N225US, cancelled Mar 6, 2017

Service difficulty reports · 35

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 = 'N225US' AND deregistration_id = 'N225US-2017-03-06'
  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 RYNA200600002Engine · bird ingestionBIRD INGESTION INTO NR 1 ENGINE OCCURRED DURING LANDING, AFTER MAIN WHEELS TOUCHED DOWN AND BEFORE NOSE WHEEL TOUCHED DOWN. THUD WAS HEARD IN COCKPIT. AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. UPON INSPECTION FOUND NR 1 ENGINE DAMAGED BEYOND REPAIR Feb 3, 2006 · N225US · Boeing 737201 · Engine (Turbine/Turboprop)SDR RYNA200500022Oil System · overtempDURING CLIMB-OUT, NR 2 ENGINE OIL TEMP INCREASED TO 122 DEG C. DURING DESCENT, OIL TEMP INCREASED TO 140 DEG C. OIL TEMP IN YELLOW BAND FOR 5 MINUTES. OIL PRESSURE WAS NORMAL IN CLIMB AND CRUISE. NR 2 ENGINE SHUTDOWN AS A PRECAUTION BECAUSE OIL TEMP COULD NOTJul 6, 2005 · N225US · Boeing 737201 · Engine Oil TemperatureSDR RYAN200500020Speed Brake · wornSPEED BRAKE TAKEOFF WARNING SWITCH WORN/BROKEN. SWITCH NOT MAKING CONTACT WHEN SPEED BRAKE ARMED, CAUSING A FALSE TAKEOFF WARNING TO SOUND WHEN THROTTLES ARE ADVANCED.Jul 3, 2005 · N225US · Boeing 737201 · Engine Thrust ReverserSDR RYNA200500011Seal · out of adjustAFTER TAKEOFF FROM TUS, A LOUD SQUEAL AND PRESSURIZATION LEAK WAS DETECTED AT THE L-1 DOOR. THE AIRCRAFT WAS RETURNED TO TUS AND LANDED WITHOUT INCIDENT. ADJUSTED L-1 DOOR SEAL. LEAK CHECK GOOD DURING FLIGHT TEST.Apr 2, 2005 · N225US · Boeing 737201 · Passenger/Crew DoorsSDR RYNA200500010Autopilot Sys · malfunctionedIMMEDIATELY AFTER TAKEOFF FROM TUS, THE AUTOPILOT PORPOISED IN PITCH. THE AIRCRAFT WAS RETURNED TO TUS AND LANDED WITHOUT INCIDENT. AMENDMENT TO BE FILED UPON COMPLETION OF TROUBLESHOOTING AND CORRECTIVE ACTION.Apr 2, 2005 · N225US · Boeing 737201 · Autopilot SystemSDR USAA011301Stringer · corrodedCLT - FOUND STRINGER CORRODED 1.5 INCH BY 13 INCHES, STRINGER 27L BETWEEN STATION 900 AND 913. INSTALLED DOUBLER AND SECTION OF STRINGER. (M)Sep 12, 2001 · N225US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA000801Skin · crackedTPA - FOUND SKIN CRACKED .25 INCH, STATION 920 PLUS 1.5 JUST ABOVE STRINGER 22L AFT FUSE. INSTALLED DOUBLER PER 53-30-3 PAGES 2C, 2D, 2E. (M)Jun 5, 2000 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00108Gearbox · leakingCLT - FLT 365 - ON CLIMB-OUT FROM CLT, THE NR 1 ENGINE OIL QTY WENT TO ZERO RESULTING IN AN INFLIGHT SHUTDOWN OF THE NR 1 ENGINE. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE Apr 8, 2000 · N225US · Boeing 737201 · Turbine Engine Oil SystemSDR USAA000388Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 15L FASTENER HOLES BS 538. INSTALLED REPAIR FILLER AND DOUBLER PER EA 66891. (M)Mar 21, 2000 · N225US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA000387Skin · crackedCLT - FOUND SKIN CRACKED 1.25 INCHES, BS 538, 1 INCH BELOW STRINGER 14L. INSTALLED DOUBLER PER EA 66891. (M)Mar 21, 2000 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00022Battery Pack · dischargedSYR - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT, IN THE FORWARD CEILING, CYCLING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Jan 25, 2000 · N225US · Boeing 737201 · Emergency LightingSDR USAA991028Stringer · corrodedCLT - DURING A RON VISUAL INSPECTION FOUND CORROSION 9 INCHES BY 2 INCHES BY .075 INCH AT BS 500B PLUS 14 INCHES, STR 28R STRINGER (KEEL BEAM). CORROSION LEVEL 2. REMOVED CORROSION, INSTALLED KEEL BEAM REPAIR ANGLES AND SHIMS PER EA 65660. (X)Sep 24, 1999 · N225US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA991027Skin · corrodedCLT - DURING A RON VISUAL INSPECTION, FOUND CORROSION APPROXIMATELY 2 INCH BY 8 INCH AT BS 500B PLUS 14 INCHES, STR 28R SKIN. DAMAGE CUT-OUT AND INSTALLED DOUBLER AND FILLER PER SRM 53-30-03 FIG 6. (X)Sep 24, 1999 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990673Skin · crackedTPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN SKIN AT STATION 727B AND STRINGER 18L, SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)Jul 10, 1999 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990663Seat Track · corrodedTPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND MINOR CORROSION AT FORWARD END OF LEFT SEAT TRACK INBOARD AND OUTBOARD, CORROSION LEVEL 1. SPLICED IN AND FABRICATED REPAIR PARTS PER SRM 53-10-5 FIG 2. (M)Jul 3, 1999 · N225US · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR USAASB98215Battery Pack · dischargedPHL - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Aug 13, 1998 · N225US · Boeing 737201 · Emergency LightingSDR USAA980008Skin · crackedROA - DURING BX-1 CHECK VISUAL INSPECTION, FOUND 1.75 INCH CRACK STATION 935 STRINGER 24L SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)Jan 10, 1998 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB97124Fuel Pump · failedCLT - FL1173, ON CLIMB-OUT AT APPROX 1,200 FT, THE NR 1 ENG LOST THRUST. THE LOW OIL PRESS LIGHT CAME ON WITH NO OTHER INDICATIONS. CAPTAIN PERFORMED SINGLE ENGINE FAILURE CHECKLIST AND SHUTDOWN THE NR 1 ENGINE. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TMay 7, 1997 · N225US · Boeing 737201 · Engine Fuel PumpSDR USAA960680Stringer · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION APPROX 2 INCH BY 2 INCH STATION 947.5 STRINGER 27L. REPLACED STRINGER FROM STATION 940 TO 1016, REPAIRED PER SRM 53-10-3. CORROSION TASK NR 53-202-01, CORROSION LEVEL 1. (M)Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960679Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.24 INCH CRACK EXT SKIN LBL 3 BS 380. INSTALLED DOUBLER, REPAIRED PER TR 53-30-04. (M)Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960678Frame · crackDURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK FRAME STATION 767 AT STRINGER 21 LEFT. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-4. (M)Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, FrameSDR USAA960677Web · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO CRACKS APPROX 1 INCH LONG EACH IN VERTICAL WEB STATION 706 LBL 24. INSTALLED DOUBLER AND ANGLES, REPAIRED PER SRM 51-40-2. (M)Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960676Web · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACKS APPROXIMATELY 1 INCH LONG IN VERTICAL WEB STATION 706 RBL 24. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960675Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2.875 INCH CRACK IN SKIN BS 727B AT STRINGER 17R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER. REPAIRED PER SRM 53-30-3. (M)Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960674Former · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STATION 500 A STRINGER 26 R FORMER. INSTALLED DOUBLER REPAIR, REPAIRED PER SRM 51-40-3, CORROSION TASK NR C53-208-01, CORROSION LEVEL 1. (M)Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960673Frame · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 CRACKS .25 INCH AND .375 INCH FORWARD SERVICE DOOR AFT FRAME 1 AT NR 3 STOP, 1 AT NR 4 STOP. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (M)Oct 18, 1996 · N225US · Boeing 737201 · Service DoorsSDR USAA960672Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK BS 754 ABOVE STRINGER 18R FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6 AND EA 58706. (M)Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960671Keel Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 SCREW HOLES CORRODED .25 INCH AROUND OPENINGS, BS 720-725 RIGHT FLANGE UPPER SIDE KEEL BEAM. INSTALLED DOUBLER AFTER SPOT FACING, REPAIRED PER EA NR 41637. CORROSION TASK NR C53-212-01, CORROSION LEVEL 1. (MOct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, KeelSDR USAASB96167Door Tape · detachedCLT - FL 1024 - CREW AND PASSENGERS HEARD A LOUD THUMPING NOISE COMING FROM THE TOP OF THE AIRCRAFT DURING CLIMB. AT APPROX 5,000 FEET, CREW DECIDED TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE DISCOVERED DUCT TAPE AT UPPERAug 23, 1996 · N225US · Boeing 737201 · Passenger/Crew DoorsSDR USAA960427Skin · crackedROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK FUSELAGE SKIN AT BS 727 A BETWEEN STRINGER 15 AND 16 LEFT. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 PAGE 01. (M)May 8, 1996 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA951335Skin · delaminationINT - DURING 'DROP IN-AV' VISUAL/ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES AND LOCATIONS, FROM BS 727-908 LEFT WINDOW BELT PANEL BS 727-908 LEFT SIDE. REPLACED UPPER ROW OF FASTENERS BS 727-908 S-14 L. REPAIRED PER EA 31780. (M)Dec 15, 1995 · N225US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB95003Fuel Pump · failedPHL - FL 330, CLIMBING OUT OF LGA, AT FL 280, THE LEFT ENGINE SHUT DOWN AND COULD NOT BE RESTARTED. FLIGHT DIVERTED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN FUEL PUMP FAILED AND REPLACED IT. (M)Oct 23, 1995 · N225US · Boeing 737201 · Engine Fuel PumpSDR USAA950926Stringer · corrodedINT - DURING 'CD-6' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BETWEEN STATION 967 AND 986.5 AT S-27L. INSTALLED REPAIR SPLICES. REPAIRED PER SRM 53-10-3. (M)Jul 20, 1995 · N225US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA950925Stringer · corrodedINT - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND 4 INCH BY 2 INCH CORRODED AREA BETWEEN STATION 947.5 AND 967 AT S-26L. INSTALLED REPAIR SPLICES. REPAIRED PER SRM 53-10-3. (M)Jul 20, 1995 · N225US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA950212Eel Assembly · inoperativeGSO - EMERGENCY LIGHT OVER DOOR 2L INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY. (Z)Mar 5, 1995 · N225US · Boeing 737201 · Emergency Lighting
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