N235US, cancelled Mar 20, 2007

Service difficulty reports · 26

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 = 'N235US' AND deregistration_id = 'N235US-2007-03-20'
  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 RYNA200600001Link · brokenON CLIMB FROM UTA, POP AND VIBRATION WAS HEARD UNDER PILOT SEAT. AIRCRAFT DIVERTED TO MEM, LANDED WITHOUT INCIDENT. GEAR INSPECTED FOR SUSPECTED BIRD STRIKE, NO EVIDENCE OF DAMAGE FOUND. AIRCRAFT DEPARTED MEM, ON CLIMB TWO POPS AND VIBRATION WERE HEARD UNDEJan 10, 2006 · N235US · Boeing 737201 · Landing Gear Door Retract SectionSDR RYNA200500014Potable Water · leakingDURING CRUISE AT FL 28.0, EXPERIENCED MULTIPLE MALFUNCTIONS. AUTO-PILOT FAILED, PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED, MACH TRIM FAIL LIGHT ILLUMINATED, ALTITUDE ALERTER FAILED, CAPTAIN'S IVSI FLAG IN VIEW, CAPTAIN'S ALTIMETER FLAG IN VIEW AND LAV SINK WApr 9, 2005 · N235US · Boeing 737201 · Potable Water SystemSDR USAA001015Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, AT FS 747 AND STRINGER 17L LT EXTERIOR SKIN. REPAIRED DOUBLER PER SRM 53-30-3 FIG 1, 17 AND EA 67683. (M)Jul 20, 2000 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000851Skin · crackedTPA - FOUND FUSELAGE SKIN CRACKED 3.5 INCHES, LT FUSELAGE SKIN STATION 727A PLUS 13 JUST BELOW STRINGER 17. INSTALLED REPAIR DOUBLER PER SRM 53-30-03 FIG 1. (M)Jun 15, 2000 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000680Skin · crackedCLT - SKIN CRACKED 3.125 INCHES, LT FUSELAGE EXT SKIN BETWEEN BS 770 AND BS 773, STR 17L. INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 6. (X)May 10, 2000 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000261Skin · crackedSKIN HAS A 3 INCH CRACK AT BS 727B STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 53-30-6 FIG 6. (M)Feb 24, 2000 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00035Harness · chafedDTW - FLT 517 - INBOUND TO DTW FROM CLT, THE NR 1 GENERATOR BUS OFF LIGHT ILLUMINATED WITH LOSS OF ASSOCIATED SYSTEMS. THE AIRCRAFTS APU WAS ON MEL FOR NOT BEING ABLE TO START. THIS RESULTED IN THE AIRCRAFT BEING REDUCED TO ONE POWER SOURCE AVAILABLE. CAPT Feb 8, 2000 · N235US · Boeing 737201 · AC Generation SystemSDR USAA990953Skin · crackedCLT - DURING WALKAROUND CHECK, VISUAL INSPECTION, FOUND A .625 INCH CRACK IN SKIN AT STATION 380 2 INCHES LEFT OF CENTER LINE. INSTALLED REPAIR DOUBLERS PER TR 53-30-04, DRAWING 65C3390. (M)Sep 10, 1999 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990850Shear Tie · corrodedTPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND CORROSION ATTACH ANGLE SHEAR TIP STRINGER 26L STATION 967 FRAME. CORROSION LEVEL 1. REINSTALLED STRINGER SHEAR TIP PER SRM 53-10-3. (M)Aug 15, 1999 · N235US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA990849Skin · crackedTPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND A 1 INCH CRACK IN SKIN AT STATION 727A PLUS 7 AND STRINGER 19L. REPAIRED PER SRM 53-30-3 FIG 1. (M)Aug 15, 1999 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990848Skin · crackedTPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND A 4 INCH CRACK IN SKIN AT STATION 727B PLUS 14 AND STRINGER 18L. REPAIRED PER SRM 53-30-3 FIG 25. (M)Aug 15, 1999 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980398Skin · crackedCLT - DURING CHECK VISUAL INSPECTION, FOUND A 2 INCH SKIN CRACK 1 INCH ABOVE STR 16L 1 INCH TO 3 INCHES FORWARD OF STA 727B ON SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 PAGE 2B, 2C, 2D, AND 2E. (X)Sep 12, 1998 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB98217Indicator · malfunctionedTYS - FLT 1797 - AT 29,000 FT, THE NR 1 ENGINE OIL QTY SLOWLY DROPPED TO ONE GALLON AND EVENTUALLY TO A HALF GALLON. ALL OTHER INDICATIONS WERE NORMAL. FLIGHT DIVERTED TO TYS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND THE NR 1 ENGINEAug 21, 1998 · N235US · Boeing 737201 · Engine Oil QuantitySDR 98ZZZM819Transmitter · malfunctionedTYS - FLT 1797 - AT 29,000 FT, THE NR 1 ENGINE OIL QTY SLOWLY DROPPED TO ONE GALLON AND EVENTUALLY TO A HALF GALLON. ALL OTHER INDICATIONS WERE NORMAL. FLIGHT DIVERTED TO TYS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND THE NR 1 ENGINEAug 21, 1998 · N235US · Boeing 737201 · Engine Oil QuantitySDR USAASB98175Battery Pack · dischargedALB - MAINTENANCE FOUND THE AFT ENTRY AND AFT SERVICE DOOR EXTERIOR EVACUATION LIGHTS AND THE INTERIOR SIDEWALL EMERGENCY EXIT SIGNS BY EACH DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE RIGHT SIDE OF THE AFT CARGO COMPARTMENT BEHIND THEJul 10, 1998 · N235US · Boeing 737201 · Emergency LightingSDR USAA980281Angle · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 727 RBL 6.5 ATTACH ANGLE. REPAIRED PER SRM 51-10-1. (M)Jun 23, 1998 · N235US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA980280Beam · frettedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 20 INCH FRETTED AREA BETWEEN BS 663-727 BEAM. INSTALLED REPAIR STRAP AND REPAIRED PER EA 44092. (M)Jun 23, 1998 · N235US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA980297Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1.3750 INCH AREA OF CORROSION ON FLOORBEAM STA 106 LBL 18. INSTALLED T-CAP PER TR 53-10-05C. (X)Jun 22, 1998 · N235US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980017Skin · crackedROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER SKIN. DOUBLER REPAIR INSTALLED, REPAIRED PER EA 61143. (M)Jan 16, 1998 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980016Skin · crackedROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK STRINGER 24L, STATION 945 SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)Jan 16, 1998 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB97250Proximity Sensor · defectivePHL (FL 993) - DURING CLIMB-OUT WITH FLAPS RETRACTED,THE NR 4 LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD (PHL). NO EMERGENCY WAS DELCARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 4 KRUEGER FLAP PSep 11, 1997 · N235US · Boeing 737201 · Leading Edge Slat Position Indicating SystemSDR USAASB96228Oil Gauge · failedBWI - FL 322 - AFTER TAKEOFF, THE NR 2 ENGINE OIL PRESSURE WENT FROM LOWER GREEN LINE TO MID YELLOW BAND. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX REPLACED THE NR 2 ENGINE OIL PRESSURE GAUGE AND TRANNov 16, 1996 · N235US · Boeing 737201 · Engine Oil PressureSDR 96ZZZM1563Oil Transmitter · failedBWI - FL 322 - AFTER TAKEOFF, THE NR 2 ENGINE OIL PRESSURE WENT FROM LOWER GREEN LINE TO MID YELLOW BAND. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX REPLACED THE NR 2 ENGINE OIL PRESSURE GAUGE AND TRANNov 16, 1996 · N235US · Boeing 737201 · Engine Oil PressureSDR USAA960689Skin · crackedINT - DURING B-CHECK, EDDY CURRENT INSPECTION, FOUND .120 INCH CRACK LOWER FORWARD CORNER OF FORWARD SERVICE DOOR LOWER CUT OUT IN RADIUS SKIN. INSTALLED DOUBLER AND REWORKED PER EA AND SRM. REPAIRED PER EA 41649, SRM 53-30-3 FIG 32. (M)Oct 20, 1996 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960608Skin · crackedCLT - INSPECTION VISUALLY FOUND 1 INCH AND 1.4 INCH SKIN CRACKS LOCATED AT STATION 727A, 2 INCH AND PLUS 7 INCH IN THE FUSELAGE SKIN, RIGHT BL 70 BETWEEN STRINGER 17 AND 18. INSTALLED DOUBLER AS PER BOEING SRM 53-10-1 AND 53-30-3. (M)Sep 13, 1996 · N235US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB96148Snubber · misinstalledPHL - FL 351 - DURING CLIMB-OUT, FLIGHT ATTENDANT REPORTED AN EXCESSIVE NOISE COMING FROM THE FORWARD MAIN ENTRANCE DOOR. THE CAPTAIN INDICATED THE CABIN WAS PRESSURIZING TOO SLOWLY AND DECIDED TO RETURN TO THE FIELD AT PHL. THE FLIGHT LANDED WITH NO FURTHERAug 6, 1996 · N235US · Boeing 737201 · Passenger/Crew Doors
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