83 FR 15041 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 68 (April 9, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 68 (April 9, 2018)
| Page Range | 15041-15043 | |
| FR Document | 2018-06710 |
[Federal Register Volume 83, Number 68 (Monday, April 9, 2018)] [Rules and Regulations] [Pages 15041-15043] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-06710] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2017-1176; Product Identifier 2017-NM-123-AD; Amendment 39-19237; AD 2018-07-06] 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 747-8 series airplanes. This AD was prompted by a report of restricted movement of the right brake pedals after landing rollout. This AD requires revising the airplane flight manual (AFM) by adding an autobrake system limitation. This AD also requires modifying intercostal webs near a main entry door, which terminates the AFM limitation. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective May 14, 2018. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of May 14, 2018. ADDRESSES: For service information identified in this final rule, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone 562-797-1717; internet https://www.myboeingfleet.com. You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017- 1176. 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-2017- 1176; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, the regulatory evaluation, any comments received, and other information. The address for Docket Operations (phone: 800-647- 5527) is Docket Operations, 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 Section, Seattle ACO Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3546; 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 certain The Boeing Company Model 747-8 series airplanes. The NPRM published in the Federal Register on January 2, 2018 (83 FR 80). The NPRM was prompted by a report of restricted movement of the right brake pedals after landing rollout. The NPRM proposed to require revising the AFM by adding an autobrake system limitation. The NPRM also proposed to require modifying intercostal webs near a main entry door, which would terminate the AFM limitation revision. We are issuing this AD to prevent restricted motion of the brake pedals, which can affect stopping performance and directional control of the airplane. This restricted motion can lead to high speed runway excursion or lateral runway excursion. Comments We gave the public the opportunity to participate in developing this final rule. We have considered the comment received. Boeing stated its support for the NPRM. Conclusion We reviewed the relevant data, considered the comment received, and determined that air safety and the public interest require adopting this final rule as proposed, except for minor editorial changes. We have determined that these minor changes:Are consistent with the intent that was proposed in the NPRM for addressing the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the NPRM. Related Service Information Under 1 CFR Part 51 We reviewed Boeing Alert Requirements Bulletin 747-32A2525 RB, dated September 6, 2017. This service information describes procedures for modifying intercostal webs near main entry door 3 by drilling two drain holes in the station-18 intercostal web at door stop 8 and applying sealant at the fore-aft drain path of the upper main sill web at station 16 near door 3R and door 3L. 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 2 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- AFM revision...................... 1 work-hour x $85 per hour = $0 $85 $170 $85. Modification...................... 10 work-hours x $85 per hour (\1\) 850 1,700 = $850. ---------------------------------------------------------------------------------------------------------------- \1\ We have received no definitive data that enables us to provide parts cost estimates for the modification specified in this AD. [[Page 15042]] 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 available 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. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes and associated appliances to the Director of the System Oversight Division. 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): 2018-07-06 The Boeing Company: Amendment 39-19237; Docket No. FAA- 2017-1176; Product Identifier 2017-NM-123-AD. (a) Effective Date This AD is effective May 14, 2018. (b) Affected ADs None. (c) Applicability This AD applies to The Boeing Company Model 747-8 series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 747-32A2525 RB, dated September 6, 2017, except for airplanes having line numbers 1443, 1451, 1453, 1456, 1470, 1472, 1475, 1477, 1480, 1492, 1494, 1497, 1498, 1500, 1503, 1511, 1512, 1513, and 1514. (d) Subject Air Transport Association (ATA) of America Code 32, Landing gear. (e) Unsafe Condition This AD was prompted by a report of restricted movement of the brake pedals after landing rollout. We are issuing this AD to prevent restricted motion of the brake pedals, which can affect stopping performance and directional control of the airplane. This restricted motion can lead to high speed runway excursion or lateral runway excursion. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Within 120 days after the effective date of this AD: Revise the airplane flight manual (AFM) by incorporating the limitation specified in figure 1 to paragraph (g) of this AD. [GRAPHIC] [TIFF OMITTED] TR09AP18.000 [[Page 15043]] (h) Terminating Action for AFM Limitation Within 60 months after the effective date of this AD, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Alert Requirements Bulletin 747-32A2525 RB, dated September 6, 2017, except where the requirements bulletin specifies applying sealant, the following type of sealant must be used: BMS 5-142, TYPE 2; BMS 5-95; PR-1826; or PR-1828. Doing the actions specified in this paragraph terminates the AFM limitation revision required by paragraph (g) of this AD. The AFM limitation required by paragraph (g) of this AD may be removed from the AFM after accomplishing the actions specified in this paragraph. Note 1 to paragraph (h) of this AD: Guidance for accomplishing the actions required by paragraph (h) of this AD can be found in Boeing Alert Service Bulletin 747-32A2525, dated September 6, 2017, which is referred to in Boeing Alert Requirements Bulletin 747- 32A2525 RB, dated September 6, 2017. (i) Special Flight Permit Special flight permits, as described in Section 21.197 and Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199), are not allowed, except as provided by paragraph (j) of this AD. (j) Ferry Flight Limitations Operators who are prohibited from further flight due to the autobrake system being inoperative may perform a one-time non- revenue ferry flight to fly the airplane to a maintenance facility to either fix the autobrake system or incorporate the terminating action specified in paragraph (h) of this AD. This ferry flight must be performed without passengers, and with interior modifications to allow heated cabin air to warm the brake control cables and pulleys in the vicinity of door 3L and door 3R. These interior modifications must include, at a minimum, temporarily removing the side panels and insulation immediately aft of door 3L and door 3R. (k) Alternative Methods of Compliance (AMOCs) (1) The Manager, Seattle ACO Branch, 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 certification office, send it to the attention of the person identified in paragraph (l) 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, modification, or alteration 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 Branch, to make those findings. To be approved, the repair method, modification deviation, or alteration deviation 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 Kelly McGuckin, Aerospace Engineer, Systems and Equipment Section, Seattle ACO Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3546; email: [email protected]. (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 Alert Requirements Bulletin 747-32A2525 RB, dated September 6, 2017. (ii) Reserved. (3) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740- 5600; telephone 562-797-1717; internet https://www.myboeingfleet.com. (4) You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (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 Des Moines, Washington, on March 22, 2018. Michael Kaszycki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-06710 Filed 4-6-18; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 83, No. 68 / Monday, April 9, 2018 / Rules and Regulations 15041
National Archives and Records (C&DS), 2600 Westminster Blvd., MC entry door, which would terminate the
Administration (NARA). For information on 110–SK57, Seal Beach, CA 90740–5600; AFM limitation revision. We are issuing
the availability of this material at NARA, call telephone 562–797–1717; internet this AD to prevent restricted motion of
202–741–6030, or go to: http:// https://www.myboeingfleet.com. You the brake pedals, which can affect
www.archives.gov/federal-register/cfr/ibr-
locations.html.
may view this service information at the stopping performance and directional
FAA, Transport Standards Branch, 2200 control of the airplane. This restricted
Issued in Des Moines, Washington, on South 216th St., Des Moines, WA. For motion can lead to high speed runway
March 20, 2018. information on the availability of this excursion or lateral runway excursion.
Michael Kaszycki, material at the FAA, call 206–231–3195.
Acting Director, System Oversight Division, It is also available on the internet at Comments
Aircraft Certification Service. http://www.regulations.gov by searching We gave the public the opportunity to
[FR Doc. 2018–06711 Filed 4–6–18; 8:45 am] for and locating Docket No. FAA–2017– participate in developing this final rule.
BILLING CODE 4910–13–P 1176. We have considered the comment
Examining the AD Docket received. Boeing stated its support for
the NPRM.
DEPARTMENT OF TRANSPORTATION You may examine the AD docket on
the internet at http:// Conclusion
Federal Aviation Administration www.regulations.gov by searching for
We reviewed the relevant data,
and locating Docket No. FAA–2017–
14 CFR Part 39 considered the comment received, and
1176; or in person at Docket Operations
determined that air safety and the
[Docket No. FAA–2017–1176; Product between 9 a.m. and 5 p.m., Monday
public interest require adopting this
Identifier 2017–NM–123–AD; Amendment through Friday, except Federal holidays.
final rule as proposed, except for minor
39–19237; AD 2018–07–06] The AD docket contains this final rule,
editorial changes. We have determined
the regulatory evaluation, any
RIN 2120–AA64 that these minor changes:
comments received, and other
information. The address for Docket • Are consistent with the intent that
Airworthiness Directives; The Boeing was proposed in the NPRM for
Company Airplanes Operations (phone: 800–647–5527) is
Docket Operations, U.S. Department of addressing the unsafe condition; and
AGENCY: Federal Aviation Transportation, Docket Operations, M– • Do not add any additional burden
Administration (FAA), DOT. 30, West Building Ground Floor, Room upon the public than was already
ACTION: Final rule. W12–140, 1200 New Jersey Avenue SE, proposed in the NPRM.
Washington, DC 20590. Related Service Information Under 1
SUMMARY: We are adopting a new FOR FURTHER INFORMATION CONTACT:
airworthiness directive (AD) for certain CFR Part 51
Kelly McGuckin, Aerospace Engineer,
The Boeing Company Model 747–8 Systems and Equipment Section, Seattle We reviewed Boeing Alert
series airplanes. This AD was prompted ACO Branch, FAA, 2200 South 216th Requirements Bulletin 747–32A2525
by a report of restricted movement of St., Des Moines, WA 98198; telephone RB, dated September 6, 2017. This
the right brake pedals after landing and fax 206–231–3546; email: service information describes
rollout. This AD requires revising the Kelly.McGuckin@faa.gov. procedures for modifying intercostal
airplane flight manual (AFM) by adding SUPPLEMENTARY INFORMATION: webs near main entry door 3 by drilling
an autobrake system limitation. This AD two drain holes in the station-18
also requires modifying intercostal webs Discussion intercostal web at door stop 8 and
near a main entry door, which We issued a notice of proposed applying sealant at the fore-aft drain
terminates the AFM limitation. We are rulemaking (NPRM) to amend 14 CFR path of the upper main sill web at
issuing this AD to address the unsafe part 39 by adding an AD that would station 16 near door 3R and door 3L.
condition on these products. apply to certain The Boeing Company This service information is reasonably
DATES: This AD is effective May 14, Model 747–8 series airplanes. The available because the interested parties
2018. NPRM published in the Federal have access to it through their normal
The Director of the Federal Register Register on January 2, 2018 (83 FR 80). course of business or by the means
approved the incorporation by reference The NPRM was prompted by a report of identified in the ADDRESSES section.
of a certain publication listed in this AD restricted movement of the right brake
as of May 14, 2018. Costs of Compliance
pedals after landing rollout. The NPRM
ADDRESSES: For service information proposed to require revising the AFM by We estimate that this AD affects 2
identified in this final rule, contact adding an autobrake system limitation. airplanes of U.S. registry. We estimate
Boeing Commercial Airplanes, The NPRM also proposed to require the following costs to comply with this
Attention: Contractual & Data Services modifying intercostal webs near a main AD:
ESTIMATED COSTS
Cost on
Cost per
Action Labor cost Parts cost U.S.
product operators
sradovich on DSK3GMQ082PROD with RULES
AFM revision ..... 1 work-hour × $85 per hour = $85 ............................................................... $0 $85 $170
Modification ....... 10 work-hours × $85 per hour = $850 ......................................................... (1) 850 1,700
1 We have received no definitive data that enables us to provide parts cost estimates for the modification specified in this AD.
VerDate Sep<11>2014 16:01 Apr 06, 2018 Jkt 244001 PO 00000 Frm 00023 Fmt 4700 Sfmt 4700 E:\FR\FM\09APR1.SGM 09APR1](https://thefederalregister.org/doc/83_FR_15109/page/1.svg)
![Federal Register / Vol. 83, No. 68 / Monday, April 9, 2018 / Rules and Regulations 15043
(h) Terminating Action for AFM Limitation been authorized by the Manager, Seattle ACO DEPARTMENT OF TRANSPORTATION
Within 60 months after the effective date Branch, to make those findings. To be
of this AD, do all applicable actions approved, the repair method, modification Federal Aviation Administration
identified in, and in accordance with, the deviation, or alteration deviation must meet
Accomplishment Instructions of Boeing Alert the certification basis of the airplane, and the 14 CFR Part 39
Requirements Bulletin 747–32A2525 RB, approval must specifically refer to this AD.
dated September 6, 2017, except where the [Docket No. FAA–2018–0285; Product
requirements bulletin specifies applying (l) Related Information Identifier 2018–CE–010–AD; Amendment
sealant, the following type of sealant must be (1) For more information about this AD, 39–19245; AD 2018–07–14]
used: BMS 5–142, TYPE 2; BMS 5–95; PR– contact Kelly McGuckin, Aerospace RIN 2120–AA64
1826; or PR–1828. Doing the actions
Engineer, Systems and Equipment Section,
specified in this paragraph terminates the Airworthiness Directives; Pacific
AFM limitation revision required by Seattle ACO Branch, FAA, 2200 South 216th
paragraph (g) of this AD. The AFM limitation St., Des Moines, WA 98198; telephone and Aerospace Limited Airplanes
required by paragraph (g) of this AD may be fax 206–231–3546; email: Kelly.McGuckin@
faa.gov.
AGENCY: Federal Aviation
removed from the AFM after accomplishing
(2) Service information identified in this
Administration (FAA), DOT.
the actions specified in this paragraph.
Note 1 to paragraph (h) of this AD: AD that is not incorporated by reference is ACTION: Final rule; request for
Guidance for accomplishing the actions available at the addresses specified in comments.
required by paragraph (h) of this AD can be paragraphs (m)(3) and (m)(4) of this AD.
found in Boeing Alert Service Bulletin 747– SUMMARY: We are adopting a new
32A2525, dated September 6, 2017, which is (m) Material Incorporated by Reference airworthiness directive (AD) for certain
referred to in Boeing Alert Requirements (1) The Director of the Federal Register Pacific Aerospace Limited Model 750XL
Bulletin 747–32A2525 RB, dated September approved the incorporation by reference airplanes. This AD results from
6, 2017. (IBR) of the service information listed in this mandatory continuing airworthiness
paragraph under 5 U.S.C. 552(a) and 1 CFR information (MCAI) issued by the
(i) Special Flight Permit
part 51. aviation authority of another country to
Special flight permits, as described in identify and correct an unsafe condition
(2) You must use this service information
Section 21.197 and Section 21.199 of the
Federal Aviation Regulations (14 CFR 21.197 as applicable to do the actions required by on an aviation product. The MCAI
and 21.199), are not allowed, except as this AD, unless the AD specifies otherwise. describes the unsafe condition as
provided by paragraph (j) of this AD. (i) Boeing Alert Requirements Bulletin insufficient engagement of the couplings
747–32A2525 RB, dated September 6, 2017. with the flex drive of the rudder trim
(j) Ferry Flight Limitations
(ii) Reserved. drive system. We are issuing this AD to
Operators who are prohibited from further (3) For service information identified in require actions to address the unsafe
flight due to the autobrake system being this AD, contact Boeing Commercial condition on these products.
inoperative may perform a one-time non- Airplanes, Attention: Contractual & Data
revenue ferry flight to fly the airplane to a DATES: This AD is effective April 30,
Services (C&DS), 2600 Westminster Blvd., 2018.
maintenance facility to either fix the
autobrake system or incorporate the MC 110–SK57, Seal Beach, CA 90740–5600; The Director of the Federal Register
terminating action specified in paragraph (h) telephone 562–797–1717; internet https:// approved the incorporation by reference
of this AD. This ferry flight must be www.myboeingfleet.com. of a certain publication listed in the AD
performed without passengers, and with (4) You may view this service information as of April 30, 2018.
interior modifications to allow heated cabin at the FAA, Transport Standards Branch, We must receive comments on this
air to warm the brake control cables and 2200 South 216th St., Des Moines, WA. For
pulleys in the vicinity of door 3L and door
AD by May 24, 2018.
information on the availability of this
3R. These interior modifications must ADDRESSES: You may send comments by
material at the FAA, call 206–231–3195.
include, at a minimum, temporarily
(5) You may view this service information any of the following methods:
removing the side panels and insulation
that is incorporated by reference at the • Federal eRulemaking Portal: Go to
immediately aft of door 3L and door 3R. http://www.regulations.gov. Follow the
National Archives and Records
(k) Alternative Methods of Compliance Administration (NARA). For information on instructions for submitting comments.
(AMOCs) the availability of this material at NARA, call • Fax: (202) 493–2251.
(1) The Manager, Seattle ACO Branch, 202–741–6030, or go to: http:// • Mail: U.S. Department of
FAA, has the authority to approve AMOCs www.archives.gov/federal-register/cfr/ibr- Transportation, Docket Operations, M–
for this AD, if requested using the procedures locations.html. 30, West Building Ground Floor, Room
found in 14 CFR 39.19. In accordance with W12–140, 1200 New Jersey Avenue SE,
14 CFR 39.19, send your request to your Issued in Des Moines, Washington, on Washington, DC 20590.
principal inspector or local Flight Standards March 22, 2018. • Hand Delivery: U.S. Department of
District Office, as appropriate. If sending Michael Kaszycki, Transportation, Docket Operations, M–
information directly to the manager of the
certification office, send it to the attention of Acting Director, System Oversight Division, 30, West Building Ground Floor, Room
the person identified in paragraph (l) of this Aircraft Certification Service. W12–140, 1200 New Jersey Avenue SE,
AD. Information may be emailed to: 9-ANM- [FR Doc. 2018–06710 Filed 4–6–18; 8:45 am] Washington, DC 20590, between 9 a.m.
Seattle-ACO-AMOC-Requests@faa.gov. BILLING CODE 4910–13–P and 5 p.m., Monday through Friday,
(2) Before using any approved AMOC, except Federal holidays.
notify your appropriate principal inspector, For service information identified in
or lacking a principal inspector, the manager this AD, contact Pacific Aerospace
sradovich on DSK3GMQ082PROD with RULES
of the local flight standards district office/ Limited, Airport Road, Hamilton,
certificate holding district office.
Private Bag 3027, Hamilton 3240, New
(3) An AMOC that provides an acceptable
level of safety may be used for any repair, Zealand; phone: +64 7843 6144; fax: +64
modification, or alteration required by this 843 6134; email: pacific@
AD if it is approved by the Boeing aerospace.co.nz; Internet:
Commercial Airplanes Organization www.aerospace.co.nz. You may view
Designation Authorization (ODA) that has this referenced service information at
VerDate Sep<11>2014 16:01 Apr 06, 2018 Jkt 244001 PO 00000 Frm 00025 Fmt 4700 Sfmt 4700 E:\FR\FM\09APR1.SGM 09APR1](https://thefederalregister.org/doc/83_FR_15109/page/3.svg)
Document Created: 2018-04-07 02:38:57
Document Modified: 2018-04-07 02:38:57
| 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 May 14, 2018. | |
| Contact | Kelly McGuckin, Aerospace Engineer, Systems and Equipment Section, Seattle ACO Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3546; email: [email protected] | |
| FR Citation | 83 FR 15041 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
2025 Federal Register | Disclaimer | Privacy Policy
USC | CFR | eCFR