Kontiki99
Circuit breakers are a necessary pain. When they need to work is when they are absolutely a life saver... however...
They age and deteriorate, corrode internally, fatigue [springs, pins, plastic, etc] and need constant maintenance such as visual isnspection for signs of overheating and manual breaking/popping and resetting to clean-off any arc-flash welds or corrosion between contact surfaces, etc [an make sure they work "ok" to the touch.
They SHOULD be tested every few years on a CB tester [used to verify that breakers function as planned under high stress circuit loads].
Most convential breakers under typical loads can last 15+/- years... however, if Mods are added and/or wiring loads increase, they may fail dramatically sooner [IE: a high current electric motor starts to sieze, etc]. This only gets worse in a extremely corrosive [sea coast] atmosphere.
OH yeah a single failed breaker in the middle of a panel can over-heat/burn and spread the damage through-out the adjacent breakers on the panel.
Typical CB related data/info [not specific CB specs] is as follows...
NOTE: Circuit breakers are technically an "electric overcurrent protective device".
NOTE: within these specs are references to many other useful/relevant specs/data, etc.
FAA AC25.13567-1 Circuit protective devices
FAA AC25-16 Electrical Fault and Fire Prevention and Protection
FAA AC43-206 Inspection, Prevention, Control, and Repair of Corrosion on Avionics Equipment
SAE ARP1199, DEVICES, ELECTRIC OVERCURRENT PROTECTIVE, SELECTION, APPLICATION, AND INSPECTION OF
SAE ARP4101/5 Aircraft Circuit Breaker and Fuse Arrangement
SAE ARP4404 Aircraft Electrical Installations
SAE AS50881 WIRING, AEROSPACE VEHICLE
SAE AS58091 Circuit Breakers, Trip-Free, Aircraft General Specification For
SAE J553 Circuit Breakers
SAE/TP 2006-01-2419 Arc Fault Protection, Application Techniques for Aircraft Circuit Breakers
MIL-DTL-27715 CIRCUIT BREAKER, TRIP-FREE, HIGH TEMPERATURE, AIRCRAFT GENERAL SPECIFICATION FOR
MIL-DTL-23928 PANELS, ELECTRICAL, POWER DISTRIBUTION AND MANUAL TRANSFER, CIRCUIT BREAKER TYPE
MIL-HDBK-522 GUIDELINES FOR INSPECTION OF AIRCRAFT ELECTRICAL WIRING INTERCONNECT SYSTEMS
MIL-HDBK-5400 ELECTRONIC EQUIPMENT, AIRBORNE GENERAL GUIDELINES FOR
MIL-STD-7080 SELECTION AND INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
WRDC-TR-90-4075 FAILURE ANALYSIS TECHNIQUES FOR THE EVALUATION OF ELECTRICAL AND ELECTRONIC COMPONENTS IN AIRCRAFT ACCIDENT INVESTIGATIONS
WL-TR-95-4004 AIRCRAFT MISHAP INVESTIGATION HANDBOOK FOR ELECTRONIC HARDWARE
DOT/FAA/AR-01/118 Aircraft Age-Related Degradation Study on Single- and Three-Phase Circuit Breakers
USAF T.O. 1-1-686-1, CLEANING AND CORROSION CONTROL VOLUME I CORROSION PROGRAM AND CORROSION THEORY
USAF T.O. 1-1-686-3, CLEANING AND CORROSION CONTROL VOLUME III AVIONICS AND ELECTRONICS
USAF T.O. 1-1-686-5, CLEANING AND CORROSION CONTROL VOLUME V CONSUMABLE MATERIALS AND EQUIPMENT FOR AVIONICS
USAF T.O. 1-1A-14 INSTALLATION AND REPAIR PRACTICES VOLUME 1 AIRCRAFT ELECTRIC AND ELECTRONIC WIRING
Etc... Gotta go back to work...
Regards, Wil Taylor
Trust - But Verify!
We believe to be true what we prefer to be true.
For those who believe, no proof is required; for those who cannot believe, no proof is possible.
Unfortunately, in science what You 'believe' is irrelevant – "Orion"