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Atlas / Aircraft / ELOS findings

ELOS ACE-09-03

Current · Issued 02/24/2009 · FAA DRS

Longitudinal Control During Takeoff Flap PDF ↗

14 CFR sections Project Other ELOS Same CFR sections

14 CFR sections deviation applies to

§ 23.145

Project

Finding #: ACE-09-03
Applicant: Aero Twin, Inc.
Make: Cessna Aircraft Company
Model: 208B
Office: AIR-770: West Certification Branch LA

Other ELOS on this aircraft

ELOS ST02289AC-A-F-1INFORMATION: Equivalent Level of Safety (ELOS) Finding for Aircraft Structures International Corporation STC Cessna Model 208 Airplane, Longitudinal Control Force During Takeoff Flap Retraction, FAA Project #ST02289AC-A
ELOS ACE-11-01AStall Warning and Ice Protection
ELOS ACE-08-19AStall Warning
ELOS ACE-13-06Longitudinal Control
ELOS ACE-08-06AElectronic Engine Instrument Display
ELOS ACE-11-01Stall Warning for Model 208B Airplane

Same CFR sections

ELOS AT13893AT-A -F-1Equivalent Level of Safety (ELOS) Finding for Piper Aircraft Inc., Models PA-46-600TP and PA-46-701TP, Control Forces
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 ST02289AC-A-F-1INFORMATION: Equivalent Level of Safety (ELOS) Finding for Aircraft Structures International Corporation STC Cessna Model 208 Airplane, Longitudinal Control Force During Takeoff Flap Retraction, FAA Project #ST02289AC-A
ELOS AT13893AT-A-F-1INFORMATION: Equivalent Level of Safety (ELOS) Finding for Piper Aircraft Inc., Model PA-46-600TP, Control Forces, FAA Project # AT13893AT-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

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