N266US, cancelled Sep 26, 2013

Service difficulty reports · 44

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 = 'N266US' AND deregistration_id = 'N266US-2013-09-26'
  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 2002F00644Regulator · malfunctionedDURING CLIMB-OUT OF PHL, GEN 1 BTB, GB AND FIELD LIGHTS ILLUMINATED FOLLOWED ABNORMAL PROCEDURES DUMPED 22,000 LBS RETURNED TO AIRPORT ONE GENERATOR ALREADY ON DMI SWAPPED RN 1 AND NR 2 VOLTAGE REGULATOR. OPS CHECK GOOD PER MM 24-20. AIRCRAFT RETURNED TO SERApr 12, 2002 · N266US · Boeing 727251 · AC RegulatorSDR 2002F00400Window · crackedR2 WINDOW OUTER PANEL CRACKED A/C DIVERTED TO KMIA FROM KMCO EN ROUTE TO CCS. REMOVED AND REPLACED R2 WINDOW PER MM 56-12-11 A/C RETURNED TO SERVICE. (M)Mar 27, 2002 · N266US · Boeing 727251 · Flight Compartment WindowsSDR 2002F00403Inverter · malfunctionedON PUSHBACK, POWER FLAG ON STANDBY ATTITUDE INDICTOR RERACKED STATIC INVERTER AND CLEANED CONNECTOR. OPS CHECKED NORMAL PER MM 34-25. A/C RETURNED TO SERVICE. (M)Mar 22, 2002 · N266US · Boeing 727251 · Attitude Gyro and Indicating SystemSDR 2002F00026Control Box · faultyDURING TAXIING SPEED BRAKE/FLAP WARNING TEST FAILED A/C RETURNED TO GATE AURAL WARNING BOX WAS REPLACED PER MM 31-26. AIRCRAFT WAS RETURNED TO SERVICE. (M)Nov 23, 2001 · N266US · Boeing 727251 · Central WarningSDR FX72001F00001Pin · looseUPON LANDING INC CCS, NOSE GEAR SCISSOR LINK CAME LOOSE. RECONNECTED PIN AND CONTINUE TO THE RAMP. PRECAUTIONARY REPLACED NLG APEX PIN RETURNED AIRCRAFT TO SERVICE.Jul 26, 2001 · N266US · Boeing 727251 · Nose/Tail Landing Gear Strut/AxleSDR 20010214SG001Mount Bracket · brokenON TAKEOFF FROM CAE SLAT INDICATION SHOWED RIGHT WING NR 3 SLAT EXTENDED. FLIGHT CREW RECYCLED THE FLAP SYSTEM AND SLAT REMAINED EXTENDED. CREW REPORTED HEARING A NOISE AND THEN LOSS OF THE ''''A'''' HYDRAULIC SYSTEM PRESSURE AND QT. THE CREW CONDUCTED A AIDec 31, 2000 · N266US · Boeing 727251 · Leading Edge Slat ActuatorSDR S84A2000001Light · inoperativeMBJ - FLT 302 - R1 DOOR O/H EMERGENCY LIGHT INOPERABLE. RESECURED OPS CHECK IAW 33-50-01. OPS CHECK GOOD. (X)Jan 2, 2000 · N266US · Boeing 727251 · Emergency LightingSDR 99ZZZX4172Bracket · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON GIRT BAR BASES NR 1 GALLEY.Oct 8, 1999 · N266US · Boeing 727251 · Emergency EquipmentSDR 99ZZZX4169Pin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON LEFT MAIN LANDING GEAR LOWER TORSION LINK PIN RETAINING PIN.Oct 6, 1999 · N266US · Boeing 727251 · Landing Gear Retraction/Extension SystemSDR 99ZZZX4168Floorbeam · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM UPPER T-CHORD LBL 24 AT STA 344.Oct 6, 1999 · N266US · Boeing 727251 · Fuselage Main, Floor BeamSDR 99ZZZX3957Seat Track · corrodedDURING A C-CHECK, CORROSION WAS NOTED AT FS 344 - FS 380 (RT) SEAT TRACK.Sep 27, 1999 · N266US · Boeing 727251 · Fuselage, Seat/Cargo Attach FittingsSDR 99ZZZX3956Channel · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON RT AFT LAVATORY WALL HAT CHANNEL AND ATTACH ANGLES.Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX3955Angle · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON RT AFT LAVATORY WALL HAT CHANNEL AND ATTACH ANGLES.Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX3954Channel · corrodedDURING A C-CHECK, CORROSION WAS NOTED LT AFT LAVATORY FORWARD WALL HAT CHANNEL AND SUPPORT ANGLES.Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX3953Angle · corrodedDURING A C-CHECK, CORROSION WAS NOTED LT AFT LAVATORY FORWARD WALL HAT CHANNEL AND SUPPORT ANGLES.Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX3952Floor Pan · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON FLOOR PAN, RT AFT LAVATORY.Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX3951Angle · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON T-ANGLE STA 812 KEEL BEAM.Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX3950Web · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON KEEL BEAM WEB STA 770.Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX3948Tie · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON TENSION TIES FS 1183 - 29R AND 23L.Sep 27, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX3949Tie · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON TENSION TIE STR 17 FS 1183.Sep 18, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX2917Frame · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT BS 1166 OUTBOARD OF MOP SILL AT FLOOR LEVEL.Jun 18, 1999 · N266US · Boeing 727251 · Fuselage Main, FrameSDR 99ZZZX2916Channel · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON FORWARD LAVATORY HAT CHANNEL.Jun 18, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX2915Floorbeam · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM FS 344, LBL 24 OUTBOARD.Jun 18, 1999 · N266US · Boeing 727251 · Fuselage Main, Floor BeamSDR 99ZZZX2914Web · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON SHEAR WEB UNDER BS 1176 CHORD LBL 25 - RBL 25.Jun 18, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX2913Seat Track · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK RT CENTER BS 344 - BS 460. (ALSO ON LT INBOARD).Jun 18, 1999 · N266US · Boeing 727251 · Fuselage, Seat/Cargo Attach FittingsSDR 99ZZZX2912Seat Track · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK BS 1070- BS 1130 LBL 48 AND LBL 25.Jun 18, 1999 · N266US · Boeing 727251 · Fuselage, Seat/Cargo Attach FittingsSDR 99ZZZX2228Skin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON EXTERIOR AFT FUSELAGE LAMP SEAM FS 1283 - FS 1343 BELOW NR 1 ENGINE PYLON.May 12, 1999 · N266US · Boeing 727251 · Fuselage Main, Plate/SkinSDR 99ZZZX2227Angle · corrodedDURING A C-CHECK, CORROSION WAS NOTED IN RADOME AREA FS 178 LOWER MOST Z-ANGLE LBL 18 TO RBL 18.May 12, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX2226Beam · corrodedDURING A C-CHECK, COROSION WAS NOTED ON RT HORIZONTAL STABILIZER, UPPER TRAILING EDGE BEAM.May 12, 1999 · N266US · Boeing 727251 · Horizontal Stabilizer StructureSDR 99ZZZX2225Skin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON UPPER SURFACE AFT EDGE OF RT INBOARD AFT FLAP (ABOVE NR 5 CANOE).May 12, 1999 · N266US · Boeing 727251 · Trailing Edge FlapsSDR 99ZZZX2224Beam · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON THE LEFT HORIZ STABILIZER, LOWER T/E BEAM BETWEEN NR 5 AND NR 6 ELEVATOR HINGES.May 12, 1999 · N266US · Boeing 727251 · Horizontal Stabilizer StructureSDR 99ZZZX2223Beam · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM ABOVE NR 7 ELEVATOR HINGE.May 12, 1999 · N266US · Boeing 727251 · Horizontal Stabilizer StructureSDR 99ZZZX2459Door · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON AFT LAVATORY SERVICE DOOR.May 1, 1999 · N266US · Boeing 727251 · Fixed Inner DoorsSDR 99ZZZX1750Angle · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON APU AIR INLET SCREEN MOUNT FLANGE (ANGLES).Apr 12, 1999 · N266US · Boeing 727251 · APU Cowling/ContainmentSDR 99ZZZX1749Hinge · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.Apr 12, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX1748Hinge · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.Apr 12, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX1747Hinge · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.Apr 12, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 99ZZZX1746Hinge · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.Apr 12, 1999 · N266US · Boeing 727251 · Fuselage Miscellaneous StructureSDR 98ZZZM296Pressurization · malfunctionedFLT 758 - DURING CLIMB-OUT, LOST PRESSURIZATION, AFTER DUMPING FUEL RETURNED TO KMIA, LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED FOR OPEN DOORS AND COMPARTMENTS, NONE FOUND, DOOR SEAL INSPECTED FOUND NORMAL. ACCOMPLISHED GROUND PRESSURIZATION CHECK, NORFeb 6, 1998 · N266US · Boeing 727251 · Cabin Pressure Control SystemSDR 97ZZZM573Bracket · failedMDSD - AT PUSHBACK FROM GATE, FOUND THE NOSE LANDING DOOR OPERATIONAL BRACKET BROKEN. INSPECTED DOOR OPERATIONAL ASSEMBLY AND AREA, FOUND NO ADDITIONAL DAMAGE. REPLACED DOOR OPERATOR BRACKET, RETURNED AIRCRAFT TO SERVICE. (M)Apr 7, 1997 · N266US · Boeing 727251 · Landing Gear Door Retract SectionSDR 97ZZZM574Outflow Valve · jammedFRY KBWI-KMIA - FLT F429 - DURING CLIMB STAGE LOST PARTIAL PRESSURIZATION. DESCENDED TO A LOWER ALTITUDE AND WERE ABLE TO HOLD PRESSURIZATION, LANDING UNEVENTFUL. INSPECTED AIRCRAFT FOR ABNORMAL CONDITIONS, FOUND ONE INSULATION BLANKET, P/N (6567242475) STUCApr 5, 1997 · N266US · Boeing 727251 · Pressure Regulator/Outflow ValveSDR 97ZZZM273Window · failedCAPTAIN'S SLIDING WINDOW (L2) ARCHING WITH WINDOW HEAT ON. NO ELECTRICAL FIRE, LANDING UNEVENTFUL. INSPECTED WINDOW AREA, NO EVIDENCE OF FIRE OR BURNING. REPLACED NR 2 LEFT SLIDING WINDOW. AIRCRAFT RETURNED TO SERVICE. (M)Feb 10, 1997 · N266US · Boeing 727251 · Flight Compartment WindowsSDR 96ZZZX3735Turbine · damagedKMIA - AFTER DEPARTURE DURING CLIMB STAGE, SEVERE VIBRATION ON NR 2 ENGINE. INITIATED EMERGENCY PROCDURES, SHUT DOWN NR 2 ENGINE, DUMPED FUEL AND RETURNED TO KMIA LANDING UNEVENTFULLY. FOUND NR 2 ENGINE TURBINE DAMAGED.Jun 8, 1996 · N266US · Boeing 727251 · Turbine SectionSDR 96ZZZX3734Connector · looseKMIA - AFTER DEPARTURE DURING CLIMB STAGE, UNABLE TO OBTAIN CABIN PRESSURE. DUMPED FUEL AND RETURNED TO KMIA LANDING UNEVENTFULLY. FOUND LOOSE ELECTRICAL CONNECTOR AT THE PNEUMATIC FLOW CONTROL/SHUT-OFF VALVE, P/N 39608831. TIGHTENED THE CONNECTOR, OPERATIOJun 3, 1996 · N266US · Boeing 727251 · Cabin Pressure Control System
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