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  • New LAA Inspector - Tom Bootyman | Light Aircraft Assoc

    < Back New LAA Inspector - Tom Bootyman 20 Jun 2024 We are pleased to welcome Tom Bootyman as an LAA Inspector. Tom attended an Assessment Day at LAA HQ at the start of June. Tom is a serial aircraft builder/maintainer/repairer, also with several years’ experience as an engineer with a global aerobatic team. He has experience building and repairing Zenair and Vans RV types, along with working on many aerobatic aircraft. He is also an experienced aircraft painter. Tom has a love and devotion to all things aviation, so he is always open to requests for information, advice and Permit inspections. He is based at Netherthorpe (Sheffield), but willing to travel. Next Previous

  • MTD-04-2025 upissued to Issue 2 - Rans Control Linkage Rod End Connector Safety Washers | Light Aircraft Assoc

    < Back MTD-04-2025 upissued to Issue 2 - Rans Control Linkage Rod End Connector Safety Washers 18 Nov 2025 MTD-04-2025 Issue 2 - Rans Control Linkage Rod End Connector Safety Washers MTD-04-2025 Issue 1 was recently published to mandate the replacement of all plastic control linkage rod end connector washers with metal washers . It has become apparent that the washers specified in this MTD are not suitable to replace the plastic washers due to their dimensions. MTD-04-2025 Issue 2 has been raised in order to amend the specification of the metal washers that must used to replace plastic washers. Therefore, MTD-04-2025 Issue 2 supersedes Issue 1. Issue 1 of this MTD is now cancelled. Please refer to the attached MTD document for full details and compliance instructions, which can also be found on the LAA website HERE . MTD-04-2025 - Rans Rod End Washers - Issue 2 .pdf Download PDF • 293KB Next Previous

  • LAA Alert for some models of Rotax Engines | Light Aircraft Assoc

    < Back LAA Alert for some models of Rotax Engines 1 Mar 2025 LAA Alert A-02-2025 has been published on the LAA website (and is also attached), highlighting a recent service bulletin published by Rotax regarding the inspection and/or replacement of the crankcase and/or gearbox housing on affected engines. Rotax has identified a potential manufacturing issue affecting the hardness values of the crankcase and/or gearbox housing materials in certain engines. These components may not meet the required specifications for material hardness, which could lead to reduced component durability and/or potential oil leakage. Rotax regards this bulletin as mandatory. A-02-2025 - Rotax Crankcase .pdf Download PDF • 220KB Next Previous

  • Mandatory Technical Directive issued for Eurofox aircraft | Light Aircraft Assoc

    < Back Mandatory Technical Directive issued for Eurofox aircraft 6 Dec 2024 Inspection of Trim Tab Operating Cable Attachment to Prevent In-Flight Failures and replacement with Improved Design of Cable Attachment In 2016, the LAA issued an Alert, LAA/AWA/16/08 , regarding reported problems with the thin stranded steel elevator trim cable on Eurofox aircraft fraying at the attachment point to the trim tab operating horn, where the design forced the cable to be bent around the sharp edges of the clevis. The 2016 Alert also provided a link to, and served to promulgate, the Eurofox UK Service Bulletin on the subject, SB 04/2016 . Recently we’ve been advised of a potentially serious incident of elevator flutter on a Eurofox while towing a glider, which was caused by the trim cable failing altogether in flight where it passes around the trim tab operating horn clevis. This resulted in violent shaking of the elevator with serious potential for structural damage or loss of control. Since the cable had evidently frayed considerably before failing altogether, this occurrence highlights the importance inspecting the trim cable for signs of fraying at this point at each pre-flight and maintenance check, and, as the service bulletin explains, of keeping the clevis free-moving about its attachment to the tab so the clevis remains in line with the cable as the tab moves. This minimises the relative movement between the two which if occurring, would accelerate the wear on the cable. Eurofox UK advises that since the issue of the 2016 Service Bulletin, they have revised the design of the cable attachment clevis so that the cable now passes around a circular bush rather than being forced into two sharp bends, which reduces the wear on the cable and tendency to fray and eventually break. MTD-07-2024 , issued today, requires Owners/Operators to check whether the old or new design of clevises are fitted and for any signs of trim cable fraying before further flight. Owners/Operators must obtain and use a copy of the up-issued AEROPRO Checklist - B Service/Maintenance plan (Update Nov 2024 LAA aircraft) before the next 50-hour check. Finally, the trim cable system must be replaced immediately if any trim cable fraying is found, as detailed in the MTD. Furthermore, all Eurofoxes with the old-style of clevis must have the trim cable system replaced, as described in the MTD, by 1st June 2025. MTD-07-2024 Eurofox Trim Cable .pdf Download PDF • 495KB Next Previous

  • Air to Ground Radio Operator's Course | Light Aircraft Assoc

    Air to Ground Radio Operator's Course Price Member - £310, Non-Member - £330 (Additional fee of £48 to CAA for ROCC certificate) Duration Day 1: 09:15 for 09:30 PROMPT start. Finish 17:00 (approx). Day 2: 08:30 PROMPT start. Finish 16:00 < Back About the Course This course, held at Popham Airfield is hosted by Chris Thompson, an experienced 'AirGround' person, CAA examiner and LAA member. It will provide both the theoretical and practical training required to sit the examinations for the CAA Radio Operator's Certificate of Competence (ROCC) qualification required by operators of ground-based radio equipment at flying sites and events where an air-to-ground radio service is provided. The course is in two parts. Day One is made up of the core training and radio procedures practice on simulated ground-to-air communications. Day Two will consist of the CAA written and practical examinations which will allow candidates to directly apply for the CAA ROCC Certificate. Landing fees will be waivered for those attending the course and flying in. All delegates MUST have some basic knowledge of GA airfield circuit procedures and a level 6 English language proficiency * PLEASE READ THE DOCUMENT BELOW VERY CAREFULLY BEFORE ATTENDING THE COURSE. Course description 2025 .pdf Download PDF • 41KB Your Instructor Chris Thompson Dates 17 & 18 January 2026 AND 7 & 8 March 2026 Times Day 1: 09:15 for 09:30 PROMPT start. Finish 17:00 (approx). Day 2: 08:30 PROMPT start. Finish 16:00 Duration Two day course Venue Popham Airfield Price Member - £310, Non-Member - £330 (Additional fee of £48 to CAA for ROCC certificate) Booking Pls call the LAA on 01280 846 786 to enquire/book or email [email protected] . *Please note that payment is required when booking, to confirm your place. NO place will be held without confirmed payment* **Please note that your booking payment is non-refundable unless we can fill your place timeously or there are exceptional circumstances**

  • New LAA Inspector - Lewis Harper | Light Aircraft Assoc

    < Back New LAA Inspector - Lewis Harper 18 Aug 2025 We are pleased to welcome Lewis Harper as a new LAA Inspector, having attended an LAA Inspector Assessment Day at Turweston recently. Working full-time as a CAA and EASA Licensed Aircraft Engineer, Lewis has pursued his lifelong passion for aviation since entering the industry at age 16, and have also achieved his PPL along the way. Next Previous

  • Detail Design | Light Aircraft Assoc

    Detail Design Having worked out a promising-looking layout, initial three-view and performance and weight specifications, now is the stage where the hard work begins of transforming concepts to working drawings. Essential decisions have to be made about types of material to be used, the structural arrangement, exact choice of powerplant and so on. You’ll probably need to make a cockpit mock-up to check the ergonomics and control system arrangements, and maybe build a flying radio controlled model of the design to give faith in the handling characteristics. With the basic geometry laid out, stress calculations and assembly drawings come next, then drawings of individual piece parts. Keep an up-to-date tally on weights. As the drawings get more detailed you must re-evaluate whether you are going to meet your original targets in terms of weight, strength and aerodynamic cleanliness, whether you need to re-visit your original assumptions or re-design from scratch. Is there a way that the part or assembly can be made more easily, more cheaply, lighter, stronger, more fatigue or corrosion resistant? Fewer parts and fewer joints generally means fewer problems and less weight. Can you use off the shelf parts rather than having to make them specially? Are there other aeroplanes around that have already solved a particular problem in a clever way? Will the aircraft be easy to inspect in service, easy to repair if it gets damaged? Can it be broken down for transportation? If the handling isn’t quite right when the prototype is test flown, does the design make provision for ‘tweaks’ to put it right? Does the design include reserves of strength to cope with weight growth in service and more powerful engines, or is everything pared down to the minimum? Design Tutorials

  • Continuing Airworthiness Information | Light Aircraft Assoc

    Continuing Airworthiness Information One of the key strengths of the LAA's system is that we can monitor the fleet centrally and keep track of airworthiness incidents from around the world. Where necessary, we can then let our owners know, to help them keep flying safely. A full listing of Airworthiness Alerts, Technical Service Bulletins and Mandatory Technical Directives can be found below: ALERTS, TECHNICAL SERVICE BULLETINS & MANDATORY TECHNICAL DIRECTIVES

  • MTD-03-2025 - Marquart Charger Aileron Slave Strut | Light Aircraft Assoc

    < Back MTD-03-2025 - Marquart Charger Aileron Slave Strut 25 Jul 2025 LAA MTD-03-2025 - Marquart Charger Aileron Slave Strut The starboard aileron slave strut on Marquart Charger G-BHBT failed at the AN490 threaded fitting welded into the bottom end. A large proportion of the cross-section was cracked due to fatigue prior to final failure. The root cause of the fatigue cracking was probably flutter. Due to the difficulty of reliably inspecting for fatigue cracking at the base of threads, it has been decided to withdraw this strut design from the UK fleet. MTD-03-2025 can be found HERE and is found below. MTD-03-2025 - Marquart Charger Aileron Slave Strut .pdf Download PDF • 194KB Next Previous

  • New LAA Inspectors - Cameron Bunce & Brian Davies | Light Aircraft Assoc

    < Back New LAA Inspectors - Cameron Bunce & Brian Davies 11 Jan 2024 Back in December, seven potential LAA Inspectors attended LAA Inspector Assessment Days at Turweston with our Chief Inspector, Lucy. We are pleased to announce that all seven were successful. Here is an introduction to the first two: Cameron Bunce - Cameron is based north of Aberdeen. He is a Chartered Engineer working in the Energy Industry. He has been involved with aviation since 2007 and currently is building a VANS RV-3. He has experience with metal, composite and wooden aircraft having flown over 30 types - but most familiar with the VANS RV series. Brian Davies - Brian has experience in building and maintaining composite, metal and wood aircraft, but tends to specialise in Rotax-powered aircraft. He is also experienced in Avionic installation and trouble-shooting. Brian is also on the LAA Board of Directors and our Vice-President. Congratulations Cameron and Brian! Next Previous

  • Strut Governance Documents | Light Aircraft Assoc

    Strut Governance Documents Strut Governance Documents Electronic versions of the Strut Event Management Procedures can be found below. Click each document to access it online. Updated April 2019 Member Club Regulations The Member Club Regulations describe the manner in which an LAA Member Club should form, govern its affairs and conduct its activities. Strut Event Management Procedure Procedures for Strut events (fly-ins etc..) Annex A Normal and Prohibited Club Activities Annex B Summary Insurance Certificate for Member Clubs of the LAA Annex C LAA Member Club - Event Notification Annex D LAA Club Event Risk Assessment (air side/ground activities) Annex E Event Safety Review and Operations Summary Annex F Third Party Passenger Flying at LAA Member Club Events Annex G Incident Checklist / Incident Plan Appendix 1 TPPF Pilot and Aircraft Checklist Appendix 2 Indemnity Agreement Appendix 3 Information for those Attending an LAA Member Club Flying Event Model Club Constitution A model constitution for member clubs

  • New LAA Inspector - Malcolm Talbot | Light Aircraft Assoc

    < Back New LAA Inspector - Malcolm Talbot 14 Jul 2025 We are pleased to welcome Malcolm Talbot as a new LAA Inspector, having attended an LAA Inspector Assessment Day at Turweston recently. Malcolm holds a BSc(Hons) with the Open University in Maths, Technology and Engineering. He has held a PPL since 2010 and been a Flight Instructor FI since 2019, (having passed the CPL theory exams),. He is currently instructing for Moray Flying Club and Highland Aviation, and recently become a ground examiner. Malcolm built and flies a Eurofox, which first flew in 2013. He thoroughly enjoyed the build process. Next Previous

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