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Published 1999-03-01 · Federal Register document 99-4890

Airworthiness Directives; British Aerospace Jetstream Model 3101 Airplanes

Publication summary

This action confirms the effective date of Airworthiness Directive (AD) 99-01-07, which applies to certain British Aerospace Jetstream Model 3101 airplanes. AD 99-01-07 requires installing additional stringers at the lower fuselage skin panels between the main and rear spar frames. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified in this AD are intended to correct a strength deficiency in the area of the lower fuselage skin panels between the main rear spar frames, which, if not corrected, could result in reduced or loss of control of the airplane during maximum speed limit operations.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:22:57.343810+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_1999-e9a7378e7e7d30d5
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results[91]
Raw source SHA-256
e9a7378e7e7d30d51578560dc0677c56bb1fef0a9323224e2a0afe1544919217

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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 3f02cf12ea3aee4b0110e32e37a00b61de1e953d81222506433c786d66d8b24c. Source manifest: 7bc5e75d4ebe2db1f35cd13e608507f13631585198ad528d5ddebc54a65029e8.

Official source · 1999-03-01

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 64, Number 39 (Monday, March 1, 1999)]
[Rules and Regulations]
[Pages 9911-9912]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 99-4890]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98-CE-100-AD; Amendment 39-10974; AD 99-01-07]
RIN 2120-AA64


Airworthiness Directives; British Aerospace Jetstream Model 3101 
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) 99-01-07, which applies to certain British Aerospace 
Jetstream Model 3101 airplanes. AD 99-01-07 requires installing 
additional stringers at the lower fuselage skin panels between the main 
and rear spar frames. This AD is the result of mandatory continuing 
airworthiness information (MCAI) issued by the airworthiness authority 
for the United Kingdom. The actions specified in this AD are intended 
to correct a strength deficiency in the area of the lower fuselage skin 
panels between the main rear spar frames, which, if not corrected, 
could result in reduced or loss of control of the airplane during 
maximum speed limit operations.

EFFECTIVE DATE: March 19, 1999.

FOR FURTHER INFORMATION CONTACT: Mr. S.M. Nagarajan, Aerospace 
Engineer, FAA, Small Airplane Directorate, 1201 Walnut, suite 900, 
Kansas City, Missouri

[[Page 9912]]

64106; telephone: (816) 426-6932; facsimile: (816) 426-2169.

SUPPLEMENTARY INFORMATION: The FAA published this direct final rule 
with request for comments in the Federal Register on December 31, 1998 
(63 FR 72139). 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, was received within the comment period, the regulation would 
become effective on March 19, 1999. 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 February 22, 1999.
Marvin R. Nuss,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 99-4890 Filed 2-26-99; 8:45 am]
BILLING CODE 4910-13-P


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d231bedad2e3b8a383c6b0a94d04154f89d7a0016bfdf7231ceb67652cb33c3f
Text SHA-256
3f02cf12ea3aee4b0110e32e37a00b61de1e953d81222506433c786d66d8b24c

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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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