Published 2012-02-07 · Federal Register document 2012-2004
Airworthiness Directives; The Boeing Company Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-100, -200, -200C, and -300 series airplanes. This AD was prompted by a report from the airplane manufacturer that airplanes were assembled with air distribution ducts in the environmental control system (ECS) wrapped with Boeing Material Specification (BMS) 8-39 or Aeronautical Materials Specifications (AMS) 3570 polyurethane foam insulation, a material with fire-retardant properties that deteriorate with age. This AD requires reworking certain air distribution ducts in the ECS. We are issuing this AD to prevent ignition of the BMS 8-39 or AMS 3570 polyurethane foam insulation on the duct assemblies of the ECS due to a potential electrical arc, which could start a small fire and lead to a larger fire that may spread throughout the airplane through the ECS.
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[28]
- Raw source SHA-256
- 08bffa249ae9a2053bbfc0d74663d089914e83fb91f9bc4c8409ea28239f6875
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2012-02-09
- Effective date printed in this edition
- 2012-03-13
Read 12 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective March 13, 2012.
Exact source excerpt. Text positions 7607–7669, end exclusive, in the original decoded publication. SHA-256: ac71098dcf13468be6f6ab1e0785c175617d23f38a1caa3852687f9328da5b57
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 7669–7698, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to The Boeing Company Model 737-100, -200, -
200C, and -300 series airplanes, certificated in any category; as
identified in Boeing Service Bulletin 737-21A1132, Revision 3, dated
February 16, 2011.
Exact source excerpt. Text positions 7698–7939, end exclusive, in the original decoded publication. SHA-256: 6c2b6cc767a7713d967909984b07ced5766418441d51ceee514949ca96e520fc
Subject
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 21, Air conditioning.
Exact source excerpt. Text positions 7939–8067, end exclusive, in the original decoded publication. SHA-256: ef133f87855c6f81ce78d09e0b273464f724c890fc4eede4d2efe123df00dafe
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by a report from the airplane manufacturer
that airplanes were assembled with air distribution ducts in the
environmental control system (ECS) wrapped with Boeing Material
Specification (BMS) 8-39 or Aeronautical Materials Specifications
(AMS) 3570 polyurethane foam insulation, a material with fire
retardant properties that deteriorate with age. We are issuing this
AD to prevent ignition of the BMS 8-39 or AMS 3570 polyurethane foam
insulation on the duct assemblies of the ECS due to a potential
electrical arc, which could start a small fire and lead to a larger
fire that may spread throughout the airplane through the ECS.
Exact source excerpt. Text positions 8067–8755, end exclusive, in the original decoded publication. SHA-256: c6ddd1937979fc167026dccf299aab78e26cd273d46e3dcae5847b971c83a611
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 8755–8857, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Air Distribution Duct Rework
(g) Air Distribution Duct Rework
Within 72 months after the effective date of this AD, rework the
applicable duct assemblies in the ECS specified in and in accordance
with the Accomplishment Instructions and Appendix A of Boeing
Service Bulletin 737-21A1132, Revision 3, dated February 16, 2011.
Exact source excerpt. Text positions 8857–9162, end exclusive, in the original decoded publication. SHA-256: 87134b1c987600dd2d38dafb331d292cc7ea8f56729fdaa386e778a3f57b2265
Credit for Actions Accomplished in Accordance With Previous Service Information
(h) Credit for Actions Accomplished in Accordance With Previous Service
Information
Reworking the applicable duct assemblies in the ECS in
accordance with the Accomplishment Instructions and Appendix A of
Boeing Service Bulletin 737-21A1132, Revision 2, dated June 13,
2007, before the effective date of this AD is acceptable for
compliance with the corresponding actions required by paragraph (g)
of this AD.
Exact source excerpt. Text positions 9162–9584, end exclusive, in the original decoded publication. SHA-256: 08b1cc6710ffa00f4f0958802051568a46881debe80924f8fe2de88fc41fedb5
Parts Installation
(i) Parts Installation
As of the effective date of this AD, no person may install an
ECS duct assembly with BMS 8-39 or AMS 3570 polyurethane foam
insulation on any airplane.
Exact source excerpt. Text positions 9584–9767, end exclusive, in the original decoded publication. SHA-256: 647865ee43f214c739ed53ff4eebecba62571dbed0fd48bdaf2d454d9f0eca32
Alternative Methods of Compliance (AMOCs)
(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 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 9767–10559, end exclusive, in the original decoded publication. SHA-256: c7215eac071e4e970cdef4605fdf14fd8d03fd9601b142ddd92ab580e0081b3d
Related Information
(k) Related Information
(1) For more information about this AD, contact Kimberly A.
DeVoe, Aerospace Engineer, Cabin Safety and Environmental Systems
Branch, ANM-150S, FAA, Seattle Aircraft Certification Office, 1601
Lind Avenue SW., Renton, Washington 98057-3356; phone: 425-917-6495;
fax: (425) 917-6590; email: [email protected].
(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; phone:
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.
Exact source excerpt. Text positions 10559–11451, end exclusive, in the original decoded publication. SHA-256: 7a07969b02e48810afd21d2acf2f2276e61234aca7cc9c194977b74c69d1bc0a
Material Incorporated by Reference
(l) 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) under 5 U.S.C. 552(a) and 1 CFR part 51 of the
following service information:
(i) Boeing Service Bulletin 737-21A1132, Revision 3, dated
February 16, 2011.
(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 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 11451–12747, end exclusive, in the original decoded publication. SHA-256: 4e38db8133060e8d32ef52de2c0ba1cd3bdbb3272aa602d7a021fc2c028c4ec1
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 2012-02-09 · 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: 051ca95a5f5c8d879334e5a9d52011f2bb73a058ec0b7e46bf363508dc885ca0. Source manifest: d25cee64474662a08a934d9909479f3e850777b7a5b2917fbfb353f9527a92c0.
Official source · 2012-02-07
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 77, Number 25 (Tuesday, February 7, 2012)]
[Rules and Regulations]
[Pages 5996-5997]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-2004]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2011-1171; Directorate Identifier 2011-NM-101-AD;
Amendment 39-16932; AD 2012-02-09]
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 737-100, -200, -200C, and -300 series
airplanes. This AD was prompted by a report from the airplane
manufacturer that airplanes were assembled with air distribution ducts
in the environmental control system (ECS) wrapped with Boeing Material
Specification (BMS) 8-39 or Aeronautical Materials Specifications (AMS)
3570 polyurethane foam insulation, a material with fire-retardant
properties that deteriorate with age. This AD requires reworking
certain air distribution ducts in the ECS. We are issuing this AD to
prevent ignition of the BMS 8-39 or AMS 3570 polyurethane foam
insulation on the duct assemblies of the ECS due to a potential
electrical arc, which could start a small fire and lead to a larger
fire that may spread throughout the airplane through the ECS.
DATES: This AD is effective March 13, 2012.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of March 13,
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: Kimberly A. DeVoe, Aerospace Engineer,
Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle
Aircraft Certification Office, 1601 Lind Avenue SW., Renton, Washington
98057-3356; phone: (425) 917-6495; 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 November 7, 2011 (76 FR
68666). That NPRM proposed to require reworking certain air
distribution ducts in the ECS.
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 68666, November 7, 2011).
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 68666, November 7, 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 68666, November 7, 2011).
Costs of Compliance
We estimate that this AD affects 292 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
----------------------------------------------------------------------------------------------------------------
Duct assembly rework/part marking........ 250 work-hours x $85 per $3,545 $24,795 $7,240,140
hour = $21,250.
----------------------------------------------------------------------------------------------------------------
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
[[Page 5997]]
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):
2012-02-09 The Boeing Company: Amendment 39-16932; Docket No. FAA-
2011-1171; Directorate Identifier 2011-NM-101-AD.
(a) Effective Date
This AD is effective March 13, 2012.
(b) Affected ADs
None.
(c) Applicability
This AD applies to The Boeing Company Model 737-100, -200, -
200C, and -300 series airplanes, certificated in any category; as
identified in Boeing Service Bulletin 737-21A1132, Revision 3, dated
February 16, 2011.
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 21, Air conditioning.
(e) Unsafe Condition
This AD was prompted by a report from the airplane manufacturer
that airplanes were assembled with air distribution ducts in the
environmental control system (ECS) wrapped with Boeing Material
Specification (BMS) 8-39 or Aeronautical Materials Specifications
(AMS) 3570 polyurethane foam insulation, a material with fire
retardant properties that deteriorate with age. We are issuing this
AD to prevent ignition of the BMS 8-39 or AMS 3570 polyurethane foam
insulation on the duct assemblies of the ECS due to a potential
electrical arc, which could start a small fire and lead to a larger
fire that may spread throughout the airplane through the ECS.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Air Distribution Duct Rework
Within 72 months after the effective date of this AD, rework the
applicable duct assemblies in the ECS specified in and in accordance
with the Accomplishment Instructions and Appendix A of Boeing
Service Bulletin 737-21A1132, Revision 3, dated February 16, 2011.
(h) Credit for Actions Accomplished in Accordance With Previous Service
Information
Reworking the applicable duct assemblies in the ECS in
accordance with the Accomplishment Instructions and Appendix A of
Boeing Service Bulletin 737-21A1132, Revision 2, dated June 13,
2007, before the effective date of this AD is acceptable for
compliance with the corresponding actions required by paragraph (g)
of this AD.
(i) Parts Installation
As of the effective date of this AD, no person may install an
ECS duct assembly with BMS 8-39 or AMS 3570 polyurethane foam
insulation on any airplane.
(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 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.
(k) Related Information
(1) For more information about this AD, contact Kimberly A.
DeVoe, Aerospace Engineer, Cabin Safety and Environmental Systems
Branch, ANM-150S, FAA, Seattle Aircraft Certification Office, 1601
Lind Avenue SW., Renton, Washington 98057-3356; phone: 425-917-6495;
fax: (425) 917-6590; email: [email protected].
(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; phone:
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.
(l) 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) under 5 U.S.C. 552(a) and 1 CFR part 51 of the
following service information:
(i) Boeing Service Bulletin 737-21A1132, Revision 3, dated
February 16, 2011.
(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 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 12, 2012.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-2004 Filed 2-6-12; 8:45 am]
BILLING CODE 4910-13-P
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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.
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