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Published 2011-02-07 · Federal Register document 2011-2428

Airworthiness Directives; The Boeing Company Model MD-90-30 Airplanes

Publication summary

We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires installing new fire handle shutoff system wiring. This AD was prompted by a possible latent failure in the fire handle shutoff relay circuit due to a lack of separation between engine wires. We are issuing this AD to minimize the possibility of a multiple engine shutdown due to single fire handle activation.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:36.067984+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2011-e3661fa6ab35b428
Source row
results[36]
Raw source SHA-256
e3661fa6ab35b428e6e5ee3716d50c22e985c092328ad8ce2f0f440b962ae0cd

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2011-03-09
Effective date printed in this edition
2011-03-14
Read 8 complete recorded clauses
Effective Date
Effective Date

    (a) This AD is effective March 14, 2011.

Exact source excerpt. Text positions 7103–7165, end exclusive, in the original decoded publication. SHA-256: ca01a7eb5c285c2e86bbe30c89948913936867015fcb6dab00953d74ade71c42

Affected ADs
Affected ADs

    (b) None.

Exact source excerpt. Text positions 7165–7194, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b

Applicability wording · Applicability
Applicability

    (c) This AD applies to all The Boeing Company Model MD-90-30 
airplanes, certificated in any category.

Exact source excerpt. Text positions 7194–7317, end exclusive, in the original decoded publication. SHA-256: e290dd3fc7c4dea0c78db5fa65963c6cb1cdb25ac71e3f3e522ab48ba04c57a8

Subject
Subject

    (d) Joint Aircraft System Component (JASC)/Air Transport 
Association (ATA) of America Code 74, Ignition.

Exact source excerpt. Text positions 7317–7437, end exclusive, in the original decoded publication. SHA-256: 6f9374326efa099cb7680c57c5ed6b380ab5f8a7fdab4ea95246073edbc3b898

Unsafe Condition
Unsafe Condition

    (e) This AD was prompted by a possible latent failure in the 
fire handle shutoff relay circuit due to a lack of separation 
between engine wires. We are proposing this AD to minimize the 
possibility of a multiple engine shutdown due to single fire handle 
activation.

Exact source excerpt. Text positions 7437–7730, end exclusive, in the original decoded publication. SHA-256: 6142f02b61a394647d9bcbe4dae8bba18ae416a1e24354cb60dc8a17e0424ad6

Compliance
Compliance

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

Exact source excerpt. Text positions 7730–7832, end exclusive, in the original decoded publication. SHA-256: 76a8ec0548389ac4eaa60ddcc67a7a3de5aedefd320c767b7cf621baa6140ea8

Wire Installation
Wire Installation

    (g) Within 4,200 flight hours after the effective date of this 
AD, install new fire handle shutoff system wiring, in accordance 
with the Accomplishment Instructions of Boeing Alert Service 
Bulletin MD90-74A002, dated August 17, 2010.

Alternative Methods of Compliance (AMOCs)

    (h)(1) The Manager, Los Angeles Aircraft Certification Office, 
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 the Related Information 
section of this AD.
    (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.

Exact source excerpt. Text positions 7832–8832, end exclusive, in the original decoded publication. SHA-256: e3c5ffd2ae53fe849f13be30f8710b7dc510bf7c3191cae0c108795c48905a2f

Related Information
Related Information

    (i) For more information about this AD, contact William S. Bond, 
Aerospace Engineer, Propulsion Branch, ANM-140L, FAA, Los Angeles 
Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, 
CA 90712-4137; phone: 562-627-5253; fax: 562-627-5210; e-mail: 
[email protected].

 Material Incorporated by Reference

    (j) You must use Boeing Alert Service Bulletin MD90-74A002, 
dated August 17, 2010, to do the actions required by this AD, unless 
the AD specifies otherwise.
    (1) The Director of the Federal Register approved the 
incorporation by reference of Boeing Alert Service Bulletin MD90-
74A002, dated August 17, 2010, under 5 U.S.C. 552(a) and 1 CFR part 
51.
    (2) For service information identified in this AD, contact 
Boeing Commercial Airplanes, Attention: Data & Services Management, 
3855 Lakewood Boulevard, MC D800-0019, Long Beach, California 90846-
0001; telephone 206-544-5000, extension 2; fax 206-766-5683; e-mail 
[email protected]; Internet https://www.myboeingfleet.com.
    (3) You may review copies of the service information at the FAA, 
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, 
Washington. For information on the availability of this material at 
the FAA, call 425-227-1221.
    (4) You may also review copies of the service information that 
is incorporated by reference at the National Archives and Records 
Administration (NARA). For information on the availability of this 
material at an NARA facility, call 202-741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

Exact source excerpt. Text positions 8832–10451, end exclusive, in the original decoded publication. SHA-256: bc9744ca006aad4c406266369331ebe5ed1ba43b1cfa8331f32940accf434004

No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.

Find all recorded historical references to AD 2011-03-09 · 0 printed reference observations in this pinned collection.

These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.

Why these observations are shown

They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.

Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: fda8ea121fa0cfcd4a692f116bb256d445afd9a1fcb2bf60497af9df1fae581d. Source manifest: 54894e4e75ad2ac6052f0546543e823a5c1d5faab363f27f8731ede793b1c823.

Official source · 2011-02-07

Publication text

This is the complete recorded text of this dated publication.

Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.

Read the complete official publication text
[Federal Register Volume 76, Number 25 (Monday, February 7, 2011)]
[Rules and Regulations]
[Pages 6535-6536]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2011-2428]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-1043; Directorate Identifier 2010-NM-200-AD; 
Amendment 39-16593; AD 2011-03-09]
RIN 2120-AA64


Airworthiness Directives; The Boeing Company Model MD-90-30 
Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for the 
products listed above. This AD requires installing new fire handle 
shutoff system wiring. This AD was prompted by a possible latent 
failure in the fire handle shutoff relay circuit due to a lack of 
separation between engine wires. We are issuing this AD to minimize the 
possibility of a multiple engine shutdown due to single fire handle 
activation.

DATES: This AD is effective March 14, 2011.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in the AD as of March 14, 
2011.

ADDRESSES: For service information identified in this AD, contact 
Boeing Commercial Airplanes, Attention: Data & Services Management, 
3855 Lakewood Boulevard, MC D800-0019, Long Beach, California 90846-
0001; telephone 206-544-5000, extension 2; fax 206-766-5683; e-mail 
[email protected]; Internet https://www.myboeingfleet.com. You may 
review copies of the referenced service information at the FAA 
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, 
Washington. For information on the availability of this material at the 
FAA, call 425-227-1221.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; 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 Document 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: William S. Bond, Aerospace Engineer, 
Propulsion Branch, ANM-140L, FAA, Los Angeles Aircraft Certification 
Office, 3960 Paramount Boulevard, Lakewood, CA 90712; phone: 562-627-
5253; fax: 562-627-5210; e-mail: [email protected].

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to include an airworthiness directive (AD) that would apply to 
the specified products. That NPRM published in the Federal Register on 
November 5, 2010 (75 FR 68245). That NPRM proposed to require 
installing new fire handle shutoff system wiring.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM or on the determination of 
the cost to the public.

Explanation of Change Made to the AD

    We have revised this AD to identify the legal name of the 
manufacturer as published in the most recent type certificate data 
sheet for the affected airplane models.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting the AD with the change described 
previously. We also determined that this change will not increase the 
economic burden on any operator or increase the scope of the AD.

Costs of Compliance

    We estimate that this AD will affect 25 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                                  Cost on U.S.
              Action                    Labor cost           Parts cost      Cost per product      operators
----------------------------------------------------------------------------------------------------------------
Wiring change....................  8 work-hours x $85                $489             $1,169            $29,225
                                    per hour = $680.
----------------------------------------------------------------------------------------------------------------

 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

[[Page 6536]]

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):

2011-03-09 The Boeing Company: Amendment 39-16593; Docket No. FAA-
2010-1043; Directorate Identifier 2010-NM-200-AD.

Effective Date

    (a) This AD is effective March 14, 2011.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to all The Boeing Company Model MD-90-30 
airplanes, certificated in any category.

Subject

    (d) Joint Aircraft System Component (JASC)/Air Transport 
Association (ATA) of America Code 74, Ignition.

Unsafe Condition

    (e) This AD was prompted by a possible latent failure in the 
fire handle shutoff relay circuit due to a lack of separation 
between engine wires. We are proposing this AD to minimize the 
possibility of a multiple engine shutdown due to single fire handle 
activation.

Compliance

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

Wire Installation

    (g) Within 4,200 flight hours after the effective date of this 
AD, install new fire handle shutoff system wiring, in accordance 
with the Accomplishment Instructions of Boeing Alert Service 
Bulletin MD90-74A002, dated August 17, 2010.

Alternative Methods of Compliance (AMOCs)

    (h)(1) The Manager, Los Angeles Aircraft Certification Office, 
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 the Related Information 
section of this AD.
    (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.

Related Information

    (i) For more information about this AD, contact William S. Bond, 
Aerospace Engineer, Propulsion Branch, ANM-140L, FAA, Los Angeles 
Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, 
CA 90712-4137; phone: 562-627-5253; fax: 562-627-5210; e-mail: 
[email protected].

 Material Incorporated by Reference

    (j) You must use Boeing Alert Service Bulletin MD90-74A002, 
dated August 17, 2010, to do the actions required by this AD, unless 
the AD specifies otherwise.
    (1) The Director of the Federal Register approved the 
incorporation by reference of Boeing Alert Service Bulletin MD90-
74A002, dated August 17, 2010, under 5 U.S.C. 552(a) and 1 CFR part 
51.
    (2) For service information identified in this AD, contact 
Boeing Commercial Airplanes, Attention: Data & Services Management, 
3855 Lakewood Boulevard, MC D800-0019, Long Beach, California 90846-
0001; telephone 206-544-5000, extension 2; fax 206-766-5683; e-mail 
[email protected]; Internet https://www.myboeingfleet.com.
    (3) You may review copies of the service information at the FAA, 
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, 
Washington. For information on the availability of this material at 
the FAA, call 425-227-1221.
    (4) You may also review copies of the service information that 
is incorporated by reference at the National Archives and Records 
Administration (NARA). For information on the availability of this 
material at an NARA facility, call 202-741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

    Issued in Renton, Washington, on January 26, 2011.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2011-2428 Filed 2-4-11; 8:45 am]
BILLING CODE 4910-13-P


Why this text is shown

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:10:53.755394+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
b019323d1a1777186d88776f0fdff0e758730377696ce1c746776f4e58151e75
Text SHA-256
fda8ea121fa0cfcd4a692f116bb256d445afd9a1fcb2bf60497af9df1fae581d

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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.