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Service Bulletins Samburo

MD00-DTB-003-SB-Database_engl_AVo68.pdf

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_808-19
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