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Atlas / Aircraft / ELOS findings

ELOS AT10150IB-T-C-101

Current · Issued 01/14/2015 · FAA DRS

Graphical Exit Signs PDF ↗

14 CFR sections Project Other ELOS Special conditions Same CFR sections

14 CFR sections deviation applies to

§ 25.811
§ 25.812

Project

Finding #: AT10150IB-T-C-101
Applicant: Dassault Aviation
Make: Dassault Aviation
Model: Falcon 7X
Office: AIR-770: West Certification Branch LA

Other ELOS on this aircraft

ELOS AT19534IB-T-ESF-B25.251-01Equivalent Level of Safety (ELOS) Finding for Vibration and Buffeting
ELOS AT10962IB-T-D-41Equivalent Level of Safety (ELOS) Finding for Aisle Width Reduction
ELOS AT10266IB-T-SE-13INFORMATION: Equivalent Level of Safety (ELOS) Finding for High Altitude Takeoff and Landing Operation for the Dassault Aviation Model Falcon7X, FAA Project #AT10266IB-T
ELOS TD00818IB-T-SE-101Equivalent Level of Safety (ELOS) Finding for the Dassault Falcon 7X airplane modification M1015
ELOS TC0030IB-T-P-12Fuel tank
ELOS TC0030IB-T-P-5Primary display unit (PDU)

Special conditions on this aircraft

SC 25-751-SCSpecial Conditions: Dassault Aviation Model Falcon 7X Airplanes; Large Non-Structural Glass in the Passenger Compartment
SC 25-711-SCSpecial Conditions: Dassault Aviation, Model Falcon 7X Airplane; Non-Rechargeable Lithium Battery Installations

Same CFR sections

ELOS SA-02-2024-0018-C-2Equivalent Level of Safety (ELOS) Finding for Gulfstream Aerospace Corporation’s Project on Model G300, Project No. SA-02-2024-0018 - Emergency Exit Marker, Locator and Bulkhead/Divider Signs
ELOS PS13-1000-C-9Inside Passenger Door Operational Arrow Location and Color
ELOS AT5177AT-T-C-1-R3Equivalent Level of Safety Finding on Emergency Exit Marking, Locator and Bulkhead/Divider Signs; Revision to address bulkhead between overwing exits.
ELOS N0698ODA0077Equivalent Level of Safety (ELOS) Finding for Symbolic Exit Signs and Green Emergency Exit Instructions
ELOS ODA-2366-03-CS-1Equivalent Level of Safety (ELOS) Finding for Symbolic Exit Signs on a Model Bombardier CL-600-2D24 airplane, FAA Project ODA- 2556-01

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