Boeing 727-1A7C

Service difficulty reports · 118

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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 aircraft_model_key = '7271A7C'
  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 UPS07249687Duct · blownEMERGENCY DECLARED, LWR AFT BODY OVERHEAT WARNING LIGHT ILLUM. ALL EPR INDICATIONS INOP. STDBY HYD OVERHEAT LT ILLUM. CAPT'S RADIO INTERMITTENT CREW WAS ASKED TO DEVIATE DUE TO WEATHER, BUT DECLARED EMERGENCY DUE TO VARIOUS MALFUNCTIONS. FOUND BLOWN DUCT IApr 24, 2007 · N935UP · Boeing 7271A7C · Air Distribution SystemSDR UPS06247519Web · crackedCRACK FOUND ON I/B WEB OF REMOVABLE LEADING EDGE AT BS 740 RT. DAMAGED AREA REMOVED AND REPAIR CARRIED OUT IAW SRM 51-40-2.Jul 26, 2006 · N935UP · Boeing 7271A7C · Leading Edge DevicesSDR UPS06247593Skin · corrodedINSPECTION TYPE:C HTD B-NUT HAS FRETTED SKIN IN HYD BAY AT BS 1000 AT STR 23 LEFT. MEASURED AND EVALUATED FRETTED SKIN AND FOUND OUT OF LIMITS IAW SRM 53-30-01. PREVIOUS REPAIR REMOVED IAW SRM 51-30-02. DAMAGE REPAIRED IAW SRM 53-30-3.Jul 14, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Plate/SkinSDR UPS06247457Carriage · wornINSPECTION TYPE:C WEAR IN NR 7 FLAP CARRIAGE SIDE ROLLER ASSY BRACKETS. FLAP CARRIAGE REPLACED IAW MM 27-51-13.Jul 14, 2006 · N935UP · Boeing 7271A7C · Trailing Edge FlapsSDR UPS06247428Link · corrodedINSPECTION TYPE:C NR 5 FLAP CARRIAGE BEARING LINK BEARING A DRIFT AND BUSHING CORRODED. CORROSION FOUND ON INNER SURFACE OF BEARING LINK. BEARING LINK ASSY AND BUSHING REPLACED IAW MM 27-51-03.Jul 14, 2006 · N935UP · Boeing 7271A7C · Trailing Edge FlapsSDR UPS06247460Seat Track · corrodedINSPECTION TYPE:C SEAT TRACK AT RBL 40 2 BETWEEN BS 740-760 CORRODED. CORROSION FOUND OUT OF LIMITS IAW SRM 51-30-02. REPLACED SEAT TRACK IAW SRM 51-30-02.Jul 13, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06247456Carriage · wornINSPECTION TYPE:C NR 8 FLAP CARRIAGE AFT SIDE ROLLERS FWD ATTACH HOLES WORN. FLAP CARRIAGE REPLACED IAW MM 27-51-13.Jul 13, 2006 · N935UP · Boeing 7271A7C · Trailing Edge FlapsSDR UPS06247436Beam · corrodedINSPECTION TYPE:C SIDE LOAD BEAM AT RIGHT BS 740 CORRODED. ANGLE FABRICATED IAW DRWG 65-15940. INSTALLED SIDE LOAD BEAM ANGLE IAW B727-5310-7477.Jul 13, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous StructureSDR UPS06247434Carriage · corrodedINSPECTION TYPE:C NR 4 FLAP CARRIAGE FWD LOWER FLANGE CORRODED. FLAP CARRIAGE REPLACED IAW MM 27-51-03.Jul 13, 2006 · N935UP · Boeing 7271A7C · Trailing Edge FlapsSDR UPS06247386Carriage · corrodedINSPECTION TYPE:C NR 5 FLAP CARRIAGE HAS CORROSION ON LWR FWD FLANGE UPPER AND LOWER SURFACES CARRIAGE REPLACED IAW MM 27-51-03.Jul 13, 2006 · N935UP · Boeing 7271A7C · Trailing Edge FlapsSDR UPS06247385Carriage · corrodedINSPECTION TYPE-C, 3 SEQUENCE CARRIAGE HAS CORROSION ON AFT UPPER LUGS SEQUENCE CARRIAGE REPLACED IAW MM 27-51-04.Jul 12, 2006 · N935UP · Boeing 7271A7C · Trailing Edge FlapsSDR UPS06247373Floor Support · crackedINSPECTION TYPE-C AND SI FLOOR SUPPORT CRACKED AT BS 850 RBL 24.75. FLOOR SUPPORT REMOVED IAW SRM 51-30-02. NEW FLOOR SUPPORT FABRICATED I AW SRM 51-40-03. FLOOR SUPPORT PROTECTED IAW SRM 51-10-02. FLOOR SUP PORT PAINTED AND INSTALLED IAW SRM 51-40-03, 51-3Jul 12, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous StructureSDR UPS06247433Flap Track · corrodedINSPECTION TYPE:C CORROSION IN \1 FLAP TRACK HOLES E, D AND C. BUSHING FABRICATED IAW AAAE EO 2006-042-005. HEAT TREATMENT REFERENCE 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.Jul 11, 2006 · N935UP · Boeing 7271A7C · Trailing Edge FlapsSDR UPS06247429Flap Track · corrodedINSPECTION TYPE:C CORROSION IN NR 6 FLAP TRACK HOLES G AND F. BUSHINGS FABRICATED IAW AAAE-EO-2006-042-08. HEAT TREATED IAW 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.Jul 11, 2006 · N935UP · Boeing 7271A7C · Trailing Edge FlapsSDR UPS06247375Floorbeam · corrodedINSPECTION TYPE-C AND SI CORROSION ON UPPER SURFACE OF FLOORBEAM UPPER FLANGE REPAIR AT BS 560 LBL 37. CORROSION REMOVED IAW SRM 51-10-6 AND FOUND TO BE OUT OF LIMITS. REPA IR STRAP REMOVED, NEW REPAIR STRAP FABRICATED IAW SRM 51-20-1. REPAIR STRAP REPROTEJul 11, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Floor BeamSDR UPS06247353Support · corrodedINSPECTION TYPE: C AND SI CORROSION ON INTERCOSTAL SUPPORT CONTROL CABIN FLOOR, BL 0, FS 277 TO 29 4.5. CORROSION CLEANED AND SUPPORT FOUND TO BE OUTSIDE LIMITS. NEW SUPPORT FABRICATED IAW BOEING DRG 65-17593. NEW SUPPORT INSTALLED IAW SRM 51-30-2 WITH REFEJul 11, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous StructureSDR UPS06247568Structure · corrodedINSPECTION TYPE:C EVIDENCE OF CORROSION AT BS 850 RT UNDER STR 18A. FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-06. FASTENER REINSTALLED IAW SRM 51-30-02.Jul 10, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, StructureSDR UPS06247463Seat Track · corrodedINSPECTION TYPE:C EVIDENCE OF EXFOLIATION CORROSION ON UPPER FLANGE OF SEAT TRACK AT BS 690-720 RBL 65. CORROSION OUT OF LIMITS IAW SRM 53-10-01. SEAT TRACK REPLACED IAW SRM 51-30-02.Jul 10, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06247432Attach Fitting · corrodedINSPECTION TYPE:C CORROSION ON NR 7 FLAP TRACK ATTACH PAD HOLE E. BUSHING FABRICATED IAW EO 2006-042-0009. HEAT TREATMENT REFERENCE 06-4 2-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.Jul 10, 2006 · N935UP · Boeing 7271A7C · Trailing Edge FlapsSDR UPS06247431Attach Fitting · corrodedINSPECTION TYPE:C NR 8 FLAP TRACK ATTACH PAD HAS CORROSION IN HOLES E, D AND C. BUSHINGS FABRICATED FOR HOLES IAW AAAE EO 2006-042-10. HEAT TREATMENT REFERENCE 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.Jul 10, 2006 · N935UP · Boeing 7271A7C · Trailing Edge FlapsSDR UPS06247381Web · crackedINSPECTION TYPE-C SI RT WING STRUCTURE INNER WEB CRACKED AT NR 8 SLAT ACTUATOR CUTOUT, REPAIR OR REPLACE. REPAIRED IAW SRM 51-40-02 FIG 1.Jul 10, 2006 · N935UP · Boeing 7271A7C · Wing Miscellaneous StructureSDR UPS06247365Seat Track · corrodedINSPECTION TYPE-C AND SI EVIDENCE OF EXFOLIATION CORROSION ON UPPER FLANGE OF SEAT TRACK AT BS 5 92 RBL 45. NEW SEAT TRACK FABRICATED, PAINTED AND INSTALLED IAW MM 51-20-90 AND SRM 51-30-2, 53-10-5, AND 51-10-2.Jul 10, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06247364Seat Track · crackedINSPECTION TYPE-C AND IS CRACKED ON SEAT TRACK TOP BS 397 RBL 23 NEW SEAT TRACK FABRICATED, PAINTED AND INSTALLED IAW MM 51-21-90, SRM 5 1-10-2 AND 51-30-2.Jul 10, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06247626Skin · damagedINSPECTION TYPE:C SMALL NICK ON FUSE SKIN, DAMAGE LOCATED AT BASE OF C, D WINDOW POST. FASTENERS REMOVED FROM REPAIR AREA AND DAMAGE BLENDED OUT IAW SRM 53-30 -03. REPAIR DOUBLER INSTALLED IAW SRM 53-30-03.Jul 8, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Plate/SkinSDR UPS06247462Stiffener · corrodedINSPECTION TYPE:C CORROSION ON FLOOR STRUCTURE STIFFENER AT RT SIDE AT BS 230 RBL 36. STIFFENER REPLACED IAW SRM 51-30-02.Jul 8, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous StructureSDR UPS06247374Intercostal · corrodedINSPECTION TYPE-C AND SI CORROSION AROUND ANCHOR NUT HOLE UNDER COCKPIT DOOR SILL BS 303. REMOVED INTERCOSTAL UNDER COCKPIT DOOR IAW SRM 51-30-02. FABRICATED I NTERCOSTAL IAW SRM 51-20-1. INTERCOSTAL REPROTECTED IAW SRM 51-10-2. INTERCOSTAL PAINTED IAW MM Jul 8, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous StructureSDR UPS06247352Intercostal · gougedINSPECTION TYPE: C AND SI DEEP GOUGE ON UPPER SURFACE OF INTERCOSTAL BETWEEN BS 328 AND 334 LBL 30. DEEP GOUGE ON INTERCOSTAL REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-6. INTERCOSTAL REMOVED AND NEW INTERCOSTAL INSTALLED IAW SRM 51-30-2 AND DRG 6Jul 8, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous StructureSDR UPS06247351Intercostal · gougedINSPECTION TYPE: C AND SI DEEP GOUGE ON UPPER SURFACE OF INTERCOSTAL BETWEEN BS 312 - 328 LBL 30. DEEP GOUGE ON INTERCOSTAL REMOVED AND FOUND TO BE OUTSIDE LIMITS OF SRM 51-10-6. INTERCOSTAL REMOVED AND REPLACED IAW MM 51-20-90.Jul 8, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous StructureSDR UPS06247520Rib · crackedSUSPECT CRACK ON NR 6 SLAT ON 4TH RIB OB OF ACTUATOR AT UPPER AFT CORNER RIB REPLACED IAW SRM 51-30-02.Jul 7, 2006 · N935UP · Boeing 7271A7C · Leading Edge DevicesSDR UPS06247518Rib · crackedSUSPECT CRACK ON NR 6 SLAT ON 1ST RIB O/B OF I/B TRACK ALONG AFT FLANGE. RIB REPLACED IAW SRM 51-10-02, AND INSTALLED IAW SRM 51-30-02.Jul 7, 2006 · N935UP · Boeing 7271A7C · Leading Edge DevicesSDR UPS06247437Rib · crackedINSPECTION TYPE:C SUSPECT CRACK ON NR 5 SLAT 3RD RIB O/B OF IB TRACK AT AFT UPPER CORNER. SLAT REPLACED.Jul 7, 2006 · N935UP · Boeing 7271A7C · Leading Edge DevicesSDR UPS06247366Seat Track · corrodedINSPECTION TYPE-C AND SI CORROSION ON SEAT TRACK TOP CHORD BS 590-630 LBL 45.5 NEW SEAT TRACK FABRICATED, PAINT AND INSTALLED IAW MM 51-20-90, SRM 51- 30-2, 53-10-5Jul 7, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06247636Wedge · delaminatedRT O/B AILERON HAS DELAM ON TRAILING EDGE WEDGE. AILERON BEYOND REPAIRABLE LIMITS, AILERON REPLACED IAW MM 27-10-14.Jul 6, 2006 · N935UP · Boeing 7271A7C · AileronsSDR UPS06247569Structure · corrodedINSPECTION TYPE:C SURFACE CORROSION AT BOTH I/B STATIC DISCHARGERS LEFT WING TIP T/E. CORROSION REMOVED IAW SRM 51-10-01 AND FASTENERS REMOVED IAW SRM 51-3 0-02. AREA O/B FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01. DAMAGED AREA REPAIRED IAW SRM 57-20-05. Jul 6, 2006 · N935UP · Boeing 7271A7C · Wing Main, Frame StructureSDR UPS06247566Fitting · crackedINSPECTION TYPE:C BS 740 TERMINAL FITTING REQUIRES REPLACING. FITTING REPLACED IAW EO B727-5310-7477 AND DRWG 65C13724.Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Attach FittingsSDR UPS06247464Seat Track · corrodedINSPECTION TYPE:C CORROSION ON SEAT TRACK TOP CHORD AT BS 950-962 RBL 62.5. CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-01. SEAT TRACK REPLACED IAW SRM 51-30-02.Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06247461Floorbeam · corrodedINSPECTION TYPE:C CORROSION ON FLOORBEAM TOP CHORD BS 950 RBL 51-56. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-10-06 AND 53-1001. FLOORBEAM TOP CHORD REPLACED IAW SRM 51-30-02.Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Floor BeamSDR UPS06247455Panel · delaminatedINSPECTION TYPE:C LT WING UPPER SURFACE PANEL FWD OF NR 5 AND 6 SPOILERS DELAM AT PREVIOUS REPAIR. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 51-40-20. PANEL REPLACED IAW SRM 51-30-02.Jul 6, 2006 · N935UP · Boeing 7271A7C · Wing, Plate/SkinSDR UPS06247430Floorbeam · corrodedINSPECTION TYPE:C CORROSION ON FLOORBEAM TOP CHORD BS 420 RBL 52-55. SPLICE ANGLE AND FILLER INSTALLED IAW SRM 53-10-8.Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Floor BeamSDR UPS06247384Seat Track · corrodedINSPECTION TYPE-C CORROSION ON SEAT TRACK TOP BS 418-427 RBL 45.5. SEAT TRACK REPLACED IAW SRM 53-10-05 AND SRM 51-30-02.Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06247369Floorbeam · corrodedINSPECTION TYPE-C AND SI CORROSION ON FLOORBEAM TOP CHORD BS 328 LBL 27-31 CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10-1. NEW FLOOBEAM TOP CHORD FABRICATED, PAINTED AND INSTALLED IAW MM 51-21-90 AND SRM 53-10-8.Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Floor BeamSDR UPS06247368Floorbeam · corrodedINSPECTION TYPE-C AND SI CORROSION ON FLOORBEAM TOP CHORD BS 344 LBL 16-23 CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-6. FLOORBEAM TOMP P CHORD FABRICATED, PAINTED AND INSTALLED IAW SRM 53-10-08 AND MM 51-21- 90.Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Floor BeamSDR UPS06247354Fitting · crackedINSPECTION TYPE: C AND SI CRACKS DETECTED ON BS 740 STR 18R - STR 24R. ON INVESTIGATION CRACKS FOUND TO BE OUTSIDE LIMITS IAW SB 727-53-0062. REFERENCE NRC 100347 FOR BS 740 FITTING REPLACEMENT.Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous StructureSDR UPS06247567Channel · corrodedINSPECTION TYPE:C AFT SUPPORT CHANNEL FOR APU EXHAUST ON THE LOWER SIDE UPPER WING PANEL IS CORRODED. CHANNEL REPLACED IAW SRM 51-20-01.Jul 5, 2006 · N935UP · Boeing 7271A7C · APU Exhaust SystemSDR UPS06247383Seat Track · corrodedINSPECTION TYPE-C CORROSION ON SEAT TRACK, TOP CHORD BS 481 RBL 45.5 CORROSION FOUND OUTSIDE LIMITS IAW SRM 53-10-1. SEAT TRACK AND CONNECT OR REPLACED IAW SRM 53-10-05 AND SRM 51-30-02.Jun 11, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06247382Flap Track · corrodedINSPECTION TYPE-C CORROSION IN NR 5 FLAP TRACK HOLE G. CORROSION REMOVED IAW OHM 57-40-01. MPI CARRIED OUT IAW BSOPM 20-20-0 1. BUSHING FABRICATED IAW EO 20065-042-007. STYLUS CAD PLATING CARRIED OUT IAW SOPM 20-42-10. INSTALLED BUSHING IAW SOPM 20-50-03.Jun 11, 2006 · N935UP · Boeing 7271A7C · Trailing Edge FlapsSDR UPS05243879Angle · crackedLT WING PANEL ON UPPER SURFACE ABOVE NR 1 TRANSMISSION AFT FAIRING I/B ANGLE AND REPAIR CRACKED. ANGLE REPLACED IAW SRM 51-30-01 AND 51-30-02.Feb 3, 2005 · N935UP · Boeing 7271A7C · Wing Miscellaneous StructureSDR UPS05243890Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 680 LBL 56 FOUND ON REMOVAL OF FLOOR PANELS FOR DOOR SILL INSPECTION. REPAIR CARRIED OUT IAW SRM 51-10-2, 53-10-8, 51-20-4 AND AAAE EO 2005-01 0-004 UPS ENGINEERING FILE NR 727-53-20183.Feb 2, 2005 · N935UP · Boeing 7271A7C · Fuselage Main, Floor BeamSDR UPS05243888Angle · crackedAFT AIRSTAIRS ANGLE CRACKED AT FORWARD SIDE OF BS 1203 FRAME LT AT S13L. STOP DRILLED CRACK IAW 51-10-1. HFEC CARRIED OUT IAW NDTM PT6 51-00 -00, CRACK CONTAINED BY STOP DRILLED HOLE. REFER TO UPS FILE NUMBER 727-53-20182.Feb 1, 2005 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous StructureSDR UPS05243878Casting · crackedNR 8 SPOILER I/B END HINGE CASTING IS CRACKED AT FASTENER HOLE. HINGE CASTING REPLACED IAW SRM 51-30-2.Feb 1, 2005 · N935UP · Boeing 7271A7C · Spoilers
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