< Back MTD-02-2025 issued - Mission M108 Nose Leg Failures 6 Jun 2025 MTD-02-2025 - 'Nose leg failures' was issued today for Mission M108 aircraft. This MTD can be found HERE and is also attached below. Three instances of nose leg failure have occurred in the past 12 months, two of which recently. This MTD mandates the regular inspection of this area until a long-term fix has been put in place. Lambert Aircraft Engineering is working to finalise a solution as soon as possible, working closely with the LAA. We will update the MTD as appropriate once a solution is in place. MTD-02-2025 - Mission M108 Nose Leg .pdf Download PDF • 212KB Next Previous

< 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

< 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

< Back MTD-01-2025 ISSUE 2 published - Zenair Tailplane Brackets 28 Aug 2025 MTD-01-2025 - 'Inspection of horizontal stabiliser (tailplane) attachment brackets and associated hardware for cracks, looseness and other forms of distress' for Zenair CH601, CH650, CH701, CH750 and variants of these four models has been upissued to Issue 2. This is in order to correct an error in the 'Effective Date' of this MTD. 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. 20250828 - MTD-01-2025 - Zenair Tailplane Brackets - Issue 2 .pdf Download PDF • 183KB Next Previous

< Back CAA Licencing Update 11 Jun 2025 ** The final legislation has not yet come into force and we’ll provide more comprehensive details when we have confirmation of the actual legislation (hopefully late July) that has gone to Parliament ** Link to document can be found below: CAA Licencing update .pdf Download PDF • 459KB Next Previous

< 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

< 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

< Back Spaces left on the 'Caring for your Gypsy Major Course' 26 Sept 2023 We have a few remaining spaces on the following LAA workshop: Caring for your Gipsy Major - Basic Course Date: Tuesday 3 October 2023 Time: 9.45am - 5.00pm Cost: £120 for members/£140 for non-members Booking deadline: Thursday 28 September Please click here to send an email if you are interested or call the office on 01280 846786. Next Previous

Preliminary Design Preliminary Design is the stage where the design is sized and developed in outline, leading to a three view drawing, performance and weight predictions. To help with this, LAA has developed a number of spreadsheets. Spreadsheet 1 is used to develop the basic geometry of the proposed aircraft, size the wing, fuselage and tail surfaces and work out some of the key parameters used later. Spreadsheet 2 is used to estimate the performance of the aircraft based on the geometry, initial weight estimates, engine power and guestimates of the drag coefficient and prop efficiency, allowing you to see how the performance is affected by changing each parameter in turn. Spreadsheet 3 is used to work out the critical structural speeds, develop the flight envelope and predict the aerodynamic loads on the main surfaces which can be used to size the structure, and as the basis for a load test program. The weight and balance spreadsheet elsewhere on our website allows the designer to quickly evaluate the implications on weight and cg of different positions for the crew, fuel tanks and baggage bay, and work out what empty aircraft weight and cg he must aim for. Thanks to the simplicity of these programs it takes only minutes to study the implications of changing the aircraft’s specification, for example the effect of changing the wing aspect-ratio, the trade-off between extra weight and cleaning up the airframe drag, extra power etc. Downloadable Spreadsheets Worked Spreadsheet Examples Design Tutorials

< Back Alert A-11-2025 - Eurostar aileron rose joint and rudder hinge inspection 8 Oct 2025 LAA Engineering has issued Alert A-11-2025 to highlight the recent issue of an Airmasters service bulletin that requires checks on the integrity of a rose joint in the aileron controls and the rudder hinge, following examples of these joints migrating and jamming aileron controls. Following the up-issue of Airmasters SB/EUR/023 to issue 3, on 07/10/25 CAA has issued MPD 2025-004-E to mandate the checks contained in the SB, which supersedes MPD 2025-003-E initially issued on the subject. A-11-2025 - Eurostar Rose Joints issue 1 .pdf Download PDF • 372KB Next Previous

< Back Engineering updates in January 5 Feb 2026 The following documents have been issued/updated in the Engineering 'Info Library' during January. Technical Leaflets : TL 3.29 Installation of changes approved by STC (new) Forms : LAA/FT-NEW Flight test schedule Continuing airworthiness information : MTD-05-2025 Eurofox rudder pedal cracking (issue 4) TADS: Bristell Next Previous

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