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Atlas / Aircraft / ELOS findings

ELOS ACE-08-12

Current · Issued 06/24/2008 · FAA DRS

Turning Flight and Accelerated Turning Stalls PDF ↗

14 CFR sections Project Other ELOS Same CFR sections

14 CFR sections deviation applies to

§ 23.201
§ 23.203

Project

Finding #: ACE-08-12
Applicant: Eclipse Aviation
Make: Eclipse Aviation Corporation
Model: EA500
Office: AIR-770: West Certification Branch LA

Other ELOS on this aircraft

ELOS ACE-07-04Airspeed indicator
ELOS ACE-06-05Installation of Automatic Power Reserve (APR) System
ELOS ACE-06-01Airspeed indicator (white arc)
ELOS ACE-05-35Storage battery
ELOS ACE-05-36Airspeed indicating (water drainage)
ELOS ACE-05-34Dynamic stabiltiy

Same CFR sections

ELOS TC00607CE-A-F-3INFORMATION: Equivalent Level of Safety (ELOS) Finding for Pilatus Aircraft, Ltd., Model PC-24, Use of 1-g Stall Speed Criteria, Project TC00607CE-A
ELOS TC11773SE-A-F-1INFORMATION: Equivalent Level of Safety (ELOS) Finding for Epic Aircraft, LLC., Model E1000 Airplane, Use of Stick Pusher/Shaker System in lieu of compliance with Spin Recovery Requirements, FAA Project # TC11773SE-A
ELOS ACE-15-08INFORMATION: Equivalent Level of Safety (ELOS) Finding for Honda Aircraft Company, Model HA-420, Use of 1-g Stall Speed in lieu of Minimum Speed in Stall as a Basis for Determining Compliance, Project #: TC9438AT-A
ELOS ACE-05-04Use of 1-g Stall Speed Criteria Instead of Minimum Speed in the Stall
ELOS ACE-98-2Stalls and spins

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