Permit Aircraft Electrics - Basic Course Price Member - £224, Non-Member - £244 (includes printed course material) Duration Arrival 09:00. Finish 17:00. < Back About the Course This course provides the theory and practical knowledge to enable the implementation of a basic electrical system in permit aircraft. Although the course necessarily includes a small amount of technical theory; it is only included at a level needed (essentially Ohms Law) to understand how wire sizes, fuses, circuit breakers and other components etc are selected. The basic premise of the introductory course is that the owner/builder already has a circuit diagram to work from (few kit manufacturers provide electrical diagrams, so the course includes details of where such ‘standard’ diagrams may be found). They are not expected to do any design work, but they do need to source the materials and components and build a working, reliable and safe installation. 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. The course uses a PowerPoint presentation for the theory side, a demonstration electrical panel in the classroom so that attendees can see the various options and good practice for wiring and systems installation and also runs two practical sessions in the LAA workshop which includes practical soldering, wire stripping and connector crimping, cable marking options, use of heat shrink, radio antenna coax connector installation and the correct crimping and installation of typical D Sub connectors used for avionics systems. What this course will try to do is: Introduce and explain the components of a wiring system Help you understand a circuit diagram Give practical experience in wiring techniques Give the knowledge to select and source cables and components Explain failure modes and reliability issues Help you conduct basic fault finding Warn about the ‘gotcha’ areas and the things to look out for What the course will not do is: Turn you into a design engineer Enable you to design an aircraft EWIS Enable you to fault find on an undocumented aircraft installation Solve interference issues Delve into avionics Your Instructor Mark Castle-Smith Dates Date tbc 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

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

Flight Testing Aircraft The following current flight test schedules are available for printing. These schedules are subject to change at any time and without notice. Ensure that the current flight test schedule is used otherwise it may not be accepted. For this reason it is not advisable to save these document on your computer. Flight Testing Forms & Schedules Other useful documentation is as follows: TL 1.19 Initial Testing Flying Pilot Briefing for First Flight TL 2.00 Revalidating a Permit to Fly CAP 1038 CAA Check Flight Handbook TL 3.19 Auto-Pilot Flight Test Notes TL 3.22 Flight Test Reports TL 3.23 Constant Speed Prop Set-Up TL 3.25 General notes and limitations on test flights Airpseed Indicator Calibration Climb-Performance Plotter FAA Flight Testing Handbook

< Back LAA Alert for some models of Rotax Engines 1 Mar 2025 LAA Alert A-02-2025 has been published on the LAA website (and is also attached), highlighting a recent service bulletin published by Rotax regarding the inspection and/or replacement of the crankcase and/or gearbox housing on affected engines. Rotax has identified a potential manufacturing issue affecting the hardness values of the crankcase and/or gearbox housing materials in certain engines. These components may not meet the required specifications for material hardness, which could lead to reduced component durability and/or potential oil leakage. Rotax regards this bulletin as mandatory. A-02-2025 - Rotax Crankcase .pdf Download PDF • 220KB Next Previous

Strut Governance Documents Strut Governance Documents Electronic versions of the Strut Event Management Procedures can be found below. Click each document to access it online. Updated April 2019 Member Club Regulations The Member Club Regulations describe the manner in which an LAA Member Club should form, govern its affairs and conduct its activities. Strut Event Management Procedure Procedures for Strut events (fly-ins etc..) Annex A Normal and Prohibited Club Activities Annex B Summary Insurance Certificate for Member Clubs of the LAA Annex C LAA Member Club - Event Notification Annex D LAA Club Event Risk Assessment (air side/ground activities) Annex E Event Safety Review and Operations Summary Annex F Third Party Passenger Flying at LAA Member Club Events Annex G Incident Checklist / Incident Plan Appendix 1 TPPF Pilot and Aircraft Checklist Appendix 2 Indemnity Agreement Appendix 3 Information for those Attending an LAA Member Club Flying Event Model Club Constitution A model constitution for member clubs

Over the years this has led to several commercially successful kitplanes (Europa, Streak Shadow, Sherwood Ranger), as well as designs that have been released for plans-building (Flitzer, Isaacs Fury, FRED) and a whole range of fascinating on-off personal aircraft – the Acro Advanced, Bonsall Mustang, Mickleburgh Sparrow to name just a few. There will always be LAA’ers keen on the ‘retro’ look, but with ever-increasing fuel costs we foresee a greater emphasis in future on aircraft exploring higher efficiency, alternative powerplants (electric?) and renewable materials. High hangarage fees mean that aircraft enthusiasts are more than ever interested in folding or de-riggable aircraft that can be kept at home. Using the information provided by clicking the links below, the LAA hopes to stimulate interest in light aircraft design, help potential designers through the process and encourage the development of high quality designs. With the decline in UK manufacturing over the recent decades, it seems more than ever important to keep alive a thread of creativity and enthusiasm for design and development. For some, the ability to bring a personal design from first concept to a flying prototype provides the ultimate source of satisfaction within the LAA scene. Designing Aircraft Since its formation in 1948, one of the stated aims of the LAA has been to encourage the designing and building of new types of light aircraft. For our own purposes, we in LAA Engineering have been producing a series of Excel spreadsheets to use as tools in the verification of calculations in the many aircraft design submissions we deal with. The spreadsheets have been designed to carry out the various calculations that are necessary during the design of light aircraft. Some of them have been written against specific paragraphs in the design code CS-VLA, whereas others, for example, cover areas related to the development of aircraft undergoing flight testing. In addition, simple spreadsheets for straightforward mathematical calculations have been written. It is for information and educational purposes that these spreadsheets are now available to LAA members on the LAA web site. Use the buttons below for more information on each design stage: Preliminary Design Detail Design Certification/Approval

< Back Eurofox Rudder Pedal Failures - LAA Standard Modification Approved & MTD-05-2025 Issue 4 19 Jan 2026 LAA Standard Modification SM16826 provides a terminating action to the 10-hour inspections required in LAA MTD-05-2025, which has now been up-issued to ISSUE 4 The LAA Standard Modification – SM16826 ‘ Reinforcement of Rudder Pedal to Torque Tube Joints ’ has been through our internal review process and is now formally approved. SM16826 strengthens all 4 pedal joints by the addition of welded steel, wrap-around finger plates. Incorporating this standard modification provides a terminating action to the 10-hour inspections required in LAA MTD-05-2025, which has now been up-issued to Issue 4. The CAA have also confirmed that incorporating this modification will be a terminating action for CAA MPD-2026-002-E and we expect the MPD to be upissued this week to reflect this. Once Standard Modification SM16826 is completed, owners will need to submit an LAA/MOD 1 Form ( Standard Mod Incorporation ) to let us know that the modification has been embodied, so that we can update our records at LAA HQ. A copy of Form LAA/MOD 1 is here . As a CAA-approved welder is required for this modification, owners have been provided with a list of CAA welders known to the LAA. MTD-05-2025 - Eurofox Rudder Pedal Cracking Issue 4 .pdf Download PDF • 913KB SM16826 Reinforcement of Rudder Pedals Issue 1 .pdf Download PDF • 743KB Next Previous

Hirth 2 Stroke Covering Letter to Owners Fuel System Inspection Checklist

Rotax Carburetted 912/914 Installation & Operation Price Member - £213, Non-Member - £233 Duration Arrival 09:30. Finish 17:00. < Back About the Course Kevin Dilks of SAS, a well-respected and Rotax trained engineer, has many years of experience in the field and will be hosting this course at the LAA’s Training facility at Turweston. The course covers everything those who own/operate a carburetted Rotax 912 (UL, ULS and 914 turbocharged) engine need to know about getting the best out of these very popular engines and keeping them in tiptop condition. Your Instructor Kevin Dilks Dates New date tbc Times Arrival 09:30. Finish 17:00. Duration One day course Venue LAA HQ, Turweston Aerodrome, NN13 5YD Price Member - £213, Non-Member - £233 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 New LAA Inspector - Keith Troughton 4 Sept 2025 We are pleased to welcome Keith Troughton as a new LAA Inspector, having attended an LAA Inspector Assessment Day at Turweston recently. With an active aviation interest from a very young age, he has been involved in certified, homebuilt, and microlight aircraft for over 40 years. He is currently operating within a C.A.O. General Aviation Facility as a Licensed Aircraft Engineer (L.A.E.). He is a CAA-approved maintenance manager within an approved Aircraft Maintenance Facility, with access to most of the necessary tooling for standard aircraft maintenance support, including facilities to weigh aircraft, if required. Next Previous

Engineering INFO LIBRARY CONTINUING AIRWORTHINESS INFORMATION INSPECTOR ZONE FLIGHT TESTING AIRCRA FT NIGHT/ IFR REVALIDATING A PERMIT TO FLY TECHNICAL LEAFLETS OPERATING & MAINTAINING BUILDING AIRCRAFT MODIFYING & REPAIRING AIRCRAFT FIND AN INSPECTOR TADS ENGINEERING FEES DESIGNING AIRCRAFT BUYING AIRCRAFT