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2010-09-23
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Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes
Rules and Regulations
D09002ee1bdefa2b8
D09002ee1bdefa959
United States
Department of Transportation
originator
org
United States Government Agency or Subagency
United States
Federal Aviation Administration
originator
org
United States Government Agency or Subagency
This amendment adopts a new airworthiness directive (AD) that is applicable to certain EMBRAER Model EMB-135 and -145 series airplanes. This action requires repetitive inspections (tests) of the actuator clutches of the primary and backup pitch trim systems of the horizontal stabilizer for proper pitch trim indications, and replacement of the actuator, if necessary. This action is necessary to prevent loss of pitch trim command during the takeoff and climb phase of flight due to improper set point of the actuator clutches, which could result in high pitch control forces and consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.
67 FR 21567
https://www.govinfo.gov/app/details/FR-2002-05-01/02-10246
02-10246
fr01my02-3
RIN 2120-AA64
4910-13-P
Docket No. 2002-NM-68-AD
Amendment 39-12730
AD 2002-08-18
https://www.govinfo.gov/app/details/FR-2002-05-01/02-10246
https://www.govinfo.gov/content/pkg/FR-2002-05-01/html/02-10246.htm
https://www.govinfo.gov/content/pkg/FR-2002-05-01/pdf/02-10246.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
21567
21569
67 FR 21567
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes; Federal Register Vol. 67, Issue
RULE
02-10246
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2002-05-16
Docket No. 2002-NM-68-AD
Amendment 39-12730
AD 2002-08-18
4910-13-P
02-10246
Final rule; request for comments.
This amendment adopts a new airworthiness directive (AD) that is applicable to certain EMBRAER Model EMB-135 and -145 series airplanes. This action requires repetitive inspections (tests) of the actuator clutches of the primary and backup pitch trim systems of the horizontal stabilizer for proper pitch trim indications, and replacement of the actuator, if necessary. This action is necessary to prevent loss of pitch trim command during the takeoff and climb phase of flight due to improper set point of the actuator clutches, which could result in high pitch control forces and consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.
Effective May 16, 2002.
Robert Capezzuto, Aerospace Engineer, Systems and Flight Test Branch, ACE-116A, FAA, Atlanta Aircraft Certification Office, One Crown Center, 1895 Phoenix Boulevard, suite 450, Atlanta, Georgia 30349; telephone (770) 703-6071; fax (770) 703- 6097.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Empresa Brasileira de Aeronautica S.A. (EMBRAER),
9-anm-iarcomment@faa.gov
Federal Register
Vol. 67, no. 84
Office of the Federal Register, National Archives and Records Administration
2002-05-01
continuing
daily
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born digital
426 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2002-05-01
P0b002ee1809ecf81
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr01my02
https://www.govinfo.gov/app/details/FR-2002-05-01
https://www.govinfo.gov/content/pkg/FR-2002-05-01/pdf/FR-2002-05-01.pdf
https://www.govinfo.gov/content/pkg/FR-2002-05-01/xml/FR-2002-05-01.xml
fdlp
21559
21974
DGPO
2010-09-23
2023-05-04
FR-2002-05-01
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eng
FR
FR-2002-05-01
67
84