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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 Issue 3 - Rans Control Linkage Rod End Connector Safety Washers | Light Aircraft Assoc

    < Back MTD-04-2025 Issue 3 - Rans Control Linkage Rod End Connector Safety Washers 4 Dec 2025 MTD-04-2025 upissued to Issue 3 to amend the specification of the metal washers that must used to replace plastic washers. MTD-04-2025 Issue 3 is published in order to amend the specification of the metal washers that must be used to replace plastic washers. Therefore, MTD-04-2025 Issue 3 supersedes Issue 1 and 2. Issue 1 and 2 of this MTD are 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 3 .pdf Download PDF • 130KB Next Previous

  • ROTAX® Service Bulletins – Inspection of the Propeller Gearbox | Light Aircraft Assoc

    < Back ROTAX® Service Bulletins – Inspection of the Propeller Gearbox 2 Dec 2025 Inspection of the propeller gearbox of ROTAX® 915 i and 916 i(Series) Aircraft Engines ROTAX has issued new Service Bulletins regarding the inspection of the propeller gearbox on ROTAX® 915 i and 916 i (Series) aircraft engines. These bulletins below outline the required inspection procedures, affected serial numbers, and any necessary corrective actions. · ASB-915 i-021R1 / ASB-916 i-009R1 · ASB-915 i-021iS R1 / ASB-916 i-009iS R1 Compliance with these bulletins is important to ensure continued airworthiness and safe operation of your aircraft. ASB_915 i-021R1_916 i-009R1 .pdf Download PDF • 1.31MB ASB_915 i-021iSR1_916 i-009iSR1 .pdf Download PDF • 85KB Next Previous

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

    < Back Mandatory Technical Directive issued for Pioneer aircraft 6 Mar 2024 The control horn on the elevator trim tab on a Pioneer 300 failed in flight, which resulted in sever trim tab flutter. A safe landing was made and there was no further damage to the aircraft. MTD-02-2024 requires the checking of this horn on all Pioneer variants to ensure that it is of the correct design standard and recommends regular checks for free-play in the system. Next Previous

  • Mandatory Technical Directive issued for many Zenair types | Light Aircraft Assoc

    < 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

  • Armstrong-Isaacs Bursaries for 2026 | Light Aircraft Assoc

    < Back Armstrong-Isaacs Bursaries for 2026 21 Nov 2025 Armstrong-Isaacs bursaries for 2026! The LAA is proud to announce the opening of applications for its Armstrong-Isaacs bursaries for 2025. Five bursaries of up to £1,500 are offered to young pilots already in PPL training, offering extra funding to help them complete their courses, at a time when, all too often, money starts to run out. More information on the bursaries can be found here . 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. 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

  • 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

  • Alert A-10-2025 - Cracking in E-Props Carbon Propeller Hubs | Light Aircraft Assoc

    < Back Alert A-10-2025 - Cracking in E-Props Carbon Propeller Hubs 28 Aug 2025 LAA Alert A-10-2025 - Cracking in E-Props Carbon Propeller Hubs A recent report of a crack appearing on an E-Props carbon composite propeller hub was received by the British Microlight Aircraft Association (BMAA). The crack was in the flange forming the periphery of the circular hub, in the close vicinity of one of the bolts in the outer ring of blade clamping bolts. Alert A-10-2025 shows photographs of the crack discovered and details required actions if cracks are found on LAA aircraft. A-10-2025 is available HERE and shown below. A_10_2025_E_Props_Propeller_Hub_Cracking_Issue_1 .pdf Download PDF • 382KB Next Previous

  • LAA Alert for Rotax 900 series engines regarding the oil spray nozzle | Light Aircraft Assoc

    < Back LAA Alert for Rotax 900 series engines regarding the oil spray nozzle 18 Dec 2024 Inspection and/or Replacement of Oil Spray Nozzle On 16.12.24, Rotax issued a new MANDATORY Service Bulletin SB 912 i-016/SB 915 i-016 / SB 916 i-006 which calls for urgent action for engines of specified models within certain serial number ranges, if the engine has run for less than 200 hours from new, or engines which have been fitted with specific overhaul kits supplied between 01.01.22 and 31.10.24 inclusive. The bulletin concerns problems with a possible full or partial blockage of the oil spray nozzle due to an excessive application of Loctite at the manufacturing stage, when assembling the sprag clutch housing. This can lead to inadequate cooling of the stator assembly, potentially causing loss of electrical power to the engine’s ECU. A-05-2024 Rotax Engine Oil Spray Nozzle .pdf Download PDF • 205KB Next Previous

  • General Information | Light Aircraft Assoc

    LAA are proud to announce our Rally 2025 sponsors General Information Event Opening Hours 9.30am – 5.00pm each day (Fri & Sat) 9.30am – 4.00pm (Sun) Fly-In Instructions Up to date fly-in instructions can be found here . Please read these before you fly into the Rally. Camping Camping facilities providing basic amenities including hot showers will be available on site. There is ample ground for caravans and motorhomes. The site will be up and running from Thursday afternoon and will close early on Monday morning. Camping passes can be bought in advance via the LAA Shop . In addition to catering provision on the exhibition site, evening food and a bar will be available on the Thursday, Friday and Saturday evenings with entertainment on Friday and Saturday evenings, provided by Leicestershire Aero Club. Parking Please follow the signs to the designated free Rally Car parks. Designated parking will be signed for Disabled and Exhibitor users. You must display a Blue Badge if using Disabled Parking areas - any car without a Blue Badge will be asked to move to the main parking area. All emergency access ways must be kept clear. Please ensure you are familiar with the routes and do not block with vehicles or stock. Please do not block emergency gates onto the airfield. You must ensure that you keep the roadway clear for all other users. Dogs We understand that many visitors wish to bring their dogs with them, we welcome dogs on site. However, as this is an operational airfield, all dogs MUST BE KEPT ON A LEAD when on any part of the site. Dogs are not allowed in the aircraft parking areas. Please ensure you pick up after your dog. Anyone caught allowing their dog to foul without picking up will be asked to remove the dog from site. All dogs must have an identity tag with contact tel no on. WiFi Should you require WiFi, then please bring your own supply. Please be aware that due to the remote location of the airfield, WiFi reception can be unreliable. Water Drinking water is on the campsite and at the tower. There is an outside tap at the tower. Waste We operate a clean site policy and therefore all exhibitors, visitors and traders should remove their own rubbish from their pitch. A skip will be provided on site for cardboard and general rubbish. No electrical or hazardous materials should be disposed of in the skip. Toilets & Shower Facilities Toilets will be provided in the exhibition site, in the aircraft park and on the campsite, together with hot shower facilities. First Aid First Aid cover is provided by an external third party for the duration of the event. In the event of an emergency, please contact them or a member of Leicester Airfield staff. Fire Fire Marshals will be in attendance and should be contacted in the unlikely event of fire. Please ensure all flammable materials are kept away from possible sources of ignition. Dispose of any rubbish in the skips provided. No naked flames are allowed on any exhibition stand or trading stand. Security Regular patrols are carried out by our contracted security staff. e-Scooters No e-Scooters are permitted on site.

  • Certification & Approval | Light Aircraft Assoc

    Certification & Approval 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 ? Downloadable Spreadsheets Technical Leaflets Design Tutorials

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