80 FR 34244 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 115 (June 16, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 115 (June 16, 2015)
| Page Range | 34244-34246 | |
| FR Document | 2015-14397 |
[Federal Register Volume 80, Number 115 (Tuesday, June 16, 2015)] [Rules and Regulations] [Pages 34244-34246] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-14397] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2014-0575; Directorate Identifier 2014-NM-086-AD; Amendment 39-18181; AD 2015-12-07] 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 all The Boeing Company Model 747-8F and 747-8 series airplanes. This AD was prompted by reports of delamination damage to leading edge (LE) variable camber krueger (VCK) flaps. This AD requires repetitive inspections to detect delamination damage of the lightning strike applique (LSA) on certain LE VCK flaps, and corrective actions if necessary. We are issuing this AD to detect and correct delamination damage to certain LE VCK flaps, which can reduce the lightning strike protection capability on certain LE VCK flaps and result in an uncommanded motion of the trailing edge flap system; such uncommanded flap motion, without shutdown of the trailing edge or leading edge flaps, could cause unexpected changes in lift, potentially resulting in asymmetric lift and loss of control of the airplane. DATES: This AD is effective July 21, 2015. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 21, 2015. ADDRESSES: For 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. 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 2014-0575. Examining the AD Docket You may examine the AD docket on the Internet at http:// [[Page 34245]] www.regulations.gov by searching for and locating Docket No. FAA-2014- 0575; 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: Kelly McGuckin, Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-6490; fax: 425-917-6590; email: [email protected]. 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 all The Boeing Company Model 747-8F and 747-8 series airplanes. The NPRM published in the Federal Register on August 26, 2014 (79 FR 50875). The NPRM was prompted by reports of delamination damage to LE VCK flaps. The NPRM proposed to require repetitive inspections to detect delamination damage of the LSA on the LE VCK flaps at positions 6 through 9 (left wing) and 18 through 21 (right wing), and corrective actions if necessary. We are issuing this AD to detect and correct delamination damage to certain LE VCK flaps, which can reduce the lightning strike protection capability on the LE VCK flaps and result in an uncommanded motion of the trailing edge flap system. Such uncommanded flap motion, without shutdown of the trailing edge or leading edge flaps, could cause unexpected changes in lift, potentially resulting in asymmetric lift and loss of control of the airplane. Comments We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the NPRM (79 FR 50875, August 26, 2014) and the FAA's response to each comment. Request To Revise Component Description Boeing requested that we revise the NPRM (79 FR 50875, August 26, 2014) to describe the affected LE flaps with lightning strike applique installed as the LE VCK flaps at positions 6 through 9 (left wing) and 18 through 21 (right wing). Boeing pointed out that only the affected flaps should be specified, instead of all LE VCK flaps. We agree with the commenter's request. Not all LE VCK flaps are affected by the identified unsafe condition. We have revised the SUMMARY section of this final rule and paragraph (e) of this AD to specify ``certain'' LE VCK flaps. We have also revised the DISCUSSION section of this final rule and paragraph (g) of this AD to specify LE VCK flaps at position 6 through 9 (left wing) and 18 through 21 (right wing). Request To Correct Typographical Errors Boeing requested that we revise the service bulletin title in the ``Differences Between this Proposed AD and the Service Information'' section and paragraphs (g) and (h) of the NPRM (79 FR 50875, August 26, 2014) from Boeing Alert Service Bulletin 747-57-2338, dated January 14, 2014; to Boeing Special Attention Service Bulletin 747-57-2338, dated January 14, 2014. Boeing also requested that we revise ``Original issue'' in paragraph (h) of the NPRM (79 FR 50875, August 26, 2014) to ``Original Issue.'' We agree with the commenter's request to correct the identified typographical errors. We have revised paragraphs (g) and (h) of this AD accordingly. However, because the ``Differences Between this Proposed AD and the Service Information'' section is not repeated in the final rule, no change is necessary in this regard. 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 50875, August 26, 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 50875, August 26, 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 We reviewed Boeing Special Attention Service Bulletin 747-57-2338, dated January 14, 2014. The service information describes procedures for inspections to detect delamination damage of the LSA on the LE VCK flaps 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 of this AD. Costs of Compliance We estimate that this AD affects 6 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost on U.S. Action Labor cost Parts cost Cost per product operators ---------------------------------------------------------------------------------------------------------------- Inspection....................... 8 work-hours x $85 $0 $680 per inspection $4,080 per per hour = $680 cycle. inspection cycle per inspection cycle. ---------------------------------------------------------------------------------------------------------------- We have received no definitive data that would enable us to provide cost estimates for the on-condition actions specified in this AD. 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: [[Page 34246]] 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 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] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2015-12-07 The Boeing Company: Amendment 39-18181; Docket No. FAA- 2014-0575; Directorate Identifier 2014-NM-086-AD. (a) Effective Date This AD is effective July 21, 2015. (b) Affected ADs None. (c) Applicability This AD applies to all The Boeing Company Model 747-8F and 747-8 series airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 57, Wings. (e) Unsafe Condition This AD was prompted by reports of delamination damage to leading edge (LE) variable camber krueger (VCK) flaps. We are issuing this AD to detect and correct delamination damage to certain LE VCK flaps, which can reduce the lightning strike protection capability on certain LE VCK flaps and result in an uncommanded motion of the trailing edge flap system. Such uncommanded flap motion, without shutdown of the trailing edge or leading edge flaps, may cause unexpected changes in lift, potentially resulting in asymmetric lift and loss of control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Inspections and Corrective Actions Except as specified in paragraph (h) of this AD, at the applicable time specified in paragraph 1.E., ``Compliance,'' of Boeing Special Attention Service Bulletin 747-57-2338, dated January 14, 2014: Do a general visual inspection to detect delamination damage of the lightning strike applique (LSA) on the LE VCK flaps at positions 6 through 9 (left wing) and 18 through 21 (right wing); and do all applicable corrective actions before further flight; in accordance with the Accomplishment Instructions of Boeing Special Attention Service Bulletin 747-57-2338, dated January 14, 2014. Repeat the inspection of the LSA on the LE VCK flaps at positions 6 through 9 (left wing) and 18 through 21 (right wing) thereafter at the applicable intervals specified in paragraph 1.E., ``Compliance,'' of Boeing Special Attention Service Bulletin 747-57- 2338, dated January 14, 2014. (h) Exception to Service Information Where Paragraph 1.E., ``Compliance,'' of Boeing Special Attention Service Bulletin 747-57-2338, dated January 14, 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. (i) 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 (j)(1) of this AD. Information may be emailed to: [email protected]. (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. (j) Related Information For more information about this AD, contact Kelly McGuckin, Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-6490; fax: 425-917-6590; email: [email protected]. (k) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Boeing Special Attention Service Bulletin 747-57-2338, dated January 14, 2014. (ii) Reserved. (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 referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Renton, Washington on June 3, 2015. Jeffrey E. Duven, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-14397 Filed 6-15-15; 8:45 am] BILLING CODE 4910-13-P
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Citation extinguisher on the ground or in flight) DEPARTMENT OF TRANSPORTATION
The authority citation for these from entering any personnel
compartment, even though a defect may Federal Aviation Administration
special conditions is as follows:
exist in the extinguishing system. This
Authority: 49 U.S.C. 106(g), 40113 and must be shown by test except for built- 14 CFR Part 39
44701; 14 CFR 21.16 and 21.17; and 14 CFR
in carbon dioxide fuselage compartment [Docket No. FAA–2014–0575; Directorate
11.38 and 11.19.
fire extinguishing systems for which— Identifier 2014–NM–086–AD; Amendment
The Special Conditions (1) Five pounds or less of carbon 39–18181; AD 2015–12–07]
■ Accordingly, pursuant to the authority dioxide will be discharged, under RIN 2120–AA64
delegated to me by the Administrator, established fire control procedures, into
the following special conditions are any fuselage compartment; or Airworthiness Directives; The Boeing
issued as part of the type certification (2) Protective breathing equipment is Company Airplanes
basis for Honda Airplane Company available for each flight member on
flight deck duty. AGENCY: Federal Aviation
model HA–420 airplanes. Administration (FAA), DOT.
1. Fire Extinguishing for Overwing SC 23.1199 Extinguishing Agent ACTION: Final rule.
Pylon Mounted Engines Containers
SUMMARY: We are adopting a new
SC 23.1195 Fire Extinguishing The following applies: airworthiness directive (AD) for all The
Systems (a) Each extinguishing agent container Boeing Company Model 747–8F and
must have a pressure relief valve to 747–8 series airplanes. This AD was
(a) Fire extinguishing systems must be prevent bursting of the container by
installed and compliance shown with prompted by reports of delamination
excessive internal pressures. damage to leading edge (LE) variable
the following:
(b) The discharge end of each camber krueger (VCK) flaps. This AD
(1) Except for combustor, turbine, and
discharge line from a pressure relief requires repetitive inspections to detect
tailpipe sections of turbine-engine
connection must be located so that delamination damage of the lightning
installations that contain lines or
discharge of the fire-extinguishing agent strike applique (LSA) on certain LE VCK
components carrying flammable fluids
would not damage the airplane. The line flaps, and corrective actions if
or gases for which a fire originating in
must also be located or protected to necessary. We are issuing this AD to
these sections is shown to be
prevent clogging caused by ice or other detect and correct delamination damage
controllable, a fire extinguisher system
foreign matter. to certain LE VCK flaps, which can
must serve each engine compartment.
(2) The fire extinguishing system, the (c) A means must be provided for reduce the lightning strike protection
quantity of the extinguishing agent, the each fire extinguishing agent container capability on certain LE VCK flaps and
rate of discharge, and the discharge to indicate that the container has result in an uncommanded motion of
distribution must be adequate to discharged or that the charging pressure the trailing edge flap system; such
extinguish fires. An individual ‘‘one- is below the established minimum uncommanded flap motion, without
shot’’ system may be used except for necessary for proper functioning. shutdown of the trailing edge or leading
embedded engines where a ‘‘two shot’’ (d) The temperature of each container edge flaps, could cause unexpected
system must be used. must be maintained under intended changes in lift, potentially resulting in
(3) The fire extinguishing system for operating conditions, to prevent the asymmetric lift and loss of control of the
a nacelle must be able to simultaneously pressure in the container from— airplane.
protect each compartment of the nacelle (1) Falling below that necessary to DATES: This AD is effective July 21,
for which protection is provided. provide an adequate rate of discharge; or 2015.
(b) If an auxiliary power unit is (2) Rising high enough to cause The Director of the Federal Register
installed in any airplane certificated to premature discharge. approved the incorporation by reference
this part, that auxiliary power unit (e) If a pyrotechnic capsule is used to of a certain publication listed in this AD
compartment must be served by a fire discharge the extinguishing agent, each as of July 21, 2015.
extinguishing system meeting the container must be installed so that ADDRESSES: For service information
requirements of paragraph (a)(2) of this temperature conditions will not cause identified in this AD, contact Boeing
section. hazardous deterioration of the Commercial Airplanes, Attention: Data
pyrotechnic capsule. & Services Management, P. O. Box 3707,
SC 23.1197 Fire Extinguishing Agents MC 2H–65, Seattle, WA 98124–2207;
The following applies: SC 23.1201 Fire Extinguishing System telephone 206–544–5000, extension 1;
(a) Fire extinguishing agents must— Materials fax 206–766–5680; Internet https://
(1) Be capable of extinguishing flames The following apply: www.myboeingfleet.com. You may view
emanating from any burning of fluids or (a) No material in any fire this referenced service information at
other combustible materials in the area extinguishing system may react the FAA, Transport Airplane
protected by the fire extinguishing chemically with any extinguishing agent Directorate, 1601 Lind Avenue SW.,
system; and so as to create a hazard. Renton, WA. For information on the
(2) Have thermal stability over the (b) Each system component in an availability of this material at the FAA,
temperature range likely to be engine compartment must be fireproof. call 425–227–1221. It is also available
asabaliauskas on DSK5VPTVN1PROD with RULES
experienced in the compartment in on the Internet at http://
which they are stored. Issued in Kansas City, Missouri, on June 9, www.regulations.gov by searching for
(b) If any toxic extinguishing agent is 2015.
and locating Docket No. FAA 2014–
used, provisions must be made to Earl Lawrence, 0575.
prevent harmful concentrations of fluid Small Airplane Directorate, Aircraft
or fluid vapors (from leakage during Certification Service. Examining the AD Docket
normal operation of the airplane or as a [FR Doc. 2015–14816 Filed 6–15–15; 8:45 am] You may examine the AD docket on
result of discharging the fire BILLING CODE 4910–13–P the Internet at http://
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![34246 Federal Register / Vol. 80, No. 115 / Tuesday, June 16, 2015 / Rules and Regulations
Aviation Programs, describes in more (a) Effective Date or local Flight Standards District Office, as
detail the scope of the Agency’s This AD is effective July 21, 2015. appropriate. If sending information directly
authority. to the manager of the ACO, send it to the
(b) Affected ADs attention of the person identified in
We are issuing this rulemaking under
the authority described in Subtitle VII, None. paragraph (j)(1) of this AD. Information may
be emailed to: 9-ANM-Seattle-ACO-AMOC-
Part A, Subpart III, Section 44701: (c) Applicability Requests@faa.gov.
‘‘General requirements.’’ Under that This AD applies to all The Boeing (2) Before using any approved AMOC,
section, Congress charges the FAA with Company Model 747–8F and 747–8 series notify your appropriate principal inspector,
promoting safe flight of civil aircraft in airplanes, certificated in any category. or lacking a principal inspector, the manager
air commerce by prescribing regulations of the local flight standards district office/
(d) Subject
for practices, methods, and procedures certificate holding district office.
the Administrator finds necessary for Air Transport Association (ATA) of (3) An AMOC that provides an acceptable
safety in air commerce. This regulation America Code 57, Wings. level of safety may be used for any repair
is within the scope of that authority (e) Unsafe Condition required by this AD if it is approved by the
because it addresses an unsafe condition This AD was prompted by reports of Boeing Commercial Airplanes Organization
that is likely to exist or develop on delamination damage to leading edge (LE) Designation Authorization (ODA) that has
products identified in this rulemaking variable camber krueger (VCK) flaps. We are been authorized by the Manager, Seattle
action. issuing this AD to detect and correct ACO, to make those findings. For a repair
delamination damage to certain LE VCK method to be approved, the repair must meet
Regulatory Findings flaps, which can reduce the lightning strike the certification basis of the airplane.
This AD will not have federalism protection capability on certain LE VCK flaps (j) Related Information
implications under Executive Order and result in an uncommanded motion of the
trailing edge flap system. Such For more information about this AD,
13132. This AD will not have a contact Kelly McGuckin, Aerospace
uncommanded flap motion, without
substantial direct effect on the States, on shutdown of the trailing edge or leading edge Engineer, Systems and Equipment Branch,
the relationship between the national flaps, may cause unexpected changes in lift, ANM–130S, FAA, Seattle Aircraft
government and the States, or on the potentially resulting in asymmetric lift and Certification Office, 1601 Lind Avenue SW.,
distribution of power and loss of control of the airplane. Renton, WA 98057–3356; phone: 425–917–
responsibilities among the various 6490; fax: 425–917–6590; email:
(f) Compliance kelly.mcguckin@faa.gov.
levels of government.
For the reasons discussed above, I Comply with this AD within the
compliance times specified, unless already (k) Material Incorporated by Reference
certify that this AD:
(1) Is not a ‘‘significant regulatory done. (1) The Director of the Federal Register
action’’ under Executive Order 12866, approved the incorporation by reference
(g) Inspections and Corrective Actions
(2) Is not a ‘‘significant rule’’ under (IBR) of the service information listed in this
Except as specified in paragraph (h) of this paragraph under 5 U.S.C. 552(a) and 1 CFR
DOT Regulatory Policies and Procedures AD, at the applicable time specified in part 51.
(44 FR 11034, February 26, 1979), paragraph 1.E., ‘‘Compliance,’’ of Boeing (2) You must use this service information
(3) Will not affect intrastate aviation Special Attention Service Bulletin 747–57– as applicable to do the actions required by
in Alaska, and 2338, dated January 14, 2014: Do a general this AD, unless the AD specifies otherwise.
(4) Will not have a significant visual inspection to detect delamination (i) Boeing Special Attention Service
economic impact, positive or negative, damage of the lightning strike applique (LSA) Bulletin 747–57–2338, dated January 14,
on a substantial number of small entities on the LE VCK flaps at positions 6 through 2014.
under the criteria of the Regulatory 9 (left wing) and 18 through 21 (right wing);
(ii) Reserved.
and do all applicable corrective actions
Flexibility Act. (3) For Boeing service information
before further flight; in accordance with the
identified in this AD, contact Boeing
List of Subjects in 14 CFR Part 39 Accomplishment Instructions of Boeing
Commercial Airplanes, Attention: Data &
Special Attention Service Bulletin 747–57–
Air transportation, Aircraft, Aviation 2338, dated January 14, 2014. Repeat the Services Management, P. O. Box 3707, MC
safety, Incorporation by reference, inspection of the LSA on the LE VCK flaps 2H–65, Seattle, WA 98124–2207; telephone
Safety. at positions 6 through 9 (left wing) and 18 206–544–5000, extension 1; fax 206–766–
through 21 (right wing) thereafter at the 5680; Internet https://
Adoption of the Amendment applicable intervals specified in paragraph www.myboeingfleet.com.
Accordingly, under the authority 1.E., ‘‘Compliance,’’ of Boeing Special (4) You may view this referenced service
delegated to me by the Administrator, Attention Service Bulletin 747–57–2338, information at the FAA, Transport Airplane
dated January 14, 2014. Directorate, 1601 Lind Avenue SW., Renton,
the FAA amends 14 CFR part 39 as WA. For information on the availability of
follows: (h) Exception to Service Information this material at the FAA, call 425–227–1221.
Where Paragraph 1.E., ‘‘Compliance,’’ of (5) You may view this service information
PART 39—AIRWORTHINESS that is incorporated by reference at the
Boeing Special Attention Service Bulletin
DIRECTIVES 747–57–2338, dated January 14, 2014, National Archives and Records
specifies a compliance time ‘‘after the Administration (NARA). For information on
■ 1. The authority citation for part 39 Original Issue date of this service bulletin,’’ the availability of this material at NARA, call
continues to read as follows: this AD requires compliance within the 202–741–6030, or go to: http://
Authority: 49 U.S.C. 106(g), 40113, 44701. specified compliance time after the effective www.archives.gov/federal-register/cfr/ibr-
date of this AD. locations.html.
asabaliauskas on DSK5VPTVN1PROD with RULES
§ 39.13 [Amended]
(i) Alternative Methods of Compliance Issued in Renton, Washington on June 3,
■ 2. The FAA amends § 39.13 by adding (AMOCs) 2015.
the following new airworthiness (1) The Manager, Seattle Aircraft
directive (AD): Jeffrey E. Duven,
Certification Office (ACO), FAA, has the
Manager, Transport Airplane Directorate,
2015–12–07 The Boeing Company: authority to approve AMOCs for this AD, if
Aircraft Certification Service.
Amendment 39–18181; Docket No. requested using the procedures found in 14
FAA–2014–0575; Directorate Identifier CFR 39.19. In accordance with 14 CFR 39.19, [FR Doc. 2015–14397 Filed 6–15–15; 8:45 am]
2014–NM–086–AD. send your request to your principal inspector BILLING CODE 4910–13–P
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Document Created: 2018-02-22 10:22:59
Document Modified: 2018-02-22 10:22:59
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final rule. | |
| Dates | This AD is effective July 21, 2015. | |
| Contact | Kelly McGuckin, Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-6490; fax: 425-917-6590; email: [email protected] | |
| FR Citation | 80 FR 34244 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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