Boeing 727-185C

Service difficulty reports · 425

Newest first. General aviation reporting is voluntary.

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 = '727185C'
  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 UPS02237500Flap Track · corrodedINSPECTION TYPE:C+SI NR 5 FLAP TRACK PITTING CORROSION ON AUX SPAR ATTACH PAD. TRACK REPLACED.Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237499Flap Track · corrodedINSPECTION TYPE:C+SI NR 4 FLAP TRACK PITTING CORROSION ON BORE OF AFT LT HOLE ON MLG SUPPORT BEAM PAD. FLAP TRACK REPLACED.Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237482Flap Track · corrodedINSPECTION TYPE:C+SI NR 4 FLAP TRACK, PITTING CORROSION ON BORE OF HOLE C AND ON COUNTER BORE OF HOLE C. TRACKS REPLACED.Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237481Flap Track · corrodedINSPECTION TYPE:C+SI NR 4 FLAP TRACK PITTING CORROSION ON AUX SPAR PAD. CORROSION ON PAD REMOVED BY MACHINING IAW OHM 57-40-01. TRACK REPLACED IAW 27-51-31.Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237479Flap Track · corrodedINSPECTION TYPE:C+SI NR 4 FLAP TRACK PITTING CORROSION ON FACE OF LANDING GEAR ATTACH PAD. LANDING GEAR ATTACH PAD MACHINED IAW OHM 57-40-01. TRACK REPLACED IAW MM 27-51-31.Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237476Flap Track · corrodedINSPECTION TYPE:C+SI NR 1 FLAP TRACK HAS PITTING CORROSION ON LT FWD SUPPORT LUG OUTER FACE. CORROSION REMOVED BY MACHINING IAW OHM 57-40-01. NDT COMPLIED WITH AND NDF IAW SOPM 20-20-01, FLAP PEENED IAW SOPM 20-10-03, STRESS RELIEVED IAW SOPM 20-10-02, CADPLJan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237463Fitting · corrodedINSPECTION TYPE:C+SI NR 7 FLAP TRACK WING SUPPORT FITTING HAS PITTING CORROSION ON INBOARD FACE OF LUG. CORROSION REMOVED, NDT COMPLIED WITH AND NDF. FLAP PEENED AND CADPLATED IAW OHM.Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237462Fitting · corrodedINSPECTION TYPE:C+SI RT WING NR 8 FLAP TRACK SUPPORT FITTING (WING FITTING) HAS PITTING CORROSION ON INBOARD FACE. CORROSION REMOVED BY MACHINING, NDT COMPLIED WITH AND NDF. FLAP PEENED AND CADPLATED IAW OHM.Jan 2, 2002 · N940UP · Boeing 727185C · Wing Miscellaneous StructureSDR UPS02237461Flap Track · corrodedINSPECTION TYPE:C+SI NR 6 FLAP TRACK PITTING CORROSION ON FACE OF AUX SPAR PAD. CORROSION REMOVED BY MACHINING IAW OHM 57-40-01. NDT COMPLIED WITH NDF SOPM 20-20-01, FLAP PEENED IAW SOPM 20-10-03, STRESS RELIEVED IAW SOPM 20-10-02, CADPLATED IAW SOPM20-42-10Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237460Flap Track · corrodedINSPECTION TYPE:C+SI NR 7 FLAP TRACK, PITTING CORROSION ON FWD SUPPORT LUG BORE LT LUG. BUSHING REMOVED AND CORROSION REMOVED BY MACHINING. NDT COMPLIED WITH AND NDF. BUSHING FABRICATED, HEAT TREATED, CADPLATED, POST BAKED AND INSTALLED.Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237474Bracket · crackedINSPECTION TYPE:C+SI NR 4 FLAP TRACK CRACK IN FAIRING SUPPORT BRACKET FWD LT . BRACKET FABRICATED AND REPLACED IAW SRM.Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237447Rib · crackedINSPECTION TYPE:C+SI CRACK IN ELEV SUPPORT RIB, O/B LWR AFT FLANGE AT ST 173.21 RT. RIB REPLACED.Dec 28, 2001 · N940UP · Boeing 727185C · Elevator, Spar/RibSDR UPS02237511Flap Track · corrodedINSPECTION TYPE:C+S,I NR 3 FLAP TRACK PITTING CORROSION ON AUX SPAR ATTACH PAD.Dec 21, 2001 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237459Flap Track · corrodedINSPECTION TYPE:C+SI NR 8 FLAP TRACK, PITTING CORROSION FOUND ON INNER FACE OF FWD SUPPORT LUG LT. CORROSION REMOVED BY MACHINING, NDT COMPLIED WITH AND NDF. FLAP PEENED AND CADPLATED IAW OHM.Dec 21, 2001 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237458Flap Track · corrodedINSPECTION TYPE:C+SI NR 8 FLAP TRACK, PITTING CORROSION ON OUTER FACE OF FWD SUPPORT LUG LT. CORROSION REMOVED BY MACHINING, NDT COMPLIED WITH NDF FLAP PEENED IAW OHE AND CADPLATED IAW OHM.Dec 21, 2001 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237457Flap Track · corrodedINSPECTION TYPE:C+SI PITTING CORROSION ON INNER FACE OF FWD SUPPORT LUG LT NR 7 FLAP TRACK. CORROSION REMOVED BY MACHINING NDT COMPLIED WITH AND NO DEFECTS WERE FOUND. FLAP PEENED AND CADPLATED IAW OHM.Dec 21, 2001 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237445Flap Track · corrodedINSPECTION TYPE:C+SI, NR 7 FLAP TRACK LOOSE BUSHING ON FWD SUPPORT LUG RT, LOOSE BUSHING REMOVED AND BORE FOUND CORRODED. PITTING CORROSION REMOVED BY MACHINING IAW SOPM 20-10-02. NDT C/W NDF. BUSHING FAB'D THEN HEAT TREATED, CADPLATED, POSTBAKED AND INDec 21, 2001 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237545Crankshaft · corrodedINSPECTION TYPE:C AILERON PCU INPUT CRANK IN LT WHEEL WELL IS BADLY CORRODED AROUND PIVOT BOLT. PCU INPUT CRANK REPLACED IAW OHM 27-40-00 & OHM 29-00-00.Dec 20, 2001 · N940UP · Boeing 727185C · Aileron Control SystemSDR UPS02237450Carriage · corrodedINSPECTION TYPE:C+SI PITTING CORROSION IN FLT ROLLER BEARING MOUNT HOLES NR 1 FLAP CARRIAGE. CARRIAGE REPLACED IAW OHM 57-52-11.Dec 20, 2001 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237446Rib · crackedINSPECTION TYPE:C+SI CRACK IN ELEVATOR SUPPORT RIB AT ELEVATOR STA 17.20 LEFT I/B UPPER FLANGE. RIB REPLACED.Dec 20, 2001 · N940UP · Boeing 727185C · Elevator, Spar/RibSDR UPS02237537Skin · corrodedINSPECTION TYPE:C+SI RIVET HEAD POPPED AT STR 4R AT BS 710 APPROX. REPAIR CARRIED OUT IAW SRM.Dec 19, 2001 · N940UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS02237510Bushing · corrodedINSPECTION TYPE:C+SI, RT WING REAR TERMINAL FORGING FWD BUSHING IS CORRODED. RETAINER REPLACED IAW MM 57-41-11, BUSHING REPLACED IAW OHM20-50-03.Dec 19, 2001 · N940UP · Boeing 727185C · Wing Miscellaneous StructureSDR UPS02237469Carriage · corrodedINSPECTION TYPE:C+SI CORROSION ON FLT ROLLER BEARING MOUNT HOLE NR 5 FLAP CARRIAGE. CARRIAGE ASSY REPLACED IAW OHM.Dec 19, 2001 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237468Carriage · corrodedINSPECTION TYPE:C+SI CORROSION ON INNER SPINDLE BORE OF NR 7 FLAP CARRIAGE SPINDLE. REPLACED CARRIAGE ASSY IAW OHM.Dec 19, 2001 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237467Carriage · corrodedINSPECTION TYPE:C+SI CORROSION ON INNER BORE OF NR 8 FLAP CARRIAGE SPINDLE, AND ON END OF SPINDLE UNDER BEARING. CARRIAGE ASSY REPLACED IAW OHM.Dec 19, 2001 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237465Carriage · corrodedINSPECTION TYPE:C+SI NR 2 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BORE CORROSION CONFINED TO SPINDLE BORE, NOT POSSIBLE TO MEASURE EXTENT. CARRIAGE REPLACED AS NO REPAIR POSSIBLE IAW 57-52-01.Dec 19, 2001 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237473Frame · crackedINSPECTION TYPE:C+SI FRAME CRACKED AT BS 580 ATR STR 18L, ADJACENT TO MCD LATCH SUPPORT FITTINGS. CRACKED AREA CUT OUT AND REPAIR PARTS FABRICATED, REPAIR PARTS INSTALLED.Dec 19, 2001 · N940UP · Boeing 727185C · Fuselage Main, FrameSDR UPS02237472Frame · crackedINSPECTION TYPE:C+SI FRAME CRACKED AT BS 540 STR STR 18L ADJACENT TO MCD LATCH SUPPORT FITTING. DAMAGED AREA CUT OUT AND REPAIR PARTS FABRICATED, REPAIR PARTS INSTALLED.Dec 19, 2001 · N940UP · Boeing 727185C · Fuselage Main, FrameSDR UPS02237471Frame · crackedINSPECTION TYPE:C+SI FRAME CRACKED AT BS 500 AT STR 18L ADJACENT TO LATCH SUPPORT FITTINGS. REPAIR PARTS FABRICATED AND DAMAGED AREA CUT OUT. REPAIR PARTS INSTALLED IAW SRM, VERTICAL STIFFENER INSTALLED.Dec 19, 2001 · N940UP · Boeing 727185C · Fuselage Main, FrameSDR UPS02237470Frame · crackedINSPECTION TYPE:C+SI FRAME CRACKED AT BS 487.1 AT STR 19L ADJACENT TO LATCH SUPPORT FITTINGS. CRACKED AREA CUT OUT, REPAIR PARTS FABRICATED, PARTS INSTALLED AND VERTICAL STIFFENER INSTALLED.Dec 19, 2001 · N940UP · Boeing 727185C · Fuselage Main, FrameSDR UPS02237548Mount · corrodedINSPECTION TYPE:C+SI NR 3 ENGINE FWD MOUNT FWD OUTBOARD HOLE HAS PITTING CORROSION ON INSIDE OF BORE.Dec 18, 2001 · N940UP · Boeing 727185C · Engine Mount SectionSDR UPS02237543Spar · corrodedINSPECTION TYPE:C+SI WING CENTER SECTION FRONT SPAR UPPER CHORD HAS CORROSION AT RT END OF CHORD AT RBL 55 APPROX. FOUND TO BE EXFOLIATED.Dec 18, 2001 · N940UP · Boeing 727185C · Wing SparSDR UPS02237534Mount · corrodedINSPECTION TYPE:C=SI NR 1 ENGINE FWD TRUNNION MOUNT AFT OUTBOARD HOLE HAS PITTING CORROSION IN BORE OF HOLE.Dec 18, 2001 · N940UP · Boeing 727185C · Engine Mount SectionSDR UPS02237547Fitting · corrodedINSPECTION TYPE:C+SI VERTICAL FLANGE OF RT 740 FITTING AT I/B END HAS CORROSION. REPLACED FITTING IAW UPS EO B727-5310-7477 E AND DWG 65C13724.Dec 17, 2001 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS02237536Frame · crackedINSPECTION TYPE:C+SI SUSPECT CRACK IN MLG WW STRUCTURE AT BS 910 FWD FLANGE BELOW MLG CEILING. REPAIRED IAW EO B727-5310-1896B.Dec 17, 2001 · N940UP · Boeing 727185C · Fuselage Main, FrameSDR UPS02237529Fitting · corrodedINSPECTION TYPE:C+SI VERTICAL FLANGE OF LT 740 FITTING AT I/B END HAS CORROSION. LT 740 FITTING REPLACED IAW UPS EO B727-5310-7477E APPB AND DWG 65C 13724.Dec 17, 2001 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS01236605Control Unit · faultyINSPECTION TYPE:PFLT D/D M220970 LOWER AFT CARGO SMOKE DETECTOR. SUP SYS INOP. INSTALLED CONTROL UNIT IAW MM 26-18-04. REQUIRES ADJ/TEST KSM 55919 PERFORMED SMOKE DETECTOR / CONFIG MODULE ADJ/TEST MM 26-18-01 AND LOWER CARGO COMP SMOKE DETECTION ADJ/TEST MM Aug 11, 2001 · N954UP · Boeing 727185C · Smoke DetectionSDR UPS01236172Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACKS, OPS NORMAL.Jun 25, 2001 · N954UP · Boeing 727185C · Emergency LightingSDR UPS01235475Unknown · odorSMOKE ODOR IN FLT DECK AREA. RAN ALL 3 ENGINES AND OPERATED ALL PACKES AT FULL HOT AND COLD. COULD NOT DUPLICATE. OPERATED ALL NAV AND COMM EQUIPMENT. NO DEFECTS NOTED. OK TO CONTINUE SERVICEMar 30, 2001 · N940UP · Boeing 727185C · Air Distribution SystemSDR UPS01235092Fire Bottle · lowINSPECTION TYPE:N/A, PORTABLE CARGO COMP FIRE EXTINGUISHER BELOW LIMITS. REMOVED AND REPLACED FIRE BOTTLE.Feb 27, 2001 · N940UP · Boeing 727185C · Fire Bottle, PortableSDR UPS01235012Apu · overservicedINSPECTION TYPE:N/A, AFTER RUNNING PACK ON COCKPIT FILLED WITH SMOKE. SHUTDOWN PACK, SMOKE STARTED TO DISSIPATE. SMELLED LIKE BURNING OIL. *S/D* FOUND APU OVER SERVICED OPERATED PACK COOL AND HOT. NO PROBLEM NOTED.Feb 18, 2001 · N940UP · Boeing 727185C · APU Oil SystemSDR UPS02237505Support Fitting · corrodedINSPECTION TYPE:C+SI LT WING SUPPORT BRACKET FOR NR 3 FLAP TRACK FWD END HAS PITTING CORROSION ON RT FACE OF LUG.Jan 2, 2001 · N940UP · Boeing 727185C · Wing, Control Surface Attach FittingsSDR UPS01234574Switch · failedINSPECTION TYPE:N/A PILOT REPORT NR 2 L/E FLAP DISAGREE LIGHT ILLUM (RFD) REPEAT ITEM - NR 2 LED AMBER FLAP LIGHT ILLUM TECH RECOMMENDS:REPLACE NR 2 LEADING EDGE FLAP SWITCH(PREVIOUS SWITCH WAS REPLACED IN RFD ON 12/27 WAS BAD FROM STOCK NEW SWITCH & ACTUDec 29, 2000 · N954UP · Boeing 727185C · Leading Edge Slat Control SystemSDR UPS00233154Skin · crackedINSPECTION TYPE: C+SI. DURING INSPECTION OF SECTION 41 RT SKIN. 13 FASTENER HOLES HAVE CRACKED INDICATIONS. HFEC INSP. C/O IN SECT.41 AREA IAW B727 NDT MANUAL D6-48875,PT6,SUB 51-00-00 FIG16 ON ACCESSED HOLES.RESULT NDF. HFEC INSP C/O IAW B727 NDT MANUALJul 1, 2000 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS00233210Bracket · crackedINSPECTION TYPE: C+SI, WHILE REPLACING REINFORCEMENT FRAME, SUPPORT BRACKET FOUND CRACKED. FABRICATED NEW BRACKET IAW SSRM 51-20-01. INSTALLED BRACKET IAW SRM 51-30-2Jun 26, 2000 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS00233209Gimbal Pin · corrodedINSPECTION TYPE: C+SI, HORIZONTAL STABILIZER JACKSCREW-GIMBLE ASSY HAS CORROSION IN BORE AND PIN OUTER SURFACE. REPLACE GIMBLE ASSY IAW MM 51-10-01 AND ACTUATOR PINS IAW MM 51-10-0 1Jun 23, 2000 · N954UP · Boeing 727185C · Stabilizer Control SystemSDR UPS00233163Rib · crackedINSPECTION TYPE: C+SI. NR 8 FLAP TRACK SECOND RIB FROM FWD END, CRACKED ON MID FAIRING. RIB REPLACED IAW DRAWING NR 65-21796.Jun 23, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00233208Floorbeam · corrodedINSPECTION TYPE: C+SI, WHILE RECTIFING CORROSION ON FLOORBOARD, TRANSVERSE FLOORBEAM AT BS 1183, FOUND TO BE CORRODED. CORROSION REMOVED IAW SRM 51-10-6. CORROSION FOUND TO BE OUTSIDE LIMITS AND REINFORCED CHORD REPLACED IAW DRW #65-19606.Jun 19, 2000 · N954UP · Boeing 727185C · Fuselage Main, Floor BeamSDR UPS00233207Seat Track · corrodedINSPECTION TYPE: C+SI, ON REMOVAL OF CORRODED BOLT BS 740 FRONT SPAR BULKHEAD LINK & SEAT TRACK FOUND CORRODED. LINK & SEAT TRACK REPLACED IAW SRM 51-10-01 & SRM 51-30-02 BS740-BS7 60.Jun 16, 2000 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS00232941Carriage · corrodedINSPECTION TYPE:C+SI, NR 2 FLAP TRACK SPINDLE BORE CORRODED. REPLACED FLAP TRACK CARRIAGE IAW 27-51-13 & OHM 57-52-11.Jun 16, 2000 · N954UP · Boeing 727185C · Trailing Edge Flaps
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