Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR PNSA0901Transducer · malfunctionedTORQUE INDICATION WENT TO ZERO DURING DESCENT. AFTER UNEVENTFUL LANDING, REPLACED TORQUE TRANSDUCER. OPERATIONAL CHECK OK. (X)SDR PNSA000401Fan · failedDURING CLIMB, A SMOKEY SMELL WAS NOTICED IN THE CABIN. BLEED AIR WAS SHUT OFF BUT SMELL CONTINUED. RETURNED FOR LANDING. DISCOVERED WINDINGS FOR CABIN FRESH AIR FAN HAD MELTED. REPLACED FAN.SDR PNSA000206Engine · lack of lubeDURING TAXI OIL PRESSURE INDICATED LOWER THAN NORMAL. RETURNED TO BLOCK. SERVICED OIL, OPS CHECKED OK.SDR PNSA000103Linkage · out of adjustON ROLL OUT WHILE RETARDING SPEED LEVER TO THE TAXI POSITION, ENGINE SHUT DOWN. FOUND FUEL SHUT-OFF LINKAGE OUT OF DETENT. RE-INDEXED LINKAGE TO SPEED LEVER, OPS CHECKED OK.SDR PNSA000105Tire · failedWHILE HOLDING AT FAI AT -39F OAT LT MAIN TIRE WENT FLAT. FLIGHT DELAYED WHILE WHEEL ASSY CHANGED.SDR PNSA991102Cooler · crackedEN ROUTE FROM BFI TO ANC, RT OIL PRESSURE BEGAN TO FLUCTUATE, DIVERTED TO SIT. ON FINAL, LOST RT OIL PRESSURE COMPLETELY SECURED ENGINE AND LANDED. OIL COOLER WAS LEAKING ALONG MOUNTING FLANGE. REPLACED COOLER. LEAK CHECK OK.SDR PNSA991101Circuit Breaker · failedWHILE CLIMBING-OUT PILOT NOTICED SMOKE COMING FROM THE RECOGNITION LIGHT SWITCH-BREAKER. SYSTEM WAS TURNED OFF, SMOKE STOPPED. LANDING WAS NORMAL. SWITCH BREAKER WAS REPLACED.SDR PNSA990901Pump · siezedON RUNWAY, SELECTED SPEEDS HIGH FOR TAKEOFF, RT ENGINE FLAMED OUT. RETURNED TO BLOCK. REPLACED ENGINE DRIVEN FUEL PUMP, OPS CHECKED OK.SDR PNSA980207Wire · looseENGINES WOULD NOT CRANK. SECURED WIRE AT SQUAT SWITCH, OPS CHECK OK.SDR PNSA980206Hsi Card · failedCAPTAINS HSI CARD DID NOT TURN DURING TAXI. REPLACED HSI, OPS CHECK OK.SDR PNSA971213Tire · flatDURING ROLL OUT, NO BRAKE ACTION FROM RT MAIN, TIRE HAD LOST PRESSURE, WHILE REMOVING AIRCRAFT FROM RUNWAY LT MAIN ALSO WENT FLAT. REPLACED BOTH WHEEL ASSY. NOTE AMBIENT TEMP -37 F.SDR 96ZZZX5113Rib · crackedDURING PHASE INSPECTION, FOUND 1.5 INCH CRACK IN RT WING CANTED RIB TOP CAP. CRACK STARTS AT AFT SIDE OF FORWARD SPAR AND RUNS AFT PARALLEL TO THE BEND RADIUS. STOP DRILL CRACK PER CESSNA INSTRUCTIONS.