# Service difficulty reports: North American NA-265-60 A list on [North American NA-265-60](https://openairdocs.org/model/north-american-na-265-60.md). Newest first. General aviation reporting is voluntary. - [SDR UVVR2012101700028](https://openairdocs.org/sdr/UVVR2012101700028.md): Longeron · corroded · Dec 24, 2013 · N11LX · Rkwell NA26560 · Fuselage Main, Longeron/Stringer > DURING VISUAL INSPECTION OF COCKPIT FLOORS LOWER LONGERONS. FOUND CORROSION LT LOWER LONGERON CORRODED & SIGN OF EXFOLIATION FROM FS 108-134. - [SDR 2012FA0000643](https://openairdocs.org/sdr/2012FA0000643.md): Stiffener · cracked · Sep 17, 2012 · Rkwell NA26560 · Fuselage Miscellaneous Structure > WHILE 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. - [SDR 2009FA0000877](https://openairdocs.org/sdr/2009FA0000877.md): Valve · failed · Mar 17, 2009 · N11LX · Rkwell NA26560 · Landing Gear Retraction/Extension System > ACFT 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 LOCATE - [SDR 2008FA0000663](https://openairdocs.org/sdr/2008FA0000663.md): Pump · worn · Aug 26, 2008 · Rkwell NA26560 · Engine Fuel Pump > AFTER 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 MADE - [SDR 2007FA0001032](https://openairdocs.org/sdr/2007FA0001032.md): Duct · deformed · Oct 22, 2007 · N59K · Rkwell NA26560 · Air Distribution System > ATTACHING 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) - [SDR UVVR200600001](https://openairdocs.org/sdr/UVVR200600001.md): Nut · cracked · Feb 21, 2006 · N71CC · Rkwell NA26560 · Wing Spar > WHILE 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 PRECAUTION - [SDR CAR110](https://openairdocs.org/sdr/CAR110.md): Mixing Valve · not bonded · Jun 4, 2005 · Rkwell NA26560 · Cabin Pressure Control System > HOT 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 EQUIP - [SDR WK42004F00003](https://openairdocs.org/sdr/WK42004F00003.md): Tire · damaged · Feb 10, 2004 · N353CA · Rkwell NA26560 · Tire > CENTER 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). - [SDR WK42004F00001](https://openairdocs.org/sdr/WK42004F00001.md): Tire · damaged · Feb 10, 2004 · N353CA · Rkwell NA26560 · Tire > CENTER TREAD CHUNKED AFTER 23 LANDINGS ON RT HAND TIRE. - [SDR T2C2004F00000](https://openairdocs.org/sdr/T2C2004F00000.md): Casting · cracked · Feb 4, 2004 · N789SG · Rkwell NA26560 · Rudder Control System > DURING 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 A - [SDR 20000516SH026](https://openairdocs.org/sdr/20000516SH026.md): Fairing · corroded · Apr 25, 2000 · N39CB · Rkwell NA26560 · Aerodynamic Fairings > DURING 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 OFF - [SDR 20000516SH025](https://openairdocs.org/sdr/20000516SH025.md): Fairing · corroded · Apr 25, 2000 · N39CB · Rkwell NA26560 · Aerodynamic Fairings > DURING 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 OFF - [SDR 20000516SH024](https://openairdocs.org/sdr/20000516SH024.md): Fairing · corroded · Apr 25, 2000 · N39CB · Rkwell NA26560 · Aerodynamic Fairings > DURING 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 OFF - [SDR 20000516SH023](https://openairdocs.org/sdr/20000516SH023.md): Fairing · corroded · Apr 25, 2000 · N39CB · Rkwell NA26560 · Aerodynamic Fairings > DURING 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 OFF - [SDR 2000ZZZX27](https://openairdocs.org/sdr/2000ZZZX27.md): Switch · out of rig · Dec 7, 1999 · N66GE · Rkwell NA26560 · Landing Gear Retraction/Extension System > CREW 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. - [SDR 99ZZZX3469](https://openairdocs.org/sdr/99ZZZX3469.md): Thermostat · failed · Aug 6, 1999 · N400JH · Rkwell NA26560 · Engine Oil Indicating System > THERMOSTAT INSTALLED ON A FRESHLY OVERHAULED ENGINE. ENGINE WAS OVERHAULED BY FAA CRS OTUR438L. PART DID NOT FAIL UNTIL ONE HOUR INTO FIRST FLIGHT. - [SDR 96ZZZX1360](https://openairdocs.org/sdr/96ZZZX1360.md): Blade · overlap · Feb 9, 1996 · N401MS · Rkwell NA26560 · Turbine Section > DUE 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 ELECTE - [SDR 96ZZZX1359](https://openairdocs.org/sdr/96ZZZX1359.md): Blade · rub · Feb 9, 1996 · N401MS · Rkwell NA26560 · Turbine Engine Compressor Section > DURING 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 - [SDR 95ZZZX5865](https://openairdocs.org/sdr/95ZZZX5865.md): Actuator · leaking · Oct 4, 1995 · N113T · Rkwell NA26560 · Engine Thrust Reverser > REMOVED 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. - [SDR 95ZZZX5864](https://openairdocs.org/sdr/95ZZZX5864.md): Actuator · leaking · Oct 4, 1995 · N113T · Rkwell NA26560 · Engine Thrust Reverser > REMOVED 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. - [SDR 95ZZZX5863](https://openairdocs.org/sdr/95ZZZX5863.md): Actuator · leaking · Oct 4, 1995 · N113T · Rkwell NA26560 · Engine Thrust Reverser > REMOVED 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. - [SDR 95ZZZX6460](https://openairdocs.org/sdr/95ZZZX6460.md): Wheel Assy · rim bolts loose · Sep 4, 1995 · N2MIL · Rkwell NA26560 · Wheel/Ski/Float > NOSE 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, O - [SDR 95ZZZX5314](https://openairdocs.org/sdr/95ZZZX5314.md): Guide Vane · burned · Aug 28, 1995 · N8NR · Rkwell NA26560 · Turbine Section > ENGINE 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 RESUL - [SDR 95ZZZX906](https://openairdocs.org/sdr/95ZZZX906.md): Probe · cracked · Jan 31, 1995 · N8NR · Rkwell NA26560 · Fuel Quantity Sensor > PILOTS 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 O ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/model/north-american-na-265-60/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.