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Published 2006-06-16 · Federal Register document 06-5427

Airworthiness Directives; Engine Components Incorporated (ECi) Reciprocating Engine Connecting Rods; Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2006-10-21. That AD applies to Engine Components Incorporated (ECi) reciprocating engine connecting rods. We published AD 2006-10-21 in the Federal Register on May 18, 2006, (71 FR 28769). An incorrect amendment number exists under the Sec. 39.13 amended heading. This document corrects the amendment number. In all other respects, the original document remains the same.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:20.745856+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2006-8d787f8b35bc8016
Source row
results[217]
Raw source SHA-256
8d787f8b35bc80165a417cea66de09cd32a1700face13759db364c607e405963

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2006-10-21
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: 7e9325490ce80e95933c9e9b48018ebf579caa3bdb6fcbf95bc148f7d4c36657. Source manifest: 3d6502937aa4b1f103edc1db5fa38968e5948696d0730942d73890847636b7c9.

Official source · 2006-06-16

Publication text

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Read the complete official publication text
[Federal Register Volume 71, Number 116 (Friday, June 16, 2006)]
[Rules and Regulations]
[Page 34811]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 06-5427]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-21331; Directorate Identifier 2005-NE-07-AD; 
Amendment 39-14604; AD 2006-10-21]
RIN 2120-AA64


Airworthiness Directives; Engine Components Incorporated (ECi) 
Reciprocating Engine Connecting Rods; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2006-10-21. That AD applies to Engine Components Incorporated 
(ECi) reciprocating engine connecting rods. We published AD 2006-10-21 
in the Federal Register on May 18, 2006, (71 FR 28769). An incorrect 
amendment number exists under the Sec.  39.13 amended heading. This 
document corrects the amendment number. In all other respects, the 
original document remains the same.

DATES: Effective Date: Effective June 16, 2006.

FOR FURTHER INFORMATION CONTACT: Peter Hakala, Aerospace Engineer, 
Special Certification Office, FAA, Rotorcraft Directorate, 2601 Meacham 
Blvd., Fort Worth, TX 76193; telephone (817) 222-5145; fax (817) 222-
5785.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 06-4046, that 
applies to Engine Components Incorporated (ECi) reciprocating engine 
connecting rods was published in the Federal Register on May 18, 2006, 
(71 FR 28769). The following correction is needed:


Sec.  39.13  [Corrected]

0
On page 28771, in the third column, under Sec.  39.13 [Amended], in the 
fifth and sixth lines, ``Amendment 39-14605'' is corrected to read 
``Amendment 39-14604''.

    Issued in Burlington, MA, on June 9, 2006.
Thomas A. Boudreau,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 06-5427 Filed 6-15-06; 8:45 am]
BILLING CODE 4910-13-P


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Source SHA-256
e2cb5450cbb07561f7baeaf027a5af5d0f361e335099495553b6e53a980c269b
Text SHA-256
7e9325490ce80e95933c9e9b48018ebf579caa3bdb6fcbf95bc148f7d4c36657

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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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