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|
Attributes | |
ACN | 600705 |
Time | |
Date | 200311 |
Day | Sun |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : opf.airport |
State Reference | FL |
Altitude | agl single value : 0 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tower : cle.tower |
Operator | general aviation : personal |
Make Model Name | Skylane 182/RG Turbo Skylane/RG |
Operating Under FAR Part | Part 91 |
Flight Phase | ground : holding ground : taxi |
Flight Plan | VFR |
Person 1 | |
Affiliation | other |
Function | flight crew : single pilot |
Qualification | pilot : private |
Experience | flight time last 90 days : 3 flight time total : 500 flight time type : 55 |
ASRS Report | 600705 |
Person 2 | |
Affiliation | government : faa |
Function | controller : local |
Events | |
Anomaly | aircraft equipment problem : critical non adherence : published procedure |
Independent Detector | other flight crewa |
Resolutory Action | none taken : detected after the fact |
Consequence | other other |
Supplementary | |
Problem Areas | Aircraft Flight Crew Human Performance |
Narrative:
After taxiing approximately +/-1 mi, aircraft was difficult to maintain on taxiway centerline. I attributed this to strong quartering tailwinds at first. Eventually, condition worsened to extent that it was nearly impossible to fight left turning tendency of aircraft. Additionally, taxi speed was decreasing. I pulled aircraft over to left side of taxiway to try to ascertain cause of problem after advising ground control. It seemed that the left brake was dragging, making aircraft pull to left. I tried pumping the brakes alternately trying to free the brake. I also was looking at left wheel pant assembly to see if I had rolled over anything, possibly lodging it between tire and wheel pant. Nothing was apparent. While pumping the brakes, I was increasing and decreasing power, in an attempt to 'rock' the airplane, hopefully to free the brake. I was also communicating with ground control, updating them of my situation. I went through the preflight checklist again, and cycled the parking brake. That seemed to free the offending brake. I obtained permission to taxi, and while taxiing, applied alternating brakes to check that brake would not 'stick' again. I made normal run-up and all system, temperatures, etc, were normal. Cleared onto active, I applied full power for takeoff. Aircraft accelerated normally, climb was normal as well. Upon reaching cruise altitude, checked that airspeed, temperatures, RPM's, etc were normal. Upon arriving at eyw, I taxied to parking area whereupon I shut down engine. Line man parked aircraft, after pilot and passenger disembarked. I returned to the aircraft after it was parked and noticed damage to both propeller tips (line man had not noticed damage). There seemed to be an equal amount of damage to both blades. This may account for the lack of any apparent engine vibrations. Damage was leading edge gouges with very slight twisting at blade tips. I decided to not fly the aircraft back to opf. I contacted the aircraft owner and advised them of situation. I did not experience an in-flight bird strike, so damage must have occurred while on ground. Possible, while trying to free left brake, with aircraft on left side of taxiway, and while throttling up and down, aircraft may have crept close enough to edge of taxiway so that propeller nicked an obstacle on taxiway edge. I did not hear adverse sounds during this incident, though there was much radio communication ongoing as well as typical radio static, etc. Aircraft pulling to left probably caused by parking brake not fully released, and/or brakes not adjusted properly or sticking left caliper.
Original NASA ASRS Text
Title: A C182 SINGLE PLT MISHANDLED AND OR MISDIAGNOSED A CRITICAL ACFT PROB DURING TAXI. PRESSING ON TO HIS DEST, THE RPTR DISCOVERED PROP DAMAGE AFTER LNDG AT EYW.
Narrative: AFTER TAXIING APPROX +/-1 MI, ACFT WAS DIFFICULT TO MAINTAIN ON TXWY CTRLINE. I ATTRIBUTED THIS TO STRONG QUARTERING TAILWINDS AT FIRST. EVENTUALLY, CONDITION WORSENED TO EXTENT THAT IT WAS NEARLY IMPOSSIBLE TO FIGHT L TURNING TENDENCY OF ACFT. ADDITIONALLY, TAXI SPD WAS DECREASING. I PULLED ACFT OVER TO L SIDE OF TXWY TO TRY TO ASCERTAIN CAUSE OF PROB AFTER ADVISING GND CTL. IT SEEMED THAT THE L BRAKE WAS DRAGGING, MAKING ACFT PULL TO L. I TRIED PUMPING THE BRAKES ALTERNATELY TRYING TO FREE THE BRAKE. I ALSO WAS LOOKING AT L WHEEL PANT ASSEMBLY TO SEE IF I HAD ROLLED OVER ANYTHING, POSSIBLY LODGING IT BTWN TIRE AND WHEEL PANT. NOTHING WAS APPARENT. WHILE PUMPING THE BRAKES, I WAS INCREASING AND DECREASING PWR, IN AN ATTEMPT TO 'ROCK' THE AIRPLANE, HOPEFULLY TO FREE THE BRAKE. I WAS ALSO COMMUNICATING WITH GND CTL, UPDATING THEM OF MY SIT. I WENT THROUGH THE PREFLT CHKLIST AGAIN, AND CYCLED THE PARKING BRAKE. THAT SEEMED TO FREE THE OFFENDING BRAKE. I OBTAINED PERMISSION TO TAXI, AND WHILE TAXIING, APPLIED ALTERNATING BRAKES TO CHK THAT BRAKE WOULD NOT 'STICK' AGAIN. I MADE NORMAL RUN-UP AND ALL SYS, TEMPS, ETC, WERE NORMAL. CLRED ONTO ACTIVE, I APPLIED FULL PWR FOR TKOF. ACFT ACCELERATED NORMALLY, CLB WAS NORMAL AS WELL. UPON REACHING CRUISE ALT, CHKED THAT AIRSPD, TEMPS, RPM'S, ETC WERE NORMAL. UPON ARRIVING AT EYW, I TAXIED TO PARKING AREA WHEREUPON I SHUT DOWN ENG. LINE MAN PARKED ACFT, AFTER PLT AND PAX DISEMBARKED. I RETURNED TO THE ACFT AFTER IT WAS PARKED AND NOTICED DAMAGE TO BOTH PROP TIPS (LINE MAN HAD NOT NOTICED DAMAGE). THERE SEEMED TO BE AN EQUAL AMOUNT OF DAMAGE TO BOTH BLADES. THIS MAY ACCOUNT FOR THE LACK OF ANY APPARENT ENG VIBRATIONS. DAMAGE WAS LEADING EDGE GOUGES WITH VERY SLIGHT TWISTING AT BLADE TIPS. I DECIDED TO NOT FLY THE ACFT BACK TO OPF. I CONTACTED THE ACFT OWNER AND ADVISED THEM OF SIT. I DID NOT EXPERIENCE AN INFLT BIRD STRIKE, SO DAMAGE MUST HAVE OCCURRED WHILE ON GND. POSSIBLE, WHILE TRYING TO FREE L BRAKE, WITH ACFT ON L SIDE OF TXWY, AND WHILE THROTTLING UP AND DOWN, ACFT MAY HAVE CREPT CLOSE ENOUGH TO EDGE OF TXWY SO THAT PROP NICKED AN OBSTACLE ON TXWY EDGE. I DID NOT HEAR ADVERSE SOUNDS DURING THIS INCIDENT, THOUGH THERE WAS MUCH RADIO COM ONGOING AS WELL AS TYPICAL RADIO STATIC, ETC. ACFT PULLING TO L PROBABLY CAUSED BY PARKING BRAKE NOT FULLY RELEASED, AND/OR BRAKES NOT ADJUSTED PROPERLY OR STICKING L CALIPER.
Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.