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Summary of Airworthiness Directives 38144 Braunschweig G E R M a N Y Published by Luftfahrt-Bundesamt / Germany Tel Luftfahrt-Bundesamt Airworthiness Directive Section Summary of Airworthiness Directives 38144 Braunschweig G E R M A N Y published by Luftfahrt-Bundesamt / Germany Tel. +49 (0) 531-2355-5223 email [email protected] Fax +49 (0) 531-2355-5298 URL www.lba.de Aircraft: Dornier / Do 28 D-6, Dornier 128-6, -228-100, -228-200 German Type Certificate No.: 2031 a No. LTA-Nr. Date of Description of Problem Service Bulletins Note issue 1 1983-215 11.01.1984 Actuator motors ARC-PA 520B and ARC-PA 500A Dornier SB No. 1084-2820, dated 21.11.198 - Dornier SB No. 1069-2820, dated 12.09.1980 ARC Field Engineering SB No. 181, dated 01.12.1975 2 1983-216 11.01.1984 Leather bellows on control columns Dornier SB No. 1094-2401, dated 21.11.1983 - 3 1985-040/2 31.05.1985 Flight controls, horizontal stabilizer trim, trim relays 4CC and 9CC Dornier ASB No. 228-019 Rev. 1, dated 19.04.1985 supersedes AD-No. 85-040 4 1985-097/3 22.07.1986 Horizontal stabilizer, front spar Dornier SB No. 228-035 Rev. 1, dated 18.02.1986 supersedes AD-No. 85-097/2 Dornier SB No. 228-024 Rev. 1, dated 25.04.1985 5 1985-158 02.08.1985 Wiring harness on cockpit roof Dornier SB No. 228-025, dated 30.05.1985 - 6 1987-001 15.01.1987 Main Wheel/Brake Assembly Dornier AOT 228/86/012, dated 04.11.1986 - Dornier AOT 228/86/012 Rev. 1, dated 06.11.1986 Goodyear SB Do 228-32-7, dated 30.05.1986 Goodyear SB Do 228-32-8, dated 15.09.1986 7 1987-101 13.05.1987 Engine Nacelle LH/RH Dornier SB No. 1111-3601 Model Dornier 128-6, - dated 20.02.1987 8 1987-102 10.09.1987 Wing, attachment points for the tanks Dornier SB No. 1113-3829 Model Do 28 D-1 and D-2, - Dornier 128-6, dated 08.04.1987 9 1987-217 13.01.1988 Hartzell Propeller - propeller mid-blade failure Dornier AOT No. 228/87/17, dated 09.10.1987 - Hartzell SB No. 140 C, dated 30.09.1987 10 1988-010 29.01.1988 Rod End on flap actuator motor Dornier SB No. 1114-3405, dated 08.05.1987 - 11 1988-131 12.07.1988 Horizontal tail bearing-fitting Dornier SB No. 1110-3204 Model Do 28 D, Do 28 D- - 1, Do 28 D-2, Dornier 128-6, dated 15.04.1988 Page 1 of 3 12 1989-004 24.01.1989 Emergency Exit Door Dornier SB No. 1117-3848 Model Do 28D-2, 128-6, - dated 02.05.1988 13 1989-107 03.08.1989 Electrical system, Essential BUS Modification Dornier SB No. 228-143, dated 03.03.1989 - 14 1989-156 13.09.1989 Nose Wheel Steering Dornier SB No. 228-148, dated 22.05.1989 - 15 1990-182/2 20.12.1990 Trim Relays 4CC, 5CC, 8CC, 9CC Dornier SB No. 228-160, dated 18.12.1989 for supersedes AD-No. 90-182 Aircraft without Autopilot (S20) and without Trim coupling (C01) Dornier SB No. 228-164 for Aircraft with Autopilot (S20) and with Trim coupling (C01) 16 1990-183 12.07.1990 Ground connection wing/Fuselage Dornier SB No. 228-162, dated 19.12.1990 - 17 1990-294 03.09.1990 Startergenerator Fa. APC P/N 250 SG 117 Q Dornier SB No. 228-173, dated 17.07.1990 - APC SB No. 150 SG 111, dated 26.06.1990 18 1992-188 02.03.1992 Wiring Harness, Installation in fuselage Dornier SB No. 228-192, dated 18.11.1991 - 19 1994-042 09.02.1994 Change of main landing gear axle P/N A-511000 B28B against an improved version Dornier SB No. 228-214, dated 28.01.1994 - 20 1994-151 25.08.1994 Flight Controls, L/H Control Column In The Cockpit, Pipe Area Under The Gust Lock Dornier 128-6 SB No. 1137-1401 Rev. 1, dated - 20.06.1994 Airplane Maintenance Manual (AMM), Appendix 1 - Temporary Revisions TR A1-003, dated 14.03.1994 and TR A1-004, dated 15.06.1994 21 1995-175/2 02.08.1995 Horizontal Stabilizer Rib - Inspection for cracks Daimler Benz Aerospace Dornier 328 SB No. 228- supersedes AD-No. 95-175 211 Rev. 3, dated 07.07.1995 22 1995-246 23.08.1995 Landing Gear - Modification of Gear Warning System Daimler Benz Aerospace Dornier 228 SB No. 228- - 215 Rev. 1, dated 01.01.1995 23 1998-141/2 21.05.1998 Landing Gear - Inspection of landing gear actuator Dornier SB No. 228-226 Rev. 1, dated 23.03.1997 supersedes AD-No. 98-141 24 1999-030/3 29.05.2003 Ice and rain protection – Modification of Windshield wash system Dornier 228 SB No. SB-28-235 Rev. 1, dated supersedes AD-No. 99-030/2 18.12.2001 25 2001-045/2 24.07.2003 Horizontal Stabilizer Leading Edge and Ribs - Inspection for cracks Dornier Airplane Maintenance Manual Temporary supersedes AD-No. 2001-045 Revision No. 55-6, dated 03.03.2003 and No. AMM TR 05-88, dated 22.04.2003 26 2002-264 19.09.2002 Air Conditioning - Change of Cockpit and Cabin Auxiliary Heating Wiring Dornier 228 SB-228-249, dated 19.11.2001 - Page 2 of 3 27 2005-438R1 15.10.2013 (ATA 05) Time Limits / Maintenance Checks – Maintenance Requirements - RUAG AMM-228-00014-080184 Rev. 3, dated supersedes AD-No. 2005-438 Implementation 30.10.2012 RUAG Dornier 228 TLMCM-090305-ALL Rev. 5, dated 20.03.2011 RUAG Dornier 228 TLMCM-228-00002-150610 Rev. 1, dated 03.03.2011 28 2007-079R1 27.05.2009 Fuselage – Reinforcement and Inspections of fuselage Frame 19 RUAG Aerospace Services GmbH SB 228-273 supersedes AD-No. 2007-079 29 2007-350R1 30.01.2009 Partial de-bonding of the surface protection on rudders and elevators RUAG SB-228-270 Rev. 1, dated 28.11.2008 supersedes AD-No. D-2007-350 30 2007-353 28.12.2007 Cracks in rudder control cable terminals due to production errors RUAG SB-228-269, dated 23.03.2007 - 31 2008-149 05.05.2008 Fatigue cracks at the connection between nose landing gear cylinder and strut RUAG SB-228-274, dated 05.03.2008 - support because of a manufacturing error during the welding process RUAG ASB-228-272, dated 30.11.2007 32 2008-337 16.12.2008 Flight Controls – Aileron Trim Actuator and Rod Spring Lever Attachment Bracket RUAG Aerospace Services SB 228-275, dated - Riveting – Inspection / Modification 08.10.2008 33 2008-381R1 18.06.2009 Möglicher Verlust von Propellerblattausgleichsgewichten im Fluge durch Bruch der - none - supersedes AD-No. 2008-381 Befestigungsbolzen infolge eines Produktionsfehlers 34 2009-039R2 30.06.2016 Engine Controls – Throttle Box Assembly-Inspection RUAG Aerospace Dornier 228 ASB-228-279 or supersedes AD-No. 2009-039R1 Rev. 1, dated 22.09.2015 35 2009-077 01.04.2009 Main Landing Gear – Identification / Replacement of the Main Landing Gear Stub RUAG Aerospace Dornier 228 SB 228-276 - Axle - END- Datum der letzten Änderung: 30.06.2016 Hinweis: Die Erstellung und Pflege der Übersichtslisten ist eine Service-Leistung des Luftfahrt-Bundesamtes. Obwohl wir die Übersichtslisten mit größtmöglicher Sorgfalt bearbeiten, können wir keine Fehler ausschließen. Bitte beachten Sie, dass deshalb keine Gewährleistung hinsichtlich Richtigkeit und Vollständigkeit für diese Listen übernommen werden kann. Weiterhin ist zu beachten, dass noch weitere Lufttüchtigkeitsanweisungen, z. B. für Motor, Propeller oder andere Ausrüstung für Ihr Luftfahrzeug gelten könnten. Page 3 of 3 .
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