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2019-05-08
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Special Conditions: Embraer Model EMB-550 Airplanes; Flight Envelope Protection: Normal Load Factor (g) Limiting
Rules and Regulations
D09002ee1bdb77222
D09002ee1bdb772f2
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
These amended special conditions are issued for Embraer Model EMB-550 airplanes. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is associated with an electronic flight control system that prevents the pilot from inadvertently or intentionally exceeding the positive or negative airplane limit load factor. 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.
84 FR 20021
https://www.govinfo.gov/app/details/FR-2019-05-08/2019-09398
2019-09398
fr08my19-2
4910-13-P
Docket No. FAA-2013-0772
Special Conditions No. 25-520A-SC
https://www.govinfo.gov/app/details/FR-2019-05-08/2019-09398
https://www.govinfo.gov/content/pkg/FR-2019-05-08/html/2019-09398.htm
https://www.govinfo.gov/content/pkg/FR-2019-05-08/pdf/2019-09398.pdf
Aircraft
Aviation Safety
Reporting and Recordkeeping Requirements
3 p.
20021
20023
84 FR 20021
Code of Federal Regulations
Title 14 Part 25
14 CFR Part 25
Special Conditions: Embraer Model EMB-550 Airplanes; Flight Envelope Protection: Normal Load Factor (g) Limiting; Federal Register Vol. 84, Issue
RULE
2019-09398
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2019-05-08
Docket No. FAA-2013-0772
Special Conditions No. 25-520A-SC
4910-13-P
2019-09398
Final special conditions.
These amended special conditions are issued for Embraer Model EMB-550 airplanes. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is associated with an electronic flight control system that prevents the pilot from inadvertently or intentionally exceeding the positive or negative airplane limit load factor. 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.
Effective May 8, 2019.
Joe Jacobsen, Airplane & Flight Crew Interface Section, AIR-671, Transport Standards Branch, Policy and Innovation Division, Aircraft Certification Service, Federal Aviation Administration, 2200 South 216th Street, Des Moines, Washington 98198; telephone and fax 206-231-3158; email joe.jacobsen@faa.gov.
Aircraft
Aviation Safety
Reporting and Recordkeeping Requirements
Special Conditions:
Embraer Model EMB-550 Airplanes; Flight Envelope Protection: Normal Load Factor (g) Limiting
,
joe.jacobsen@faa.gov
Federal Register
Vol. 84, no. 89
Office of the Federal Register, National Archives and Records Administration
2019-05-08
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243 p.
Table of Contents:
AE 2.7:
GS 4.107:
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https://www.govinfo.gov/app/details/FR-2019-05-08
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0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr08my19
https://www.govinfo.gov/app/details/FR-2019-05-08
https://www.govinfo.gov/content/pkg/FR-2019-05-08/pdf/FR-2019-05-08.pdf
https://www.govinfo.gov/content/pkg/FR-2019-05-08/xml/FR-2019-05-08.xml
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2019-05-08
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FR-2019-05-08
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FR
FR-2019-05-08
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