< Back Alert A-04-2025 - Jabiru Flywheel Bolts 12 Jun 2025 LAA Alert A-04-2025 - Jabiru Flywheel Bolts LAA Alert A-04-2025 has been published on the LAA website (and is also attached), highlighting the Installation Procedure, Torque Checks and Replacement Interval for Flywheel Attachment Bolts on aircraft equipped with Jabiru 2200, 3300 and 5100 engines, and withdrawal of LAA Alert AWA/20/15. With the advice in JSB-012 (Issue 9 onward) having been promulgated by Jabiru, LAA has withdrawn Alert AWA/20/15, which means that provided the advice in JSB-012 Issue 9 or subsequent is followed, along with regular bolt torque checks at every 100 hours and annual check as called for in the Engine Maintenance Manual, the recommended bolt life is as stated in the Engine Maintenance Manual (currently 500 hrs). For LAA aircraft having the flywheel bolts replaced, or torque checked, the work must be overseen and signed-for by a suitably approved LAA Inspector. Engine logbook entries must be made and certified with a PMR statement referencing JSB-012 in the logbook white pages, as well as an entry in the logbook pink pages (or equivalent method for tracking continued airworthiness compliance). A-04-2025 - Jabiru Flywheel Bolts .pdf Download PDF • 202KB Next Previous

< Back New LAA Inspector - Mark Wilkinson 15 Aug 2025 We are pleased to welcome Mark Wilkinson as a new LAA Inspector, having attended an LAA Inspector Assessment Day at Turweston recently. Mark’s aviation career began with 11 years of service in the Royal Air Force, where he initially worked on the Bulldog and Chipmunk aircraft before progressing to the Tornado. Following his military service, Mark spent 25 years in commercial aviation, working primarily on large passenger aircraft - focusing on turboprops and regional jets. This period included a three-year relocation to France, where he was responsible for supporting a BAE146 aircraft. Mark then dedicated eight years to the initial setup and maintenance of the A400M program, before taking on a role maintaining the Grob Tutor aircraft - bringing his career full circle back to light aviation. From his early days working on the Bulldog, he has always had a genuine passion for light aviation. Mark would welcome the opportunity to contribute to the light aviation community, offering support and advice wherever he can. Next Previous

LAA Clubs & Struts FIND MY LOCAL CLUB/STRUT Local Clubs, or Struts, as many of them are called, look forward to welcoming you along as a friend and fellow LAA member. They are an excellent source of advice and help, whether building, buying, training or simply wanting to be involved in the local aviation scene. The Clubs and Struts also arrange a number of flying and social events throughout the year, and most hold monthly meetings. LAA TYPE CL UBS You can also find details of LAA-Type clubs by clicking the icon below. These clubs are associated to the LAA and are dedicated to a specific aircraft manufacturer or model. They can offer social activities and technical support for owners or those interested in a particular type.

Find a Coach All Coaches are CAA qualified Instructors and CAA 'R' Examiners. They are all highly experienced and generally able to do licence revalidations, differences training, refresher courses and any specialised training. This would be dependent on their own experience of any aircraft type on which training was requested, so please check with the Coach nearest to your location as to their availability to carry out your request. The map below can be increased in size and moved, as required. The icons represent the postal location of the Coach. Clicking on any icon will display a photo, a contact number, a preferred location or home airfield, and a short profile of the Coach you will be looking at. Most Coaches are happy to travel reasonable distances to accommodate your needs.

< Back Mandatory Technical Directive issued for many Zenair types 14 Jan 2025 MTD-01-2025 - 'Inspection of horizontal stabiliser (tailplane) attachment brackets and associated hardware for cracks, looseness and other forms of distress' is issued for Zenair CH601, CH650, CH701, CH750 and variants of these four models. This MTD can be found HERE and is also available below. A number of cases have been found whereby the structural integrity of the horizontal stabiliser mountings on the Zenair types identified above have been compromised by one or more of the following: cracking of the attachment brackets oversize holes loose rivets distorted and chafed brackets. These problems could occur due to a number of factors including poor build quality, a build-up of tolerances in the positioning or dimensions of the brackets, improper assembly, rough treatment or in-flight vibration. Failure of a tailplane attachment could result in degraded controllability in flight or loss of control. Special inspections of this area have been recommended by Zenair since January 2017, in their document ‘Mandatory Action. Jan. 2017 – Inspection of Horizontal Stabilizer tail attachment brackets’. This Mandatory Technical Directive mandates this safety action for aircraft operating on LAA Permits to Fly. MTD-01-2025 - Zenair Tailplane Brackets .pdf Download PDF • 162KB Next Previous

< Back LAA AGM 2025 Full article on the AGM and elected directors will be in the November issue of Light Aviation due out next week. Elected Directors : Alan Crutcher, Alistair Seymour, Clive Shipley, Paul Kirkham, David Millin, Peter Pengilly Next Previous

< Back Francis Donaldson is awarded the Honourable Company of Air Pilots Sword of Honour 22 Sept 2023 This year’s Sword of Honour – which recognises an outstanding contribution to General Aviation – goes to Francis Donaldson. For more than 30 years, as Chief Engineer of the then Popular Flying Association and then Light Aircraft Association, Donaldson has recommended the issuing of permits to fly for more than 3,000 aircraft and overseen the engineering and handling reviews of around 200 different types. He stood down from his role at the beginning of 2022 but has remained involved as a consultant. Few people have been more influential to the progress and development of light aircraft in the past three decades, with an encyclopedic knowledge backed by real world engineering and flight testing expertise. Press release - Air Pilots Trophies and Awards 2023 (2) .pdf Download PDF • 167KB . Next Previous

< Back Engineering updates in July 7 Aug 2025 The following documents have been issued/updated in the Engineering 'Info Library' during July. Continuing airworthiness information : Mandatory Technical Directive MTD-05-2024 issue 2 - Jabiru distributor caps Mandatory Technical Directive MTD-03-2025 - Marquart Charger aileron slave strut Alert A-05-2024 issue 2 - Rotax engine oil spray nozzle Alert A-07-2025 - Glastar aileron servo-tab pushrod cracking Alert A-08-2025 - Gen 4 Jabiru engine crankshafts Technical leaflets : TL 2.00 - Revalidating your aircraft's Permit to Fly TL 2.19 - The LAA Generic Maintenance Schedule TL 2.33 - Insepctor categories for type TADS : 274 - Europa 315 - Eurostar 324 - Supermarine Spitfire mk26 Propeller type lists PTL/1 : Kitfox mk1/mk2/mk3 Forms : LAA/AR-REF (FB GYROPLANE) - Airworthiness review reference guide (crib sheet) LAA/AR-REF (HOMEBUILT GYROPLANE) - Airworthiness review reference guide (crib sheet) LAA/AR-REF (FIXED WING) - Airworthiness review reference guide (crib sheet) LAA/CFS-1 (GYRO) - Check flight schedule LAA/CFS-1 (FIXED WING) - Check flight schedule LAA/FBG-SUPP - Supplement to factory-built gyroplane revalidaton form LAA/PFRC-1 - Permit Flight Release Certificate LAA/FT-NEW - Flight test schedule, new builds, transfers, modifications and repairs LAA/FT-ENG - Flight test schedule, engine modifications Next Previous

< Back Mandatory Technical Directive issued for Supermarine Spitfire mk26 and mk26a 16 Feb 2024 It has been found that there is potential for the fin of the Supermarine Spitfire Mk26 and 26B to be misaligned during build, due to a build-up of tolerances in the fin and its attachment, possibly leading to a mis-rigging of the rudder and failure to achieve the desired range of rudder travel. This could possibly result in degraded controllability in flight and on take-off and landing. In the interests of safety MTD 01-2024 calls for mandatory checks to be made on the fin alignment and rudder range of movement. Next Previous

Light Aviation Magazine 2012 Click on the links below to open each issue of Light Aviation Magazine from 2012 January 2012 April 2012 July 2012 October 2012 February 2012 May 2012 August 2012 November 2012 March 2012 June 2012 September 2012 December 2012

< Back Employment Opportunity - Advertising, Sales, Marketing and Social Media Manager 30 Nov 2023 The LAA are hiring! Advertising Sales, Marketing and Social Media Manager The Light Aircraft Association supports its members build, maintain, fly and enjoy light aircraft. We have over 7000 members and look after over 4000 aircraft across the UK. We are looking someone to take control of our advertising, sales, marketing and social media. This is a fantastic opportunity for the right person to help define, implement and then deliver the strategy to transform the way the LAA communicates with its 7000-plus members. What you will do:- Work with our advertising partners to ensure they get the best ROI for their advertising spend in our magazine – Light Aviation Work with the Editor to ensure all advertising space is filled Work with the CEO ang HQ team to develop and implement a multichannel communications strategy Grow and manage the LAA’s social media presence What we offer: The chance to make a difference – We are a small team, we are all passionate about aviation and everyone counts! Develop your skills The opportunity to get flying Hybrid working Paid holidays This role would ideally suit someone with a Degree in Business/Business Management with an interest in Sales and Marketing Next Previous

< Back MTD-06-2025 published - Europa Tailplane Torque Tube Mod Failure 16 Dec 2025 Ref: LAA Mandatory Technical Directive MTD-06-2025 – Europa Tailplane Torque Tube Clamp Mod A recent inspection of a Europa fitted with the tailplane torque tube clamp modification, LAA MOD 10623, revealed both halves of the clamp had broken and fallen apart. These clamps are intended to prevent relative movement between the tailplane torque tube, the tailplane drive plates and the central drive horn, on which the mass balance arm is mounted. Failure of these clamps could allow free play to develop, potentially leading to taper pin hole damage, tailplane flutter, or jamming of the pitch control mechanism. An inspection must be carried out within the next 5 flying hours to determine whether MOD 10623 is fitted. If MOD 10623 clamps are fitted, making use of a light source and mirror as necessary, inspect the alloy clamp blocks for any signs of cracking (in particular along the sharp corner between the bolt flanges and main body), for any signs of looseness or relative movement between the parts and for any other abnormalities. If any of these are detected, the aircraft must not be flown and LAA Engineering must be contacted. This must be repeated at intervals not exceeding 25 flight-hours or the next Permit revalidation inspection, whichever occurs first, for as long as MOD 10623 remains fitted. Please refer to the below Mandatory Technical Directive for full details, compliance times, and certification requirements. This MTD can be found HERE and is also available below. MTD-06-2025 - Europa Tailplane Torque Tube Mod Failure .pdf Download PDF • 259KB Next Previous