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FAA airworthiness directive publication

AD 2019-01-01

2019-01-29 · Correction notice · Federal Register document 2019-00297

This page records a selected historical publication. Its current legal status, applicability to an individual aircraft and compliance have not been determined. Consult the current FAA directive and aircraft configuration and maintenance records.

This correction remains a separate publication; it is not presented as a newly issued independent directive.

What this historical correction says

Source publication 2019-01-29 · Document 2019-00297.

The notice republishes the complete rule. The complete applicability clause from this reprint is retained below with its conditions unevaluated.

Need for the Correction

    As published, a document specified in the regulatory text is 
incorrect. Specifically, a service bulletin that is referenced in 
figure 1 to paragraph (g) of AD 2019-01-01 was incorrectly identified 
as Rolls Royce Non Modification Service Bulletin Trent 1000 ``72-
AK132.'' The correct number is ``72-K132.'' Service bulletin ``72-
AK132'' does not exist, and therefore, operators cannot directly comply 
with the AD requirement that refers to that service bulletin.

Correction of Publication

    The error appeared in figure 1 to paragraph (g) of AD 2019-01-01. 
Although no other part of the preamble or regulatory information has 
been corrected, we are publishing the entire rule in the Federal 
Register.
    The effective date of this AD remains February 4, 2019.

Original date wording

DATES: This correction is effective February 4, 2019.

Dates describing the correction and the original rule remain separate as written.

Complete applicability clause in this reprint

(c) Applicability

    This AD applies to The Boeing Company Model 787-8 airplanes, 
certificated in any category, powered by Rolls-Royce plc (RR) Trent 
1000-A (including -A/01 and -A/01A), Trent 1000-AE (including -AE/
01A), Trent 1000-C (including -C/01 and -C/01A), Trent 1000-CE 
(including -CE/01A), Trent 1000-D (including -D/01 and -D/01A), 
Trent 1000-E (including -E/01 and -E/01A), Trent 1000-G (including -
G/01 and -G/01A), and Trent 1000-H (including -H/01 and H/01A) 
turbofan engines.

Literal source labels for discovery: 787-8. Labels remain as written; series, aliases and engine suffixes are not expanded.

Dated original publication

  • AD 2019-01-01 · 2019-01-18 · document 2019-00078
    SUPPLEMENTARY INFORMATION: As published, Airworthiness Directive 2019-
    01-01, Amendment 39-19540 (84 FR 129, January 18, 2019) (``AD 2019-01-
    01''), requires revising the airplane flight manual (AFM) to limit 
    extended operations (ETOPS) for The Boeing Company Model 787-8 
    airplanes powered by RR Trent 1000-A (including -A/01 and -A/01A), 
    Trent 1000-AE (including -AE/01A), Trent 1000-C (including -C/01 and -
    C/01A), Trent 1000-CE (including -CE/01A), Trent 1000-D (including -D/
    01 and -D/01A), Trent 1000-E (including -E/01 and -E/01A), Trent 1000-G 
    (including -G/01 and -G/01A), and Trent 1000-H (including -H/01 and H/
    01A) turbofan engines.
    
    Need for the Correction
    
        As published, a document specified in the regulatory text is 
    incorrect. Specifically, a service bulletin that is referenced in 
    figure 1 to paragraph (g) of AD 2019-01-01 was incorrectly identified 
    as Rolls Royce Non Modification Service Bulletin Trent 1000 ``72-
    AK132.'' The correct number is ``72-K132.'' Service bulletin ``72-
    AK132'' does not exist, and therefore, operators cannot directly comply 
    with the AD requirement that refers to that service bulletin.
    
    Correction of Publication
    
        The error appeared in figure 1 to paragraph (g) of AD 2019-01-01. 
    Although no other part of the preamble or regulatory information has 
    been corrected, we are publishing the entire rule in the Federal 
    Register.
        The effective date of this AD remains February 4, 2019.
    
    

Each link opens a separate dated source. These words and dates do not determine which directive controls today, aircraft applicability, installed configuration or compliance. No corrected rule body has been merged.

Historical relationship observation unknown

This correction notice is a separate source edition and was not interpreted as a new rule. This does not establish that there are no related or currently applicable directives.

Earlier extraction record

The earlier extraction kept these fields unknown. Its original record is preserved below. Newly retained correction excerpts are shown above; applicability and compliance remain undetermined.

Applicability text in this publication

An applicability clause was not extracted from this publication. Applicability remains undetermined.

Effective-date text

An effective-date observation was not extracted from this publication.

Publication context

A relationship to prior directives has not been established from this publication.

Official sources

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Sources retrieved: HTML 2026-09-08; PDF 2026-09-08.

The displayed text comes from the HTML publication. Refer to the official documents for the original wording.

This selected source edition is not a complete list of current airworthiness directives. Referenced manufacturer service documents are not reproduced here.

Related sources

Explore all recorded source editions of this AD identifier · Find selected publications with this AD number. Matching numbers are discovery links; source identity, current legal status and aircraft applicability remain separate.

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