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Atlas / Aircraft / ELOS findings

ELOS AT0012IB-T-P-12

Current · Issued 06/15/2010 · FAA DRS

Thrust reverser PDF ↗

14 CFR sections Project Other ELOS Special conditions Same CFR sections

14 CFR sections deviation applies to

§ 25.933

Project

Finding #: AT0012IB-T-P-12
Applicant: Dassault Aviation
Make: Dassault Aviation
Model: FALCON 2000EX
Office: AIR-770: West Certification Branch LA

Other ELOS on this aircraft

ELOS AT20300IB-T-ESF-B25.251-01Equivalent Level of Safety (ELOS) Finding for Vibration/Buffeting Compliance Criteria, Large Antenna Installation
ELOS AT10010IB-T-CI-101INFORMATION: Equivalent Level of Safety (ELOS) Finding for Seat Encroachment into the Emergency Exit Access on a Dassault Aviation Models Falcon7X, Falcon 2000EX and Falcon 900EX airplanes, FAA Project #AT10010IB-T
ELOS AT10121IB-T-C-101Emergency Exit Access
ELOS SP00843IB-T-C-1Type III and IV exits
ELOS AT0012IB-T-P-15Fire detection
ELOS AT0012IB-T-F-4INFORMATION: Equivalent Level of Safety (ELOS) Finding for Dassault s project on the Falcon 2000EX airplane, FAA Project # AT0012IB-T

Special conditions on this aircraft

SC 25-713-SCSpecial Conditions: Dassault Aviation Model Falcon 2000EX Airplanes; Non-Rechargeable Lithium Battery Installations
SC 25-608-SCSpecial Conditions: Dassault Aviation, Model Falcon 2000EX Airplanes, Head-Up Display (HUD) With Vision-System Video

Same CFR sections

ELOS TC0544IB-T-P-10Equivalent Level of Safety (ELOS) Finding for Flight Critical Thrust Reverser on Airbus Model A350-900, A350-1000 and A330-841, A330-941 (New Engine Option) airplanes, FAA Project Numbers TC0544IB-T, AT10383IB-T and AT10413IB-T.
ELOS TC00952IB-T-G-5-P-7Equivalent Level of Safety Finding for Flight Critical Thrust Reverser
ELOS PS12-0038-P-2-TREquivalent Level of Safety (ELOS) Finding for Flight Critical Thrust Reverser on Boeing Model 737-7/-8/-9/-8200/-10Airplanes, Project # PS12-0037, PS12-0038, PS12-0039, PS15-0560, and PS17-0010
ELOS AT5080AT-T-P-1 Rev. 2Flight Critical Thrust Reverser
ELOS AT-01-2015-0016-P-1-GVIIReverse Thrust Control and Indication

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