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2010-09-23
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Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Rules and Regulations
D09002ee1bde6a4c4
D09002ee1bde6abe2
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
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This AD requires repetitive inspections for cracks, sealant damage, and corrosion of the main fittings of the main landing gear (MLG), and corrective actions if necessary. This AD is prompted by a report of a cracked main fitting of the MLG. We are issuing this AD to detect and correct fatigue cracking of the main fitting of the MLG and consequent failure of the main fitting, which could result in the collapse of the MLG.
69 FR 59790
https://www.govinfo.gov/app/details/FR-2004-10-06/04-22266
04-22266
fr06oc04-8
RIN 2120-AA64
4910-13-P
Docket No. FAA-2004-19229
Directorate Identifier 2004-NM-195-AD
Amendment 39-13814
AD 2004-20-09
https://www.govinfo.gov/app/details/FR-2004-10-06/04-22266
https://www.govinfo.gov/content/pkg/FR-2004-10-06/html/04-22266.htm
https://www.govinfo.gov/content/pkg/FR-2004-10-06/pdf/04-22266.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
4 p.
59790
59793
69 FR 59790
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes; Federal Register Vol. 69, Issue
RULE
04-22266
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2004-10-21
Docket No. FAA-2004-19229
Directorate Identifier 2004-NM-195-AD
Amendment 39-13814
AD 2004-20-09
4910-13-P
04-22266
Final rule; request for comments.
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This AD requires repetitive inspections for cracks, sealant damage, and corrosion of the main fittings of the main landing gear (MLG), and corrective actions if necessary. This AD is prompted by a report of a cracked main fitting of the MLG. We are issuing this AD to detect and correct fatigue cracking of the main fitting of the MLG and consequent failure of the main fitting, which could result in the collapse of the MLG.
Effective October 21, 2004.
Technical information: Serge Napoleon, Aerospace Engineer, Airframe and Propulsion Branch, ANE-171, FAA, New York Aircraft Certification Office, 1600 Stewart Avenue, suite 410, Westbury, New York 11590; telephone (516) 228-7312; fax (516) 794-5531.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Bombardier,
marcia.walters@faa.gov
faa.gov/language
http://dms.dot.gov
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
http://www.plainlanguage.gov
http://www.regulations.gov
Federal Register
Vol. 69, no. 193
Office of the Federal Register, National Archives and Records Administration
2004-10-06
continuing
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330 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2004-10-06
P0b002ee18096f7b7
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr06oc04
https://www.govinfo.gov/app/details/FR-2004-10-06
https://www.govinfo.gov/content/pkg/FR-2004-10-06/pdf/FR-2004-10-06.pdf
https://www.govinfo.gov/content/pkg/FR-2004-10-06/xml/FR-2004-10-06.xml
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60076
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2010-09-23
2023-05-03
FR-2004-10-06
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FR
FR-2004-10-06
69
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