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  • Alert A-08-2025 - Gen 4 Jabiru 3300 Engine Crankshafts | Light Aircraft Assoc

    < Back Alert A-08-2025 - Gen 4 Jabiru 3300 Engine Crankshafts 25 Jul 2025 LAA Alert A-08-2025 - Gen 4 Jabiru 3300 Engine Crankshafts On 11.4.25, Jabiru Aircraft Pty Ltd issued a new Service Bulletin, JSB 046, which applies to specific Jabiru 3300 engines and requires the replacement of the crankshafts on engines within certain serial number ranges, which they state were supplied between April 2017 and June 2024. Jabiru regards the Bulletin as mandatory. The Bulletin advises that Jabiru has identified that, as a result of an issue with heat treatment, crankshafts supplied with the affected engines are in some cases susceptible to failure. Jabiru have specified that the crankshaft must be replaced by a crankshaft of the later, improved design. Affected crankshafts must be replaced prior to 15th December 2026, or 150 hours total time in service (TTIS), whichever occurs later. A-08-2024 can be found HERE and is also shown below. A-08-2025 - Gen 4 Jabiru 3300 Engine Crankshafts .pdf Download PDF • 202KB Next Previous

  • Positive Progress | Light Aircraft Assoc

    < Back Positive Progress 11 Sept 2026 Positive progress on the investigation into the tailplane attachment bolt hole positioning issue We wanted to provide a further update on the investigation into the tailplane attachment bolt hole positioning issue identified in some RV aircraft, and to share the encouraging progress that has been made. Since issuing MTD-07-2026 on 19th August and the revised Issue 2 on 25th August, which included a helpful relaxation of one of the edge-distance limits, we have received around twenty reports from owners whose aircraft were found to be outside the published criteria. Van's Aircraft has received more than sixty similar notifications following the release of Service Bulletin SB-00134. Many of these reports have provided valuable data, which is helping build a clearer understanding of the issue across the wider RV fleet. Over recent weeks, LAA Engineering and Van's Engineering Team have been working closely together, reviewing these reports on a daily basis. By examining the various types of edge-margin discrepancies in detail, we have been able to develop a much better understanding of the structural implications and the most appropriate solutions. Following a very productive meeting on 9th September with Van's Chief Engineer, Rian Johnson, LAA Engineering will now reassess all reported LAA cases in light of this latest technical work. We are optimistic that a number of aircraft may be able to return to flight immediately without further action. Others may require only limited rework, while a smaller number may need more extensive rectification. These reported cases are our highest priority, and we intend to provide individual responses to affected owners by 18 September 2026. Where a straightforward solution is not immediately available, we will look to Van’s for a proposal of how to deal with the individual aircraft. A particularly positive development is that Van's has completed additional finite element analysis of the affected structure and, based on these findings, has released Revision 2.1 of Service Bulletin SB-00134, dated 4th September. This latest revision introduces further relaxations to some of the bolt-position criteria, reflecting increased confidence in the structural capability of the design. In certain cases, aircraft previously considered non-compliant may now be acceptable for continued operation, subject to periodic inspections. We are currently awaiting some additional technical data relating to Service Bulletin revisions 2.0 and 2.1 before publishing MTD-07-2026 at Issue 3. Until the revised MTD is issued, owners carrying out MTD-07-2026 Issue 2 must continue to apply the criteria contained within SB-00134 Revision 1 and continue reporting any non-conformances to both the LAA and Van's. We are in the process of updating MTD-07-2026 to reflect the latest engineering findings from Van's and to incorporate any additional improvements that can simplify inspections and minimise disruption to owners. Our aim is to provide clear, practical guidance that supports both safety and continued flying activity wherever possible. If your aircraft is found to be non-conforming, we would be grateful if you could also include photographs of both bolt groups from above and below (using a mirror or endoscope where necessary). These images are proving extremely valuable in helping our engineers assess each case efficiently and determine whether any corrective action is required. We appreciate the patience and cooperation shown by RV owners throughout this process. The close collaboration between owners, the LAA and Van's has already produced significant progress, and we remain committed to restoring aircraft to service safely and as quickly as possible. For reference, copies of the documents mentioned above are provided below. 20260825 - MTD-07-2026 - Vans Horizontal Stabiliser Attach Position Iss 2 .pdf Download PDF • 476KB SB 00134 - Horizontal Stabilizer Forward Attach Bolts - Rev 1 .pdf Download PDF • 1.57MB Next Previous

  • LAA HQ will be closed on Friday 3rd July due to the Silverstone Grand Prix | Light Aircraft Assoc

    < Back LAA HQ will be closed on Friday 3rd July due to the Silverstone Grand Prix 29 Jun 2026 LAA HQ will be closed on Friday 3rd July 2026 due to the Silverstone Grand Prix. All staff will be working from home, so can continue to deal with your calls and emails, but will not be on site at Turweston to answer any questions directly or receive any hand-delivered documents. Next Previous

  • Alert A-07-2025 - Glastar Aileron Servo-Tab Pushrod Cracking | Light Aircraft Assoc

    < Back Alert A-07-2025 - Glastar Aileron Servo-Tab Pushrod Cracking 25 Jul 2025 LAA Alert A-07-2025 - Glastar Aileron Servo-Tab Pushrod Cracking A cracked aileron servo-tab pushrod was found on a UK Glastar aircraft. The pushrod consists of a thin-walled aluminium tube with an adjustable clevis at one end, and a fixed clevis at the other. The crack was at the adjustable end of the pushrod, and extended from the end of the aluminium tube to the hole approximately 1 inch from the end. A cracked aileron servo-tab pushrod must be considered unairworthy, and replaced before further flight. A-07-2024 can be found HERE and is also attached. A-07-2025 - Glastar Aileron Servo-Tab Pushrod Cracking .pdf Download PDF • 562KB Next Previous

  • Rally 2026 Trophy Winners | Light Aircraft Assoc

    < Back Rally 2026 Trophy Winners 22 Sept 2026 Best Auster Best Jodel Best Kit Build and Best RV Best Part Complete Homebuild Best Plans Built and Concours Winner Steve Rickett, congratulated by LAA CEO Simon Tilling Best Plans Built and Concours Best Vintage and Best DH Most Meritorious Arrival by Air Roy Mills Best Classic Runner Up Best Kit Build and Runner Up Best RV Runner Up Best Plans Built Next Previous

  • Engineering updates in November and December | Light Aircraft Assoc

    < Back Engineering updates in November and December 7 Jan 2026 The following documents have been issued/updated in the Engineering 'Info Library' during November and December. Technical Leaflets : TL 2.18 Change of owner/co-owner details TL 3.12 Engines and propellers fitted to LAA aircraft TL 3.17 List of approved prototype modifications Standard modifications : SM12871 Europa fresh air rotory ventilators SM16618 Europa PTFE lined hinges SM16770 LED exernal lights (new) Continuing airworthiness information : Alert A-13-2025 Sporcruiser nose leg failures Alert A-14-2025 Eurofox fuel line disconnected in flight Alert A-15-2025 Glasair rudder pedal bearing failures MTD-04-2025 Rans control linkage rode end connector washers MTD-05-2025 Eurofox rudder pedal cracking MTD-06-2025 Europa tailplane torque tube clamp mod failure TADS: Continental engines Eurofox Ikarus C42 Jabiru engines Pioneer 300 and 300 Hawk Piper J3C/L4 Woodcomp propellers Next Previous

  • The New Permit Revalidation System - Step-by-Step Guide | Light Aircraft Assoc

    < Back The New Permit Revalidation System - Step-by-Step Guide 9 Apr 2025 The new LAA Permit to Fly revalidation system will go live on 15th April 2025. This streamlined, fully online process offers an easier and faster way for aircraft Owners and Inspectors to handle Permit to Fly revalidations. Watch this video for a step-by-step guide on how to complete the online Permit Revalidation process, both as an Owner and as an Inspector. https://www.youtube.com/watch?v=rOGRQ89dOA8 There are a few key considerations to ensure your revalidation under the new system goes smoothly: Please make sure you know your username and password before applying for your aircraft’s revalidation. If you have forgotten your login details, please contact the LAA Office. All aircraft using the new system for the first time will require a check flight no older than 3 months at the time you submit the revalidation application. This is in order to provide a baseline for the online system. The 3-year check flight schedule will then apply subsequently to most aircraft types. Some aircraft will still require a check flight at every revalidation, these are: Aircraft cleared for glider tugging in their Operating Limitations document. Aircraft cleared for Night/IFR. Aircraft which have flown less than 12 hours since the previous revalidation inspection. You will not have to submit your CFS-1 Check Flight Schedule when applying through the new system. However, a CFS-1 will need to be completed for each check flight and stored with the aircraft’s documentation, so that it is available when needed. We encourage you submit your revalidation application through the new online system, as processing time is expected to be faster than an ‘old-style’ revalidation. If you still wish to make an ‘old-style’ application up until 15th May 2025, all 3 forms must be submitted by this date and you will only transition to the 3-year check flight schedule after your first revalidation through the new system. Note: The option to apply for revalidation in ‘My Aircraft Data’ on the LAA website may appear shortly before the go-live date on 15th April 2025 as our IT infrastructure is updated. However, we will only be able to process applications received on or after the official go-live date. A handy list of 'Frequently Asked Questions' is available below: 20240409 - Permit Revalidation Process FAQs V1.0 .pdf Download PDF • 175KB Next Previous

  • AGM | Light Aircraft Assoc

    < Back AGM The awards ceremony will start at 11.30 a.m. Registration for entry into the AGM will be open at 10.45. For more details, please see link below. https://www.lightaircraftassociation.co.uk/agm2025 Next Previous

  • New LAA Inspector - James Coyne-Downhill | Light Aircraft Assoc

    < Back New LAA Inspector - James Coyne-Downhill 15 Sept 2025 We are pleased to welcome James Coyne-Downhill as a new LAA Inspector, having attended an LAA Inspector Assessment Day at Turweston recently. James started flying at the age of 14 with the Air Cadets, flew solo on his 16th birthday, and earned his Private Pilot’s Licence at 18. By day, he works on Dassault Falcon 20 business jets as part of a base maintenance team, following an aircraft engineering apprenticeship at Cobham. Outside of work, he enjoys flying and maintaining Luscombe 8As. Next Previous

  • LAA host British Young Pilots | Light Aircraft Assoc

    < Back LAA host British Young Pilots 19 Feb 2026 The LAA is happy to support British Young Pilot's Weekend Club at LAA HQ, Turweston Aerodrome. More details about these events can be found below: BYP .png Download PNG • 2.87MB Weekend Club Turweston .pdf Download PDF • 688KB Next Previous

  • New LAA Factory-Built Gyroplane Inspector - Kevin Whitehead | Light Aircraft Assoc

    < Back New LAA Factory-Built Gyroplane Inspector - Kevin Whitehead 3 Apr 2026 We are pleased to welcome Kevin Whitehead as a new LAA Inspector, having attended an LAA Inspector Assessment Day at Turweston recently. Kevin joins us as an LAA Factory-Built Gyroplane Inspector based in Scotland, further strengthening our support for members and aircraft owners in the region. In his role, Kevin will carry out maintenance and repairs, conduct permit renewal inspections, and provide recommendations to help ensure the continued safety and airworthiness of LAA aircraft. We are delighted to have Kevin on board and look forward to his contribution to the LAA community. Next Previous

  • E10 Mogas | Light Aircraft Assoc

    E10 Mogas From 1st September 2021, the government mandated that all regular grade unleaded petrol must contain up to 10% ethanol, rather than up to 5% as previously. In the autumn of 2021, most filling stations around the UK re-marked their E5 petrol pumps to show that they now supply E10 specification fuel, and started receiving tanker-loads blended with up to 10 percent ethanol content. For the automotive world this means reduced carbon dioxide emissions, which is better for the environment, and, arguably in terms of eco-desirability, a small further reduction in the reliance on fossil fuel. The automotive industry had been preparing for this change, and people with road vehicles registered after 2002 should be able to switch to E10 without noticing any difference. Unfortunately, the additional ethanol content is bad news for aviation users if we were to ignore the change and start putting E10 in our aircraft regardless. Ethanol is a powerful chemical solvent which can attack components including rubberised gaskets and fuel pipes, older lacquered carburettor floats and composite or plastic components in some newer fuel systems. The doubling of the concentration of ethanol in E10 compared to E5 makes it much more likely that problems will be experienced if these parts are not designed to be ethanol-proof. Ethanol also has an affinity for absorbing water, which over time can then become acidic, attacking metal components in the fuel system and engine. Even if there was a practical way to do so in the volumes of fuel we use in our aircraft, we cannot safely remove the ethanol content from the fuel because the ethanol acts as an octane enhancer, so the washed-out fuel would be left with a reduced octane value, likely to cause detonation problems. Another issue is that ethanol-blended fuel has a lower energy density than petrol, so to develop full power from our engines using an E10 fuel, we may need to richen the fuel/air mixture, for example using a bigger carburettor jet size. Owners of Rotax and Jabiru engines are probably already aware that many of these engines are supplied as being able to use E10 fuel – though with Jabiru engines, in particular, it’s far from straightforward because some of the earlier engines require cylinder head modifications and reduced compression ratio if they are to avoid detonation issues when using any form of Mogas. Jabiru also say that Mogas of any type should not be used in commercial flight schools and only at the owners own risk. Even with a supposedly E10-compatable engine, the chemical compatibility problems with fuel system components are such that the LAA does not at present approve the use of E10 Mogas in any LAA amateur-built or vintage aircraft. For factory-built microlights and factory-built gyroplanes, where LAA is not the approving authority but only renews the CAA’s Permits to Fly, owners need to refer to the TADS for the types for details of the approved fuel types, and monitor the service bulletins from the approved manufacturers for news of any updates. Where we need to be particularly careful in reading-across from (hopefully) a trouble-free transition to E10 in automotive use is the big difference between our petrol cars and the way our aircraft engines are configured. Our cars generally have submerged fuel pumps in their petrol tanks and a sealed fuel system. In our aircraft we have an open-vented tank and usually a fuel pump several feet away, often mounted in a hot area of the engine bay near to the engine exhaust, dragging the fuel through a fairly convoluted pipework system, a filter and fuel selector – all features encouraging a vapour lock - and then to make matters worse we want to climb up to altitude and operate in reduced atmospheric pressure. Modern petrol cars have a fuel injection systems rather than carburettors, a circulating fuel system designed to purge any vapour forming in the fuel line, and an ECU that monitors the engine’s parameters constantly and adjusts the fuel mixture strength and ignition timing to prevent damage to the engine – and if all else fails and the engine should ‘pink’, we can hear it from the driver’s seat and drop a gear to lighten the load. Because of the much higher background noise level in our aircraft, detonation cannot be heard and the pilot’s first indication of a problem may be when the first piston crown disintegrates, or a valve head departs its stem. In conclusion - E10 is presently not approved for use in any LAA aircraft. ‘Hoping for the best’ and using E10 fuel in your aircraft regardless could risk ruining the fuel system components, fibreglass tanks falling to bits, engine failure through contamination of the fuel or ruptured fuel pump diaphragms etc, or more serious engine damage. For most of our engines, UL91 Avgas is the best choice, but 97 octane E5 Super Unleaded remains an alternative to the now-obsolete E5 spec Mogas.

Light Aircraft Association Ltd, Turweston Aerodrome, Nr Brackley, Northamptonshire, NN13 5YD

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Registered in England & Wales

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Company No: 00606312

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