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2010-09-24
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Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes
Rules and Regulations
D09002ee1be35ccf4
D09002ee1be35d18f
United States
Department of Transportation
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United States Government Agency or Subagency
United States
Federal Aviation Administration
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United States Government Agency or Subagency
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.
64 FR 25200
https://www.govinfo.gov/app/details/FR-1999-05-11/99-11780
99-11780
fr11my99-5
RIN 2120-AA64
4910-13-P
Docket No. 99-CE-03-AD
Amendment 39-11081
AD 99-06-17
https://www.govinfo.gov/app/details/FR-1999-05-11/99-11780
https://www.govinfo.gov/content/pkg/FR-1999-05-11/html/99-11780.htm
https://www.govinfo.gov/content/pkg/FR-1999-05-11/pdf/99-11780.pdf
2 p.
25200
25201
64 FR 25200
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes; Federal Register Vol. 64, Issue
RULE
99-11780
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Docket No. 99-CE-03-AD
Amendment 39-11081
AD 99-06-17
4910-13-P
99-11780
Direct final rule; confirmation of effective date.
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.
June 16, 1999.
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.
Federal Register
Vol. 64, no. 90
Office of the Federal Register, National Archives and Records Administration
1999-05-11
continuing
daily
deposited
born digital
238 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-1999-05-11
P0b002ee180a5a63c
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr11my99
https://www.govinfo.gov/app/details/FR-1999-05-11
https://www.govinfo.gov/content/pkg/FR-1999-05-11/pdf/FR-1999-05-11.pdf
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DGPO
2010-09-24
2023-05-17
FR-1999-05-11
machine generated
eng
FR
FR-1999-05-11
64
90