N233US, cancelled Jul 23, 2001

Service difficulty reports · 36

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 = 'N233US' AND deregistration_id = 'N233US-2001-07-23'
  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 USAA001558Skin · crackedCLT - FOUND CRACK IN SKIN 2 INCHES, S16L BETWEEN STATION 727A AND 727B. INSTALLED REPAIR DOUBLER PER RM 53-30-3 FIG 17. (M)Sep 25, 2000 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00148Battery · dischargedCLT - FOUND EMERGENCY LIGHTS INOPERATIVE FROM ROW 1 THROUGH 6. MAINTENANCE REPLACED THE BATTERY PACK. (M)May 19, 2000 · N233US · Boeing 737201 · Emergency LightingSDR USAA000611Keelbeam · corrodedCLT - FOUND KEEL BEAM CORRODED 5 INCHES BY 9 INCHES BY .060 INCHES, BS 814 TO 814.5 STRINGER 27L KEEL BEAM. FABRICATED AND INSTALLED REPAIR PER EA 67056. (M)Apr 26, 2000 · N233US · Boeing 737201 · Fuselage Main, KeelSDR USAA000559Skin · corrodedCLT - FOUND CORROSION ON SKIN 6 INCHES BY 2 INCHES, STATINO 807 BETWEEN STRIGNER 26R AND 27R. INSTALLED FILLER AND DOUBLER PER SRM 53-10-4 AND 53-30-03. CORROSION LEVEL 1. (M)Apr 14, 2000 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000560Skin · corrodedCLT - FOUND SKIN CORROSION, STATION 827 BETWEEN STRINGER 26R AND 27R BELOW CARGO DOOR. REPAIRED PER SRM 53-10-4. CORROSION LEVEL 1. (M)Apr 14, 2000 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000546Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STATION 505, STRINGER 16L. INSTALLED FILLER AND DOUBLER CHANNEL PER EA 67037. (M)Apr 12, 2000 · N233US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB99255unknownGSO - FLT 2660 - UPON PUSHBACK, THE NR 1 TRU C/B TRIPPED. THE NR 1 ENG GEN READ ZERO AMPS AND ZERO VOLTS. CREW RESET THE NR 1 TRU C/B ALONG WITH THE NORMAL EQUIP BLOWER C/B'S THAT HAD ALSO TRIPPED AND THE NR 1 GEN CAME ON LINE. HOWEVER, EN ROUTE FROM ATL TOOct 20, 1999 · N233US · Boeing 737201 · AC Generation SystemSDR USAASB99212Line · failedMCO FLT 2692 - SHORTLY AFTER TAKEOFF FROM MCO, AFTER GEAR AND FLAP RETRACTION, THE 'A' HYDRAULIC SYSTEM LOW PRESSURE LIGHT AND MASTER CAUTION LIGHT FLICKERED. HYDRAULIC QUANTITY RAPIDLY WENT TO ZERO. AIRCRAFT LEVELED OFF AT 5,000 FEET AS CREW ACCOMPLISHED CHAug 28, 1999 · N233US · Boeing 737201 · Hydraulic System, MainSDR USAASB99196Connector · failedBWI - FLT 2620 - AFTER TAKEOFF, THE STANDBY HYDRAULIC QTY LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGNCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CANNON PLUG FOR THE STANDBY HYDRAULIC LOW QUANTIAug 9, 1999 · N233US · Boeing 737201 · Hydraulic Quantity SensorSDR USAA990662Skin · crackedCLT - DURING A PILOTS REPORT VISUAL INSPECTION CHECK, FOUND A 2. 5 FT CRACK JUST BELOW STRINGER 21L FROM STATION 978 TO 980 IN FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-30-03 FIG 6 AND EA 65015. (M)Jun 30, 1999 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB99132Ballast · failedALB - FL 548 - AFTER TAKEOFF, AT APPROXIMATELY 2,000 FEET, CREW NOTICED SMOKE IN THE COCKPIT. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO FIELD AT ALB. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE BALLAST FOR THE ENMay 30, 1999 · N233US · Boeing 737201 · Passenger Compartment LightingSDR USAA990086Skin · crackedTPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 2.75 INCH CRACK IN EXTERNAL SKIN STATION 727B PLUS 4 INCHES AND STRINGER 17R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 25. (M)Feb 12, 1999 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990085Skin · crackedTPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN DOOR SKIN FORWARD SERVICE DOOR UPPER HINGE CUTOUT DOOR EXT SKIN. INSTALLED DOUBLER PER SB 737-32-1016, EA 63767 AND TR 52-40-03A. (M)Feb 12, 1999 · N233US · Boeing 737201 · Service DoorsSDR USAASB99004Light · failedDCA - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT AT THE AFT ENTRY DOOR FLICKERS OFF AND ON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ABOVE THE AFT ENTRY DOOR. OPERATIONAL CHECK GOOD. (M)Jan 5, 1999 · N233US · Boeing 737201 · Emergency LightingSDR USAASB98307Light · inoperativeCLT - MAINTENANCE FOUND THE AFT LEFT EMERGENCY EXIT LIGHT WOULD NOT TURN OFF WHEN THE AIRCRAFT WAS POWERED DOWN. MAINTENANCE REPLACED THE AFT LEFT ENTRY DOOR OVERHEAD EMRGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. (M)Nov 19, 1998 · N233US · Boeing 737201 · Emergency LightingSDR USAA980434Skin · crackedCLT - DURING PCI 1703 CHECK VISUAL AND HFEC, FOUND A .375 INCH LONG CRACK FUSELAGE STATION 947 RIGHT AFT SERV DOOR LOWER HINGE CUTOUT OF SKIN. INSTALLED DOUBLER PER EA62590. (M)Sep 20, 1998 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB98227Batteries · dischargedALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE AFT PASSENGER ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPERATIONAL CHECK GOOD. (M)Sep 3, 1998 · N233US · Boeing 737201 · Emergency LightingSDR USAASB98104Light · inoperativePIT - PILOT REPORTED THE AFT RIGHT-HAND EMERGENCY EXIT LIGHT ABOVE THE AFT SERVICE DOOR IS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT-HAND EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (X)May 3, 1998 · N233US · Boeing 737201 · Emergency LightingSDR USAA980114Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 15 INCH CORROSION ON STR 25R FROM STA 360 - STA 340. INSTALLED NEW STRINGER, REPAIRED PER SRM 53-10-3 FIG 1. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980113Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .0625 INCH CRACK BS 304 BETWEEN S9L AND S10L SKIN. (EDDY CURRENT). INSTALLED DOUBLER, REPAIRED PER EA 43634. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980112Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .0625 INCH CRACK FORWARD ENTRY DOOR FUSELAGE LOWER AFT CORNER WL 207, STA 344 SKIN. INSTALLED DOUBLER, REPAIRED PER BOEING DWG 65C27257. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980111Floorbeam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK BS 663 BL ZERO WL 205 FLOORBEAM WEB. INSTALLED DOUBLER, REPAIRED PER BAC DRAWING NR 65C34537. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980110Frame · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK IN BODY FRAME RADIUS BS 294.5, 5 INCHES BELOW S26R. INSTALLED FRAME REPAIR, REPAIRED PER SRM 51-40-3. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, FrameSDR USAA980109Stringer · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT 2 SKIN ATTACH FASTENER HOLES 5 INCHES TO 11 INCHES FOWARD OF BS 540 FRAME S15L STRINGER (FUSELAGE). INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1 AND EA 43631. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980108Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT 2 EACH SKIN ATTACH FASTENER HOLES 7 INCHES AND 8 INCHES FORWARD OF BS 540 FRAME S15R STRINGER FUSELAGE. INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3 FIG 1 AND EA 43631. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980107Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 379 BETWEEN BL ZERO AND S28L SKIN (FUSELAGE). INSTALLED DOUBLER, REPAIRED PER TR 53-30-04. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB98012Bypass Sw · failedBOS - FLT 786 - CLIMBING OUT FROM BOS ABOUT 8,000 FEET, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CREW SHUT DOWN THE NR 1 ENGINE, DECLARED AND EMERGENCY AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIMJan 14, 1998 · N233US · Boeing 737201 · Engine Oil Indicating SystemSDR 98ZZZM203Connector · dirtyBOS - FLT 786 - CLIMBING OUT FROM BOS ABOUT 8,000 FEET, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CREW SHUT DOWN THE NR 1 ENGINE, DECLARED AND EMERGENCY AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIMJan 14, 1998 · N233US · Boeing 737201 · Engine Oil Indicating SystemSDR USAASB98005Seal · failedBWI - FLT 2299 - FLT DEPARTED MHT THEN DIVERTED TO BWI DUE TO HYDRAULIC SYSTEM QTY DROPPING BELOW REFILL LINE. HYDRAULIC SYSTEM WAS SERVICED AND CHECKED FOR LEAKS. NO LEAKS WERE NOTED. FLIGHT THEN DEPARTED BWI AND RETURNED TO FIELD SHORTLY THEREAFTER DUE TOJan 6, 1998 · N233US · Boeing 737201 · Drag Control ActuatorSDR USAASB97306Separator · iced upPIT - FL 253 - EN ROUTE CLT TO BUF AT FL310, CABIN ALT WARNING HORN SOUNDED WITH CABIN ALT INDICATING 10,000 FT. CREW ATTEMPTED TO REGAIN CONTROL OF CABIN IN STANDBY AND MANUAL MODE BUT CABIN CONTINUED TO CLIMB. CREW BEGAN A DESCENT TO 10,000 FT AND DECLAREDNov 7, 1997 · N233US · Boeing 737201 · Humidity Control SystemSDR 97ZZZM1207Sensor · malfunctionedPIT - FL 253 - EN ROUTE CLT TO BUF AT FL310, CABIN ALT WARNING HORN SOUNDED WITH CABIN ALT INDICATING 10,000 FT. CREW ATTEMPTED TO REGAIN CONTROL OF CABIN IN STANDBY AND MANUAL MODE BUT CABIN CONTINUED TO CLIMB. CREW BEGAN A DESCENT TO 10,000 FT AND DECLAREDNov 7, 1997 · N233US · Boeing 737201 · Cabin Pressure Control SystemSDR 97ZZZM1206Valve · malfunctionedPIT - FL 253 - EN ROUTE CLT TO BUF AT FL310, CABIN ALT WARNING HORN SOUNDED WITH CABIN ALT INDICATING 10,000 FT. CREW ATTEMPTED TO REGAIN CONTROL OF CABIN IN STANDBY AND MANUAL MODE BUT CABIN CONTINUED TO CLIMB. CREW BEGAN A DESCENT TO 10,000 FT AND DECLAREDNov 7, 1997 · N233US · Boeing 737201 · Cabin Pressure Control SystemSDR USAASB97083Fuel Heat Mnfld · failedRSW - FL 1115, ON TAKEOFF ROTATION, CREW RECEIVED ON OVERHEAT DETECTION LIGHT FROM THE NR 2 ENGINE. CREW CONTINUED TAKEOFF, WENT THROUGH PROCEDURES AND RETURNED TO FIELD AT RSW. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE NMar 19, 1997 · N233US · Boeing 737201 · Engine Anti-Icing SystemSDR USAASB96226Windshield · crackedPIT - FL 820 - ON CLIMB-OUT, CAPTAINS FORWARD WINDSHIELD ARCED AND THEN CRACKED. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD. (M)Nov 9, 1996 · N233US · Boeing 737201 · Flight Compartment WindowsSDR USAA960334Stringer · corrosionROA - DURING CX-4 CHECK VISUAL INSPECTION FOUND 2 INCH BY 20 INCH CORROSION STRINGER 27 LEFT FROM BS 947 TO BS 967 DUE TO LAV SPILLS. REMOVED DAMAGED SECTION OF STRINGER. FABRICATED NEW STRINGER, DOUBLERS, SPLICES AND SHIMMS, INSTALLED SAME. REPAIRED PER SRMar 24, 1996 · N233US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB96046Light · failedFLT NR 492 - PHL - FOUND OVERWING EXIT LIGHT INOP AT LEFT AISLE SEAT EXIT. MAINTENANCE REPLACED LIGHT ASSEMBLY. (M)Mar 11, 1996 · N233US · Boeing 737201 · Emergency Lighting
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