| LTA/AD No. | SB No. | Affected Models and Serial No. | Subject | Time of Compliance |
|---|---|---|---|---|
| TM_808-01 15.10.1976 |
(-v, -s) all | Check main landing gear for damage; Check airspeed indicator for leaks | during next 50 h or 100 h check | |
| TM_808-02 29.09.1977 |
(-v, -s) all | Replace control cable rubber grommets in firewall with nylon bushes | during next 50 h or 100 h check | |
| TM 808-03 03.11.1977 |
(-v, -s) all | Shims on wing lift pin Labelling | during next 100 h check | |
| TM 808-04 04.01.1978 |
(-v, -s) all | Engine cowling, paint interior with fire protection paint | during next 50 h or 100 h check | |
| TM 808-04/2 14.09.1994 |
(-v, -s) all | Engine cowling, paint interior with fire protection paint | with import to Germany or during repair | |
| TM 808-05 18.01.1978 |
(-v, -s) all Germanregistered motorgliders | Labelling: airspeed indicator markings, type plates, ignition lock, fuel and oil pipes, rubber grommets in firewall, deviation table, flight manual, maintenance manual, cockpit placard | immediately after import to Germany | |
| N/A 15.03.1978 |
AVo 68-v and -s | Additional requirements for certification in Germany | when registering in Germany | |
| LTA_80-70 28.02.1980 |
TM 808-06 30.10.1979 |
(-v, -s) all | Ignition lock | during next 50 h check |
| LTA_81-116/2 18.02.1982 |
TM 808-07 21.09.1981 |
(-v, -s) all | Inspect and renew aileron bearing blocks | 1) every 20 h 2) during next 100 h check, by 31.12.1982 at the least |
| TM 808/HO-V 62 [Limbach] 11.07.1984 |
AVo 68-s | Conversion to variant AVo 68-v | optional | |
| TM 808/L 2000 [Limbach] 11.07.1984 |
AVo 68-v AVO 68-s |
Replace Limbach SL 1700 EI with L 2000 EO 1; Replace HO-V R/L 150 A with HO-V 62 R/L 160 T Replace Limbach SL 1700 EI with L 2000 EO 1; Replace HO-11-150 B 75 L with HO-11 A-150 B 90 L | optional | |
| TM 169 [Hoffmann] 17.05.1988 |
AVo 68-s | Conversion to variant AVo 68-v | optional | |
| TM 170 [Hoffmann] 17.05.1988 |
AVo 68-v | Replace engine in accordance with Limbach TM 808/L2000 Replace HO-V 62 R/L 150 A with HO-V 62()/L160BT | optional | |
| LTA_1995-005 05.01.1995 |
TM_808-08 14.09.1994 |
(-v) with SL 1700 EI, HO V62 R | Change of RPM indicator markings | during next annual inspection |
| TM_808-09 14.05.1996 |
(-v, -s) all | Conversion of AVo68-s & AVo68-v to variant AVo68 -R “Samburo” | optional | |
| TM_808-10 28.04.1996 |
(-v, -s) all | Welding using state-of-the-art processes – in this case, TIG (Tungsten Inert Gas) | optional | |
| TM_808-11 01.12.1997 |
(-v, -s) all | Revision of manuals | during next annual inspection | |
| TM_808-12 15.12.1997 |
(-v) all with L2000 EO 1 engine | Cooling air duct Modify engine cowling | optional | |
| TM_808-13 17.04.1998 |
(-R) all | Aerotowing | optional | |
| LTA_1999-020 11.02.1999 |
TM_808-14 18.09.1998 |
(-v, -s) all with L2000 EO1 and SL 1700 E 1 engine | Engine suspension bolt | by 31.03.1999 at the least |
| LTA_2000-096 10.08.2000 |
TM_808-15 18.02.2000 |
all, AVo 68-s, -v, -R | Inspect horizontal stabilizer connection | immediately before next flight |
| LTA_2000-274 07.09.2000 |
TM_808-16 07.03.2000 |
all, AVo 68-s, -v, -R | Corrosion on leading edge spar fittings | within one month; with every annual insepction |
| LTA_2000-361 22.09.2000 |
TM_808-17 22.09.2000 |
AVo 68- series, all | Horizontal stabilizer – connector fitting The sheet metal of the horizontal stabilizer connector fitting may have been galvanised incorrectly, which can lead to corrosion and failure of the fitting. | immediately before next flight |
| LTA_2001-371 30.11.2001 |
TM 808-18 23.11.2001 |
AVo68-series, all | Horizontal stabilizer, elevator Cracks on elevator mass balance fitting | immediately before next flight |
| LTA_2001-371/2 05.02.2002 |
TM 808-18 Ausg-2 21.01.2002 |
AVo68-series, all | Horizontal stabilizer, elevator Cracks on elevator mass balance fitting | immediately before next flight; with every annual inspection |
| TM 808-18 R04 10.10.2018 |
AVo68-series, all | Horizontal stabilizer, elevator Cracks on elevator mass balance fitting | 1. within the next 14 calendar days or 5 flight hours whichever comes first 2. exchange after detection of cracks 3. every 25 flight hours |
|
| TM_808-19 09.03.2007 |
AVo68-R all | Fitting of ROTAX aircraft engine type 912 S3 in compliance with model range AVo68-R100 | optional | |
| TM_808-20 10.04.2007 |
AVo68-R all | Change of material: hollow screws for main spar fitting (to avoid delivery bottlenecks) | optional | |
| TM_808-21 Rev 0 27.02.2008 |
AVo68-R all | Modification of engine bracket to enable fitting of a larger starter motor | optional | |
| TM_808-21 Rev 1 09.04.2014 |
AVo68-R100 AVo68-R115 |
Modification of engine bracket to enable fitting of a larger starter motor | optional | |
| TM_808-22 16.06.2010 |
all | Approved repair procedures in accordance with EUVO 1702/2003 Part 21, Section M Minor Change 10030464 |
in case of a major repair | |
| TM_808-24 01.05.2009 |
AVo68-R100, all AVo68-R115, all |
Fitting of WIMI FVA 24c rope retraction mechanism Minor Change 10027821 |
optional | |
| TM_808-25 01.05.2009 |
AVo68-R100, all AVo68-R115, all |
Conversion of air brake lever from right-hand to lefthand Minor Change 10027833 |
optional | |
| TM_808-30 12.07.2013 |
AVo68-R100, all AVo68-R115, all |
Mounting plate for wheel cowling | optional | |
| TM 808-31 07.05.2015 |
AVo68-R100, all AVo68-R115, all |
Change of measurement method from cylinder head temperature to coolant temperature for ROTAX Engine Type 912 and 914 (Series) | 1) within the next 25 h of operation, but by 31.03.2015 at least; 2) by 31.12.2015 at least | |
