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Alexander Schleicher ASH 26 E Maintenance Manual

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  • Page 213 Alexander Schleicher Maintenance Instruction GmbH & Co. Sheet: 1 of 4 PAINT CRACKS Segelflugzeugbau D-36163 Poppenhausen Subject: Paint cracks on fiber composite gliders. Types affected: ASW 12, ASW 15, ASW 17, ASW 19, ASW 20, ASK 21, ASW 22, ASK 23, ASW 24, ASH 25; ALL variants and all serial no.s.
  • Page 214 Alexander Schleicher Maintenance Instruction GmbH & Co. Sheet: 2 of 4 PAINT CRACKS Segelflugzeugbau D-36163 Poppenhausen A competition pilot will always be anxious to preserve or restore the performance of his glider to its full extent, but unfortunately owners of training and instruction gliders are generally of the opinion that they may accept such a performance loss with those gliders.
  • Page 215 Alexander Schleicher Maintenance Instruction GmbH & Co. Sheet: 3 of 4 PAINT CRACKS Segelflugzeugbau D-36163 Poppenhausen Action: To repair the paint cracks, these have to be removed generally by sanding them down to their ground. But in doing so, the fiber compos- ite structure lieing under the gel coat should not be sanded on.
  • Page 216 Alexander Schleicher Maintenance Instruction GmbH & Co. Sheet: 4 of 4 PAINT CRACKS Segelflugzeugbau D-36163 Poppenhausen If in the case of older glider models such data are not contained in the manuals, then the mass of the control surfaces and their tailheavy static balance moment must be determined prior to the paint job and must be readjusted after the repainting by ±...
  • Page 217 Triebwerk/Engine AE50R Alexander Schleicher Blatt / Sheet GmbH & Co. Wartungsanweisung 1 von/of 1 Segelflugzeugbau Maintenance Instruction D - 36163 Poppenhausen Entlüften der Ölpumpe Wenn zu Wartungs- oder Reparaturarbeiten die Ölleitung demontiert wurde oder das Triebwerk umgedreht wor- den ist, ohne die Hinweise unter Punkt 2.11 im Wartungshandbuch zu beachten, muß die Ölpumpe der Verlust- ölschmierung entlüftet werden.
  • Page 218 ASH 26 E / ASH 25 M(i) Alexander Schleicher Sheet GmbH & Co. Maintenance Instruction „Fuel“ of 1 Segelflugzeugbau Issue II D - 36163 Poppenhausen Subject: Fuel types Applicability: All engine production series AE 50 R Reason: Use of motor vehicle fuel types.
  • Page 219 ASH 26 Alexander Schleicher Sheet GmbH & Co. Maintenance Instruction A 1 of 7 Segelflugzeugbau Issue III D - 36163 Poppenhausen Replacing the elastic fairing tape at the control surface gaps of ver- Subject: tical & horizontal tail, aileron, flaps and at the gaps of the engine bay doors.
  • Page 220 ASH 26 Alexander Schleicher Sheet GmbH & Co. Maintenance Instruction A 2 of 7 Segelflugzeugbau Issue III D - 36163 Poppenhausen Wing under side and horizontal tail upper side: Fig. 1 (Wing under side) Apply the sealing/slip tape [1] (3M Scotch Teflon Tape 30 mm wide) with a clearance of 16 mm to the front edge of the recessed step (22 mm wide).
  • Page 221 ASH 26 Alexander Schleicher Sheet GmbH & Co. Maintenance Instruction A 3 of 7 Segelflugzeugbau Issue III D - 36163 Poppenhausen Wing upper side and horizontal tail lower side: Fig. 3 Remove protective backing from elastic fairing tape and stick it on abutting the front edge of the recessed step (about 15 mm wide) in the wing upper side and stabilizer lower side respectively, by means of its adhesive film layer.
  • Page 222 ASH 26 Alexander Schleicher Sheet GmbH & Co. Maintenance Instruction A 4 of 7 Segelflugzeugbau Issue III D - 36163 Poppenhausen Vertical Tail: Fig. 4 There are no recessed steps at the fin. As shown in Fig. 4 the elastic fairing tape [6]...
  • Page 223 5 of 7 Segelflugzeugbau Issue III D - 36163 Poppenhausen The materials required can be obtained from Messrs. Alexander Schleicher. Engine bay doors: Fig. 5 Engine bay doors, rear end Fig. 6 Engine bay doors, front end The elastic fairing tape [4] (Mylar foil 22-15 mm wide) is adhered along the lower edge of the engine bay door with an overhang of 7 mm (only the 15 mm wide adhesive film of the elastic faring tape is on the engine bay door).
  • Page 224 ASH 26 Alexander Schleicher Sheet GmbH & Co. Maintenance Instruction A 6 of 7 Segelflugzeugbau Issue III D - 36163 Poppenhausen Notes: 1. The actions under points can be accomplished by a competent person. 2. Ensure that the elastic fairing tape is in tight contact even when the control surfaces and flaps are fully deflected.
  • Page 225 ASH 26 Alexander Schleicher Sheet GmbH & Co. Maintenance Instruction A 7 of 7 Segelflugzeugbau Issue III D - 36163 Poppenhausen Winglet: zig-zag tape, length = 460 mm till the fillet Material: Horizontal Horizontal Vertical Winglet in front of Tail...
  • Page 226 Alexander Schleicher ASH 26 E / ASH 25 M(i) Blatt GmbH & Co. Wartungsanweisung „Zündkerzen“ 1 von 1 Segelflugzeugbau Ausgabe I D - 36163 Poppenhausen Gegenstand: Austausch von Zündkerzen Betroffen: Alle AE 50 R und IAE 50 R Baureihen Vorgang: Verwendung von Zündkerzen ohne EASA Form 1...
  • Page 227 ILEC GmbH D-95444 Bayreuth TM 13 of ASH 26 E includes the information of an improvement in the circuitry of the ILEC by the manufacturer of the device, which is now internally closer to the version of the ASH 25 Mi.
  • Page 228 Alexander Schleicher Maintenance Instruction Sheet GmbH & Co. Adjusting the drive belt 1 of Segelflugzeugbau Issue I D - 36163 Poppenhausen Power-plant AE50R and IAE50R-AA Subject: The belt tension is adjusted such that the belt eigenfrequency - in the area where it is running in the channel inside both swivel support arms - corresponds to 48 Hz.
  • Page 229 Alexander Schleicher Maintenance Instruction Sheet GmbH & Co. Adjusting the drive belt 2 of Segelflugzeugbau Issue I D - 36163 Poppenhausen Frequency Measurement: As frequency meters for the special purpose of measuring belt eigenfrequency are relatively ex- pensive, there is a cheaper alternative: by means...
  • Page 230 Alexander Schleicher Maintenance Instruction Sheet GmbH & Co. Adjusting the drive belt 3 of Segelflugzeugbau Issue I D - 36163 Poppenhausen Belt running: An increased wear occurs also if the belt is running up at the washer discs of the pul- ley, particularly at the upper pulley.
  • Page 231 Alternative rim for main wheel Applicability: ASH 26 Type Certificate LBA 383 ASH 26 E Type Certificate LBA 883 all serial numbers Reason: The rim Tost Penta 125 – 1¼“ can be installed instead of the rim specified in the Mainte-...
  • Page 236 For the purpose of getting compliance with the Type Certificate Status for those aircraft ASH 26 E which were delivered to the US prior to the German Type Certification, a special In- spection Program was compiled, which becomes part of this TN. In accordance with this In- spection Program the aircraft must be inspected and where applicable necessary actions must be accomplished.
  • Page 237 Alexander Schleicher ASH 26 E Sheet GmbH & Co. 2 of 2 Technical Note Segelflugzeugbau D - 36163 Poppenhausen No. 2 Notes: The amendment to the Manual can be done by the operator of the glider himself. The constructional actions must only be accomplished by the manufacturer Alexan- der Schleicher or by a technical aviation service station holding an appropriate license.
  • Page 238 TN No. 3 D - 36163 Poppenhausen Improvement of airbrake efficiency. Subject: Serial number applicability: All sailplanes ASH 26 and all powered sailplanes ASH 26 E, all production series. None. Compliance: Reason: For improvement of the airbrake efficiency SCHLEICHER offers a mod kit to convert the airbrakes to a double-panel system.
  • Page 240 The failure can be favored by engine operation with RPM above 6900. The manufacturer of the ASH 26 E engine offers an upgraded fan impeller by issue of their Service Bulletin 002. As the efficiency of the new impeller has also been improved distinctly, the drive belt transmission could be reduced.
  • Page 241 Maintenance Manual. The installation must be done only by the manufacturer Alexander Schleicher or by a technical aviation service station holding an appropriate license. The exchange of the pages in the Manual can be done by the operator of the glider him- self.
  • Page 242 Reason: In the case of one ASH 26 E with about 36 hours engine operating time, engine oil in the heat damping layer of the exhaust fairing has ignited, presumably after switching off the engine, and has caused a smolder in this fairing.
  • Page 243 The inspections can be accomplished by a skilled person and must be entered in the glider logbook under the block Maintenance Works. The exchange of parts must be done by the manufacturer Alexander Schleicher or by a technical aviation service station holding an appropriate license, and is to be checked and entered by a licensed aviation inspector in the sailplane's log and relevant inspection documents.
  • Page 244 Schleicher aircraft, suggested to develop winglets also for the ASH 26 and ASH 26 E. As it was not feasible to fit these relatively high winglets of 0.45 m at the existing wing tip, it was necessary to develop a wing separation joint at y = 8.7 where the winglet including a short wing piece (but without additional aileron) can be fitted.

  • Page 245: Table Of Contents

    Winglets, assembly drawings and instructions must be obtained from the manu- facturer Schleicher GmbH & Co. The installation of the wing separation joint and the alignment works can be accom- plished by either the manufacturer Alexander Schleicher or by a technical aviation service station holding an appropriate license. Contact: Alexander Schleicher GmbH &...
  • Page 246 Inspection and exchange of the exhaust damper of the power-plant. Amendment and corrections to the manuals. Affected: ASH 26 E, Data Sheet No. 04.883, all serial numbers. Compliance: Prior to the next engine flight all powered sailplanes must be inspected to make which version of the exhaust damper has been installed.

  • Page 247: Notes

    The exchange of the exhaust damper system must only be accomplished by the manufacturer Alexander Schleicher or by a technical aviation service station holding an appropriate license. The exchange of the pages in the Manuals can be done by the operator of the aircraft himself.

  • Page 248: Tn No

    TN-No. ASW 24 TOP TN-No. ASH 25 TN-No. ASH 25 E / ASH 25 M TN-No. ASH 26 TN-No. ASH 26 E TN-No Subject: Nose bolt with O-Ring Serial number applicability: ASK 21 German TC No. 339 all Serial Numbers ASK 23 / ASK 23 B German TC No.

  • Page 249: Alexander Schleicher

    General Alexander Schleicher Page GmbH & Co. Technical Note 2 of 2 Segelflugzeugbau for: D - 36163 Poppenhausen Action: In accordance with drawing 000.33.9001, Sheet 1 drill a hole into the nose fitting at the stabilizer underside and ream. As shown on Sheet 2 a groove must be milled into the nose bolt for the O-ring;...
  • Page 250 In accordance with the instructions in drawing 800.9005 (Mod Power-plant 800 ASH 26 E TM 10) the gear reduction must be changed. The swiveling propeller support arms must also be changed as detailed in this drawing. The engine doors must be replaced for the new version (drawing 260.11.0360/0361).
  • Page 251 Part I: Subject: Fixed re-fuelling system Serial number applicability: All ASH 26 E Compliance: None, optional extra on customer request. Reason: The components of the external re-fuelling system may also be in- stalled fixed in the fuselage; this is offered as an optional extra. Two...
  • Page 252 Part II: Subject: Return of the wing tank ventilation into the fuselage tank Serial number applicability: All ASH 26 E Compliance: None, optional extra on customer request. Reason: If during re-fuelling the wing tanks are overfilled inadvertently, fuel could escape via the ventilation at the end rib of the inner wing, fuel which better should be collected for environmental rea- sons.
  • Page 253 ASH 26 E Alexander Schleicher Sheet GmbH & Co. 3 of Technical Note Segelflugzeugbau No. 11 D - 36163 Poppenhausen The following points apply to Part I and Part II: Action: The following pages in the manuals must be exchanged - or added respectively - for new pages with the corresponding revision entry „TN 11 dated 25.09.00“.
  • Page 254 Diamond Aircraft Industries GmbH (DAI). At the same time the Type Certi- fication for the engine types which are installed by Alexander Schleicher in their aircraft, was moved from the British CAA to the Austrian ACG. The designation of the engine types was not changed.
  • Page 255 ASH 26 E Maintenance Manual According to NfL II-7/90 (German notice to airmen) the removing of the power-plant is regarded as a maintenance task according to § 6 LuftBO. A special inspection according to § 9 LuftBO is therefore not necessary in that case.
  • Page 256 ASH 26 E Maintenance Manual The rear engine mounting bolt [29] must be threaded into the thread of the rear engine support mount by carefully moving the engine unit. After having tightened the bolt secure it with locking wire. Locking wire (see Fig.2.3-10):...
  • Page 257 ASH 26 E Maintenance Manual 2.5 Landing gear 2.5.1 Main Wheel The sprung main wheel consists of a Cleveland rim (P/N 40 78B) with a Goodyear tire 5.00-5 6pr TT and inner tube 5.00-5 TR67A. The wheel is equipped with a hydraulic brake:- - Cleveland wheel brake cylinder 30-9 and Master Cylinder 10-20.
  • Page 258 ASH 26 E Maintenance Manual Detail numbers [x] relating to Figures: Detail In Figure Front engine support bearing 2.3-2 Rear engine support bearing 2.3-2 Spindle 2.3-1 Toggle crank 2.3-1 Propeller assembly, entire 2.3-1 Gas spring 2.3-2 Starter 2.3-1 Exhaust silencer 2.3-2...
  • Page 259 ASH 26 E Maintenance Manual Fig. 2.3 – 10 Locking Wire and Lock plates rear mounting screw at oil tank: Fuel hose line disconnent piont: front engine mounting bearing: Lock plates at both starter cables: NOTE: according to TN 13 both starter cables can be united in a common self-locking plug.
  • Page 260 AS2F1 is subject to a service life limitation. Fuel Lines According TN 13 the ASH 26 E can be fitted with PUR-fuel-lines without limited service life (series standard for new built aircrafts or for retrofitting). Exception: the fuel line connection of the two halfes of the fuel tank in the fuselage.
  • Page 261 After five years: Replace all rubber fuel hose lines. Note: According TN 13 the ASH 26 E can be fitted with PUR- fuel-lines without limited service life, Section 4.2! b.) Once-Only Maintenance Tasks After 1 hour and every time the propeller has been reinstalled re-...
  • Page 262 ASH 26 E Maintenance Manual ASH 26 E POWER-PLANT MAINTENANCE INTERVALS Engine Hours Period Years Period Once-only Maintenance after 1 hour: 0 - 150 450 - 600 1 - 5 Retighten M8 bolts at prop.flange 150 - 300 600 - 750...
  • Page 263 Blatt ASH 26 TM Nr. 6 Ausgabe II GmbH & Co. 1 von 2 ASH 26 E Segelflugzeugbau TM Nr. 14 Ausgabe II D - 36163 Poppenhausen Gegenstand: Einbau von Transponder-Antennen am Rumpf hinter dem Fahrwerk oder seitlich davon bei Flugzeugen mit CFK-Rumpf...

  • Page 264: Ash 26

    Blatt ASH 26 TM Nr. 6 Ausgabe II GmbH & Co. 2 von 2 ASH 26 E Segelflugzeugbau TM Nr. 14 Ausgabe II D - 36163 Poppenhausen Hinweise: Transponder müssen eine Mindestabstrahlleistung besitzen, können aber zu höheren Werten hin eine deutliche Streuung aufweisen. Das kann bei Einbauten mit maximaler Kabellänge und Wechsel zu einem anderen Transponder dazu führen, dass die zulässi-...
  • Page 265 ASH 26 E Flight Manual i) Any kinks in Bowden cables or fuel lines and hoses? Elastic cords of the engine bay doors in good condition? j) Inspect hoses (especially fuel and coolant hoses) and all compo- nents for signs of chafing.
  • Page 266 ASH 26 E Maintenance Manual completely covered by neatly fitting doors. 2.3.1.2 Engine controls in the cockpit The throttle and the propeller stop block are operated via Bowden cables by a pair of control levers in the engine control console which is fitted beneath the instrument panel.
  • Page 267 ASH 26 E Maintenance Manual TN 15: The original text is being replaced by the Mainenance Instruction “Ad- justing the drive belt” (Section 12.6) Rev.No. / Date Sig. Author Date Page No. 2.14 Heide 31.01.95 TN 15 / Jan. 08...
  • Page 268 ASH 26 E Maintenance Manual TN 15: The original text is being replaced by the Mainenance Instruction “Ad- justing the drive belt” (Section 12.6) Rev.No. / Date Sig. Author Date Page No. 2.15 Heide 31.01.95 TN 15 / Jan. 08...
  • Page 269 ASH 26 E Maintenance Manual TN 15: The original text is being replaced by the Mainenance Instruction “Ad- justing the drive belt” (Section 12.6) 2.3.1.4 Oil and Fuel Systems - Total loss oil lubrication: The engine uses a total loss oil lubrication which is supplied by a me- tering pump [9].
  • Page 270 ASH 26 E Maintenance Manual Fig.2.3-6 Belt Adjustment TN 15: The Fig. 2.3-6 is being replaced by the Mainenance Instruction “Ad- justing the drive belt” (Section 12.6) Rev.No. / Date Sig. Author Date Page No. 2.68 Heide 31.01.95 TN 15 / Jan. 08...
  • Page 271 The following Maintenance Instructions are established from time to time as required, in accordance with experience accumulated in oper- ating the ASH 26 E. The Maintenance Manual is to be supplemented by inserting any new Maintenance Instruction which may have been issued for the ASH 26 E.
  • Page 272 Alexander Schleicher Maintenance Instruction Sheet GmbH & Co. 1 of Adjusting the drive belt Segelflugzeugbau Issue I D - 36163 Poppenhausen Power-plant AE50R and IAE50R-AA Subject: The belt tension is adjusted such that the belt eigenfrequency - in the area where it is running in the channel inside both swivel support arms - corresponds to 48 Hz.
  • Page 273 Alexander Schleicher Maintenance Instruction Sheet GmbH & Co. 2 of Adjusting the drive belt Segelflugzeugbau Issue I D - 36163 Poppenhausen Frequency Measurement: As frequency meters for the special purpose of measuring belt eigenfrequency are relatively ex- pensive, there is a cheaper alternative: by means...
  • Page 274 Alexander Schleicher Maintenance Instruction Sheet GmbH & Co. 3 of Adjusting the drive belt Segelflugzeugbau Issue I D - 36163 Poppenhausen Belt running: An increased wear occurs also if the belt is running up at the washer discs of the pul- ley, particularly at the upper pulley.

  • Page 275: Type Certificate Lba

    Muster ASW 22 BE..........TM-Nr. 14 Type: ASH 25 E ..........TM-Nr. 29 ASH 26 E ..........TM-Nr. 16 Gegenstand: Austausch des Vergaserdeckels, Dichtigkeit der Entlüftungsschraube der Ölpumpe Subject Replacement of the carburettor cap, tightness of the bleeding screw on the oil pump Betroffen: ASW 22 BE..Kennblatt...

  • Page 276: Gmbh & Co

    Alexander Schleicher Blatt Technische Mitteilung für GmbH & Co. 2 von 2 Technical Note for Segelflugzeugbau D - 36163 Poppenhausen Kraftstoffleitung aufweist (Pfeile mit dunklem Rand im Bild). Kabelbinder zur Befesti- gung der Kraftstoffleitung verwenden. Nach dem Anschließen der Krafftstoffleitung ist unbedingt eine Dichtigkeitsprüfung des Kraftstoffsystems durchzuführen.
  • Page 277 Recommended Service Austro Engine GmbH Rudolf-Diesel-Strasse 11 Bulletin A-2700 Wiener Neustadt Tel: +43 2622 23000 No. RSB-AE50R-005/2 FAX: +43 2622 23000-2711 BASIC INFORMATION 1.1. SUBJECT Carburetor cap Retrofit 1.2. ENGINES AFFECTED Type: AE50RAB Serial numbers: 1.3. REASON This RSB ensures the usability of the new carburetor cap design in case of retrofit for the engine serial numbers defined under chapter 1.2.
  • Page 278 Recommended Service Austro Engine GmbH Rudolf-Diesel-Strasse 11 Bulletin A-2700 Wiener Neustadt Tel: +43 2622 23000 No. RSB-AE50R-005/2 FAX: +43 2622 23000-2711 TECHNICAL DETAILS 2.1. ACCOMPLISHMENT / INSTRUCTIONS WI-RSB-AE50R-005, latest effective issue is recommended to be complied with. 2.2. ILLUSTRATIONS None. 2.3.
  • Page 279 Recommended Service Austro Engine GmbH Rudolf-Diesel-Strasse 11 Bulletin A-2700 Wiener Neustadt Tel: +43 2622 23000 No. RSB-AE50R-005/2 FAX: +43 2622 23000-2711 3.4. CREDIT Not applicable. REMARKS NOTE: o All measures must be carried out by a certified engine station and certified engine mechanic.
  • Page 280 Austro Engine GmbH Work Instruction Rudolf-Diesel-Strasse 11 A-2700 Wiener Neustadt No. WI-RSB-AE50R-005/1 Tel: +43 2622 23000 FAX: +43 2622 23000-2711 WORK INSTRUCTION WI-RSB-AE50R-005/1 SUPERSEDES WI-RSB-AE50R-005 “EXCHANGE OF CARBURETOR CAP” I GENERAL INFORMATION I.1 Subject: All AE50R engines that are affected by service bulletin RSB-AE50R-005/2. I.2 Reference documents: None.
  • Page 281 Austro Engine GmbH Work Instruction Rudolf-Diesel-Strasse 11 A-2700 Wiener Neustadt No. WI-RSB-AE50R-005/1 Tel: +43 2622 23000 FAX: +43 2622 23000-2711 III INSTRUCTIONS III.1 Disassembly of the carburetor Release the two stop nuts [1] securing the carburetor to the engine housing and detach the carburetor from the engine housing.
  • Page 282 Austro Engine GmbH Work Instruction Rudolf-Diesel-Strasse 11 A-2700 Wiener Neustadt No. WI-RSB-AE50R-005/1 Tel: +43 2622 23000 FAX: +43 2622 23000-2711 III.3 Modification of the carburetor: The carburetor filter cap has to be modified to be able to use the new carburetor cap design.
  • Page 283 Austro Engine GmbH Work Instruction Rudolf-Diesel-Strasse 11 A-2700 Wiener Neustadt No. WI-RSB-AE50R-005/1 Tel: +43 2622 23000 FAX: +43 2622 23000-2711 Install the new carburetor cap and mount it with the cap screw and cap screw – sealing ring hand tight to the carburetor as shown in Figure 7. Secure the cap with securing wire according to Figure 7 in accordance with standard maintenance procedures.
  • Page 284 Austro Engine GmbH Work Instruction Rudolf-Diesel-Strasse 11 A-2700 Wiener Neustadt No. WI-RSB-AE50R-005/1 Tel: +43 2622 23000 FAX: +43 2622 23000-2711 WORK INSTRUCTION ARBEITSANWEISUNG WI-RSB-AE50R-005/1 SUPERSEDES /Ersetzt WI-RSB-AE50R-005 “EXCHANGE OF CARBURETOR CAP” “AUSTAUSCH DES VERGASERDECKELS” I GENERAL INFORMATION I ALLGEMEINE INFORMATION I.1 Gegenstand: I.1 Subject: Alle vom Service Bulletin RSB-AE50R-005/2 betroffenen Motoren.
  • Page 285 Austro Engine GmbH Work Instruction Rudolf-Diesel-Strasse 11 A-2700 Wiener Neustadt No. WI-RSB-AE50R-005/1 Tel: +43 2622 23000 FAX: +43 2622 23000-2711 III INSTRUCTIONS III.1 Disassembly of the carburetor Release the two stop nuts [1] securing the carburetor to the engine housing and detach the carburetor from the engine housing.
  • Page 286 Austro Engine GmbH Work Instruction Rudolf-Diesel-Strasse 11 A-2700 Wiener Neustadt No. WI-RSB-AE50R-005/1 Tel: +43 2622 23000 FAX: +43 2622 23000-2711 III.3 Modification of the carburetor: The carburetor filter cap has to be modified to be able to use the new carburetor cap design.
  • Page 287 Austro Engine GmbH Work Instruction Rudolf-Diesel-Strasse 11 A-2700 Wiener Neustadt No. WI-RSB-AE50R-005/1 Tel: +43 2622 23000 FAX: +43 2622 23000-2711 Install the new carburetor cap and mount it with the cap screw and cap screw – sealing ring hand tight to the carburetor as shown in Figure 7. Secure the cap with securing wire according to Figure 7 in accordance with standard maintenance procedures.
  • Page 288 Segelflugzeugbau No. 18 D - 36163 Poppenhausen Subject: Exchange of the steerable tailwheel Applicability: ASH 26 E, Type-Certificate LBA 383 Urgency: Optional modification, see Notes Classification: Minor Change Reason: Improvement of product by change of the steerable tailwheel and its fairing...
  • Page 289 LBA- app.:12.11.96 d) Inspection of further engine & exchange of manual pages Inspection 02.08.97 Aircraft ASH 26 E (Data Sheet Obtaining Type Certificate status as per Data Sheet 883, none, only required for FAA- No. 883) , which were exported issue 1, dated 07.08.95...
  • Page 290 ALEXANDER SCHLEICHER Table of AD-Notes and Technical Notes GMBH & CO Segelflugzeugbau ASH 26 E 04.883 Type: Data Sheet No.: D-36163 Poppenhausen Sheet: DE.21G.0010 License: LBA-AD-No. Version & Serial No. Inspec- TN-No Subject Compliance Issue Date Issue Date affected tion Ref.

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