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2010-09-24
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Special Conditions: Rockwell Collins; Boeing Model 737-300/-400/- 500 Series Airplanes; High-Intensity Radiated Fields (HIRF)
Rules and Regulations
D09002ee1bdfbec18
D09002ee1bdfbecdf
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 Boeing Model 737-300/- 400/-500 series airplanes modified by Rockwell Collins. These modified airplanes will have a novel or unusual design feature associated with the Rockwell Collins Multi-Mode Receiver (MMR) System. 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.
64 FR 47649
https://www.govinfo.gov/app/details/FR-1999-09-01/99-22751
99-22751
fr01se99-1
4910-13-U
Docket No. NM-163
Special Conditions No. 25-147-SC
https://www.govinfo.gov/app/details/FR-1999-09-01/99-22751
https://www.govinfo.gov/content/pkg/FR-1999-09-01/html/99-22751.htm
https://www.govinfo.gov/content/pkg/FR-1999-09-01/pdf/99-22751.pdf
3 p.
47649
47651
64 FR 47649
Code of Federal Regulations
Title 14 Part 25
14 CFR Part 25
Special Conditions: Rockwell Collins; Boeing Model 737-300/-400/- 500 Series Airplanes; High-Intensity Radiated Fields (HIRF); Federal Register Vol. 64, Issue
RULE
99-22751
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
1999-08-23
1999-10-01
Docket No. NM-163
Special Conditions No. 25-147-SC
4910-13-U
99-22751
Final special conditions; request for comments.
These special conditions are issued for Boeing Model 737-300/- 400/-500 series airplanes modified by Rockwell Collins. These modified airplanes will have a novel or unusual design feature associated with the Rockwell Collins Multi-Mode Receiver (MMR) System. 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 August 23, 1999. Comments must be received on or before October 1, 1999.
Mark Quam, FAA, Standardization Branch, ANM-113, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98055-4056; telephone (425) 227-2145; facsimile (425) 227-1149.
Federal Register
Vol. 64, no. 169
Office of the Federal Register, National Archives and Records Administration
1999-09-01
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Table of Contents:
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https://www.govinfo.gov/app/details/FR-1999-09-01
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https://www.govinfo.gov/app/details/FR-1999-09-01
https://www.govinfo.gov/content/pkg/FR-1999-09-01/pdf/FR-1999-09-01.pdf
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47649
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2010-09-24
2023-05-05
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FR-1999-09-01
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