.co.uk > Publications > Subscriptions and choose the ‘Safety Critical Information’ category. Existing Subscribers should ensure this category is added to their subscription. Subscribers will then be notified every time a new EAD is published on the CAA website. 7.3.4 EADs will be available for download from the CAA website for a period of two months from the date of publication and will then be removed. EADs issued by the CAA will have been incorporated into CAP 747 before they are removed; other EADs may be obtained from EASA or the originating NAA as applicable. 7.3.5 In order for NAAs of ICAO Contracting States of Registry to receive UK Emergency ADs in a timely manner they must also subscribe to the above service. 8 Responsibilities of Owners/Operators and Individuals/Organisations Carrying Out Maintenance and Overhaul 8.1 In order to ensure compliance with all applicable mandatory requirements, the owners and operators of aircraft must ensure that they are aware of the content of any Airworthiness Directives issued by the National Aviation Authority of the State of Design and EASA and of any applicable CAA Airworthiness Directives or mandatory requirements. 8.2 In addition, organisations or individuals undertaking maintenance and overhaul must ensure that they are in receipt of Airworthiness Directives issued by the National Aviation Authority of the State of Design and EASA, and any CAA Airworthiness Directives or mandatory requirements applicable to the Products, Parts and Appliances which they maintain or overhaul. NOTE: When an individual or organisation maintains or overhauls Products, Parts and Appliances for an owner/operator whose aircraft is not registered in the United Kingdom, the individual/organisation must make arrangements with that owner/ operator to receive any Airworthiness Directives issued or adopted by the Civil Aviation Authority of the State of Registry. 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Page 4 9 Repetitive Inspection 9.1 Non-EASA Aircaft used for Purposes Other Than Commercial Air Transport 9.1.1 Where an Airworthiness Directive requires an inspection to be carried out at intervals not exceeding 24 hours (elapsed time) the CAA may invoke the authorisation given under paragraph 9.1.2 below, for inspection by the pilot in command. In such cases, the text of the Airworthiness Directive will prescribe the authorisation. 9.1.2 The Civil Aviation Authority (CAA), in exercise of its powers under Article 48(1) (c) of the Air Navigation Order 2016 as amended, hereby authorises a pilot as a person competent to issue a Certificate of Release to Service in respect of a mandatory inspection required by an Airworthiness Directive where the inspection recurs at periods not exceeding 24 hours elapsed time, subject to the following conditions: a) The pilot must hold a Group or Type rated licence applicable to the type quoted in the inspection. b) The pilot must have sufficient technical knowledge and have received specific training to provide that person with the competence to accomplish the inspection which may also require the use of simple visual inspection aids. c) The specific training must be provided by an appropriately licenced aircraft maintenance engineer or organisation approved by the CAA for that purpose. 9.1.3 When certifying an inspection in accordance with paragraph 9.1.2 the certifying signature will be that of the pilot followed by his licence number. 9.2 Commercial Air Transport by Licensed Air Carriers 9.2.1 All maintenance-related certifications for aircraft operated for Commercial Air Transport must be made by persons authorised in accordance with Regulation (EU) No. 1321/2014, Annex II (Part 145). The authorisation of 9.1.2 above cannot be used. 9.2.2 In accordance with 145.A.30(j)(3): for compliance with a repetitive pre-flight mandatory action, where the Airworthiness Directive states specifically that the flight crew may carry out the action, a Part-145 organisation may issue a limited certification authorisation to the aircraft commander and/or the flight engineer on the basis of the flight crew licence held. 9.2.3 When certifying an inspection in accordance with paragraph 9.2.2 the certifying signature will be that of the person authorised by the Part-145 organisation and the relevant authorisation reference shall be recorded. 10 Mandatory Changes to Flight Manuals or Performance Schedules 10.1 Where an Airworthiness Directive introduces a change to an aircraft Flight Manual or Performance Schedule, the Owner/Operator of the affected aircraft must ensure that the change is made by attaching the Airworthiness Directive or the documents that it specifies, to the Flight Manual or Performance Schedule. NOTE: Where permission has been given to utilise an Operations Manual in lieu of the Flight Manual, the Owner/Operator must ensure that the information specified in the Airworthiness Directive is embodied in the Operations Manual within the specified compliance time. 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Page 5 11 Extension of Airworthiness Directive Compliance Timescale 11.1 Aircraft owners, operators and contracted maintenance organisations must assess all Airworthiness Directives relating to relevant aircraft types and initiate early requisition and/or provision of aircraft parts and/or maintenance resources to meet the Airworthiness Directive compliance timescales. 11.2 Any application to extend an Airworthiness Directive compliance timescale will be assessed by the CAA on a case-by-case basis. The applicant, normally supported by the organisation responsible for the type design, must demonstrate, to the satisfaction of the CAA, an equivalent level of safety. Extensions of this nature are intended to be used in exceptional circumstances that could not reasonably have been foreseen by the owner, operator or contracted maintenance organisation. 12 Airworthiness Directive Alternative Method of Compliance (AMOC) 12.1 EASA Aircraft 12.1.1 Any application to satisfy an Airworthiness Directive by means of an ‘alternative method of compliance’ will be assessed by EASA on a case by case basis and will normally need to be supported by the organisation responsible for the type design.The applicant must demonstrate, to the satisfaction of the Agency, an equivalent level of safety. A request for an AMOC should be made using an EASA Form 42. 12.1.2 The EU Bilateral arrangements with Canada, Brazil and the United States allow for acceptance of certain AMOCs issued by the airworthiness authorities of these countries when acting as State of Design for the product, part or appliance.The text of these decisions may be obtained from the Agency website at https://www.easa.europa.eu/ document-library/bilateral-agreements 12.2 Non-EASA Aircraft 12.2.1 Any application to satisfy an Airworthiness Directive by means of an ‘alternative method of compliance’ will be assessed by the CAA on a case by case basis and will normally need to be supported by the organisation responsible for the type design.The applicant must demonstrate, to the satisfaction of the CAA, an equivalent level of safety. 13 Accuracy of Information 13.1 The information presented in CAP 747 is the best available on the date that each amendment is approved for publication and printing. 14 Amendments 14.1 Amendments to CAP 747 are published as required. Each page is identified by the date of issue or date at which it is amended. Material differences from the previous issue are marked with marginal lines. Where text has overflowed, the affected pages are identified by the date of re-issue. The remaining pages retain their existing dates and are therefore not re-supplied. 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Page 6 24 March 2020 15 Enquiries 15.1 Any enquiries regarding CAP 747 should be sent to the Future Safety Technical Support Team (mail to: FSTechnicalSupportTeam@caa.co.uk). CAP 747 Mandatory Requirements for Airworthiness Page 1 Revision History Initial Issue June 2004 The initial issue of CAP 747 was brought about by the coming into force of European legislation, creating the European Aviation Safety Agency (EASA) and the consequent need for the CAA to declare its intention to retain certain requirements for UK registered aircraft. Issue 2 September 2004 The purpose of Issue 2 was to provide a single point of reference for all mandatory information for continuing airworthiness, including airworthiness directives, as applicable to civil aircraft registered in the UK. Issue 3 November 2009 The purpose of Issue 3 was to provide all mandatory information for continuing airworthiness as issued by the CAA in one CAP. Therefore all ADs issued by EASA have been removed and are available on the EASA website. Issue 3, amdt 2010/01 January 2010 CAP 747 is amended to update the EAD Subscription link in the Foreword and to correct errors incorporated at Issue 3, including: • the removal of previously cancelled ADs, the inclusion of AD G-2005-0030 as this is currently unavailable elsewhere, and a correction to the names in the footers in Section 2, Part 1; • the removal from Section 2 Part 3 of GR Nos. 5 and 7 (both previously cancelled); and • the inclusion of – Aircraft engaged in Military, Police, Customs or similar services in Section 2, Part 2. Issue 3, amdt 2010/02 February 2010 CAP 747 is amended to update the references to the ANO 2009 and incorporate some editorial corrections. Issue 3, amdt 2010/03 March 2010 CAP 747 has been amended to: • update the product list; • remove CAA AD 003-10-2001 which has been cancelled and superseded by EASA AD 2010-0023; • replace in its entirety GR No. 23. Issue 3, amdt 2010/04 June 2010 CAP 747 is amended to revise the Lists of Products, their Classification, and States of Design, following an update by EASA. 30 June 2010 CAP 747 Mandatory Requirements for Airworthiness Page 2 Issue 3, amdt 2010/05 September 2010 CAP 747 has been amended to: • update the product list; • update some of the Foreign NAAs’ website addresses; • revise GR No. 3. Issue 3, amdt 2010/06 November 2010 CAP 747 has been amended to: • update the product list; • revise GR No. 3; • correct an error in Appendix 1. Issue 3, amdt 2011/01 February 2011 CAP 747 has been amended to: • update the product list; • insert CAA AD 001-07-78 which should have been included in the original issue of Issue 3, and which negates the need for the inclusion of CAA AD 2854 pre 80; • remove CAA AD 2854 pre 80; • revise GC No. 6, Appendix 1 to GC No. 6 and Schedule 2 to GC No. 6; • add CAA AD 2854 pre 80 to Appendix 1 Requirements Removed. Issue 3, amdt 2011/02 March 2011 CAP 747 has been amended to: • update the product list. Issue 3, amdt 2011/03 May 2011 CAP 747 has been amended to: • update the product list; • update the Dutch NAA contact details; • correct a typographical error in Schedule 2 to GC No. 6. Issue 3, amdt 2011/04 June 2011 CAP 747 has been amended to: • update the product list. Issue 3, amdt 2011/05 August 2011 CAP 747 has been amended to: • update the product list. 31 October 2011 CAP 747 Mandatory Requirements for Airworthiness Page 3 Issue 3, amdt 2011/06 October 2011 CAP 747 has been amended to: • update the product list. • update Part 2 Requirements applicable to State/public service aircraft. Issue 3, amdt 2012/01 February 2012 CAP 747 has been amended to: • update Figure 3 reference to Mandatory Permit Directives under General Information; • update the product list; • update the NAA contact details for New Zealand; • remove CAA AD 004-05-91 which has been cancelled and superseded by FAA AD 93-06-06; • update Appendix 1 to include the cancellation of AD 004-05-91 and to correct an entry; • insert new GR No 25. Issue 3, amdt 2012/02 May 2012 CAP 747 has been amended to: • update the product list; • replace in its entirety GC No 6. Issue 3, amdt 2012/03 June 2012 CAP 747 has been amended to: • insert UK CAA AD G-2012-0001. Issue 3, amdt 2012/04 November 2012 CAP 747 has been amended to: • Revise Section 1, Parts 1 and 2 NOTE: All EASA products with a type-certificate either issued or accepted by EASA, or a specific airworthiness specification issued by EASA are removed from Section 1, Part 2 ‘List of Products, their Classification, and States of Design’; • Update references to CAP 562; • Revise GR No. 23; • Insert new GC No. 7, its Appendix 1 and Schedule 1. 21 December 2012 CAP 747 Mandatory Requirements for Airworthiness Page 4 Issue 3, amdt 2012/05 December 2012 CAP 747 has been amended to: • Update Foreword, paragraph 1; • Update Section 1 Part 1 and Part 2; • Update GR No. 23; NOTE: In addition to the technical revision of GR No. 23 at 2012/04 amdt, further editorial changes and minor technical amendments, convenient to be included at this time have been incorporated; • Revise GR No. 24. Issue 3, amdt 2014/01 February 2014 CAP 747 has been amended to: • Insert UK CAA ADs: G-2013-0001, G-2013-0002 and RAF Radio Equipment; • Revise GR 24, Paragraph 5; • Incorporate some editorial corrections. Issue 3, amdt 2014/02 November 2014 CAP 747 has been amended to: • Insert UK CAA ADs: G-2014-0001-E, G-2014-0002-E and G-2014-0003-E; • Delete GRs: 2, 3, 13, 14, 20, 21 and 22; • Delete GCs: 2, 3, 4 and 5; • Incorporate some editorial corrections. NOTE: Several Generic Requirements (GRs) have been deleted as a result of the implementation of EASA EU OPS rules. Also, several Generic Concessions (GCs) have been withdrawn from CAP 747 to support CAA’s updated policy on Motor Gasoline (MOGAS). Issue 3, amdt 2016/01 30 July 2016 CAP 747 has been amended to: • Update Section 1 Part 1, Introduction and Guide to Use; • Update Section 1 Part 2, Products List; • Update Section 1 Part 3, Sources of Data; • Insert UK CAA AD: G-2015-0001R1; • Replace in entirety GR No 10; • Update GRs: 17 and 24. Issue 3, amdt 2017/01 21 July 2017 CAP 747 has been amended to: • Update Section 1 Part 2, Products List; • Replace in entirety GR No 10. 21 July 2017 CAP 747 Mandatory Requirements for Airworthiness Page 5 Issue 3, amdt 2020/01 24 March 2020 The primary purpose of amendment 2020/01 was to update GR No 15, GR No 17 and GR No 24 to align with the introduction of Part M Light (Part-ML) under Regulation (EU) 2019/1383, which became applicable on 24 March 2020. In addition, the opportunity was taken to update some of Section 2, including various references to the EU Regulations and UK ANO Articles as applicable at the date of publication. The main changes include: • Text changes to the Foreword. • Text changes to Section 1, Part 1. • An update to the list of non-EASA products in Section 1, Part 2. • The inclusion of CAA AD G-2018-0001 for Slingsby T61 in Section 2, Part 1. • The minor update of Section 2, Part 2. • The minor update of GR No 10 and GR No 25 in Section 2, Part 3. • The update of GR No 15, GR No 17 and GR No 24 in Section 2, Part 3. • The revision of GC No 6, including an updated Appendix 1 and 3, in Section 2, Part 4. • The minor update of GC No 1 and GC No 7, in Section 2, Part 4. 24 March 2020 INTENTIONALLY LEFT BLANK CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 1 Page 1 Section 1 General Information Part 1 Introduction and Guide to Use 1 Classification of aircraft as “EASA Aircraft” and “Non-EASA Aircraft” 1.1 Under Regulation (EU) 2018/1139 the European Aviation Safety Agency (EASA) has responsibility for the airworthiness standards applicable to the majority of the civil aircraft registered in the Member States of the European Union. However, the Regulation also stipulates that certain aircraft are subject to national regulations. • “EASA aircraft” are those aircraft that are included in the scope of Regulation (EU) 2018/1139. • “Non-EASA aircraft” are aircraft that fall within the categories set out in Annex I of Regulation (EU) 2018/1139 (reference Article 2 of the Regulation). Non-EASA aircraft are not subject to regulation of airworthiness by EASA, but are subject to national regulations. 1.2 All EASA products with a type-certificate either issued or accepted by EASA, or a specific airworthiness specification issued by EASA, are listed on the EASA website at the following website addresses: https://www.easa.europa.eu/document-library/product-certification/type-certificates /easa-product-lists https://www.easa.europa.eu/document-library/specific-airworthiness-specifications 1.3 Annex I of Regulation (EU) 2018/1139 defines various categories of aircraft as “non- EASA aircraft”. These categories include homebuilts, microlights, gyroplanes and foot- launched gliders. Additional categories in Annex II are historic aircraft (or aircraft having historical relevance), research aircraft and ex-military aircraft. The list of aircraft given in Section 1, Part 2 of this CAP 747 shows aircraft types on the UK register in these last three categories and which have therefore been designated as “non-EASA aircraft”. The list also includes aircraft notified by EASA as “not transferred” and which remain subject to regulation under National Procedures. NOTE: This CAP 747 also contains UK additional mandatory requirements for EASA aircraft types on the UK register. 1.4 Individual aircraft engaged in certain State or public services are subject to national airworthiness regulations, even if other aircraft of the same type (that are not engaged in such activities) are subject to regulation by EASA (reference Article 2 of Regulation (EU) 2018/1139). These individual aircraft are not identified in CAP 747 because their status may change depending upon the purpose of a particular flight. For further guidance see CAP 562 (CAAIP) Leaflet B-60. 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 1 Page 2 2 Guide to identifying the Applicable Requirements Figure 1 How to determine the applicable requirements for your product 24 March 2020 Is your product included in the product lists on the EASA website? Go to Figure 2 Is your product listed as “Annex I” or “Not” Transferred in the alphabetical lists in Section 1, Part 2? Go to Figure 3 Contact the CAA No No Yes Yes CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 1 Page 3 Figure 2 How to locate mandatory requirements for an EASA product Figure 2 – How to locate mandatory requirements for an EASA product Contact the National Aviation Authority of the State of Design for applicable requirements. A contact list is available on the CAA website (see Section 1 Part 3) Was the product designed in the UK? See Section 2, Part 1 for any applicable Mandatory Requirements See the EASA website for applicable Airworthiness Directives issued by EASA Generic Concessions and Generic Requirements may apply. See Section 2 Parts 3 and 4 Is the aircraft engaged in military, police, customs or similar services? Add any requirements notified in Section 2, Part 2 End No Yes Yes No See CAP 476 for applicable Airworthiness Directives issued by the CAA before 28/09/2004 30 July 2016 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 1 Page 4 Figure 3 How to locate mandatory requirements for a non-EASA (Annex I) product 24 March 2020 Figure 3 – How to locate mandatory requirements for a non-EASA (Annex II) product No Yes Yes No Was the product designed in the UK? Generic Concessions and Generic Requirements may apply. See Section 2 Parts 3 and 4 Is the aircraft engaged in military, police, customs or similar services? End Contact the National Aviation Authority of the State of Design for applicable requirements. A contact list is available on the CAA website (see Section 1, Part 3) Add any requirements notified in Section 2, Part 2 See Section 2, Part 1 for any applicable Mandatory Requirements issued by the CAA Is the aircraft operating on a Permit to Fly? See CAP 661 and the CAA website for applicable Mandatory Permit Directives Yes No CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 1 Page 5 3 Applicability of Mandatory Requirements to engines, propellers, parts and appliances installed in “EASA Aircraft” and “Non-EASA Aircraft” with a Certificate of Airworthiness (CofA) 3.1 Where an EASA Airworthiness Directive is in force for any engine, propeller, part or appliance, it shall be complied with regardless of whether the engine, propeller, part or appliance is installed in an EASA aircraft or a non-EASA aircraft, unless the CAA notifies otherwise. 3.2 A product, part or appliance installed in a non-EASA aircraft shall comply with the mandatory requirements for non-EASA aircraft that are applicable to the product, part or appliance. 3.3 Where a product, part or appliance is installed in a non-EASA aircraft and there is a conflict between EASA Airworthiness Directives and other Airworthiness Directives or mandatory requirements applicable to the product, part or appliance, the advice of the CAA shall be obtained. 3.4 Where a product, part or appliance is transferred from one aircraft to another, the installer shall ensure that the mandatory requirements applicable to the receiving aircraft are complied with. 4 Applicability of Mandatory Requirements to engines, propellers, parts and appliances installed in aircraft with a UK National Permit to Fly 4.1 A product, part or appliance installed in an aircraft with a National Permit to Fly shall comply with the Mandatory Permit Directives published by the CAA. 4.2 Where an EASA Airworthiness Directive is in force for any engine, propeller, part or appliance used on a Permit to Fly aircraft, it shall be complied with, unless CAA notifies otherwise. 24 March 2020 INTENTIONALLY LEFT BLANK CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 1 Part 2 Lists of Non-EASA Products, their Classification, and States of Design NOTE: In the followingTables the abbreviations “N” and “A” are used in the last column to signify: N Aircraft notified by EASA as ‘not transferred’ and which remain subject to regulation under National Procedures; A Aircraft classified as Annex I (non-EASA) aircraft. Table 1.1 Large Aeroplanes Manufacturer/ TC Holder Product Name TC number State of Design N/A Aviation Traders ATL 98 Carvair UK A AVRO Lancaster UK A BAE Systems (Operations) Limited Jetstream 3102 s/n 614 UK A Boeing (Including McDonnell Douglas/ Douglas) B-17G USA A Bristol 170 UK A British Aerospace 146-301 ARA UK A Consolidated PBY-5A 28-5ACF Catalina USA A Douglas DC-3C-R-1830-90C USA A DC-6 Series USA A English Electric Canberra Series UK A Ilyushin IL-18 Russia N IL-62 N PZL AN-28 Poland N Tupolev TU-134M Russia N TU-154B2 N Yakovlev YAK-42D Russia N Table 1.2 Light / Commuter / Very Light Aeroplanes Aero 145 Czech Republic A C104 A L-29 Delfin A L-39 Albatros Series A L-159 Albatros Series A Aeronca 11 A-761/A-796 USA A 65 Series A-728 A 100 A-396 A C3 A-396 A K A-676/688 A O-58B A-751 A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 2 Table 1.2 Light / Commuter / Very Light Aeroplanes (Continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A Aeronca/American Champion/Bellanca/ Champion 7AC A-759 USA A 7ACA A-759 A 7BCM A-759 A 7ECA with Continental O-200-A/McCauley Prop. A-759 A 7ECA with Lycoming O-235-C1/McCauley Prop. A-759 A 7ECA with Lycoming O-235-C1/Sensenich Prop. A-759 A 7ECA with Lycoming O-235- K2C/Sensenich Prop. (pre 1981) A-759 A 7FC A-759 A 7GCAA with Lycoming O-320- A2B/McCauley Prop. A-759 A 7GCAA with Lycoming O-320- A2B/Sensenich Prop. A-759 A 7GCBC with Lycoming O-320- A2B/McCauley Prop. A-759 A 7GCBC with Lycoming O-320- A2B/Sensenich Prop. A-759 A 7KCAB A-759 A AESL Airtourer 115 (modified) New Zealand A Albatros D.Va-1 Replica Germany A Alon A-2 USA A ANEC II UK A Antonov An-2 Russia A Arrow Active II UK A ARV Aviation Ltd ARV1 ARV1 Super 2 UK A Auster All Series UK A Avia FL3 Italy A Aviamilano/Aeromere Falco F8L Italy A Avro 504K UK A 643 Cadet Series A 652A Anson T21 A Avian Series A C19 Series 2 A Triplane Replica A Tutor A BA Eagle 2 UK A Swallow 2 A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 3 Table 1.2 Light / Commuter / Very Light Aeroplanes (Continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A BAC 167 Strikemaster Series UK A BAC (1935) Ltd. Drone UK A Barfuss Marabu Switzerland A Beagle A.61 Terrier Series UK A A.109 Airedale A B206 Series A E3 A Beagle Auster D5 Series 180 UK A Beech 35, G35 A-777 USA (A-777 Models) A D17S USA A Expeditor Series A Bell P-39Q Airacobra USA A P-63 Kingcobra TC-21 A Bellanca Model 14 Series A-773 USA A Binder-Aviatick GmbH CP 301 Smaragd 564/SA Germany A Blackburn 1912 Monoplane UK A B.2 Series 1 A Bleriot XI France A Boeing 75 Stearman Series A-743 USA A Bristol Bolingbroke MK.IV T UK A Boxkite Replica A Fighter F2B A M1C Monoplane Replica A Bucker BU131 Jungmann LBA 717/SA Germany A BU133 Jungmeister Series LBA 582/SA A BU181 Bestmann (including Heliopolis Gomhouria MK6) LBA 716/SA A Canadian Car & Foundry Harvard Series A-80 Canada A CASA 1-131E Series Germany A Cessna 120 Series FAA A-768 USA A 140 Series FAA 5A2/A-768 A C-165 A 170 Series FAA A-799 A 190/195 Series FAA A-790 A 305C A Chance-Vought FG-1D Corsair USA A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 4 Table 1.2 Light / Commuter / Very Light Aeroplanes (Continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A Chilton DW1 Series UK A Chrislea CH3 Super Ace Series 2 UK A Civilian Coupe 02 UK A CMC Leopard 001/002 Prototypes UK A Commonwealth CA 18 MK 22 (Mustang P-51D) USA A Comper CLA7 Swift UK A CLA7 Swift Replica A Crofton Auster J1-A UK A Culver LCA Cadet USA A Curtiss C-2 Robin (Modified) USA A H-75A-1 Hawk A P-36 A P-40 Series A Travel Air 12Q A Dart Kitten UK A de Havilland DH9 UK A DH51 A DH53 Hummingbird A DH60G AAN 27543 Iss 2 A DH60M/GM/GMW AAN 29290 Iss 1 A DH60GIII AAN 28474 Iss 2 A DH60X AAN 28787 Iss 2 (G-EBWD only) A DH71 Tiger Moth A DH80A Puss Moth AAN 28870 Iss 1 A DH82A (Aust) Tiger Moth A DH82A Tiger Moth AAN 22556 Iss 9 A DH82B Queen Bee A DH83 Fox Moth Series AAN 24808 Iss 4 A DH84 Dragon AAN 28148 Iss 1 A DH85 Leopard Moth AAN 24160 Iss 3 A DH87B Hornet Moth AAN 27522 Iss 4 A DH88 Comet Racer A DH89A Rapide Series AAN 25002 Iss 2 A DH90A Dragonfly AAN 23636 Iss 1 (G-AEDU only) A DH94 Moth Minor AAN 29291 Iss 1 A DH100 Vampire Series A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 5 Table 1.2 Light / Commuter / Very Light Aeroplanes (Continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A de Havilland contd. DH104 Dove Series UK A DH110 Sea Vixen FAW MK2 A DH112 Venom Series A DH114 Sea Heron C MK1 AAN 23020 Iss 2 A DH115 Vampire Series A de Havilland Canada DHC-1 Chipmunk Mk21 AAN 1399 Iss 1 UK A DHC-1 Chipmunk Mk22 + 22A AAN 4383 Add4 Iss 6 A DHC-1 Chipmunk Mk23 AAN 10239 A de Havilland Canada (Viking Air) DHC-1A-1 Chipmunk A-19 Canada A DHC-2 Beaver 1 A-22 A DHC-3 Otter A-27 A Deperdussin Monoplane France A Desoutter Monoplane UK A Dornier Do 27 LBA 514/SA Germany A Douglas Skyraider AD4-NA USA A Druine/Rollason D.31 Turbulent UK A D.62 Condor Series A EADS PZL PZL-101 Gawron Poland A PZL-111 Koliber A Edgar Percival EP9 Prospector UK A English Electric Wren UK A Ercoupe 415 Series USA A Extra Flugzeugbau GmbH EA 230 Germany A Fairchild 24R-46A Argus Series USA A M62 Cornell A Fairey Battle UK A Gannet Series A Federal Aircraft Factory C3605 Schlepp Switzerland A Fiat CR42 Italy A G46-3B A Fieisler F156 Series LBA 725/SA Germany A Fleet Model 80 Canuck Canada A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 6 Table 1.2 Light / Commuter / Very Light Aeroplanes (Continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A Flugzeugbau W. Uetz U3M Pelikan Switzerland A U4M Pelikan A Focke-Wulfe FW189A-1 Germany A FW44J Steiglitz LBA 726/SA A Focke-Wulfe/Flug + Werk FW190 Series Germany A Fokker DR1 Replica Germany A Fokker S11-1 Netherlands A Folland Gnat T MK 1 UK A Forney F-1A USA A Foster-Wikner Wicko GM-1 UK A Fouga CM.170 Magister France A Garland-Bianchi/ Fairtravel Linnet 1/2 UK A Globe CG-1B Swift USA A Glos-Air Airtourer Series New Zealand A Gloster Gladiator UK A Meteor NF11 A Meteor T-7 A Gould-Taylorcraft Plus D Special USA A Great Lakes 2T-1A USA A Grumman F6F-3 Hellcat USA A F7F-3 Tigercat A F8F-2P Bearcat LTC-23 A FM2 Wildcat A TBM-3R Avenger A Hawker Audax UK A Cygnet Replica A Demon A Fury Mk1 A Fury/Sea Fury Series A Hind A Hunter Series A Hurricane Series A Nimrod Series A Tempest II/V A Tomtit A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 7 Table 1.2 Light / Commuter / Very Light Aeroplanes (Continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A Helton Lark 95 USA A Hindustan HAL-26 Push Pak India A Hispano HA1112M1L Spain A Hispano HA1112M4L Buchon Germany A Hunting P84 Jet Provost Series UK A Jodel D14 France A D112 TCDS 3 A D117 A D119 TCDS 21 A D120 TCDS 17 A D127 TCDS 3 A D128 TCDS 21 A D140 TCDS 20 A D150 TCDS 81/TC 27 A D1120 TC 23 A D1190 TC 23 A DR100 TCDS 34 A DR105 TCDS 34 A DR1050 TCDS 34/TC 6 A DR1051 TCDS 34/TC 6 A Junkers JU87/R4 Germany A Klemm KI 35 LBA 710/SA Germany A L25-1A LBA 573/SA A Lake Aircraft Corp LA-4-180 USA A Latinoamericana de Aviacion (Lavia) SA (Lavia manufactured aircraft) Note: Piper manufactured PA-25 aircraft are eligible for an EASA C of A. PA-25 AV-0004 Argentina N PA-25-235 N PA-25-260 N Lockheed T-33 Silver Star 3 USA A Luscombe Aircraft Corp. Luscombe 8 Series A-694 USA A LVG CVI Germany A Max Holste MH1521 Series TCS 47 & 57 France A Menavia/Piel/Scintex CP 301 A/B Emeraude TCDS 18/28 France A CP 1310/1320/1330/Super Emeraude TCDS 75 A CP 1315 Super Emeraude TCDS 75 A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 8 Table 1.2 Light / Commuter / Very Light Aeroplanes (Continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A Messerschmitt BF108 LBA 572/SA Germany A BF109 Series A Miles M2L Hawk Six UK A M2W Hawk A M3A Falcon A M5 Sparrowhawk A M11A Whitney Straight A M14A Magister/Hawk Trainer 3 A M17 Monarch A M28 Mercury A M38 Messenger Series A M65 Gemini 1A A Monocoupe 90A USA A Morane Saulnier MS.230 France A MS.315E D2 A MS.317 A MS.505 Criquet A MS.733 Alcyon A MS.760 A N Replica A Nanchang CJ-6A China A NAS Tiger Moth UK A Naval Aircraft Factory N3N-3 A-2-569 USA A Nieuport Scout 17/23 Replica France A Noorduyn AT-16 Harvard IIB Canada A Nord 1002 TCDS 45 France A 1101 TCS 89 A N3202-B1 A NC 854 S A NC 856 Norvigie A NC 858 S A Norman Aeroplane Co. NAC-1/2 Series 180 Freelance UK A NDN-1 Firecracker A NDN-1 Turbo Firecracker A North American F86A Sabre USA A P-51 Mustang Series A OV-10 Bronco A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 9 Table 1.2 Light / Commuter / Very Light Aeroplanes (Continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A North American contd. T-6 Harvard Texan Series A-2-575 A T28A Trojan A Orlican Werke L40 Meta Sokol Czech Republic A Parnall ELF II UK A Partenavia/Vulcanair P57 Fachiro II Italy A Percival Mew Gull UK A P10 Vega Gull A P40 Prentice 1 A P56 Provost T1 A P57 Sea Prince T1 A P66 Pembroke C MK1 A Proctor Series A Piaggio Aero Industries FW P149D Italy A Pilatus P2 Series Switzerland A Piper Aircraft Corp J2 USA A J3C A J3C (Modified) A J3C-65 A J3C-65 (Modified) A J3C-90 A J3F-50 A Piper J3L Cub FAA TCDS A-698 A J4A A J4E A J5A 1A2 A J5B 1A2 A L18C 1A2 A L21A (Modified) 1A2 A L21B 1A2 A L21B (Modified) 1A2 A L4H A L4J A PA-11 A-691 A PA-12 A-780 A PA-14 A-797 A PA-15 A-800 A PA-16 1A1 A PA-17 A-805 A PA-18 1A2 A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 10 Table 1.2 Light / Commuter / Very Light Aeroplanes (Continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A Piper Aircraft Corp contd. PA-19 1A2 A PA-20 1A4 A PA-22 1A6 A PA-23-160 Apache 1A10 A Polikarpov PO-2 Russia A Porterfield CP50/65 USA A Putzer Elster B LBA 584/SA Germany A Rearwin 175 USA A 8125 Cloudster A 8500 A Reid and Sigrist RS4 Desford UK A Republic Aviation Corporation (Sky Enterprises Inc) RC-3 Seabee FAA TCDS A-769 USA A Republic/Curtiss P-47 Thunderbolt Series USA A Robinson Redwing UK A Rollason BETA UK A Royal Aircraft Factory SE5A UK A Be2 Series Replica A Ryan PT-22 USA A ST3KR A Saab 91D Safir Sweden A Scottish Aviation Bulldog Series UK A Twin Pioneer 3 A Short Brothers S312 Tucano T.Mk1 UK A SIPA 903 TCDS 8 France A S91 TCS 7 A SNCAN Stampe SV4 Series DGAC-F TCDS 6 Belgium A Soko P-2 KRAGUJ Yugoslavia A Sokol M1C Czech Republic A Somers Kendall SK1 UK A Sopwith 1 1/2 Replica Strutter UK A 7F.1 Snipe Replica A Camel Replica A Dove A Pup A Triplane Replica A Southern Martlet UK A Spartan Arrow UK A SPP Super Aero 45 Poland A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 11 Table 1.2 Light / Commuter / Very Light Aeroplanes (Continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A Stinson 108 USA A HW-75 A Stinson contd. L -1 Vigilant A V-77 Reliant A-774 A Taylorcraft 65 Series USA A BC12D A F-19 Series A F-21 Series A Taylorcraft contd. F-22 Series USA A Plus D A Thruxton Jackaroo UK A Tipsy Belfair Belgium A Nipper A Trainer 1 A Trago Mills Ltd SAH-1 UK A UTVA 66 Yugoslavia A Vickers-Supermarine Seafire Series UK A Spitfire Series A Walrus MK1 A Victa Airtourer Series Australia A Vought/Goodyear F4U/FG-1D Corsair USA A Waco UPF-7 USA A YKS-7 A Wassmer/Issoire WA 51 France A WA 52 A WA 80 TC 51 A WA 81 TC 51 A Westland Lysander IIIA UK A Widgeon III Yakovlev Yak-1 Russia A Yak-3U A Yak-9 A Yak-12 A Yak-18 (But NOT -18T) A Yak-50 A Yak-52 A Yak C.11 A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 12 Table 1.3 Sailplanes/Powered Sailplanes Manufacturer/TC Holder Product Name TC number State of Design N/A Akaflieg Munchen Mu 13 Germany A Alexander Schleicher GmbH Rhönlerche II LBA 164 Germany A Auto-Aero Budapest - Ungarn R 26 SU “Gòbè” Hungary N Birmingham Guild BG-135 UK A Breguet 900 France A 901-7 A 904 Series A Carmam M100 Italy A Carden/Abbott-Baynes Scud Series UK A Edgley EA9 Optimist UK A Elan Flight Ltd. Begunje - Slovenia DG 303 Elan Slovenia N Elliot’s Olympia Series UK A ERI Aviation PIK-16 Vasama Finland A Ets Roche AIR 100/102 France A Fabrika Aviona i Jadrilica ´Jastreb´ Vr ST CIRRUS G/81 Slovenia N Fauvel AV22 France A AV36/361 A Focke Wulfe Kranich Series LBA 111 Germany A Olympia Meise A Weihe LBA 68 A Fournier Aerostructure RF 8 France A RF 10 A Grunau Baby Series Germany A Heine Dittmar Condor 4 Germany A Issoire Aviation D77 Germany A E75, 78, 78B A WA 20 A WA 21 A WA 22, 22A A WA 30 A Loavia LA France A Lunak LF-107 Czech Republic A Moswey-Werke Moswey III S-38-04 Switzerland A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 13 Table 1.3 Sailplanes / Powered Sailplanes (continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A Neukom Elfe PM3 Switzerland A Elfe S-2 A Oberlechner Mg19 Series SF15/92 Austria A Rolladen Schneider Ls8-tpw Germany A Scheibe Rhonsperber Germany A Schempp-Hirth Flugzeugbau GmbH Go3 Mimimoa LBA 59 Germany A Hutter 17 LBA 67 A Schleicher Ka2 Series LBA 140/203 Germany A Ka3 Series LBA 154 A Rhonbussard LBA 50 A Scott Viking UK A Shenstone Harbinger UK A Siren Bertin C34 France A Slingsby Kestrel 22 UK A All models up to and including T50 A T59 Kestrel 19 S/no SSK/JP/054 A T.61 A SNCAN C800 France A Swales SD3 UK A Voigt Alfred Lo100 Germany A Zlin 24 Kranjanek Czech Republic A Table 1.4 Balloons Manufacturer/TC Holder Product Name TC number State of Design N/A Airtour All Models UK A Balóny Kubícek spol.s.r.o AB 3 Czech Republic N AV 2 N Cameron Balloons GB1000 UK A S-31 A Thunder AX3 Sky Chariot A V-20 A Colt Balloons Colt 56C UK A Dragon Balloons All Models UK A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 2 Page 14 Table 1.4 Balloons (Continued) Manufacturer/ TC Holder Product Name TC number State of Design N/A Flying Pictures Apoly1 44000 UK A Interavia 70TA Russia A 80TA A Thunder Balloons 0-5 UK A AX-3 Sky Chariot Series UK A Ultramagic SA Ultramagic V-14 Spain A Western Balloons All Models UK A Table 1.5 Airships Manufacturer/ TC Holder Product Name TC number State of Design N/A Lindstrand Hot Air Balloons Ltd LBL GT110 UK A Thunder Balloons AS-33 UK A Table 1.6 Rotorcraft Manufacturer/ TC Holder Product Name TC number State of Design N/A Agusta/Bell/Westland 47 Series USA A Bristol B.171 Sycamore UK A Hiller Helicopters UH 12 Series USA A ICA Brasov SA316B Alouette III Romania A SARO Skeeter 12 UK A Sud Aviation SE313/3130 Alouette II France A Westland Gazelle AH.MK1 UK A Gazelle HT.MK2 A Gazelle HT.MK3 A Scout AH1 A Wasp HAS1 A Wasp MK1B A Whirlwind HAR MK.10 A WS.58 Wessex Series A 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 1 Part 3 Page 1 30 July 2016 Part 3 Sources of Data This CAP 747 makes reference to data published by ICAO Member States, but does not republish that information. Owners/operators must obtain the data from the issuing organisation. To ensure continuous and timely receipt of mandatory Continuing Airworthiness Information it is necessary to subscribe to a service from the relevant State of Design. Links to foreign NAA websites are listed on the Airworthiness Directives webpage of the CAA website. INTENTIONALLY LEFT BLANK CAP 747 Mandatory Requirements for Airworthiness Section 2 Introduction Page 1 Section 2 Mandatory Information Introduction 1 This Section of CAP 747 provides the airworthiness directives and mandatory information issued by the CAA for specific types of aircraft, engine, propeller and equipment; with the information presented in alphabetical order of each type. (Generic requirements that may apply to any number of products are provided in Section 2, Part 3). 2 Due to the details of the scope of European and UK legislation, mandatory requirements may be applied by the CAA under European regulations, national regulations or both, depending upon the particular circumstance. For each Airworthiness Directive or other mandatory requirement published in CAP 747, that relevant legislation is indicated by annotating the entry according to the following key: Regulation Requirement (1) Requirement applied to EASA aircraft and notified under Article 70 of Regulation (EU) No. 2018/1139; (2) Applied to non-EASA aircraft under the UK Air Navigation Order; (3) Maintenance or Operations related requirements applied under the UK Air Navigation Order or Commission Regulation (EU) No. 1321/2014 Annex I (Part M). NOTE: Only those Mandatory requirements that are currently applicable have been transferred from CAP 476 Mandatory Modifications and Inspections Summary (UK aircraft). Those items that were cancelled or superseded have not been included. 24 March 2020 INTENTIONALLY LEFT BLANK CAP 747 Mandatory Requirements for Airworthiness Section 2 Contents Page 1 Part 1 Airworthiness Directives and Mandatory Information Issued by the CAA Aircraft (2) AESL, Glos Air Airtourer and Victa Airtourer Series and Airtourers Modified to AESL-T3 Standard (2) ARV Aviation ARV 1 Super 2 Aircraft (2) Auster 3, 4 and 5 Variants ‘J’ and ‘D’ Series and Taylorcraft Plus ‘C’ and ‘D’ Aircraft (2) Auster 6A and Beagle A.61 Series Aircraft (2) Aviation Traders ATL98 Carvair (2) Avro Anson and Avro 19 (2) Beagle A.109 Aircraft (2) Beagle B.121 Series Aircraft (2) Beagle B.206 Series 1 and 2 Aircraft (1) Bell 206 Series Helicopters (1) Bell 212 Series Helicopters (1) Boeing 727 Series 100, 100C and 200 (1) Boeing 737-200 and -200 Adv Series (1) Boeing 737-300, 400 and 500 Series (1) Boeing 737-300 Pemco Freighter/QC STC Conversion (1) Boeing 747 Series Aircraft (1) Boeing 757 Series Aircraft (1) Boeing 767 Series Aircraft (1) Boeing (Douglas) DC8 Series 50 (1) Boeing (Douglas) DC8-63 and 63F (1) Boeing (McDonnell Douglas) DC-9 Series (1) Boeing (McDonnell Douglas) DC-10 Series (1) Boeing (Autair, Hawker Siddeley Canada Ltd) Harvard all variants (1) Bombardier (De Havilland Canada) DHC-7 (1) Cessna Series Aircraft (2) De Havilland DHC–1 Chipmunk Series Aircraft (2) De Havilland DH60, DH80, DH82, DH83, DH85, DH87, DH94 and Queen Bee Series Aircraft (2) De Havilland DH89 Rapide Series Aircraft (2) De Havilland DH104 Dove Series Aircraft 24 March 2020 Section 2, Contents Key: (1) Requirement applied to EASA aircraft and notified under Article 70 of Regulation (EU) No. 2018/1139; (2) Applied to non-EASA aircraft under the UK Air Navigation Order; (3) Maintenance or Operations related requirements applied under the UK Air Navigation Order or Commission Regulation (EU) No. 1321/2014 Annex I (Part M). CAP 747 Mandatory Requirements for Airworthiness Section 2 Contents Page 2 (2) DH 104 Riley Dove Series 1 and 2 (2) De Havilland DH114 Heron Series Aircraft (1) Dornier Do.28 Series Aircraft (2) Douglas DC-3 and Dakota (2) Jodel Series Aircraft (1) Learjet 35A/36A (1) Lockheed L–188 Series Aircraft (2) Luscombe Series Aircraft (2) Miles M14a Hawk Trainer III (Magister) (2) Miles M38 Messenger (2) Miles M65 Gemini (2) Percival Prentice (2) Percival Proctor and Vega Gull (2) Rollason Druine Condor (1) Scheibe Series Motor Gliders (2) All Scottish Aviation Bulldog Aircraft (2) Scottish Aviation Bulldog Series 100 and 120 Aircraft (2) Scottish Aviation Twin Pioneer (1) Sikorsky S61 Series Helicopters (2) Slingsby T61 (2) SNCAN Stampe et Renard and Aerospatiale Stampe SV4 Series Aircraft (2) Trago Mills SAH 1 Series Aircraft (2) Westland Bell 47 Series Helicopters Engines (2) Alvis Leonides Engines (2) Rolls Royce (Bristol Siddeley) Cheetah Engines (2) Rolls Royce (De Havilland) Cirrus Engines (2) Cirrus Minor II and IIA (2) Cirrus Major II and III (2) Cirrus Engine Inspections (2) Rolls Royce Continental Engines (2) Rolls Royce Gem Series Engines (2) Rolls Royce (De Havilland) Gipsy Engines Gipsy Major 1 (All Series) and Major 10 Mark 1 Gipsy Queen 30 Series Gipsy Queen 70 Series Gipsy Engine Inspections (2) Rolls Royce Gnome Engines (2) Rolls Royce Tyne Engines (2) Rolls Royce Viper Engines 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 2 Contents Page 3 Propellers (2) British Aerospace Dynamics Group Britannia Propellers and Equipment Heron Hydromatic Propellers and Equipment Pembroke, Prince and President Propellers and Equipment Pioneer (Twin and Single) Propellers and Equipment Vanguard Propeller and Equipment CL44 Propeller and Equipment (2) Dowty Aerospace Propellers (2) Fairey Reed Fixed Pitch Metal Propellers (2) Permali Group – Horden Richmond Wooden Fixed Pitch Propellers Equipment (2) Cameron Balloons Ltd – Fuel Cylinders with CB-0824-0001 Liquid Valve Fitted (2) Kidde Graviner Ltd – Automatic Fire Extinguishers (2) Lindstrand Hot Air Balloons – Replacement of Defective Fuel Hoses (2) Mann Aviation Group (Engineering) Ltd – Camera System Installation (2) Installation of Helicopter Health and Usage Monitoring Systems (2) RAF Radio Equipment Part 2 Requirements applicable to State/public service aircraft (1) MD 900 (902 configuration) Part 3 Generic Requirements GR No. 4 Electrical Generation Systems – Aircraft Not Exceeding 5,700 kg Maximum Authorised Weight GR No. 6 Electrical Generation Systems – Bus-Bar Low Voltage Warning Single-Engined Aircraft With a UK Certificate of Airworthiness GR No. 8 Cotton, Linen and Synthetic Fabric-Covered Aircraft GR No. 9 Helicopter Emergency Escape Facilities GR No. 10 Painting of Aircraft GR No. 11 Maintenance of Cockpit and Cabin Combustion Heaters and their associated Exhaust Systems GR No. 15 Light Aircraft Maintenance Schedule (Non-EASA Aircraft – Annex I) GR No. 16 Tyre Bursts In Flight – Inflation Media GR No. 17 Maintenance Requirements for Variable Pitch Propellers Installed on Aircraft Holding a UK Certificate of Airworthiness GR No. 18 Electrical Power Supplies for Aircraft Radio Systems GR No. 19 Emergency Power Supply for Electrically Operated Gyroscopic Bank and Pitch Indicators (Artificial Horizons) 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 2 Contents Page 4 GR No. 23 Personnel Certification for Non-Destructive Testing of Aircraft, Engines, Components and Materials GR No. 24 Light Aircraft Piston Engine Overhaul Periods GR No. 25 Aerobatic Smoke Systems Part 4 Generic Concessions (GCs) GC No. 1 Airworthiness Concessions in Respect of Foreign Built Aircraft GC No. 6 Flight in UK Air Space of Foreign Registered Home-Built Aircraft GC No. 7 Use of Unleaded Aviation Gasoline (Avgas) UL 91 in Annex I Aircraft 24 March 2020 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, AESL, Page 1 Part 1 Airworthiness Directives and Mandatory Information Issued by the CAA Aircraft (2) AESL, Glos Air Airtourer and Victa Airtourer Series and Airtourers Modified to AESL-T3 Standard 1 CAA Additional Airworthiness Directives 1.1 002–08–2001 Description Inspection of tailplane support brackets for corrosion. Applicability – Compliance – Requirement Applicable to AESL Airtourer T3 aircraft, Victa Airtourer 100 and 115 aircraft and Glos- Airtourer 115, 150 and Super 150 aircraft. Compliance is initially required not later than 10 flying hours or three months whichever is the sooner from the effective date of this Directive which is 24 August 2001. Clean and visually inspect the left and right tailplane support brackets for corrosion. Any corrosion detected must be removed and the area re-protected, in accordance with the AESL Airtourer 100, 115, 150, super 150 and T6 Maintenance and Repair Manual dated June 1970 chapter 50 ‘Repair Manual – General Repair Procedures’, before further flight. If corrosion is blended out the depth must be recorded in the aircraft log book. Brackets with corrosion which exceeds the limits stated in chapter 50 paragraph 2 (c) of the Maintenance and Repair Manual, must be replaced with Part Nos. 20031/1 or 20031/2 or an alternative approved part. Repeat inspection of the tailplane support brackets must be carried out at intervals not exceeding 12 months. 1.2 020–03–81 Description Inspection of upper and lower cut outs on control column torque tube assembly. Applicability – Compliance – Requirement Applicable to all Victa, Glos Air and AESL Airtourers. Inspect in accordance with Glos Air Service Bulletin No. 15 within 25 flight hours from 30 April 1981. Repeat Inspection at intervals of 100 flight hours or 1 year whichever is the soonest. 30 November 2009 INTENTIONALLY LEFT BLANK CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, ARV, Page 1 (2) ARV Aviation ARV 1 Super 2 Aircraft UK National Airworthiness Directives previously published in CAP 476 – Mandatory Aircraft Modifications and Inspections Summary CAA AD No: 010–08–86 Associated Material: Maintenance Manual Description: Mandatory Fatigue Lives Applicability – Compliance – Requirement The fatigue lives listed in Chapter 4 of the Maintenance Manual are mandatory for aircraft on the United Kingdom Register. CAA AD No: 025-05-87 Associated Material: ARV-SB-002 Description: Hewland AE75C Aero Engine – Loctiting carburetor bellmouth screws and wirelocking carburetor heat box retaining screws Applicability – Compliance – Requirement Applicable to aircraft as detailed in Service Bulletin. Compliance required as detailed in Service Bulletin. CAA AD No: 001-11-87 Associated Material: ARV-SB-008 Description: Hewland AE75C Engine – Propeller shaft Applicability – Compliance – Requirement Applicable to all aircraft fitted with Hewland AE75C engine gearboxes. Compliance required as detailed in Service Bulletin. CAA AD No: 015-11-87 Associated Material: ARV-SB-007 Description: Damage to rudder pedals Applicability – Compliance – Requirement Applicable to aircraft up to and including Constructors No 024. Compliance required as detailed in Service Bulletin. CAA AD No: 007-03-89 Associated Material: ARV-SB-012 Description: Cracks under the bearing sleeve on noseleg downtube Applicability – Compliance – Requirement Applicable to aircraft Constructors Nos. 001, 004K, 005K, 006K, 007K, 009K, 011, 012, 013, 017, 019 and 021. Compliance required as detailed in Service Bulletin. 30 November 2009 INTENTIONALLY LEFT BLANK CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Auster, Page 1 (2) Auster 3, 4 and 5 Variants ‘J’ and ‘D’ Series and Taylorcraft Plus ‘C’ and ‘D’ Aircraft UK National Airworthiness Directives previously published in CAP 476 – Mandatory Aircraft Modifications and Inspections Summary CAA AD No: 2463 PRE 80 Associated Material: Mod No. 135 Description: To introduce strengthened flap shaft levers and flap torque tube levers. Applicability – Compliance – Requirement Applicable to Marks 4, 5, 5C and 5D aircraft. CAA AD No: 2464 PRE 80 Associated Material: Mod No. 142 Description: To change the specification of rear undercarriage and lift strut fittings from 3S3 to DTD-124A. Applicability – Compliance – Requirement Applicable to the first sixty-one Mark 3 aircraft only. Constructors Nos. 233–248 inclusive, 251– 264 inclusive and 266–296 inclusive. CAA AD No: 2465 PRE 80 Associated Material: Mod No. 144 Description: Introduction of 5/8” diameter rudder mass balance arm. Applicability – Compliance – Requirement Applicable to Marks 3, 4, 5, 5C and Taylorcraft Plus Model ‘C’ and ‘D’ only. Mod. 159 (Introduction of rudder mass balance weight to Part No. J4252) is an alternative to this modification. CAA AD No: 2466 PRE 80 Associated Material: Mod No. 154 Description: Introduction of wing fabric DTD 575, using specially woven tape of greater strength with 3” pitch stringing. Applicability – Compliance – Requirement Applicable to Marks 3, 4, 5, 5C, 5D and Taylorcraft Plus Model ‘C’ and ‘D’ mainplanes only. Mod. 138 (Strengthened fabric attachments) and Mod. 167 (Fabric to DTD 540, superseded by BS 7F1) are alternatives. On all other variants, the modification is incorporated into the build standard, but if mainplanes and/or ailerons are to be re-covered, Mod 154 must be embodied in accordance with the relevant fabric covering drawings. (Use of DTD 540 fabric, now superseded by BS 7F1 is an alternative fabric to DTD 575). Beagle Service Bulletin No. 53 (Auster Series) and R F Saywell Ltd. Service Bulletin RFS/73/2 refer. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Auster, Page 2 CAA AD No: 2467 PRE 80 Associated Material: Mod No. 164 Description: Introduction of redesigned engine mounting to Drawings Nos. DFF 18 Mark 3 and DFF 19 Mark 3. Applicability – Compliance – Requirement Applicable to Marks 4 and 5. Mod. 118 (Mountings to Drawings Nos. DFF 18 and 19 Mark 2) is an alternative to this modification. CAA AD No: 2468 PRE 80 Associated Material: Mod No. 1381 Description: Introduction of redesigned engine mounting to Drawings Nos. DFF 18 Mark 3 and DFF 19 Mark 3. Applicability – Compliance – Requirement Applicable to Marks 4 and 5. Mod. 118 (Mountings to Drawings Nos. DFF 18 and 19 Mark 2) is an alternative to this modification. CAA AD No: 2469 PRE 80 Associated Material: Mod No. 1670 Description: To introduce improved engine mounting to Drawing No. EJF 106 Issue ‘K’ by addition of wrapper plate at rear bearer foot attachment. Applicability – Compliance – Requirement Applicable to Mark 5J1 CAA AD No: 2470 PRE 80 Associated Material: Mod No. 1838 Description: Introduction of starter isolation switch. Applicability – Compliance – Requirement Applicable to all Auster aircraft with electric starter motors. CAA AD No: 2471 PRE 80 Associated Material: Mod No. 2555 Description: To introduce safety tube in tailplane attachment tube. Applicability – Compliance – Requirement CAA AD No: 2472 PRE 80 Associated Material: Mod No. 2601 Description: To introduce throttle lever in mild steel. Applicability – Compliance – Requirement Applicable to Marks J5F, J5G and J5H. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Auster, Page 3 CAA AD No: 2473 PRE 80 Associated Material: Mod No. 2737 Description: To introduce cap nut at engine fuel pipe banjo connection to facilitate locking. Applicability – Compliance – Requirement Applicable to all Auster 5J2 aircraft and to Auster Mark 4 and 5 fitted with Pesco type Vacuum Pumps and Electric Starters. Auster Service Bulletin Issue No. 36 refers. CAA AD No: 2474 PRE 80 Associated Material: Mod Nos. 2898, 2899 and 2902 Description: Introduction of flexible mounted whip aerial. Applicability – Compliance – Requirement Only applicable to aircraft cleared for flight in icing conditions. CAA AD No: 2475 PRE 80 Associated Material: Mod No. 3234 Description: Introduction of retaining pin for forward tailplane attachment safety tube. Applicability – Compliance – Requirement Auster Service Bulletin No. 41 refers. CAA AD No: 2476 PRE 80 Associated Material: Mod No. 3285 Description: Radius on trimmer guide tubes. Applicability – Compliance – Requirement Applicable to Auster types 5J1, 5J1B, J1N, 5J2, 5J4, 5J5, J5B and J5P. Not applicable to aircraft fitted with belled mouth guide tubes at elevator trailing edge. Auster Service Bulletin No. 41 refers. CAA AD No: 2477 PRE 80 Associated Material: Mod No. 3663 Description: Strengthened Actuator Lever Assemblies on Flap Control Torque Shaft. Applicability – Compliance – Requirement Should have been embodied by 1 April 1961. Applicable to Auster types Mark 4, 5, 5C, 5D, 5J1, 5J1B, J1N, J1U, 5J5, J5F, J5K, J5L, J5B, J5G, J5H, J5P, J5Q, J5R, J5V. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Auster, Page 4 CAA AD No: 2478 PRE 80 Associated Material: Mod No. 4069 Description: Introduction of additional stringing. Applicability – Compliance – Requirement Applicable to Model C, Model D, Mark 3, 4, 5, 5C, 5D, 5J1, 5J1B, J1N, J1S, J1U, J2, J4, J5, J5B, J5F, J5G, J5H, J5K, J5L, J5P, J5Q, J5R, J5V, J8L, D4, D5, D6. This modification is applicable to all mainplanes of aircraft of the above types in which incorrect taping and/or stringing materials have been used during the last recovering of the components. NOTE: This modification is an acceptable alternative to Auster Mod. 138 referred to in connection with Mod. 154. Beagle Service Bulletin No. 53 (Auster Series) and RF Saywells Ltd. Service Bulletin RFS/73/2 refer. CAA AD No: 2479 PRE 80 Associated Material: Mod No. 4073 Description: Introduction of Cockpit Placard and Loading Chart. Applicability – Compliance – Requirement Applicable to mark 4, 5, 5C, 5D, J1, J1B, J1N, J1S, J1U, J5, J5B, J5F, J5G, J5H, J5K, J5L, J5P, J5Q, J5R, J5V, D5, D6. Beagle Service Bulletin No. 52 (Auster Series) refers. CAA AD No: 2480 PRE 80 Associated Material: Mod No. 4179 Description: Replacement of toxic type fire extinguishers. Applicability – Compliance – Requirement Applicable to Model ‘D’ Mark 3, J1, J1N, J2, J4, D6/160, D6/180 and 6A. Should have been embodied by 30 September 1965. CAA AD No: 2481 PRE 80 Associated Material: Mod No. A182 Description: Fuel and Oil Vent Restriction for AC lightweight diaphragm Fuel Pumps. Applicability – Compliance – Requirement Applicable to D5/160, D5/180, D6/160, D6/180, J1U and J5V. Compliance required by 1 September 1964. Beagle Service Bulletin (Auster Series) No. 55 refers. CAA AD No: 2482 PRE 80 Associated Material: SB 32 Description: Inspection of the tailplane front attachments. Applicability – Compliance – Requirement Applicable to all variants except Taylorcraft Plus C and Auster J1U. Inspect for signs of fracture of the leading edge tube in the vicinity of the saddle washers at periods not exceeding 300 flight hours. NOTE: This inspection is not necessary if the saddle washers are welded to the tube (instead of brazed) or if the aircraft has Modifications No. 3252 or 3413 embodied. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Auster, Page 5 CAA AD No: 2483 PRE 80 Associated Material: SB 30 Description: Inspection of the tailplane attachment stubs. Applicability – Compliance – Requirement Applicable to all variants except Taylorcraft Plus C and Auster J1U. Inspect for signs of failure at periods not exceeding 100 flight hours (Auster J5F, J5L and J8L Aiglet Trainers) or 300 flight hours (Taylorcraft Plus D and all other variants other than J5F, J5L and J8L). This inspection need not be carried out if Modifications No. 3252 or 3413 together with 2555 and 3234 are embodied. CAA AD No: 2484 PRE 80 Associated Material: - Description: Life limitation of rudder control cables. Applicability – Compliance – Requirement Rudder cables Part Nos. JA 2393X and JA 2394X when installed over small (13/4”) diameter pulleys at the change of direction some 12” rearward from the rudder bar must be renewed at periods not exceeding 200 flight hours. In all other cases cables Part Nos. JA 2393X and JA 2394X may remain in service up to a maximum of 1200 flight hours. NOTE: Reference should be made to Auster Service Bulletin No. 50. The inspections of rudder cables detailed in this bulletin are mandatory. CAA AD No: 2485 PRE 80 Revision 1 Associated Material: Beagle SB 54 Description: Inspection of the engine mounting attachment bolts. Applicability – Compliance – Requirement Applicable to Models as detailed in Service Bulletin. Compliance is required at intervals not exceeding 1000 flight hours. Inspect the engine mounting attachment bolts in accordance with the Service Bulletin. NOTE: This AD revision removes the 5 year repeat requirement of the Service Bulletin. CAA AD No: 2486 PRE 80 Associated Material: HS/Auster SB 1 Description: Propeller operating restriction placard. Applicability – Compliance – Requirement Applicable to aircraft fitted with Propeller Models 2D36C14–X/78KM, 2D34C53–X/74E and B2D34C53–X/7. Compliance required as detailed in Service Bulletin. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Auster, Page 6 CAA AD No: 2487 PRE 80 Associated Material: - Description: Rear seat loading limitations amendment. Applicability – Compliance – Requirement Applicable to Auster Models Mk4, Mk5, Mk5C, Mk5D, J1, J1B, J1N, J1S, J5, J5B, J5F, J5G, J5H, J5K, J5L, J5P, J5Q, J5R, J5V, D5 and D6 which are fitted with a forward fuselage fuel tank. Compliance is required prior to the next flight on which it is intended to carry passengers on the rear bench seat, but in any case not later than 30 September 1976. Amend the loading limitation chart which is displayed in a plastic holder on the rear cabin bulkhead, as follows: (1) Draw a line, parallel to the base line of the chart, from the rear seat load at zero fuel, i.e. the intersection of the loading limitation line with the left-hand vertical axis of the chart, and continue this horizontal line to intersect with the right-hand slope of the loading limitation line. (2) Erase all that part of the original loading limitation line, which lies above the new line (drawn in accordance with 1). NOTE: The following sketch illustrates an amended loading chart. If the existing loading chart should differ significantly from this illustration, advice must be obtained from the CAA prior to amendment. This Directive hereby authorises the Operator to make an entry in the aircraft Log Book, quoting the AD number, and this entry must be made when the loading chart has been amended in accordance with these instructions. NOTE: This requirement was previously issued under CAA Letter Reference 9/92/LTO/1 dated 16 August 1976. CAA AD No: 015–11–80 Associated Material: R F Saywell SB RFS/AUS/3 Description: Inspection of Bendix brake back plates. Applicability – Compliance – Requirement Applicable to all aircraft fitted with Bendix mechanical brakes. INSPECT in accordance with Service Bulletin at next 50 hour inspection and thereafter at each 100 flight hour or Annual Inspection whichever is the sooner. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Auster, Page 7 (2) Auster 6A and Beagle A.61 Series Aircraft UK National Airworthiness Directives previously published in CAP 476 – Mandatory Aircraft Modifications and Inspections Summary CAA AD No: 2488 PRE 80 Associated Material: - Description: Inspection of the tailplane front attachments. Applicability – Compliance – Requirement Inspect for signs of fracture of the leading edge tube in the vicinity of the saddle washers at periods not exceeding 300 flight hours. NOTE: This inspection is not necessary if the saddle washers are welded to the tube (instead of brazed) or if the aircraft has Modification No. 3252 or 3413 embodied. CAA AD No: 2489 PRE 80 Associated Material: - Description: Inspection of the tailplane attachment stubs. Applicability – Compliance – Requirement Inspect for signs of failure at periods not exceeding 300 flight hours. This inspection need not be carried out if Modification No. 3252 or 3413 together with 2555 and 3234 are embodied. CAA AD No: 2490 PRE 80 Associated Material: - Description: Life limitation of rudder control cables. Applicability – Compliance – Requirement Rudder cables Part Nos. JA 2393X and JA 2394X when installed over small (13/4”) diameter pulleys at the change of direction some 12” rearward from the rudder bar must be renewed at periods not exceeding 200 flight hours. In all other cases cables Part No. JA 2393X and JA 2349X may remain in service up to a maximum of 1200 flight hours. NOTE: Reference should be made to Auster Service Bulletin No. 50. The inspection of rudder cables detailed in this bulletin are mandatory. CAA AD No: 2491 PRE 80 Revision 1 Associated Material: Beagle SB Nos. A9 and 54 Description: Inspection of the engine mounting attachment bolts. Applicability – Compliance – Requirement Applicable to Auster 6A and Beagle A.61 Series 1 and Revision 1 Nos. A9 and 54 attachment bolts. 2 aircraft. Compliance is required at intervals not exceeding 1000 flight hours. Inspect the engine mounting attachment bolts in accordance with the Service Bulletins. NOTE: This AD revision removes the 5 year repeat requirement of the Service Bulletins. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Auster, Page 8 CAA AD No: 2492 PRE 80 Associated Material: Beagle SB Nos. A14 and 58 Description: Replacement of toxic type fire extinguishers. Applicability – Compliance – Requirement Applicable to models as detailed in Service Bulletin. Should have been complied with by 30 September 1965. CAA AD No: 015–11–80 Associated Material: R F Saywell Ltd SB No. RFS/AUS/3 Description: Inspection of Bendix brake back plates. Applicability – Compliance – Requirement Applicable to all aircraft fitted with Bendix mechanical brakes. INSPECT in accordance with Service Bulletin at next 50 hour inspection and thereafter at each 100 flight hour or Annual Inspection whichever is the sooner. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Av. Traders, Page 1 (2) Aviation Traders ATL98 Carvair UK National Airworthiness Directives previously published in CAP 476 – Mandatory Aircraft Modifications and Inspections Summary CAA AD No: 2603 PRE 80 Associated Material: CSB/1 Description: Inspection of emergency air brake valve. Applicability – Compliance – Requirement Applicable to all aircraft. Compliance required as detailed in Carvair Service Bulletin. CAA AD No: 2604 PRE 80 Associated Material: CSB/2 Description: Inspection of nose door upper pivot support structure. Applicability – Compliance – Requirement Applicable to aircraft S/N 10528/ATL 98/1, 10311/ATL 98/2, 18339/ATL 98/3, 10338/ATL 98/4, 10365/ATL 98/5, 7480/ATL 98/6, 10273/ATL 98/7. Compliance required at each Check 1 inspection until embodiment of Modification No. 98/5104. CAA AD No: 2605 PRE 80 Associated Material: CSB/10 Description: Inspection of Bendix (Eclipse Pioneer) type 9054 fuel flow transmitters. Applicability – Compliance – Requirement Applicable to all aircraft. Compliance required at next Check 1 as referred to in Carvair Service Bulletin. CAA AD No: 2606 PRE 80 Associated Material: CSB/13 Description: Strengthening of upper boom – Fin spar frame (Station X953). Applicability – Compliance – Requirement Applicable to aircraft detailed in Carvair Service Bulletin. Should have been embodied by 29 February 1964, Carvair Modification No. 98/5155 refers. CAA AD No: 2607 PRE 80 Associated Material: CSB/20 Description: Operation of emergency brake system controls. Applicability – Compliance – Requirement Applicable to all aircraft. Compliance required as detailed in Carvair Service Bulletin. Modification 98/5258 refers. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Av. Traders, Page 2 CAA AD No: 2608 PRE 80 Associated Material: CSB/22 Description: Flying Controls – Replacement of bolt attaching aileron operating rod assembly to bell crank at wing station 485. Applicability – Compliance – Requirement Applicable to all aircraft. Compliance required as detailed in Carvair Service Bulletin. Modification 98/5301 refers. CAA AD No: 2609 PRE 80 Associated Material: CSB/24 Description: Inspection of fin rear stub spar boom and fin rear shear saddle. Applicability – Compliance – Requirement Compliance required by 7 March 1974 and then at intervals of one year. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Avro, Page 1 (2) Avro Anson and Avro 19 UK National Airworthiness Directives previously published in CAP 476 – Mandatory Aircraft Modifications and Inspections Summary CAA AD No: 1496 PRE 80 Associated Material: 108 Description: Tailplane wire bracing. Applicability – Compliance – Requirement Applicable to Anson Mark 1 only, with wooden tailplane. CAA AD No: 1497 PRE 80 Associated Material: 121 Description: Guard for rudder bar torque tubes. Applicability – Compliance – Requirement To prevent loose items falling into the spur gears and locking the rudder control. Applicable to Anson Mark 1 only. CAA AD No: 1498 PRE 80 Associated Material: 122 Description: Introduction of petrol trap in boost gauge lines. Applicability – Compliance – Requirement To prevent boost gauges being damaged by petrol. Applicable to Anson Mark 1 only. CAA AD No: 1499 PRE 80 Associated Material: 173 Description: Strengthening of aileron hinge. Applicability – Compliance – Requirement This changes the end hinge from steel to brass. Applicable to Anson Mark 1 only. CAA AD No: 1500 PRE 80 Associated Material: 265 Description: Pilot’s Emergency Exit. Applicability – Compliance – Requirement To improve the ‘rip-off’ strip method of operating exits. Applicable to Anson Mark 1 only. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Avro, Page 2 CAA AD No: 1501 PRE 80 Associated Material: 289 Description: Combined filter and non-return valve in flap hydraulic circuit. Applicability – Compliance – Requirement Introduced to prevent dirt reaching the pump relief valve. Applicable to hand operated flaps only on Anson Marks 1, 10 and 11. CAA AD No: 1502 PRE 80 Associated Material: 308 Description: To reposition oil tank cock and thermometer pocket. Applicability – Compliance – Requirement Introduce brackets to support oil cock and thermometer pocket. Applicable to Anson Mark 1 only. CAA AD No: 1503 PRE 80 Associated Material: 654 Description: Strengthened tailwheel rocker beam. Applicability – Compliance – Requirement Mandatory only for aircraft with AUW of 9540 lb. Applicable to Anson Marks 1, 10 and 11. CAA AD No: 1504 PRE 80 Associated Material: 661 Description: Strengthened wing (retrospective). Applicability – Compliance – Requirement Introduces strengthened underside wing panels between spars (diagonal plywood). To be introduced in conjunction with Mod. No. 695. Applicable where Mod. No. 657 is not embodied. See Note 2. Applicable to Anson Marks 1, 10 and 11. CAA AD No: 1505 PRE 80 Associated Material: 669 Description: To introduce engine fire warning. Applicability – Compliance – Requirement To be embodied in conjunction with Mod No. 844. Switches to Mod No. 855 are an approved alternative to those of Mod No. 669. Applicable to Avro 19 Series I and II. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Avro, Page 3 CAA AD No: 1506 PRE 80 Associated Material: 687 Description: To introduce strengthened wheels, tyres and brakes. Applicability – Compliance – Requirement Applicable to Avro 19 Series I with wooden wing. Embody in conjunction with Mod. No. 637 Heywood compressor. CAA AD No: 1507 PRE 80 Associated Material: 695 Description: To strengthen the glued joints of mainplane spars. Applicability – Compliance – Requirement Introduces woodscrews in joints of plywood webs to top and bottom booms. To be embodied in conjunction with Mod. No. 661 when Mod. No. 657 is not incorporated. See Notes 1 and 2. Applicable to Anson Marks 1, 10 and 11. CAA AD No: 1508 PRE 80 Associated Material: 709 Description: To strengthen rear seat attachment between spars. Applicability – Compliance – Requirement Applicable to wooden wing aircraft only. Introduces internal block and stiffeners in floor between spars. Applicable to Anson Mark 11 and Avro 19 Series I. CAA AD No: 1509 PRE 80 Associated Material: 716 Description: General Improvements to drainage. Applicability – Compliance – Requirement Applicable to Anson Marks 1, 10 and 11 and Avro 19 Series 1 and II. CAA AD No: 1510 PRE 80 Associated Material: 725 Description: To lower accumulators charging pressure from 200 lb/in2 to 165–170 lb/ in2. Applicability – Compliance – Requirement Mandatory to aircraft embodying Mod. No. 682 (direct flap linkage). Applicable to Avro 19 Series I only. 30 November 2009 CAP 747 Mandatory Requirements for Airworthiness Section 2 Part 1, Avro, Page 4 CAA AD No: 1511 PRE 80 Associated Material: 732 Description: Improvements to passenger seat locking. Applicability – Compliance – Requirement Applicable to all seats having spring loaded vertical locking plungers. Applicable to Anson Marks 1, 10 and 11. CAA AD No: 1512 PRE 80 Associated Material: 744 Description: To change position of ‘Press to Speak’ switch. Applicability – Compliance – Requirement Changed from right to left. Applicable to Anson Mark 11 and Avro 19 Series I and II. CAA AD No: 1513 PRE 80 Associated Material: 750 Description: To introduce wire locking of AGS couplings. Applicability – Compliance – Requirement Applicable to Anson Marks 1, 10, 11 and Avro 19 Series I and II CAA AD No: 1514 PRE 80 Associated Material: 759 Description: To introduce strengthened oil cooler support clip. Applicability – Compliance – Requirement To be embodied