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2010-09-23
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Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes
Rules and Regulations
D09002ee1bdfb4507
D09002ee1bdfb45bd
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 amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC- 12/45 airplanes. This AD requires replacing the stick pusher capstan and the stick pusher servo with parts of improved design. The AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified by this AD are intended to prevent improper operation of the stick pusher system caused by the existing design configuration, which could result in loss of control of the airplane during a stall.
65 FR 5428
https://www.govinfo.gov/app/details/FR-2000-02-04/00-2399
00-2399
fr04fe00-11
RIN 2120-AA64
4910-13-P
Docket No. 99-CE-64-AD
Amendment 39-11549
AD 2000-02-31
https://www.govinfo.gov/app/details/FR-2000-02-04/00-2399
https://www.govinfo.gov/content/pkg/FR-2000-02-04/html/00-2399.htm
https://www.govinfo.gov/content/pkg/FR-2000-02-04/pdf/00-2399.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
2 p.
5428
5429
65 FR 5428
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. 65, Issue
RULE
00-2399
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2000-03-27
Docket No. 99-CE-64-AD
Amendment 39-11549
AD 2000-02-31
4910-13-P
00-2399
Final rule.
This amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC- 12/45 airplanes. This AD requires replacing the stick pusher capstan and the stick pusher servo with parts of improved design. The AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified by this AD are intended to prevent improper operation of the stick pusher system caused by the existing design configuration, which could result in loss of control of the airplane during a stall.
Effective March 27, 2000.
Mr. Roman T. Gabrys, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4141; facsimile: (816) 329- 4090.
Air Transportation
Aircraft
Aviation Safety
Safety
Federal Register
Vol. 65, no. 24
Office of the Federal Register, National Archives and Records Administration
2000-02-04
continuing
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335 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2000-02-04
P0b002ee1809f07af
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr04fe00
https://www.govinfo.gov/app/details/FR-2000-02-04
https://www.govinfo.gov/content/pkg/FR-2000-02-04/pdf/FR-2000-02-04.pdf
https://www.govinfo.gov/content/pkg/FR-2000-02-04/xml/FR-2000-02-04.xml
fdlp
5407
5731
DGPO
2010-09-23
2023-05-05
FR-2000-02-04
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FR
FR-2000-02-04
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