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Published 1999-05-11 · Federal Register document 99-11780

Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes

Publication summary

This action confirms the effective date of Airworthiness Directive (AD) 99-06-17, which applies to certain Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC-12/45 airplanes. AD 99-06-17 requires installing a support bracket and a cut-out relay for the second generator control unit. AD 99-06-17 also requires making all the wiring additions and adjustments necessary for the above-referenced installations. This AD was the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified in this AD are intended to prevent damage to electrical components because incorrectly connected cables or broken or damaged wires cause excessive voltages to the second generator, which could result in loss of electrical power during any phase of flight.

Why this record is shown

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
Source row
results[204]
Raw source SHA-256
e9a7378e7e7d30d51578560dc0677c56bb1fef0a9323224e2a0afe1544919217

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Recorded publication clauses

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Effective date printed in this edition
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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: adda11e21b6565855570e0c7fe48f187d3a00dca8040b26139df70094b7f583c. Source manifest: 21fed66fb851e32aec47c88ad55a52a939dc0586eaaddea72cb873f3da1ad447.

Official source · 1999-05-11

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 90 (Tuesday, May 11, 1999)]
[Rules and Regulations]
[Pages 25200-25201]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 99-11780]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99-CE-03-AD; Amendment 39-11081; AD 99-06-17]
RIN 2120-AA64


Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and 
PC-12/45 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) 99-06-17, which applies to certain Pilatus Aircraft Ltd. 
(Pilatus) Models PC-12 and PC-12/45 airplanes. AD 99-06-17 requires 
installing a support bracket and a cut-out relay for the second 
generator control unit. AD 99-06-17 also requires making all the wiring 
additions and adjustments necessary for the above-referenced 
installations. This AD was the result of mandatory continuing 
airworthiness information (MCAI) issued by the airworthiness authority 
for Switzerland. The actions specified in this AD are intended to 
prevent damage to electrical components because incorrectly connected 
cables or broken or damaged wires cause excessive voltages to the 
second generator, which could result in loss of electrical power during 
any phase of flight.

EFFECTIVE DATE: June 16, 1999.

FOR FURTHER INFORMATION CONTACT: Mr. Roman T. Gabrys, Aerospace 
Engineer, FAA, Small Airplane Directorate, 1201 Walnut, suite 900, 
Kansas City, Missouri 64106; telephone: (816) 426-6932; facsimile: 
(816) 426-2169.


[[Page 25201]]


SUPPLEMENTARY INFORMATION: The FAA published this direct final rule 
with request for comments in the Federal Register on March 23, 1999 (64 
FR 13882). 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 June 16, 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 May 4, 1999.
Michael Gallagher,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 99-11780 Filed 5-10-99; 8:45 am]
BILLING CODE 4910-13-P


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Source SHA-256
bf1fdb1b8e7f0a07bb557a756a6e5c33f401aba6447cb7897d7ade17b686e2c5
Text SHA-256
adda11e21b6565855570e0c7fe48f187d3a00dca8040b26139df70094b7f583c

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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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