Number |
2021-0142 |
Issued by |
Europe |
Issue date |
2021-06-17 |
Effective date |
2021-07-01 |
EASA approval number |
|
Contributor |
EASA VTOL Department |
ATA Chapter |
05 |
Approval Holder / Type Designation |
-
AIRBUS HELICOPTERS DEUTSCHLAND
-
BO 105
-
BO 105 A
-
BO 105 C
-
BO 105 D
-
BO 105 LS A-1
-
BO 105 LS A-3
-
BO 105 S
-
EASA STC 10039633
-
LBA EMZ (STC) 0654/3058
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2019-0024 dated 04 February 2019, AD 2015-0042 dated 09 March 2015, AD 2013-0015 dated 16 January 2013 and AD 2010-0153 dated 27 July 2010; and Luftfahrt-Bundesamt (LBA) Germany AD 2001-281 dated 18 October 2001 and AD 76-136/2 dated 05 October 1978.
|
Publication(s) and related information |
AHD BO105 AMM Chapter 101-15 - ALS, Issue 2, Revision 31 dated 15 December 2020.
AHD BO105 LS A-3 AMM Chapter 101-15 - ALS, Issue 4, Revision 7 dated 27 November 2018.
AHD BO105 LS A-3 ('Superlifter') AMM Appendix 010, Issue 1, Revision 4 dated 24 May 2012.
AH ASB BO105-10A-129 original issue dated 03 December 2018.
AH ASB BO105 LS-10A-017 original issue dated 03 December 2018.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
21-067 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 10 May 2021 as PAD 21-067 for consultation until 07 June 2021.
No comments were received during the consultation period.
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.
|