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< Back Mandatory Technical Directive issued for Pietenpol Air Campers 19 Jul 2024 Mandatory Technical Directive, MTD-06-2024 has been issued to introduce mandatory checks for corrosion on the wing rear struts. This follows a recent in-service finding where servere corrosion was found in a flying example of the type in the UK. The MTD must be carried out before further flight on or after 18th July 2024 on Pietenpol Air Camper aircraft fitted with the 'Jim Wills' wing rear struts. Next Previous

< Back CAA MPD-2026-003-E – Rotax 912/914 Series Engines 6 Jul 2026 Propeller Gearbox Inspection (Rotax 912/914 Series Engines) Please note that the UK Civil Aviation Authority (CAA) has published Emergency Mandatory Permit Directive MPD-2026-003-E, which was issued on 30 th June 2026 and became effective on 07 th July 2026. The directive applies to Rotax 912 UL, 912 ULS, 912 iS Sport, and 914 UL series engines fitted with affected propeller gearboxes as defined in the MPD. The MPD mandates inspection of the affected propeller gearboxes due to a potential assembly process deviation that could result in oil loss and/or an in-flight engine shutdown. Please note for the most seriously affected engines mandatory action is required BEFORE THE NEXT FLIGHT. Please review the MPD to determine whether it applies to your aircraft or engine and ensure that the required inspection and any necessary corrective actions are completed within the specified compliance times. If you have an engine of one of the effected types, please note the pink pages of the engine logbook should have a new entry made for this MPD, either on the applicable or non-applicable page, as appropriate. The directive (MPD-2026-003-E) for your reference and can also be found HERE or below. The Rotax Alert Service Bulletin containing the list of affected Rotax engines and their serial numbers is available via the following link HERE and is also provided as an attachment below. MPD-2026-003-E - Rotax 912, 912 i and 914 (series) engines .pdf Download PDF • 236KB ASB_A-2026-001R01 - Inspection of the propeller gearbox for ROTAX 912,914 and 912i Series .pdf Download PDF • 1.46MB Next Previous

< Back Engineering updates in February and March 11 Apr 2025 The following documents have been issued/updated in the Engineering 'Info Library' during February and March. Technical leaflets : TL 1.10 - List of aircraft parts and materials suppliers TL 2.01 - A guide to LAA aircraft ownership TL 2.22 - Non-type specfic MPDs TL 3.25 - Flight test briefing Continuing airworthiness information : Alert A-01-2025 - Piper rudder post Alert A-02-2025 - Rotax crankcase Alert A-03-2025 - Gen 4 Jabiru 2200 and 3300 engines TADS : Brandli Cherry Cessna 120 Eurostar Groppo Trail Rans S5 (204 and 204B) Rotax 4-stroke Sportcruiser Next Previous

< Back Mandatory Technical Directive issued for Eurofox aircraft 6 Dec 2024 Inspection of Trim Tab Operating Cable Attachment to Prevent In-Flight Failures and replacement with Improved Design of Cable Attachment In 2016, the LAA issued an Alert, LAA/AWA/16/08 , regarding reported problems with the thin stranded steel elevator trim cable on Eurofox aircraft fraying at the attachment point to the trim tab operating horn, where the design forced the cable to be bent around the sharp edges of the clevis. The 2016 Alert also provided a link to, and served to promulgate, the Eurofox UK Service Bulletin on the subject, SB 04/2016 . Recently we’ve been advised of a potentially serious incident of elevator flutter on a Eurofox while towing a glider, which was caused by the trim cable failing altogether in flight where it passes around the trim tab operating horn clevis. This resulted in violent shaking of the elevator with serious potential for structural damage or loss of control. Since the cable had evidently frayed considerably before failing altogether, this occurrence highlights the importance inspecting the trim cable for signs of fraying at this point at each pre-flight and maintenance check, and, as the service bulletin explains, of keeping the clevis free-moving about its attachment to the tab so the clevis remains in line with the cable as the tab moves. This minimises the relative movement between the two which if occurring, would accelerate the wear on the cable. Eurofox UK advises that since the issue of the 2016 Service Bulletin, they have revised the design of the cable attachment clevis so that the cable now passes around a circular bush rather than being forced into two sharp bends, which reduces the wear on the cable and tendency to fray and eventually break. MTD-07-2024 , issued today, requires Owners/Operators to check whether the old or new design of clevises are fitted and for any signs of trim cable fraying before further flight. Owners/Operators must obtain and use a copy of the up-issued AEROPRO Checklist - B Service/Maintenance plan (Update Nov 2024 LAA aircraft) before the next 50-hour check. Finally, the trim cable system must be replaced immediately if any trim cable fraying is found, as detailed in the MTD. Furthermore, all Eurofoxes with the old-style of clevis must have the trim cable system replaced, as described in the MTD, by 1st June 2025. MTD-07-2024 Eurofox Trim Cable .pdf Download PDF • 495KB Next Previous

< Back New LAA Inspector - Andrew Williams 31 Mar 2025 We are pleased to welcome Andrew Williams as a new LAA Inspector, having attended an LAA Inspector Assessment Day at Turweston recently. Andrew has been involved with aircraft maintenance for approximately 36 years. Types he has worked on include Rolls-Royce Dart and Pratt & Whitney PT6-powered passenger and freighter aircraft, followed by working on short-to-medium range jet aircraft. For the last 10 years, Andrew has been involved with general aviation single and twin-engined aircraft, carrying out maintenance and certification. He holds a CAA approval to perform Airworthiness Reviews in order to issue Airworthiness Review Certificates. His qualifications include: CAA Part 66 Licence, inc. Full Group 3 and a BCAR Sec L Licence. In the LAA ‘world,’ Andrew has a share in a Jodel 1050. Congratulations Andrew. Welcome to the team! Next Previous

< 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

< Back LAA Alert issued for Lycoming Engines 28 Nov 2024 The LAA has issued Alert A-02-2024 (link below) to highlight the recent Lycoming Airworthiness Directive regarding connecting rod bushings and connecting rod assemblies. The FAA has issued a new airworthiness directive (AD) for models of Lycoming engines that have an affected part installed and are assembled within the ship date range, as specified in Table 1 to paragraph (c) of this Airworthiness Directive (AD 2024-21-02). The AD comes into effect on 5th December 2024. This AD was prompted by several reports of connecting rod failures which resulted in uncontained engine failure and in-flight shutdowns. The AD requires repetitive oil inspections for bronze metal particulates at each oil change, and if found, additional inspections of the connecting rod bushings for damage, proper fit, movement, and wear, and replacement if necessary. The first oil inspection must take at the next oil change or within 4 months after the AD becomes effective i.e. 5th April 2025, whichever occurs first. As terminating action to the connecting rod bushing inspections, this AD requires replacement of the connecting rod bushings with parts eligible for installation. LAA A-02-2024 - Lycoming Connecting Rod Assemblies .pdf Download PDF • 203KB Next Previous

LAA Member Discounts

< 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

< 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

< Back MTD-02-2025 issued - Mission M108 Nose Leg Failures - ISSUE 2 14 Aug 2025 MTD-02-2025 - 'Nose leg failures' has been upissued to reflect the availability of alternative parts from the manufacturer. This MTD can be found HERE 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 replacement parts, now available from Lambert Aircraft Engineering, are installed. Next Previous

< 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