AUGUSTINE G. CAMPOS
1158 Huntington Place
Manteca, California 95336
(209) 239-5853 / cell (209) 679-7541
agc3737[at]yahoo.com
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PROFESSIONAL EXPERIENCE
Field Service Supervisor: GoodCents SOLUTIONS, March 2007 to June 2009
Supervise 15-30 Electronics Field Technicians. Responsible for implementation of load management installation program. High voltage 240 vac, 120vac and low voltage 24vac control. Contracted by PGE for Smart AC program. Successfully completed 250,000 installations in first two years of program.
Engine Accessory/Electronic Shop: AERO TURBINE January 2003 to March 2007
Responsible for the production of engine accessories and electronic parts.
This includes all phases of overhaul, operational checks, troubleshooting, repair, disassembly and assembly. Plan monthly work schedule. Requisition parts and supplies. Solve production problems. Track workload process efficiency.
Electrician: SELF EMPLOYED April 2002 to January 2003
Perform all phases of residential electrical work. Installation, repair and troubleshooting.
Radio Electronic Mechanic: UNITED AIRLINES, August 1990 to April 2002
Perform aircraft line maintenance checks and repairs of Avionics systems, engine and hydraulic systems, air conditioning systems, fuel quantity, ADC, engine instrument systems, communication systems, all lighting assemblies and lighting systems, passenger entertainment and passenger cabin systems. Qualified category 3 Autopilot on B737 aircraft Maintained and troubleshot all systems using wire diagrams, schematics, maintenance and repair manuals, engineering drawings and instructions. Test aircraft electrical, electronic instrument, and pneumatic systems using manual or automatic test devices. Repair and replace wiring and conduit, connectors and plugs and all parts associated with above systems.
Avionics Mechanic: PAN AM AIRLINES, May 1989 to August 1990
Analyze aircraft electrical, pneumatic and hydraulic systems for normal operation
and to determine airworthiness impact and compliance with Federal Air Regulations. Check for normal operation using approved check lists and maintenance manuals. Perform checks using approved ramp test sets, built in self test circuits and reading on board computer analysis. Repair and/or replace component or subsystem at fault. Inspect and test repair for release and airworthiness.
Relief Lead Avionics Mechanic: PAN AM AIRLINES, May 1989 to August 1990
Provide leadership to the working group, layout, control, quantity and quality of work produced. Train the group in related technical information, job procedures, safety and general shop practices. Prepare and process all forms required in conjunction with work assigned.
PROFESSIONAL EXPERIENCE (con’t)
Radio Electronic Mechanic: WORLD AIRWAYS, January 1987 to April 1987
Perform aircraft overhaul and line maintenance checks of complex Avionics systems, engine and hydraulic systems, air conditioning systems, fuel quantity, ADC, engine instrument systems, and communication systems to journey level. Circuit tested aircraft electrical systems involving numerous pieces of test equipment. Repair and replace wiring and conduit, connectors, plugs and all components associated with above systems. Certified to run DC-10 flight engineer's panel during routine engine maintenance checks.
Avionics Instrument Mechanic: UNITED STATES AIR FORCE, 1978 to 1984
Install, maintain, troubleshoot and repair Avionic electro-mechanical instrument systems and automatic flight control systems. Perform aircraft systems line and bench work. Perform all launch/recovery operations, functional checks and repairs. Supervise work of subordinates and administer on-the-job training. Train newcomers on flight line navigation, capacitive liquid quantity indicating systems, pilot static and central air data computer systems, flight control systems and engine instrumentation. Troubleshoot and repair test equipment.
Federal Communication Commission
General Radio Telephone Operator license
RELATED TRAINING AND EDUCATION
Avionics Instrument System Special Course (612 hours)
Avionics Instrument Technician Course (162 hours)
High Reliability Soldering Course (60 hours)
Fundamentals of Solid State Circuits
Engine Instrument Maintenance
Flt/Nav Instrument Maintenance
Basic Electronics Principles
Vacuum Tube Principles
SYSTEMS MAINTAINED
Boeing 727, 737, 747, 767
Collins ADF system 51Y4 Collins ATC system 621A3
Bendix air data computer system Inertial navigation system
Ground proximity warning system Collins HF transceiver
Selective calling system decoder Bendix maker beacon system
Emergency lighting system Power distribution system
RCA weather radar AVQ30 system Cabin pressurization system
Air-conditioning system Passenger Entertainment system
Pneumatic systems Hydraulic systems
Brake temperature/auto braking systems Flight control position indicators
Performance management system Auxiliary power unit system
Anti-skid system Cargo systems
Aural warning system Auto pilot/flight director control system
Critical engine monitoring Fuel pressure/temperature
Oil pressure/temperature Fuel Quantity
Fuel flow/fuel used Fire warning
Cockpit instruments Horizontal Situation indicator
Magnetic compass system Mach/airspeed indicator
Attitude director indicator Standby compass
Vertical speed indicator Sundstrand cockpit voice recorder 93A100-82
Altimeter King distance measuring equipment KDM7000
Radio magnetic indicator Bendix low range radio altimeter 2067631-5114
Airbus A300
Air-conditioning Air bleed
Cabin temperature Cabin ventilation
Yaw damper/pitch trim systems Interphone communications
Cockpit voice recorder DC power generation
AC electrical power distribution Fire warning
Low speed aileron Fuel used/fuel pressure
Hydraulic quantity/pressure Ice and rain protection
Master warning Landing gear control and indication
Brake temperature Heading and attitude system
Horizontal situation indicator Automatic direction finder
Marker beacon receiver Wing anti-ice system monitoring and Operation
Distance measuring equipment Instrument landing system
Radio altimeter Angel of attack (test & monitoring)
Air data systems Attitude director indicator
Pneumatic controls Door warning
Critical engine monitoring N1 rpm/N2 RPM
Exhaust gas temperature Nacelle temperature
Engine vibration pickup Engine starting
Reverser monitoring logic Galley and cabin service control
Oil pressure, temperature, quantity Bleed valve control & monitoring
Airbus A310
VOR/DME navigation system Altimeter Indicator
VOR/ILS navigation system Vertical speed indicator
Auto brake operation and control Mach/airspeed Indicator
Cabin pressurization Landing Gear
Autopilot/flight director system Fire Warning
Spoiler/speed brakes Electrical power distribution
AC generation/DC power Bleed air indication
Anti-ice control Fuel quantity
Pitch trim/yaw damper systems VHF communication system
Inertial navigation Air traffic control system
HF communication system Selective calling system
Automatic direction finder Passenger entertainment system
Thrust control computer Exhaust gas temperature
Air data computer system Fuel flow indication
Critical engine monitoring Engine pressure ratio
Nl/N2 rpm N1 limit computation
Electronic flight instrument system Electronic centralized aircraft monitor system
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