Federal Register / Vol. 78, No. 220 / Thursday, November 14, 2013 / Rules and Regulations 68357 

pyrotechnical cartridges for batch number 

and date, and check the cartridges for 

electrical continuity and resistance, in 

accordance with the Accomplishment 

Instructions of Dassault Mandatory Service 

Bulletin F20–783, Revision 1 (also referred to 

as 783–R1), dated June 11, 2012 (for Model 

Fan Jet Falcon and Mystere-Falcon 20–C5, 

20–D5, 20–E5, and 20–F5 airplanes); or 

Dassault Mandatory Service Bulletin F200– 

128, Revision 1 (also referred to as 128–R1), 

dated June 11, 2012 (for Model MystereFalcon 200 airplanes). 

(1) P/N 12–12–11707S1–4, with batch up 

to 44 inclusive, manufactured before May 

2012. 

(2) P/N 12–12–11707S2–4, with batch up 

to 33 inclusive, manufactured before May 

2012. 

(3) P/N 12–12–11707S3–4, with batch up 

to 44 inclusive, manufactured before May 

2012. 

(h) Replacement 

If, during any check as required by 

paragraphs (g) and (i) of this AD, a 

discrepancy [excessive resistance] is 

identified, before next flight, replace the 

discrepant fire extinguisher bottle cartridge(s) 

with a serviceable part, in accordance with 

the Accomplishment Instructions of Dassault 

Mandatory Service Bulletin F20–783, 

Revision 1 (also referred to as 783–R1), dated 

June 11, 2012 (for Model Fan Jet Falcon and 

Mystere-Falcon 20–C5, 20–D5, 20–E5, and 

20–F5 airplanes); or Dassault Mandatory 

Service Bulletin F200–128, Revision 1 (also 

referred to as 128–R1), dated June 11, 2012 

(for Model Mystere-Falcon 200 airplanes). 

Replacement of discrepant fire extinguisher 

bottle cartridges with a serviceable part 

terminates the repetitive actions required by 

paragraph (i) of this AD for that cartridge. 

(i) Repetitive Checks 

At the applicable time specified in 

paragraph (i)(1) or (i)(2) of this AD, repeat the 

checks required by paragraph (g) of this AD. 

(1) For airplanes equipped with fire 

extinguisher bottle cartridges having P/N 12– 

12–11707S3–4, having a batch number, and 

manufacturing date, as listed in paragraph 

(g)(3) of this AD, at intervals not to exceed 

65 days. 

(2) For airplanes equipped with fire 

extinguisher bottle cartridges having P/N 12– 

12–11707S1–4 or P/N 12–12–11707S2–4, 

having a batch number, and manufacturing 

date, as listed in paragraph (g)(1) or (g)(2) of 

this AD, at intervals not to exceed 12 months. 

(j) Replacement 

Except as required by paragraph (h) of this 

AD: Within 30 months after installation of an 

affected fire extinguisher bottle cartridge on 

an airplane, or within 36 months since 

cartridge manufacturing date, whichever 

occurs first after the effective date of this AD, 

replace each affected fire extinguisher bottle 

cartridge listed in paragraphs (g)(1), (g)(2), 

and (g)(3) of this AD, with a serviceable part, 

in accordance with the Accomplishment 

Instructions of Dassault Mandatory Service 

Bulletin F20–783, Revision 1 (also referred to 

as 783–R1), dated June 11, 2012 (for Model 

Fan Jet Falcon and Mystere-Falcon 20–C5, 

20–D5, 20–E5, and 20–F5 airplanes); or 

Dassault Mandatory Service Bulletin F200– 

128, Revision 1 (also referred to as 128–R1), 

dated June 11, 2012 (for Model MystereFalcon 200 airplanes). Replacing the affected 

fire extinguisher bottle cartridge with a 

serviceable part as required by paragraph (h) 

or (j) of this AD, terminates the repetitive 

actions required by paragraph (i) of this AD 

for that cartridge. 

(k) Parts Installation Prohibition 

As of the effective date of this AD, no 

person may install any fire extinguisher 

bottle cartridge having a part number, batch 

number, and manufacturing date as specified 

in paragraph (g)(1), (g)(2), or (g)(3) of this AD, 

on any airplane. 

(l) Other FAA AD Provisions 

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 emailed 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. 

(m) Related Information 

Refer to Mandatory Continuing 

Airworthiness Information (MCAI) European 

Aviation Safety Agency (EASA) 

Airworthiness Directive 2012–0190, dated 

September 24, 2012, for related information. 

You may examine this AD on the Internet at 

http://www.regulations.gov/

#!documentDetail;D=FAA-2013-0626-0002. 

(n) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless this AD specifies otherwise. 

(i) Dassault Mandatory Service Bulletin 

F20–783, Revision 1 (also referred to as 783– 

R1), dated June 11, 2012. 

(ii) Dassault Mandatory Service Bulletin 

F200–128, Revision 1 (also referred to as 

128–R1), dated June 11, 2012. 

(3) For service information identified in 

this AD, contact Dassault Falcon Jet, P.O. Box 

2000, South Hackensack, NJ 07606; 

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

www.dassaultfalcon.com. 

(4) You may review this referenced service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue SW., Renton, 

WA. For information on the availability of 

this material at the FAA, call 425–227–1221. 

(5) You may view this 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/cfr/ibrlocations.html. 

Issued in Renton, Washington, on October 

18, 2013. 

Jeffrey E. Duven, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2013–27071 Filed 11–13–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0939; Directorate 

Identifier 2013–CE–043–AD; Amendment 

39–17655; AD 2013–22–23] 

RIN 2120–AA64 

Airworthiness Directives; Aermacchi 

S.p.A. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for 

Aermacchi S.p.A. Models F.260, F.260B, 

F.260C, F.260D, F.260E, F.260F, S.208, 

and S.208A airplanes equipped with a 

Lycoming O–540 wide cylinder flange 

engine with a front crankcase mounted 

propeller governor. This AD results 

from mandatory continuing 

airworthiness information (MCAI) 

issued by the aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as the set screw that fixes the 

setting of the propeller governor idler 

gear shaft was not in the proper 

position. We are issuing this AD to 

require actions to address the unsafe 

condition on these products. 


TKELleY on DSK3SPTVN1PROD with RULES
68358 Federal Register / Vol. 78, No. 220 / Thursday, November 14, 2013 / Rules and Regulations 

DATES: This AD is effective December 

16, 2013. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the AD 

as of December 16, 2013. 

We must receive comments on this 

AD by December 30, 2013. 

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. 

For service information identified in 

this AD, contact Alenia Aermacchi 

S.p.A, Via Paola Foresio, 1, 21040 

Venegono Superiore (Varese)—Italy; 

telephone: 0331–813111; fax: 0331– 

827595; Internet: http://

www.aleniaaermacchi.it/en-US/Pages/

custsupp.aspx. You may view this 

referenced service information at the 

FAA, Small Airplane Directorate, 901 

Locust, Kansas City, Missouri 64106. 

For information on the availability of 

this material at the FAA, call (816) 329– 

4148. 

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: 

Mike Kiesov, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4144; fax: (816) 

329–4090; email: mike.kiesov@faa.gov. 

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 AD No.: 

2012–0228R1, dated November 13, 2012 

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

correct an unsafe condition for the 

specified products. The MCAI states: 

A case of in-flight complete loss of engine 

oil pressure indications has been reported, 

resulting in an emergency landing. During 

the post-flight inspection on the affected 

engine, some metallic parts (2–4 mm) have 

been found. Although the origin of these 

parts has not been established, it seems 

probable that they originated from the set 

screw, Part Number (P/N) AN565B1032H, 

that fixes the setting of the propeller governor 

idler gear shaft, because in the affected 

engine, it was not found in the proper 

position. 

This condition, if not detected and 

corrected, could lead to engine failure, 

possible resulting in a forced landing, 

consequent damage to the aeroplane, and 

injury to occupants. 

To address this potential unsafe condition, 

Alenia Aermacchi issued Bollettino Tecnico 

(BT) 205B65 and BT 260SB–136 to instruct 

owners and operators of the aeroplanes that 

could be affected. 

To correct this potential unsafe condition, 

EASA issued Emergency AD 2012–0228–E to 

require repetitive inspections of the affected 

engines and, in case any discrepancy is 

found, accomplishment of the applicable 

corrective actions. 

Since AD 2012–0228–E was issued, it has 

become clear that only ‘wide cylinder flange’ 

engines equipped with a front crankcase 

propeller governor (ref to Lycoming Service 

Instruction No. 1343B and Lycoming Service 

Letter L220C) are equipped with the affected 

set screw P/N AN565B1032H that is the 

subject of this AD. 

For the reason described above, this AD is 

revised to reduce the Applicability, requiring 

only actions on aeroplanes fitted with a ‘wide 

cylinder flange’ engine equipped with a front 

crankcase propeller governor. This AD is also 

revised to remove, after the first inspection/ 

correction, the limitation that prohibited 

aerobatic manoeuvres. 

This is still considered to be a temporary 

measure and further AD action may follow. 

You may examine the MCAI on the 

Internet at http://www.regulations.gov 

by searching for and locating it in 

Docket No. FAA–2013–0939. 

Relevant Service Information 

Alenia Aermacchi Una Societa 

Finmeccanica has issued Mandatory 

Bollettino Tecnico (English Translation: 

Technical Bulletin) No. 205B65, 

Revision 1, dated November 12, 2012; 

and Alenia Aermacchi Una Societa 

Finmeccanica has issued Mandatory 

Bollettino Tecnico (English Translation: 

Technical Bulletin) No. 260SB–136, 

Revision 1, dated November 12, 2012. 

The actions described in this service 

information are intended to correct the 

unsafe condition identified in the 

MCAI. 

FAA’s Determination and Requirements 

of the 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 this State of 

Design Authority, they have notified us 

of the unsafe condition described in the 

MCAI and service information 

referenced above. We are issuing this 

AD because we evaluated all 

information provided by the State of 

Design Authority and determined the 

unsafe condition exists and is likely to 

exist or develop on other products of the 

same type design. 

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 improper position of the 

set screw that fixes the setting of the 

propeller governor idler gear could 

result in loss of engine oil pressure 

indications resulting in emergency 

landing. 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–2013–0939; 

Directorate Identifier 2013–CE–043– 

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. 

Costs of Compliance 

We estimate that this AD will affect 

43 products of U.S. registry. We also 

estimate that it would take about 2 

work-hours per product to comply with 


TKELleY on DSK3SPTVN1PROD with RULES
Federal Register / Vol. 78, No. 220 / Thursday, November 14, 2013 / Rules and Regulations 68359 

the basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Required parts would cost about $50 per 

product. 

Based on these figures, we estimate 

the cost of the AD on U.S. operators to 

be $9,460, or $220 per product. 

Since there currently are no repair 

instructions available when 

discrepancies are found during the 

required inspection, the FAA has no 

way of determining what the cost would 

be per airplane that would need such 

repairs. 

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 that this AD: 

(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), 

(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: 

2013–22–23 Aermacchi S.p.A.: Amendment 

39–17655; Docket No. FAA–2013–0939; 

Directorate Identifier 2013–CE–043–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective December 16, 2013. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to the following 

AERMACCHI S.p.A. airplanes that are 

certificated in any category: 

(1) Models F.260, F.260B, F.260C, F.260D, 

F.260E, and F.260F airplanes, all serial 

numbers, that are equipped with either a 

Lycoming O–540, IO–540, or AEIO–540 wide 

cylinder flange engine (identified by the 

suffix ‘‘A’’ or ‘‘E’’ in the serial number) with 

a front crankcase mounted propeller 

governor; and 

(2) Models S.208 and S.208A airplanes, all 

serial numbers, that are equipped with a 

Lycoming O–540 wide cylinder flange engine 

(identified by the suffix ‘‘A’’ or ‘‘E’’ in the 

serial number) with a front crankcase 

mounted propeller governor. 

(d) Subject 

Air Transport Association of America 

(ATA) Code 71: Powerplant. 

(e) Reason 

This AD was prompted by mandatory 

continuing airworthiness information (MCAI) 

issued by the aviation authority of another 

country to identify and correct an unsafe 

condition on an aviation product. The MCAI 

describes the unsafe condition as the set 

screw that fixes the setting of the propeller 

governor idler gear shaft was not in the 

proper position. We are issuing this AD to 

detect and correct improper position of the 

set screw, which could lead to complete loss 

of engine oil pressure indications and result 

in emergency landing. 

(f) Actions and Compliance 

Unless already done, do the following 

actions in paragraphs (f)(1) through (f)(5) of 

this AD. 

(1) For Models F.260, F.260B, F.260C, 

F.260D, F.260E, and F.260F airplanes: Before 

further flight after December 16, 2013 (the 

effective date of this AD), fabricate and 

install a placard that states: ‘‘AEROBATIC 

MANEUVERS ARE PROHIBITED.’’ Fabricate 

the placard using 1/8-inch black lettering on 

a white background and install the placard 

on the instrument panel in clear view of the 

pilot. 

(2) In lieu of installing the placard, a copy 

of this AD may be inserted into the 

limitations section of the applicable airplane 

flight manual (AFM) to comply with the 

action required by paragraph (f)(1) of this AD. 

The insertion of the AD into the AFM may 

be done by an owner/operator (pilot) holding 

at least a private pilot certificate and must be 

entered into the airplane records showing 

compliance with this AD in accordance with 

14 CFR 43.9 (a)(1)(4) and 14 CFR 

91.417(a)(2)(v). The record must be 

maintained as required by 14 CFR 91.173, 

121.380, or 135.439. 

(3) For all airplanes: Within the next 10 

hours time-in-service (TIS) after December 

16, 2013 (the effective date of this AD) and 

repetitively thereafter at intervals not to 

exceed 100 hours TIS, inspect the propeller 

governor idler gear shaft set screw, part 

number (P/N) AN565B1032H, following the 

Compliance Instructions of Alenia 

Aermacchi Una Societa Finmeccanica 

Mandatory Bollettino Tecnico (English 

Translation: Technical Bulletin) No. 205B65, 

Revision 1, dated November 12, 2012; or 

Alenia Aermacchi Una Societa Finmeccanica 

Mandatory Bollettino Tecnico (English 

Translation: Technical Bulletin) No. 260SB– 

136, Revision 1, dated November 12, 2012, as 

applicable. 

(4) If a discrepancy (e.g., set screw missing 

or unscrewed) is found during any inspection 

required by paragraph (f)(3) of this AD, before 

further flight, contact Alenia Aermacchi 

S.p.A. for repair instructions approved by the 

FAA specifically for this AD and incorporate 

the repair instructions. You may contact 

Alenia Aermacchi S.p.A. using the contact 

information found in paragraph (k)(3) of this 

AD. 

(5) After the initial inspection required by 

paragraph (f)(3) of this AD, provided no 

discrepancies were found or any 

discrepancies found were corrected as 

required by paragraph (f)(4) of this AD, 

remove the placard or the copy of the AD that 

was inserted into the AFM required by 

paragraphs (f)(1) or (f)(2) of this AD. 

(g) Credit for Actions Accomplished in 

Accordance With Previous Service 

Information 

This AD allows credit for the actions 

required in paragraphs (f)(2) and (f)(3) of this 

AD if done before December 16, 2013 (the 

effective date of this AD) following Alenia 

Aermacchi Una Societa Finmeccanica 

Mandatory Bollettino Tecnico (English 

Translation: Technical Bulletin) No. 205B65, 

dated October 26, 2012; or Alenia Aermacchi 

Una Societa Finmeccanica Mandatory 

Bollettino Tecnico (English Translation: 

Technical Bulletin) No. 260SB–136, dated 

October 26, 2012, as applicable. 


TKELleY on DSK3SPTVN1PROD with RULES
68360 Federal Register / Vol. 78, No. 220 / Thursday, November 14, 2013 / Rules and Regulations 

(h) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Office, 

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: Mike Kiesov, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4144; fax: (816) 329– 

4090; email: mike.kiesov@faa.gov. 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 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. 

(i) Special Flight Permit 

Special flight permits are permitted with 

the following limitation: Aerobatic 

maneuvers are prohibited until the actions of 

the AD are complied with. 

(j) Related Information 

Refer to MCAI European Aviation Safety 

Agency (EASA) AD No.: 2012–0228R1, dated 

November 13, 2012, for related information. 

You may examine the MCAI on the Internet 

at http://www.regulations.gov by searching 

for and locating it in Docket No. FAA–2013– 

0939. 

(k) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless the AD specifies otherwise. 

(i) Alenia Aermacchi Una Societa 

Finmeccanica Mandatory Bollettino Tecnico 

(English Translation: Technical Bulletin) No. 

205B65, Revision 1, dated November 12, 

2012. 

(ii) Alenia Aermacchi Una Societa 

Finmeccanica Mandatory Bollettino Tecnico 

(English Translation: Technical Bulletin) No. 

260SB–136, Revision 1, dated November 12, 

2012. 

(3) For service information identified in 

this AD, contact Alenia Aermacchi S.p.A, Via 

Paola Foresio, 1, 21040 Venegono Superiore 

(Varese)—Italy; telephone: 0331–813111; fax: 

0331–827595; Internet: http://

www.aleniaaermacchi.it/en-US/Pages/

custsupp.aspx. 

(4) You may view this referenced service 

information at the FAA, Small Airplane 

Directorate, 901 Locust, Kansas City, 

Missouri 64106. For information on the 

availability of this material at the FAA, call 

(816) 329–4148. 

(5) You may view this 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/cfr/ibrlocations.html. 

Issued in Kansas City, Missouri, on 

October 31, 2013. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2013–26681 Filed 11–13–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0029; Directorate 

Identifier 2013–NE–01–AD; Amendment 39– 

17599; AD 2013–19–17] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

plc Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting an 

airworthiness directive (AD) that 

published in the Federal Register. That 

AD applies to all Rolls-Royce plc (RR) 

RB211–535E4–B–37 series turbofan 

engines. The AD number is incorrect in 

the Regulatory text. This document 

corrects that error. In all other respects, 

the original document remains the 

same. 

DATES: This final rule is effective 

November 7, 2013. 

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 (phone: 800–647–5527) is 

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: 

Robert Green, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7754; fax: 781–238– 

7199; email: robert.green@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Airworthiness Directive 2013–19–17, 

Amendment 39–17599 (78 FR 61171, 

October 3, 2013), currently requires 

removal of affected parts using a 

drawdown plan for all RR RB211– 

535E4–B–37 series turbofan engines. 

As published, the AD number 2013– 

19–17 under § 39.13 [Amended], is 

incorrect. 

No other part of the preamble or 

regulatory information has been 

changed; therefore, only the changed 

portion of the final rule is being 

published in the Federal Register. 

The effective date of this AD remains 

November 7, 2013. 

Correction of Regulatory Text 

§ 39.13 [Corrected] 

In the Federal Register of October 3, 

2013, on page 61173, in the first 

column, lines 4 and 5, under § 39.13 

[Amended] of AD 2013–19–17, are 

corrected to read as follows: 

* * * * * 

2013–19–17 Rolls-Royce plc: Amendment 

39–17599; Docket No. FAA–2013–0029; 

* * * * * 

Issued in Burlington, Massachusetts, on 

October 25, 2013. 

Colleen M. D’Alessandro, 

Assistant Directorate Manager, Engine & 

Propeller Directorate, Aircraft Certification 

Service. 

[FR Doc. 2013–27190 Filed 11–13–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 91 

[Docket No. FAA–2013–0061] 

Unmanned Aircraft System Test Site 

Program 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of availability of final 

privacy requirements for the unmanned 

aircraft system (‘‘UAS’’) test site 

program; response to comments. 

SUMMARY: On February 22, 2013 the 

FAA published and requested public 

comment on the proposed privacy 

requirements (the ‘‘Draft Privacy 

Requirements’’) for UAS test sites (the 

‘‘Test Sites’’) that the FAA will establish 

pursuant to the FAA Modernization and 

Reform Act of 2012 (‘‘FMRA’’). This 

document responds to the public 

comments received and publishes the 

FAA’s final privacy requirements for the 

Test Sites (the ‘‘Final Privacy 

Requirements’’). 


TKELleY on DSK3SPTVN1PROD with RULES