Safety Publications Tool
21-093R2 : UMLAUT ENGINEERING GmbH – Hand-operated Fire Extinguishers – Inspection / Replacement
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EASA approval number
EASA General Aviation & VTOL Department
/ Type Designation
ATA 26 FIRE PROTECTION
Prompted by operator comments on the need to capture all aircraft that could have an affected extinguisher installed, PAD 21-093R2 is issued to make the AD applicable to the affected fire extinguishers, irrespective of the aircraft type(s) on which they are (to be) installed. This revised PAD also refers to the VSB at issue B and introduces text changes, not affecting the requirements, to improve clarity. The consultation period is further extended.
Publication(s) and related information
umlaut Engineering GmbH VSB P3VSB000003 (formerly P3 Engineering GmbH) original issue (issue A) dated 10 May 2021 or issue B dated 14 July 2021. The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD.
1. This Proposed AD will be closed for consultation on 30 July 2021. This Proposed AD was previously posted on 01 July 2021 as PAD 21-093, republished on 13 July 2021 as PAD 21-093R1 and closed for consultation on 15 July 2021. The Comment Response Documents can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this PAD. 2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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.
EASA_PAD_21_093_R2.pdf (209 kb)
EASA_PAD_21_093_R2.zip (1 mb)
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