Sabreliner NA-265-40
Service difficulty reports · 55
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'NA26540' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'NA26540' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR C2XA06TY067Bulkhead · corrodedTYS - DURING A CURRENT 2C INSPECTION THE VENTRAL TANK FWD BULKHEAD WAS FOUND CORRODED AT THE FUEL LINE SUPPORT BRACKET. MAINTENANCE CUT OUT THE EFFECTED AREA, FABRICATED AND INSTALL A DOUBLER AND FILLER. ALODINED AND PRIMED IAW EC 2810-01027. A/C WILL BE RESDR 2003FA0000661Selector Valve · failedMAIN LANDING GEAR DOOR SELECTOR VALVE FAILED CAUSING MAIN GEAR FAIRING DOORS TO REMAIN OPEN. THE LANDING GEAR UN-SAFE LIGHT REMAINED ON WITH GEAR UP. WITH MAIN DOOR SELECTOR VALVE FAILED, HYDRAULIC PRESSURE WAS NOT SUPPLIED TO THE NOSE STEERING SYSTEM. POSSSDR 98ZZZX3632Trunnion · crackedDURING SCHEDULED INSPECTION, THE NOSE LANDING GEAR UPPER BARREL ASSY WAS FOUND WITH A CRACK COMPLETELY THROUGH THE RT TRUNNION PIN HOLE. THE TRUNNION/BEARING PIN AND RETAINING BOLT WERE IN PLACE AND HOLDING THE TRUNNION PORTION OF THE UPPER BARREL TOGETHER. SDR 98ZZZX2725Pin · failedTHE CLIP THAT RETAINS THE DRAG CHUTE RETAINING PIN VIBRATES LOOSE WHEN CHUTE WAS DEPLOYED, IT DETACHED FROM THE AIRCRAFT. THE YOKE AND RETAINING PIN CAUGHT ON THE EDGE OF THE SKIN CAUSING DAMAGE TO LOWER TAIL SKIN AND STRUCTURE. THIS IS A ONE OF A KIND INSTASDR 98ZZZX481Line · leakLINE INSTALLED AT NOSE STEERING ACTUATOR TO SWIVEL JOINT IN NOSE WHEELWELL. LINE STARTED TO LEAK AT POINT IN LINE WHERE LINE BENDS WHEN NLG ACTIVATED.SDR 97ZZZX3779Regulator · corrodedPART RECEIVED FROM SUPPLY WITH CORROSION ON TERMINAL ENDS. THESE ARE NEWLY OVERHAULED UNITS. SUBMITTER STATED THIS IS AN ONGOING PROBLEM, APPARENTLY, THIS AREA IS NOT BEING LOOKED AT DURING OVERHAUL.SDR 97ZZZX3778Regulator · corrodedPART RECEIVED FROM SUPPLY WITH CORROSION ON TERMINAL ENDS. THESE ARE NEWLY OVERHAULED UNITS. SUBMITTER STATED THIS IS AN ONGOING PROBLEM, APPARENTLY, THIS AREA IS NOT BEING LOOKED AT DURING OVERHAUL.SDR 97ZZZX3783Pump · seal damagedHYDRAULIC PUMP WAS REMOVED AFTER 7.9 HOURS TIME IN SERVICE DUE TO SHAFT SEAL FAILURE AND EXCESSIVE FLUID LEAKAGE. PUMP, SN MX193803A, REJECTED FOR INSTALLATION DUE TO SHAFT SEAL WAS DAMAGED AND STICKING OUT AROUND THE PUMP DRIVE SHAFT. BOTH PUMPS WERE OVERHAUSDR 97ZZZX3782Pump · seal damagedHYDRAULIC PUMP WAS REMOVED AFTER 7.9 HOURS TIME IN SERVICE DUE TO SHAFT SEAL FAILURE AND EXCESSIVE FLUID LEAKAGE. PUMP, SN MX193803A, REJECTED FOR INSTALLATION DUE TO SHAFT SEAL WAS DAMAGED AND STICKING OUT AROUND THE PUMP DRIVE SHAFT. BOTH PUMPS WERE OVERHAUSDR 97ZZZX2939Line Assy · chafedDURING PYLON MATCHING ANGLES AND FUSELAGE SKIN INSPECTION, NOTED AN ADEL CLAMP, PN MS21919DG6, WAS BROKEN ON THE RIGHT HAND SIDE FS 367. FURTHER INSPECTION REVEALED THE THRUST REVERSER STOW HYDRAULIC PRESSURE LINE ASSY, PN 306-588003-039, HAD WORN THROUGH APPSDR 96ZZZX5327Bellcrank · corrodedSEVERELY CORRODED MAGNESIUM BELLCRANK PN 265-522130-3 WHICH OPERATES THE BIAS BUNGEE ELEVATOR TO STABILIZER LONGITUDINAL CONTROL. THIS UNIT IS LOCATED IN THE AFT LOWER LEFT SIDE OF FS 457. VISUAL INSPECTION IS VERY DIFFICULT DUE TO LOCATION AND POSITION OF RSDR 96ZZZX5326Bellcrank · corrodedSEVERELY CORRODED MAGNESIUM BELLCRANK, PN 265-522130-3, WHICH OPERATES THE BIAS BUNGEE FOR ELEVATOR TO STABILIZER LONGITUDINAL CONTROL. THIS UNIT IS LCOATED IN THE AFT LOWER LEFT SIDE OF FS 457. VISUAL INSPECTION IS VERY DIFFICULT DUE TO LOCATION AND POSITIONSDR 96ZZZX5270Bellcrank · corrodedSEVERELY CORRODED MAGNESIUM BELLCRANK WHICH OPERATES THE BIAS BUNGEE FOR ELEVATOR TO STABILIZER LONGITUDINAL CONTROL. THIS UNIT IS LOCATED IN THE AFT LOWER LEFT SIDE OF FS 457. VISUAL INSPECTION IS VERY DIFFICULT DUE TO LOCATION AND POSITION OF ROD END ATTACHSDR 96ZZZX5272Control Cable · corrodedLOWER AFT ELEV CONTROL CABLE FS 388 TO FS 457 SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF THE FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-540425-37, FS 368 TO FS 390. CABLES ARE VISUALLY INSPECTED AT 150-HOUR INTERVALS. CABLES ARE MANUFACTURESDR 96ZZZX5274Control Cable · corrodedLOWER AFT ELEV CONTROL CABLE FS 388 TO FS 457 SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-540425-37, FS 368 TO FS 390. CABLES ARE VISUALLY INSPECTED AT 150-HOUR INTERVALS. CABLES ARE MANUFACTURED OFSDR 96ZZZX5273Bellcrank · corrodedSEVERELY CORRODED MAGNESIUM BELLCRANK WHICH OPERATES THE BIAS BUNGEE FOR ELEVATOR TO STABILIZER LOCATED IN AFT LOWER LEFT SIDE OF FS 457. VISUAL INSPECTION IS VERY DIFFFICULT DUE TO LOCATION AND POSITION OF ROD END ATTACHMENT POINTS. SUBMITTER SUGGESTS THIS SDR 96ZZZX5271Control Cable · corrodedLOWER AFT ELEV CONTROL CABLE FS 388 TO FS 457 SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-540425-37 FS 368 TO FS 390. CABLES ARE VISUALLY INSPECTED AT 150 HR INTERVALS. CABLES ARE MANUFACTURED OF CASDR 96ZZZX5144Control Cable · brokenLOWER AFT ELEVATOR CONTROL CABLE FS 388 TO FS 457, SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-540425-37, FS 368 TO FS 390. CABLES ARE VISUALLY INSPECTED AT 150-HR INTERVALS. CABLES ARE MANUFACTUREDSDR 96ZZZX5145Control Cable · frayedLOWER AFT ELEVATOR CONTROL CABLE FS 388 TO FS 457, SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-540425-37, FS 368 TO FS 390. CABLES ARE VISUALLY INSPECTED AT 150-HR INTERVALS. CABLES ARE MANUFACTUREDSDR 96ZZZX5142Control Cable · frayedLOWER AFT ELEVATOR CONTROL CABLE, FS 388 TO FS 457, SHOWED SIGNS OF CORROSION ON UPPER SURFACE 'ONLY' JUST AFT OF THE FIBERGLASS PROTECTIVE CABLE SHROUD PN 265-540425-37, FS 368 TO FS 390. CABLES ARE VISUALLY INSPECTED AT 150-HOUR INTERVALS. CABLES ARE MANUFSDR 96ZZZX4331Compressor · bindingCOMPRESSOR VERY DIFFICULT TO ROTATE, IINTERNAL BINDING COULD BE FELT WHEN ROTATING BY HAND WITH SHORT SPOOL DOWN TIME. NO FOD NOTED, NO DAMAGE OR VISUAL DEFECTS NOTED IN TURBINE HOT SECTION. ALL IN-FLIGHT AND GROUND TEST PARAMETERS NORMAL. ENGINE WAS REMOVEDSDR 96ZZZX4332Actuator · leakACTUATOR WAS INSTALLED ON THE AIRCRAFT, OPERATIONALLY CHECKED, AND REMOVED DUE TO LEAKAGE THROUGH A HOLE (OR CRACK) IN THE ACTUATOR CYLINDER (BARREL) WALL. THE ACTUATOR WAS OVERHAULED 9-7-95. ACTUATOR TIME SINCE OVERHAUL WHEN REMOVED: ZERO HOURS. AIRCRAFT SDR 96ZZZX4385Power Supply · failedSTROBE POWER SUPPLY WAS INSTALLED IN THE AIRCRAFT, OPERATED FOR 25 HOURS, AND WAS REMOVED FOR INTERNAL FAILURE WITH NO POWER OUTPUT. UNIT WAS OVERHAULED ON 10-18-95. RELIABILITY OF OVERHAULED UNITS FROM THIS REPAIR STATION HAS BEEN POOR. AIRCRAFT TT: 10,62SDR 96ZZZX3905Pump · seal failedHYDRAULIC PUMP SHAFT SEAL FAILURE IN-FLIGHT 'WITHOUT INCIDENT', BUT ELECTRIC DRIVE MOTOR AND SURROUNDING AFT FUSELAGE AREA TO TAIL WAS SATURATED WITH APPROXIMATELY 2 GALLONS OF FLUID WHICH POSED A SEVERE FIRE HAZARD.SDR 96ZZZX4135Valve · failedAIRCRAFT WAS INITIALLY EXPERIENCING LANDING GEAR OPERATION PROBLEMS. PROBLEM WAS TROUBLESHOT TO A BAD LANDING GEAR HYDRAULIC CONTROL VALVE. REQUIRED A REPAIRED VALVE AND INSTALLED. ALL OPS CHECKS WERE GOOD. ON THE FIRST TRIP, PILOT REPORTED HEARING THE HYDSDR 96ZZZX4033Transducer · failedUNIT WAS INSTALLED IN THE AIRCRAFT, TESTED, AND FOUND TO BE INOPERATIVE. UNIT WAS TESTED AGAIN (IN OPPOSITE POSITION ON SAME AIRCRAFT) AND WAS STILL INOPERABLE. UNIT WAS TESTED AND RELEASED BY REPAIR STATION ON 7-9-96. AIRCRAFT TOTAL TIME: 12,813.4 HRS.SDR 96ZZZX3906Compressor · bindingCOMPRESSOR VERY DIFFICULT TO ROTATE AND SPOOL DOWN VERY SHORT. INTERNAL BINDING COULD BE FELT WHEN ROTATING BY HAND. THIS IS A MULTI-STAGE UNIT, SO VISUAL INSPECTION/DETECTION OF A PARTICULAR PART FAILURE IS VERY DIFFICULT. NO FOD NOTED AND NO DAMAGE OR DEFSDR 96ZZZX4166Sensor · inoperativeRECEIVING INSPECTION CONDUCTED BY RAYTHON AEROSPACE. THERE IS 'NO WAY' THAT THIS NR 7 FUEL QUANTITY TANK UNIT COULD HAVE BEEN BENCH CHECKED/FUNCTIONAL TESTED. RECEIVING INSPECTION READINGS WERE 35MMF'S AND WOULD NOT 'NULL' READINGS SUGGEST THAT THE UNIT IS WSDR 96ZZZX4034Compressor · bindingCOMPRESSOR VERY DIFFICULT TO ROTATE AND SPOOL DOWN VERY SHORT. INTERNAL BINDING COULD BE FELT WHEN ROTATING BY HAND. THIS IS A MULTI 9-STAGE UNIT, SO VISUAL INSPECTION/DETECTION OF A PARTICULAR PARTS FAILURE IS VERY DIFFICULT. NO FOD NOTED AND NO DAMAGE OR DSDR 96ZZZX4035Compressor · bindingCOMPRESSOR VERY DIFFICULT TO ROTATE AND SPOOL DOWN VERY SHORT. INTERNAL BINDING COULD BE FELT WHEN ROATING BY HAND. THIS IS A MULTI 9-STAGE UNIT, SO VISUAL INSPECTION/DETECTION OF A PARTICULAR PARTS FAILURE IS VERY DIFFICULT. NO FOD NOTED AND NO DAMAGE OR DSDR 96ZZZX3523Compressor · bindingCOMPRESSOR VERY DIFFICULT TO ROTATE AND SPOOL DOWN VERY SHORT. INTERNAL BINDING COULD BE FELT WHEN ROTATING BY HAND. THIS IS A MULTI-STAGE UNIT, SO VISUAL INSPECTION/DETECTION OF A PARTICULAR PARTS FAILURE IS VERY DIFFICULT. NO FOD NOTED AND NO DAMAGE OR DESDR 96ZZZX3016Transducer · failedTRANSDUCER WAS INSTALLED IN THE AIRCRAFT, TESTED, AND REMOVED WITH ZERO HOURS SINCE OVERHAUL. UNIT WAS REMOVED DUE TO EPR INDICATION WOULD STICK AT 2.0 AND WOULD NOT CHANGE WITH CHANGES IN ENGINE POWER SETTING. UNIT WAS OVERHAULED 3-29-96. SUBMITTER STATED SDR 96ZZZX3051Blade · brokenSECOND STAGE TURBINE ROTOR BLADE FAILURE IN-FLIGHT, WITHOUT INCIDENT. ENGINE TT, 11,164.7 HRS, CYCLES, 8,081, TSO, 330.9 HRS, TTHSI, 330.9 HRS, TOTAL PART TIME 330.9 HRS. UNIT WAS OVERHAULED 4-12-95.SDR 96ZZZX3050Pump · failedUNIT FAILED IN-FLIGHT WITHOUT INCIDENT, SUSPECT INTERNAL MOTOR BRUSH OR COMMUTATOR FAILURE. UNIT OVERHAULED.SDR 96ZZZX2638Pump · seal failedPUMP WAS INSTALLED, TEST RUN FOR 30 SECONDS, AND REMOVED WITH ZERO HOURS TIME IN SERVICE SINCE OVERHAUL. PUMP WAS REMOVED DUE TO SHAFT SEAL FAILED WHICH PUMPED FLUID OUT THROUGH THE CASE DRAIN AND CONTAMINATED THE DRIVE MOTOR. PUMP WAS OVERHAULED ON 1-19-96.SDR 96ZZZX3052O-Ring · missingWHEEL ASSY OVERHAULED 4-11-96. UNITS FUSIBLE PLUG O-RING, PN 9524796, NOT REPLACED DURING OVERHAUL.SDR 96ZZZX3049O-Ring · missingWHEEL ASSY OVERHAULED 4-5-96. UNITS FUSIBLE PLUG O-RING NOT REPLACED DURING OVERHAUL.SDR 96ZZZX3017Beacon Assy · failedBEACON WAS REMOVED FROM SERVICE WITH 27.0 HRS SINCE OVERHAUL DUE TO WOULD NOT ROTATE. UNIT WAS OVERHAULED BY REPAIR STATION. SUBMITTER STATED RELIABILITY OF REPAIRED AND OVERHAULED UNITS HAS BEEN POOR. AIRCRAFT TT: 1,683.0 HRS.SDR 96ZZZX3823Turbine · failedCLIMBING THROUGH 5,000 FEET, THE CREW HEARD AND FELT A LOUD REPORT FOLLOWED IMMEDIATELY BY THE LT ENGINE FIRE WARNING LIGHT. THE LT ENGINE SPEED ROLLED BACK TO APPROXIMATELY 12 PERCENT. PILOT SHUT ENGINE DOWN, DISCHARGED THE FIRE BOTTLE AND MADE A SINGLE ENGSDR 96ZZZX1962Transducers · erraticTRANSDUCER WAS INSTALLED IN AIRCRAFT, TESTED DURING GROUND RUN, AND REMOVED WITH ZERO HOURS TIME IN SERVICE SINCE OVERHAUL. E.P.R. READINGS WERE ERRATIC IN ALL POWER RANGES. UNIT WAS OVERHAULED BY REPAIR STATION ON 3-17-96. SUBMITTER STATED RELIABILITY OF OSDR 96ZZZX1964Pump · failedPUMP WAS REMOVED AND REPLACED DUE TO AFTER SEVERAL MINUTES OF OPERATION, PUMP BECAME EXTREMELY NOISY AND ROUGH INDICATING A POSSIBLE IMPENDING FAILURE. TIME IN SERVICE AT TIME OF REMOVAL (T.S.M.O.N.): 195.4 HOURS. PUMP WAS OVERHAULED 10-2-95. SUBMITTER STASDR 96ZZZX831Seat Assy · weld brokenPILOT'S SEAT WOULD NOT ADJUST FORWARD AND AFT OR VERTICALLY, AND SEAT WOULD NOT SIT LEVEL. INSPECTION FOUND SEAT STRUCTURAL MEMBERS (WELD ASSYS) BROKEN AT WELDED AREAS. SEPARATION OF THESE SUPPORT MEMBERS ALLOWS THE SEAT TO PARTIALLY COLLAPSE AND PREVENTS THSDR 96ZZZX830Seat Assy · weld brokenPILOT'S SEAT WOULD NOT ADJUST FORWARD AND AFT OR VERTICALLY, AND SEAT WOULD NOT SIT LEVEL. INSPECTION FOUND SEAT STRUCTURAL MEMBERS (WELD ASSYS) BROKEN AT WELDED AREAS. SEPARATION OF THESE SUPPORT MEMBERS ALLOWS THE SEAT TO PARTIALLY COLLAPSE AND PREVENTS THSDR 96ZZZX763Vane · debondedUNDER NORMAL OPERATING CONDITIONS, THE PROTECTIVE COATING IS DEBONDING FROM THE SURFACE OF NEW VANES. DEFECT WAS FOUND BY BORESCOPING THE ENGINE.SDR 96ZZZX750Vane · debondingUNDER NORMAL OPERATING CONDITIONS, THE PROTECTIVE COATING IS DEBONDING FROM THE SURFACE (LEADING EDGE) OF NEW VANES. DEFECT WAS FOUND BY BORESCOPING THE ENGINE.SDR 95ZZZX6606Pump · defectiveTHIS BOOST PUMP WAS RECEIVED FROM THE VENDOR WITH A FRESH OVERHAUL. ON OPS CHECK, THE PUMP HAD A RUBBING NOISE. THE SCREEN WAS REMOVED AND THE IMPELLER WAS FOUND RUBBING THE WALL ON ONE SIDE AND THE HOUSING BASE ON THE OTHER SIDE. EITHER THE SHAFT IS BENT OSDR 95ZZZX6605Pump · failedBOOST PUMP CAUSES CIRCUIT BREAKER TO TRIP IN-FLIGHT. SUSPECT CAUSE, INTERNAL SHORT OR BAD BEARINGS.SDR 95ZZZX6604Pump · shortedBOOST PUMP CAUSES CIRCUIT BREAKER TO TRIP IN-FLIGHT. SUSPECT INTERNAL SHORT OR BAD BEARINGS.SDR 95ZZZX5545Pump · failurePUMP WAS REMOVED FROM AIRCRAFT WITH 5.6 HOURS TIME IN SERVICE SINCE OVERHAUL DUE TO PUMP CAUSED CIRCUIT BREAKER TO TRIP AND WOULD NOT RESET. UNIT WAS OVERHAULED BY REPAIR STATION NR HAXR577E UNDER WORK ORDER NR L3201 ON 7-17-95. THIS IS THE THIRD LOW-TIME FASDR 95ZZZX5546Pump · failedPUMP WAS REMOVED FROM AIRCRAFT WITH 52.0 HOURS TIME IN SERVICE SINCE OVERHAUL DUE TO INTERNAL FAILURE CAUSING BOOST PUMP CIRCUIT BREAKER TO TRIP AND WOULD NOT RESET. PUMP WAS OVERHAULED BY REPAIR STATION NR NAXR577E ON 7-12-95 UNDER WORK ORDER NR L3211. SUBM
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