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Atlas / Aircraft / ELOS findings

ELOS TC0030IB-T-SE-20

Current · Issued 06/26/2007 · FAA DRS

Environmental Control System (ECS) PDF ↗

14 CFR sections Project Other ELOS Special conditions Same CFR sections

14 CFR sections deviation applies to

§ 25.831

Project

Finding #: TC0030IB-T-SE-20
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 AT10150IB-T-C-101Graphical Exit Signs
ELOS TD00818IB-T-SE-101Equivalent Level of Safety (ELOS) Finding for the Dassault Falcon 7X airplane modification M1015
ELOS TC0030IB-T-P-12Fuel tank

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 TC8700AT-T-S-28 Rev. 1Equivalent Level of Safety (ELOS) Finding for Acceptable High Temperature Physiological Environment During Failure Conditions
ELOS PS05-0020-ES-3Equivalent Level of Safety (ELOS) Finding for an Acceptable High Temperature Physiological Environment during Failure Conditions on Boeing Models 777F, 747-8/-8F, and 737-7/-8/-9/-10/-8200 Airplanes, FAA Project Nos. PS05-0020, PS05-0211, PS05-0212, PS12-0037, PS12-0038, PS12-0039, PS15-0560, and PS17-0010
ELOS AT10219IB-T-S-34Cabin Ventilation Humidity Requirement
ELOS TC0777IB-T-S-25Acceptable High Temperature Physiological Environment During Failure Conditions
ELOS TC-01-2010-0024-S-14Acceptable High Temperature Physiological Environment During Failure Conditions
LI 2007-023Whatley

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