48022 Federal Register / Vol. 80, No. 154 / Tuesday, August 11, 2015 / Rules and Regulations 

(xv) 201428351 

(xvi) 201428352 

(5) Where Airbus A330 ALS Part 4—Aging 

Systems Maintenance, Revision 04, dated 

August 27, 2013, defines a calendar 

compliance time for the modification of SSCs 

on three hydraulic circuits having part 

numbers MZ4339390–01X, MZ4306000–01X, 

MZ4339390–02X, MZ4306000–02X, 

MZ4339390–10X, or MZ4306000–10X as 

‘‘March 5, 2010,’’ the calendar compliance 

time is April 14, 2011 (18 months after 

October 14, 2009 (the effective date of AD 

2009–18–20, Amendment 39–16017 (74 FR 

46313, September 9, 2009))). 

(6) Where Note (6) of ‘‘ATA 27–64–00 

Flight Control—Spoiler Hydraulic 

Actuation,’’ of Sub-part 4–2–1, ‘‘Life Limits,’’ 

of Sub-part 4–2, ‘‘Systems Life Limited 

Components,’’ of Airbus A330 ALS Part 4— 

Aging Systems Maintenance, Revision 04, 

dated August 27, 2013, defines a calendar 

date of ‘‘September 5, 2008,’’ as a date for the 

determination of accumulated flight cycles 

since the aircraft initial entry into service, the 

date is October 14, 2009 (the effective date 

of AD 2009–18–20, Amendment 39–16017 

(74 FR 46313, September 9, 2009)). 

(7) Where Note (6) of ‘‘ATA 27–64–00 

Flight Control—Spoiler Hydraulic 

Actuation,’’ of Sub-part 4–2–1, ‘‘Life Limits,’’ 

of Sub-part 4–2, ‘‘Systems Life Limited 

Components,’’ of Airbus A330 ALS Part 4— 

Aging Systems Maintenance, Revision 04, 

dated August 27, 2013, defines a calendar 

compliance time as ‘‘March 5, 2010,’’ for the 

modification of affected servo controls, the 

calendar compliance time is April 14, 2011 

(18 months after October 14, 2009 (the 

effective date of AD 2009–18–20, 

Amendment 39–16017 (74 FR 46313, 

September 9, 2009))). 

(i) No Alternative Actions or Intervals 

After accomplishing the revision required 

by paragraph (g) of this AD, no alternative 

actions (e.g., inspections) or intervals may be 

used unless the actions or intervals are 

approved as an alternative method of 

compliance (AMOC) in accordance with the 

procedures specified in paragraph (j)(1) of 

this AD. 

(j) 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: 

Vladimir Ulyanov, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

telephone 425–227–1138; fax 425–227–1149. 

Information may be emailed to: 9-ANM-116- 

ACO-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) Contacting the Manufacturer: For any 

requirement in this AD to obtain corrective 

actions from a manufacturer, the action must 

be accomplished using a method approved 

by the Manager, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the European Aviation Safety Agency 

(EASA); or Airbus’s EASA Design 

Organization Approval (DOA). If approved by 

the DOA, the approval must include the 

DOA-authorized signature. 

(k) Related Information 

Refer to Mandatory Continuing 

Airworthiness Information (MCAI) European 

Aviation Safety Agency (EASA) AD 2013– 

0268, dated November 7, 2013, for related 

information. This MCAI may be found in the 

AD docket on the Internet at http://

www.regulations.gov by searching for and 

locating Docket No. FAA–2013–0834. 

(l) 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) Airbus A330 Airworthiness Limitations 

Section ALS Part 4—Aging Systems 

Maintenance, Revision 04, dated August 27, 

2013. 

(ii) Airbus A330 ALS Part 4—Aging 

Systems Maintenance (ASM), Variation 4.1, 

dated July 23, 2014. 

(iii) Airbus A330 ALS Part 4—Aging 

Systems Maintenance (ASM), Variation 4.2, 

dated July 23, 2014. 

(3) For service information identified in 

this AD, contact Airbus SAS, Airworthiness 

Office—EAL, 1 Rond Point Maurice Bellonte, 

31707 Blagnac Cedex, France; telephone +33 

5 61 93 36 96; fax +33 5 61 93 45 80; email 

airworthiness.A330-A340@airbus.com; 

Internet http://www.airbus.com. 

(4) You may view this 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 July 28, 

2015. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2015–19182 Filed 8–10–15; 08:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0751; Directorate 

Identifier 2013–NM–188–AD; Amendment 

39–18229; AD 2015–16–04] 

RIN 2120–AA64 

Airworthiness Directives; Kidde 

Graviner 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Kidde Graviner hand-operated fire 

extinguishers. This AD was prompted 

by a report that a fire extinguisher failed 

to operate when the activation lever was 

pressed. This AD requires modifying the 

affected fire extinguishers. We are 

issuing this AD to prevent fire 

extinguishers from failing to operate in 

the event of a fire, which could 

jeopardize occupants’ safety and 

continuation of safe flight and landing. 

DATES: This AD becomes effective 

September 15, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of September 15, 2015. 

ADDRESSES: You may examine the AD 

docket on the Internet at http://

www.regulations.gov/

#!docketDetail;D=FAA-2014-0751 or in 

person at the 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. 

For service information identified in 

this AD, contact Kidde Graviner 

Limited, Mathisen Way, Colnbrook, 

Slough, Berkshire, SL3 0HB, United 

Kingdom; telephone +44 (0) 1753 

583245; fax +44 (0) 1753 685040. 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 http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

0751. 

FOR FURTHER INFORMATION CONTACT: Ian 

Lucas, Aerospace Engineer, Boston 

Aircraft Certification Office (ACO), 

ANE–150, FAA, Engine and Propeller 

Directorate, 12 New England Executive 


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Federal Register / Vol. 80, No. 154 / Tuesday, August 11, 2015 / Rules and Regulations 48023 

Park, Burlington, MA 01803; phone: 

781–238–7757; fax: 781–238–7170; 

email: ian.lucas@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 Kidde Graviner handoperated fire extinguishers. The NPRM 

published in the Federal Register on 

October 16, 2014 (79 FR 62070). 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA Airworthiness 

Directive 2012–0037, dated March 9, 

2012 (referred to after this as the 

Mandatory Continuing Airworthiness 

Information, or ‘‘the MCAI’’), to correct 

an unsafe condition for certain Kidde 

Graviner hand-operated fire 

extinguishers. The MCAI states: 

An instance occurred where an operator 

tried to use the fire extinguisher, but the 

extinguisher failed to operate when the 

activation lever was pressed. 

This condition, if not detected and 

corrected, could lead, in case of need to use 

the device to extinguish a fire on an aircraft, 

to jeopardize the occupants’ safety as well as 

the flight continuation and safe landing. 

The part manufacturer Kidde Graviner has 

introduced a design change to remove the 

root cause of the possible failure. 

This [EASA] AD requires to modify all 

potentially defective fire extinguishers 

[including applying adhesive to the gland 

nut]. 

You may examine the MCAI in the AD 

docket on the Internet at http://

www.regulations.gov/

#!documentDetail;D=FAA-2014-0751- 

0004. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. The 

following presents the comments 

received on the NPRM (79 FR 62070, 

October 16, 2014) and the FAA’s 

response to each comment. One 

anonymous commenter supported the 

NPRM. 

Request To Refer to ‘‘Aircraft’’ Instead 

of ‘‘Various Transport and Small 

Airplanes’’ 

One anonymous commenter requested 

that we revise paragraph (c) of the 

proposed AD (79 FR 62070, October 16, 

2014) to refer to ‘‘aircraft’’ instead of 

‘‘various transport and small airplanes.’’ 

The commenter stated that the change is 

in the interest of improving accuracy 

and for clarification. The commenter 

added the request is based on the fact 

that the key to addressing the unsafe 

condition is finding suspected products, 

defined by the manufacturer’s part 

numbers, and the category under which 

the aircraft operates is not material. 

We agree with the request to refer to 

‘‘aircraft’’ instead of ‘‘various transport 

and small airplanes’’ for the reasons 

stated by the commenter. We have 

replaced the text ‘‘various transport and 

small airplanes’’ with the word 

‘‘aircraft’’ in paragraph (c) of this AD. 

Change to Manufacturer’s Name 

We have revised paragraph (c)(3) of 

this AD to identify the manufacturer 

name for the Model C–212–CB, C–212– 

CC, C–212–CD, C–212–CE, C–212–CF, 

C–212–DE, and C–212–DF airplanes as 

Airbus Defense and Space S.A. (Type 

Certificate previously held by EADS 

CASA; Construcciones Aeronauticas, 

S.A.). Airbus Defense and Space S.A. 

(Type Certificate previously held by 

EADS CASA; Construcciones 

Aeronauticas, S.A.) is the manufacturer 

name published in the most recent type 

certificate data sheet for those models. 

Clarification of Parts Installation 

Prohibition 

We have added a reference to 

‘‘paragraph (h) of this AD’’ within 

paragraph (i) of this AD to clarify which 

modified parts may be installed. 

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 (79 FR 

62070, October 16, 2014) for correcting 

the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (79 FR 62070, 

October 16, 2014). 

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 

Kidde Graviner has issued Alert 

Service Bulletin A26–081, Revision 1, 

dated January 31, 2012. The service 

information describes procedures for 

modifying fire extinguishers. 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 of 

this AD. 

Costs of Compliance 

We estimate that this AD affects 400 

appliances installed on, but not limited 

to, various aircraft of U.S. registry. 

We also estimate that it will take 

about 25 work-hours per product to 

comply with the basic requirements of 

this AD. The average labor rate is $85 

per work-hour. Based on these figures, 

we estimate the cost of this AD on U.S. 

operators to be $850,000, or $2,125 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 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. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov/

#!docketDetail;D=FAA-2014-0751; or in 

person at the Docket Management 


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48024 Federal Register / Vol. 80, No. 154 / Tuesday, August 11, 2015 / Rules and Regulations 

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 Operations office (telephone 

800–647–5527) is in the ADDRESSES

section. 

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): 

2015–16–04 Kidde Graviner: Amendment 

39–18229. Docket No. FAA–2014–0751; 

Directorate Identifier 2013–NM–188–AD. 

(a) Effective Date 

This AD becomes effective September 15, 

2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Kidde Graviner handoperated fire extinguishers having part 

numbers 56412–001 (34H), 56411–001 (35H), 

and 56412–002 (38H). These fire 

extinguishers may be installed on, but not 

limited to, aircraft, certificated in any 

category, specified in paragraphs (c)(1), (c)(2), 

(c)(3), (c)(4), (c)(5), and (c)(6) of this AD. 

(1) BAE Systems (Operations) Limited 

Model ATP airplanes. 

(2) BAE Systems (Operations) Limited 

Model 4101 airplanes. 

(3) Airbus Defense and Space S.A. (Type 

Certificate previously held by EADS CASA; 

Construcciones Aeronauticas, S.A.) Model C– 

212–CB, C–212–CC, C–212–CD, C–212–CE, 

C–212–CF, C–212–DE, and C–212–DF 

airplanes. 

(4) Fokker Services B.V. Model F.27 Mark 

050, 100, 200, 300, 400, 500, 600, and 700 

airplanes. 

(5) Short Brothers PLC Model SD3–60 

SHERPA, SD3–SHERPA, SD3–30, and SD3– 

60 airplanes. 

(6) SHORT BROTHERS & HARLAND LTD 

SC–7 Series 2 and SC–7 Series 3 airplanes. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 26, Fire Protection. 

(e) Reason 

This AD was prompted by a report that a 

fire extinguisher failed to operate when the 

activation lever was pressed. We are issuing 

this AD to prevent fire extinguishers from 

failing to operate in the event of a fire, which 

could jeopardize occupants’ safety and 

continuation of safe flight and landing. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Modification 

Within 6 months after the effective date of 

this AD, modify all Kidde Graviner handoperated fire extinguishers having part 

numbers 56412–001 (34H), 56411–001 (35H), 

and 56412–002 (38H), in accordance with the 

Accomplishment Instructions of Kidde 

Graviner Alert Service Bulletin A26–081, 

Revision 1, dated January 31, 2012. 

(h) Credit for Previous Actions 

This paragraph provides credit for actions 

required by paragraph (g) of this AD, if those 

actions were performed before the effective 

date of this AD using Kidde Graviner Alert 

Service Bulletin A26–081, dated August 23, 

2011, which is not incorporated by reference 

in this AD. 

(i) Parts Installation Prohibition 

As of the effective date of this AD, no 

person may install any Kidde Graviner handoperated fire extinguisher having part 

number 56412–001 (34H), 56411–001 (35H), 

or 56412–002 (38H) on any airplane unless 

the fire extinguisher has been modified as 

specified in paragraph (g) or (h) of this AD. 

(j) Other FAA AD Provision 

The following provision for Alternative 

Methods of Compliances (AMOCs) also 

applies to this AD: The manager of the office 

having certificate responsibility for the 

affected product 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. The Manager, Boston Aircraft 

Certification Office (ACO), FAA, will 

coordinate requests for approval of AMOCs 

with the manager of the appropriate office for 

the affected product. Send information to 

ATTN: Ian Lucas, Aerospace Engineer, 

Boston ACO, ANE–150, FAA, Engine and 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7757; fax: 781–238–7170; 

email: ian.lucas@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. 

(k) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) European 

Aviation Safety Agency (EASA) 

Airworthiness Directive 2012–0037, dated 

March 9, 2012, for related information. This 

MCAI may be found in the AD docket on the 

Internet at http://www.regulations.gov/

#!documentDetail;D=FAA–2014–0751–0004. 

(2) Service information identified in this 

AD that is not incorporated by reference is 

available at the addresses specified in 

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

(l) 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) Kidde Graviner Alert Service Bulletin 

A26–081, Revision 1, dated January 31, 2012. 

Page 2 of this document is dated August 23, 

2011. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Kidde Graviner Limited, 

Mathisen Way, Colnbrook, Slough, Berkshire, 

SL3 0HB, United Kingdom; telephone +44 (0) 

1753 583245; fax +44 (0) 1753 685040. 

(4) You may view this 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 July 29, 

2015. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2015–19474 Filed 8–10–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HOUSING AND 

URBAN DEVELOPMENT 

24 CFR Parts 200 and 232 

[Docket No. FR–5632–F–02] 

RIN 2502–AJ27 

Federal Housing Administration (FHA): 

Updating Regulations Governing HUD 

Fees and the Financing of the 

Purchase and Installation of Fire 

Safety Equipment in FHA-Insured 

Healthcare Facilities 

AGENCY: Office of the Assistant 

Secretary for Housing-Federal Housing 

Commissioner, HUD. 

ACTION: Final rule. 

SUMMARY: This rule updates HUD fees 

for multifamily housing and residential 

healthcare facilities, and updates and 


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