Federal Register / Vol. 74, No. 65 / Tuesday, April 7, 2009 / Rules and Regulations 15665 

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; request for 

comments. 

SUMMARY: This document publishes in 

the Federal Register an amendment 

adopting airworthiness directive (AD) 

2008–26–03. This AD requires 

modifying the electronic strike system 

of the cockpit door. This AD results 

from a report indicating that the 

equipment is defective. We are issuing 

this AD to prevent failure of this 

equipment, which could compromise 

flight safety. 

DATES: This AD becomes effective 

April 13, 2009 to all persons. 

We must receive comments on this 

AD by May 7, 2009. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: 202–493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue, SE., 

Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue, SE., 

Washington, DC 20590, between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. 

Examining the AD Docket 

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 street address for 

the Docket Office (telephone 800–647– 

5527) is in the ADDRESSES section. 

Comments will be available in the AD 

docket shortly after receipt. 

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: 

Discussion 

Transport Canada Civil Aviation 

(TCCA), which is the airworthiness 

authority for Canada, notified us that an 

unsafe condition may exist on 

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) 

SA03–70 issue No. 1 or issue No. 2 

(which is equivalent to STC 

ST02014NY). TCCA advises that the 

electronic strike system of the cockpit 

door is defective. (STC SA03–70 issue 

No. 3 incorporates the enhanced 

security measures for these doors.) 

Defective equipment, if not corrected, 

could compromise flight safety. 

Transport Canada Civil Aviation (TCCA) 

issued Canadian airworthiness directive 

CF–2008–26R1, dated August 15, 2008 

(referred to after this as the Mandatory 

Continuing Airworthiness Information 

or ‘‘MCAI’’) to ensure the continued 

airworthiness of these airplanes in 

Canada. 

FAA’s Determination and Requirements 

of this AD 

This product has been approved by 

the aviation authority of another 

country, and is approved for operation 

in the United States. Pursuant to our 

bilateral agreement with the State of 

Design Authority, we have been notified 

of the unsafe condition described in the 

MCAI referenced above. We are issuing 

this AD because we evaluated all 

pertinent information and determined 

an unsafe condition exists and is likely 

to exist or develop on other products of 

the same type design. 

Therefore, we are issuing AD 2008– 

26–03 to prevent failure of the 

electronic strike system, which could 

compromise flight safety. This AD 

requires modifying the electronic strike 

system of the cockpit door in 

accordance with a method approved by 

the Manager, New York Aircraft 

Certification Office (ACO), FAA. 

None of the airplanes affected by this 

action are on the U.S. Register. 

Therefore, providing notice and 

opportunity for public comment is 

unnecessary before this AD is issued, 

and this AD may be made effective in 

less than 30 days after it is published in 

the Federal Register. However, this rule 

is necessary to ensure that the described 

unsafe condition is addressed if any of 

these products are placed on the U.S. 

Register in the future. The AD is hereby 

published in the Federal Register as an 

amendment to section 39.13 of the 

Federal Aviation Regulations (14 CFR 

39.13) to make it effective to all persons. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not provide you with notice and 

an opportunity to provide your 

comments before it becomes effective. 

However, we invite you to send any 

written data, views, or arguments about 

this AD. Send your comments to an 

address listed under the ADDRESSES

section. Include ‘‘Docket No. FAA– 

2009–0313; Directorate Identifier 2008– 

NM–144–AD’’ at the beginning of your 

comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this AD. We will consider all 

comments received by the closing date 

and may amend this AD because of 

those comments. 

We will post all comments we 

receive, without change, to http:// 

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

about this AD. 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. Subtitle I, 

Section 106, describes the authority of 

the FAA Administrator. Subtitle VII, 

Aviation Programs, describes in more 

detail the scope of the Agency’s 

authority. 

We are issuing this rulemaking under 

the authority described in Subtitle VII, 

Part A, Subpart III, Section 44701, 

‘‘General requirements.’’ Under that 

section, Congress charges the FAA with 

promoting safe flight of civil aircraft in 

air commerce by prescribing regulations 

for practices, methods, and procedures 

the Administrator finds necessary for 

safety in air commerce. This regulation 

15666 Federal Register / Vol. 74, No. 65 / Tuesday, April 7, 2009 / Rules and Regulations 

1 17 CFR 232.201. 

2 17 CFR 232.202. 

3 17 CFR 232.405. 

4 17 CFR 232.10 et seq. 

5 17 CFR 239.39. 

6 17 CFR 239.40. 

7 15 U.S.C. 77a et seq. 

8 17 CFR 249.220f. 

9 17 CFR 249.240f. 

10 17 CFR 249.306. 

11 15 U.S.C. 78a et seq. 

12The corrections we are making in this release 

do not affect the amendments we adopted in 

Release No. 33–9006 (Feb. 11, 2009) [74 FR 7748] 

even though some of the amendments restated text 

that we now are correcting. We anticipate, however, 

that we will make conforming corrections to such 

amendments. 

13 17 CFR 232.201(a). 

14See Release No. 33–8981 (Oct. 29, 2008) [73 FR 

65516]. 

15 15 U.S.C. 80a–1 et seq. 

is within the scope of that authority 

because it addresses an unsafe condition 

that is likely to exist or develop on 

products identified in this rulemaking 

action. 

Regulatory Findings 

We have determined that this AD will 

not have federalism implications under 

Executive Order 13132. This AD will 

not have a substantial direct effect on 

the States, on the relationship between 

the national government and the States, 

or on the distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify that the regulation: 

1. Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866; 

2. Is not a ‘‘significant rule’’ under the 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979); and 

3. Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Safety. 

Adoption of the Amendment 

■ Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 14 CFR part 39 as 

follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive (AD): 

2008–26–03 TTF Aerospace LLC: 

Amendment 39–15769. Docket No. 

FAA–2009–0313; Directorate Identifier 

2008–NM–144–AD. 

Effective Date 

(a) This sensitive security airworthiness 

directive (AD) is effective April 13, 2009. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to 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, certificated 

in any category, equipped with a cockpit 

door electronic strike system installed in 

accordance with supplemental type 

certificate (STC) ST02014NY (which is 

equivalent to STC SA03–70). 

Unsafe Condition 

(d) This AD results from a report indicating 

that the equipment is defective. We are 

issuing this AD to prevent failure of this 

equipment, which could compromise flight 

safety. 

Compliance 

(e) Comply with this AD within the 

compliance times specified, unless already 

done. 

Modification 

(f) Within 90 days after the effective date 

of this AD, modify the electronic strike 

system of the cockpit door in accordance 

with a method approved by the Manager, 

New York Aircraft Certification Office (ACO), 

FAA, or Transport Canada Civil Aviation 

(TCCA) (or its delegated agent). 

Alternative Methods of Compliance 

(AMOCs) 

(g)(1) The Manager, New York ACO, FAA, 

has the authority to approve AMOCs for this 

AD, if requested using the procedures found 

in 14 CFR 39.19. Send information to ATTN: 

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. 

(2) To request a different method of 

compliance or a different compliance time 

for this AD, follow the procedures in 14 CFR 

39.19. Before using any approved AMOC on 

any airplane to which the AMOC applies, 

notify your principal maintenance inspector 

(PMI) or principal avionics inspector (PAI), 

as appropriate, or lacking a principal 

inspector, your local Flight Standards District 

Office. The AMOC approval letter must 

specifically reference this AD. 

Related Information 

(h) Canadian airworthiness directive CF– 

2008–26R1, dated August 15, 2008, also 

addresses the subject of this AD. 

Material Incorporated by Reference 

(i) None. 

Issued in Renton, Washington, on 

March 30, 2009. 

Stephen P. Boyd, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. E9–7781 Filed 4–6–09; 8:45 am] 

BILLING CODE 4910–13–P 

SECURITIES AND EXCHANGE 

COMMISSION 

17 CFR Parts 232, 239 and 249 

[Release Nos. 33–9002A; 34–59324A; 39– 

2461A; IC–28609A; File No. S7–11–08] 

RIN 3235–AJ71 

Interactive Data To Improve Financial 

Reporting 

AGENCY: Securities and Exchange 

Commission. 

ACTION: Final rule; correction. 

SUMMARY: We are making technical 

corrections to rules adopted in Release 

No. 33–9002 (January 30, 2009), which 

were published in the Federal Register 

on February 10, 2009 (74 FR 6776). The 

rules relate to requiring specified public 

companies and foreign private issuers to 

provide financial statement information 

to the Commission and on their 

corporate Web sites in interactive data 

format using the eXtensible Business 

Reporting Language (XBRL). 

DATES: Effective Date: April 13, 2009. 

FOR FURTHER INFORMATION CONTACT: 

Mark W. Green, Senior Special Counsel 

(Regulatory Policy), Division of 

Corporation Finance at (202) 551–3430; 

or Jeffrey W. Naumann, Assistant 

Director, Office of Interactive Disclosure 

at (202) 551–5352, U.S. Securities and 

Exchange Commission, 100 F Street, 

NE., Washington, DC 20549–3628. 

SUPPLEMENTARY INFORMATION: We are 

correcting Rules 201,1 202 2 and 405 3 of 

Regulation S–T4 and Forms F–9 5 and 

F–10 6 under the Securities Act of 1933 

(Securities Act) 7 and Forms 20–F,8 40– 

F 9 and 6–K 10 under the Securities 

Exchange Act of 1934 (Exchange Act) 11

as published.12

I. Discussion of Corrections 

A. Rule 201—Temporary Hardship 

Exemption 

In the introductory text of paragraph 

(a) 13 of Rule 201, we inadvertently 

omitted language that became part of the 

text effective January 1, 2009 14 and 

serves to exclude from temporary 

hardship exemption availability an 

application for an order under any 

section of the Investment Company 

Act.15 We are correcting that omission.