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2010-09-23
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Special Conditions: Bombardier Aerospace Model CL-600-2D24 (RJ900) Airplane; Sudden Engine Stoppage
Rules and Regulations
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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
These special conditions are issued for the Bombardier Aerospace Model CL-600-2D24 (RJ900) airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes, associated with engine size and torque load which affects sudden engine stoppage. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
67 FR 64309
https://www.govinfo.gov/app/details/FR-2002-10-18/02-26584
02-26584
fr18oc02-1
4910-13-P
Docket No. NM233
Special Conditions No. 25-217-SC
https://www.govinfo.gov/app/details/FR-2002-10-18/02-26584
https://www.govinfo.gov/content/pkg/FR-2002-10-18/html/02-26584.htm
https://www.govinfo.gov/content/pkg/FR-2002-10-18/pdf/02-26584.pdf
Aircraft
Aviation Safety
Reporting and Recordkeeping Requirements
3 p.
64309
64311
67 FR 64309
Code of Federal Regulations
Title 14 Part 25
14 CFR Part 25
Special Conditions: Bombardier Aerospace Model CL-600-2D24 (RJ900) Airplane; Sudden Engine Stoppage; Federal Register Vol. 67, Issue
RULE
02-26584
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2002-10-04
2002-11-18
Docket No. NM233
Special Conditions No. 25-217-SC
4910-13-P
02-26584
Final special conditions; request for comments.
These special conditions are issued for the Bombardier Aerospace Model CL-600-2D24 (RJ900) airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes, associated with engine size and torque load which affects sudden engine stoppage. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
The effective date of these special conditions is October 4, 2002. Comments must be received on or before November 18, 2002.
John Piccola, FAA Standardization Branch, ANM-113, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98055-4056; telephone (425) 227-1509; facsimile (425) 227-1149.
Aircraft
Aviation Safety
Reporting and Recordkeeping Requirements
Airworthiness standards:
Special conditions
Bombardier Aerospace Model CL-600-2D24 (RJ900) series airplanes,
Federal Register
Vol. 67, no. 202
Office of the Federal Register, National Archives and Records Administration
2002-10-18
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Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2002-10-18
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0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr18oc02
https://www.govinfo.gov/app/details/FR-2002-10-18
https://www.govinfo.gov/content/pkg/FR-2002-10-18/pdf/FR-2002-10-18.pdf
https://www.govinfo.gov/content/pkg/FR-2002-10-18/xml/FR-2002-10-18.xml
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DGPO
2010-09-23
2023-05-04
FR-2002-10-18
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FR
FR-2002-10-18
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