North American NA-265-60

Service difficulty reports · 24

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 = 'NA26560'
  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.

SDR UVVR2012101700028Longeron · corrodedDURING VISUAL INSPECTION OF COCKPIT FLOORS LOWER LONGERONS. FOUND CORROSION LT LOWER LONGERON CORRODED & SIGN OF EXFOLIATION FROM FS 108-134.Dec 24, 2013 · N11LX · Rkwell NA26560 · Fuselage Main, Longeron/StringerSDR 2012FA0000643Stiffener · crackedWHILE PERFORMING A ROUTINE INSPECTION, FOUND A CRACK IN THE LT STIFFENER. CRACK PROPAGATED FROM A CORROSION PIT IN THE HAT SECTION STIFFENER. REPLACED IAW SRM AND RETURNED TO SERVICE.Sep 17, 2012 · Rkwell NA26560 · Fuselage Miscellaneous StructureSDR 2009FA0000877Valve · failedACFT EXPERIENCED AN UNCOMMANDED GEAR UP DURING TROUBLE SHOOTING FOR FREQUENT HYD CYCLING, WHILE IN HANGAR. MX WAS ATTEMPTING TO LOCATE THE SOURCE OF HYDARULIC FLUID BYPASS, WHICH WAS ORIGINALLY THOUGHT TO BE ONE OF THE BRAKE ACTUATING VALVES. BOTH ARE LOCATEMar 17, 2009 · N11LX · Rkwell NA26560 · Landing Gear Retraction/Extension SystemSDR 2008FA0000663Pump · wornAFTER TAKEOFF THE PILOT COULD NOT ADJUST THE LT ENGINE POWER OUTPUT. ENGINE REMAINED AT TAKEOFF POWER WHILE POWER LEVER WAS RETARDED TO IDLE. PILOT RETURNED TO AIRPORT AND SUCCESSFULLY SHUTDOWN THE LT ENGINE BY PLACING POWER LEVER TO CUT-OFF POSITION AND MADEAug 26, 2008 · Rkwell NA26560 · Engine Fuel PumpSDR 2007FA0001032Duct · deformedATTACHING SLEEVE SLID OFF OF DUCT CAUSING LOSS OF PRESSURIZATION. EMERGENCY PRESSURIZATION FUNCTIONED NORMALLY. CLAMPS TIGHTENED TOO TIGHT AND DEFORMED FIBERGLASS DUCT. RECOMMEND METAL SLEEVE BE INSTALLED TO ALLEVIATE DEFORMATION. (K)Oct 22, 2007 · N59K · Rkwell NA26560 · Air Distribution SystemSDR UVVR200600001Nut · crackedWHILE PERFORMING MAINTENANCE ON AIRCRAFT, IT WAS DISCOVERED THAT APPROXIMATELY 10 NUTS ON EACH WING THAT SECURES UPPER WING PLANK TO REAR SPAR UPPER FLANGE, FROM REAR SPAR STATION 161.1 TO 281.8 WERE CRACKED, WITH SOME MISSING PARTS OF THE NUT. AS A PRECAUTIONFeb 21, 2006 · N71CC · Rkwell NA26560 · Wing SparSDR CAR110Mixing Valve · not bondedHOT AIR MIXING VALVE WAS OVERHAULED BY ROCKER, 1-25-05, REF WO 56559. INSTALLED IN AIRCRAFT FROM STOCK ON 6-4-05. DURING FUNCTIONAL TEST FLIGHT FOR PRESSURIZATION PROBLEM, THE UP STREAM FLANGE SEPARATED FROM VALVE HOUSING. RELEASING BLEED AIR INTO AFT EQUIPJun 4, 2005 · Rkwell NA26560 · Cabin Pressure Control SystemSDR WK42004F00003Tire · damagedCENTER TREAD CHUNKED AFTER 23 LANDINGS ON RT TIRE. THE REVISION IS TO THE SN OF THE TIRE WHICH HAS THE DAMAGE TO IT. THE PREVIOUS SN WAS TO THE WHEEL ASSY ITSELF AND NOT THE DEFECTIVE PART(TIRE).Feb 10, 2004 · N353CA · Rkwell NA26560 · TireSDR WK42004F00001Tire · damagedCENTER TREAD CHUNKED AFTER 23 LANDINGS ON RT HAND TIRE.Feb 10, 2004 · N353CA · Rkwell NA26560 · TireSDR T2C2004F00000Casting · crackedDURING RUDDER RIGGING CHECK, FOUND CRACKED CASTING AT RUDDER PEDAL TORQUE TUBE SUPPORT, BELOW CO-PILOTS FLOOR. SUSPECT WIND GUST DAMAGE AS POSSIBLE CAUSE. ALSO NOTED RUDDER STOP BOLTS ON CASTING ADJUSTED BEYOND MAX TRAVEL LIMITS. RECOMMEND INSPECTING THIS AFeb 4, 2004 · N789SG · Rkwell NA26560 · Rudder Control SystemSDR 20000516SH026Fairing · corrodedDURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION THAT CAUSED A HOLE THROUGH UPPER WING SKIN. AFTER FINDING CORROSION ON LEFT SIDE, DECIDED TO PULL OFFApr 25, 2000 · N39CB · Rkwell NA26560 · Aerodynamic FairingsSDR 20000516SH025Fairing · corrodedDURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION THAT CAUSED A HOLE THROUGH UPPER WING SKIN. AFTER FINDING CORROSION ON LEFT SIDE, DECIDED TO PULL OFFApr 25, 2000 · N39CB · Rkwell NA26560 · Aerodynamic FairingsSDR 20000516SH024Fairing · corrodedDURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION THAT CAUSED A HOLE THROUGH UPPER WING SKIN. AFTER FINDING CORROSION ON LEFT SIDE, DECIDED TO PULL OFFApr 25, 2000 · N39CB · Rkwell NA26560 · Aerodynamic FairingsSDR 20000516SH023Fairing · corrodedDURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION THAT CAUSED A HOLE THROUGH UPPER WING SKIN. AFTER FINDING CORROSION ON LEFT SIDE, DECIDED TO PULL OFFApr 25, 2000 · N39CB · Rkwell NA26560 · Aerodynamic FairingsSDR 2000ZZZX27Switch · out of rigCREW EXTENDED LANDING GEAR ON APPROACH TO SUS. NO GREEN DOWN AND LOCKED LIGHT ON LT SIDE. LANDING GEAR WAS CYCLED WITH SAME RESULTS. CREW PERFORMED EMERGENCY EXTENSION PROCEDURES AND DID FLY-BY OF TOWER AT SUS. TOWER REPORTED GEAR APPEARED DOWN AND LOCKED.Dec 7, 1999 · N66GE · Rkwell NA26560 · Landing Gear Retraction/Extension SystemSDR 99ZZZX3469Thermostat · failedTHERMOSTAT INSTALLED ON A FRESHLY OVERHAULED ENGINE. ENGINE WAS OVERHAULED BY FAA CRS OTUR438L. PART DID NOT FAIL UNTIL ONE HOUR INTO FIRST FLIGHT.Aug 6, 1999 · N400JH · Rkwell NA26560 · Engine Oil Indicating SystemSDR 96ZZZX1360Blade · overlapDUE TO CORROSION DMG DISCOVERED ON RT ENG, CUSTOMER ELECTED TO DISASSEMBLE LT ENG FOR CORROSION INSP, & SUBSEQUENT COMPR OVERHAUL PER P&WA. UPON DISASSEMBLY OF COMPR, SEVERE CORROSION NOTED ON STEEL COMPONENTS. CORRRODED STEEL DISK REJECTED. CUSTOMER ELECTEFeb 9, 1996 · N401MS · Rkwell NA26560 · Turbine SectionSDR 96ZZZX1359Blade · rubDURING INSPECTION OF ENGINE, SN P673149NB, A CRACKED INLET GUIDE VANE PROMPTED REMOVAL OF INLET CASE FOR REPAIRS. WITH CASE REMOVED, A COMPRESSOR BLADE RUB, WHICH RESULTED IN DETERIORATION TO A STATOR, WAS NOTED AND REPORTED. AUTHORIZATION WAS RECEIVED FROM Feb 9, 1996 · N401MS · Rkwell NA26560 · Turbine Engine Compressor SectionSDR 95ZZZX5865Actuator · leakingREMOVED THRUST REVERSER ACTUATOR DUE TO LEAKING AT SHAFT. PARKER HANNIFIN CALLS OUT MINOR LEAKING AFTER SO MANY CYCLES. ACTUATOR REMOVED HAS 12.8 HOURS TSO AND IS LEAKING SMALL 'PUDDLES' UNDER COWL.Oct 4, 1995 · N113T · Rkwell NA26560 · Engine Thrust ReverserSDR 95ZZZX5864Actuator · leakingREMOVED THRUST REVERSER ACTUATOR DUE TO LEAKING AT SHAFT. PARKER HANNIFIN CALLS OUT MINOR LEAKING AFTER SO MANY CYCLES. ACTUATOR REMOVED, HAS 18 HOURS TSO AND IS LEAKING SMALL 'PUDDLES' UNDER COWL.Oct 4, 1995 · N113T · Rkwell NA26560 · Engine Thrust ReverserSDR 95ZZZX5863Actuator · leakingREMOVED TRUST REVERSER ACTUATOR DUE TO LEAKING AT SHAFT. PARKER HANNIFIN CALLS OUT MINOR LEAKING AFTER SO MANY CYCLES. ACTUATOR REMOVED HAS 18 HOURS TSO AND IS LEAKING SMALL 'PUDDLES' UNDER COWL.Oct 4, 1995 · N113T · Rkwell NA26560 · Engine Thrust ReverserSDR 95ZZZX6460Wheel Assy · rim bolts looseNOSE WHEEL ASSY VIBRATED DURING ROUTINE TAKEOFF. WHILE ON GROUND, NOSE WHEEL ASSY WAS INSPECTED AND 2 RIM RETAINING BOLTS WERE FOUND LOOSE. TIRE WAS DEFLATED AND ALL RIM RETAINING BOLTS WERE FOUND LOOSE. THIS UNIT WAS OVERHAULED BY SABRE LINER ON 11-2-94, OSep 4, 1995 · N2MIL · Rkwell NA26560 · Wheel/Ski/FloatSDR 95ZZZX5314Guide Vane · burnedENGINE RECEIVED FOR CORR & HOT SECT INSP PER SB 1508. ENG OPERATED TO 1,227 HRS TIME SINCE LAST HOT SECT INSP. ENG SUFFERED LOSS OF 3 EA NOZZLE GUIDE VANES COMPLETELY BURNED IN HALF ALLOWING INNER SHROUD HALVES TO ENTER GAS PATH & DAMAGE TURB. FAILURE RESULAug 28, 1995 · N8NR · Rkwell NA26560 · Turbine SectionSDR 95ZZZX906Probe · crackedPILOTS REPORTED THAT FUEL QUANTITY INDICATION BECAME ERRATIC IN-FLIGHT. AFTER TROUBLESHOOTING AND PINPOINTING PROBLEM TO BE AUXILIARY FUEL TANK PROBE, REMOVAL OF PROBE REVEALED THAT BARREL WAS CRACKED THE FULL CIRCUMFERENCE. CAUSE: EFFECT OF FUEL SLOSHING OJan 31, 1995 · N8NR · Rkwell NA26560 · Fuel Quantity Sensor
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