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Published 1998-12-08 · Federal Register document 98-32473

Airworthiness Directives; British Aerospace Jetstream Model 3101 Airplanes

Publication summary

This action confirms the effective date of Airworthiness Directive (AD) 98-21-28, which applies to certain British Aerospace Jetstream Model 3101 airplanes. AD 98-21-28 requires modifying the propeller de-icing system to assure system performance at low ambient temperatures. This AD was 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 prevent propeller-induced vibrations from occurring during icing encounters at low ambient temperatures, which could result in decreased performance of the de-icing system during icing encounters with possible loss of control of the airplane.

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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.

Source revision
federal_register_ad_metadata_1998-f5c1cf5c93c99179
Source row
results[687]
Raw source SHA-256
f5c1cf5c93c99179023030016db80652e7593139090148c64a6fd533918aa991

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Effective date printed in this edition
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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: 7ff5d4e54bee9bfc45c3ab10822da681c3247b8098fad7afadacdf0bb14d4963. Source manifest: cd0d5f76857797bc710213daec244b09a434ab475756bc6de3312dbaf8672d0a.

Official source · 1998-12-08

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 235 (Tuesday, December 8, 1998)]
[Rules and Regulations]
[Page 67576]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-32473]



[[Page 67576]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98-CE-63-AD; Amendment 39-10836; AD 98-21-28]
RIN 2120-AA64


Airworthiness Directives; British Aerospace Jetstream Model 3101 
Airplanes

AGENCY: Federal Aviation Administration, DOT.

ACTION: Direct final rule; confirmation of effective date.

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

SUMMARY: This action confirms the effective date of Airworthiness 
Directive (AD) 98-21-28, which applies to certain British Aerospace 
Jetstream Model 3101 airplanes. AD 98-21-28 requires modifying the 
propeller de-icing system to assure system performance at low ambient 
temperatures. This AD was 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 prevent propeller-induced vibrations from occurring during icing 
encounters at low ambient temperatures, which could result in decreased 
performance of the de-icing system during icing encounters with 
possible loss of control of the airplane.

EFFECTIVE DATE: January 15, 1999.

FOR FURTHER INFORMATION CONTACT: Mr. S.M. Nagarajan, Aerospace 
Engineer, FAA, Small Airplane Directorate, 1201 Walnut, suite 900, 
Kansas City, Missouri 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 October 14, 1998 
(63 FR 55015). 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 January 15, 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 December 1, 1998.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 98-32473 Filed 12-7-98; 8:45 am]
BILLING CODE 4910-13-U


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Source SHA-256
45efe4447a645d89a32c20cb1bf78a027532649a6ebd4e0c9d22483fb29b39e4
Text SHA-256
7ff5d4e54bee9bfc45c3ab10822da681c3247b8098fad7afadacdf0bb14d4963

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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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