Published 2005-11-08 · Federal Register document 05-22214
Airworthiness Directives; Boeing Model 727 Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 727 airplanes. This AD requires revising the Limitations section of the airplane flight manual to prohibit resetting a tripped circuit breaker for a fuel pump. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prohibit the resetting of a tripped circuit breaker for a fuel pump, which could allow an electrical fault to override the protective features of the circuit breaker, and could result in sparks inside the fuel tank, ignition of fuel vapors, and consequent fire or explosion.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:17.300228+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2005-5d43d153038ee1c1
- Source row
- results[478]
- Raw source SHA-256
- 5d43d153038ee1c1c214f5c3688e38e25e37b832227fe65d52f7420a65ee20f2
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2005-23-07
- Effective date printed in this edition
- 2005-12-13
Read 7 complete recorded clauses
Effective Date
Effective Date
(a) This AD becomes effective December 13, 2005.
Exact source excerpt. Text positions 6644–6714, end exclusive, in the original decoded publication. SHA-256: 39d9409e7a12a899da526022270fca72ec231c9119cdfc21e0e27f08bdc7c9c4
Affected ADs
Affected ADs
(b) None.
Exact source excerpt. Text positions 6714–6743, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b
Applicability wording · Applicability
Applicability
(c) This AD applies to all Boeing Model 727, 727C, 727-100, 727-
100C, 727-200, and 727-200F series airplanes; certificated in any
category.
Exact source excerpt. Text positions 6743–6905, end exclusive, in the original decoded publication. SHA-256: d1cdee350680aa478efdb7b17c6901c2cbcb1a142f8e44f4cd3ad97571e46fc7
Unsafe Condition
Unsafe Condition
(d) This AD results from fuel system reviews conducted by the
manufacturer. We are issuing this AD to prohibit the resetting of a
tripped circuit breaker for a fuel pump, which could allow an
electrical fault to override the protective features of the circuit
breaker, and could result in sparks inside the fuel tank, ignition
of fuel vapors, and consequent fire or explosion.
Exact source excerpt. Text positions 6905–7310, end exclusive, in the original decoded publication. SHA-256: e37c3f5ad1bae4902543681ad432ebba936f2ef7c60d2680074012d1c7c6cbb6
Compliance
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Exact source excerpt. Text positions 7310–7488, end exclusive, in the original decoded publication. SHA-256: 64a7a1579f37f56eafecd0aeb3c528e7c89f6292ed0cb53091423917642d5847
Revise the Airplane Flight Manual (AFM)
Revise the Airplane Flight Manual (AFM)
(f) Within 30 days after the effective date of this AD, revise
the Limitations section of the Boeing 727 AFM to include the
following statement. This may be done by inserting a copy of this AD
into the AFM.
``Do not reset a tripped fuel pump circuit breaker.''
Note 1: When a statement identical to that in paragraph (f) of
this AD has been included in the general revisions of the AFM, the
general revisions may be inserted into the AFM, and the copy of this
AD may be removed from the AFM.
Alternative Methods of Compliance (AMOCs)
(g)(1) The Manager, Seattle Aircraft Certification Office, FAA,
has the authority to approve AMOCs for this AD, if requested in
accordance with the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in accordance with 14 CFR
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Exact source excerpt. Text positions 7488–8498, end exclusive, in the original decoded publication. SHA-256: 8f13648406fc8682dc4ad93869b1ed85f3d0057c4723220924b4e884b1fee260
Material Incorporated by Reference
Material Incorporated by Reference
(h) None.
Exact source excerpt. Text positions 8498–8548, end exclusive, in the original decoded publication. SHA-256: 7a84e242cfe9ae2d6acab059101af0bd1e30673b79022a8834cddd34be49ecb8
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 2005-23-07 · 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: 7f8026489357e9aa4be8e231255f72661281abc9097b38a272c82956d1cf0fbc. Source manifest: 088b8cbbf2976d5e86d3b61d4288b696ebe61340504536724c032ea052ee2e7e.
Official source · 2005-11-08
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 70, Number 215 (Tuesday, November 8, 2005)]
[Rules and Regulations]
[Pages 67644-67645]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-22214]
=======================================================================
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-21975; Directorate Identifier 2005-NM-122-AD;
Amendment 39-14365; AD 2005-23-07]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 727 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Boeing Model 727 airplanes. This AD requires revising the Limitations
section of the airplane flight manual to prohibit resetting a tripped
circuit breaker for a fuel pump. This AD results from fuel system
reviews conducted by the manufacturer. We are issuing this AD to
prohibit the resetting of a tripped circuit breaker for a fuel pump,
which could allow an electrical fault to override the protective
features of the circuit breaker, and could result in sparks inside the
fuel tank, ignition of fuel vapors, and consequent fire or explosion.
DATES: This AD becomes effective December 13, 2005.
ADDRESSES: You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif Building,
room PL-401, Washington, DC.
Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle,
Washington 98124-2207, for service information identified in this AD.
FOR FURTHER INFORMATION CONTACT: Sulmo Mariano, Aerospace Engineer,
Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification
Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone
(425) 917-6501; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the airworthiness directive (AD) docket on the
Internet at http://dms.dot.gov or in person at the Docket Management
Facility office between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The Docket Management Facility office
(telephone (800) 647-5227) is located on the plaza level of the Nassif
Building at the street address stated in the ADDRESSES section.
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to include an AD that would apply to all Boeing Model 727
airplanes. That NPRM was published in the Federal Register on July 29,
2005 (70 FR 43802). That NPRM proposed to require revising the
Limitations section of the airplane flight manual to prohibit resetting
a tripped circuit breaker for a fuel pump.
Comments
We provided the public the opportunity to participate in the
development of this AD. We have considered the one comment received.
The commenter supports the NPRM.
Clarification of Alternative Method of Compliance (AMOC) Paragraph
We have revised this action to clarify the appropriate procedure
for notifying the principal inspector before using any approved AMOC on
any airplane to which the AMOC applies.
Conclusion
We have carefully reviewed the available data, including the
comment received, and determined that air safety and the public
interest require adopting the AD with the change described previously.
We have determined that this change will neither increase the economic
burden on any operator nor increase the scope of the AD.
Costs of Compliance
There are about 600 airplanes of the affected design in the
worldwide fleet. This AD affects about 300 airplanes of U.S. registry.
The action in this AD takes about 1 work hour per airplane, at an
average labor rate of $65 per work hour. Based on these figures, the
estimated cost of the AD for U.S. operators is $19,500, or $65 per
airplane.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue
[[Page 67645]]
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
We have determined that 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); and
(3) 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.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket. See the ADDRESSES
section for a location to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
Adoption of the Amendment
0
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 Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2005-23-07 Boeing: Amendment 39-14365. Docket No. FAA-2005-21975;
Directorate Identifier 2005-NM-122-AD.
Effective Date
(a) This AD becomes effective December 13, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Boeing Model 727, 727C, 727-100, 727-
100C, 727-200, and 727-200F series airplanes; certificated in any
category.
Unsafe Condition
(d) This AD results from fuel system reviews conducted by the
manufacturer. We are issuing this AD to prohibit the resetting of a
tripped circuit breaker for a fuel pump, which could allow an
electrical fault to override the protective features of the circuit
breaker, and could result in sparks inside the fuel tank, ignition
of fuel vapors, and consequent fire or explosion.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Revise the Airplane Flight Manual (AFM)
(f) Within 30 days after the effective date of this AD, revise
the Limitations section of the Boeing 727 AFM to include the
following statement. This may be done by inserting a copy of this AD
into the AFM.
``Do not reset a tripped fuel pump circuit breaker.''
Note 1: When a statement identical to that in paragraph (f) of
this AD has been included in the general revisions of the AFM, the
general revisions may be inserted into the AFM, and the copy of this
AD may be removed from the AFM.
Alternative Methods of Compliance (AMOCs)
(g)(1) The Manager, Seattle Aircraft Certification Office, FAA,
has the authority to approve AMOCs for this AD, if requested in
accordance with the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in accordance with 14 CFR
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Material Incorporated by Reference
(h) None.
Issued in Renton, Washington, on October 26, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-22214 Filed 11-7-05; 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 2026-10-09T03:50:45.270436+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
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- Text SHA-256
- 7f8026489357e9aa4be8e231255f72661281abc9097b38a272c82956d1cf0fbc
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Coverage and limits
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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