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United States
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FR
Regulatory Information
2019_register
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2019-12-14
article
Airworthiness Directives; Bombardier, Inc., Airplanes
Proposed Rules
D09002ee1bdb66596
D09002ee1bdb6667f
United States
Department of Transportation
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org
United States Government Agency or Subagency
United States
Federal Aviation Administration
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org
United States Government Agency or Subagency
The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. This proposed AD was prompted by a report that cracking was discovered in a channel within a structural support member for the rudder quadrant, rudder feel unit assembly, and environmental control system due to fatigue. This proposed AD would require repetitive inspections of the rudder quadrant box assembly for any cracking, and modification of the rudder quadrant box assembly. The FAA is proposing this AD to address the unsafe condition on these products.
84 FR 68370
https://www.govinfo.gov/app/details/FR-2019-12-16/2019-25719
2019-25719
fr16de19-19
RIN 2120-AA64
4910-13-P
Docket No. FAA-2019-0876
Product Identifier 2019-NM-070-AD
https://www.govinfo.gov/app/details/FR-2019-12-16/2019-25719
https://www.govinfo.gov/content/pkg/FR-2019-12-16/html/2019-25719.htm
https://www.govinfo.gov/content/pkg/FR-2019-12-16/pdf/2019-25719.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
5 p.
68370
68374
84 FR 68370
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes; Federal Register Vol. 84, Issue
PRORULE
2019-25719
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2020-01-30
Docket No. FAA-2019-0876
Product Identifier 2019-NM-070-AD
4910-13-P
2019-25719
Notice of proposed rulemaking (NPRM).
The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. This proposed AD was prompted by a report that cracking was discovered in a channel within a structural support member for the rudder quadrant, rudder feel unit assembly, and environmental control system due to fatigue. This proposed AD would require repetitive inspections of the rudder quadrant box assembly for any cracking, and modification of the rudder quadrant box assembly. The FAA is proposing this AD to address the unsafe condition on these products.
The FAA must receive comments on this proposed AD by January 30, 2020.
Andrea Jimenez, Aerospace Engineer, Airframe and Mechanical Systems Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7330; fax 516-794-5531; email 9-avs-nyaco-cos@faa.gov.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
Bombardier, Inc., Airplanes,
9-avs-nyaco-cos@faa.gov
thd.crj@aero.bombardier.com
https://www.bombardier.com
https://www.regulations.gov
Federal Register
Vol. 84, no. 241
Office of the Federal Register, National Archives and Records Administration
2019-12-16
continuing
daily
deposited
born digital
465 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2019-12-16
P0b002ee1a414091f
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr16de19
https://www.govinfo.gov/app/details/FR-2019-12-16
https://www.govinfo.gov/content/pkg/FR-2019-12-16/pdf/FR-2019-12-16.pdf
https://www.govinfo.gov/content/pkg/FR-2019-12-16/xml/FR-2019-12-16.xml
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2019-12-14
2023-04-28
FR-2019-12-16
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FR-2019-12-16
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