| Number |
US-2009-13-06R1 |
| Issued by |
 United States of America |
| Issue date |
2011-10-25 |
| Effective date |
2011-11-03 |
| EASA approval number |
|
| ATA Chapter |
52 |
Approval Holder
/ Type Designation |
-
PIPER AIRCRAFT INC.
-
PA-23 (Apache)
-
PA-23 (Aztec)
-
PA-23-235
-
PA-23-250
-
PA-E23-250
-
PA-31 (Navajo)
-
PA-31
-
PA-31-300
-
PA-31-325
-
PA-31-350 (Chieftain)
-
PA-31P
-
PA-31P (Pressurised Navajo)
-
PA-31P-350 (Mojave)
-
PA-31T (Cheyenne)
-
PA-31T
-
PA-31T1
-
PA-31T2
-
PA-31T3
-
PA-42 (Cheyenne)
-
PA-42 (Cheyenne III)
-
PA-42-1000 (Cheyenne 400LS)
-
PA-42-720 (Cheyenne IIIA)
|
| Revision |
This AD revises FAA AD 2009-13-06. This AD was prompted by further investigation and a request for an alternative method of compliance (AMOC). This new AD removes the requirement for the nose baggage door compartment interior light inspection and retains the other requirements from FAA AD 2009-13-06.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Piper Aircraft, Inc. Service Bulletin No. 1194A, dated 10 November 2008. For service information identified in this AD, contact Piper Aircraft, Inc., 2926 Piper Drive, Vero Beach, Florida 32960; telephone: (772) 567-4361; fax: (772) 978-6573; Internet: http://www.newpiper.com/company/publications.asp. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
