Airworthiness News

SZD 50-3 Puchacz - Airbrake and Trimmer Controls 26th January 2012

An airbrake handle telescopic control rod became detached from forward mounting due to spherical bearing coming out of staked retainer. The trimmer control is a similar design. It is recommended that owners check to ensure the rods are secure.

Please report any further occurrences to BGA CTO.

Robin DR300 and DR400 - Oil lines Replacement 26th January 2012

EASA have issued AD 2012-0018 for the mandatory replacement of oil lines due to not being fire resistant. See AD for applicable aircraft, compliance time and SB details.

Rotax 912 and 914 Series Engines - Oil Pump and Attachment Bolts Inspection 26th January 2012

EASA have issued AD 2012-0019-E for the inspection of oil pump attachment bolts for correct torque within 4 flight hours or 30 days. See AD for applicable engine types, serial numbers and SB details.

December Updates 22nd December 2011

The January Engineering News is available to download. TNS, datasheets and airworthiness directives have also been updated.

Rotax 912/914 Engine Crankshaft Inspection 16th November 2011 UPDATED 25th November

EASA has issued AD 2011-0224-E for the inspection of crankshafts installed in specified engines within 4 flying hours or 30 days (from 16 November) whichever occurs first. Please see the notice from the UK Rotax agent, Sky Drive,  for more information. If your engine is affected please contact Sky Drive for further advice. This AD supercedes the previoulsy issued AD (2011-0222-E). The inspection and prohibition requirements are unchanged from the original AD. However, the serial number applicability has been widened.

TNS 10th November 2011

The TNS page has now been updated to allow download of all TNS since 1975.

BGA Standard Repairs to Gliders 10th November 2011

BGA Standard Repairs to Gliders is now available to download.  It was published in 1966. Please note; to use this publication for EASA aircraft the title must be included in the Type Certificate Holders list of approved publications or repair data or be referenced as part of an approved repair scheme.

Limbach Engines UPDATE 9th November 2011

Limbach have announced that the company has been sold and will not be closing. Production of new engines and product support will continue with effect from 1 January 2012. Please be aware that there is bound to be some company restructuring and there may be some hiccups to the normal service. For further details please see Limbach web site.

SZD 50-3 Puchacz Rudder Detached 4th November 2011

We have been advised that a BGA operated Puchacz recently lost its rudder on a landing roll. On initial investigation the GRP cup part of the lower rudder hinge mounted on the fuselage tail fairing, supporting and retaining the lower rudder hinge failed and the top became detached from the body of the hinge support.

The lower rudder hinge nut is accessed from the underside of the fuselage tail fairing and is contained within the cup. Please see picture attached. Operators are strongly recommended to remove the rudder and inspect the supporting cup area for cracks.

Please report any defects found to BGA CTO.

Please note; there is an existing EASA AD to replace the lower rudder hinge stiff nut with a castle nut and split pin. Ref AD 2006-0243-E

Glasflugel Sailplanes Elevator Control Rod Inspection 4th November 2011

EASA have published AD 2011-0213 for the inspection of the vertical elevator control rod in "T" tail Glasflugel sailplanes. Initial inspection must be completed before 16 December 2011 with subsequent inspection and annual inspection requirements.

November Updates 2nd November 2011

The November Engineering News is available to download. TNS and airworthiness directives have also been updated.

DG500 Series C of of G Tow Hook Mounting Bulkhead Inspection 27th October 2011

EASA has issued AD 2011-0209 for the inspection of the DG500 series C of G tow hook mounting structure by 9 December 2011. Please note that the initial inspection is permissible as pilot/owner maintenance and should be recorded in the log book. Please see AD for further details

MDM-1 Fox Control Stick Inspection 26th October 2011

EASA has issued AD 2011-0210-E for the before next flight inspection of the forward control stick. For details please see AD at http://ad.easa.europa.eu/blob/easa_ad_2011_0210_E.pdf/EAD_2011-0210-E_1

MDM-1 Fox Aileron Control Bell Crank Console 6th October 2011 UPDATED 12th October 2011

EASA has issued AD 2011-0195 for operational checks of the aileron control system following several occurrences of separation of the aileron control bell crank console from its mount being reported. 

UPDATE - EASA has revised the AD. The revision allows pilots to carry out the daily inspection requirements.

See http://ad.easa.europa.eu/blob/easa_ad_2011_0195_R1.pdf/AD_2011-0195R1_1

DG500 Series Rear Seat Headrest Modification 2nd October 2011

EASA has issued AD 2011-0191 to inspect and modify the rear headrest securing cord. See AD for applicability and compliance times. http://ad.easa.europa.eu/blob/easa_ad_2011_0191.pdf/AD_2011-0191_1

Regional Technical Officer Vacancies 29th September 2011

After many years of sterling service, Doug Jones and John Lavery are retiring as Regional Technical Officers for the SW England and Northern Ireland regions respectively and we are now seeking replacements. (The SW region covers Devon, Cornwall, Somerset, Dorset and South Gloucestershire; the Northern Ireland region covers the whole of Ireland as well as the Isle of Man). These are voluntary positions acting as the local BGA Technical Committee presence to provide advice and guidance to inspectors, make liaison visits to clubs, interview inspector candidates and generally represent the BGA and assist the CTO in the area on technical issues and training co-ordination. You will be invited to attend and contribute to the BGA technical committee. The role will suit experienced inspectors who wish to get involved with the support and regulatory side; it is not envisaged that it will involve auditing but may involve offering advice to inspectors, clubs and owners following audits on how to resolve issues.  If you interested in this challenging role, please write to the CTO cto@gliding.co.uk

Schempp-Hirth Dus Discus Series 27th September 2011

A Duo Discus aileron control recently became partially restricted due to jamming by a foreign object. On investigation, the wing tip aileron extension "up" stop (a small angle bracket bonded to the aileron extension), had become detached and found its way into the control circuit. It is believed that the stop became detached due to heavy handling of the wing tip, possibly when lifting the wing tip during transport or rigging using the aileron extension. Owners are strongly recommended to inspect the aileron extension "up" stop by viewing along from the wing/tip joint (with the tip removed). You are looking for a small angle bracket made from carbon fibre approx 30mm x 15mm, 300 mm outboard from the inboard rib. The bracket is bonded and held in place with one or two small screws. Please look for any signs of looseness. Please report any defects to BGA CTO.

Solo 2 350 and 2 350D Manufacturing Defect 15th September 2011

SOLO has issued Service Bulletin 4603-12 for the inspection of the forward carburettor housing inspection for incorrectly drilled holes filled with resin. To be carried out if power loss is experienced or within 25 operating hours or at the latest by 31 December 2011. The SB can be found at http://www.solo-germany.com/files/flug/download_dateien_de/tm_4603_12_entwurf.pdf

DG 500 Series Loose Tail Plane Location Bush 15th September 2011

Recently found on a DG505 Elan Orion: one tail plane location bush found dis-bonded and loose in tail plane spar. See photo. Owners are recommended to remove the tail plane and inspect the two location bushes for any signs of dis-bonding or cracks. The aircraft may not be flown with defects in this critical area. If defects are found please contact DG for repair instructions and advise BGA. A similar defect was previously found on a DG500/22.

September Updates 1st September 2011

The September Engineering News is available to download. TNS, airworthiness directives, inspections , AMP Manual and datasheets have also been updated.

Schempp-Hirth Ventus and Discus Turbo Sailplanes 3rd August 2011

EASA has published AD 2011-0146 for the change of daily inspection procedures and pylon replacement if cracks are found. The following types are affected - Ventus cT, Ventus 2cT, Discus bT, Discus 2T and Discus 2cT. See AD for serial number applicability and exempt aircraft. http://ad.easa.europa.eu/blob/easa_ad_2011_0146.pdf/AD_2011-0146_1

July Updates 5th July 2011

The July Engineering News is available to download. TNS, airworthiness directives and the Flight Manual revision list and TCDS links have also been updated.

Hoffmann H36 Dimona Air Brake Control Inspection 27th June 2011

EASA have published AD 2011-0110 for the inspection and protection of the air brake control torque tube on Hoffmann H36 Dimona aircraft,in accordance with MSB 36-105/1. Inspection required by end of December 2011 and repeat at 5 year intervals. See http://ad.easa.europa.eu/blob/easa_ad_2011_0110.pdf/AD_2011-0110_1 for details.

DG500 Rudder Restriction 31st May 2011 UPDATED 7th June 2011

The BGA has also received a report of a fixed trim ballast weight on a DG500/22, located on the fin rear spar in the space forward of the rudder, coming loose and partially restricting the rudder travel.

We have now completed our investigation and the earlier BGA-recommended restrictions on aerobatic flight no longer apply. However, the BGA advises that DG-500 owners should arrange to have any installed tail trim ballast weights inspected for security at the next maintenance opportunity and, if lead weights are installed in tubes mounted on the fin rear spar, consider replacement with an improved brass weight in accordance with DG drawing 5L38.

SZD-24C Foka, SZD-24-4A Foka 4, SZD-32A Foka 5 and SZD-36A Cobra 15 Sailplanes 25th May 2011

This item also refers to any sailplane with a wing attachment rigging mechanism that has no direct means to determine that the bevel bolts are fully engaged in the lug stack during rigging.

Following the AAIB recommendation made in its report into the fatal Foka 4 accident at Bicester last year, EASA has issued Safety Information Bulletin SB2011-11 “A reliable approach to rigging a sailplane”. This document, available at http://ad.easa.europa.eu/ad/2011-11 should be read by all operators and pilots of these aircraft types.  

DG500 Rudder Stops - Before Next Flight Inspection 21st May 2011

Another aircraft has been found with loose rudder stop bolts. The BGA inspection to check rudder stops for security (see below) is now raised to before next flight. The stops are quite difficult to see on the rudder control horn. Check with 10mm spanner but do not over tighten. If any stop is found loose, check that the lock nut (thin shear nut) thread has not stripped and check rudder deflections are in accordance with the maintenance manual. Warning: over tightening the lock nut may strip the thread. A low strength Thread Lock Locktite is recommended. Use low strength to allow future adjustment.

Please report any loose stops to the BGA CTO.

SZD 30 Pirat - Operational Limitations and Inspections 24th May 2011

EASA has published AD-2011-0089 for structural inspections and revised operational limitations to be complied with by end of June 2011. See AD for serial number applicability. Further information at: http://ad.easa.europa.eu/blob/easa_ad_2011_0089.pdf/AD_2011-0089_1 and http://www.szdjezow.com.pl/Biuletyny/BE_035302010eng.pdf

DG500 Rudder Stops 19th May 2011

The BGA has received a report of a rudder stop working loose and allowing the stop bolt to fall out. The consequence of this is that the rudder may over travel and restrict the elevator down travel. It is strongly recommended that operators check the rudder stops, especially prior to spin training. Please report any loose stops to the BGA CTO.

SZD 51-1 Junior BGA Mandatory Inspection 11th May 2011

BGA Mandatory Inspection 051/05/2011 issue 1 has been issued for the inspection of elevator hinges for corrosion within 20 flight hours and repeat at annual inspection. Please report findings to the BGA CTO. Details at http://www.gliding.co.uk/bgainfo/technical/inspections/051-05-2011-issue-1.pdf

Rotax 914F EnginesAirworthiness Directive 10th May 2011

EASA has published AD 2011-0082 for the identification and replacement of the fuel pressure regulator within 100 flight hours or 6 months. Details at http://ad.easa.europa.eu/blob/easa_ad_2011_0082.pdf/AD_2011-0082_2

May Updates 9th May 2011

The May Engineering News is available to download. TNS, airworthiness directives, datasheets and the Flight Manual revision list and TCDS links have also been updated.

Robin DR400 Airworthiness Directive 3rd May 2011

Emergency Airworthiness Directive AD 2011-0076 calls for the inspection and rectification of the air filter within 55 flight hours or at the next inspection (whichever is sooner) with a change to a modified type within 210 hours. Details at http://ad.easa.europa.eu/blob/easa_ad_2011_0076.pdf/AD_2011-0076_1   

Rotax 912/914 Series Airworthiness Directive 21st April 2011

EASA has published AD 2011-0067-E for replacement of magneto flywheel hub washers on Rotax 912 and 914 engines installed in, but not limited to,  AMT 200 and 300 Ximango, H36 Dimona, Grob G109, SF25 and Stemme S10 motor gliders. Compliance is required within 10 flying hours or four months. Full details are at http://ad.easa.europa.eu/blob/easa_ad_2011_0067_E.pdf/EAD_2011-0067-E_1

DG808c Airworthiness Directive 25th March 2011

Landing Gear Bolt Incorrectly Fitted. EASA has published AD 2011-0053-E: a before next flight inspection of the landing gear control bell crank bolt for correct fitment and possible damage to airbrake control rod or the flap control rod. Details at http://ad.easa.europa.eu/blob/easa_ad_2011_0053E.pdf/EAD_2011-0053-E_1

BGA ARC Initial and Refresher Training 11th March 2011

We have arranged an ARC initial and ARC refresher training course at RAF Halton on 5th April 2011, starting at 10.00.

Initial training is open to any BGA inspector who has at least seven years experience in continuing airworthiness with a minimum of three years as a BGA inspector and where it can be demonstrated there is a genuine need for additional ARC signatories in their locality.

Refresher training is open to any existing BGA ARC signatory and in particular those who have received feedback regarding ARC issues. Space is limited and must be booked by 29th March 2011 supplying vehicle details.

Click here to download application form or contact Debbie at the BGA office to book.

Exposition and Airworthiness Directives 10th March 2011

The airworthiness directives have been updated. The Airworthiness Exposition has also been updated.

March Updates 1st March 2011

The March Engineering News is available to download. TNS has also been updated, airworthiness directives will follow shortly.

AMP Manual Update 23rd February 2011

The AMP Manual has been updated with leaflet 2-14 "Customising of Maintenance Programmes and Recording of Airworthiness Directives". Click here for the AMP download page.

December Updates 24th December 2010

The January Engineering News is available to download. TNS and airworthiness directives have also been updated.

Buying and Selling a Sailplane 9th December 2010

The BGA has published a useful briefing document describing the main things to remember and actions to be taken when buying and selling a sailplane, including export and import procedures.  You can download the document here.

CEAPR DR300 and DR400 Exhaust Inspection 8th December 2010

EASA have published AD-2010-0260 for the initial and repeat inspection of the exhaust systems if equipped with Dyn' Aviation exhaust systems. The AD supercedes AD-2010-0151-E.

Schempp-Hirth Ventus 2cT and Discus 2T & 2cT "Turbo" Pylon Cracks 2nd December 2010

There have been several instances of pylons cracking on Ventus 2cT sailplanes. We understand that these are aircraft, subject to AD 2006-0227-E, that passed the inspection and where special spaces were installed in accordance with TN 825-38. No reports of Discus 2T or 2cT pylon failures to date.

It is strongly recommended that owners regularly inspect the pylon in accordance TN 825-38 or TN 863-13 action 1 as appropriate. It is essential that the pylon is clean for the inspection.

There is an on-going investigation. Please report any cracks immediately to the BGA CTO.

Click here for a photo of typical pylon crack. (courtesy of Andy Jessett)

November Updates 4th November 2010

The November Engineering News is available to download. TNS, AMP Manual and airworthiness directives have also been updated.

LET L13 Blanik - Grounding Notice 6th September 2010

September Updates 3rd September 2010

The September Engineering News is available to download. TNS and airworthiness directives have also been updated.

Rigging Safety Alert 3rd September 2010

The BGA has issued a safety alert concerning rigging of SZD Foka, Cobra, Bocian, Jaskolka, Schempp-Hirth SHK & Austria series and any other sailplane with an expanding pin/cone main rigging pin. Owners and operators should read the Safety Alert identifying a possible safety issue with the rigging procedure.

LET L13 Blanik Wing Spar Inspection and Aerobatic Manoeuvre Prohibition 2nd August 2010 UPDATED

EASA have issued AD 2020-0160-E (superseding AD 2010-0122-E and AD 2010-0119-E). Gliders that fall outside the operational life limitations as required by SB L13/109a and gliders where the records are incomplete - no further flights are permitted.

For more information and clarification please contact LET Aircraft Industries direct.

Office move 30th July 2010

Due to the BGA office move, there is a special edition of the Engineering News which contains important information about ARC Renewals during the office move. Click here to read the newsletter.

ASK 21 Trim Push Rod Inspection (GFA Alert) 27th July 2010

BGA Information Only. The Gliding Federation of Australia have published an airworthiness alert A2010-1 for the inspection of the trim control rod under the rear seat for bending and possible foul of aileron control rod. The importance of diligent daily inspections to detect control restrictions is highlighted.

Comment from one of our professionals; changing the trim push rod is not possible without first removing the rear rudder pedal assembly. It may be possible to slightly bend the rod around the pedals and this may initiate the problem. Once a tube is bent it is severely weakened, additionally the control rods in the area are vulnerable in the case of a nose wheel push up (common occurrence)

Robin DR 300 & DR 400 Exhaust Inspection 25th July 2010

EASA have published AD 2010-0151-E for the before next flight inspection of DR300 and DR400 exhaust systems and a 12 flight hour re-inspect for aircraft modified with minor change MD09K0012.

July Updates 3rd July 2010

The July Engineering News is available to download. TNS and airworthiness directives have also been updated.

ZSJ PW6U Tail Plane Attachment Fitting Inspection 9th June 2010

EASA have issued AD 2010-0108-E for a before flight and repetitive inspection of the PW6U aft tail plane attachment fitting. This airworthiness directive supersedes and cancels BGA inspection 048-01-2010.

Centrair 101 Pegase Rudder Bar Inspection 27th May 2010

EASA have issued AD 2010-0099 for the inspection of the rudder bar locking adjustment tube to determine type fitted and for damage by 09 July 2010. In 1984 a reinforced tube was introduced into production and optional on older aircraft, this is now a mandatory fitment. If non reinforced tube is fitted and not damaged it must be replaced with a reinforced type at next annual inspection but no later than 12 months, if damaged, it must be replaced before further flight. For further details see AD.

Swift S-1 Control Column Inspection 27th May 2010

EASA have issued AD 2010-0094-E for the before next flight inspection of the control column for cracks or damage. For further details see AD.

May Updates 11th May 2010

The May Engineering News is available to download. TNS, airworthiness directives and inspections have also been updated.

Glasflugal Libelle 201 Aileron Drive 21st April 2010

The BGA strongly recommends that the aileron drive torque tube be inspected prior to next flight in accordance with Technical Note 201-33 due to an instance where an unmodified aileron drive torque tube failed.

If a modified drive is installed then there is no further action other than normal annual routine inspections.

If an unmodified drive is installed it is recommended that the drive torque tube is inspected at each daily inspection.

If a cracked torque tube is found it must be replaced prior to next flight.

A torch and inspection mirror are required for the inspection. Further information will follow advising on terminating action compliance.

Grob Astir Sailplanes with Water Ballast - Inspection 8th April 2010

EASA have issued AD 2010-0053 for the inspection of the water ballast hose connector for security. Failure of the connector may cause water to drain into fuselage or interfere with flight controls. Initial inspection must be completed before 30th May 2010 and repeated annually. See MSB-GROB-003 for applicability and inspection details (This MSB can be found in the General section of the Grob SB web site).

The current AD specifies repeat inspection at Airworthiness Review, this will shortly be amended to read at Annual Inspection.

BGA Airworthiness Web Site Updates 18th March 2010

The BGA Airworthiness Exposition has been updated to Amendment 02 and now includes a master list revision list. The BGA AMP manual has been updated; AMP 2-5 and AMP 2-11 have been revised together with BGA 202 and BGA 276 forms. Contacts list of ARC signatories by region has been updated.

Announcing Revised ARC Renewal Procedure 18th March 2010

The requirement to send a copy of the BGA 267 GMS Report for EASA aircraft at time of ARC renewal has been withdrawn. Inspectors must still continue to complete a 267 as this form records the annual inspection and is an essential part of the BGA GMS maintenance programme, the 267 must be filed in the aircraft maintenance records as before. For EASA motor gliders and Tugs the BGA 202 has been withdrawn. The BGA 267 and BGA 202 are sent to the BGA only for Annex II aircraft as before at C of A renewal.

For all ARC renewals we now only require a BGA 276, Signed copy of the ARC and fee.

As an added service to owners and inspectors there is now a section on the BGA 276 for you to complete an email address if you would like acknowledgement of receipt by BGA. Please note the email address must be typed or printed clearly if you want an answer.

Schempp-Hirth Ventus 2cM, Nimbus 4DM, Nimbus 4M 15th March 2010

EASA have issued AD 2010-0039-E for the before next flight and repetitive inspections of certain starter ring gears due to cracks detected from the lightening holes. Initial inspection before flight by BGA inspector and if no fault found, the repetitive daily inspection may be carried out under pilot/owner maintenance previsions until the starter ring gear is replaced. See AD for aircraft serial number applicability.

Super Blanik L32 Elevator Hinge Inspection 9th March 2010

EASA have issued AD 2010-0037-E for the before next flight inspection of the elevator hinges (Published as SB L32/052a in TNS 1-2010) and repeat 1000 hour inspections. Please note the before flight and 1000 hour inspections must be certified by a BGA inspector.

March Updates 5th March 2010

The March Engineering News is available to download. TNS and airworthiness directives have also been updated.

Scheibe SF25C and SF25E Inspection of Tubular Rivets 26th January 2010

EASA have issued AD 2010-0011-E for the before next flight inspection of tubular rivets used on the aileron hinges and tail plane connecting fittings and immediate replacement if brass tubular rivets found (Steel tubular rivets are OK). Please see AD for aircraft serial number applicability and Scheibe SB 653-64 for instructions and details of how to obtain a repair kit if required.

Thinback T104 and Slimpack T204 Parachutes 22nd January 2010

EASA have issued AD 2010-0009-E prohibiting use until inspected and reworked, certain emergency parachutes manufactured by Fallschirmbau Buchsein/Hermesdorf GbR - Thinback T104 and Slimpack T204, due to ripcord cable faults that may cause parachute not to deploy. Please see AD and Safety Bulletin 1/2010 for further information and applicable parachute serial numbers.

PW5 and PW6 Tail plane Aft Attach Fitting - Inspection 22nd January 2010

The BGA have issued Inspection 048/01/2010 issue 1 for the before next flight precautionary inspection of tail plane aft attachment fittings. Further action may follow depending on the conclusion of an ongoing investigation.

MT Propeller Blade Leading Edge Protection Inspection 22nd January 2010

EASA have revised the inspection requirements by now allowing the repetitive pre flight (DI) part of the inspection to be carried out and certified under the provisions of Pilot/Owner maintenance. See AD 2006-0345R1 for further details.

Proposed EASA Airworthiness Directive - Gadringer Gurte 18th January 2010

EASA has issued a Proposed Airworthiness Directive (PAD 10-010).   Gadringer Gurte GMBH have supplied cockpit harnesses to many glider owners and repair both their and other manufacturers’ harnesses. We believe that this proposed AD does not apply to harnesses manufactured and released by Gadringer, but to ones from other manufacturers that have been repaired by Gadringer and the other companies named in the AD. The BGA is investigating this PAD and will respond to the proposed AD before the closing date of 10th February 2010 and will report its views here.

December Updates 22nd December 2009

The January Engineering News is available to download. TNS, airworthiness directives and Inspections have also been updated.

News Affecting Certain Gliders Supported by DG Flugzeugbau 21st December 2009 (Updated 29th December 2009)

The BGA is aware of some owners concerns over recent comments on the DG Flugzeugbau website noting a requirement for annual support contracts with DG for certain glider types where the Type Certificate is held by DG. The latest detail is on the DG web site.

The BGA understands and expects that any company will charge for supplied goods and services but does not agree with requiring someone to contract to and pay for a service that they do not need and/or is not accessible to them. . The BGA is working with a number of key stakeholders to understand the implications of the proposed change by this leading TC holder. The BGA Maintenance Organisation does not intend to change any of its requirements affecting ARC issue unless the CAA directs otherwise. Meanwhile, the BGA is advising concerned owners to contact DG direct. The BGA will keep owners aware of any developments.

Modifications to Gliders 12th December 2009

AMP 3-3 has been revised to clarify the Annex Ii and EASA modification procedures. Please note: the procedure described in AMP 3-3 is for Annex II gliders only.

BGA Airworthiness Organisation 2nd December 2009

Many inspectors will already be aware of proposed changes to the BGA Airworthiness Organisation as mentioned in recent seminars. As from 1st January 2010 the revised organisational procedures become live. A key development is that BGA inspectors are only authorised to certify and are only insured to work on EASA aircraft within the BGA Airworthiness Organisation. Owners of aircraft within the BGA Airworthiness Organisation are able demonstrate to inspectors that their aircraft are in the system.

For the vast majority of aircraft, owners and inspectors this means no change at all. If the last ARC was renewed using the BGA CAMO then the aircraft is in, no problem. The only issues come if the ARC was not issued using the BGA CAMO or the aircraft has a BGA ARC expired more than 3 months ago. In that case, there is a straightforward administration process for bringing the aircraft into the BGA Airworthiness Organisation.

Annex II aircraft are not affected in any way.

For more details see December 09/January 10 issue of Sailplane & Gliding and visit the Part M page here.

Click here for a very useful Q & A section that should answer all your questions. More detailed guidance for inspectors will accompany the January 2010 issue of Engineering News.

Halon Fire Extinguishers 26th November 2009

EASA have issued AD 2009-0251-E for hand held Halon 1211 fire extinguishers manufactured by Fire Fighting Enterprises Ltd. that may be stowed in aircraft and may be filled with contaminated Halon gas. If you have a FFE fire extinguisher with a part number starting with "BA" please see AD for affected product list.

Chief Engineer / ARC Signatory Training Seminar 6th November 2009

A small seminar has been arranged for Sunday 13th December 2009 at Lasham Gliding Society for inspectors who wish to become ARC signatories and where there is a genuine geographical need. The minimum requirements; you must have held a BGA Inspector authorisation for at least 3 years and have another 4 years experience in aircraft continued airworthiness (7 years total). Please note space is limited and this will probably be the last seminar for some time.

Please apply to CTO - cto@gliding.co.uk indicating where the requirement is located.

November Updates 5th November 2009

The November 2009 Engineering News is available to download. TNS, airworthiness directives and AMP Manual have also been updated.

DG 500MB, DG 808C & DG 800B Starter Ring Gear Inspection 3rd November 2009

EASA have issued AD 2009-0239-E for the before next flight inspection of starter ring gear amended to include DG 808C motor gliders. AD 2009-0225-E is superseded but the inspection requirements remain unchanged. To remain in compliance on aircraft already inspected a log book entry is required stating compliance with AD 2009-0239-E due to previous inspection. Aircraft not previously inspected (DG 808C) must be inspected before next flight with the appropriate action being taken.

DG500MB and DG800B Starter Ring Gear inspection 23th October 2009

EASA have published a before next flight inspection of DG500 and DG800 Solo engine starter ring gears ref; AD 2009-0225-E. This inspection supersedes AD 2009-0169-E published in July 2009. For full details please see AD.

Transition Update 12th October 2009

Glider owners wishing to transition gliders to EASA C of A and ARC after 28th September 2009 please note new procedures, forms and fees. Please visit "EASA C of A Transition" for the latest information.

Chief Engineer / ARC Signatory Training Seminar 1st October 2009

A small seminar has been arranged for 21 November 2009 at Bowland Forest Gliding Club for inspectors who wish to become ARC signatories and where there is a genuine geographical need. The minimum requirements; you must have held a BGA Inspector authorisation for at least 3 years and have another 4 years experience in aircraft continued airworthiness (7 years total).

Please apply to CTO - cto@gliding.co.uk indicating where the requirement is located.

BGA Maintenance and Complex Maintenance Task Approval 30th September 2009

Now that almost all the UK EASA glider fleet has made the transition to a non-expiring EASA Certificate of Airworthiness, refreshed each year by the renewal of an Airworthiness Review Certificate, owners and maintainers may find it helpful to have a brief update on the rationale behind current BGA maintenance policy. Follow this link for a document describing this rationale and giving information about the importance of our newly acquired Part M Subpart F approval to owners and inspectors.

This Part M Subpart F approval permits BGA inspectors to operate within the revised and Part M compliant BGA airworthiness organisation and means that we can continue to employ the system that we have enjoyed and benefited from over many years.

Complex Maintenance Tasks on BGA Aircraft 22nd September 2009

With immediate effect any complex maintenance task carried out and due to be certified after 28th September 2009 on BGA aircraft will require prior authorisation unless you hold BGA part M List 1 site approval.

Please see AMP 2-13 for guidance on what constitutes a complex task and how to apply using form BGA 277.

There will be an administration charge for this authorisation.

Foreign Registered Gliders with Permit to Fly 9th September 2009

The CAA has advised us that gliders with temporary EU registrations (usually German or French) flying on an EASA Permit to Fly in the UK may not be legal unless they are fully registered in the country that issued the permit. This usually applies to new design gliders where the manufacturer has issued a temporary registration and an EASA Permit to Fly whilst the glider is in the final stages of type certification. Please see CAA advice on this and how to apply for an exemption if needed.

ARC Renewal Interim Process Ends 3rd September 2009

The interim process for BGA ARC renewals has now come to an end and the BGA CAMO will now only be able to accept renewed Airworthiness Review Certificates (ARC) from authorised BGA inspectors who are also ARC signatories.

To find a BGA ARC signatory please visit the Airworthiness Contacts page on the BGA web site where you will find BGA ARC signatories by region. You will also find details of your Regional Technical Officer and gliding clubs.

Grob Twin Astir & G103 Twin 3 Airworthiness Directive 2nd September 2009

The LBA have published AD-D-2008-231 and AD-D-2008-232 for the inspection of Air Brake control system for cracked bolts. Grob MSB 315-76/1 and MSB 869-27/1 apply. This AD was not published by EASA but is applicable to affected UK aircraft.

August Updates 17th August 2009

The August 2009 Engineering News is available to download. TNS, airworthiness directives and datasheets have also been updated.

EASA AD's and Form 267 correction 5th August 2009

Form BGA 267 (AMP 1-3 appendix 1) has been corrected, please use latest version.

DG-100 series sailplanes. Before next flight inspection & replacement within 5 months of elevator stand bearing in accordance with EASA AD 2009-0163-E.

DG-100 and DG-200 series sailplanes. Before next flight inspection & replacement within 5 months of control column rod end in accordance with EASA AD 2009-0167-E.

DG-500MB and DG-800 B powered sailplanes. Before next flight and every DI inspection or optional replacement of zinc coated starter ring gear in accordance with EASA AD 2009-0169-E.

Airworthiness Directives – Notification 5th August 2008

Aircraft owners (including glider owners) are responsible for ensuring that their aircraft remain airworthy. This includes staying up to date with Airworthiness Directives. The BGA recommends that owners subscribe to the CAA airworthiness newsletter Email service to receive Emergency Airworthiness Directives (EADs) at http://www.caa.co.uk/subscriptions. We recommend ticking the Notify box and including the Emergency Airworthiness Directives, Aviation Maintenance and Aviation Safety categories in your preferences.

The CAA maintains a list of EADs at http://www.caa.co.uk/eads and EASA also publishes Airworthiness Directives at http://ad.easa.europa.eu/. The very comprehensive EASA web site contains all EASA ADs. There is a filtering system and a free subscription notification service.

The BGA Airworthiness organisation provides important guidance and advice for all BGA owners of EASA and Annex 2 gliders, motor gliders and tugs. This support will continue to grow and we recommend that all owners subscribe to receive free BGA  airworthiness Email alerts at https://www.gliding.co.uk/subscriptions. Owners without internet access should discuss how they can access relevant airworthiness information with their club Technical Officer or with a BGA inspector.

BGA Cs of A and Transitioned Gliders 20th July 2009

As the transition to EASA C of A nears conclusion, it is possible that some owners will have a glider with both an EASA C of A and a BGA C of A document with an expiry date towards late 2009. Owners of gliders that have transitioned are reminded that a BGA C of A is not valid on a glider that holds an EASA C of A. A glider with an EASA C of A must have a valid ARC to be airworthy. A copy of the ARC should be held with the glider. BGA Cs of A are only currently valid for BGA gliders that have not transitioned, including Annex 2 types. After September 2009, the BGA C of A will only apply to Annex 2 types. If an owner or operator is unsure whether or not a particular glider has been transitioned to an EASA C of A, they can use the CAA G-INFO website. Advice regarding transition, ARCs and more is available in this section of the web site.

Part 21 and EASA Gliders 15th July 2009

Owners, operators and inspectors are reminded that once a glider has been transitioned into Part 21 and therefore holds an EASA C of A, the manufacturer’s design or the glider’s declared transitioned modification state cannot be materially changed or added to, including through maintenance and repair activity, without formal EASA modification action by way of a manufacturer’s maintenance instruction, TN (technical note), SB (service bulletin), or an EASA approved modification. The BGA is developing guidance material to assist owners, operators and inspectors with the maintenance of instrument panel installations etc which will also include guidance regarding modification action where required. As soon as that information is available, it will be published and made accessible to all.

Binder ASH 25 EB 28 Airworthiness Directive 26th June 2009

EASA have published AD 2009-0131 for inspection of Aileron hinge bonding. Inspection before 21 July 2009. Please see AD for details http://ad.easa.europa.eu/blob/easa_ad_2009_0131.pdf/AD_2009-0131_1

Scheibe Mu13E Bergefalke series, SF25 series, SF26A, SF28A Airworthiness Directive 26th June 2009

EASA have published AD 2009-0132 for inspection of Elevator tab drive arm at next scheduled maintenance check and repeat annually. Please see AD for details http://ad.easa.europa.eu/blob/easa_ad_2009_0132.pdf/AD_2009-0132_1

AMP Leaflet 2-11 update 26th June 2009

AMP 2-11 ARC renewal process has been corrected and updated. Please note documents to be forwarded to BGA with renewed ARC.

June Updates 5th June 2009

The May 2009 Engineering News is available to download. TNS, airworthiness directives and the AMP Manual have also been updated.

BGA Chief Engineer / ARC Signatory Training Seminars updated 5th June 2009

One additional seminar has been arranged for inspectors at Ulster Gliding Club, Northern Ireland on 8 July 2009. Priority will be given to UGC, IOM and IGA inspectors. Mainland inspectors are welcome to attend but space is limited. Further seminars will now only be available on a geographical need basis where a shortage of ARC signatories is demonstrated. Contact your Regional Technical Officer for advice.

For details and how to book please see the booking form.

ARC Renewal Extension of Interim Procedure 24th April 2009

As part of the completion of the EASA transition process, the interim ARC renewal process has been extended with a final end date of 28 September 2009. See revised AMP leaflet 2-11.

April Updates 3rd April 2009

The March 2009 Engineering News is available to download. TNS and airworthiness directives have also been updated.

EASA Glider ARC Renewal 31st March 2009

Please read carefully;

• To fly legally, an EASA glider that holds an EASA C of A (an EASA C of A is non-expiring) must also hold a valid Airworthiness Review Certificate (ARC) and have up to date maintenance in accordance with the glider maintenance programme (in most cases, that boils down to an annual inspection within the last 12 months)
• EASA gliders without an EASA C of A and ARC are not eligible for ARC renewal
• The ARC renewal process for eligible gliders is described here. The ARC renewal fee for a glider is £95.

Further advice to owners;

• If your EASA glider does not hold an EASA C of A and ARC (for example your transition application is in the BGA and CAA 'system'), to fly legally your glider must have a current BGA C of A. If you want to fly your EASA glider but your glider has neither an EASA C of A and ARC nor a valid BGA C of A, please talk to your friendly BGA inspector as soon as possible.
• The transition period ends 1 May 09. Any EASA glider that has not had a transition application submitted to the BGA by that date will not be eligible to fly even if it has a BGA C of A
• Annex 2 gliders (ie non-EASA types) are only required to hold a valid BGA C of A as per the established BGA processes
• More guidance regarding Part M, including various documents, is available here

BGA Chief Engineer / ARC Signatory Training Seminars updated 27th February 2009

New seminar venue added - Wolds Gliding Club 25 April 2009.

The first round of BGA Chief Engineer / ARC signatory training is now arranged. For details and how to book please see booking form. This training is for BGA inspectors to upgrade to Chief Engineer and become an ARC signatory, this will allow you to carry out airworthiness reviews and issue the ARC directly on behalf of the BGA CAMO.

Please note that the seminars at Husbands Bosworth, Lasham and Parham are now fully booked, although places are still available at Portmoak and Pocklington. More seminars planned very soon.

AMP Manual Update 5th February 2009

AMP manual forms have been updated, including BGA 267 GMS Report and BGA 276 Airworthiness Review Checklist updates with Part M release to service.

ARC Renewal, Pilot Maintenance & Fees Update 7th January 2009

In the new 'Part M' section on the BGA web site Airworthiness section, a new guidance leaflet AMP 2-11 has been published. The aim of this leaflet is to provide guidance for BGA inspectors and information for owners on how to carry out an airworthiness review and thereby renewal of the ARC. Details include;

• The interim procedure currently in use
• Who may certify the review
• The new BGA Form 276 Airworthiness Review Checklist

Airworthiness fees have also been revised to take into account the CAA fee that the BGA is required to pay for each ARC renewal. The BGA is continuing to limit its fees to the minimum possible.

AMP 2-1 Pilot/Owner maintenance has also been updated.

Part M 24th December 2008

A Part M page has been added to this Airworthiness section.

December Updates 24th December 2008

The January 2009 Engineering News is available to download. TNS has also been updated.

ARC Dating Protocol 17th December 2008

Further to the the information in the last BGA Newsletter, you can find additional guidance & information on the ARC dating protocol and what this means for owners and inspectors here.

Part M and ARCs 10th December 2008

The BGA is currently working with the CAA to fine tune the details of the BGA ARC renewal process under Part M. The BGA will be supplying detailed advice to owners and inspectors during December. Please stay tuned to this website. Meanwhile, the transition recommendations continue to be fed to the CAA for EASA C of A and initial ARC issue in time for the application of Part M to all EASA gliders by May 2009.

Part M - update 13th November 2008

EASA has published the long awaited revision to Part M as regulation EC 1056/2008 amending 2042/2003. This is a complex revision to Part M developed as a result of campaigning by the BGA and many others within Europe and could have far reaching and helpful changes for gliding and continued airworthiness.  The BGA is currently waiting for the CAA to review the amended regulation and to interpret how it will affect General Aviation and gliding in particular. We will publish further information on the BGA web site as soon as it is available. Meanwhile, any glider maintenance organisation seeking its own Part M subpart F approval is advised to hold back until further information is available, or alternatively contact the CAA regional office who is dealing with their subpart F approval application.

November Updates 7th November 2008

The November 2008 Engineering News is available to download. TNS and airworthiness directives have also been updated.

EASA C of A Postponement and Transition Refresh - update 31st October 2008

Gliders that were transitioned in the latter part of 2007 are eligible for EASA C of A and ARC postponement. This is because if the ARC is issued it will expire before there is an approved process to renew it. The postponement also applies to gliders where there is a certification or registration query. The postponement requires a simple "Transition Refresh" to be carried out as part of a normal BGA C of A renewal. We have written to all the owners of gliders affected with full details and refresh form, however we have been asked to make the form (BGA 275) available to download. There is no refresh fee, all you need to pay is the normal BGA C of A renewal fee (currently £75)

Please note: the transition refresh is only applicable to gliders on the applicability list and is only completed at time of BGA C of A renewal together with the BGA 267.

Slingsby Aircraft Flight Manuals/Pilot Notes updated 16th October 2008

SAS Gliders Only. Please note; gliders certified against an Specific Airworthiness Specification (SAS), (Slingsby Kestrel, Dart & T53B), do not normally require a flight manual/pilot notes for transition or ARC renewal. However, there may be some additional maintenance or operational data within the flight manual, where available, that may be useful. This note is advising you of the availability of the information.

Flight manuals/pilot notes are available for EASA Slingsby Gliders and Motor Gliders. Vega, Kestrel, Dart, T53b, T61A to G (T61A manual plus supplements). An up to date and complete manual will be required for transition to EASA C of A and for ARC renewal. To obtain copies please contact Slingsby Advanced Composites on 01751 432474.

Motor Gliders Only;
Slingsby motor gliders previously issued with a C of A with conditions, now require a flight manual or pilot notes and a DFMS must be completed at time of C of A/ARC renewal. A printer friendly version of the DFMS (Declaration of Flight Manual Standard) can be downloaded from the G-INFO database on the CAA web site here. Send the completed and signed DFMS with the renewal request to BGA.

BGA Airworthiness Fees 13th October 2008

Please note, with effect from 1st October 2008, BGA Airworthiness fees have been revised to reflect additional costs for EASA aircraft ARC renewal. Please visit the fees section for details.

To avoid any delay in processing your ARC renewal please ensure the application is supported with the correct fee.

Stemme S10 and S10-V Engine Fuel & Control AD 13th October 2008

EASA have issued AD 2008-0186-E for the before every flight inspection of fuel lines until replaced.
Fuel lines must be replaced within 25 days. See AD for full details.

BGA Inspector Renewal 30th September 2008

BGA Inspectors are reminded that the BGA Inspector Authorisation expires today. To maintain validity, please forward your renewal application to the BGA office without delay.

Due to some important Part M information we need to include with your Inspector Authorisation Certificate, there will be a short delay in receiving your renewed certificate. 

Provided you have applied for renewal, we are allowing 1 month extension of your pre existing authorisation to 30 October 2008 in accordance with approved procedures.

SPEKON Parachutes 19th September 2008

EASA have published Airworthiness Directive 2008-0174 identifying a fault in SPEKON RE-5L emergency parachutes manufactured between 21 April 2008 and 21 August 2008. See AD for serial number details and compliance information.

September Updates 12th September 2008

The September 2008 Engineering News is available to download. TNS and airworthiness directives have also been updated.

Final Inspector Seminar 19th August 2008

There are still a few places left on the final inspector seminar to be held on 30 August 2008 at the Gliding Centre, Husbands Bosworth. The seminar is FREE although you need to pay for own lunch. Contact debbie@gliding.co.uk or telephone the BGA office to book.   This is the final notification - any BGA Inspector who has not attended a BGA continuation training seminar (the first one was 21 September 2007) will be unable to renew their BGA Inspector Authorisation in September 2008 and thus, unable to certify any glider with a BGA C of A or any aircraft aircraft within the BGA Part M approval.

Motor Glider and Tug ARC Renewal 1st August 2008  

The first motor glider and tug Airworthiness Review Certificates (ARC) will be becoming due for renewal from 28th September onwards.  We appreciate that some owners may wish to take advantage of the 90 day anticipation period.  However, as there is currently no CAA process available for the renewal of the ARC, full anticipation is not available. We have been advised that the process will be in place by the end of August.  Details will be published when known.

July Updates 9th July 2008

The July 2008 Engineering News is available to download. TNS and airworthiness directives have also been updated.

Final Inspector Seminar 27th June 2008

An additional seminar for BGA inspectors to introduce the new and revised procedures for the continuing airworthiness of gliders, motor gliders and tugs under the BGA umbrella has been arranged for Saturday 30 August 2008 at Husbands Bosworth.  This will be the last such seminar to be held.  Any BGA inspector who has not attended one of these seminars will not be able to renew their inspector authorisation in September 2008.  Please book using the form available here and email to Debbie Carr.

EASA Transition Update 29th May 2008

The BGA process for transition of EASA gliders to EASA C of A in time for the 28 September 2008 deadline is working well. Many thanks to the inspectors and owners involved. The CAA part of the process is currently stalled pending receipt of the expected written formal approval from the European political system. To ensure that owners are unaffected by the CAA delay, the BGA has negotiated a contingency plan with the DfT and the CAA. That contingency plan is underway.

 All the transitions currently received will have their BGA C of A extended to full validity. Owners will be receiving a replacement BGA C of A in due course. Due to the high number this may take a month or two (if you have not received the replacement C of A by August, please contact the BGA office).  All transitions will from now result in the issue of a full validity BGA C of A.  A BGA C of A that expires after 28 September 2008 will be renewed in the normal way. Inspectors will receive guidance on what will be required to ensure that the already submitted transition package remains valid. Another transition will not be required.  Please note that this is a contingency process that in fact may not be required. As usual, the BGA is taking a proactive approach on behalf of pilots and owners.

May Newsletter 23rd May 2008

The May 2008 Newsletter has been updated.

May Updates 8th May 2008

The May 2008 Engineering News is available to download. TNS and the motor-glider TCDS have also been updated. Compendium updates will be published soon.

Motor Glider and Tug C of A renewal process has changed 28th March 2008

All new applications for motor glider and tug C of A renewals using the BGA should follow the new procedure. You can download a quick guide here. BGA AMP manual leaflet 2-5 and C of A renewal forms have been updated. The New BGA 202 form is available as PDF or Word document.

EASA Transition Documents & Downloads 28th March 2008

Glider flight manual and TCDS list has been updated, a new Motor glider TCDS list has been published.

DG1000 ALL VARIANTS including "T" 19th March 2008

EASA have revised the elevator crank pivot inspection and modification AD-2007-0316-R1-E.

SN Centrair SNC-34 (Alliance 34) 19th March 2008

EASA have issued AD-2008-0057-E for the inspection of the wing rook ball joints and aerobatics prohibited.

Stemme S10-VT Fuel System 12th March 2008

EASA have just issued AD 2008-0053-E for the inspection and replacement of fuel connectors and single ear clamps.
http://ad.easa.europa.eu/blob/easa_ad_2008_0053_E.pdf/EAD_2008-0053-E_1

March Updates 11th March 2008

The March 2008 Engineering News is available to download. EASA transition forms and TNS have also been updated. Compendium updates will be published soon.

BGA Inspector Seminars - Update 11th March 2008

Space available - RAF Halton 5 April 2008 (booked places only, no turn up on spec). The booking form is available by clicking here.

Further seminars have been arranged for:

Ulster Gliding Club - 19 April 2008
The Gliding Centre, Hus Bos - 7 June 2008
Lasham - 27 June 2008

Please note: Lasham will probably be the past seminar in this series, inspectors who have not attended a seminar will be unable to renew their BGA inspector authorisation in September 2008.

Transition Flight Manual and TCDS 21st January 2008

The Transition Flight Manual and TCDS list has been updated. Please see updated page in EASA C of A Transition, Documents and Downloads.

January Updates 4th January 2008

The January 2008 Engineering News is available to download. Airworthiness directives, datasheets and TNS have also been updated.

DG1000 Control inspections 4th January 2008

DG 1000 all models up to serial number 10-109. EASA have published a before flight inspection of the elevator bell crank pivot bolt and air brake control hook. Modification before 30 March 2008. Click here for Airworthiness Directive 2007-0316-E.

Stemme S10-VT Fuel connector inspection 4th January 2008

EASA have published a before flight, daily inspection of the fuel system connectors. Replacement of plastic connectors before 31 March 2008 or next maintenance check. Click here for Airworthiness Directive 2007-0315-E.

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