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Published 2012-02-17 · Federal Register document 2012-2973

Airworthiness Directives; The Boeing Company Airplanes

Publication summary

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 767-200, -300, and -300F series airplanes. This AD was prompted by reports of loss of avionics cooling due to an unserviceable relay installed on a panel as part of the cabin air conditioning and temperature control system (CACTCS). This AD requires doing certain wiring changes, installing a new relay and necessary wiring in the CACTCS, and performing an operational test of the cooling pack system. We are issuing this AD to prevent loss of electrical equipment bay cooling and the overheating of flight deck instruments, which would result in the eventual loss of primary flight displays, an unusually high pilot workload, and depressurization of the cabin.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:39.502075+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2012-08bffa249ae9a205
Source row
results[43]
Raw source SHA-256
08bffa249ae9a2053bbfc0d74663d089914e83fb91f9bc4c8409ea28239f6875

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2012-03-02
Effective date printed in this edition
2012-03-23
Read 10 complete recorded clauses
Effective Date
(a) Effective Date

    This AD is effective March 23, 2012.

Exact source excerpt. Text positions 7767–7829, end exclusive, in the original decoded publication. SHA-256: 9d820cf5c4fa6896d03a15a374898a0a2820f643ea28b6cfeaeef451d9dad353

Affected ADs
(b) Affected ADs

    None.

Exact source excerpt. Text positions 7829–7858, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0

Applicability wording · Applicability
(c) Applicability

    This AD applies to The Boeing Company Model 767-200 and -300 
series airplanes, certificated in any category, as identified in 
Boeing Special Attention Service Bulletin 767-21-0246, dated January 
7, 2011; and Model 767-300F series airplanes, certificated in any 
category, as identified in Boeing Special Attention Service Bulletin 
767-21-0234, dated August 6, 2009.

Exact source excerpt. Text positions 7858–8252, end exclusive, in the original decoded publication. SHA-256: a474a96c97bf3cb5ed79feda65a7c39073682aa30d3f8d656494ad27390a2119

Subject
(d) Subject

    Joint Aircraft System Component (JASC)/Air Transport Association 
(ATA) of America Code 21: Air conditioning.

Exact source excerpt. Text positions 8252–8380, end exclusive, in the original decoded publication. SHA-256: bbde2602cc2e272b61957401489a95f0fe40a58ea2015d37d436ea6000e0b725

Unsafe Condition
(e) Unsafe Condition

    This AD results from reports of loss of avionics cooling due to 
an unserviceable relay installed on a panel as part of the cabin air 
conditioning and temperature control system (CACTCS). We are issuing 
this AD to prevent loss of electrical equipment bay cooling and the 
overheating of flight deck instruments, which would result in the 
eventual loss of primary flight displays, an unusually high pilot 
workload, and depressurization of the cabin.

Exact source excerpt. Text positions 8380–8860, end exclusive, in the original decoded publication. SHA-256: 644f5ab274af81704bb4ab207e06fc38c69d71ce1ce12229c501fb460d0c4cd3

Compliance
(f) Compliance

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

Exact source excerpt. Text positions 8860–8962, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

Installation of New Relay and Wiring Bundle
(g) Installation of New Relay and Wiring Bundle

    Within 72 months after the effective date of this AD: Change the 
wire bundle route and wiring, install a new relay and applicable 
wiring in the CACTCS, and do an operational test of the cooling pack 
system, in accordance with the Accomplishment Instructions of the 
service information specified in paragraph (g)(1) or (g)(2) of this 
AD, as applicable.
    (1) For Model 767-200 and 767-300 series airplanes: Boeing 
Special Attention Service Bulletin 767-21-0246, dated January 7, 
2011.
    (2) For Model 767-300F series airplanes: Boeing Special 
Attention Service Bulletin 767-21-0234, dated August 6, 2009.

Exact source excerpt. Text positions 8962–9632, end exclusive, in the original decoded publication. SHA-256: 68ce70d59bef013532c8d82a81a288302111d6dd4ca76a06e897d18b32dc8f0c

Alternative Methods of Compliance (AMOCs)
(h) 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 the Related Information 
section 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.

Exact source excerpt. Text positions 9632–10424, end exclusive, in the original decoded publication. SHA-256: fb7d90ffb437408d9e0a7760be4bd3449b0e299402efd7af90ec2d7862cd4269

Related Information
(i) Related Information

    For more information about this AD, contact Ana Martinez Hueto, 
Aerospace Engineer, Cabin Safety and Environmental Systems Branch, 
ANM-150S, FAA, Seattle Aircraft Certification Office, 1601 Lind 
Avenue SW., Renton, WA 98057-3356; phone 425-917-6592; fax 425-917-
6590; email: [email protected].

Exact source excerpt. Text positions 10424–10752, end exclusive, in the original decoded publication. SHA-256: 4d3df36ab64b3a57a505f23a767a0d478afefd9a647754f0d935e176bfcda666

Material Incorporated by Reference
(j) Material Incorporated by Reference

    (1) You must use the following service information to do the 
actions required by this AD, unless the AD specifies otherwise. The 
Director of the Federal Register approved the incorporation by 
reference (IBR) of the following service information under 5 U.S.C. 
552(a) and 1 CFR part 51:
    (i) Boeing Special Attention Service Bulletin 767-21-0246, dated 
January 7, 2011.
    (ii) Boeing Special Attention Service Bulletin 767-21-0234, 
dated August 6, 2009.
    (2) For service information identified in this AD, contact 
Boeing Commercial Airplanes, Attention: Data & Services Management, 
P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 
206-544-5000, extension 1; fax 206-766-5680; email 
[email protected]; Internet https://www.myboeingfleet.com.
    (3) You may review copies of the referenced service information 
at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., 
Renton, Washington. For

[[Page 9520]]

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 NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

Exact source excerpt. Text positions 10752–12145, end exclusive, in the original decoded publication. SHA-256: bb13911a39bbdfc86fc772db90b20a542da40770bf175472dfe060ac4a58f8d1

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 2012-03-02 · 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: c55f18e3c00456b8390277b5b351d318528ff8f55c0b29f25cb134559a594656. Source manifest: c333a8d7936ce8fb857beb9494c75d2f29e2fe0c456c24de90619a8a500eb67a.

Official source · 2012-02-17

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 77, Number 33 (Friday, February 17, 2012)]
[Rules and Regulations]
[Pages 9518-9520]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-2973]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-0725; Directorate Identifier 2011-NM-065-AD; 
Amendment 39-16943; AD 2012-03-02]
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 767-200, -300, and -300F series airplanes. 
This AD was prompted by reports of loss of avionics cooling due to an 
unserviceable relay installed on a panel as part of the cabin air 
conditioning and temperature control system (CACTCS). This AD requires 
doing certain wiring changes, installing a new relay and necessary 
wiring in the CACTCS, and performing an operational test of the cooling 
pack system. We are issuing this AD to prevent loss of electrical 
equipment bay cooling and the overheating of flight deck instruments, 
which would result in the eventual loss of primary flight displays, an 
unusually high pilot workload, and depressurization of the cabin.

DATES: This AD is effective March 23, 2012.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in the AD as of March 23, 
2012.

ADDRESSES: For service information identified in this AD, contact 
Boeing Commercial Airplanes, Attention: Data & Services Management, 
P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206-
544-5000, extension 1; fax 206-766-5680; email: [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: Ana Martinez Hueto, Aerospace 
Engineer, Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, 
Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 
98057-3356; phone: 425-917-6592; fax: 425-917-6590; email: 
[email protected].

SUPPLEMENTARY INFORMATION: 

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to include an AD that would apply to the specified products. 
That NPRM published in the Federal Register on August 24, 2011 (76 FR 
52899). That NPRM proposed to require doing certain wiring changes, 
installing a new relay and necessary wiring in the CACTCS, and 
performing an operational test of the cooling pack system.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We have considered the comments received. Boeing supports the 
NPRM (76 FR 52899, August 24, 2011). American Airlines stated that it 
is not affected by the NPRM.

Conclusion

    We reviewed the relevant data, considered the comments received, 
and determined that air safety and the public interest require adopting 
the AD as proposed except for minor editorial changes. We have 
determined that these minor changes:
    <bullet> Are consistent with the intent that was proposed in the 
NPRM (76 FR 52899, August 24, 2011) for correcting the unsafe 
condition; and
    <bullet> Do not add any additional burden upon the public than was 
already proposed in the NPRM (76 FR 52899, August 24, 2011).

Costs of Compliance

    We estimate that this AD affects 35 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

[[Page 9519]]



                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
               Action                        Labor cost           Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
Change wire bundle, install relay,    29 work-hours x $85 per          $1,240           $3,705         $129,675
 and operational test.                 hour = $2,465 per
                                       relay installation.
----------------------------------------------------------------------------------------------------------------

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 the 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):

2012-03-02 The Boeing Company: Amendment 39-16943; Docket No. FAA-
2011-0725; Directorate Identifier 2011-NM-065-AD.

(a) Effective Date

    This AD is effective March 23, 2012.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to The Boeing Company Model 767-200 and -300 
series airplanes, certificated in any category, as identified in 
Boeing Special Attention Service Bulletin 767-21-0246, dated January 
7, 2011; and Model 767-300F series airplanes, certificated in any 
category, as identified in Boeing Special Attention Service Bulletin 
767-21-0234, dated August 6, 2009.

(d) Subject

    Joint Aircraft System Component (JASC)/Air Transport Association 
(ATA) of America Code 21: Air conditioning.

(e) Unsafe Condition

    This AD results from reports of loss of avionics cooling due to 
an unserviceable relay installed on a panel as part of the cabin air 
conditioning and temperature control system (CACTCS). We are issuing 
this AD to prevent loss of electrical equipment bay cooling and the 
overheating of flight deck instruments, which would result in the 
eventual loss of primary flight displays, an unusually high pilot 
workload, and depressurization of the cabin.

(f) Compliance

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

(g) Installation of New Relay and Wiring Bundle

    Within 72 months after the effective date of this AD: Change the 
wire bundle route and wiring, install a new relay and applicable 
wiring in the CACTCS, and do an operational test of the cooling pack 
system, in accordance with the Accomplishment Instructions of the 
service information specified in paragraph (g)(1) or (g)(2) of this 
AD, as applicable.
    (1) For Model 767-200 and 767-300 series airplanes: Boeing 
Special Attention Service Bulletin 767-21-0246, dated January 7, 
2011.
    (2) For Model 767-300F series airplanes: Boeing Special 
Attention Service Bulletin 767-21-0234, dated August 6, 2009.

(h) 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 the Related Information 
section 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.

(i) Related Information

    For more information about this AD, contact Ana Martinez Hueto, 
Aerospace Engineer, Cabin Safety and Environmental Systems Branch, 
ANM-150S, FAA, Seattle Aircraft Certification Office, 1601 Lind 
Avenue SW., Renton, WA 98057-3356; phone 425-917-6592; fax 425-917-
6590; email: [email protected].

(j) Material Incorporated by Reference

    (1) You must use the following service information to do the 
actions required by this AD, unless the AD specifies otherwise. The 
Director of the Federal Register approved the incorporation by 
reference (IBR) of the following service information under 5 U.S.C. 
552(a) and 1 CFR part 51:
    (i) Boeing Special Attention Service Bulletin 767-21-0246, dated 
January 7, 2011.
    (ii) Boeing Special Attention Service Bulletin 767-21-0234, 
dated August 6, 2009.
    (2) For service information identified in this AD, contact 
Boeing Commercial Airplanes, Attention: Data & Services Management, 
P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 
206-544-5000, extension 1; fax 206-766-5680; email 
[email protected]; Internet https://www.myboeingfleet.com.
    (3) You may review copies of the referenced service information 
at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., 
Renton, Washington. For

[[Page 9520]]

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 NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on January 26, 2012.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2012-2973 Filed 2-16-12; 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 2026-10-09T03:04:37.162471+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
87f90699f174ce33e80bf15eac71a8b11ae8d9459e6f2b51cc1853222d56e55a
Text SHA-256
c55f18e3c00456b8390277b5b351d318528ff8f55c0b29f25cb134559a594656

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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.