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2010-09-23
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Airworthiness Directives; Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes
Rules and Regulations
D09002ee1bdfb6e25
D09002ee1bdfb6e95
United States
Department of Transportation
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United States Government Agency or Subagency
United States
Federal Aviation Administration
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org
United States Government Agency or Subagency
This amendment revises Airworthiness Directive (AD) 98-19-15, which currently requires incorporating information into the Limitations Section of the airplane flight manual (AFM) that imposes a speed restriction and a minimum pilot requirement for Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes equipped with Barber- Colman pitch trim actuators, part number (P/N) 27-19008-001/-004 or P/N 27-19008-002/-005. Since AD 98-19-15 became effective, improved design pitch trim actuators have been developed that, when installed, will eliminate the speed restriction and minimum pilot requirements of the current AD. This AD requires incorporating these installations as a method of complying with the current AD. The actions specified by this AD are intended to lessen the possibility of airplane pitch up caused by mechanical failure of the pitch trim actuator, which could result in a pitch upset and structural failure of the airplane.
65 FR 1540
https://www.govinfo.gov/app/details/FR-2000-01-11/00-537
00-537
fr11ja00-4
RIN 2120-AA64
4910-13-U
Docket No. 98-CE-84-AD
Amendment 39-11507
AD 98-19-15 R1
https://www.govinfo.gov/app/details/FR-2000-01-11/00-537
https://www.govinfo.gov/content/pkg/FR-2000-01-11/html/00-537.htm
https://www.govinfo.gov/content/pkg/FR-2000-01-11/pdf/00-537.pdf
3 p.
1540
1542
65 FR 1540
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes; Federal Register Vol. 65, Issue
RULE
00-537
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2000-03-03
Docket No. 98-CE-84-AD
Amendment 39-11507
AD 98-19-15 R1
4910-13-U
00-537
Final rule.
This amendment revises Airworthiness Directive (AD) 98-19-15, which currently requires incorporating information into the Limitations Section of the airplane flight manual (AFM) that imposes a speed restriction and a minimum pilot requirement for Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes equipped with Barber- Colman pitch trim actuators, part number (P/N) 27-19008-001/-004 or P/N 27-19008-002/-005. Since AD 98-19-15 became effective, improved design pitch trim actuators have been developed that, when installed, will eliminate the speed restriction and minimum pilot requirements of the current AD. This AD requires incorporating these installations as a method of complying with the current AD. The actions specified by this AD are intended to lessen the possibility of airplane pitch up caused by mechanical failure of the pitch trim actuator, which could result in a pitch upset and structural failure of the airplane.
Effective March 3, 2000.
Mr. Werner G. Koch, Aerospace Engineer, FAA, Aircraft Certification Office, 2601 Meacham Boulevard, Fort Worth, Texas 76193-0150; telephone: (817) 222-5133; facsimile: (817) 222-5960.
Federal Register
Vol. 65, no. 7
Office of the Federal Register, National Archives and Records Administration
2000-01-11
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237 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2000-01-11
P0b002ee1809f6036
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr11ja00
https://www.govinfo.gov/app/details/FR-2000-01-11
https://www.govinfo.gov/content/pkg/FR-2000-01-11/pdf/FR-2000-01-11.pdf
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2010-09-23
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