Airworthiness Directives; Kidde Graviner, 48022-48024 [2015-19474]

Download as PDF 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))). rmajette on DSK2TPTVN1PROD with RULES (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-116ACO-AMOC-REQUESTS@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a VerDate Sep<11>2014 15:24 Aug 10, 2015 Jkt 235001 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 https:// 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 https://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: https:// 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 PO 00000 Frm 00022 Fmt 4700 Sfmt 4700 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 Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: 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 https:// 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 https:// 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 SUMMARY: E:\FR\FM\11AUR1.SGM 11AUR1 Federal Register / Vol. 80, No. 154 / Tuesday, August 11, 2015 / Rules and Regulations 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 https:// www.regulations.gov/ #!documentDetail;D=FAA-2014-07510004. rmajette on DSK2TPTVN1PROD with RULES 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, VerDate Sep<11>2014 15:24 Aug 10, 2015 Jkt 235001 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. PO 00000 Frm 00023 Fmt 4700 Sfmt 4700 48023 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 https:// www.regulations.gov/ #!docketDetail;D=FAA-2014-0751; or in person at the Docket Management E:\FR\FM\11AUR1.SGM 11AUR1 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. rmajette on DSK2TPTVN1PROD with RULES (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. VerDate Sep<11>2014 15:24 Aug 10, 2015 Jkt 235001 (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 PO 00000 Frm 00024 Fmt 4700 Sfmt 4700 MCAI may be found in the AD docket on the Internet at https://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: https:// 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 Office of the Assistant Secretary for Housing-Federal Housing Commissioner, HUD. ACTION: Final rule. AGENCY: This rule updates HUD fees for multifamily housing and residential healthcare facilities, and updates and SUMMARY: E:\FR\FM\11AUR1.SGM 11AUR1

Agencies

[Federal Register Volume 80, Number 154 (Tuesday, August 11, 2015)]
[Rules and Regulations]
[Pages 48022-48024]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-19474]


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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 https://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 https://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

[[Page 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 
hand-operated 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 https://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 https://www.regulations.gov/#!docketDetail;D=FAA-2014-0751; or in person at the 
Docket Management

[[Page 48024]]

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

0
1. The authority citation for part 39 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

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2. The FAA amends Sec.  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 hand-operated 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 hand-operated 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 hand-operated 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 https://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: https://www.archives.gov/federal-register/cfr/ibr-locations.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
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