N240AU, cancelled Feb 28, 2017

Service difficulty reports · 38

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N240AU' AND deregistration_id = 'N240AU-2017-02-28'
  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 RYAN20050018Warning System · activatedDURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN NR 1 ENGINE WAS SHUTDOWN.Jun 12, 2005 · N240AU · Boeing 737201 · Engine Oil Indicating SystemSDR RYAN200500018Bulb · faultyDURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN.Jun 12, 2005 · N240AU · Boeing 737201 · Engine Oil TemperatureSDR 193Bulb · malfunctionedDURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN.Jun 12, 2005 · N240AU · Boeing 737201 · Engine Oil TemperatureSDR RYNA200500003Intercostal · crackedMAIN CABIN FLOOR BEAM INTERCOSTAL CRACKED AT BS 328 TO 344, LBL 45. REPAIRED CRACKED INTERCOSTAL AT BS 328 TO 344, LBL 45.Jan 17, 2005 · N240AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR RYNA200500002Floorbeam · corrodedMAIN CABIN FLOOR BEAM, UPPER CHORD, UPPER SURFACE CORRODED AT BS 1006, LBL 29. REMOVED CORROSION ON FLOOR BEAM, FABRICATED, TREATED AND INSTALLED REPAIR PARTS.Jan 17, 2005 · N240AU · Boeing 737201 · Fuselage Main, Floor BeamSDR 2004F00170Line · leakingDURING CRUISE FROM GSO-ACY, EXPERIENCED A LOSS OF THE A-SYSTEM HYDRAULICS. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED AT ACY WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC FEED LINE. CONDUCTED 'A' SYSTEM TROUBLESHOOTING PROCEDURES FOR PUMP Mar 14, 2004 · N240AU · Boeing 737201 · Hydraulic System, MainSDR USAASB00177Indicator · failedCLE - FLT 1231 - ON APPROACH TO CLE, CREW WAS UNABLE TO EXTEND FLAPS. CREW ACCOMPLISHED GO AROUND AND QUICK REFERENCE HANDBOOK PROCEDURES. CREW RECEIVED PARTIAL FLAPS USING ALTERNATE FLAP METHOD. HAD FULL LEADING EDGE DEVICES AND 15 DEGREES FLAPS ON TRAILINJun 23, 2000 · N240AU · Boeing 737201 · Trailing Flap Position Indicating SystemSDR USAASB00169Connector · damagedIAD - FLT 797 - ON APPROACH TO IAD, THE FLAPS WOULD NOT EXTEND BEYOND 10 DEGREES. CRWE COMPLETED CHECK FOR FLAPS AND FIRST OFFICER WENT BACK INTO CABIN FOR VISUAL CHECK. INDICATOR REMAINED AT 10 DEGREES REGARDLESS OF FLAP HANDLE POSITION. FLIGHT LANDED WITHJun 17, 2000 · N240AU · Boeing 737201 · Trailing Flap Position Indicating SystemSDR USAASB00066Light · inoperativeORD - PILOT REPORTED THE EMERGENCY EVACUATION LIGHT AT SEAT ROW 16 ABC IS INOPERABLE AND THE WIRING UNDER SEAT 16C IS HANGING DOWN. MAINTENANCE REPAIRED WIRING AND RESECURED WIRING UNDER SEAT ROW 16C. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. (X)Mar 6, 2000 · N240AU · Boeing 737201 · Emergency LightingSDR USAA000196Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, BS 765, STRINGER 19R FUSELAGE SKIN. REPAIRED PER SRM 53-30-3 FIG 6. (M)Feb 15, 2000 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB98156Switch · failedPHL - FLT 452 - ON CLIMB-OUT FROM PHL, AT APPROX 5,000 FT, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. LIGHT REMAINED ON WHEN POWER WAS REDUCED TO IDLE THRUST ON THE NR 1 ENGINE. CREW SHUTDOWN THE NR 1 ENGINE IN FLIGHT AND RETURNED TO FIELD AT PHL WJun 25, 1998 · N240AU · Boeing 737201 · Engine Oil Indicating SystemSDR USAASB97327Wire · loosePHL - FLT 461 - PILOT REPORTED THAT THE SEAT LEVEL EMERGENCY EXIT LIGHTS BRIEFLY ILLUMINATED TWICE IN FLIGHT AND EXTINGUISHED ONTHEIR OWN. MAINTENANCE INSPECTED BATTERY PACKS AT ROWS 5, 11 AND 16L AND COULD NOT DUPLICATE FAULT. OPERATIONAL CHECK WAS NORMAL ANov 28, 1997 · N240AU · Boeing 737201 · Light System WiringSDR USAASB97320Battery Pack · dischargedCLT - FLT 596 - PILOT REPORTED, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS. OPS CHECK GOOD. (M)Nov 21, 1997 · N240AU · Boeing 737201 · Emergency LightingSDR USAASB97268Battery Pack · dischargedPHL - FOUND LEFT HAND ENTRY OVERHEAD EMERGENCY LIGHT INOPERABLE; BOTH EMERGENCY SLIDE LIGHTS (FORWARD LEFT) INOPERABLE AND THE LEFT HAND OVERWING EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD. (X)Sep 28, 1997 · N240AU · Boeing 737201 · Emergency LightingSDR USAA970264Skin · crackedROA - DURING 'A' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN A/C SKIN, SKIN WAS CRACKED AT STRINGER 24L BETWEEN STATION 924 AND 947. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3. (M)Aug 15, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970263Stringer · corrodedROA - DURING 'A' CHECK VISUAL INSPECTION, FOUND CORRODED AREA IN STRINGER 2 INCHES LONG STRINGER 28L, STATION 372. REPLACED DEFECTIVE PORTION OF STRINGER, REPAIRED PER SRM 53-10-3. (M)Aug 15, 1997 · N240AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA970262Skin · crackedROA - DURING 'A' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1 INCH SKIN CRACK BS 378 BETWEEN BL 0 AND STRINGER 28L. INSTALLED DOUBLER REPAIR, REPAIRED PER TYPICAL REPAIR 53-30-04. (M)Aug 15, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB97190Link Assembly · brokenRDU - FL 607 - IMMEDIATELY FOLLOWING ROTATION, DURING GEAR RETRACTION, THE FLIGHT CREW HEARD A LOUD BANG NOISE FOLLOWED BY A VERY LOUD RUSH OF AIR. THE FIRST OFFICER OBSERVED AND OBJECT TO GO PAST THE WINDSCREEEN. CREW ASSUMED IT WAS A BIRDSTRIKE AND RETURNEJul 14, 1997 · N240AU · Boeing 737201 · Landing Gear Door Retract SectionSDR USAASB97158Power Supply · failedCLT - FL354, EMERGENCY EXIT LIGHTS ON LEFT FORWARD SEATS COME ON DURING FLIGHT AND STAY ON, EVEN IF EMERGENCY EXIT SWITCH IS TURNED OFF. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AT ROW 11 AND 16. OPERATIONAL CHECK GOOD. (M)Jun 10, 1997 · N240AU · Boeing 737201 · Emergency LightingSDR USAASB97154Diode · failedPHL - AFTER ENGINE SHUTDOWN, THE SEAT MOUNTED EMERGENCY LIGHTS ILLUMINATED. MAINTENANCE REPLACED A SYSTEM DIODE. (M)Jun 8, 1997 · N240AU · Boeing 737201 · Emergency LightingSDR USAASB97153Batteries · dischargedBDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE IN FORWARD AND MID CABIN AREAS. MAINTENANCE REPLACED TWO BATTERY PACKS. (M)Jun 7, 1997 · N240AU · Boeing 737201 · Emergency LightingSDR USAASB97136Lights · malfunctionedDCA - FLT 1727 - FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHTS IN THE CABIN ILLUMINATED DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH, SEVERAL BATTERY PACKS AND CLEANED THE EMERGENCY EXIT SWITCHES. SYSTEMS OPS CHECK GOOD. (M)May 22, 1997 · N240AU · Boeing 737201 · Emergency LightingSDR USAASB97133Battery · dischargedCLT - FLT 7900 - DURING TEST FLIGHT AFTER HEAVY MAINTENANCE VISIT, THE LOW LEVEL EMERGENCY EXIT LIGHTS FROM SEAT ROW 7 AND BACK ILLUMINATED. AFTER LANDING, THE AFT MOST LIGHTS WENT OUT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACKS AT SEMay 21, 1997 · N240AU · Boeing 737201 · Emergency LightingSDR USAA970203Stringer · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT OUTER AREA OF STRINGER WHERE MATES W/SKIN 15 INCHES LONG BY 1 INCH WIDE, SOME AREAS COMPLETELY THROUGH STRINGER, STATION 360-375 STRINGER 25L. INSTALLED NEW SEGMENT OF STRINGER, REPAIRED PER SRM 53-May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA970202Doubler · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND BELL CRANK CUTOUT DOUBLERS CRACKED STATION 677, RBL 25 AND LBL 25 STATION 677, RBL 25 AND LBL 25. INSTALLED NEW REINFORCEMENTS IN AREA, ACCOMPLISHED EO 5791G632, PART 3B. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA970201Frame · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 639 STRINGER 16L FRAME. INSTALLED REPAIR PER DRAWING 65C31658. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, FrameSDR USAA970200Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH AND .25 INCH CRACK LOWER HINGE CUT OUT UPPER AND LOWER CORNERS (FWD ENTRY DOOR) SKIN. INSTALLED DOUBLERS, REPAIRED PER TR 52-10-05. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970199Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK LOWER FORWARD CORNER OF FORWARD CARGO DOOR CUTOUT SKIN. INSTALLED DOUBLER, REPAIRED PER EA 42403. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970198Stringer · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED AREA BS 919, STRINGER 25L. SPLICED STRINGER, REPAIRED PER SRM 53-10-3. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA970197Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AFT SERVICE DOOR UPPER HINGE CUTOUT UPPER FORWARD CORNER SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970196Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACKS 4 INCHES AND 2 INCHES AT STRINGER 18R STATION 727 A PLUS 16 INCHES AND STRINGER 18R STATION 727 A PLUS 3 INCHES SKIN. INSTALLED ONE DOUBLER FOR BOTH CRACKS PER SRM 53-30-03 FIG 6. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970195Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK LEFT UPPER CORNER OF CAPTAINS NR 1 WINDOW FRAME FLIGHT COMPARTMENT SKIN. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR, REPAIRED PER SRM 53-30-3 FIG 11. (M)May 21, 1997 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970058Bracket · crackedCLT - I NSPECTION VISUALLY FOUND A 3 INCH CRACK LOCATED AT RADIUS OF SUPPORT BRACKET, FOR NLG ACTUATOR SUPPORT BEAM AFT END. FABRICATED REPAIR BRACKET AS PER SRM 51-40-03. (M)Feb 10, 1997 · N240AU · Boeing 737201 · Landing Gear ActuatorSDR USAA960693Skin · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION STRINGER 26R BS 797 FUSELAGE SKIN. REMOVED CORROSION AND INSTALLED DOUBLER. REPAIRED PER SRM 53-30-3 FIG 6. CORROSION TASK NR C53-100-01, CORROSION LEVEL 2. (M)Oct 26, 1996 · N240AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB96109Oil Press Ind · failedBWI - FLT 2539 - ABOUT 50 MILES OUT OF BWI, THE CREW OBSERVED ZERO OIL PRESSURE ON THE NR 1 ENGINE. ALL OTHER INDICATIONS WERE NORMAL. FLIGHT RETURNED TO FIELD AT BWI. THE ENGINE WAS NOT SHUT DOWN AND NO EMERGENCY EQUIPMENT WAS CALLED OUT. THE FLIGHT LANDEJun 15, 1996 · N240AU · Boeing 737201 · Engine Oil PressureSDR USAA951134Stringer · corrosionCLT - DURING A PCI INSPECTION, A 10 INCH BY 1 INCH CORROSION WAS FOUND AT STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. REPLACED END STRINGER 28R, RBL 6. (M)Sep 18, 1995 · N240AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA951089Stringer · corrodedCLT - DURING A PCI INSPECTION, FOUND CORROSION 10 INCHES BY 1 INCH ON STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. CORROSION TASK NR C53-202-02/PCI 1227, CORROSION LEVEL 2. REPLACED END STRINGER 28R, RBL 6. (M)Sep 18, 1995 · N240AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA950748Hydraulic Line · leakingROC - FLT 2274 - UPON GEAR RETRACTION ON TAKEOFF, A-SYSTEM QUANTITY WENT TO ZERO AND A-SYSTEM LOW PRESSURE LIGHTS CAME ON. FLIGHT RETURNED TO ROC WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE LEAKING AT RT MAIN GEAR UPLOCK CYCJul 8, 1995 · N240AU · Boeing 737201 · Hydraulic System, Main
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