| Publication(s) and related information |
Saab AB SB 340-21-018 original issue dated 13 February 1987, or Revision 1 dated 18 August 1987,
or Revision 2 dated 21 June 2000, or Revision 3 dated 22 March 2001.
Saab AB SB SB340-21-063 original issue dated 26 June 2026.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD
with Request for Comments, postponing the public consultation process until after publication.
All interested persons may send their comments, referencing the AD Number, to the E-mail
address specified in below Remark 3, prior to 11 August 2026. Only if any comment is received
during the consultation period, a Comment Response Document will be published in the EASA
Safety Publications Tool, in a compressed (zipped) file, attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs[at]easa.europa.eu.
4. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on
a product, part or appliance not affected by this AD, can be reported to the EU aviation safety
reporting system. This may include reporting on the same or similar components, other than
those covered by the design to which this AD applies, if the same unsafe condition can exist or
may develop on an aircraft with those components installed. Such components may be
installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate
(STC) or other modification.
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