83 FR 44204 - Airworthiness Directives; The Boeing Company Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 83, Issue 169 (August 30, 2018)

Page Range		44204-44207
FR Document		2018-18664
We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 727 airplanes. This AD was prompted by significant changes made to the airworthiness limitations (AWLs) related to fuel tank ignition prevention. This AD requires revising the maintenance or inspection program, as applicable, to incorporate the latest revision of the AWLs. We are issuing this AD to address the unsafe condition on these products.
Federal Register, Volume 83 Issue 169 (Thursday, August 30, 2018)
[Federal Register Volume 83, Number 169 (Thursday, August 30, 2018)]
[Rules and Regulations]
[Pages 44204-44207]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2018-18664]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0031; Product Identifier 2017-NM-127-AD; Amendment 
39-19374; AD 2018-17-20]
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 727 airplanes. This AD was prompted by 
significant changes made to the airworthiness limitations (AWLs) 
related to fuel tank ignition prevention. This AD requires revising the 
maintenance or inspection program, as applicable, to incorporate the 
latest revision of the AWLs. We are issuing this AD to address the 
unsafe condition on these products.

[[Page 44205]]


DATES: This AD is effective October 4, 2018.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of October 4, 
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-2018-
0031.

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-2018-
0031; 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: Christopher Baker, Aerospace Engineer, 
Propulsion Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des 
Moines, WA 98198; phone and fax: 206-231-3552; 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 727 airplanes. The NPRM published in the Federal Register on 
February 8, 2018 (83 FR 5576). The NPRM was prompted by significant 
changes made to the AWLs related to fuel tank ignition prevention. The 
NPRM proposed to require revising the maintenance or inspection 
program, as applicable, to incorporate the latest revision of the AWLs.
    We are issuing this AD to address the potential for ignition 
sources inside fuel tanks caused by latent failures, alterations, 
repairs, or maintenance actions, which, in combination with flammable 
fuel vapors, could result in fuel tank explosions and consequent loss 
of the airplane.

Comments

    We gave the public the opportunity to participate in developing 
this final rule. We have considered the comment received. Boeing 
supported the NPRM.

Clarification of Affected Airplanes in Paragraph (g)(4)(ii) of This AD

    The phrase ``as of the effective date of this AD'' was 
inadvertently not included in the description of affected airplanes in 
paragraph (g)(4)(ii) of the proposed AD. We have revised paragraph 
(g)(4)(ii) of this AD accordingly.

Clarification of Alternative Wire Types and Sleeving

    Paragraph (h) of this AD allows operators to revise AWL No. 28-AWL-
03 to identify certain alternative wire types and sleeving materials. 
AWL No. 28-AWL-03 was originally mandated by AD 2008-04-10 R1, 
Amendment 39-16121 (74 FR 66227, December 15, 2009) (``AD 2008-04-10 
R1''). Since the issuance of AD 2008-04-10 R1, which will be terminated 
by this AD, we received numerous requests for approval of alternative 
methods of compliance (AMOCs) from operators and supplemental type 
certificate (STC) holders (or applicants) to allow the installation of 
the alternative wire types and sleeving identified in paragraphs (h)(1) 
and (h)(2) of this AD. We evaluated certain attributes of those 
alternative wire types and sleeving for each installation, and issued 
numerous AMOC approvals based on our determination that the 
installation of those wire types and sleeving would provide an 
acceptable level of safety. Although paragraph (h) of this AD provides 
certain allowances, it does not provide approval of alternative wire 
types and sleeving that are installed as part of an aircraft design 
change. Each applicant for any design change is still responsible to 
show that the installation of alternative wire types and sleeving 
identified in paragraphs (h)(l) and (h)(2) of this AD complies with all 
applicable regulatory requirements. This responsibility includes, but 
is not limited to, substantiation of compliance with flammability 
requirements, and substantiation to show that sleeve installation, 
including the selection of sleeve thickness, is adequate to protect 
wires from chafing for the life of installation. If such an 
installation is found to be compliant with all applicable regulatory 
requirements, revision of AWL No. 28-AWL-03 in accordance with 
paragraph (h) of this AD would allow the installation of the 
alternative wire types and sleeving.

Conclusion

    We reviewed the relevant data, considered the comment received, and 
determined that air safety and the public interest require adopting 
this final rule with the change described previously and 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.
    We also determined that these changes will not increase the 
economic burden on any operator or increase the scope of this final 
rule.

Related Service Information Under 1 CFR Part 51

    We reviewed Boeing 727-100/200 Airworthiness Limitations (AWLs) D6-
8766-AWL, Revision December 2016. This service information describes 
AWL tasks that include airworthiness limitation instructions (ALIs) and 
critical design configuration control limitations (CDCCLs) related to 
fuel tank ignition prevention. 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 20 airplanes of U.S. registry. We 
estimate the following costs to comply with this AD:
    We have determined that revising the maintenance or inspection 
program takes an average of 90 work-hours per operator, although we 
recognize that this number may vary from operator to operator. In the 
past, we have estimated that this action takes 1 work-hour per 
airplane. Since operators incorporate maintenance or inspection program 
changes for their affected fleet(s), we have determined that a per-
operator estimate is more accurate than a per-airplane estimate. 
Therefore, we estimate the total cost per operator to be $7,650 (90 
work-hours x $85 per work-hour).

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue

[[Page 44206]]

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):

2018-17-20 The Boeing Company: Amendment 39-19374; Docket No. FAA-
2018-0031; Product Identifier 2017-NM-127-AD.

(a) Effective Date

    This AD is effective October 4, 2018.

(b) Affected ADs

    This AD affects the ADs specified in paragraphs (b)(1) through 
(b)(5) of this AD.
    (1) AD 2008-04-10 R1, Amendment 39-16121 (74 FR 66227, December 
15, 2009) (``AD 2008-04-10 R1'').
    (2) AD 2009-05-03, Amendment 39-15827 (74 FR 8851, February 27, 
2009) (``AD 2009-05-03'').
    (3) AD 2011-12-05, Amendment 39-16712 (76 FR 33991, June 10, 
2011) (``AD 2011-12-05'').
    (4) AD 2013-22-03, Amendment 39-17635 (78 FR 65193, October 31, 
2013) (``AD 2013-22-03'').
    (5) AD 2013-24-15, Amendment 39-17692 (78 FR 72791, December 4, 
2013) (``AD 2013-24-15'').

(c) Applicability

    This AD applies to The Boeing Company Model 727, 727C, 727-100, 
727-100C, 727-200, and 727-200F series airplanes, certificated in 
any category, with an original certificate of airworthiness or 
original export certificate of airworthiness issued on or before the 
effective date of this AD.

(d) Subject

    Air Transport Association (ATA) of America Code 28, Fuel.

(e) Unsafe Condition

    This AD was prompted by significant changes made to the 
airworthiness limitations (AWLs) related to fuel tank ignition 
prevention. We are issuing this AD to prevent the potential for 
ignition sources inside fuel tanks caused by latent failures, 
alterations, repairs, or maintenance actions, which, in combination 
with flammable fuel vapors, could result in fuel tank explosions and 
consequent loss of the airplane.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Maintenance or Inspection Program Revision

    Within 60 days after the effective date of this AD, revise the 
maintenance or inspection program, as applicable, to incorporate all 
information in Section A, including Subsections A.1 and A.2, of 
Boeing 727-100/200 Airworthiness Limitations (AWLs) D6-8766-AWL, 
Revision December 2016. The initial compliance times for the 
airworthiness limitation instruction (ALI) items are within the 
applicable compliance times specified in paragraphs (g)(1) through 
(g)(6) of this AD.
    (1) For AWL No. 28-AWL-01, ``External Wires Over Center Fuel 
Tank (Tank No. 2)'': At the applicable time specified in paragraph 
(g)(1)(i) or (g)(1)(ii) of this AD.
    (i) For airplanes that have been previously inspected as 
specified in 28-AWL-01 as of the effective date of this AD: Conduct 
the inspection within 120 months after the most recent inspection.
    (ii) For airplanes that have not been inspected as specified in 
28-AWL-01 as of the effective date of this AD: Conduct the 
inspection within 12 months after the effective date of this AD.
    (2) For AWL No. 28-AWL-16, ``Over-Current and Arcing Protection 
Electrical Design Features Operation--Boost Pump Ground Fault 
Interrupter (GFI)'': At the applicable time specified in paragraph 
(g)(2)(i) or (g)(2)(ii) of this AD.
    (i) For airplanes that have been previously inspected as 
specified in 28-AWL-16 as of the effective date of this AD: Conduct 
the inspection within 12 months after the most recent inspection.
    (ii) For airplanes that have not been inspected as specified in 
28-AWL-16 as of the effective date of this AD: Conduct the 
inspection within 90 days after the effective date of this AD.
    (3) For AWL No. 28-AWL-17, ``Auxiliary Tank Fuel Boost Pump 
Power Failed On Protection System'': At the applicable time 
specified in paragraph (g)(3)(i) or (g)(3)(ii) of this AD.
    (i) For airplanes that have been previously inspected as 
specified in 28-AWL-17 as of the effective date of this AD: Conduct 
the inspection within 12 months after the most recent inspection.
    (ii) For airplanes that have not been inspected as specified in 
28-AWL-17 as of the effective date of this AD: Conduct the 
inspection within 90 days after the effective date of this AD.
    (4) For AWL No. 28-AWL-18, ``Fuel Quantity Indicating System 
(FQIS)--Out-Tank Wiring Lightning Shield to Ground Termination and 
Joint Resistance for the Volumetric Top-Off (VTO) Unit (If 
Installed)'': At the applicable time specified in paragraph 
(g)(4)(i) or (g)(4)(ii) of this AD.
    (i) For airplanes that have been previously inspected as 
specified in 28-AWL-18 as of the effective date of this AD: Conduct 
the inspection within 120 months after the most recent inspection.
    (ii) For airplanes that have not been inspected as specified in 
28-AWL-18 as of the effective date of this AD: Conduct the 
inspection within 12 months after the effective date of this AD.
    (5) For AWL No. 28-AWL-22, ``AC Fuel Boost Pump Bonding 
Installation'': At the applicable time specified in paragraph 
(g)(5)(i) or (g)(5)(ii) of this AD.
    (i) For airplanes that have been previously inspected as 
specified in 28-AWL-22 as of

[[Page 44207]]

the effective date of this AD: Conduct the inspection within 72 
months after the most recent inspection.
    (ii) For airplanes that have not been inspected as specified in 
28-AWL-22 as of the effective date of this AD: Conduct the 
inspection within 12 months after the effective date of this AD.
    (6) For AWL No. 28-AWL-24, ``Motor Operated Valve Bonding Jumper 
Installation--Fault Current Protection'': At the applicable time 
specified in paragraph (g)(6)(i) or (g)(6)(ii) of this AD.
    (i) For airplanes that have been previously inspected as 
specified in 28-AWL-24 as of the effective date of this AD: Conduct 
the inspection within 60 months after the most recent inspection.
    (ii) For airplanes that have not been inspected as specified in 
28-AWL-24 as of the effective date of this AD: Conduct the 
inspection within 12 months after the effective date of this AD.

(h) Additional Acceptable Wire Types and Sleeving

    As an option, when accomplishing the actions required by 
paragraph (g) of this AD, the changes specified in paragraphs (h)(1) 
and (h)(2) of this AD can be made to AWL No. 28-AWL-03.
    (1) Where AWL No. 28-AWL-03 identifies wire types BMS 13-48, BMS 
13-58, and BMS 13-60, add the following acceptable wire types: MIL-
W-22759/16, SAE AS22759/16 (M22759/16), MIL-W-22759/32, SAE AS22759/
32 (M22759/32), MIL-W-22759/34, SAE AS22759/34 (M22759/34), MIL-W-
22759/41, SAE AS22759/41 (M22759/41), MIL-W-22759/86, SAE AS22759/86 
(M22759/86), MIL-W-22759/87, SAE AS22759/87 (M22759/87), MIL-W-
22759/92 and SAE AS22759/92 (M22759/92); and MIL-C-27500 and NEMA WC 
27500 cables constructed from these military or SAE specification 
wire types identified above.
    (2) Where AWL No. 28-AWL-03 identifies TFE-2X Standard wall for 
wire sleeving, add the following acceptable sleeving materials: 
Roundit 2000NX and Varglas Type HO, HP, or HM.

(i) No Alternative Actions, Intervals, and Critical Design 
Configuration Control Limitations (CDCCLs)

    After the maintenance or inspection program, as applicable, has 
been revised as required by paragraph (g) of this AD, no alternative 
actions (e.g., inspections), intervals, and CDCCLs may be used 
unless the actions, intervals, and CDCCLs are approved as an 
alternative method of compliance (AMOC), in accordance with the 
procedures specified in paragraph (k) of this AD.

(j) Terminating Actions

    Accomplishment of the maintenance or inspection program revision 
required by paragraph (g) of this AD terminates the actions 
specified in paragraphs (j)(1) through (j)(5) of this AD.
    (1) The revision required by paragraph (g) of AD 2008-04-10 R1.
    (2) The revision required by paragraph (h) of AD 2009-05-03.
    (3) The revision required by paragraph (j) of AD 2011-12-05.
    (4) The revision required by paragraph (h) of AD 2013-22-03.
    (5) The revision required by paragraphs (n)(1) and (n)(2) of AD 
2013-24-15.

(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, FAA, 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

    For more information about this AD, contact Christopher Baker, 
Aerospace Engineer, Propulsion Section, FAA, Seattle ACO Branch, 
2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-
3552; email: [email protected].

(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 727-100/200 Airworthiness Limitations (AWLs) D6-8766-
AWL, Revision December 2016.
    (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 August 17, 2018.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2018-18664 Filed 8-29-18; 8:45 am]
 BILLING CODE 4910-13-P
Federal Register / Vol. 83, No. 169 / Thursday, August 30, 2018 / Rules and Regulations 44205

DATES: This AD is effective October 4, tanks caused by latent failures, found to be compliant with all
2018. alterations, repairs, or maintenance applicable regulatory requirements,
The Director of the Federal Register actions, which, in combination with revision of AWL No. 28–AWL–03 in
approved the incorporation by reference flammable fuel vapors, could result in accordance with paragraph (h) of this
of a certain publication listed in this AD fuel tank explosions and consequent AD would allow the installation of the
as of October 4, 2018. loss of the airplane. alternative wire types and sleeving.
ADDRESSES: For service information Comments Conclusion
identified in this final rule, contact
Boeing Commercial Airplanes, We gave the public the opportunity to We reviewed the relevant data,
Attention: Contractual & Data Services participate in developing this final rule. considered the comment received, and
(C&DS), 2600 Westminster Blvd., MC We have considered the comment determined that air safety and the
110–SK57, Seal Beach, CA 90740–5600; received. Boeing supported the NPRM. public interest require adopting this
telephone 562–797–1717; internet Clarification of Affected Airplanes in final rule with the change described
https://www.myboeingfleet.com. You Paragraph (g)(4)(ii) of This AD previously and minor editorial changes.
may view this service information at the We have determined that these minor
The phrase ‘‘as of the effective date of changes:
FAA, Transport Standards Branch, 2200 this AD’’ was inadvertently not
South 216th St., Des Moines, WA. For • Are consistent with the intent that
included in the description of affected was proposed in the NPRM for
information on the availability of this airplanes in paragraph (g)(4)(ii) of the
material at the FAA, call 206–231–3195. addressing the unsafe condition; and
proposed AD. We have revised • Do not add any additional burden
It is also available on the internet at paragraph (g)(4)(ii) of this AD
http://www.regulations.gov by searching upon the public than was already
accordingly. proposed in the NPRM.
for and locating Docket No. FAA–2018–
0031. Clarification of Alternative Wire Types We also determined that these
and Sleeving changes will not increase the economic
Examining the AD Docket burden on any operator or increase the
Paragraph (h) of this AD allows
You may examine the AD docket on scope of this final rule.
operators to revise AWL No. 28–AWL–
the internet at http:// 03 to identify certain alternative wire Related Service Information Under 1
www.regulations.gov by searching for types and sleeving materials. AWL No. CFR Part 51
and locating Docket No. FAA–2018– 28–AWL–03 was originally mandated
0031; or in person at Docket Operations We reviewed Boeing 727–100/200
by AD 2008–04–10 R1, Amendment 39– Airworthiness Limitations (AWLs) D6–
between 9 a.m. and 5 p.m., Monday 16121 (74 FR 66227, December 15,
through Friday, except Federal holidays. 8766–AWL, Revision December 2016.
2009) (‘‘AD 2008–04–10 R1’’). Since the This service information describes AWL
The AD docket contains this final rule, issuance of AD 2008–04–10 R1, which
the regulatory evaluation, any tasks that include airworthiness
will be terminated by this AD, we limitation instructions (ALIs) and
comments received, and other received numerous requests for
information. The address for Docket critical design configuration control
approval of alternative methods of limitations (CDCCLs) related to fuel tank
Operations (phone: 800–647–5527) is compliance (AMOCs) from operators
Docket Operations, U.S. Department of ignition prevention. This service
and supplemental type certificate (STC) information is reasonably available
Transportation, Docket Operations, holders (or applicants) to allow the
M–30, West Building Ground Floor, because the interested parties have
installation of the alternative wire types access to it through their normal course
Room W12–140, 1200 New Jersey and sleeving identified in paragraphs
Avenue SE, Washington, DC 20590. of business or by the means identified
(h)(1) and (h)(2) of this AD. We in the ADDRESSES section.
FOR FURTHER INFORMATION CONTACT: evaluated certain attributes of those
Christopher Baker, Aerospace Engineer, alternative wire types and sleeving for Costs of Compliance
Propulsion Section, FAA, Seattle ACO each installation, and issued numerous We estimate that this AD affects 20
Branch, 2200 South 216th St., Des AMOC approvals based on our airplanes of U.S. registry. We estimate
Moines, WA 98198; phone and fax: 206– determination that the installation of the following costs to comply with this
231–3552; email: christopher.r.baker@ those wire types and sleeving would AD:
faa.gov. provide an acceptable level of safety. We have determined that revising the
SUPPLEMENTARY INFORMATION: Although paragraph (h) of this AD maintenance or inspection program
provides certain allowances, it does not takes an average of 90 work-hours per
Discussion provide approval of alternative wire operator, although we recognize that
We issued a notice of proposed types and sleeving that are installed as this number may vary from operator to
rulemaking (NPRM) to amend 14 CFR part of an aircraft design change. Each operator. In the past, we have estimated
part 39 by adding an AD that would applicant for any design change is still that this action takes 1 work-hour per
apply to certain The Boeing Company responsible to show that the installation airplane. Since operators incorporate
Model 727 airplanes. The NPRM of alternative wire types and sleeving maintenance or inspection program
published in the Federal Register on identified in paragraphs (h)(l) and (h)(2) changes for their affected fleet(s), we
February 8, 2018 (83 FR 5576). The of this AD complies with all applicable have determined that a per-operator
NPRM was prompted by significant regulatory requirements. This estimate is more accurate than a per-
changes made to the AWLs related to responsibility includes, but is not airplane estimate. Therefore, we
fuel tank ignition prevention. The limited to, substantiation of compliance estimate the total cost per operator to be
amozie on DSK3GDR082PROD with RULES

NPRM proposed to require revising the with flammability requirements, and $7,650 (90 work-hours × $85 per work-
maintenance or inspection program, as substantiation to show that sleeve hour).
applicable, to incorporate the latest installation, including the selection of
revision of the AWLs. sleeve thickness, is adequate to protect Authority for This Rulemaking
We are issuing this AD to address the wires from chafing for the life of Title 49 of the United States Code
potential for ignition sources inside fuel installation. If such an installation is specifies the FAA’s authority to issue

VerDate Sep<11>2014 16:35 Aug 29, 2018 Jkt 244001 PO 00000 Frm 00033 Fmt 4700 Sfmt 4700 E:\FR\FM\30AUR1.SGM 30AUR1
44206 Federal Register / Vol. 83, No. 169 / Thursday, August 30, 2018 / Rules and Regulations

rules on aviation safety. Subtitle I, the FAA amends 14 CFR part 39 as program, as applicable, to incorporate all
section 106, describes the authority of follows: information in Section A, including
the FAA Administrator. Subtitle VII: Subsections A.1 and A.2, of Boeing 727–100/
PART 39—AIRWORTHINESS 200 Airworthiness Limitations (AWLs) D6–
Aviation Programs, describes in more 8766–AWL, Revision December 2016. The
detail the scope of the Agency’s DIRECTIVES
initial compliance times for the airworthiness
authority. limitation instruction (ALI) items are within
We are issuing this rulemaking under ■ 1. The authority citation for part 39
the applicable compliance times specified in
the authority described in Subtitle VII, continues to read as follows: paragraphs (g)(1) through (g)(6) of this AD.
Part A, Subpart III, Section 44701: Authority: 49 U.S.C. 106(g), 40113, 44701. (1) For AWL No. 28–AWL–01, ‘‘External
‘‘General requirements.’’ Under that Wires Over Center Fuel Tank (Tank No. 2)’’:
§ 39.13 [Amended] At the applicable time specified in paragraph
section, Congress charges the FAA with
■ 2. The FAA amends § 39.13 by adding (g)(1)(i) or (g)(1)(ii) of this AD.
promoting safe flight of civil aircraft in (i) For airplanes that have been previously
air commerce by prescribing regulations the following new airworthiness
inspected as specified in 28–AWL–01 as of
for practices, methods, and procedures directive (AD): the effective date of this AD: Conduct the
the Administrator finds necessary for 2018–17–20 The Boeing Company: inspection within 120 months after the most
safety in air commerce. This regulation Amendment 39–19374; Docket No. recent inspection.
is within the scope of that authority FAA–2018–0031; Product Identifier (ii) For airplanes that have not been
because it addresses an unsafe condition 2017–NM–127–AD. inspected as specified in 28–AWL–01 as of
the effective date of this AD: Conduct the
that is likely to exist or develop on (a) Effective Date inspection within 12 months after the
products identified in this rulemaking This AD is effective October 4, 2018. effective date of this AD.
action. (2) For AWL No. 28–AWL–16, ‘‘Over-
This AD is issued in accordance with (b) Affected ADs Current and Arcing Protection Electrical
authority delegated by the Executive This AD affects the ADs specified in Design Features Operation—Boost Pump
Director, Aircraft Certification Service, paragraphs (b)(1) through (b)(5) of this AD. Ground Fault Interrupter (GFI)’’: At the
as authorized by FAA Order 8000.51C. (1) AD 2008–04–10 R1, Amendment 39– applicable time specified in paragraph
16121 (74 FR 66227, December 15, 2009) (g)(2)(i) or (g)(2)(ii) of this AD.
In accordance with that order, issuance
(‘‘AD 2008–04–10 R1’’). (i) For airplanes that have been previously
of ADs is normally a function of the (2) AD 2009–05–03, Amendment 39–15827 inspected as specified in 28–AWL–16 as of
Compliance and Airworthiness (74 FR 8851, February 27, 2009) (‘‘AD 2009– the effective date of this AD: Conduct the
Division, but during this transition 05–03’’). inspection within 12 months after the most
period, the Executive Director has (3) AD 2011–12–05, Amendment 39–16712 recent inspection.
delegated the authority to issue ADs (76 FR 33991, June 10, 2011) (‘‘AD 2011–12– (ii) For airplanes that have not been
applicable to transport category 05’’). inspected as specified in 28–AWL–16 as of
airplanes and associated appliances to (4) AD 2013–22–03, Amendment 39–17635 the effective date of this AD: Conduct the
(78 FR 65193, October 31, 2013) (‘‘AD 2013– inspection within 90 days after the effective
the Director of the System Oversight
22–03’’). date of this AD.
Division. (3) For AWL No. 28–AWL–17, ‘‘Auxiliary
(5) AD 2013–24–15, Amendment 39–17692
Regulatory Findings (78 FR 72791, December 4, 2013) (‘‘AD 2013– Tank Fuel Boost Pump Power Failed On
24–15’’). Protection System’’: At the applicable time
This AD will not have federalism specified in paragraph (g)(3)(i) or (g)(3)(ii) of
implications under Executive Order (c) Applicability this AD.
13132. This AD will not have a This AD applies to The Boeing Company (i) For airplanes that have been previously
substantial direct effect on the States, on Model 727, 727C, 727–100, 727–100C, 727– inspected as specified in 28–AWL–17 as of
the relationship between the national 200, and 727–200F series airplanes, the effective date of this AD: Conduct the
government and the States, or on the certificated in any category, with an original inspection within 12 months after the most
certificate of airworthiness or original export recent inspection.
distribution of power and (ii) For airplanes that have not been
certificate of airworthiness issued on or
responsibilities among the various before the effective date of this AD. inspected as specified in 28–AWL–17 as of
levels of government. the effective date of this AD: Conduct the
For the reasons discussed above, I (d) Subject inspection within 90 days after the effective
certify that this AD: Air Transport Association (ATA) of date of this AD.
(1) Is not a ‘‘significant regulatory America Code 28, Fuel. (4) For AWL No. 28–AWL–18, ‘‘Fuel
action’’ under Executive Order 12866, Quantity Indicating System (FQIS)—Out-
(e) Unsafe Condition Tank Wiring Lightning Shield to Ground
(2) Is not a ‘‘significant rule’’ under
DOT Regulatory Policies and Procedures This AD was prompted by significant Termination and Joint Resistance for the
changes made to the airworthiness Volumetric Top-Off (VTO) Unit (If
(44 FR 11034, February 26, 1979),
limitations (AWLs) related to fuel tank Installed)’’: At the applicable time specified
(3) Will not affect intrastate aviation ignition prevention. We are issuing this AD in paragraph (g)(4)(i) or (g)(4)(ii) of this AD.
in Alaska, and to prevent the potential for ignition sources (i) For airplanes that have been previously
(4) Will not have a significant inside fuel tanks caused by latent failures, inspected as specified in 28–AWL–18 as of
economic impact, positive or negative, alterations, repairs, or maintenance actions, the effective date of this AD: Conduct the
on a substantial number of small entities which, in combination with flammable fuel inspection within 120 months after the most
under the criteria of the Regulatory vapors, could result in fuel tank explosions recent inspection.
Flexibility Act. and consequent loss of the airplane. (ii) For airplanes that have not been
inspected as specified in 28–AWL–18 as of
List of Subjects in 14 CFR Part 39 (f) Compliance the effective date of this AD: Conduct the
Air transportation, Aircraft, Aviation Comply with this AD within the inspection within 12 months after the
amozie on DSK3GDR082PROD with RULES

compliance times specified, unless already effective date of this AD.
safety, Incorporation by reference, done. (5) For AWL No. 28–AWL–22, ‘‘AC Fuel
Safety. Boost Pump Bonding Installation’’: At the
(g) Maintenance or Inspection Program applicable time specified in paragraph
Adoption of the Amendment Revision (g)(5)(i) or (g)(5)(ii) of this AD.
Accordingly, under the authority Within 60 days after the effective date of (i) For airplanes that have been previously
delegated to me by the Administrator, this AD, revise the maintenance or inspection inspected as specified in 28–AWL–22 as of

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Federal Register / Vol. 83, No. 169 / Thursday, August 30, 2018 / Rules and Regulations 44207

the effective date of this AD: Conduct the (3) The revision required by paragraph (j) 202–741–6030, or go to: http://
inspection within 72 months after the most of AD 2011–12–05. www.archives.gov/federal-register/cfr/ibr-
recent inspection. (4) The revision required by paragraph (h) locations.html.
(ii) For airplanes that have not been of AD 2013–22–03.
Issued in Des Moines, Washington, on
inspected as specified in 28–AWL–22 as of (5) The revision required by paragraphs
August 17, 2018.
the effective date of this AD: Conduct the (n)(1) and (n)(2) of AD 2013–24–15.
inspection within 12 months after the Michael Kaszycki,
(k) Alternative Methods of Compliance Acting Director, System Oversight Division,
effective date of this AD. (AMOCs)
(6) For AWL No. 28–AWL–24, ‘‘Motor Aircraft Certification Service.
Operated Valve Bonding Jumper (1) The Manager, Seattle ACO Branch, [FR Doc. 2018–18664 Filed 8–29–18; 8:45 am]
Installation—Fault Current Protection’’: At FAA, has the authority to approve AMOCs
BILLING CODE 4910–13–P
the applicable time specified in paragraph for this AD, if requested using the procedures
(g)(6)(i) or (g)(6)(ii) of this AD. found in 14 CFR 39.19. In accordance with
(i) For airplanes that have been previously 14 CFR 39.19, send your request to your
principal inspector or local Flight Standards DEPARTMENT OF TRANSPORTATION
inspected as specified in 28–AWL–24 as of
District Office, as appropriate. If sending
the effective date of this AD: Conduct the Federal Aviation Administration
information directly to the manager of the
inspection within 60 months after the most
certification office, send it to the attention of
recent inspection.
the person identified in paragraph (l) of this 14 CFR Part 39
(ii) For airplanes that have not been
AD. Information may be emailed to: 9-ANM-
inspected as specified in 28–AWL–24 as of [Docket No. FAA–2018–0036; Product
Seattle-ACO-AMOC-Requests@faa.gov.
the effective date of this AD: Conduct the Identifier 2017–SW–015–AD; Amendment
(2) Before using any approved AMOC,
inspection within 12 months after the 39–19354; AD 2018–16–14]
notify your appropriate principal inspector,
effective date of this AD.
or lacking a principal inspector, the manager RIN 2120–AA64
(h) Additional Acceptable Wire Types and of the local flight standards district office/
Sleeving certificate holding district office. Airworthiness Directives; Bell
(3) An AMOC that provides an acceptable
As an option, when accomplishing the
level of safety may be used for any repair,
Helicopter Textron Inc., Helicopters
actions required by paragraph (g) of this AD,
modification, or alteration required by this AGENCY: Federal Aviation
the changes specified in paragraphs (h)(1)
AD if it is approved by the Boeing Administration (FAA), DOT.
and (h)(2) of this AD can be made to AWL
Commercial Airplanes Organization
No. 28–AWL–03. ACTION: Final rule.
Designation Authorization (ODA) that has
(1) Where AWL No. 28–AWL–03 identifies
been authorized by the Manager, Seattle ACO
wire types BMS 13–48, BMS 13–58, and BMS
Branch, FAA, to make those findings. To be SUMMARY: We are adopting a new
13–60, add the following acceptable wire approved, the repair method, modification airworthiness directive (AD) for Bell
types: MIL–W–22759/16, SAE AS22759/16 deviation, or alteration deviation must meet Helicopter Textron Inc. (Bell) Model
(M22759/16), MIL–W–22759/32, SAE the certification basis of the airplane, and the 212, Model 412, and Model 412EP
AS22759/32 (M22759/32), MIL–W–22759/34, approval must specifically refer to this AD.
SAE AS22759/34 (M22759/34), MIL–W–
helicopters. This AD requires replacing
22759/41, SAE AS22759/41 (M22759/41), (l) Related Information the emergency flotation system (EFS)
MIL–W–22759/86, SAE AS22759/86 tube assembly. This AD was prompted
For more information about this AD,
(M22759/86), MIL–W–22759/87, SAE contact Christopher Baker, Aerospace by a report of an EFS tube assembly
AS22759/87 (M22759/87), MIL–W–22759/92 Engineer, Propulsion Section, FAA, Seattle failure. The actions of this AD are
and SAE AS22759/92 (M22759/92); and ACO Branch, 2200 South 216th St., Des intended to address an unsafe condition
MIL–C–27500 and NEMA WC 27500 cables Moines, WA 98198; phone and fax: 206–231– on these products.
constructed from these military or SAE 3552; email: christopher.r.baker@faa.gov. DATES: This AD is effective October 4,
specification wire types identified above.
(2) Where AWL No. 28–AWL–03 identifies (m) Material Incorporated by Reference 2018.
TFE–2X Standard wall for wire sleeving, add (1) The Director of the Federal Register ADDRESSES: For service information
the following acceptable sleeving materials: approved the incorporation by reference identified in this final rule, contact Bell
Roundit 2000NX and Varglas Type HO, HP, (IBR) of the service information listed in this Helicopter Textron, Inc., P.O. Box 482,
or HM. paragraph under 5 U.S.C. 552(a) and 1 CFR Fort Worth, TX 76101; telephone (817)
part 51.
(i) No Alternative Actions, Intervals, and
(2) You must use this service information 280–3391; fax (817) 280–6466; or at
Critical Design Configuration Control http://www.bellcustomer.com/files/.
as applicable to do the actions required by
Limitations (CDCCLs) this AD, unless the AD specifies otherwise. You may review a copy of the
After the maintenance or inspection (i) Boeing 727–100/200 Airworthiness referenced service information at the
program, as applicable, has been revised as Limitations (AWLs) D6–8766–AWL, Revision FAA, Office of the Regional Counsel,
required by paragraph (g) of this AD, no December 2016. Southwest Region, 10101 Hillwood
alternative actions (e.g., inspections), (ii) Reserved. Pkwy., Room 6N–321, Fort Worth, TX
intervals, and CDCCLs may be used unless (3) For service information identified in 76177.
the actions, intervals, and CDCCLs are this AD, contact Boeing Commercial
approved as an alternative method of Airplanes, Attention: Contractual & Data Examining the AD Docket
compliance (AMOC), in accordance with the Services (C&DS), 2600 Westminster Blvd.,
procedures specified in paragraph (k) of this MC 110–SK57, Seal Beach, CA 90740–5600; You may examine the AD docket on
AD. telephone 562–797–1717; internet https:// the internet at http://
www.myboeingfleet.com. www.regulations.gov by searching for
(j) Terminating Actions (4) You may view this service information and locating Docket No. FAA–2018–
Accomplishment of the maintenance or at the FAA, Transport Standards Branch, 0036; or in person at Docket Operations
inspection program revision required by 2200 South 216th St., Des Moines, WA. For between 9 a.m. and 5 p.m., Monday
amozie on DSK3GDR082PROD with RULES

paragraph (g) of this AD terminates the information on the availability of this through Friday, except Federal holidays.
actions specified in paragraphs (j)(1) through material at the FAA, call 206–231–3195.
(j)(5) of this AD. (5) You may view this service information
The AD docket contains this AD, the
(1) The revision required by paragraph (g) that is incorporated by reference at the economic evaluation, any comments
of AD 2008–04–10 R1. National Archives and Records received, and other information. The
(2) The revision required by paragraph (h) Administration (NARA). For information on street address for Docket Operations
of AD 2009–05–03. the availability of this material at NARA, call (phone: 800–647–5527) is U.S.

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Document Created: 2018-08-30 01:21:52
Document Modified: 2018-08-30 01:21:52
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 October 4, 2018.
Contact		Christopher Baker, Aerospace Engineer, Propulsion Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3552; email: [email protected]
FR Citation		83 FR 44204
RIN Number		2120-AA64
CFR Associated		Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety
83 FR 44204 - Airworthiness Directives; The Boeing Company Airplanes

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 83, Issue 169 (August 30, 2018)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
