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Atlas / Aircraft / ELOS findings

ELOS TC0067-AT-S-7

Current · Issued 11/03/2005 · FAA DRS

Ventilation System PDF ↗

14 CFR sections Project Other ELOS Same CFR sections

14 CFR sections deviation applies to

§ 25.831

Project

Finding #: TC0067-AT-S-7
Applicant: Gulfstream Aerospace
Make: Gulfstream Aerospace LP
Model: G150
Office: AIR-770: West Certification Branch LA

Other ELOS on this aircraft

ELOS GACD-05-11-DAS-C-1Emergency Exit Marker
ELOS ST10438AT-T-F-9Landing surface
ELOS TC0067-AT-P-6Gulfstream Aerospace LP Amended Type Certificate Project on Model G150
ELOS TC0067-AT-P-2Gulfstream Aerospace LP Amended Type Certificate project on Model G150
ELOS TC0067-AT-P-7Auxiliary Power Unit (APU)
ELOS TC0067-AT-F-7Maneuvering stability and controllability in a mistrim condition

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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