Service Bulletin SAMBURO
LTA Nr. | Release date | TM Nr. | Release date | Affected series and serial number | Object | Deadlines |
|---|---|---|---|---|---|---|
15/10/1976
| (-v, -s) all
| Check main running gear for damage; check airspeed indicator system for leaks
| at the next 50 or 100 h inspection
| |||
29/09/1977
| (-v, -s) all
| Replace the rubber grommets of the cable bushings in the firewall with nylon bushes
| at the next 50 or 100 h inspection
| |||
03/11/1977
| (-v, -s) all
| Spacer discs on sash connection bolts; marking
| at the next 100 h inspection
| |||
04/01/1978
| (-v, -s) all
| Engine panelling, paint inside with fire protection paint
| at the next 50 or 100 h inspection
| |||
14/09/1994
| (-v, -s) all
| Engine panelling, paint inside with fire protection paint
| at the next 50 or 100 h inspection
| |||
18/01/1978
| (-v, -s)all German-licensed motor gliders
| Airspeed indicator markings, type plates, ignition lock, fuel and oil lines, rubber grommets in the firewall, deviation table, flight manual, maintenance manual, information sign in the driver's cab, labelling
| immediately after import to Germany
| |||
–missing –
| 15/03/1978
| AVo 68-v and -s
| Since authorisation in the BRD
| |||
28/02/1980
| 30/10/1979
| (-v, -s) all
| Ignition lock
| at the next 50 h inspection
| ||
18/02/1982
| 21/09/1981
| (-v, -s) all
| Checking and replacing the cross bearing blocks
| 1. every 20 h
2. at the next 100 h inspection, at the latest by 31.12.82 | ||
[Limbach]
11/07/1984 | AVo 68-s
| Conversion to series AVo 68-v
| optional
| |||
[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
| |||
[Hoffmann]
17/05/1988 | AVo 68-v
| Replacement engine according to Limbach TM 808/L2000; replacement HO-V 62 R/L 150 A with HO-V 62()/L160BT
| optional
| |||
05/01/1995
| (-v) with SL 1700 EI, HO V62 R
| Changing the speed sensor markings
| at the next annual inspection
| |||
14/05/1996
| (-v, -s) all
| Conversion AVo68-s & AVo68-v to the AVo68 -R ‘Samburo’ pattern
| optional
| |||
(-v, -s) all
| Welding work with modern welding processes - here WIG (Wolfram Inert Gas)
| optional
| ||||
(-v, -s) all
| Manual revision
| at the next annual inspection
| ||||
15/12/1997
| (-v) each combined with L2000 EO 1 engine
| Cooling air routing; changing the motor cowling
| optional
| |||
(-R) all
| Aerotow
| optional
| ||||
(-v, -s) all with L2000 EO 1 and SL 1700 E 1 engine
| Engine suspension bolt
| until 31.03.99
| ||||
all, AVo68-s, -v, -R
| Inspection the tailplane connection
| immediately before the next flight
| ||||
07/09/2000
| all, AVo68-s, -v, -R
| Corrosion on the nose bar fitting
| within a month
| |||
22/09/2000
| all, AVo68-s, -v, -R
| Faulty galvanic treatment in the sheet metal package of the HLW connection fitting can lead to corrosion and breakage of the fitting.
| immediately before next flight
| |||
AVo68-series, all
| Tailplane, elevator Crack formation during mass equalisation on the elevator at the connection point
| immediately before the next flight within the next 10 flight hours
| ||||
21/01/2002
| AVo68-series, all
| Tailplane, elevator Cracking during mass equalisation on the elevator
| immediately before the next flight within the next 10 flight hours
| |||
++ NEW ++
| ++ NEW ++
| ++ NEW ++
| ++ NEW ++
| ++ NEW ++
| ++ NEW ++
| ++ NEW ++
|
AVo68-R all
| Installation of the ROTAX type 912 S3 aircraft engine based on the AVo68-R100 series
| optional
| ||||
AVo68-R alle
| Changing the material of the banjo bolts for the main spar fitting (avoidance of supply bottlenecks)
| wahlweise
| ||||
Rev 0
27/02/2008 | AVo68-R all
| Modification of the engine mount to allow the installation of a larger starter motor
| optional
| |||
Rev 1
09/04/2014 | AVo68-R100
AVo68-R115 | Modification of the engine mount to allow the installation of a larger starter motor
| optional
| |||
all
| Recognised repair procedures in accordance with EU Regulation 1702/2003 Part 21, Section M
| in the case of a major repair
| ||||
[TM 808 – 23]
| im Zulassungsverfahren
| all
| Installation of authorised avionics devices
| optional
| ||
AVo68-R100, all
AVo68-R115, all | Installation of a WIMI FVA 24c rope winch
| optional
| ||||
09/11/2009
| AVo68-R100, all
AVo68-R115, all | Convert right brake lever to left
| optional
| |||
AVo68-R100, all
AVo68-R115, all | Mounting plate for wheel panelling
| optional
| ||||
19/03/2015
| AVo68-R100, all
AVo68-R115, all | Changing the cylinder head temperature to coolant temperature measurement
| 1) within the next 25 operating hours, but no later than 31 March 2015
2) by 31.12.2015 at the latest | |||
30/11/2017
| AVo68-R Samburo, TM 808-19 performed
AVo68-R100 Samburo, all MSN AVo68-R115 Samburo, all MSN | Adaption of Oil Cooler Mount and attachment of new Oil Cooler Mount on Cowling.
| Optional
| |||
27/04/2021
| AVo68-R Samburo
All serial numbers | Replacement of the elevator mass balance due to recurring formation of cracks
| Mandatory
| |||
21/06/2021
| AVo68-R Samburo
All serial numbers | Slotted hole modification of the elevator mass balance
| Optional
| |||
AVo68-R Samburo
All serial numbers | Replacement of bowden cable for the control of the engine cooling air flap at cowling bottom side (following cowlflap) of the company Hartmann with equivalent product. Supplement of existing drawing AVo68-08.06.01 Cowlflap Zusammenbau to new revision status “a” including reference to new drawing AVo68-08.06.01.06 Cowlflap Control Cable.
| Optional
|
