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Published 2002-09-09 · Federal Register document 02-22760

Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F and 914 F Series Reciprocating Engines; Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2002-16-26, applicable to Bombardier-Rotax GmbH type 912 F and 914 F series reciprocating engines. AD 2002-16-26 was published in the Federal Register on August 15, 2002 (67 FR 53296). The effective date in the DATES: section is incorrect. This document corrects that date. In all other respects, the original document remains the same.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:07.262592+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2002-c8c2ee537a56d16c
Source row
results[324]
Raw source SHA-256
c8c2ee537a56d16c3d3246bbaa55e183792a136494260623f45827707b4e2a64

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2002-16-26
Effective date printed in this edition
Unknown

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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: 1aef7b9e27076de39a804e7024c7a9bf1f8dd0c782286d362b9c44ca386099d1. Source manifest: 02238b4c98915cd8bc81a345199ff7d2eef91c91b8ed227ccbcb0ccf1b5eebf0.

Official source · 2002-09-09

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 67, Number 174 (Monday, September 9, 2002)]
[Rules and Regulations]
[Pages 57145-57146]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-22760]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2002-NE-08-AD; Amendment 39-12865; AD 2002-16-26]
RIN 2120-AA64


Airworthiness Directives; Bombardier-Rotax GmbH Type 912 F and 
914 F Series Reciprocating Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; request for comments, correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2002-16-26, applicable to Bombardier-Rotax GmbH type 912 F and 914 
F series reciprocating engines. AD 2002-16-26 was published in the 
Federal Register on August 15, 2002 (67 FR 53296). The effective date 
in the DATES: section is incorrect. This document corrects that date. 
In all other respects, the original document remains the same.

EFFECTIVE DATE: August 30, 2002.

FOR FURTHER INFORMATION CONTACT: James Lawrence, Aerospace Engineer,

[[Page 57146]]

Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803-5299; telephone (781) 
238-7176; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule; request for comments 
airworthiness directive FR DOC. 02-20679, applicable to Bombardier-
Rotax GmbH type 912 F and 914 F series reciprocating engines, was 
published in the Federal Register on August 15, 2002 (67 FR 53296). The 
following correction is needed:
    On page 53296, in the second column, in the DATES: section, 
``Effective September 16, 2002'' is corrected to read ``Effective 
August 30, 2002''.

    Issued in Burlington, MA, on August 30, 2002.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 02-22760 Filed 9-6-02; 8:45 am]
BILLING CODE 4910-13-P


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faf8a7d3c21a884f411e5373625238a3e6b66e89b85129a6a707c5d2965d6249
Text SHA-256
1aef7b9e27076de39a804e7024c7a9bf1f8dd0c782286d362b9c44ca386099d1

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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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