Federal Register / Vol. 81, No. 91 / Wednesday, May 11, 2016 / Rules and Regulations 29119 

Program, 1700 G Street NW., Washington DC 

20552. 

* * * * * 

VIII. Property Report for Statement of 

Record—§ 1010.100(b) 

Property Report 

Heading and Section Number 

Cover Sheet .............................. 1010.105 

Table of Contents ..................... 1010.106 

Risks of Buying Land .............. 1010.107 

General Information ................ 1010.108 

Title and Land Use .................. 1010.109 

(a) General Instructions 

(b) Method of Sale 

(c) Encumbrances, Mortgages and Liens 

(d) Recording the Contract and Deed 

(e) Payments 

(f) Restrictions 

(g) Plats, Zoning, Surveying, Permits, 

Environment 

Roads ........................................ 1010.110 

Utilities .................................... 1010.111 

(a) Water 

(b) Sewer 

(c) Electricity 

(d) Telephone 

(e) Fuel or other Energy Source 

Financial Information .............. 1010.112 

Local Services .......................... 1010.113 

Recreational Facilities ............. 1010.114 

Subdivision Characteristics 

and Climate .......................... 1010.115 

(a) General Topography 

(b) Water Coverage 

(c) Drainage and Fill 

(d) Flood Plain 

(e) Flooding and Soil Erosion 

(f) Nuisances 

(g) Hazards 

(h) Climate 

(i) Occupancy 

Additional Information ........... 1010.116 

(a) Property Owners’ Association 

(b) Taxes 

(c) Violations and Litigation 

(d) Resale or Exchange Program 

(e) Unusual Situations 

1. Leases 

2. Foreign Subdivision 

3. Time Sharing 

4. Membership 

(f) Equal Opportunity in Lot Sales 

(g) Listing of lots 

Cost Sheet ................................ 1010.117 

Receipt, Agent Certification 

and Cancellation Page ......... 1010.118 

ADDITIONAL INFORMATION AND 

DOCUMENTATION 

General Information ................ 1010.208 

Title and Land Use .................. 1010.209 

Roads ........................................ 1010.210 

Utilities .................................... 1010.211 

Financial Information .............. 1010.212 

Recreational Facilities ............. 1010.214 

Subdivision Characteristics .... 1010.215 

Additional Information ........... 1010.216 

Affirmation .............................. 1010.219 

The Bureau’s OMB control number for this 

information collection is: 3170–0012. 

* * * * * 

PART 1012—SPECIAL RULES OF 

PRACTICE (REGULATION L) 

■ 24. The authority citation for part 

1012 continues to read as follows: 

Authority: 12 U.S.C. 5512, 5581; 15 U.S.C. 

1718. 

■ 25. Section 1012.35 is revised to read 

as follows: 

§ 1012.35 Prefiling assistance. 

Persons intending to file with the 

Bureau of Consumer Financial 

Protection, Office of Supervision 

Examinations may receive advice of a 

general nature as to the preparation of 

the filing including information as to 

proper format to be used and the scope 

of the items to be included in the 

format. Inquiries and requests for 

informal discussions with staff members 

should be directed to the Consumer 

Financial Protection Bureau, Interstate 

Land Sales Registration Program, 1700 G 

Street NW., Washington, DC 20552. 

■ 26. Section 1012.40 is amended by 

revising paragraph (a) introductory text 

to read as follows: 

§ 1012.40 Processing of filings. 

(a) Statements of Record and 

accompanying filing fees will be 

received on behalf of the Director by the 

Office of Supervision Examinations, for 

determination of whether the criteria set 

forth in paragraphs (a)(1) through (3) of 

this section have been satisfied. Where 

it appears that all three criteria are 

satisfied and it is otherwise practicable, 

acceleration of the effectiveness of the 

Statement of Record will normally be 

granted. 

* * * * * 

■ 27. Section 1012.236 is amended by 

revising paragraph (b) to read as follows: 

§ 1012.236 Notice of proceedings to 

withdraw a State’s certification. 

* * * * * 

(b) A clear and concise statement of 

material facts, sufficient to inform the 

respondent with reasonable definiteness 

of the basis for the Director’s 

determination, pursuant to § 1010.505, 

that the State’s laws, regulations and the 

administration thereof, taken as a 

whole, no longer meet the requirements 

of subpart C of part 1010. 

* * * * * 

Dated: May 1, 2016. 

Richard Cordray, 

Director, Bureau of Consumer Financial 

Protection. 

[FR Doc. 2016–10715 Filed 5–10–16; 8:45 am] 

BILLING CODE 4810–AM–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0247; Directorate 

Identifier 2014–NM–178–AD; Amendment 

39–18513; AD 2016–10–02] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

The Boeing Company Model 777–200 

and –300 series airplanes equipped with 

Rolls-Royce Trent 800 series engines. 

This AD was prompted by reports of 

heat damage to the strut aft fairing heat 

shield primary seal, as well as heat and 

wear damage to the heat shield 

insulation blankets. This AD requires 

repetitive inspections for cracks and 

heat damage to the strut aft fairing lower 

spar web structure (a flammable fluid 

zone barrier), for wear to the heat shield 

primary seal, and, as applicable, for heat 

and wear damage to heat shield 

insulation blankets; and related 

investigative and corrective actions if 

necessary. This AD also provides 

optional terminating action for the 

repetitive inspections. We are issuing 

this AD to detect and correct cracks and 

heat damage to the strut aft fairing lower 

spar web structure (a flammable fluid 

zone barrier), wear to the heat shield 

primary seal, and heat and wear damage 

to heat shield insulation blankets, 

which could lead to through-cracks in 

the aft fairing lower web structure and 

heating of the aft fairing lower web 

structure, and consequent uncontrolled 

fire in the aft fairing, fuel tank ignition 

or possible departure of the engine. 

DATES: This AD is effective June 15, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of June 15, 2016. 

ADDRESSES: For service information 

identified in this final rule, contact 

Boeing Commercial Airplanes, 

Attention: Data & Services Management, 


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P. O. Box 3707, MC 2H–65, Seattle, WA 

98124–2207; telephone: 206–544–5000, 

extension 1; fax: 206–766–5680; 

Internet: https://

www.myboeingfleet.com. You may view 

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. It is also available 

on the Internet at https://

www.regulations.gov by searching and 

locating Docket No. FAA–2015–0247. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

0247; 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 

Docket 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: 

Kevin Nguyen, Aerospace Engineer, 

Propulsion Branch, ANM–140S, FAA, 

Seattle Aircraft Certification Office 

(ACO), 1601 Lind Avenue SW., Renton, 

WA 98057–3356; phone: 425–917–6501; 

fax: 425–917–6590; email: 

kevin.nguyen@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to certain The Boeing Company 

Model 777–200 and –300 series 

airplanes equipped with Rolls-Royce 

Trent 800 series engines. The NPRM 

published in the Federal Register on 

March 12, 2015 (80 FR 12954) (‘‘the 

NPRM’’). The NPRM was prompted by 

reports of heat damage to the strut aft 

fairing heat shield primary seal, as well 

as heat and wear damage to the heat 

shield insulation blankets. The NPRM 

proposed to require repetitive 

inspections for cracks and heat damage 

to the strut aft fairing lower spar web 

structure (a flammable fluid zone 

barrier), for wear to the heat shield 

primary seal, and, as applicable, for heat 

and wear damage to heat shield 

insulation blankets; and related 

investigative and corrective actions if 

necessary. The NPRM also provided 

optional terminating action for the 

repetitive inspections. We are issuing 

this AD to detect and correct cracks and 

heat damage to the strut aft fairing lower 

spar web structure (a flammable fluid 

zone barrier), wear to the heat shield 

primary seal, and heat and wear damage 

to heat shield insulation blankets, 

which could lead to through-cracks in 

the aft fairing lower web structure and 

heating of the aft fairing lower web 

structure, and consequent uncontrolled 

fire in the aft fairing, fuel tank ignition 

or possible departure of the engine. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. The 

following presents the comments 

received on the NPRM and the FAA’s 

response to each comment. Marc 

Philippi stated that he supports the 

NPRM. 

Request To Clarify Precipitating Event 

and Unsafe Condition 

Boeing requested that we revise the 

SUMMARY and parts of the Discussion 

section of the NPRM to clarify that we 

received reports of heat damage to the 

strut aft fairing heat shield primary seal 

as well as heat and wear damage to the 

heat shield insulation blankets. Boeing 

also requested that we revise the 

SUMMARY of the NPRM and paragraph (e) 

of the proposed AD to clarify that the 

unsafe condition could lead to throughcracks in the aft fairing lower web 

structure and heating of the aft fairing 

lower web structure. Boeing further 

requested that we revise the Discussion 

section of the NPRM to indicate that the 

design of the strut aft fairing #1 heat 

shield (a titanium pan casting) and #1 

heat shield insulation blanket allows 

hot turbulent gas from the exhaust 

nozzle to cause wear and degradation of 

the front face of the #1 insulation 

blanket, enter the heat shield cavity (the 

space or cavity between the heat shields 

and insulation blankets), and contact 

the strut aft fairing lower spar web 

structure. Boeing additionally pointed 

out that continuous exposure to hot 

turbulent gas further damages the 

primary seal and #1 insulation blanket, 

increasing the temperature in the heat 

shield cavity, and causes damage to the 

insulation blankets and lower web 

structure. 

We agree that the requested changes 

provide clarity about the unsafe 

condition and consistency to the entire 

AD, and have revised the SUMMARY of 

this final rule and paragraph (e) of this 

AD accordingly. However, the requested 

revisions to the Discussion section of 

the NPRM are not included since certain 

paragraphs of the Discussion section of 

NPRMs are not restated in final rules. 

Request To Remove References to the 

Lower Spar Web Structure as a 

Firewall 

Boeing requested that we remove 

references to the strut aft fairing lower 

spar web structures as a firewall from 

the preamble of the NPRM and 

paragraph (e) of the proposed AD. 

Boeing indicated that the strut aft fairing 

lower spar web structure acts as a 

flammable fluid zone barrier, not a 

firewall. Boeing pointed out that a fire 

zone is defined as a region where 

flammable fluid and/or vapor leakage 

can occur where there is an ignition 

source present. Boeing also pointed out 

that a flammable fluid leakage zone is 

defined as an area in which flammable 

fluid and/or vapor leakage can occur, 

but where no ignition sources are 

present, and that since there are no 

ignition sources present in the strut aft 

fairing cavity, The Boeing Company 777 

strut fire protection document defines 

the strut aft fairing cavity as a 

flammable fluid leakage zone. 

We agree with the commenter, and 

have revised the preamble of this final 

rule and paragraph (e) of this AD 

accordingly. 

Request To Include Information Notice 

in the Final Rule 

Air New Zealand (ANZ) requested 

that we revise paragraph (h) of the 

proposed AD to include reference to 

Boeing Information Notice 777–54–0030 

IN 01, dated April 7, 2015. ANZ pointed 

out that Boeing Information Notice 777– 

54–0030 IN 01, dated April 7, 2015, 

includes a statement to clarify part 

interchangeability and part 

intermixability. ANZ also pointed out 

that Boeing Service Bulletin 777–54– 

0030, dated May 27, 2014, does not 

include the statement to clarify part 

interchangeability and part 

intermixability and that the 

modification included in the optional 

terminating action could therefore 

potentially be removed by installing 

older design parts as specified in Boeing 

Service Bulletin 777–54A0031, Revision 

1, dated May 9, 2014. ANZ noted that 

Boeing Information Notice 777–54–0030 

IN 01, dated April 7, 2015, is not 

approved by the FAA or any other 

regulatory authority. 

We acknowledge that Boeing 

Information Notice 777–54–0030 IN 01, 

dated April 7, 2015, contains the 

updated part interchangeability and part 

intermixability restriction statement for 

certain parts (such as insulation 

blankets). Boeing has issued Boeing 

Service Bulletin 777–54–0030, Revision 


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Federal Register / Vol. 81, No. 91 / Wednesday, May 11, 2016 / Rules and Regulations 29121 

1, dated September 30, 2015, which 

contains the information specified in 

Boeing Information Notice 777–54–0030 

IN 01, dated April 7, 2015. Once an 

airplane has been modified as specified 

in Boeing Service Bulletin 777–54– 

0030, dated May 27, 2014, or Boeing 

Service Bulletin 777–54–0030, Revision 

1, dated September 30, 2015 (optional 

terminating action of installing 

redesigned or newer insulation blankets, 

and other associated parts), and the 

operator has shown compliance with 

paragraph (h)(1) of this AD, the 

modification cannot be removed 

without requesting approval of an 

Alternative Method of Compliance 

(AMOC). Any change to install the older 

design parts would invalidate the 

terminating action accomplished as 

specified in Boeing Service Bulletin 

777–54–0030, dated May 27, 2014, or 

Boeing Service Bulletin 777–54–0030, 

Revision 1, dated September 30, 2015. 

Therefore, we have revised paragraph 

(h)(1) of this AD to refer to Boeing 

Service Bulletin 777–54–0030, Revision 

1, dated September 30, 2015, and 

provided credit for actions 

accomplished using Boeing Service 

Bulletin 777–54–0030, dated May 27, 

2014, in paragraph (j)(2) of this AD. 

ANZ stated that they believe the 

AMOC statement in the impending 

Airworthiness Notice should include 

Boeing Information Notice 777–54–0030 

IN 01, dated April 7, 2015. We infer that 

ANZ is requesting an AMOC for that 

information notice. 

We disagree with giving AMOC 

approval for Boeing Information Notice 

777–54–0030 IN 01, dated April 7, 2015, 

because we are requiring Boeing Service 

Bulletin 777–54–0030, Revision 1, dated 

September 30, 2015, that already 

includes the information contained in 

Boeing Information Notice 777–54–0030 

IN 01, dated April 7, 2015. 

Request for Revised Service 

Information and Credit 

ANZ requested that we revise 

paragraph (j) of the proposed AD to 

include credit for actions accomplished 

as specified in Boeing Service Bulletin 

777–54–0030, dated May 27, 2014. ANZ 

pointed out that they have 

accomplished the actions required by 

paragraph (h)(1) of the proposed AD, on 

multiple 777–200 airplanes in their 

fleet, as specified in Boeing Service 

Bulletin 777–54–0030, dated May 27, 

2014. ANZ also stated that they believe 

that credit for accomplishing the actions 

required by paragraph (h)(1) of the 

proposed AD, as specified in Boeing 

Service Bulletin 777–54–0030, dated 

May 27, 2014, should be added to 

paragraph (j) of the proposed AD. 

We agree with the request to include 

actions accomplished as specified in 

Boeing Service Bulletin 777–54–0030, 

dated May 27, 2014, in paragraph (j) of 

this AD. Therefore, as stated previously, 

we have revised this final rule to 

provide credit for actions accomplished 

using Boeing Service Bulletin 777–54– 

0030, dated May 27, 2014, in paragraph 

(j)(2) of this AD. 

Request To Correct a Typographical 

Error 

Boeing requested that we correct a 

typographical error by inserting missing 

dollar signs in the Cost of Compliance 

column of the On-Condition Costs table. 

We agree and have revised this final 

rule to include the missing information. 

Clarification of Actions 

Boeing issued Information Notice 

777–54A0031 IN 01, dated September 

24, 2015, to clarify access information 

when removing and installing pan 

casting number 6. Information Notice 

777–54A0031 IN 01, dated September 

24, 2015, specifies that when removing 

pan casting number 6 in FIGURE 9 and 

FIGURE 10 of Boeing Service Bulletin 

777–54A0031, Revision 1, dated May 9, 

2014, it is acceptable to remove and 

keep the bracket attached to the drain 

lines or remove the P-clamps for access. 

We refer to Boeing Service Bulletin 777– 

54A0031, Revision 1, dated May 9, 

2014, as the appropriate source of 

service information for accomplishing 

the actions required by paragraph (g) of 

this AD. Note 12 in Paragraph 3.A., 

‘‘General Information,’’ of Boeing Alert 

Service Bulletin 777–54A0031, dated 

June 7, 2013; and Revision 1, dated May 

9, 2014; contains statements informing 

and permitting removal of more parts 

for access when necessary. Also, 

operators may have been performing 

these same or similar access steps when 

removing pan casting number 6. Thus, 

the clarification in the information 

notice is neither new nor additional 

work. Further, this clarification of 

access information is already included 

in Boeing Service Bulletin 777–54– 

0030, Revision 1, dated September 30, 

2015, which is the appropriate source of 

service information for accomplishing 

the actions required by paragraph (h)(1) 

of this AD. Therefore, we have 

determined it is not necessary to 

include reference to Information Notice 

777–54A0031 IN 01, dated September 

24, 2015, in the regulatory text of this 

AD. 

Clarification of Credit 

Although the Accomplishment 

Instructions of Boeing Alert Service 

Bulletin 777–54A0031, dated June 7, 

2013, correctly show all nine insulation 

blankets for doing the actions, 

paragraph 2., ‘‘Material Information’’ 

only lists eight insulation blankets and 

is missing part number 313W5421–29. 

Therefore, we have clarified paragraph 

(j)(1) of this AD to specify that credit for 

previous actions are acceptable, 

provided that insulation blanket part 

number 313W5421–29 is inspected and 

reinstalled, or replaced with a new 

insulation blanket; as applicable, as 

specified in the Accomplishment 

Instructions of Boeing Alert Service 

Bulletin 777–54A0031, dated June 7, 

2013. 

Conclusion 

We reviewed the relevant data, 

considered the comments received, and 

determined that air safety and the 

public interest require adopting this AD 

with the changes described previously 

and minor editorial changes. We have 

determined that these minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM for 

correcting the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM. 

We also determined that these 

changes will not increase the economic 

burden on any operator or increase the 

scope of this AD. 

Related Service Information Under 

1 CFR Part 51 

We reviewed the following service 

information: 

• Boeing Service Bulletin 777– 

54A0031, Revision 1, dated May 9, 

2014. 

• Boeing Service Bulletin 777–54– 

0030, Revision 1, dated September 30, 

2015. 

The service information describes 

procedures for repetitive inspections for 

heat damage to the strut aft fairing lower 

spar web structure (a flammable fluid 

zone barrier) and heat shield primary 

seal, and heat and wear damage to heat 

shield insulation blankets; and related 

investigative and corrective actions. 

This service information is reasonably 

available because the interested parties 

have access to it through their normal 

course of business or by the means 

identified in the ADDRESSES section. 

Costs of Compliance 

We estimate that this AD affects 57 

airplanes of U.S. registry. 

We estimate the following costs to 

comply with this AD: 


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29122 Federal Register / Vol. 81, No. 91 / Wednesday, May 11, 2016 / Rules and Regulations 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per product Cost on U.S. operators 

Inspections .. 40 work-hours × $85 per hour = $3,400 per inspection cycle.$0 $3,400 per inspection 

cycle.

$193,800 per inspection 

cycle 

We estimate the following costs to do 

any necessary replacements that would 

be required based on the results of the 

required inspection. We have no way of 

determining the number of airplanes 

that might need these replacements: 

ON-CONDITION COSTS

Action Labor cost Parts cost Cost per product 

Heat shield primary seal replacement ...... 10 work-hours × $85 per hour = $850 ............................................. $1,940 $2,790 

Cracked or damaged parts replacement .. 110 work-hours × $85 per hour = $9,350 ........................................ $52,992 $62,342 

According to the manufacturer, some 

of the costs of this AD may be covered 

under warranty, thereby reducing the 

cost impact on affected individuals. We 

do not control warranty coverage for 

affected individuals. As a result, we 

have included all costs in our cost 

estimate. 

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 airworthiness 

directive (AD): 

2016–10–02 The Boeing Company: 

Amendment 39–18513; Docket No. 

FAA–2015–0247; Directorate Identifier 

2014–NM–178–AD. 

(a) Effective Date 

This AD is effective June 15, 2016. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to The Boeing Company 

Model 777–200 and –300 series airplanes 

equipped with Rolls-Royce Trent 800 series 

engines, certificated in any category, as 

identified in Boeing Service Bulletin 777– 

54A0031, Revision 1, dated May 9, 2014. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 54, Nacelles/Pylons. 

(e) Unsafe Condition 

This AD was prompted by reports of heat 

damage to the strut aft fairing heat shield 

primary seal, as well as heat and wear 

damage to the heat shield insulation 

blankets. We are issuing this AD to detect 

and correct cracks and heat damage to the 

strut aft fairing lower spar web structure (a 

flammable fluid zone barrier), wear to the 

heat shield primary seal, and heat and wear 

damage to heat shield insulation blankets, 

which could lead to through-cracks in the aft 

fairing lower web structure and heating of the 

aft fairing lower web structure, and 

consequent uncontrolled fire in the aft 

fairing, fuel tank ignition or possible 

departure of the engine. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Repetitive Inspections 

At the applicable time specified in 

paragraph 1.E., ‘‘Compliance,’’ of Boeing 

Service Bulletin 777–54A0031, Revision 1, 

dated May 9, 2014, except as required by 

paragraph (i) of this AD: Do the inspections 

specified in paragraphs (g)(1), (g)(2), and 

(g)(3) of this AD, and do all applicable related 

investigative and corrective actions, in 

accordance with the Accomplishment 

Instructions of Boeing Service Bulletin 777– 

54A0031, Revision 1, dated May 9, 2014. Do 

all applicable related investigative and 

corrective actions before further flight. 

Repeat the inspections specified in 

paragraphs (g)(1), (g)(2), and (g)(3) of this AD 

at the applicable time specified in paragraph 

1.E., ‘‘Compliance,’’ of Boeing Service 

Bulletin 777–54A0031, Revision 1, dated 

May 9, 2014. 

(1) Do a detailed inspection for cracks and 

heat damage of the aft fairing lower spar 

upper surface. 

(2) Do a conductivity inspection for heat 

damage of the aft fairing lower spar upper 

surface. 

(3) Do a detailed inspection for wear of the 

heat shield primary seal. 


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Federal Register / Vol. 81, No. 91 / Wednesday, May 11, 2016 / Rules and Regulations 29123 

(h) Optional Terminating Action 

The concurrent accomplishment of the 

actions specified in paragraphs (h)(1) and 

(h)(2) of this AD terminates the requirements 

of paragraph (g) of this AD. 

(1) Replacement of all heat shield 

insulation blankets (rub strips, heat shield 

pan casting, Velcro strips, aft fairing web 

drain sump, drain screen, and drain tubes, as 

applicable) in accordance with the 

Accomplishment Instructions of Boeing 

Service Bulletin 777–54–0030, Revision 1, 

dated September 30, 2015. 

(2) A one-time detailed inspection for 

cracks and heat damage of the aft fairing 

lower spar upper surface, conductivity 

inspection for heat damage of the aft fairing 

lower spar upper surface, and detailed 

inspection for wear of heat shield primary 

seal, and all applicable related investigative 

and corrective actions, in accordance with 

the Accomplishment Instructions of Boeing 

Service Bulletin 777–54A0031, Revision 1, 

dated May 9, 2014, provided all applicable 

related investigative and corrective actions 

are done before further flight. 

(i) Exception to Service Information 

Specifications 

Where Boeing Service Bulletin 777– 

54A0031, Revision 1, dated May 9, 2014, 

specifies a compliance time ‘‘After the 

Original Issue Date of this Service Bulletin,’’ 

this AD requires compliance within the 

specified compliance time after the effective 

date of this AD. 

(j) Credit for Previous Actions 

(1) This paragraph provides credit for the 

actions specified in paragraphs (g)(1), (g)(2), 

(g)(3), and (h)(2) of this AD, if those actions 

were performed before the effective date of 

this AD using Boeing Alert Service Bulletin 

777–54A0031, dated June 7, 2013, provided 

that insulation blanket part number 

313W5421–29 is inspected and reinstalled, or 

replaced with a new insulation blanket, as 

applicable, as specified in the 

Accomplishment Instructions of Boeing Alert 

Service Bulletin 777–54A0031, dated June 7, 

2013. This service information is not 

incorporated by reference in this AD. 

(2) This paragraph provides credit for the 

actions specified in paragraph (h)(1) of this 

AD, if those actions were performed before 

the effective date of this AD using Boeing 

Service Bulletin 777–54–0030, dated May 27, 

2014. This service information is not 

incorporated by reference in this AD. 

(k) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle Aircraft 

Certification Office (ACO), 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 manager of the ACO, send it to the 

attention of the person identified in 

paragraph (l)(1) of this AD. Information may 

be emailed to: 9-ANM-Seattle-ACO-AMOCRequests@faa.gov. 

(2) 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. 

(3) An AMOC that provides an acceptable 

level of safety may be used for any repair 

required by this AD if it is approved by the 

Boeing Commercial Airplanes Organization 

Designation Authorization (ODA) that has 

been authorized by the Manager, Seattle 

ACO, to make those findings. For a repair 

method to be approved, the repair must meet 

the certification basis of the airplane, and the 

approval must specifically refer to this AD. 

(l) Related Information 

(1) For more information about this AD, 

contact Kevin Nguyen, Aerospace Engineer, 

Propulsion Branch, ANM–140S, FAA, Seattle 

ACO, 1601 Lind Avenue SW., Renton, WA 

98057–3356; phone: 425–917–6501; fax: 425– 

917–6590; email: kevin.nguyen@faa.gov. 

(2) Service information identified in this 

AD that is not incorporated by reference is 

available at the addresses specified in 

paragraphs (m)(3) and (m)(4) of this AD. 

(m) 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) Boeing Service Bulletin 777–54A0031, 

Revision 1, dated May 9, 2014. 

(ii) Boeing Service Bulletin 777–54–0030, 

Revision 1, dated September 30, 2015. 

(3) For Boeing service information 

identified in this AD, contact Boeing 

Commercial Airplanes, Attention: Data & 

Services Management, P. O. Box 3707, MC 

2H–65, Seattle, WA 98124–2207; telephone: 

206–544–5000, extension 1; fax: 206–766– 

5680; Internet: https://

www.myboeingfleet.com. 

(4) You may view this service information 

at 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 April 28, 

2016. 

Dionne Palermo, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–10931 Filed 5–10–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2016–4256; Directorate 

Identifier 2016–CE–002–AD; Amendment 

39–18512; AD 2016–10–01] 

RIN 2120–AA64 

Airworthiness Directives; M7 

Aerospace LLC Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all M7 

Aerospace LLC Models SA226–AT, 

SA226–T, SA226–T(B), SA226–TC, 

SA227–AC (C–26A), SA227–AT, 

SA227–BC (C–26A), SA227–CC, SA227– 

DC (C–26B), and SA227–TT airplanes. 

We received reports of failed elevator 

control rod ends due to corrosion and 

lack of lubrication. This AD requires 

initial and repetitive inspections and 

lubrication of the elevator control rod 

ends and bearings with replacement as 

necessary. We are issuing this AD to 

correct the unsafe condition on these 

products. 

DATES: This AD is effective June 15, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of June 15, 2016. 

ADDRESSES: For service information 

identified in this final rule, contact M7 

Aerospace LLC, 10823 NE Entrance 

Road, San Antonio, Texas 78216; phone: 

(210) 824–9421; fax: (210) 804–7766; 

Internet: http://www.elbitsystemsus.com; email: MetroTech@

M7Aerospace.com. 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. It is also available on the Internet 

at http://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2016–4256. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2016– 

4256; 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 


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