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Published 2008-11-28 · Federal Register document E8-28108

Airworthiness Directives; MD Helicopters, Inc. Model 600N Helicopters

Publication summary

This document corrects airworthiness directive (AD) 2008-20-05 which was published on October 10, 2008 (73 FR 60102) and applies to MD Helicopters, Inc. (MDHI) Model 600N helicopters. AD 2008-20-05 requires modifying the fuselage aft section, repetitively inspecting the tailboom attachment fittings, installing inspection holes and attachment bolt washers, modifying both access covers, and replacing broken attachment bolts. This document corrects the AD number that is incorrectly listed as 2008-20-08 on page 60104 of the AD.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:26.953736+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2008-e9cf118935fdae82
Source row
results[448]
Raw source SHA-256
e9cf118935fdae82a000e2c01764c770bd79679c1dd4c2b00fdcd3b030f92fe5

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2008-20-05
Effective date printed in this edition
Unknown

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Find all recorded historical references to AD 2008-20-05 · 0 printed reference observations in this pinned collection.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.

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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: 29bccd391bf5e934cc971a24446784e25932537954294364920e02d26655d5c9. Source manifest: f7cc094a8ca43fa0bcfc5424422757df68b98b9cb2a40501b5b502403cab7ad6.

Official source · 2008-11-28

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 73, Number 230 (Friday, November 28, 2008)]
[Rules and Regulations]
[Page 72316]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E8-28108]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-0835; Directorate Identifier 2008-SW-34-AD; 
Amendment 39-15684; AD 2008-20-05]
RIN 2120-AA64


Airworthiness Directives; MD Helicopters, Inc. Model 600N 
Helicopters

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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

SUMMARY: This document corrects airworthiness directive (AD) 2008-20-05 
which was published on October 10, 2008 (73 FR 60102) and applies to MD 
Helicopters, Inc. (MDHI) Model 600N helicopters. AD 2008-20-05 requires 
modifying the fuselage aft section, repetitively inspecting the 
tailboom attachment fittings, installing inspection holes and 
attachment bolt washers, modifying both access covers, and replacing 
broken attachment bolts. This document corrects the AD number that is 
incorrectly listed as 2008-20-08 on page 60104 of the AD.

DATES: The effective date of AD 2008-20-05 remains October 27, 2008.

FOR FURTHER INFORMATION CONTACT: Eric Schrieber, Aviation Safety 
Engineer, FAA, Los Angeles Aircraft Certification Office, Airframe 
Branch, 3960 Paramount Blvd., Lakewood, California 90712, telephone 
(562) 627-5348, fax (562) 627-5210.

SUPPLEMENTARY INFORMATION:
    Discussion: On September 25, 2008, we issued AD 2008-20-05 to amend 
14 CFR part 39 to include an AD that applies to MDHI Model 600N 
helicopters. That AD requires modifying the fuselage aft section, 
repetitively inspecting the tailboom attachment fittings, installing 
inspection holes and attachment bolt washers, modifying both access 
covers, and replacing broken attachment bolts.
    As published, AD 2008-20-05 contains an incorrect AD number (2008-
20-08) in the regulatory text on page 60104 of the AD. The correct AD 
number is 2008-20-05.
    No other part of the regulatory information has been changed; 
therefore, the AD is not republished in the Federal Register.

Correction of Publication

    Accordingly, the publication on October 10, 2008 of Amendment 39-
15684, AD 2008-20-05, Docket No. FAA-2008-0835, Directorate Identifier 
2008-SW-34-AD (73 FR 60102), which is the subject of FR Doc. E8-23540, 
is corrected as follows:


Sec.  39.13  [Corrected]

    On page 60104, in the second column, in the paragraph under Sec.  
39.13 [Amended], change ``2008-20-08'' to read ``2008-20-05''.

    Issued in Fort Worth, Texas, on November 14, 2008.
Scott A. Horn,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. E8-28108 Filed 11-26-08; 8:45 am]
BILLING CODE 4910-13-P


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The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:26:32.127480+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
2498b76b1c09006863b76188ac56df054378c29c3705b64ece5381f93d02db5d
Text SHA-256
29bccd391bf5e934cc971a24446784e25932537954294364920e02d26655d5c9

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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.

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