Published 2009-07-20 · Federal Register document E9-17116
Airworthiness Directives; Bombardier Model DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315 Airplanes Equipped With a Cockpit Door Electronic Strike System Installed in Accordance With Supplemental Type Certificate (STC) ST02014NY
Publication summary
The FAA is correcting an error in an existing airworthiness directive (AD) that was published in the Federal Register on April 7, 2009 (74 FR 15665). The error resulted in an incorrect product identification line in the regulatory portion of the AD. This AD applies to the transport category airplanes listed above. This AD requires modifying the electronic strike system of the cockpit door.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:30.011257+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2009-cb57e588bd107238
- Source row
- results[194]
- Raw source SHA-256
- cb57e588bd10723805ef0ea28ddc0685de14711012023c7e7d12178879efaeed
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2008-26-03
- Effective date printed in this edition
- Unknown
This correction is a separate source edition; it is not counted as a new adopted rule.
No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2008-26-03 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 9c45f890942d82554ae45baec29c1e294c6bf2c73e3878b33d417ae33375eaa1. Source manifest: b3c1cc09cc3193ef2b677373b5ba38ba8d83a5bed1516b284b62d4dc58e41a86.
Official source · 2009-07-20
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 74, Number 137 (Monday, July 20, 2009)]
[Rules and Regulations]
[Page 35115]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E9-17116]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-0313; Directorate Identifier 2008-NM-144-AD;
Amendment 39-15769; AD 2008-26-03]
RIN 2120-AA64
Airworthiness Directives; Bombardier Model DHC-8-102, DHC-8-103,
DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315
Airplanes Equipped With a Cockpit Door Electronic Strike System
Installed in Accordance With Supplemental Type Certificate (STC)
ST02014NY
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting an error in an existing airworthiness
directive (AD) that was published in the Federal Register on April 7,
2009 (74 FR 15665). The error resulted in an incorrect product
identification line in the regulatory portion of the AD. This AD
applies to the transport category airplanes listed above. This AD
requires modifying the electronic strike system of the cockpit door.
DATES: Effective April 13, 2009.
ADDRESSES: 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 CONTACT: Fabio Buttitta, Aerospace Engineer,
Systems and Flight Test Branch, ANE-171, FAA, New York Aircraft
Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New
York 11590; telephone (516) 228-7303; fax (516) 794-5531.
SUPPLEMENTARY INFORMATION: On March 30, 2009, the FAA issued AD 2008-
26-03, Amendment 39-15769 (74 FR 15665, April 7, 2009), for Bombardier
Model DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301,
DHC-8-311, and DHC-8-315 airplanes equipped with a cockpit door
electronic strike system installed in accordance with supplemental type
certificate (STC) ST02014NY. The AD requires modifying the electronic
strike system of the cockpit door.
As published in the Federal Register, the AD identifies ``TTF
Aerospace LLC'' in the product identification line of the AD; however,
the name in the product identification line was changed to
``Bombardier, Inc.,'' in the version posted to the FAA Web site (i.e.,
the Regulatory and Guidance Library (http://rgl.faa.gov)). All copies
of ADs available to the public must be consistent; therefore, we are
correcting the version of the AD published in the Federal Register to
appropriately identify Bombardier, Inc., in the product identification
line.
No other part of the regulatory information has been changed;
therefore, the final rule is not republished in the Federal Register.
The effective date of this AD remains April 13, 2009.
Sec. 39.13 [Corrected]
0
In the Federal Register of April 7, 2009, on page 15666, in the first
column, the paragraph that states ``2008-26-03 TTF Aerospace LLC:'' of
AD 2008-26-03 is corrected to read as follows:
* * * * *
2008-26-03 Bombardier, Inc.:
* * * * *
Issued in Renton, Washington, on July 8, 2009.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E9-17116 Filed 7-17-09; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:22:46.132814+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 834c595114c08f4e0d6780e805e77a756cfa63b7bd703937803557de43fd2994
- Text SHA-256
- 9c45f890942d82554ae45baec29c1e294c6bf2c73e3878b33d417ae33375eaa1
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.