- Effective
- September 2, 2009
- Published
- July 29, 2009 · 74 FR 37528–37530
- Issued
- July 13, 2009
- Models
- BAe 146-100A, BAe 146-200A
- Data sheet
- TCDSA49EU
- Registered aircraft
- 8 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-15982
- Docket
- FAA-2009-0432
- Project
- 2008-NM-168-AD
- Issued as
- Final rule
Unofficial copy from the Federal Register XML, document E9-17542. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| Official PDF | 152 KB | 6f365806…5768dde | E9-17542.pdf on govinfo.gov |
| Official PDF | 139 KB | a5646ff1…44d4a0a | E9-21039.pdf on govinfo.gov |
| Federal Register XML | 22 KB | 136cc9e1…87cc26f | E9-17542.xml on federalregister.gov |
| Federal Register XML | 5 KB | 55913850…c418337 | E9-21039.xml on federalregister.gov |
| FAA DRS HTML attachment | 68 KB | 2490c4e6…ce1a0ca | FAA DRS (API key needed) |
| FAA DRS PDF | 40 KB | e6e6e71b…4defe93 | FAA DRS (API key needed) |
On this page
Summary
The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on July 29, 2009. The error resulted in an incorrect AD number appearing in one location of the document. This AD applies to certain BAE Systems (Operations) Limited Model BAe 146-100A and 146-200A series airplanes. This AD requires inspecting for damage of the horizontal stabilizer lower skin and joint plates, and doing related investigative and corrective actions.
The airworthiness directive
2009-15-19 BAE Systems (Operations) Limited (Formerly British Aerospace Regional Aircraft): Amendment 39-15982. Docket No. FAA-2009-0432; Directorate Identifier 2008-NM-168-AD.
The effective date of this AD remains September 2, 2009.
In the Federal Register of July 29, 2009, on page 37529, in the first column, paragraph 2. of PART 39—AIRWORTHINESS DIRECTIVES is corrected to read as follows:
Rule preamble
The FAA’s background, reasoning and cost estimate, published with the AD.
DatesPage 1
Effective September 2, 2009.
AddressesPage 1
You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (telephone 800-647-5527) is the Document Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590.
For further information contactPage 1
Todd Thompson, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1175; fax (425) 227-1149.
Supplementary informationPage 1
On July 13, 2009, the FAA issued AD 2009-15-19, amendment 39-15982 (74 FR 37528, July 29, 2009), for certain BAE Systems (Operations) Limited Model BAe 146-100A and 146-200A series airplanes. This AD requires inspecting for damage of the horizontal stabilizer lower skin and joint plates, and doing related investigative and corrective actions.
As published, the final rule incorrectly specified the AD number in a single location in the AD as “2008-15-19” instead of “2009-15-19.”
No other part of the regulatory information has been changed; therefore, the final rule is not republished in the Federal Register.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 8
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1985 | 1 |
|---|---|
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 2 |
2 with no year recorded