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ASW 20, all production versions Technical Note No. 39

ALEXANDER SCHLEICHER ASW 20 C · Maintenance Manual

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Overview

This document is a technical note regarding the maintenance and inspection program for the Alexander Schleicher ASW 20 C glider. It outlines amendments to the maintenance manual and details an inspection program aimed at increasing the service life of the aircraft.

  • Applicable to all production versions of ASW 20.
  • Amendments must be made prior to the next annual C. of A. inspection.
  • Inspection program required before reaching 3000 or 6000 flight hours.
  • CFRP wings and spars can reach a service life of 12000 hours.
  • Long-term airworthiness must be demonstrated through a multi-stage inspection.
  • Maintenance manual pages must be updated and documented.
  • Inspections must be performed by the manufacturer or licensed service stations.
  • The amendment can be done by the operator.

Document

Source

Originally published by alexander-schleicher.de. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Maintenance Manual
Year
·
1998
File size
·
13 KB
Publisher
·
alexander-schleicher.de
Language
·
en
About this document
What is the ASW 20, all production versions Technical Note No. 39?

The ASW 20, all production versions Technical Note No. 39 is a maintenance manual for the ALEXANDER SCHLEICHER ASW 20 C, dated 1998.

Where does the ASW 20, all production versions Technical Note No. 39 come from?

This copy of the ASW 20, all production versions Technical Note No. 39 was originally published by alexander-schleicher.de and is hosted on Sprinkle as a free, searchable reference copy.

What year was the ASW 20, all production versions Technical Note No. 39 published?

The ASW 20, all production versions Technical Note No. 39 — the ALEXANDER SCHLEICHER ASW 20 C maintenance manual on file — is dated 1998.

Documentation completeness
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In this document

Subject

Amendment of the Maintenance Manual and Inspection Program to Increase Service Life.

Compliance

Changes must be made before the next annual C. of A. inspection or by Dec. 31, 1998, and before reaching specified flight hours.

Reason

Fatigue tests indicate a potential service life of 12000 hours for CFRP components, contingent on individual aircraft inspections.

Action

Exchange maintenance manual pages and document changes in the Index of Corrections or Amendments.

Material & Drawings

Maintenance manual pages and inspection program can be ordered from the manufacturer or local agency.

Notes

Inspections must be certified by a licensed aviation inspector and can only be performed by authorized personnel.

Safety notes

  • Inspection to increase service life must be done by the manufacturer or licensed service stations.
  • Accomplishment must be certified in the glider logbook.
  • Operators can amend the manual themselves.

Full document text

Sheet 1 of 1 \TM\20\20tm39e.doc //translated RBG// ASW 20, all production versions Technical Note No. 39 Alexander Schleicher GmbH & Co. Segelflugzeugbau D - 36163 Poppenhausen Subject: A) Amendment of the Maintenance Manual. B) Inspection Program To Increase The Service Life. Serial number applicability: ASW 20, all production versions, Data Sheet No. L-314. Compliance: A) Prior to the next annual C. of A. inspection, but before or on Dec. 31, 1998, at the latest. B) Prior to reaching a total service life of 3000 or 6000 flight hours respectively. Reason: Fatigue tests on CFRP wings and CFRP wing spars have shown that a service life ex- pectancy of 12000 hours can be reached for these components without problems. However, as this fatigue test program did not examine the entire aircraft made of CFRP and GRP, this service life of 12000 hours can be granted only if the long-term airworthi- ness of each individual aircraft is demonstrated in a special multi-stage inspection pro- gram (over and above the mandatory annual C of A inspections) for the purpose of in- creasing the service life. Action: The Maintenance Manual pages must be exchanged for new pages with the same page no., but with the revision entry & date „Issue 16.02.98 Jumtow / Revision: TN-No. 39“ and the additional new pages must be inserted. The accomplishment of the change to the Manual must be documented on Page "Index of Corrections" (Maintenance Manual) or Page "Amendments to the Manual" (Operations Manual) respectively. The instruc- tions and notes given in the amended and in the new manual pages must be regarded! For ASW 20 Operations Manual pages: 40a, 40b, 40l & 40s For ASW 20 L Operations Manual pages: 44a, 44b, 44l & 44s For ASW 20 B Maintenance Manual pages: 57, 58, 59 & 71 For ASW 20 BL Maintenance Manual pages: 57, 58, 59 & 71 For ASW 20 C Maintenance Manual pages: 57, 58, 59 & 71 For ASW 20 CL Maintenance Manual pages: 57, 58, 59 & 71 Material & Drawings: Maintenance Manual pages, Maintenance Instructions, as well as the "Inspection Pro- gram To Increase The Service Life" can be ordered from Messrs. SCHLEICHER, or from the SCHLEICHER agency in your country. You always need to state the glider type and serial number. Alexander Schleicher GmbH & Co. P.O.Box 60 D-36161 Poppenhausen Tel +49 6658 890 or Fax +49 6658 8940 Notes: The "Inspection To Increase The Service Life" must only be accomplished by the manu- facturer or by a technical aviation service station holding an appropriate license; the ac- complishment must be certified by a licensed aviation inspector in the glider logbook and in the glider inspection certificates. The amendment to the Manual can be done by the operator of the glider himself. Poppenhausen, February 16, 1998 Alexander Schleicher GmbH & Co. By order Lutz-W. Jumtow) The German original of this Technical Note has been approved by the LBA under the date of April 7, 1998 (signature: U. Kopp). The translation into English has been done by best knowledge and judge- ment; in any case of doubt the German original is controlling.