Published 2006-03-29 · Federal Register document 06-2983
Airworthiness Directives; GROB-WERKE Model G120A Airplanes
Publication summary
This document makes a correction to Airworthiness Directive (AD) 2005-13-09, which published in the Federal Register on August 23, 2005 (70 FR 49184), and applies to certain GROB-WERKE Model G120A airplanes. AD 2005-13-09 requires replacement of the main landing gear (MLG) up-lock hook assembly. Current language in paragraph (e)(2) of AD 2005-13-09 incorrectly references the MLG up-lock assembly as "elevator and aileron hinge pins." This AD corrects that paragraph to reference the appropriate part number MLG up-lock hook assembly.
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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.
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Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2005-13-09
- Effective date printed in this edition
- Unknown
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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: f681ae7115b0fe4540f29140d4ee6ba4631f3c55ee23d5e51a626d4afe4a6b78. Source manifest: 2328ca58a4c6f9e5cb5461c17c9bd353abfee5a3edfa675ddeec84d65b1431ef.
Official source · 2006-03-29
Publication text
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Read the complete official publication text
[Federal Register Volume 71, Number 60 (Wednesday, March 29, 2006)]
[Rules and Regulations]
[Page 15559]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 06-2983]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-19473; Directorate Identifier 2004-CE-35-AD;
Amendment 39-14146; AD 2005-13-09]
RIN 2120-AA64
Airworthiness Directives; GROB-WERKE Model G120A Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
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SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 2005-13-09, which published in the Federal Register on August 23,
2005 (70 FR 49184), and applies to certain GROB-WERKE Model G120A
airplanes. AD 2005-13-09 requires replacement of the main landing gear
(MLG) up-lock hook assembly. Current language in paragraph (e)(2) of AD
2005-13-09 incorrectly references the MLG up-lock assembly as
``elevator and aileron hinge pins.'' This AD corrects that paragraph to
reference the appropriate part number MLG up-lock hook assembly.
DATES: The effective date of this AD (2005-13-09) remains July 26,
2005.
FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer,
ACE-112, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: 816-329-4146; facsimile: 816-329-4090.
SUPPLEMENTARY INFORMATION:
Discussion
On August 15, 2005, the FAA issued AD 2005-13-09, Amendment 39-
14146 (70 FR 49184, August 23, 2005), which applies to certain GROB-
WERKE Model G120A airplanes.
AD 2005-13-09 requires replacement of the MLG up-lock hook
assembly. Current language in paragraph (e)(2) of AD 2005-13-09
incorrectly references the MLG up-lock assembly as ``elevator and
aileron hinge pins.'' This AD corrects that paragraph to reference the
appropriate part number MLG up-lock hook assembly.
Need for the Correction
This correction is needed to ensure that reference to the MLG up-
lock hook assembly part number is correct for future reference. All
airplanes currently on the U.S. Register have the actions of AD 2005-
13-09 incorporated.
Correction of Publication
0
Accordingly, the publication of August 23, 2005 (70 FR 49184), of
Amendment 39-14146; AD 2005-13-09, which was the subject of FR Doc.
05'16440, is corrected as follows:
Sec. 39.13 [Corrected]
0
On page 49184, in Sec. 39.13 [Amended], in paragraph (e)(2), replace
the Current Text in the Actions column with the Replacement Text.
Current Text: ``(2) For all serial numbers: Do not install any
elevator and aileron hinge pins that are not part number SY991A hinge
pins.''
Replacement Text: ``(2) Do not install any MLG up-lock hook
assembly that is not part number X03-0020-00-00.00/1 (or FAA-approved
later part number that supersedes this part number).''
Action is taken herein to correct this reference in AD 2005-13-09
and to add this AD correction to Sec. 39.13 of the Federal Aviation
Regulations (14 CFR 39.13).
The effective date remains July 26, 2005.
Issued in Kansas City, Missouri, on March 22, 2006.
William J. Timberlake,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 06-2983 Filed 3-28-06; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
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