Published 2000-10-18 · Federal Register document 00-26237
Airworthiness Directives; Boeing Model 747 and 767 Series Airplanes Powered by General Electric Model CF6-80C2 Series Engines; Correction
Publication summary
This document corrects a typographical error that appeared in airworthiness directive (AD) 2000-11-08, amendment 39-11756, that was published in the Federal Register on June 1, 2000 (65 FR 34935). The typographical error resulted in a reference to an incorrect fuel specification. That AD is applicable to certain Boeing Model 747 and 767 series airplanes. That AD supersedes an earlier airworthiness directive to require revising the FAA-approved Airplane Flight Manual (AFM) to prohibit the use of certain fuels; and either replacing an existing placard with a new placard, or replacing all dribble flow fuel nozzles (DFFN) with standard fuel nozzles, which terminates the requirements for the new placard and AFM revision. That AD also includes identical requirements applicable to airplanes on which standard fuel nozzles are not installed.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:00.616356+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2000-18aee3630151116d
- Source row
- results[463]
- Raw source SHA-256
- 18aee3630151116d2fb3a6893673332fd0937cde18bc691722f3a802a62279eb
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2000-11-08
- Effective date printed in this edition
- Unknown
This correction is a separate source edition; it is not counted as a new adopted rule.
No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.
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Find all recorded historical references to AD 2000-11-08 · 0 printed reference observations in this pinned collection.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: 81d76ce47120f257d623d865268ef89aa7939c4ca29d5b7b02468bdd61dc66fb. Source manifest: 2706632343a36600466eda048c9f2df2ebcedfd22c3156bc3c0a97da3c742eb6.
Official source · 2000-10-18
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 65, Number 202 (Wednesday, October 18, 2000)]
[Rules and Regulations]
[Pages 62281-62282]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-26237]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 99-NM-228-AD; Amendment 39-11756; AD 2000-11-08]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 747 and 767 Series
Airplanes Powered by General Electric Model CF6-80C2 Series Engines;
Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document corrects a typographical error that appeared in
airworthiness directive (AD) 2000-11-08, amendment 39-11756, that was
published in the Federal Register on June 1, 2000 (65 FR 34935). The
typographical error resulted in a reference to an incorrect fuel
specification. That AD is applicable to certain Boeing Model 747 and
767 series airplanes. That AD supersedes an earlier airworthiness
directive to require revising the FAA-approved Airplane Flight Manual
(AFM) to prohibit the use of certain fuels; and either replacing an
existing placard with a new placard, or replacing all dribble flow fuel
nozzles (DFFN) with standard fuel nozzles, which terminates the
requirements for the new placard and AFM revision. That AD also
includes identical requirements applicable to airplanes on which
standard fuel nozzles are not installed.
DATES: Effective July 6, 2000.
FOR FURTHER INFORMATION CONTACT: Ed Hormel, Aerospace Engineer,
Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification
Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone
(425) 227-2681; fax (425) 227-1181.
SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2000-11-08,
amendment 39-11756, applicable to certain Boeing Model 747 and 767
series airplanes, was published in the Federal Register on June 1, 2000
(65 FR 34935). That AD supersedes AD 98-08-23, amendment 39-10472 (63
FR 18817, April 16, 1998) to require revising the FAA-approved Airplane
Flight Manual (AFM) to prohibit the use of certain fuels; and either
replacing an existing placard with a new placard, or replacing all
dribble flow fuel nozzles (DFFN) with standard fuel nozzles, which
terminates the requirements for the new placard and AFM revision. That
AD also includes identical requirements applicable to airplanes on
which standard fuel nozzles are not installed.
As published, AD 2000-11-08 contains an erroneous fuel
specification in paragraphs (a)(1)(i) and (c)(1) of that AD. Those
paragraphs incorrectly reference MIL-T-83113, which is a specification
that does not exist. The correct reference is MIL-T-83133.
Since no other part of the regulatory information has been changed,
the final rule is not being republished.
Accordingly, in FR Doc. 00-13447 published June 1, 2000 (65 FR
34935), make the following corrections:
The effective date of this AD remains July 6, 2000.
Sec. 39.13 [Corrected]
1. On page 34937, in the second column, paragraph (a)(1)(i) of AD
2000-11-08 is corrected to read as follows:
AD 2000-11-08
* * * * *
(a) * * *
[[Page 62282]]
(1) * * *
(i) Revise paragraph 1 of the Engine Fuel System section to read as
follows: ``The fuel designation is General Electric (GE) Specification
D50TF2, as revised. Fuel conforming to commercial jet fuel
specification ASTM-D-1655, Jet A, and Jet A-1 are authorized for
unlimited use in this engine. Fuels conforming to MIL-T-5624 grade JP-5
and MIL-T-83133 grade JP-8 are acceptable alternatives. The engine will
operate satisfactorily with any of the foregoing fuels or any mixture
thereof.'' And,
* * * * *
2. On page 34937, in the third column, paragraph (c)(1) of AD 2000-
11-08 is corrected to read as follows:
* * * * *
(c) * * *
(1) Revise paragraph 1 of the Engine Fuel System section to read as
follows: ``The fuel designation is General Electric (GE) Specification
D50TF2, as revised. Fuel conforming to commercial jet fuel
specification ASTM-D-1655, Jet A, and Jet A-1 are authorized for
unlimited use in this engine. Fuels conforming to MIL-T-5624 grade JP-5
and MIL-T-83133 grade JP-8 are acceptable alternatives. The engine will
operate satisfactorily with any of the foregoing fuels or any mixture
thereof.'' And,
* * * * *
Issued in Renton, Washington, on October 5, 2000.
Lirio Liu Nelson,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 00-26237 Filed 10-17-00; 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 2026-10-09T04:35:53.349753+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- f9129206e1aa3998e97110e7e3021d802c4f477c28b30118ebb9077b6c621ed0
- Text SHA-256
- 81d76ce47120f257d623d865268ef89aa7939c4ca29d5b7b02468bdd61dc66fb
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
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.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.