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Published 2000-03-02 · Federal Register document 00-5010

Airworthiness Directives; Airbus Model A340-211, -212, -213, -311, -312, and -313 Series Airplanes; Correction

Publication summary

This document corrects a typographical error that appeared in airworthiness directive (AD) 99-27-14 that was published in the Federal Register on January 6, 2000 (65 FR 697). The typographical error resulted in a reference to an incorrect AD number. This AD is applicable to all Airbus Model A340-211, -212, -213, -311, -312, and - 313 series airplanes. This AD requires repetitive operational tests to ensure proper operation of the actuator of the secondary locks of the thrust reversers, and corrective actions, if necessary.

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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[121]
Raw source SHA-256
18aee3630151116d2fb3a6893673332fd0937cde18bc691722f3a802a62279eb

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
99-27-14
Effective date printed in this edition
Unknown

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Find all recorded historical references to AD 99-27-14 · 0 printed reference observations in this pinned collection.

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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: aa2a90c6b0c18b54dc803809fd92be76f48f4ae81fab352dc940693cdd8a76a4. Source manifest: 3a397821e11f44f4426025524affce799a60428f73ecd3059d84fd3ce1baec89.

Official source · 2000-03-02

Publication text

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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 42 (Thursday, March 2, 2000)]
[Rules and Regulations]
[Pages 11204-11205]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-5010]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99-NM-336-AD; Amendment 39-11495; AD 99-27-14]
RIN 2120-AA64


Airworthiness Directives; Airbus Model A340-211, -212, -213, -
311, -312, and -313 Series Airplanes; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

-----------------------------------------------------------------------

SUMMARY: This document corrects a typographical error that appeared in 
airworthiness directive (AD) 99-27-14 that was published in the Federal 
Register on January 6, 2000 (65 FR 697). The typographical error 
resulted in a reference to an incorrect AD number. This AD is 
applicable to all Airbus Model A340-211, -212, -213, -311, -312, and -
313 series airplanes. This AD requires repetitive operational tests to 
ensure proper operation of the actuator of the secondary locks of the 
thrust reversers, and corrective actions, if necessary.

EFFECTIVE DATE: Effective January 21, 2000.

FOR FURTHER INFORMATION CONTACT: Norman B. Martenson, Manager, 
International Branch, ANM-116, Transport Airplane Directorate, 1601 
Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-
2110; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 99-27-14, 
amendment 39-11495, applicable to all Airbus Model A340-211, -212, -
213, -311, -312, and -313 series airplanes, was published in the 
Federal Register on January 6, 2000 (65 FR 697). That AD requires 
repetitive operational tests to ensure proper operation of the actuator 
of the secondary locks of the thrust reversers, and corrective actions, 
if necessary.
    As published, AD 99-27-14 contains an erroneous reference to the AD 
number cited in the paragraph preceding the applicability of the AD. 
That paragraph incorrectly references AD 99-01-05, Amendment 39-10980. 
The correct reference is AD 99-01-15, Amendment 39-10980.
    Since no other part of the regulatory information has been changed, 
the final rule is not being republished.
    The effective date of this AD remains January 21, 2000.

[[Page 11205]]

Sec. 39.13  [Corrected]

    On page 699, in the first column, the paragraph preceding the 
applicability of AD 99-27-14 is corrected to read as follows:

99-27-14  Airbus Industrie: Amendment 39-11495. Docket 99-NM-336-AD. 
Supersedes AD 99-01-15, Amendment 39-10980.
* * * * *

    Issued in Renton, Washington, on February 25, 2000.
Donald L. Riggin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 00-5010 Filed 3-1-00; 8:45 am]
BILLING CODE 4910-13-P


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Source SHA-256
12e23064bd2b03b2ab08b6a2039f104528f01560d54b36e9305702cf1a3d701e
Text SHA-256
aa2a90c6b0c18b54dc803809fd92be76f48f4ae81fab352dc940693cdd8a76a4

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