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Assuming gfa is required, and ad is required, and beginning date after Saturday, 15 August 2015, and ending date before Monday, 24 August 2015, the following results were found.

  • GFA AD 678 Issue 1

    INCREASED RISK OF FLUTTER OF THE TAILPLANE AND DEGRADED SECURITY OF THE TAILPLANE ATTACHMENT CAUSED BY LOOSE BOLTS IN THE TAILPLANE ATTACHMENT BRACKET ASSEMBLY AND THE TAILPLANE CONTROL HORN Applicable to all Schempp-Hirth types/models with all-flying...

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1586-gfa-ad-678-issue-1&category_slug=gfa-ad-601-700&Itemid=132

  • GFA AD 680 issue 1

    EASA APPROVED MAJOR CHANGE – Life Extension from 2000 to 4000 hrs including additional checks and mandatory 300 hr/ 36 month inspection and introduces Operational Limitations through Flight Manual, Maintenance Manual and Cockpit Placarding amendments....

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1588-gfa-ad-680-issue-1&category_slug=gfa-ad-601-700&Itemid=132

  • Gfa ad 679 Issue 1

    HORIZONTAL STABILIZER REAR SPAR INSPECTION Non-compliance with this Service Bulletin may result in undetected crack(s) in the Horizontal Stabilizer Rear Spar, which could result in structural failure of the Horizontal Stabilizer. Barry Aviation Service...

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1587-gfa-ad-679-issue-1&category_slug=gfa-ad-601-700&Itemid=132

  • Gfa ad 673 Cancelled 2018.09.12

    FLIGHT CONTROLS –ELEVATOR CONTROL ROD IN VERTICAL FIN – INSPECTION / REPLACEMENT CANCELLED Refer EASA AD 2011-0213 A broken elevator control rod in the vertical fin on a Kestrel sailplane has been reported. The technical investigation revealed that...

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1581-gfa-ad-673-issue-1&category_slug=gfa-ad-601-700&Itemid=132

  • Gfa ad 676 Cancelled 2018.09.12

    FUSELAGE – CENTRE OF GRAVITY (CG) TOW HOOK MOUNTING BULKHEAD – INSPECTION / REINFORCEMENT CANCELLED Refer EASA AD 2011-0209 Occurrence of damage of the bulkhead of CG tow hook and its glued joints to fuselage shell was reported. Investigation concluded...

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1584-gfa-ad-676-issue-1&category_slug=gfa-ad-601-700&Itemid=132

  • Gfa ad 668 Cancelled 2018.09.14

    IN-FLIGHT LOSS OF PROPELLER AND PULLEY WHEEL FROM THE ENGINE OF A GROB G103 C TWIN III POWERED SAILPLANE CANCELLED Refer EASA AD 2010-0107 Grob Aircraft AG suspects that the possible reasons for this loss can be due to an incorrect propeller track (the...

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1576-gfa-ad-668-issue-1&category_slug=gfa-ad-601-700&Itemid=132

  • Gfa ad 665 Cancelled 2018-09-14

    WATER BALLAST SYSTEM FIN TANK VALVE, SPRING REPLACEMENT CANCELLED Refer EASA AD 2011-0009 Stress corrosion has been found in the zinc plated compression springs removed from the fin ballast tank valve, installed on an LS10-s sailplane. The...

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1574-gfa-ad-665-issue-1&category_slug=gfa-ad-601-700&Itemid=132

  • Gfa ad 669 Cancelled 2018.09.13

    ENGINE FUEL AND CONTROL – FUEL PRESSURE REGULATOR – IDENTIFICATION / REPLACEMENT CANCELLED Refer EASA AD 2011-0082 Isolated manufacturing deviations have been reportedly found on the threads of a certain batch of Fuel pressure Regulators, Part Number...

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1577-gfa-ad-669-issue-1&category_slug=gfa-ad-601-700&Itemid=132

  • Gfa ad 670 Cancelled 2018.09.13

    IGNITION – MAGNETO FLYWHEEL HUB WASHER – REPLACEMENT CANCELLED Refer EASA AD 2011-0067-E During a production process review, a deviation in hardening of certain Part Number (P/N) 944072 washers has been detected, which exceeds the hardness of the...

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1578-gfa-ad-670-issue-1&category_slug=gfa-ad-601-700&Itemid=132

  • Gfa ad 671 Cancelled 2018.09.13

    FLIGHT CONTROLS – AIR BRAKE CONTROL SYSTEM TORSION TUBE – TEST / INSPECTION / PROTECTION / REPLACEMENT CANCELLED Refer EASA AD 2011-0110 A report has been received of a failed air brake control system torsion tube on a Diamond (formerly Hoffmann) H 36...

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1579-gfa-ad-671-issue-1&category_slug=gfa-ad-601-700&Itemid=132

  • Gfa ad 672 Cancelled 2018.09.13

    NACELLES / PYLONS – ENGINE PYLON – INSPECTION / REPLACEMENT CANCELLED Refer EASA AD 2011-0146 Ventus cT, Ventus-2cT, Discus bT, Discus-2T, Discus-2cT powered sailplanes except those on which a new engine pylon, part number (PN) M03RT814 with modified...

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1580-gfa-ad-672-issue-1&category_slug=gfa-ad-601-700&Itemid=132

  • GFA AD 677 Cancelled 2018.09.12

    EQUIPMENT AND FURNISHINGS – SECURING ROPE FOR HEADREST OF REAR SEAT – INSPECTION / READJUSTMENT / MODIFICATION CANCELLED Refer EASA AD 2011-0191 DG-500/22 ELAN, DG-500 ELAN Trainer, DG-500/20 ELAN and DG-500 ELAN ORION sailplanes, all serial numbers,...

    http://www.doc.glidingaustralia.org/index.php?option=com_docman&view=document&alias=1585-gfa-ad-677-issue-1&category_slug=gfa-ad-601-700&Itemid=132

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