Published 1998-04-27 · Federal Register document 98-11010
Airworthiness Directives; Dornier Luftfahrt GmbH Models 228-100, 228-101, 228-200, and 228-201 Airplanes
Publication summary
This action confirms the effective date of Airworthiness Directive (AD) 98-06-13 which applies to Models 228-100, 228-101, 228- 200, and 228-201 airplanes equipped with certain main landing gear (MLG). AD 98-06-13 requires replacing the MLG axle assembly with an MLG axle assembly of improved design. This AD was the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified in this AD are intended to prevent main landing gear failure, which, if not corrected, could result in loss of control of the airplane during landing operations.
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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:22:53.985165+00:00. The title, summary and date are source facts.
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- federal_register_ad_metadata_1998-f5c1cf5c93c99179
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- results[233]
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- f5c1cf5c93c99179023030016db80652e7593139090148c64a6fd533918aa991
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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 44b5d29ca61050f50f6afd78e450cc9000cbc95bbfbcf5cfb45113c48314957f. Source manifest: 767d035af5c348ff259a3e91463265e9c99715261a559820d23d97f80eec1931.
Official source · 1998-04-27
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 63, Number 80 (Monday, April 27, 1998)]
[Rules and Regulations]
[Page 20528]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-11010]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 97-CE-124-AD; Amendment 39-10391; AD 98-06-13]
RIN 2120-AA64
Airworthiness Directives; Dornier Luftfahrt GmbH Models 228-100,
228-101, 228-200, and 228-201 Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Direct final rule; confirmation of effective date.
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SUMMARY: This action confirms the effective date of Airworthiness
Directive (AD) 98-06-13 which applies to Models 228-100, 228-101, 228-
200, and 228-201 airplanes equipped with certain main landing gear
(MLG). AD 98-06-13 requires replacing the MLG axle assembly with an MLG
axle assembly of improved design. This AD was the result of mandatory
continuing airworthiness information (MCAI) issued by the airworthiness
authority for Germany. The actions specified in this AD are intended to
prevent main landing gear failure, which, if not corrected, could
result in loss of control of the airplane during landing operations.
DATES: Effective June 15, 1998.
FOR FURTHER INFORMATION CONTACT: Mr. Karl M. Schletzbaum, Aerospace
Engineer, FAA, Small Airplane Directorate, Aircraft Certification
Service, 1201 Walnut, suite 900, Kansas City, Missouri 64106;
telephone: (816) 426-6934; facsimile: (816) 426-2169.
SUPPLEMENTARY INFORMATION: The FAA published this direct final rule
with request for comments in the Federal Register on March 16, 1998 (63
FR 12605). The FAA uses the direct final rulemaking procedure for a
non-controversial rule where the FAA anticipates that there will be no
adverse public comment. This direct final rule advised the public that
no adverse comments were anticipated, and that unless a written adverse
comment, or a written notice of intent to submit such an adverse
comment, were received within the comment period, the regulation would
become effective on June 15, 1998. No adverse comments were received,
and thus this notice confirms that this final rule will become
effective on that date.
Issued in Kansas City, Missouri, on April 17, 1998.
James A. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 98-11010 Filed 4-24-98; 8:45 am]
BILLING CODE 4910-13-U
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- d19680fd24d046094d73e5edb78b42993bd80bb8d42d1db43325dccb13b2c5ce
- Text SHA-256
- 44b5d29ca61050f50f6afd78e450cc9000cbc95bbfbcf5cfb45113c48314957f
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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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