曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

􀂌 Cockpit Controls (side-stick controllers and levers): SKF Aerospace.
HONEYWELL AEROSPACE, Glendale, AZ, USA February 2005 – present
System Safety Engineer in Avionics and Flight Controls – Consultant (telework)
􀂌 Produced the Fault Tree Analysis (FTA) for the primary flight controls of the Boeing 787 Fly-By-
Wire system Flight Control Electronic (FCE), which also comprises the autoflight function.
􀂌 Wrote associated FCE System Safety Analysis (SSA) documentation.
􀂌 Helped writing FCE system safety guidelines and plans.
􀂌 Wrote Preliminary System Safety Analysis (PSSA) on related Honeywell research activities for
advanced fault tolerant Fly-By-Wire systems (Digital Flight Control System (DFCS) project with
NASA).
􀂌 Wrote System Safety Analysis (SSA) for the Honeywell KSG7200 Air Data Attitude Heading
Reference System (ADAHRS) airborne on Dassault F7X and Pilatus PC12 planes.
􀂌 Produced the Pilatus PC12 Preliminary Common Mode Analysis (PCMA) of the Honeywell EPIC
Automatic Flight Control System (AFCS).
􀂌 Updated the System Safety Analysis (SSA) previously created for Primus EPIC AFCS and ACAC
ARJ21.
SMITHS AEROSPACE (now GE Aviation) @ BOEING, Everett, WA, USA January 2005 – July 2005
System Safety Engineer for the Boeing 787 Landing Gear Control System
􀂌 Produced the Preliminary System Safety Analyses (PSSA) for the Boeing 787 Brake System and
Nose Wheel Steering.
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HONEYWELL AEROSPACE, Glendale, AZ, USA August 2001 – July 2003
System Safety Engineer in Avionics and Flight Controls February 2004 – January 2005
􀂌 Responsible for the production of the Preliminary System Safety Analysis for the fly-by-wire
controls of the ARJ21 regional jet of China’s AVIC I Commercial Aircraft Co. (ACAC).
􀂌 Responsible for the production of certification documentation: System Safety Analyses (SSA)
and/or Common Mode Analyses (CMA) on the Primus EPIC AFCS for one helicopter
(AgustaWestland AW139) and the following fixed wing aircrafts:
- Embraer ERJ170/175/190/195,
- Dornier Do728 (discontinued),
- Gulfstream G500, G550,
- Dassault Falcon F900EX EASy, F2000 EASy, F7X,
- Raytheon Hawker 4000 Horizon,
- Cessna Citation Sovereign.
The AFCS is highly integrated and typically provides the following functions: autopilot, flight
director, yaw damper, stall warning & stall protection, auto-throttle, pitch autotrim, and Mach trim.
􀂌 Wrote safety documentation to FAA / EASA system safety regulation (FAR/JAR 25.1309), using
guidance provided by SAE ARP-4761, and SAE ARP-4754.
􀂌 Derived software and hardware design assurance levels as per RTCA DO-178B and RTCA DO-
254 to support design activities.
􀂌 Used Matlab Simulink to analyze control laws and propose design improvements, when required.
BOMBARDIER AEROSPACE, Montréal, Canada September 2000 - August 2001
System Safety, Reliability and Maintainability Engineer
􀂌 System Safety Engineer, responsible in charge of the secondary flight controls (Pitch trim /
Horizontal Stabilizer, Spoilers, Flaps) and the electrical power generation system for the
Continental Business Jet.
􀂌 Responsible for the production or review of the following Safety documentation:
- Fault Tree Analysis (FTA),
- System Safety Analysis (SSA),
- Failure Mode Effect and Criticality Analysis (FMECA),
- Functional Hazard Analysis (FHA),
- Fire Hazard Analysis,
􀂌 Involved with Airworthiness Authorities (Transport Canada) regarding the Safety demonstration of
Airworthiness as per JAR/FAR Part 25 (essentially § 25.1309) for the above systems.
􀂌 Co-ordinate Safety activities with partners in Europe and in U.S. (Moog, E.C.E, Liebherr).
SEXTANT AVIONIQUE (now THALES), Toronto, Canada January 1997 - February 2000
Avionics System Safety & Reliability Engineer
􀂌 Responsible for Safety & Reliability certification of the avionics suite on the Bombardier
Aerospace DASH 8Q400 regional Turboprop aircraft (more than 100 LRUs including the
following flight controls: Stall Protection System and Autopilot).
􀂌 Negotiated with Bombardier and Transport Canada (TCA) with regard to Safety & Reliability
contractual requirements and Safety guidelines.
􀂌 Produced most of the Avionics Safety & Reliability documentation from the preliminary design to
the final certification (e.g. system FMECA, Software Safety Level Assessment, Fault Tree
Analysis and System Safety Analysis, MMEL consolidation, Dispatch Analysis, etc.).
􀂌 Presented analysis results to the Airworthiness Authorities (Transport Canada) or their
　
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