British Gliding Association – Technical Committee TNS 12/05 Technical News Sheet 12/05 Part 1 1.1 1.2 1.3 1.4 1.5 Airworthiness issues (all categories) Glasflugal Club Libelle 205, Mosquito, Hornet (Mandatory) AD D-1998-028R1 Elevator drive bracket inspection and modification/replacement Some types were omitted in the English translation of the original AD. Inspection compliance is before next flight and for serviceable brackets modification or replacement by 12 February 2006. AD details enclosed and sent to owners If previously complied with and recorded in log book, no further action is required Grob Astir Tailplane mounting Ball (Information) Reported by Bernd Vermeulen of Kestrel Gliding Club The annual repeat inspection as required in AD-D-2004-168 and MSB 306-38 has revealed a cracked thread. Please ensure great care is taken during this inspection to prevent a catastrophic failure. It is also recommended to carry out this inspection after incidents such as heavy or rough landings. Grob Astir Tailplane location pins (Information) Reported by Stu Hoy of Anglia Sailplanes The rear Tailplane location and retention pins have shown indications of cracks on the abutment flange faces to the Tailplane spar plate attachment. The cracks only show after careful use of dye penetrant technique NDT. Aircraft operating on CAA Permit to Fly (Mandatory) The following general Mandatory Permit Directives apply MPD 1995-001 R3 Airworthiness Directives for aircraft previously issued with a CAA C of A MPD 1998-019 R1 Flexible fuel tubing Copies of MPD’s attached. Where reference is made to the person carrying out and certifying the inspections, a BGA inspector should be considered in the same light as authorised by the PFA or BMAA for certifications on BGA aircraft. Note: A BGA inspector cannot certify PFA or BMAA aircraft unless he/she holds the appropriate PFA or BMAA authorisation. SZD Junior Tailplane rigging (Information) Reported by G Reeves, East Sussex Gliding Club The rear Tailplane location arm was found not located in the lower receptacle in the fin. The glider had flown in this condition. Excessive lateral play was noted, as the Tailplane was not located correctly. Apart from some burring and difficulty in removing the locking pin, no other damage was found. 1 TNS 12/05 1.6 SZD Puchacz BGA 046/12/2005 issue 1 (Recommended) The BGA recommends that an inspection of the lower part of the control sticks are carried out at annual intervals or after incidents where excessive forces may have been applied. BGA inspection attached Part 2 Modifications Part 3 None this issue. General Matters 3.1 Variation and recording of inspections and AD’s As a general reminder, it should be noted that a BGA inspector may NOT vary the content of an Airworthiness Directive in any way. AD’s should be embodied by inspection, replacement, modification or as described, exactly and completely as detailed on the AD. Should it be necessary to necessary to vary an AD, due to an error, for example, then the issuing authority must be consulted. Compliance with AD’s and required inspections etc. must be recorded in the glider or aircraft log book. It is acceptable to record work details on worksheets but the AD must be referenced in the log book entry. 3.2 Scheibe (Information) We have been advised that Scheibe Flugzeugbau GmbH have gone into receivership. We understand that they are offering limited product support until May 2006 when the company will close. They are actively looking for someone to buy the company and/or offer continued product support. We will publish further details in due course. Compliance Statement: All mandatory inspections and modifications have been included up to the following: Airworthiness Notices, Contents issue: 137 CAA CAP 747 Mandatory Requirements for Aircraft, issue: 2 amendment: 11/2005 State of Design Airworthiness Directives review date: 15 December 2005 For reference: Mandatory Aircraft Modifications & Inspections Summary, issue 287 Final issue – continued in CAP 747 FAA Summary of Airworthiness Directives. Bi-weekly listing 2005-25 Foreign Airworthiness Directives Vol. I and II – CAA Additional Airworthiness Directives, Cancelled Foreign Airworthiness Directives Vol III, issue 372 Final issue – continued in CAP 747 CAA Mandatory Permit Directives, issue 2005/2 Jim Hammerton Chief Technical Officer 2 TNS 12/05 3 TNS 12/05 4 TNS 12/05 5 TNS 12/05 6 TNS 12/05 7 TNS 12/05 8