RADIO COM PROB NOTWITHSTANDING. ATX PLT CONTINUES TO DEST ARPT. CITES ACFT ELECTRICAL ELECTRONIC PANEL DESIGN PROB.

Date: 1994-08 · Aircraft: PA-28 Cherokee/Archer/Dakota/Pillan/Warrior

Anomalies: aircraft-equipment-problem-critical|deviation-discrepancy-procedural-published-material-policy|deviation-discrepancy-procedural-landing-without-clearance|deviation-discrepancy-procedural-far|other-unspecified

Synopsis

RADIO COM PROB NOTWITHSTANDING. ATX PLT CONTINUES TO DEST ARPT. CITES ACFT ELECTRICAL ELECTRONIC PANEL DESIGN PROB.

Narrative

THE SECOND INCIDENT EXPERIENCED DURING THIS FLT WAS COM DIFFICULTY WHICH RESULTED FROM EQUIP FAILURE ON MY ACFT. I HAD DIFFICULTY STARTING THE ACFT DUE TO A WEAK BATTERY. ON RUN UP CHK THE AMP METER INDICATED NORMAL OP OF THE ALTERNATOR SO I HAD NO REASON TO SUSPECT FURTHER DIFFICULTY. ALTHOUGH I DID NOT DETECT IT AT THE TIME; THE WEAK BATTERY AND POSSIBLE LOW CHARGE RATE MAY HAVE BEEN EFFECTING MY COMS EQUIP AT THE TIME I WAS PREPARING TO DEPART. IMMEDIATELY AFTER DEP I ATTEMPTED TO CONTACT TWR TO REQUEST A TURN ON COURSE. TWR DID NOT RESPOND AND ON MY SECOND ATTEMPT I NOTICED THAT MY XMISSION DID NOT SOUND NORMAL. I SWITCHED RADIOS AND TRIED AGAIN BUT NOTICED THE SAME INDICATION THAT I WAS NOT GETTING OUT. I THEN HEARD TWR TALKING TO ANOTHER ACFT BUT THE RECEPTION WAS WEAK AND BARELY READABLE. REALIZING I HAD A PROBABLE LOW VOLTAGE CONDITION I TURNED OFF ALL ELECTRICAL EQUIP EXCEPT THE XPONDER AND MY #1 COM RADIO. I WAS IMMEDIATELY ABLE TO CONTACT TWR AND WAS INSTRUCTED TO MAKE L TFC AND CONTACT DEP WHEN ESTABLISHED ON XWIND. I DO NOT BELIEVE I MISSED ANY COMS WITH TWR. AFTER COMPLETING THE L TURN I CONTINUED TO TROUBLE-SHOOT THE PROB AND CALLED DEP. MY INITIAL CONTACT WITH DEP WAS DIFFICULT AND REQUIRED SEVERAL EXCHANGES TO ESTABLISH RADAR CONTACT AND OBTAIN ON COURSE INSTRUCTIONS. EVENTUALLY I WAS ABLE TO GET THE ALTERNATOR ON LINE AND CONFIRM IT'S OP BY A POS DEFLECTION OF THE AMP METER INDICATOR. BELIEVING MY PROB WAS RESOLVED I DECIDED TO CONTINUE TO MY DEST. COMS WITH DEP REMAINED STRONG AND NORMAL UNTIL I WAS GIVEN FREQ CHANGE ABOUT 25 MI OUT FROM MFE. I CONTACTED SAN ANGELO FSS AND OPENED MY VFR FLT PLAN. APPROX 2/3 OF THE WAY TO LAREDO (LRD); MY DEST; I TURNED ON A VOR RECEIVER. NO SIGNAL RECEPTION WAS INDICATED. I ATTEMPTED TO CONTACT FSS WITHOUT SUCCESS. REALIZING I MAY ARRIVE AT LRD WITHOUT COM CAPABILITY I REVIEWED THE VFR SECTIONAL FOR ALTERNATIVES BUT FOUND NONE WHERE GND COMS WOULD BE AVAILABLE. I TURNED OFF ALL ELECTRICAL EQUIP IN HOPE THAT ENOUGH PWR MIGHT BE CONSERVED TO MAKE INITIAL CONTACT AT LRD. UPON ARRIVING AT LRD I TURNED THE COM RADIO ON AND ATTEMPTED TO CONTACT THE TWR. WHEN I WAS UNABLE TO MAKE CONTACT I CONTINUED INBOUND OBSERVING FOR TFC. I DETECTED AN ACFT DEPARTING RWY 17 SO I DSNDED TO TFC PATTERN ALT; APCHED AT A 45 DEG ANGLE TO RWY 17; MADE L HAND TFC; OBSERVING THE TWR FOR LIGHT SIGNALS AND LANDED ON RWY 17. THIS PROB WAS CAUSED BY EQUIP FAILURE AND INADEQUATE SYS CONDITION INDICATORS. THE ACFT WAS A PA-28-181. THE AMP METER ON THIS PARTICULAR ACFT NORMALLY HAS A VERY LOW AMP METER INDICATION; USUALLY LESS THAN 1 NEEDLE WIDTH ABOVE ZERO UNLESS FULLY LOADED WITH ALL ELECTRICAL SYS INCLUDING PITOT HEAT. THE ALT CAUTION LIGHT IS MOUNTED ON THE INST PANEL JUST BELOW A GLARE SHIELD AND IS A BUTTON TYPE WITH BACK LIGHTED LETTERS. IN DAYLIGHT IT IS VIRTUALLY IMPOSSIBLE TO DETECT WHETHER OR NOT THIS LIGHT IS ILLUMINATED. THIS PROB CAN BE RESOLVED BY INSTALLATION OF A DIFFERENT AMP METER WHICH WILL GIVE A MORE PROMINENT INDICATION OF CHARGING CONDITION AND INSTALLATION OF AN ALT FAILURE CAUTION LIGHT BETTER THAN THE WEAK BACK LIGHTED BUTTON TYPE WHICH IS CURRENTLY INSTALLED.

Source: NASA Aviation Safety Reporting System (public domain). Reports are voluntary submissions and are not verified by NASA.