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Atlas / Aircraft / ELOS findings

ELOS ST4349WI-T-A-1

Current · Issued 02/01/2007 · FAA DRS

Japan Tanker Tranport PDF ↗

14 CFR sections Project Other ELOS Same CFR sections

14 CFR sections deviation applies to

§ 25.613

Project

Finding #: ST4349WI-T-A-1
Applicant: Boeing
Make: Boeing Company, The
Model: 767-200 Series
Office: AIR-770: West Certification Branch LA

Other ELOS on this aircraft

ELOS ST06344WI-T-P-1, Revision CThis is a reuse ELOS Memorandum for FAA Project # SA06646WI-T, which adds the Boeing Model 767-200 series aircraft to STC ST01882WI. This ELOS was previously reused for FAA Project # SA06549WI-T, which added the Boeing 767- 300 series aircraft to this STC.
ELOS ST06344WI-T-P-1, Revision BEquivalent Level of Safety (ELOS) Finding for Powerplant Instrumentation for RCI LDS-2100 Installation on Boeing Models 767-300F, 767-300 Series and 767-200 Series Aircraft, FAA Project # ST06344WI-T SA06549WI-T, and SA06646WI-T
ELOS ST02844AC-T-F-1Vibration and Buffeting Requirements for External Modifications
ELOS SA06180WI-T-P-1Equivalent Level of Safety (ELOS) Finding for Powerplant Instrumentation for RCI LDS-2100 Installation on Boeing 767-200 and 767-300F Series Aircraft Equipped with General Electric or Pratt & Whitney Engines, FAA Project # SA06180WI-T
ELOS SA06091WI-T-P-1Equivalent Level of Safety (ELOS) Finding for Powerplant Instrumentation for RCI LDS-2100 installation
ELOS TD7075SE-T-C-1Finding for the Boeing 767-200/300 Type III Exit Accessibility

Same CFR sections

ELOS AT3907SE-T-A-15INFORMATION: Equivalent Level of Safety (ELOS) Finding for Material Design Values on Boeing Models 777-200LR/-300ER and 737-600/-700/-700C/-800/-900, FAA Project Nos. AT3907SE-T, AT3908SE-T, AT0328SE-T, AT2720SE-T and AT2721SE-T
ELOS AT3907SE-T-A-15Boeing project on Models 777-200LR and 777-300ER
ELOS ST5116AT-T-A-1Material Design Values
ELOS ST3073WI-T-A-2Boeing Model 767-200 Tanker / Transport Combi, FAA Projects ST3067WI-T, ST3068WI-T, ST3069WI-T, ST3072WI-T, ST3482WI-T, ST3073WI-T
ELOS TD5409SE-T-A-1Higher maximum takeoff gross weight and additional fuel capacity.

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