Search this site

< Back MTD-02-2025 Issue 3 - Mission M108 Nose Leg Failure 21 Jul 2026 MTD-02-2025 Issue 3 - Mission M108 Nose Leg Failure This MTD is applicable to all Mission M108 aircraft fitted with the tricycle landing gear configuration (LSTC 1-002). This MTD is issued in order to mandate inspection of the affected area of the original nose leg or the installation of the new design standard of nose leg. It also clarifies and expands some aspects of the Lambert Aircraft Service Bulletin (Lambert Aircraft Engineering Service Bulletin SB-108-515 Rev 1). If MTD-05-2025 Issue 2 has been complied with, no further action is required at Issue 3. Please refer to the MTD-02-2025 Issue 3 document for full identification guidance and compliance requirements - available below. MTD-02-2025 Issue 3 - Mission M108 Nose Leg Failure .pdf Download PDF • 170KB Next Previous

< Back Two new LAA Inspectors appointed 28 Sept 2023 Congratulations to our latest LAA Inspectors, Luke McMillan and Gareth Rutt. Luke and Gareth both came to LAA HQ at Turweston last Thursday for 'Induction, Examination and Interview Day' with our Chief Inspector, Lucy. We wish Luke and Gareth well as they start this exciting new chapter! Next Previous

< Back New LAA Inspector - Robin Smith 2 Apr 2026 Robin enjoys every aspect of light aircraft whether it be flying or maintenance. Robin spent 15 years with REME attached to the Army Air Corps, was Aircraft Engineering Warrant Officer. He trained and experienced on helicopters, Skeeter, Bell 47 (Sioux), Alouette, Scout and Gazelle including their respective power units. He trained and experienced on fixed wing Auster 9 and Beaver including respective power units. He saw active service in Aden and Northern Ireland. He also flew in his early days as an observer. Robin has a UK PPL; he is a CRI and Fl(A). He currently instructs at Fowlmere with the British Aviation Academy and at Flying Made Easy at Old Buckenham airfield. He has aerobatic and aerobatic instructor rating and night rating. Differences training includes tailwheel and constant speed propellors. Robin has flown Robin HR200, Maule, Grob 115D, Cessna 140, Cessna 152, F24 Argus and PA28. He has owned a Robin HR200 a Maule MXT7 180A, Auster 6 and he currently owns a Grob115A C1 Aero which is fully aerobatic. He just loves turning himself upside down! He has worked with Modern Air Ltd at Fowlmere airfield doing annuals, inspections and repairs to Cessna 140, Cessna 152, Cessna 172, Cessna 177 Cardinal, Argus, Twin Cessna 310 and Extra aircraft. Currently he works with Touchdown Engineering at Old Buckenham on average some 2 days per week. He is also Safety Manager at Fowlmere and EASA approved. Robin has a small company Beagle Flight Consultancy Ltd which can provide several services which include Flight instruction via DTO/ATO, 2-year revalidations. Prebuy surveys, aircraft transport by road in UK and Europe. Import and export handling of light aircraft, inclusive of dismantle, containerisation, shipping, customs docus and assembly. Next Previous

< Back Standard Modification for fresh air rotary ventilators added for Europa types 18 Oct 2023 A new Standard Modification (SM12871) has been uploaded to the website for Europa types. This covers the installation of rotary air vents in the forward cockpit to aid ventilation. Standard Modifications are used to enable other owners to install a modification on a given type, generally by following the instructions in the Standard Modification leaflet, having their inspector check and sign it off and letting LAA Engineering know that it's been installed. Further information on the Standard Modification process can be found in TL 3.06 Standard Modification leaflets can be found by following Engineering - Info Library - Engineering - Standard Modifictations. Technical leaflets can be found by following Engineering - Info Library - Engineering - Technical Leaflets. Next Previous

< Back The online Permit Revalidation System is live for Gyroplanes! 22 Jul 2025 We are pleased to announce that the online Permit to Fly revalidation system went live today for gyroplanes, both home-built and factory-built! Step-by-Step Video Guide, FAQs and Crib Sheet The step-by-step guide to the new online Permit Revalidation system in the form of an ‘ Online Permit Revalidation Explained ’ video can be found below. This was written for a fixed-wing example, but the majority of questions are the same for gyroplanes and the process for gyroplanes has the same three stages as for any fixed-wing aircraft. https://www.youtube.com/watch?v=rOGRQ89dOA8 We have also compiled a list of ‘ Frequently Asked Questions ’ for you, which are found below. The ' Crib Sheet ' for Inspectors referenced in the video is formally called the ' Airworthiness Review Reference Guide ' and is available HERE . There is a version of the crib sheet for homebuilt gyroplanes, entitled ARR-REF (HOMEBUILT GYROPLANE) and a version for factory-built gyroplanes, entitled ARR-REF (FB GYROPLANE). The Check Flight Schedules for both homebuilt and factory-built gyroplanes have now been combined into a single check flight schedule for gyroplanes, entitled CFS-1 (GYRO). This is available HERE . Previous check flight forms for homebuilt and factory-built gyroplanes are now obsolete. The Permit Flight Release Certificate (PFRC) is now a separate document, where it was previously contained within the application form for revalidating a Permit to Fly. It can be found HERE . Key Considerations There are a few key considerations to ensure a Permit to Fly revalidation under the new system goes smoothly: Please make sure you know your username and password for the LAA website. 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 of submission of the revalidation application. This is in order to provide a baseline for the online system. The 3-year check flight cycle will then apply subsequently to most aircraft types. Some aircraft will still require a check flight at every revalidation, these are: Aircraft cleared for Night/IFR. Aircraft which have flown less than 12 hours since the previous revalidation inspection. Aircraft Owners will not have to submit a CFS-1 (GYRO) Check Flight Schedule when applying through the new system. However, a CFS-1 (GYRO) will need to be completed for each check flight and stored with the aircraft’s documentation, so that it is available when needed. We will no longer be accepting old-style (paper or scanned) Airworthiness Reviews for homebuilt or factory-built gyroplanes conducted on or after 22 nd July 2025. Need Help? The ‘Revalidating a Permit to Fly’ page on the LAA website signposts you to all the information you will need and can be found HERE . If you have any problems or questions, please follow the steps below: Watch the ‘ Online Permit Revalidation Explained ’ video found HERE . Read Technical Leaflet 2.00 - 'Revalidating your Aircraft's Permit to Fly,' which has now been updated to include information for gyroplanes. Look at the gyroplane variants of the 'crib sheet' for LAA Inspectors, entitled ' Airworthiness Review Reference Guide ,' which is available HERE . Look at our list of FAQs ,. If steps 1-4 do not help you find the answer, contact LAA Engineering on [email protected] or call (0)1280 846786 20250721 - Permit Revalidation Process FAQs Issue 2 .pdf Download PDF • 198KB 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 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

< Back New LAA Course dates released 6 Oct 2023 Dates have now been published for upcoming LAA Courses for the rest of this year. To find out about specific courses and their dates, click here . Please note, the next 'Caring for your Gipsy Major' course is on the 11th November, not 7th November, as published in the latest edition of Light Aviation magazine. Next Previous

Weight & Balance The subject of Weight and Balance covers at least four distinct procedures: weighing an aircraft, calculating its empty weight and centre of gravity (CG), establishing the worst forward and aft CG loading cases according to an appropriate design code and calculating weights and centres of gravity for an actual flight. This section includes guidance notes on each of these aspects, forms and worked examples (imperial or metric) for recording and calculating empty weight and CG, as well as worst forward and aft CG cases and an Excel based spreadsheet that makes the weight and CG calculations for you. The table on the spreadsheet is set out in the same layout as the Loading Examples tables. This spreadsheet can, of course, also be used for carrying out calculations for an actual flight. Simply input the actual weights of the items to be loaded rather than the standard occupant or maximum fuel and baggage weights. Remember, it is important to check that the CG remains within limits with no usable fuel as well as with the loaded fuel in the tanks, even though it will not be your intention of running the tank dry. The calculator generates two sets of weight and CG values for this purpose. Weight & Balance arrangements for gyroplanes are different to those of aeroplanes and a special type of report is used, unless the manufacturers concerned provides their own special schedule in which case this should be used instead. Before accessing the documents below, please ensure you have read Technical Leaflet 3.16 - Weight and Balance Guidance Notes . Technical Leaflet 3.16 Other useful documentation is as follows: Weight & Balance Forms Weight and Balance Example Forms Weight and Balance Excel Calculators

Light Aviation Magazine 2019 Click on the links below to open each issue of Light Aviation Magazine from 2019 January 2019 April 2019 July 2019 October 2019 February 2019 May 2019 August 2019 November 2019 March 2019 June 2019 September 2019 December 2019

Aircraft Maintenance Before accessing the maintenance documents below, please ensure you have read Technical Leaflet 2.19 - General Maintenance Schedule . Technical Leaflet 2.19 Other useful documentation is as follows: Maintenance Schedules Sample Engine Condition Monitor Blank Engine Condition Monitor AC 43.13-1B Chg 1 CAP 562: CAAIP CAP 661: MPDs Latest MPDs - not in CAP 661 CAP 747: Mandatory Requirements Breaking in an Engine Engine Pre-Oiler Schematic Forms, Checklists & Worksheets

Night IFR Certain LAA types can be cleared for flight at night and/or under IMC (instrument meteorlogical conditions) - commonly referred to as 'Night/IFR' for convenience. The special Night/IFR requirements and process are detailed in technical leaflets TL 2.27 and 2.28, linked below, which are additional to the standard requirements applicable to any LAA aircraft. The special requirements involve the aircraft being of a type that demonstrates flight handling broadly in accordance with CS-23 subpart B (some types, including the RV-6 and RV-7, have a restricted aft cg limit to meet the pitch stability requirements), and each individual example must have a special IFR flight test to confirm it matches the first one tested. For a night clearance, the aircraft must also undergo a night test to check its lighting and general suitability for night flight. The aircraft must have accumulated enough flying hours in VFR to prove its reliability, and it must have an engine of a type accepted as being likely to be as reliable as a certified engine (for example we accept ‘clone’ Lycomings even though not certified). The propeller must be rain-proof, i.e. have hardened leading edges, and the aircraft must have an effective carb ice prevention system. The aircraft’s panel must have at least two independent attitude indicators, with either separate power sources or back-up internal power. If two EFIS are used to provide attitude information, with no other attitude instrument, then the two EFIS must be of different manufacturers so as to avoid the risk of simultaneous failures. There must be pitot heat, an alternative static and an OAT gauge. If the essential systems are relying on electrical power, the electrics must be designed to avoid being vulnerable to any single component failure, and if there is a single alternator there must be enough battery capacity to keep the essential systems running for an adequate time (at least 30 mins) before the battery goes flat. If two radios are fitted, they must not be both vulnerable to failure if any single component fails (e.g. must not be both fed through a single avionics master switch with no back-up power available). LAA does not specify what navigation or radio equipment is fitted, but as with a certified aircraft, the equipment fit determines what type of airspace can be used. An autopilot is not required, but certainly helps reduce pilot workload in sustained instrument flight. Non-certified equipment, including EFIS and autopilots, alternators, etc, are permitted, subject to the usual LAA checks. The aircraft has to be inspected initially and annually by an inspector with a special ‘night/IFR’ endorsement on their LAA inspector approval, and the aircraft is checked to have been built to an appropriate level of quality for a night/IFR aircraft. For example, quality of its instrument wiring, electrical power supply wiring, etc, are checked which are much more critical than in an aircraft only flying day VFR. The ASI and altimeter must be regularly calibrated, the battery must have a regular capacity check and the radios checked regularly by a qualified radio engineer. The aircraft must have an accepted pilot’s operating handbook and an acceptable maintenance schedule, and be maintained to that schedule. The application process involves not only a night/IFR inspector but also a night/IFR assessor who is one of a small band of LAA volunteers qualified to assess the design aspects of the aircraft’s systems and who compiles a technical report about the aircraft and if he is happy with it, includes a recommendation to remove the day-VFR only restriction. The report includes details of the aircraft’s systems, the special flight test reports, inspection reports, maintenance schedule and POH, a photo of the instrument panel and an electrical load analysis. This report is sent to LAA Engineering who checks through it and all being well, issues the aircraft new paperwork with the day and/or VFR restriction removed and replaced by limitations allowing IFR and/or night flight. All LAA night/IFR aircraft are restricted to not fly in the vicinity of thunderstorms and, for IFR cleared aircraft, take-off and landing in visibility less than 1500m is prohibited. The aircraft may not be operated in IMC below 500 ft agl for a precision approach, or 600 ft for a non-precision approach, or approach system limits, whichever is the greater. The pilot qualification for flying an LAA night/IFR aircraft at night or in IFR is the same as for flying a certified light aircraft at night or IFR. Aircraft types that have been successfully cleared for night/IFR flight include the RV-6, -7, -8, -9 and -10 (nosewheel and tailwheel variants – some with cg range restrictions), Europa and Cozy. Several of the modern lightweight 600 kg types have failed to comply due to low stability margins making them OK for day VFR flight but not suitable instrument platforms for night or IFR. Whilst a very few Rotax powered aircraft have been be to be cleared, most of the thirty or so LAA aircraft that have successfully transitioned are powered by Lycoming or Lycoming-clone engines. PROCESS SUMMARY LIST OF TYPES PERMIT IFR FEES NIGHT IFR INSPECTORS FAQs POH LITE TEMPLATE (PowerPoint File) NIGHT IFR PILOTS ACCEPTED INSTRUMENTS TL 2.27 - PROCEDURE FOR APPROVAL & TL 2.28 - ASSESSMENT OF AIRCRAFT LAA/MOD15 APPLICATION FORM