18566 Federal Register / Vol. 72, No. 71 / Friday, April 13, 2007 / Rules and Regulations 

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 this AD: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866; 

(2) Is not a ‘‘significant rule’’ under 

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. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this AD and placed it in the AD Docket. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://dms.dot.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 the 

NPRM, the regulatory evaluation, any 

comments received, and other 

information. The street address for the 

Docket Office (telephone (800) 647–

5227) is in the ADDRESSES section. 

Comments will be available in the AD 

docket shortly after receipt. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

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 AD: 

2007–08–06 British Aerospace Regional 

Aircraft: Amendment 39–15023; Docket 

No. FAA–2007–27070; Directorate 

Identifier 2007–CE–003–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective May 18, 2007. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Models HP.137 

Jetstream Mk.1, Jetstream Series 200, 

Jetstream Series 3101, and Jetstream Model 

3201 airplanes, all serial numbers, 

certificated in any category. 

Subject 

(d) Air Transport Association of America 

(ATA) Code 32: Landing Gear. 

Reason 

(e) The mandatory continuing 

airworthiness information (MCAI) states: 

This Airworthiness Directive * * * is 

published in order to maintain the structural 

integrity of the applicable aircraft. The 

Service Bulletin provides life limits for 

critical landing gear components. Failure of 

such items could lead to unsafe conditions. 

Actions and Compliance 

(f) Unless already done, within 60 days 

after May 18, 2007 (the effective date of this 

AD), comply with the requirements given in 

BAE Systems British Aerospace Jetstream 

Series 3100 and 3200 Service Bulletin 32–

JA981042 Rev 5, dated November 1, 2005. 

Note 1: The compliance times of this AD 

are presented in cycles (landings) since new 

(CSN). If you do not keep the total CSN, then 

you may multiply the total number of 

airplane hours time-in-service by 0.75. 

FAA AD Differences 

Note 2: This AD differs from the MCAI 

and/or service information as follows: We 

allow a different method for calculating the 

CSN of a component listed in this AD. 

Other FAA AD Provisions 

(g) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Staff, 

FAA, ATTN: Taylor Martin, Aerospace 

Engineer, FAA, Small Airplane Directorate, 

901 Locust, Room 301, Kansas City, Missouri 

64106; telephone: (816) 329–4138; fax: (816) 

329–4090, has the authority to approve 

AMOCs for this AD, if requested using the 

procedures found in 14 CFR 39.19. Before 

using any approved AMOC on any airplane 

to which the AMOC applies, notify your 

appropriate principal inspector (PI) in the 

FAA Flight Standards District Office (FSDO), 

or lacking a PI, your local FSDO. 

(2) Airworthy Product: For any 

requirement in this AD to obtain corrective 

actions from a manufacturer or other source, 

use these actions if they are FAA-approved. 

Corrective actions are considered FAAapproved if they are approved by the State 

of Design Authority (or their delegated 

agent). You are required to assure the product 

is airworthy before it is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, under the 

provisions of the Paperwork Reduction Act 

(44 U.S.C. 3501 et seq.), the Office of 

Management and Budget (OMB) has 

approved the information collection 

requirements and has assigned OMB Control 

Number 2120–0056. 

Related Information 

(h) Refer to MCAI European Aviation 

Safety Agency (EASA) AD No.: 2006–0087, 

dated April 18, 2006, and BAE Systems 

British Aerospace Jetstream Series 3100 and 

3200 Service Bulletin 32–JA981042 Rev 5, 

dated November 1, 2005, for related 

information. 

Material Incorporated by Reference 

(i) You must use BAE Systems British 

Aerospace Jetstream Series 3100 and 3200 

Service Bulletin 32–JA981042 Rev 5, dated 

November 1, 2005, to do the actions required 

by this AD, unless the AD specifies 

otherwise. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

this service information under 5 U.S.C. 

552(a) and 1 CFR part 51. 

(2) For service information identified in 

this AD, contact Customer Information 

Department, BAE Systems, Prestwick 

International Airport, Ayshire, KA9 2RW, 

Scotland; telephone: (01292) 675207; fax: 

(01292) 675704. 

(3) You may review copies at the FAA, 

Central Region, Office of the Regional 

Counsel, 901 Locust, Room 506, Kansas City, 

Missouri 64106; or at the National Archives 

and Records Administration (NARA). For 

information on the availability of this 

material at NARA, call 202–741–6030, or go 

to: http://www.archives.gov/federal-register/

cfr/ibr-locations.html. 

Issued in Kansas City, Missouri, on April 

6, 2007. 

Kim Smith, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. E7–6913 Filed 4–12–07; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2007–27109; Directorate 

Identifier 2007–CE–005–AD; Amendment 

39–15024; AD 2007–08–07] 

RIN 2120–AA64 

Airworthiness Directives; 

LATINOAMERICANA DE AVIACIO ́ N 

(LAVIA) S.A. (Type Certificate Data 

Sheets No. 2A8 and No. 2A10 

Previously Held by The New Piper 

Aircraft, Inc.) Models PA–25, PA–25–

235, and PA–25–260 Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for the 

products listed above. This AD results 

from mandatory continuing 

airworthiness information (MCAI) 


cprice-sewell on PRODPC61 with RULES
Federal Register / Vol. 72, No. 71 / Friday, April 13, 2007 / Rules and Regulations 18567 

issued by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI references 

Latinoamericana de Aviacio ́n S.A. 

Service Bulletin No. 25/53/03, dated 

May 10, 2006, which describes the 

unsafe condition as: 

REAR AND FORWARD SUPPORTS OF 

BOTH HORIZONTAL STABILIZER 

MODIFICATION. It have been found on 

several of the affected airplanes some severe 

corrosion and cracks in both supports. The 

probable cause for those failures is the 

accumulation of steam or application 

products vapors. 

We are issuing this AD to require 

actions to correct the unsafe condition 

on these products. 

DATES: This AD becomes effective May 

18, 2007. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of May 18, 2007. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

dms.dot.gov or in person at the Docket 

Management Facility, U.S. Department 

of Transportation, 400 Seventh Street 

SW., Nassif Building, Room PL–401, 

Washington, DC. 

FOR FURTHER INFORMATION CONTACT: Mr. 

Sarjapur Nagarajan, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 

Locust, Room 301, Kansas City, 

Missouri 64106; telephone: (816) 329–

4145; fax: (816) 329–4090. 

SUPPLEMENTARY INFORMATION: 

Streamlined Issuance of AD 

The FAA is implementing a new 

process for streamlining the issuance of 

ADs related to MCAI. The streamlined 

process will allow us to adopt MCAI 

safety requirements in a more efficient 

manner and will reduce safety risks to 

the public. This process continues to 

follow all FAA AD issuance processes to 

meet legal, economic, Administrative 

Procedure Act, and Federal Register 

requirements. We also continue to meet 

our technical decision-making 

responsibilities to identify and correct 

unsafe conditions on U.S.-certificated 

products. 

This AD references the MCAI and 

related service information that we 

considered in forming the engineering 

basis to correct the unsafe condition. 

The AD contains text copied from the 

MCAI and for this reason might not 

follow our plain language principles. 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an AD that would 

apply to the specified products. That 

NPRM was published in the Federal 

Register on February 14, 2007 (72 FR 

6982). That NPRM proposed to require 

compliance with Service Bulletin No. 

25/53/03 issued by Latinoamericana de 

Aviacio ́n S.A. in order to detect cracks, 

evidence of corrosion or any other 

anomalies on support tubes of the 

horizontal stabilizer. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM or 

on the determination of the cost to the 

public. 

Conclusion 

We reviewed the available data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed. 

Differences Between This AD and the 

MCAI or Service Information 

We have reviewed the MCAI and 

related service information and, in 

general, agree with their substance. But 

we might have found it necessary to use 

different words from those in the MCAI 

to ensure the AD is clear for U.S. 

operators and is enforceable in a U.S. 

court of law. In making these changes, 

we do not intend to differ substantively 

from the information provided in the 

MCAI and related service information. 

We might also have required different 

actions in this AD from those in the 

MCAI in order to follow FAA policies. 

Any such differences are described in a 

separate paragraph of the AD. These 

requirements, if any, take precedence 

over the actions copied from the MCAI. 

Costs of Compliance 

We estimate that this AD will affect 

1,144 products of U.S. registry. We also 

estimate that it will take about 10 workhours per product to comply with this 

AD. The average labor rate is $80 per 

work-hour. Required parts will cost 

about $845 per product. Where the 

service information lists required parts 

costs that are covered under warranty, 

we have assumed that there will be no 

charge for these parts. As we do not 

control warranty coverage for affected 

parties, some parties may incur costs 

higher than estimated here. Based on 

these figures, we estimate the cost of 

this AD to the U.S. operators to be 

$1,881,880, or $1,645 per product. 

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 

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 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 this AD: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866; 

(2) Is not a ‘‘significant rule’’ under 

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. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this AD and placed it in the AD Docket. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://dms.dot.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 the 

NPRM, the regulatory evaluation, any 

comments received, and other 

information. The street address for the 

Docket Office (telephone (800) 647–

5227) is in the ADDRESSES section. 

Comments will be available in the AD 

docket shortly after receipt. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

■ Accordingly, under the authority 

delegated to me by the Administrator, 


cprice-sewell on PRODPC61 with RULES
18568 Federal Register / Vol. 72, No. 71 / Friday, April 13, 2007 / Rules and Regulations 

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 AD: 

2007–08–07 LATINOAMERICANA DE 

AVIACIO ́ N (LAVIA) S.A. (Type 

Certificate Data Sheets No. 2A8 and No. 

2A10 previously held by The New Piper 

Aircraft, Inc.): Amendment 39–15024; 

Docket No. FAA–2007–27109; 

Directorate Identifier 2007–CE–005–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective May 18, 2007. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Models PA–25, PA–

25–235, and PA–25–260, all serial numbers 

up to LA–260–06008, certificated in any 

category. 

Subject 

(d) Air Transport Association of America 

(ATA) Code 55: Stabilizers. 

Reason 

(e) The mandatory continuing 

airworthiness information (MCAI) references 

Latinoamericana de Aviacio ́n S.A. Service 

Bulletin No. 25/53/03, dated May 10, 2006, 

which states: 

REAR AND FORWARD SUPPORTS OF 

BOTH HORIZONTAL STABILIZER 

MODIFICATION. It has been found on 

several of the affected airplanes some severe 

corrosion and cracks in both supports. The 

probable cause for those failures is the 

accumulation of steam or application 

products vapors. 

Actions and Compliance 

(f) Unless already done, do the following 

actions: 

(1) Upon accumulating 1,500 hours timein-service (TIS) or within the next 50 hours 

TIS after May 18, 2007 (the effective date of 

this AD), whichever occurs later, do the 

operations as specified in the paragraph 

‘‘ACTIONS,’’ subparagraph ‘‘INITIAL’’ of 

Latinoamericana de Aviacio ́n S.A. Service 

Bulletin No. 25/53/03, dated May 10, 2006. 

Repetitively inspect thereafter every 100 

hours TIS or 12 months, whichever occurs 

first, until the modification specified in 

paragraph ‘‘ACTIONS,’’ subparagraph 

‘‘DEFINITIVE’’ of Latinoamericana de 

Aviacio ́n S.A. Service Bulletin No. 25/53/03, 

dated May 10, 2006, is done. 

(2) If any evidence of cracks, signs of 

corrosion, or any other discrepancy is 

detected during any inspection required in 

paragraph (f)(1) of this AD, before further 

flight, disassemble both horizontal stabilizers 

and conduct a detailed inspection on the 

surface of both supports and take corrective 

action. Use paragraph ‘‘ACTIONS,’’

subparagraph ‘‘DEFINITIVE’’ of 

Latinoamericana de Aviacio ́n S.A. Service 

Bulletin No. 25/53/03, dated May 10, 2006. 

(3) After incorporating the modification 

specified in paragraph ‘‘ACTIONS,’’

subparagraph ‘‘DEFINITIVE’’ of 

Latinoamericana de Aviacio ́n S.A. Service 

Bulletin No. 25/53/03, dated May 10, 2006, 

no further action is required. 

(4) Upon accumulating 1,000 hours TIS 

after May 18, 2007 (the effective date of this 

AD), modify both horizontal stabilizers as 

specified in paragraph ‘‘ACTIONS,’’

subparagraph ‘‘DEFINITIVE’’ of 

Latinoamericana de Aviacio ́n S.A. Service 

Bulletin No. 25/53/03, dated May 10, 2006, 

unless already done. Incorporating this 

modification terminates the repetitive 

inspection requirement in paragraph (f)(1) of 

this AD. 

(5) As a terminating action to the 

inspection requirements of this AD, the 

modification to both horizontal stabilizers 

specified in paragraph ‘‘ACTIONS,’’

subparagraph ‘‘DEFINITIVE’’ of 

Latinoamericana de Aviacio ́n S.A. Service 

Bulletin No. 25/53/03, dated May 10, 2006, 

may be incorporated at any time after the 

effective date of this AD and before the time 

required in paragraph (f)(4) of this AD. 

FAA AD Differences 

Note: This AD differs from the MCAI and/ 

or service information as follows: No 

differences. 

Other FAA AD Provisions 

(g) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Staff, 

FAA, Small Airplane Directorate, ATTN: 

Sarjapur Nagarajan, Aerospace Engineer, 901 

Locust, Room 301, Kansas City, Missouri 

64106; telephone: (816) 329–4145; fax: (816) 

329–4090, has the authority to approve 

AMOCs for this AD, if requested using the 

procedures found in 14 CFR 39.19. 

(2) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, under the 

provisions of the Paperwork Reduction Act 

(44 U.S.C. 3501 et.seq.), the Office of 

Management and Budget (OMB) has 

approved the information collection 

requirements and has assigned OMB Control 

Number 2120–0056. 

Related Information 

(h) Refer to MCAI Direccio ́n Nacional de 

Aeronavegabilidad AD No. RA 2006–06–01, 

Rev. 1 LAVIA S.A., Amendment No. 39/03–

041, dated November 17, 2006; and 

Latinoamericana de Aviacio ́n S.A. Service 

Bulletin No. 25/53/03, dated May 10, 2006, 

for related information. 

Material Incorporated by Reference 

(i) You must use Latinoamericana de 

Aviacio ́n S.A. Service Bulletin No. 25/53/03, 

dated May 10, 2006, to do the actions 

required by this AD, unless the AD specifies 

otherwise. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

this service information under 5 U.S.C. 

552(a) and 1 CFR part 51. 

(2) For service information identified in 

this AD, contact Latinoamericana de 

Aviacio ́n S.A., Hangar No. 1 Aeropuerto ‘‘El 

Plumerillo’’ sur, Las Heras-MendozaArgentina—CP 5541; telephone: 0054–261–

4489198; e-mail: laviasa@hotmail.com. 

(3) You may review copies at the FAA, 

Central Region, Office of the Regional 

Counsel, 901 Locust, Room 506, Kansas City, 

Missouri 64106; or at the National Archives 

and Records Administration (NARA). For 

information on the availability of this 

material at NARA, call 202–741–6030, or go 

to: http://www.archives.gov/federal-register/ 

cfr/ibr-locations.html. 

Issued in Kansas City, Missouri, on April 

6, 2007. 

Kim Smith, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. E7–6929 Filed 4–12–07; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2006–26719; Airspace 

Docket No. 06–AAL–41] 

Revision of Class E Airspace; Valdez, 

AK 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action revises Class E 

airspace at Valdez, AK to provide 

adequate controlled airspace to contain 

aircraft executing Standard Instrument 

Approach Procedures (SIAPs). The FAA 

Instrument Flight Procedures 

Production and Maintenance Branch 

has drafted two new SIAPs for the 

Valdez Pioneer Field Airport at Valdez, 

AK. This rule results in the revision of 

Class E airspace upward from 700 feet 

(ft.) and 1,200 ft. above the surface at 

Valdez, AK. 

DATES: Effective Date: 0901 UTC, July 5, 

2007. The Director of the Federal 

Register approves this incorporation by 

reference action under title 1, Code of 

Federal Regulations, part 51, subject to 

the annual revision of FAA Order 


cprice-sewell on PRODPC61 with RULES