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< Back Alert A-05-2025 - Alpi Pioneer 300 - Inspection of Undercarriage Components for Cracking and Corrosion 12 Jun 2025 LAA Alert A-05-2025 - Alpi Pioneer 300 - Inspection of Undercarriage Components for Cracking and Corrosion LAA Alert A-05-2025 has been published on the LAA website (and is also attached), highlighting Alpi Pioneer 300 and 300 Hawk aircraft that have suffered different malfunctions and failures of various components that make up the undercarriage. This Alert strongly recommends a close inspection of the undercarriage at 25-hour intervals for corrosion and cracking, as well as a retraction check, to verify that the retraction system components remained correctly adjusted, to avoid undercarriage collapse due to the mechanism not being adequately over-centre when extended. A-05-2025 - Alpi Pioneer 300 Landing Gear Corrosion .pdf Download PDF • 204KB Next Previous

< Back MTD- 04-2026 Issue 1 - Vans Fuel Pick Up Failure 28 Jul 2026 MTD- 04-2026 Issue 1 - Vans Fuel Pick Up Failure Following consultation on the draft Mandatory Technical Directive (MTD), we have published the final MTD-04-2026 Issue 1, effective 28 July 2026. This MTD relates to confirming which aircraft have embodied Van’s SB 06-2-23, requiring wire locking of the fuel pick-up assemblies in the wing fuel tanks, or have the later T-715 anti-rotation brackets fitted. It follows a recent incident involving a Van’s RV-6 suffering a fuel starvation event in flight, due to a fuel pick-up tube becoming detached after the retaining nut had come undone. Upon inspection, it was found that the wire locking had not been incorporated and the airframe logbook did not show an entry confirming compliance with SB 06-2-23. Owners are required to review their aircraft records and, where compliance with SB 06-2-23 cannot be confirmed, nor the fitment of T-715 anti-rotation brackets, Owners must complete the inspections and actions specified in the MTD within the next 25 flying hours or at the next Permit to Fly revalidation, whichever occurs first. Compliance with this MTD must be recorded in the aircraft airframe logbook. If applicable, the entry must also state compliance with Van’s SB 06-2-23 or the fitment of T-715 anti-rotation brackets. Otherwise, there must be a logbook entry, signed by the Owner, explaining why SB 06-2-23 has not been embodied, or T-715 anti-rotation brackets fitted. Please refer to MTD-04-2026 Issue 1 document for full identification guidance and compliance requirements HERE and is also available below. MTD-04-2026 Issue 1 - Vans Fuel Pick-Up .pdf Download PDF • 391KB Next Previous

< Back Engineering updates in February 5 Mar 2026 The following documents have been issued/updated in the Engineering 'Info Library' during February. Technical Leaflets : TL 1.03 'Information required on completion of your build project' TL 1.10 'List of aircraft parts and materials suppliers' TL 3.03 'Avionics installations' Standard modifications : SM 16826 'Eurofox reinforcement of rudder pedals' issue 2 TADS: Eurofox Next Previous

< Back LAA RALLY 2026! 3 Nov 2025 We’re thrilled to announce that our 2026 Rally is officially in the calendar! Mark your diaries and get ready for a special rally, celebrating the LAA 80th Anniversary. 📅 Date: 4/5/6 September 2026 📍 Location: Leicestershire Aero Club, Leicester Airport. More details will follow soon. Enquiries to [email protected] We can’t wait to see you all there! Next Previous

< 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 - Conrad Ceillam 2 Sept 2025 We are pleased to welcome Conrad Ceillam as a new LAA Inspector, having attended an LAA Inspector Assessment Day at Turweston recently. As a youngster, he worked mostly on 3-engined piston aircraft for commercial flight, and on some twin turboprops in Guernsey. He then moved on to mostly narrow-bodied jets and turboprops, with some executive jets in the UK. Latterly, he worked in Finland on medium-bodied jets, scientific aircraft, and mission/patrol. Since moving to Shetland, he has mostly worked on twin-piston passenger craft. He has held BMAA inspector approvals since April 2023. Next Previous

< Back MTD-01-2026 Issue 1 Published - Shadow Aircraft Oratex Disbonding 15 Apr 2026 MTD-01-2026 - 'Oratex Disbonding' was issued today for Shadow aircraft. This MTD can be found HERE and is also attached below. This follows a reported incident in the UK in which Oratex covering on the upper surface of a Streak Shadow wing suffered a largescale disbond while in flight. No LAA Shadow aircraft with Oratex covering may fly after the effective date of this MTD unless you comply with this MTD. Please refer to the MTD-01-2026 document for full details of the mandatory requirements . For LAA Shadow aircraft not covered with Oratex, non-applicability of MTD-01-2026 should be recorded in the relevant logbook pink pages. 20260415 - MTD-01-2026 Issue 1 - Shadow Oratex Disbonding .pdf Download PDF • 259KB Next Previous

< Back New LAA Alert for all Rotax 900 series engines 13 Dec 2024 The LAA has issued Alert A-04-2024 – Highlighting loose and broken engine mounting bolts on Rotax 900 series engines A recurring problem with Rotax 912/914 engines, equally applicable to the newer 915 and 916 models, is of the four M10 bolts that attach the engine’s crankcase to the engine mounting frame becoming loose in service. Most manufacturers call for the bolts to be wire-locked in place. However, in the case of the Rotax engine mounting bolts, it seems that the bolts are coming loose not because the bolts are undoing and backing off on their threads, but because of the joint faces become imprinted over time through creep, corrosion or fretting, allowing the tension in the bolt to be lost and the joint to become loose. These problems in the field are a reminder that where it’s critical that a bolt be torqued up, this should be checked at intervals (at least annually, we’d suggest) by undoing the locking and re-torquing them, before replacing the locking wire. Be sure this check is included in your aircraft’s maintenance schedule. DO NOT RELY ON A BOLT BEING WIRE LOCKED TO BE SATISFIED THAT THESE CRITICAL BOLTS ARE STILL TIGHT. A-04-2024 - Loose Rotax Engines .pdf Download PDF • 207KB Next Previous

< Back LAA members - Make your views known! 25 Jan 2024 Basingstoke & Deane Borough Council's consultation on their draft Local Plan – which includes a proposed new Popham Garden Village on Popham Airfield, has opened. It runs until 4 March 2024. This proposal is not in line with either Government policy or their stated aim to make the UK the best place in the world for General Aviation. The Government's policy can be found in their publication ' Flightpath to the Future " and makes repeated references to the vital importance of airfields, forming a critical part of national infrastructure. You can have your say and tell Basingstoke & Deane Council that their proposal is contrary to Government policy and insist the proposal is removed from the current ‘draft’ strategic plan. Visit the Local Plan Update ' Have Your Say ' section of their webiste. Next Previous

< 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

< Back New LAA Inspector - Steve Hodge 4 Apr 2024 The LAA is pleased to welcome Steve Hodge as a new LAA Inspector. Steve came to an Assessment Day at LAA HQ at the start of March. Steve has been part of the aviation trade since 1997, when he joined Arrow Aviation Services as a trainee. He pretty much learnt his entire trade there and was very fortunate to have worked with a wide variety of components from engines and propellers, to wheels and brakes, with a lot of vintage aviation thrown in too. His is now as Owner and Accountable Manager of his own company, SOAR Aviation, a CAA Part 145 approved facility. He continues to provide the aviation industry with what he hopes is thought of as an honest, reliable, friendly and cost-effective service. He has always been involved with the LAA and enjoys serving the LAA community. Next Previous