Status Subject Detail Scheibe (Germany) Reference information Contact: SCHEIBE AIRCRAFT GMBH, Flugplatz Heubach, Am Flugplatz 5, D-73540 Heubach Tel.: +49 (0) 7173 / 184286 FAX: +49 (0) 7173 / 185587 E-Mail: info@scheibe-aircraft.de Type certificate holder for all aircraft except SF 23.34 & 36. LBA Airworthiness Directives https://www.lba.de/EN/DivisionT/Airworthiness/ADs/ADs.html EASA AD list http://ad.easa.europa.eu/ TC holder AD and TN and Sb list http:// http://www.scheibe-aircraft.de/ For complex repairs on the 277 form always quote and adhere to http://www.scheibe-aircraft.de/TM%20LTA/TM%20uebers/pdf_tm/653-79-2.pdf All welding m,ust be gas and not TIG. EASA, LBA and CAA Airworthiness Directives SF24 M M M Flexible hose life Control cables Hirth F10 engine Wooden Structure Inspection/replacement of cable sleeves Operational and maintenance instructions BGA Inspection of wooden structures using Kaurite glue and 5 year repeat TM 653-28/4 AD74-323 AD 69-142 BGA 047/02/2006 issue 1 SF 25 series General, LBA Airworthiness Directives listed in CAA Foreign Airworthiness Directives Vol. III. Page 1 BGA Compendium 01/12 TNS 10/98 1-2006 Scheibe (Germany) Status Subject Detail Reference information I Horizontal Stabiliser Flutter AD 1966-119 I Unleaded MOGAS approval (Limbach L1700 & 2000) TN 653-66 I SF-25/T-61 tailplane front attachment cracked TI 102 M SF-25 carb heat system introduced, mandatory (CAA) Mod 134 M Fuel shut off valve NK 490 fitted in place of Truma V8M SB 653-70 I Flexible hose life TM 653-28/4 etc M Engine mounting (Stamo) Cracks in lower mount bolts SF25B S/N 4601>46174. AD 71-131, TB 2/71, Mod 120 M Engine mount Cracks in bolts AD1971-144 M Luggage compartment Securing of luggage S/N 4601 > AD 72-107, Mod 132 M Carburettor heater Installation AD 73-15, Mod 133 M Ignition Switch New type SF25B S/N 4601>46253 & 4801 >4828 SF25C S/N 4401>4448 AD 73-23, Mod 4 & 134 M Ailerons Bellcrank replacement SF25A AD 74-54 M Flight control cables Inspection of cable sleeves AD 74-323 M Electrical system Installation of smoothing capacitor SF25B & C with Dittel radio FSG-12, -15 or –16 AD 75-91/2 M Aileron drive lever Inspection / reinforcement SF25B & SF25C AD 75-169/2, TI 653-5/75 M Fuel Quantity indication Incorrect indication SF25B S/N 4601>46258 & 4801>4868 SF25C S/N 4401>44133 & 4201>4252. AD 76-40, TN 653-1/76 M Fuel filler Inspection SF25A all & SF25B S/N 4601>4645 AD 76-297, TN 653-6/76 M Elevator support Inspection SF25B S/N 4801>4868 & SF25C S/N 4201>4255 AD 77-217, Sportavia TMS-02-77 M Stabiliser/Tailplane Fwd Armature Inspection SF25A,B,C,D,E & K AD 82-049, TN 653-40 M Fuel SOV Life limitation SF25B,C,D,E & K AD 82-50/2, TN 653-41 M Wing Main wing joint SF25B,C,D & E AD 82-134/2 M Flight controls Bearings in control stick SF25C,E & K AD 1984-198/2, TN 653-47 M Flight controls Inspection of airbrake pulley SF25A,B,C,D,E & K. Working instruction 653-62-142/770-18-142 AD 94-261, SB 653-62/770-18 M Fuel SOV TRUMA V8 valves AD 97-140, SB 653-67 M Flight Controls Cracks in aileron steel pipe spar SF25B & C AD 1999-340, SB 653-73 M Wing centre joint Additional limitations CAA AD 001-07-82, TI 103/T61 M Flight manual (Rotax C) Corrections and revisions AD2003-160, SB653-76 M Controls L’Hotellier ball & socket with lock plates AD 1993-001/3 Page 2 BGA Compendium 01/12 TNS 12/96 04/90 08/87 02/98 10/98 04/76 04/76 09/77 02/90 09/82 02/85 & 04/00 10/94 08/97 & 02/98 02/00 07/82 06/03 Scheibe (Germany) Status Subject M Controls R Wooden Structure M Flight controls M Flight controls Detail L’Hotellier ball & socket with locking cams BGA Inspection of wooden structures using Kaurite glue and 5 year repeat Elevator and tab drive arm Aileron and tail plane attachment rivets Reference information AD 1994-001/2 BGA 047/02/2006 issue 1 AD 2009-0132, TN 653-91 AD 2010-0011-E, SB 653-64 SF25 Series In Service Reports (Advisory) I SF-25/T-61 elevator tab cables wire lock at tab I Longerons corroded at fin post adjacent to microballoon filler R Wheel assembly bolt failures fit larger (8mm) bolts I SF-25/T-61 compass errors magnetised canopy frame I Spar deterioration water in spoiler boxes R SF-25/T-61 wing main pin holes worn & splayed oval I T-61 ignition switch “live” test I Crank case cracks numerous cases - inspect regularly I SF-25 fuel flow restriction filter incorrectly installed R Top harness attachments secure to transverse tube R Rear exhaust valve burning Limbach improved cooling kit I Tubing on fuel gauges hardens and leaks I T-61 magneto to crankshaft coupling failure of type without reinforcing ring I Rear fuselage structure corrosion near fin attachments I Aileron drive bearing failure central hanger upper bearing between sticks I Tailplane front mount cracked through inspect for cracks and poor welds I Throttle cable disconnected check security at carburettor connection I Elevator tab rigging Incorrect connection of elevator tab operating cable I Flight Manuals Due to EASA type approval all SF25 require flight manuals SF-26A Spar deterioration Top rudder hinge water penetration cracks/failure Page 3 BGA Compendium 01/12 TNS 1-2006 3/2009 1-2010 06/73 01/75 11/77 12/79 06/95 & 12/80 12/80 12/85 02/87 06/90 01/93 01/93 06/95 06/96 02/99 04/99 08/99 10/99 6-2006 2-2008 10/74 08/79 Scheibe (Germany) Status Subject M Control cables M Flying Controls M Wooden Structure M Flight controls Detail Inspection/replacement of cable sleeves Inspection of aileron bellcrank for cracks BGA Inspection of wooden structures using Kaurite glue and 5 year repeat Elevator and tab drive arm SF-26 In Service Reports (Advisory) I Rudder Unsatisfactory repair found on rudder bell crank SF-27A & M Elevator actuating lever M Elevator torque tube Top rudder hinge Flexible hose life M Control cables R Wooden Structure cracks at weld reinforce at weld cracked Inspection/replacement of cable sleeves BGA Inspection of wooden structures using Kaurite glue and 5 year repeat Reference information AD74-323 AD75-270, TN 232-1/75 BGA 047/02/2006 issue 1 AD 2009-0132, TN 232-241 TN 257 AD 75-48, TN 257-1/74 TM 653-28/4 etc AD74-323 BGA 047/02/2006 issue 1 SF-28A Tandem Falke M Main wing pin M Flight controls correct locking Inspection of airbrake pulley Working instruction 653-62-142/770-18-142 Unleaded MOGAS approval (Limbach L1700 & 2000) M Fuel shut off valve Truma V8M 8 year (seals) life limitation Fuel shut off valve NK 490 fitted in place of Truma V8M Flexible hose life M Elevator/aileron drive cracks reinforce before next flight Page 4 BGA Compendium 01/12 LTO 345 & 508, AD 82-135/2 AD 94-261, SB 653-62/770-18 TN 770-19 AD 97-140, SB 770-20 AD82-51/2, SB 770-13/2 TM 653-28/4 etc AD 1998-435, SB 770-23 TNS 1-2006 3/2009 6-2011 01/74 06/75 02/92 10/98 1-2006 12/80 & 04/95 12/96 08/97 02/98 10/98 12/98 Status Subject M Control cables M Flying controls M Electrical system M Wing centre pin M Wing centre joint M Flight Controls M Controls M Controls M Controls M Electrical system R Wooden Structure R Wooden Structure M Flight controls Scheibe (Germany) Detail Inspection/replacement of cable sleeves Inspection of rear control stick Installation of smoothing capacitor with Dittel radio FSG-12, -15 or –16 Inspection Additional limitations Cracks on the aileron/elevator bell crank L’Hotellier ball & socket with lock plates L’Hotellier ball & socket with locking cams Spoilers in the wing Safety device BGA Inspection of wooden structures using Kaurite glue and 5 year repeat BGA Inspection of wooden structures using Kaurite glue and 5 year repeat Elevator and tab drive arm Reference information AD74-323 AD81-237, TN770-12 AD 75-91 CAA AD 003-06-82 CAA AD 001-07-82, TI 103/T61 AD1998-435 AD 1993-001/3 AD 1994-001/2 AD1988-030 AD1975-091/2 BGA 047/02/2006 issue 1 BGA 047/02/2006 issue 1 AD 2009-0132, TN 770-30 TNS 1-2006 1-2006 3/2009 SF-34 M M M M M M Wing root rib modification SF34 & 34B S/N 5102>5131 AD 89-73, TN 336-2(supersedes AD 88-162/2) Spin recovery improved Aft C of G limit 2367 mm AD 96-241, TN 336-8 Rear fuselage frame disbonded inspect for bond failure (causes fin/TP flutter) Fuselage inspection (SF34, SF34B) Inspection of aft fuselage and flight restrictions BGA 001/05/2000 iss1 Fuselage inspection Inspection of aft fuselage and lifting of LBA flight restrictions (BGA restrictions remain) AD 2000-299, SB 336-9 Control cables Inspection/replacement of cable sleeves AD74-323 Flight controls Rear control stick inspection AD 2002-044, TB 336-10 MÜ-13E Bergfalke (1) M Spar deterioration reduction of span M CG hook mounting cracks caused by loose bolts M Elevator & airbrake connection “bolts” replace with new “bolts” in aircraft material Page 5 BGA Compendium 01/12 AD 75-42 AD 79-501, TN 104-15 TN 104-18 10/89 ??/96 08/98 08/00 10/00 02/02 04/75 02/80 08/85 Status Subject M Control cables M Wooden Structure M Flight controls Scheibe (Germany) Detail Inspection/replacement of cable sleeves BGA Inspection of wooden structures using Kaurite glue and 5 year repeat Elevator and tab drive arm Reference information AD74-323 BGA 047/02/2006 issue 1 AD 2009-0132, TN 104-24 Bergfalke II, II-55, III and IV CG hook mounting (Berg III only) cracks caused by loose bolts TN 104-2/76 M CG hook mounting (all) cracks caused by loose bolts AD 79-501, TN 104-15 Spar deterioration water in brake box M Main wing pin not fully through lower spar lugs, safety pin hole too low down TN 104-17 M Elevator & airbrake connection “bolts” replace with new “bolts” in aircraft material TN 104-18 Tailplane at front attachment damaged by water - inspect in depth Speed brake lever in centre section cracked – reinforce M Control cables Inspection/replacement of cable sleeves AD74-323 M Wooden Structure BGA Inspection of wooden structures using Kaurite glue and 5 year repeat BGA 047/02/2006 issue 1 Zugvogel III A & B Elevator hinge pin M Control cables M Wooden Structure sheared at the weld Inspection/replacement of cable sleeves BGA Inspection of wooden structures using Kaurite glue and 5 year repeat AD74-323 BGA 047/02/2006 issue 1 Page 6 BGA Compendium 01/12 TNS 1-2006 3/2009 02/77 02/80 05/79 02/85 08/85 08/86 10/89 1-2006 06/92 1-2006