82 FR 33007 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 137 (July 19, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 137 (July 19, 2017)
| Page Range | 33007-33009 | |
| FR Document | 2017-14584 |
[Federal Register Volume 82, Number 137 (Wednesday, July 19, 2017)] [Rules and Regulations] [Pages 33007-33009] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-14584] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-9506; Directorate Identifier 2016-NM-090-AD; Amendment 39-18957; AD 2017-14-13] 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 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD was prompted by a report of an aborted takeoff because the rudder pedals were not operating correctly. Investigation revealed a protruding screw in the rudder pedal heel rest adjacent to the pedals. This AD requires a torque check of the screws in the cover assembly of the heel rest for both the Captain and the First Officer's rudder pedals, and corrective action if necessary. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective August 23, 2017. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of August 23, 2017. ADDRESSES: For service information identified in this final rule, 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-2016- 9506. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 9506; 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 (ACO), 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 certain The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. The NPRM published in the Federal Register on December 20, 2016 (81 FR 92753). The NPRM was prompted by a report of an aborted takeoff because the rudder pedals were not operating correctly. Investigation revealed a protruding screw in the rudder pedal heel rest adjacent to the pedals. It was determined that the screws in the cover assembly of the heel rest for both the Captain and the First Officer's rudder pedals might not have been properly torqued. The NPRM proposed to require a torque check of the screws in the cover assembly of the heel rest for both the Captain and the First Officer's rudder pedals, and corrective action if necessary. We are issuing this AD to detect and correct a protruding screw in the cover assembly of the heel rest of a rudder pedal. A protruding screw could restrict rudder pedal motion and reduce differential braking control during takeoff or landing, which could cause a high speed runway excursion. Comments We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the NPRM and the FAA's response to each comment. Support for the NPRM Boeing, Air Line Pilots Association, International, and Tyler Myers supported the intent of the NPRM. Request To Allow Credit for Previously Accomplished Actions United Airlines noted that the NPRM did not address whether or not the final rule would allow operators to take credit for accomplishment of the actions in Boeing Alert Service Bulletin 737-25A1732, Revision 1, dated August 15, 2016 (``BASB 737-25A1732, Revision 1''), if completed prior to the effective date of the final rule. We infer that the commenter is requesting that the final rule include a statement that accomplishment of the actions specified in BASB 737-25A1732, Revision 1, prior to the effective date of the final rule is acceptable for compliance with the requirements of the final rule. We agree with the commenter that operators should be able to take credit for accomplishment of the actions in BASB 737-25A1732, Revision 1, prior to the effective date of this AD. This allowance was provided in paragraph (f) of the proposed AD in the statement ``Comply with this AD within the compliance times specified unless already done.'' However, since the NPRM was issued, Boeing has published, and we have reviewed, Boeing Alert Service Bulletin 737-25A1732, Revision 2, dated April 13, [[Page 33008]] 2017 (``BASB 737-25A1732, Revision 2''). BASB 737-25A1732, Revision 2, provides clarification of the actions described in the work instructions by providing supplementary details and including additional descriptive figures. No additional work is necessary and the scope of this AD is not expanded. We have revised paragraphs (c), (g), and (h) of this AD to refer to BASB 737-25A1732, Revision 2. We have also added paragraph (i) to this AD to give credit for actions accomplished using the work instructions in BASB 737-25A1732, Revision 1; and redesignated the subsequent paragraphs accordingly. Effect of Winglets on Accomplishment of the Proposed Actions Aviation Partners Boeing stated that the installation of winglets per Supplemental Type Certificate (STC) ST00830SE does not affect the accomplishment of the manufacturer's service instructions. We agree with the commenter that STC ST00830SE does not affect the accomplishment of the manufacturer's service instructions. Therefore, the installation of STC ST00830SE does not affect the ability to accomplish the actions required by this AD. We have not changed this AD 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 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 correcting 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 Service Bulletin 737-25A1732, Revision 2, dated April 13, 2017. The service information describes procedures for a torque check of the screws in the cover assembly of the heel rest for both the Captain and the First Officer's rudder pedals, and corrective action. 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 1,187 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 ---------------------------------------------------------------------------------------------------------------- Torque check...................... 2 work-hours x $85 per $0 $170 $201,790 hour = $170. ---------------------------------------------------------------------------------------------------------------- We have received no definitive data that will enable us to provide cost estimates for the on-condition actions specified in this AD. Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency's authority. We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: ``General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a ``significant regulatory action'' under Executive Order 12866, (2) Is not a ``significant rule'' under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate aviation in Alaska, and (4) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 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): 2017-14-13 The Boeing Company: Amendment 39-18957; Docket No. FAA- 2016-9506; Directorate Identifier 2016-NM-090-AD. (a) Effective Date This AD is effective August 23, 2017. (b) Affected ADs None. (c) Applicability This AD applies to The Boeing Company Model 737-600, -700, - 700C, -800, -900, and -900ER series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737- 25A1732, Revision 2, dated April 13, 2017. (d) Subject Air Transport Association (ATA) of America Code 25, Equipment and Furnishings. (e) Unsafe Condition This AD was prompted by a report of an aborted takeoff because the rudder pedals were not operating correctly. Investigation revealed a protruding screw in the rudder pedal heel rest adjacent to the pedals. It was determined that the screws in the cover assembly of the heel rest for both the Captain and the First Officer's rudder pedals might [[Page 33009]] not have been properly torqued. We are issuing this AD to detect and correct a protruding screw in the cover assembly of the heel rest of a rudder pedal. A protruding screw could restrict rudder pedal motion and reduce differential braking control during takeoff or landing, which could cause a high speed runway excursion. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Torque Check Within 21 months after the effective date of this AD: Do a one- time torque check of the screws in the cover assembly of the heel rest for both the Captain and the First Officer's rudder pedals, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 737-25A1732, Revision 2, dated April 13, 2017. (h) Corrective Action If the results of the torque check required by paragraph (g) of this AD indicate that any screw does not hold torque to the required value, before further flight, replace the affected screw and associated nutplate, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 737-25A1732, Revision 2, dated April 13, 2017. (i) Credit for Actions Accomplished Previously This paragraph provides credit for the actions specified in paragraphs (g) and (h) of this AD, if those actions were performed before the effective date of this AD using Boeing Alert Service Bulletin 737-25A1732, Revision 1, dated August 15, 2016. (j) 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 (k)(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, 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, 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. (4) For service information that contains steps that are labeled as Required for Compliance (RC), the provisions of paragraphs (j)(4)(i) and (j)(4)(ii) of this AD apply. (i) The steps labeled as RC, including substeps under an RC step and any figures identified in an RC step, must be done to comply with the AD. If a step or sub-step is labeled ``RC Exempt,'' then the RC requirement is removed from that step or sub-step. An AMOC is required for any deviations to RC steps, including substeps and identified figures. (ii) Steps not labeled as RC may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC, provided the RC steps, including substeps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition. (k) Related Information (1) For more information about this AD, contact Kelly McGuckin, Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle ACO, 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-6490; fax: 425-917-6590; email: [email protected]. (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 the AD specifies otherwise. (i) Boeing Alert Service Bulletin 737-25A1732, Revision 2, dated April 13, 2017. (ii) Reserved. (3) 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. (4) You may view this service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Renton, Washington, on June 29, 2017. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2017-14584 Filed 7-18-17; 8:45 am] BILLING CODE 4910-13-P
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(l) Material Incorporated by Reference the cover assembly of the heel rest for Register on December 20, 2016 (81 FR
(1) The Director of the Federal Register both the Captain and the First Officer’s 92753). The NPRM was prompted by a
approved the incorporation by reference rudder pedals, and corrective action if report of an aborted takeoff because the
(IBR) of the service information listed in this necessary. We are issuing this AD to rudder pedals were not operating
paragraph under 5 U.S.C. 552(a) and 1 CFR address the unsafe condition on these correctly. Investigation revealed a
part 51. products. protruding screw in the rudder pedal
(2) You must use this service information heel rest adjacent to the pedals. It was
as applicable to do the actions required by DATES: This AD is effective August 23,
2017. determined that the screws in the cover
this AD, unless this AD specifies otherwise.
(i) Fokker Service Bulletin SBF100–57– The Director of the Federal Register assembly of the heel rest for both the
027, Revision 2, dated December 11, 2013. approved the incorporation by reference Captain and the First Officer’s rudder
(ii) Fokker Service Bulletin SBF100–57– of a certain publication listed in this AD pedals might not have been properly
028, Revision 2, dated December 11, 2013. as of August 23, 2017. torqued. The NPRM proposed to require
(3) For service information identified in a torque check of the screws in the cover
ADDRESSES: For service information
this AD, contact Fokker Services B.V., assembly of the heel rest for both the
Technical Services Dept., P.O. Box 1357, identified in this final rule, contact
Captain and the First Officer’s rudder
2130 EL Hoofddorp, the Netherlands; Boeing Commercial Airplanes,
pedals, and corrective action if
telephone: +31 (0)88–6280–350; fax: +31 Attention: Data & Services Management,
necessary. We are issuing this AD to
(0)88–6280–111; email: technicalservices@ P.O. Box 3707, MC 2H–65, Seattle, WA
detect and correct a protruding screw in
fokker.com; Internet: http:// 98124–2207; telephone 206–544–5000,
www.myfokkerfleet.com. the cover assembly of the heel rest of a
extension 1; fax 206–766–5680; Internet
(4) You may view this service information rudder pedal. A protruding screw could
https://www.myboeingfleet.com. You
at the FAA, Transport Airplane Directorate, restrict rudder pedal motion and reduce
may view this referenced service
1601 Lind Avenue SW., Renton, WA. For differential braking control during
information on the availability of this
information at the FAA, Transport
takeoff or landing, which could cause a
material at the FAA, call 425–227–1221. Airplane Directorate, 1601 Lind Avenue
high speed runway excursion.
(5) You may view this service information SW., Renton, WA. For information on
that is incorporated by reference at the the availability of this material at the Comments
National Archives and Records FAA, call 425–227–1221. It is also We gave the public the opportunity to
Administration (NARA). For information on available on the Internet at http:// participate in developing this AD. The
the availability of this material at NARA, call www.regulations.gov by searching for
202–741–6030, or go to: http://
following presents the comments
and locating Docket No. FAA–2016– received on the NPRM and the FAA’s
www.archives.gov/federal-register/cfr/ibr- 9506.
locations.html. response to each comment.
Issued in Renton, Washington, on July 3, Examining the AD Docket Support for the NPRM
2017. You may examine the AD docket on Boeing, Air Line Pilots Association,
Dionne Palermo, the Internet at http:// International, and Tyler Myers
Acting Manager, Transport Airplane www.regulations.gov by searching for supported the intent of the NPRM.
Directorate, Aircraft Certification Service. and locating Docket No. FAA–2016–
[FR Doc. 2017–14583 Filed 7–18–17; 8:45 am] 9506; or in person at the Docket Request To Allow Credit for Previously
BILLING CODE 4910–13–P Management Facility between 9 a.m. Accomplished Actions
and 5 p.m., Monday through Friday, United Airlines noted that the NPRM
except Federal holidays. The AD docket did not address whether or not the final
DEPARTMENT OF TRANSPORTATION contains this AD, the regulatory rule would allow operators to take
evaluation, any comments received, and credit for accomplishment of the actions
Federal Aviation Administration other information. The address for the in Boeing Alert Service Bulletin 737–
Docket Office (phone: 800–647–5527) is 25A1732, Revision 1, dated August 15,
14 CFR Part 39 Docket Management Facility, U.S. 2016 (‘‘BASB 737–25A1732, Revision
[Docket No. FAA–2016–9506; Directorate Department of Transportation, Docket 1’’), if completed prior to the effective
Identifier 2016–NM–090–AD; Amendment Operations, M–30, West Building date of the final rule. We infer that the
39–18957; AD 2017–14–13] Ground Floor, Room W12–140, 1200 commenter is requesting that the final
New Jersey Avenue SE., Washington, rule include a statement that
RIN 2120–AA64 DC 20590. accomplishment of the actions specified
Airworthiness Directives; The Boeing FOR FURTHER INFORMATION CONTACT: in BASB 737–25A1732, Revision 1,
Company Airplanes Kelly McGuckin, Aerospace Engineer, prior to the effective date of the final
Systems and Equipment Branch, ANM– rule is acceptable for compliance with
AGENCY: Federal Aviation 130S, FAA, Seattle Aircraft Certification the requirements of the final rule.
Administration (FAA), DOT. Office (ACO), 1601 Lind Avenue SW., We agree with the commenter that
ACTION: Final rule. Renton, WA 98057–3356; phone: 425– operators should be able to take credit
917–6490; fax: 425–917–6590; email: for accomplishment of the actions in
SUMMARY: We are adopting a new Kelly.McGuckin@faa.gov. BASB 737–25A1732, Revision 1, prior
airworthiness directive (AD) for certain SUPPLEMENTARY INFORMATION: to the effective date of this AD. This
The Boeing Company Model 737–600, allowance was provided in paragraph (f)
–700, –700C, –800, –900, and –900ER Discussion of the proposed AD in the statement
mstockstill on DSK30JT082PROD with RULES
series airplanes. This AD was prompted We issued a notice of proposed ‘‘Comply with this AD within the
by a report of an aborted takeoff because rulemaking (NPRM) to amend 14 CFR compliance times specified unless
the rudder pedals were not operating part 39 by adding an AD that would already done.’’ However, since the
correctly. Investigation revealed a apply to certain The Boeing Company NPRM was issued, Boeing has
protruding screw in the rudder pedal Model 737–600, –700, –700C, –800, published, and we have reviewed,
heel rest adjacent to the pedals. This AD –900, and –900ER series airplanes. The Boeing Alert Service Bulletin 737–
requires a torque check of the screws in NPRM published in the Federal 25A1732, Revision 2, dated April 13,
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2017 (‘‘BASB 737–25A1732, Revision accomplishment of the manufacturer’s Related Service Information Under 1
2’’). BASB 737–25A1732, Revision 2, service instructions. CFR Part 51
provides clarification of the actions We agree with the commenter that
described in the work instructions by STC ST00830SE does not affect the We reviewed Boeing Alert Service
providing supplementary details and accomplishment of the manufacturer’s Bulletin 737–25A1732, Revision 2,
including additional descriptive figures. service instructions. Therefore, the dated April 13, 2017. The service
No additional work is necessary and the installation of STC ST00830SE does not information describes procedures for a
scope of this AD is not expanded. affect the ability to accomplish the torque check of the screws in the cover
actions required by this AD. We have assembly of the heel rest for both the
We have revised paragraphs (c), (g), not changed this AD in this regard. Captain and the First Officer’s rudder
and (h) of this AD to refer to BASB 737– pedals, and corrective action. This
25A1732, Revision 2. We have also Conclusion
service information is reasonably
added paragraph (i) to this AD to give We reviewed the relevant data,
available because the interested parties
credit for actions accomplished using considered the comments received, and
have access to it through their normal
the work instructions in BASB 737– determined that air safety and the
public interest require adopting this AD course of business or by the means
25A1732, Revision 1; and redesignated identified in the ADDRESSES section.
the subsequent paragraphs accordingly. as proposed, except for minor editorial
changes. We have determined that these Costs of Compliance
Effect of Winglets on Accomplishment minor changes:
of the Proposed Actions • Are consistent with the intent that We estimate that this AD affects 1,187
was proposed in the NPRM for airplanes of U.S. registry. We estimate
Aviation Partners Boeing stated that correcting the unsafe condition; and the following costs to comply with this
the installation of winglets per • Do not add any additional burden AD:
Supplemental Type Certificate (STC) upon the public than was already
ST00830SE does not affect the proposed in the NPRM.
ESTIMATED COSTS
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
Torque check .................................................. 2 work-hours × $85 per hour = $170 ............. $0 $170 $201,790
We have received no definitive data the relationship between the national Authority: 49 U.S.C. 106(g), 40113, 44701.
that will enable us to provide cost government and the States, or on the
§ 39.13 [Amended]
estimates for the on-condition actions distribution of power and
specified in this AD. responsibilities among the various ■ 2. The FAA amends § 39.13 by adding
levels of government. the following new airworthiness
Authority for This Rulemaking directive (AD):
For the reasons discussed above, I
Title 49 of the United States Code certify that this AD: 2017–14–13 The Boeing Company:
specifies the FAA’s authority to issue (1) Is not a ‘‘significant regulatory Amendment 39–18957; Docket No.
rules on aviation safety. Subtitle I, action’’ under Executive Order 12866, FAA–2016–9506; Directorate Identifier
section 106, describes the authority of (2) Is not a ‘‘significant rule’’ under 2016–NM–090–AD.
the FAA Administrator. Subtitle VII: DOT Regulatory Policies and Procedures (a) Effective Date
Aviation Programs, describes in more (44 FR 11034, February 26, 1979), This AD is effective August 23, 2017.
detail the scope of the Agency’s (3) Will not affect intrastate aviation
authority. in Alaska, and (b) Affected ADs
We are issuing this rulemaking under (4) Will not have a significant None.
the authority described in Subtitle VII, economic impact, positive or negative, (c) Applicability
Part A, Subpart III, Section 44701: on a substantial number of small entities
under the criteria of the Regulatory This AD applies to The Boeing Company
‘‘General requirements.’’ Under that Model 737–600, –700, –700C, –800, –900,
section, Congress charges the FAA with Flexibility Act. and –900ER series airplanes, certificated in
promoting safe flight of civil aircraft in List of Subjects in 14 CFR Part 39 any category, as identified in Boeing Alert
air commerce by prescribing regulations Service Bulletin 737–25A1732, Revision 2,
for practices, methods, and procedures Air transportation, Aircraft, Aviation dated April 13, 2017.
the Administrator finds necessary for safety, Incorporation by reference,
(d) Subject
safety in air commerce. This regulation Safety.
Air Transport Association (ATA) of
is within the scope of that authority Adoption of the Amendment America Code 25, Equipment and
because it addresses an unsafe condition Furnishings.
Accordingly, under the authority
that is likely to exist or develop on
delegated to me by the Administrator, (e) Unsafe Condition
products identified in this rulemaking
the FAA amends 14 CFR part 39 as This AD was prompted by a report of an
mstockstill on DSK30JT082PROD with RULES
action.
follows: aborted takeoff because the rudder pedals
Regulatory Findings were not operating correctly. Investigation
PART 39—AIRWORTHINESS revealed a protruding screw in the rudder
This AD will not have federalism DIRECTIVES pedal heel rest adjacent to the pedals. It was
implications under Executive Order determined that the screws in the cover
13132. This AD will not have a ■ 1. The authority citation for part 39 assembly of the heel rest for both the Captain
substantial direct effect on the States, on continues to read as follows: and the First Officer’s rudder pedals might
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not have been properly torqued. We are (4) For service information that contains DEPARTMENT OF THE TREASURY
issuing this AD to detect and correct a steps that are labeled as Required for
protruding screw in the cover assembly of the Compliance (RC), the provisions of Internal Revenue Service
heel rest of a rudder pedal. A protruding paragraphs (j)(4)(i) and (j)(4)(ii) of this AD
screw could restrict rudder pedal motion and apply.
(i) The steps labeled as RC, including
26 CFR Part 300
reduce differential braking control during
takeoff or landing, which could cause a high substeps under an RC step and any figures [TD 9820]
speed runway excursion. identified in an RC step, must be done to
comply with the AD. If a step or sub-step is RIN 1545–BN09
(f) Compliance labeled ‘‘RC Exempt,’’ then the RC
Comply with this AD within the requirement is removed from that step or Special Enrollment Examination User
compliance times specified, unless already sub-step. An AMOC is required for any Fee for Enrolled Agents
done. deviations to RC steps, including substeps
and identified figures. AGENCY: Internal Revenue Service (IRS),
(g) Torque Check (ii) Steps not labeled as RC may be Treasury.
Within 21 months after the effective date deviated from using accepted methods in ACTION: Final regulation.
of this AD: Do a one-time torque check of the accordance with the operator’s maintenance
screws in the cover assembly of the heel rest or inspection program without obtaining SUMMARY: This document contains a
for both the Captain and the First Officer’s approval of an AMOC, provided the RC steps, final regulation changing the amount of
rudder pedals, in accordance with the including substeps and identified figures, can the user fee for the special enrollment
Accomplishment Instructions of Boeing Alert still be done as specified, and the airplane examination to become an enrolled
Service Bulletin 737–25A1732, Revision 2, can be put back in an airworthy condition. agent. The charging of user fees is
dated April 13, 2017. (k) Related Information authorized by the Independent Offices
(h) Corrective Action (1) For more information about this AD, Appropriations Act of 1952. The final
If the results of the torque check required contact Kelly McGuckin, Aerospace regulation affects individuals taking the
by paragraph (g) of this AD indicate that any Engineer, Systems and Equipment Branch, enrolled agent special enrollment
screw does not hold torque to the required ANM–130S, FAA, Seattle ACO, 1601 Lind examination.
value, before further flight, replace the Avenue SW., Renton, WA 98057–3356;
phone: 425–917–6490; fax: 425–917–6590; DATES:
affected screw and associated nutplate, in Effective date: This regulation is
accordance with the Accomplishment email: Kelly.McGuckin@faa.gov.
(2) Service information identified in this effective August 18, 2017.
Instructions of Boeing Alert Service Bulletin
AD that is not incorporated by reference is Applicability date: For the date of
737–25A1732, Revision 2, dated April 13,
2017.
available at the addresses specified in applicability, see § 300.4(d).
paragraphs (l)(3) and (l)(4) of this AD. FOR FURTHER INFORMATION CONTACT:
(i) Credit for Actions Accomplished Jonathan R. Black, (202) 317–6845 (not
(l) Material Incorporated by Reference
Previously
(1) The Director of the Federal Register a toll-free number).
This paragraph provides credit for the
approved the incorporation by reference SUPPLEMENTARY INFORMATION:
actions specified in paragraphs (g) and (h) of
(IBR) of the service information listed in this
this AD, if those actions were performed Background and Explanation of
paragraph under 5 U.S.C. 552(a) and 1 CFR
before the effective date of this AD using Provisions
part 51.
Boeing Alert Service Bulletin 737–25A1732,
(2) You must use this service information This document contains amendments
Revision 1, dated August 15, 2016.
as applicable to do the actions required by to 26 CFR part 300 regarding user fees.
(j) Alternative Methods of Compliance this AD, unless the AD specifies otherwise. On January 26, 2016, a notice of
(AMOCs) (i) Boeing Alert Service Bulletin 737–
25A1732, Revision 2, dated April 13, 2017.
proposed rulemaking (REG–134122–15)
(1) The Manager, Seattle Aircraft proposing to change the amount of the
Certification Office (ACO), FAA, has the (ii) Reserved.
(3) For service information identified in Enrolled Agent Special Enrollment
authority to approve AMOCs for this AD, if
requested using the procedures found in 14 this AD, contact Boeing Commercial Examination (EA–SEE) user fee was
CFR 39.19. In accordance with 14 CFR 39.19, Airplanes, Attention: Data & Services published in the Federal Register (81
send your request to your principal inspector Management, P. O. Box 3707, MC 2H–65, FR 4221) (January 26, 2016 proposed
or local Flight Standards District Office, as Seattle, WA 98124–2207; telephone 206– rule). On October 25, 2016, a second
appropriate. If sending information directly 544–5000, extension 1; fax 206–766–5680; notice of proposed rulemaking (REG–
to the manager of the ACO, send it to the Internet https://www.myboeingfleet.com. 134122–15) withdrawing the January 26,
attention of the person identified in (4) You may view this service information
at the FAA, Transport Airplane Directorate,
2016 proposed rule and proposing a
paragraph (k)(1) of this AD. Information may smaller change to the EA–SEE user fee
be emailed to: 9-ANM-Seattle-ACO-AMOC- 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this was published in the Federal Register
Requests@faa.gov.
(2) Before using any approved AMOC, material at the FAA, call 425–227–1221. (81 FR 73363) (October 25, 2016
notify your appropriate principal inspector, (5) You may view this service information proposed rule). Comments responding
or lacking a principal inspector, the manager that is incorporated by reference at the to each proposed rule were received,
of the local flight standards district office/ National Archives and Records and a public hearing on the second
certificate holding district office. Administration (NARA). For information on proposed rule was held on December
(3) An AMOC that provides an acceptable the availability of this material at NARA, call 29, 2016. After consideration of the
level of safety may be used for any repair, 202–741–6030, or go to: http://
www.archives.gov/federal-register/cfr/ibr-
comments, this Treasury decision
modification, or alteration required by this adopts the regulations proposed by the
AD if it is approved by the Boeing locations.html.
October 25, 2016 proposed rule without
Commercial Airplanes Organization
mstockstill on DSK30JT082PROD with RULES
Issued in Renton, Washington, on June 29, change.
Designation Authorization (ODA) that has 2017.
been authorized by the Manager, Seattle Michael Kaszycki, A. Enrolled Agents and the Special
ACO, to make those findings. To be Enrollment Examination
Acting Manager, Transport Airplane
approved, the repair method, modification
Directorate, Aircraft Certification Service. Section 330 of title 31 of the United
deviation, or alteration deviation must meet
the certification basis of the airplane, and the [FR Doc. 2017–14584 Filed 7–18–17; 8:45 am] States Code authorizes the Secretary of
approval must specifically refer to this AD. BILLING CODE 4910–13–P the Treasury to regulate the practice of
VerDate Sep<11>2014 16:17 Jul 18, 2017 Jkt 241001 PO 00000 Frm 00023 Fmt 4700 Sfmt 4700 E:\FR\FM\19JYR1.SGM 19JYR1](https://thefederalregister.org/doc/82_FR_33144/page/3.svg)
Document Created: 2017-07-19 06:17:42
Document Modified: 2017-07-19 06:17:42
| 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 August 23, 2017. | |
| Contact | Kelly McGuckin, Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057- 3356; phone: 425-917-6490; fax: 425-917-6590; email: [email protected] | |
| FR Citation | 82 FR 33007 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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