< Back International Women in Engineering Day 23 Jun 2023 To mark this year’s International Women in Engineering Day, the UK Civil Aviation Authority had a chat with Lucy Wootton, our Chief Inspector. Simon Tilling, our CEO said: “The LAA are really proud of Lucy and the work she is doing to improve the service we offer to our members. We would be very keen to hear from more women who want to consider a career in light aviation” Learn more about how Lucy’s career has developed to encompass gliding, powered flying and aeronautical engineering. Next Previous

< Back Engineering updates in April 6 May 2025 The following documents have been issued/updated in the Engineering 'Info Library' during April. Technical leaflets : TL 2.00 - Revalidating your aircraft's Permit to Fly TL 2.33 - Inspector categories for types (new TL) Forms: LAA/AR-REF - Airworthiness review reference guide (crib sheet) (new form) LAA/CFS-1 (fixed wing) - Check flight schedule LAA/PFRC-1 (fixed wing) - Permit flight release certificate Next Previous

< Back New Permit Revalidation System Announcement 20 Mar 2025 The new Permit Revalidation System is coming on 15th April - watch the announcement video below to find out more! Next Previous

< 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 Mandatory Technical Directive issued for Rotax 914 powered Eurofox aircraft 29 May 2024 Mandatory Technical Directive, MTD-03-2024 has been issued today to introduce mandatory disabling of cabin heat on examples of the type fitted with Rotax 914 (and derivative) engines. This follows an in-service occurrence of carbon monoxide entering the cabin due to leaks from the exhaust system. The MTD must be carried out before flight on or after 5th June 2024. This MTD has been emailed to all affected owners. Next Previous

< Back LAA Alert published for Gen 4’ Jabiru 2200 and 3300 engines 1 Mar 2025 LAA Alert A-03-2025 has been published on the LAA website (and is also attached), highlighting the recent service bulletin, JSP 051, published by Jabiru Aircraft Pty Ltd, which applies to specific Jabiru 2200 and 3300 engines and requires the replacement of the pistons on engines within certain serial number ranges, which they state were supplied between April 2017 and August 2019. Jabiru regards the Bulletin as mandatory. The Bulletin advises that Jabiru has identified that pistons supplied with the affected engines were in some cases susceptible to failure, and have specified that the pistons must be replaced by pistons of the later, improved design at or before 200 hours running time, following the procedures shown in the engine overhaul book, including any necessary running-in provisions and choice of oils. A-03-2025 - Gen 4 Jabiru 2200 and 3300 engines .pdf Download PDF • 201KB Next Previous

< Back MTD-05-2025 Eurofox Rudder Pedal Cracking 19 Nov 2025 MTD-05-2025 Eurofox Rudder Pedal Cracking - Mandatory Inspection requirements, which must be completed before your next flight There have been two reported instances in the UK of Eurofox aircraft experiencing cracking at the right-foot rudder pedal on the starboard seat side, where it is welded to the rudder pedal torque tube, leading to the pedal no longer being rigidly attached to the torque tube. On at least one of these instances, aircraft handling was negatively affected, reducing yaw authority and seriously degrading flight safety. Note that failure of the starboard side right-foot rudder pedal results in loss of rudder control, even when the aircraft is flown from the Pilot in Command position i.e. from the port seat side. Please refer to the MTD-05-2025 document below for full details of the mandatory inspection requirements, which must be completed before your next flight and subsequently at intervals not exceeding 10 flight-hours or the next Permit Revalidation inspection, whichever occurs first. MTD-05-2025 can be also found here MTD-05-2025 - Eurofox Rudder Pedal Cracking .pdf Download PDF • 247KB Next Previous

Permit Aircraft Electrics - Advanced Course Price Member - £224, Non-Member - £244 (includes printed course material) Duration Arrival 09:00. Finish 17:00. < Back About the Course The Basics course covers simple DC theory and concentrates on the practical aspects of installing a basic permit aircraft electrical system. The course explains how to interpret a ‘typical’ permit aircraft electrical systems diagram and for every element, explains how to size, select and source components and then how to practically install them. This Advanced course builds on the Basics course by providing more detail about component selection and options and the use of integrated power management systems within permit aircraft. The course takes the simple systems design introduced in the Basics course and explores options for creating more complex electrical systems including the use of dual and essential system bus bars. The course introduces fault tolerant design considerations, thus allowing attendees to consider safety and fault analysis in their own designs. As a tool for understanding this aspect of the course, it will take an introductory look into the requirements of electrical systems for those wishing to fly their aircraft under IFR. What this course will try to do is: Explain power generation and distribution options in a light aircraft More advanced consisderations into component selection Discuss circuit protection devices and systems Explain failure modes and reliability issues Introduce interference and EMC issues Show correct grounding and screening techniques Provide you with the knowledge to plan an installation and create the necessary documentation Warn about the ‘gotcha’ areas and the things to look out for What the course will not do is: Turn you overnight into an expert Enable you to fault find on an undocumented aircraft installation Delve inside avionics boxes It will be useful, but not essential, for people to have previously attended the Basic course. In order to make the best of this course, if you have not attended the basics course, you will need to understand basic DC theory; Ohms Law and the Power Law. Please note that this course is primarily a classroom based course, as you will already have the practical skills you need, which are covered in the basics course. Your Instructor Mark Castle-Smith Dates 8 February 2026 Times Arrival 09:00. Finish 17:00. Duration One day course Venue LAA HQ, Turweston Aerodrome, NN13 5YD Price Member - £224, Non-Member - £244 (includes printed course material) Booking Pls call the LAA on 01280 846 786 to enquire/book or email [email protected] . *Please note that payment is required when booking, to confirm your place. NO place will be held without confirmed payment* **Please note that your booking payment is non-refundable unless we can fill your place timeously or there are exceptional circumstances**

< Back Eurofox Rudder Pedal Failures - CAA Mandatory Permit Directive 12 Jan 2026 MPD-2026-002-E – Eurofox Rudder Control System - Rudder Pedal/Rudder Pedal Torque Tube - Inspection The CAA has published a Mandatory Permit Directive (MPD) concerning cracking of Eurofox rudder pedals. Please see MPD-2026-002-E below for full details, or access it HERE . MPD-2026-002-E - Rudder Control System - Rudder Pedal_Rudder Pedal Torque Tube - Inspectio .pdf Download PDF • 175KB Next Previous

< Back Carbon Monoxide in Piston Engine Aircraft Consultation 22 Feb 2024 In recent years, the CAA has been actively engaged in raising pilot awareness of carbon monoxide (CO) in general aviation (GA) and has undertaken multiple initiatives to promote prevention and detection measures to mitigate the risk. We have now launched a public consultation seeking stakeholder views on: the barriers pilots face in obtaining an active CO detector, the role that maintenance plays in combatting CO, the importance of protecting passengers from CO, and whether active CO detectors ought to be mandatory for some operations. The consultation closes on 20 March 2024. We invite stakeholders to give us your views . Next Previous

< Back MTD-05-2025 Issue 2 published - Eurofox Rudder Pedals 5 Dec 2025 MTD-05-2025 Issue 2 has been published to provide further information on the situation as it develops and asking Owners and Inspectors to report back. The inspection schedule in unchanged from Issue 1. Therefore, Issue 2 does not require you or your Inspector to do anything different. If your aircraft has already been inspected to MTD-05-2025 Issue 1, then the next time an inspection in accordance with the MTD is due, you Inspector should reference Issue 2 in their logbook entry. LAA is continuing to work towards achieving a permanent solution via a modification to the rudder pedal/torque tube design. MTD-05-2025 Issue 2 is attached below and can be found on the website HERE . MTD-05-2025 - Eurofox Rudder Pedal Cracking Issue 2 .pdf Download PDF • 574KB Next Previous

< 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