Hier finden Sie alle Technischen Mitteilungen, LBA-LTAs und EASA-ADs von diesem Flugzeugtypen. Am unteren Ende der Liste schließen die aktuellen Wartungsanweisungen an.
Here you can find all the Technical Notes, LBA-LTAs and EASA-ADs of this glider model. The Maintenance Instructions are added at the bottom of the list.
Übersicht (PDF) Overview (PDF)
Dat.
Download
Dat.
Download
Subject
affected
Compliance
Manual
03.04.2020
Specification of service life limitations for the brake hoses of the hydraulic wheel brake
alle Werknummern
ASH 26 E
all serial numbers
optional
07.11.2019
Alternative rim for main wheel
alle Werknummern
ASH 26 E
all serial numbers
none
15.09.2017
Specification update of the flexible fuel tanks
alle Werknummern
ASH 26 E
all serial numbers
In case of replacement or new installation of a flexible fuel tank
01.02.2017
Alternative hydraulic wheel brake system TOST
alle Werknummern
ASH 26 E
all serial numbers
optional
27.05.2021
Various modifications on the power-plant system
alle Werknummern
ASH 26 E
all serial numbers
none
23.11.2016
Optional installation of a Parking Brake and a Piggott Hook
alle Werknummern
ASH 26 E
all serial numbers
none
AusgabeII
IssueII
19.07.2017
31.07.2017
Replacement of the silencer
alle Werknummern
ASH 26 E
all serial numbers
Replacement of the existing silencer after 150 engine hours, at the latest.
10.04.2014
Exchange of the steerable tailwheel
alle Werknummern
ASH 26 E
all serial numbers
none, optional
05.09.2012
Replacement of the carburettor cap, tightness of the bleeding screw on the oil pump
alle Werknummern
ASH 26 E
all serial numbers
Replacement before 12/31/2012, if an oil leak is detected.
08.01.2008
Adjusting the drive belt
alle Werknummern
ASH 26 E
all serial numbers
at the latest by the next annual C. of A. Inspection
31.01.2008
Installation of transponder antennas
alle Werknummern
ASH 26 E
all serial numbers
none, optional
22.02.2005
1.Neue Kraftstoffleitungen ohne feste Austauschintervalle
2.Neuer Anlasserstecker in Motorraum
3.Zugangsöffnungen für Zündkerzen in der Rumpfschale
4.Vorbereiteter Einbau der Winglet-Trennstelle im Flügel
5.Neuer Kühler
6.ILEC- Motorbediengerät der Version 2
7.Angabe des Zündkerzentyps in einer Wartungsanweisung
8.Neue Sp*rnradvariante
Various modifications
1.New fuel lines without firm exchange intervals
2.New starter plug in engine compartment
3.Access holes for spark plugs in the fuselage shell
4.Prepared installation of the winglet interface in the wing
5.New radiator
6.ILEC - engine control instrument, version 2
7.Indication of the type of spark plug in a Maintenance Instruction
8.New tail wheel variant
alle Werknummern
ASH 26 E
all serial numbers
none, optional
07.05.2003
Alternation of the engine manufacturer
alle Werknummern
ASH 26 E
all serial numbers
none
25.09.2000
Part I:Installation of a fixed re-fuelling system in the fuselage
Pert II:Return of the wing tank ventilation into the fuselage tank
alle Werknummern
ASH 26 E
all serial numbers
none, optional
05.10.2000
New propeller AS2F1-1/R153-92-N1
alle Werknummern
ASH 26 E
all serial numbers
none, optional
28.06.1999
Nose bolt with O-Ring for horizontal tail
all ASH 26 E
optional
23.08.1999
08.09.1999
Inspection and exchange of the exhaust damper of the power-plant. Amendment and corrections to the manuals.
all ASH 26 E
prior to the next engine flight
09.04.1999
Modification for optional operation with 0,45 m high winglets incl. a short wing piece which are fitted at a wing separation point
all ASH 26 E
---
10.08.1998
10.09.1998
Inspection of the engine compartment and silencer cover for spilled oil. Inspection of the red silicon hose
all ASH 26 E
Maßnahmen 2. u. 4: vor dem nächsten Flug nach Feststellung von Schäden
Maßnahme 5: innerhalb von 30 Kalendertagen
Action 1 & 2: prior to next take-off
Action 2 & 4: prior to next take-off when any damage is detected
Action 5: within 30 calendar days
23.07.1998
08.10.1998
Inspection and exchange of the "rotor cooling air fan according to TN 1", fitted to the engine AE 50 R made by Mid-West Engines LTD.
all ASH26E as of S/N 26134 serial standard
Pkt.2: bis zur nächsten Jahresnachprüfung
Ad1: prior to next take-off
Ad2: at the latest by the next annual C. of A. Inspection
08.09.1997
Air intake for blow holes in flap and aileron by means of NACA ducts
all ASH 26 E
---
28.08.1997
Improvement of airbrake efficiency
all ASH 26 E
---
02.08.1997
Obtaining Type Certificate status as per Data Sheet 883, issue 1, dated 07.08.95
Aircraft ASH 26 E (Data Sheet No. 883) , which were exported to the USA without C. of A.
none, only required for FAA-registration
31.10.1996
30.01.1997
b) Austausch des Kühlluftgebläses der Motorinnenkühlung
c) Austausch des Temperaturfühlers der Motorinnenkühlung
d) weitere Überprüfungen, Handbuchänderung für FAA
a) Checking the cooling air temperature in flight
b) Improvement and change of the fan of the engine internal air cooling.
c) Exchange of the temperature sensor of the internal air cooling.
d) Inspection of further engine & exchange of manual pages
all ASH 26 E
b)u.c) frühest möglich, jedoch bis zur nächsten Jahresnachprüfung
a)&d) prior to next take-off
b)&c) earliest, but at the latest by the next annual C. of A. Inspection
Maintenance Instructions
Dat.
Issue
Subject
affected
31.08.2017
Installation and Inspection Instruction for Flexible Fuel Tanks (“Working Instruction No. 32”)
all flexible fuel tanks in Schleicher aircraft
08.01.2008
Adjusting the drive belt
all ASH 26 E
01.03.2005
26.06.2003
Replacing the elastic fairing tape at the control surface gaps of vertical & horizontal tail, ailerons, flaps and at the gaps of the engine bay doors.
all ASH 26 E
01.11.2001
Fuel types
all ASH 26 E
22.05.2005
New adjustment of the fuel contents indication of the ILEC engine control unit
all ASH 26 E
25.03.1997
To vent the oil pump
all ASH 26 E
26.06.1989
Paint Cracks
all ASH 26 E
01.06.2011
Alternative rim for main wheel
ASH 26 E
all ASH 26 and
ASH 26 E