Federal Register / Vol. 76, No. 63 / Friday, April 1, 2011 / Rules and Regulations 18031 

Credit for Actions Accomplished in 

Accordance With Previous Service 

Information 

(i) Inspections accomplished before the 

effective date of this AD according to Fokker 

Service Bulletin SBF28–57–097, dated May 

6, 2010, are considered acceptable for 

compliance with the requirements of 

paragraph (g) of this AD. 

FAA AD Differences 

Note 1: This AD differs from the MCAI 

and/or service information as follows: No 

differences. 

Other FAA AD Provisions 

(j) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, FAA, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

In accordance with 14 CFR 39.19, send your 

request to your principal inspector or local 

Flight Standards District Office, as 

appropriate. If sending information directly 

to the International Branch, sent it to ATTN: 

Tom Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue, SW., Renton, Washington 98057– 

3356; telephone (425) 227–1137; fax (425) 

227–1149. Information may be e-mailed to: 9- 

ANM-116-AMOC-REQUESTS@faa.gov. 

Before using any approved AMOC, notify 

your appropriate principal inspector, or 

lacking a principal inspector, the manager of 

the local flight standards district office/ 

certificate holding district office. The AMOC 

approval letter must specifically reference 

this AD. 

(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. 

Related Information 

(k) Refer to MCAI European Aviation 

Safety Agency (EASA) Airworthiness 

Directive 2010–0156, dated August 3, 2010; 

and Fokker Service Bulletin SBF28–57–097, 

Revision 1, dated June 10, 2010; for related 

information. 

Material Incorporated by Reference 

(l) You must use Fokker Service Bulletin 

SBF28–57–097, Revision 1, dated June 10, 

2010, 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 Fokker Services B.V., 

Technical Services Dept., P.O. Box 231, 2150 

AE Nieuw-Vennep, the Netherlands; 

telephone +31 (0)252–627–350; fax +31 

(0)252–627–211; e-mail 

technicalservices.fokkerservices@stork.com; 

Internet http://www.myfokkerfleet.com. 

(3) You may review copies of the service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue, SW., Renton, 

Washington. For information on the 

availability of this material at the FAA, call 

425–227–1221. 

(4) You may also review copies of the 

service information that is incorporated by 

reference 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/ 

code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Renton, Washington, on March 

15, 2011. 

Kalene C. Yanamura, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2011–7202 Filed 3–31–11; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2011–0261; Directorate 

Identifier 2011–NM–028–AD; Amendment 

39–16648; AD 2011–07–11] 

RIN 2120–AA64 

Airworthiness Directives; Dassault 

Aviation Model Mystere-Falcon 50 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for the 

products listed above. This AD results 

from mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as: 

On two occurrences on Myste`re-Falcon 50 

aeroplanes in service, it was detected that 

two pipes had been swapped in maintenance 

at the frame 42 firewall. The swapped lines 

are the extinguishing system line to engine # 

2, and engine # 2 Low Pressure (LP) bleed 

line. 

If the swapping of these two lines is not 

detected and corrected, in case of engine # 

2 fire, the fire extinguishing capability would 

not be operational. 

* * * * * 

This AD requires actions that are 

intended to address the unsafe 

condition described in the MCAI. 

DATES: This AD becomes effective April 

18, 2011. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of April 18, 2011. 

We must receive comments on this 

AD by May 16, 2011. 

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 W12–40, 1200 New Jersey 

Avenue, SE., Washington, DC, 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 Operations office 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 Operations 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: Tom 

Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue, SW., Renton, 

Washington 98057–3356; telephone 

425–227–1137; fax 425–227–1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Community, has issued EASA 

Emergency Airworthiness Directive 

2011–0025–E, dated February 18, 2011 

(referred to after this as ‘‘the MCAI’’), to 

correct an unsafe condition for the 

specified products. The MCAI states: 

On two occurrences on Myste`re-Falcon 50 

aeroplanes in service, it was detected that 

two pipes had been swapped in maintenance 

at the frame 42 firewall. The swapped lines 

are the extinguishing system line to engine # 

2, and engine # 2 Low Pressure (LP) bleed 

line. 

If the swapping of these two lines is not 

detected and corrected, in case of engine # 


jlentini on DSKJ8SOYB1PROD with RULES
18032 Federal Register / Vol. 76, No. 63 / Friday, April 1, 2011 / Rules and Regulations 

2 fire, the fire extinguishing capability would 

not be operational. 

For the reasons described above, this 

[EASA] AD requires an [visual] inspection of 

the connection of the two lines 

(extinguishing and LP bleed lines) at frame 

42 in the rear compartment and, in case of 

findings, proper re-installation of the lines. 

This [EASA] AD requires as well reporting to 

Dassault Aviation. 

This [EASA] AD is considered to be an 

interim measure and, depending on the 

inspection results provided by operators, 

further AD action may follow. 

You may obtain further information 

by examining the MCAI in the AD 

docket. 

Relevant Service Information 

Dassault Aviation has issued Service 

Bulletin F50–519, dated February 18, 

2011. The actions described in this 

service information are intended to 

correct the unsafe condition identified 

in the MCAI. 

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 and service information 

referenced above. We are issuing this 

AD because we evaluated all pertinent 

information and determined the unsafe 

condition exists and is likely to exist or 

develop on other products of the same 

type design. 

Differences Between the 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 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 highlighted in 

a NOTE within the AD. 

FAA’s Determination of the Effective 

Date 

An unsafe condition exists that 

requires the immediate adoption of this 

AD. The FAA has found that the risk to 

the flying public justifies waiving notice 

and comment prior to adoption of this 

rule because the swapping of the 

number 2 engine fire extinguishing line 

and the number 2 engine low pressure 

bleed line results in a dormant failure of 

the fire extinguishing capabilities of the 

number 2 engine. Therefore, we 

determined that notice and opportunity 

for public comment before issuing this 

AD are impracticable and that good 

cause exists for making this amendment 

effective in fewer than 30 days. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not precede it by notice and 

opportunity for public comment. We 

invite you to send any written relevant 

data, views, or arguments about this AD. 

Send your comments to an address 

listed under the ADDRESSES section. 

Include ‘‘Docket No. FAA–2011–0261; 

Directorate Identifier 2011–NM–028– 

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 

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 

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 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), 

(3) Will not affect intrastate aviation 

in Alaska, and 

(4) 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, 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: 

2011–07–11 Dassault Aviation: 

Amendment 39–16648. Docket No. 

FAA–2011–0261; Directorate Identifier 

2011–NM–028–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective April 18, 2011. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Dassault Aviation 

Model Mystere-Falcon 50 airplanes, all serial 

numbers, certificated in any category. 

Subject 

(d) Air Transport Association (ATA) of 

America Code 26: Fire protection. 

Reason 

(e) The mandatory continued airworthiness 

information (MCAI) states: 

On two occurrences on Myst ́re-Falcon 50 

aeroplanes in service, it was detected that 

two pipes had been swapped in maintenance 

at the frame 42 firewall. The swapped lines 

are the extinguishing system line to engine 

# 2, and engine # 2 Low Pressure (LP) bleed 

line. 

If the swapping of these two lines is not 

detected and corrected, in case of engine 


jlentini on DSKJ8SOYB1PROD with RULES
Federal Register / Vol. 76, No. 63 / Friday, April 1, 2011 / Rules and Regulations 18033 

# 2 fire, the fire extinguishing capability 

would not be operational. 

* * * * * 

Compliance 

(f) You are responsible for having the 

actions required by this AD performed within 

the compliance times specified, unless the 

actions have already been done. 

Actions 

(g) Within 8 days after the effective date of 

this AD: Visually inspect the extinguishing 

system line and the low pressure bleed line 

of the number 2 engine at frame 42 in the rear 

compartment to determine proper 

installation of the lines, in accordance with 

paragraph 2.B.(1) of the Accomplishment 

Instructions of Dassault Service Bulletin 

F50–519, dated February 18, 2011. 

(1) If the lines are properly installed, no 

further action is required by this paragraph. 

(2) If the lines are improperly installed, 

before further flight, do the actions specified 

in paragraphs (g)(2)(i) and (g)(2)(ii) of this 

AD, in accordance with paragraph 2.B.(1) of 

the Accomplishment Instructions of Dassault 

Service Bulletin F50–519, dated February 18, 

2011. 

(i) Inspect the improperly installed lines 

for deformation. 

(A) If no deformation is found on the 

improperly installed lines, before further 

flight, re-install the lines using the proper 

connections, in accordance with paragraph 

2.B.(1) of the Accomplishment Instructions of 

Dassault Service Bulletin F50–519, dated 

February 18, 2011. 

(B) If any deformation is found on the 

improperly installed lines, before further 

flight, replace the lines in accordance with 

paragraph 2.B.(1) of the Accomplishment 

Instructions of Dassault Service Bulletin 

F50–519, dated February 18, 2011. 

(ii) Verify the correct connection of the 

lines in accordance with paragraph 2.B.(1) of 

the Accomplishment Instructions of Dassault 

Service Bulletin F50–519, dated February 18, 

2011. 

Reporting Requirement 

(h) Submit a report of the findings (both 

positive and negative) of the inspection 

required by paragraph (g) of this AD to 

Dassault Aviation, as specified in paragraph 

2.B.(2) of the Accomplishment Instructions of 

Dassault Service Bulletin F50–519, dated 

February 18, 2011. Submit the report at the 

applicable time specified in paragraph (h)(1) 

or (h)(2) of this AD. The report must include 

the information identified in Dassault Service 

Bulletin F50–519, dated February 18, 2011. 

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 contained in this AD and has 

assigned OMB Control Number 2120–0056. 

(1) If the inspection was done on or after 

the effective date of this AD: Submit the 

report within 10 days after the inspection. 

(2) If the inspection was done before the 

effective date of this AD: Submit the report 

within 10 days after the effective date of this 

AD. 

FAA AD Differences 

Note 1: This AD differs from the MCAI 

and/or service information as follows: No 

Differences. 

Other FAA AD Provisions 

(i) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, FAA, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

In accordance with 14 CFR 39.19, send your 

request to your principal inspector or local 

Flight Standards District Office, as 

appropriate. If sending information directly 

to the International Branch, send it to ATTN: 

Tom Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue, SW., Renton, Washington 98057– 

3356; telephone 425–227–1137; fax 425–227– 

1149. Information may be e-mailed to: 

9-ANM-116-AMOC-REQUESTS@faa.gov. 

Before using any approved AMOC, notify 

your appropriate principal inspector, or 

lacking a principal inspector, the manager of 

the local flight standards district office/ 

certificate holding district office. The AMOC 

approval letter must specifically reference 

this AD. 

(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: A federal 

agency may not conduct or sponsor, and a 

person is not required to respond to, nor 

shall a person be subject to a penalty for 

failure to comply with a collection of 

information subject to the requirements of 

the Paperwork Reduction Act unless that 

collection of information displays a current 

valid OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public reporting for 

this collection of information is estimated to 

be approximately 5 minutes per response, 

including the time for reviewing instructions, 

completing and reviewing the collection of 

information. All responses to this collection 

of information are mandatory. Comments 

concerning the accuracy of this burden and 

suggestions for reducing the burden should 

be directed to the FAA at: 800 Independence 

Ave., SW., Washington, DC 20591, Attn: 

Information Collection Clearance Officer, 

AES–200. 

Related Information 

(j) Refer to MCAI European Aviation Safety 

Agency Emergency Airworthiness Directive 

2011–0025–E, dated February 18, 2011; and 

Dassault Service Bulletin F50–519, dated 

February 18, 2011; for related information. 

Material Incorporated by Reference 

(k) You must use Dassault Service Bulletin 

F50–519, dated February 18, 2011, 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 Dassault Falcon Jet, P.O. Box 

2000, South Hackensack, New Jersey 07606; 

telephone 201–440–6700; Internet http:// 

www.dassaultfalcon.com. 

(3) You may review copies of the service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue, SW., Renton, 

Washington. For information on the 

availability of this material at the FAA, call 

425–227–1221. 

(4) You may also review copies of the 

service information that is incorporated by 

reference 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/ 

code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Renton, Washington, on March 

21, 2011. 

Kalene C. Yanamura, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2011–7427 Filed 3–31–11; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–1295; Directorate 

Identifier 2010–CE–060–AD; Amendment 

39–16635; AD 2011–06–10] 

RIN 2120–AA64 

Airworthiness Directives; Piper 

Aircraft, Inc. (Type Certificate 

Previously Held by The New Piper 

Aircraft, Inc.) Models PA–46–310P, PA– 

46–350P, and PA–46R–350T Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are superseding an 

existing airworthiness directive (AD) 

that applies to certain Piper Aircraft, 

Inc. Models PA–46–310P and PA–46– 

350P airplanes that are equipped with a 

Lewis or Transicoil turbine inlet 

temperature (T.I.T.) gauge and 

associated probe. That AD currently 

requires cleaning, inspecting, and 

calibrating the T.I.T. system; replacing 

any T.I.T. system that fails the 

calibration test; repetitively replacing 

the T.I.T. probe on certain airplanes; 

and inserting a copy of the AD into the 

pilot’s operating handbook (POH) for 

certain airplanes. This new AD retains 


jlentini on DSKJ8SOYB1PROD with RULES