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 UPS00233224Support Fitting · corrodedINSPECTION TYPE: C+SI, RT STABILIZER HINGE BEARING OB SUPPORT LUG SHOWS CORROSION INDICATION DURING HFEC INSPECTION. CORROSION REMOVED AND LUG REWORKED, COMPLETED IAW EO B727-5510-2284 APPEX B.P6 3-7 (F)-(J).HFEC INSP C/O IAW B727 NDT MANUAL,PT6,51-00-0 Jun 15, 2000 · N954UP · Boeing 727185C · Vertical StabilizerSDR UPS00232940Carriage · corrodedINSPECTION TYPE:C+SI, NR 1 FLAP TRACK CARRIAGE SPINDLE BORE CORRODED (INSIDE BORE.) NR 1 CARRIAGE REPLACED IAW MM 27-51-13.Jun 15, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00233225Shear Tie · crackedINSPECTION TYPE: C+SI, FRAME LEG CRACKED AT ATTACHMENT TO SKIN BETWEEN STR 17L - STR 18L AT BS 1110. HFEC INSP C/O ON 7 CSK HOLES AT ABOVE LOCATION IAW B727 NDT MANUAL D6-48875.PT6,SUBJECT 53-30-00 FIG 3. FRAME LEG REPAIRED IAW SRM 53-10- 4 FIG11.RESULT NDF.Jun 14, 2000 · N954UP · Boeing 727185C · Fuselage Main, StructureSDR UPS00233227Floorbeam · corrodedINSPECTION TYPE: C+SI, SURFACE CORROSION ON FLOORBEAM BS 344 LBL & RBL 0. HFEC C/O IN AREA OF BLEND CORROSION/CUTOUT IAW B727 NDT MANUAL PT6, 51-00-00 ,FIG4 .NDF. CORROSION REMOVED IAW SRM 51-10-06. FLOORBEAM REPA IRED IAW SRM 53-10-08 FIG7.Jun 14, 2000 · N954UP · Boeing 727185C · Fuselage Main, Floor BeamSDR UPS00233216Seat Track · corrodedINSPECTION TYPE: C+SI, CORROSION ON SEAT TRACK BS 560-600 LBL/RBL0. SEAT TRACK REPLACED IAW SRM 51-10-01 AND INSTALLED IAW SRM 51-30-02.Jun 14, 2000 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS00233215Floorbeam · corrodedINSPECTION TYPE: C+SI, CORROSION ON FLOORBEAM BS 640 BETWEEN RBL 24.75 & 45.5. HFEC C/O IAW B727 NDT MANUAL PT6 51-00-00 FIG4 AROUND CUTOUT.NDF.Jun 14, 2000 · N954UP · Boeing 727185C · Fuselage Main, Floor BeamSDR UPS00233146Floorbeam · corrodedINSPECTION TYPE: C+SI, CORROSION ON FLOORBEAM, BS640 BETWEEN RBL 24.75 - 45.5 (CABIN) HFEC C/O IAW B727 NDT MANUAL PT6 51-00-00 FIG4 AROUND CUTOUT.NDF. FLOORBEAM REPAIRED IAW SRM 53-10-8 FIG 5.Jun 14, 2000 · N954UP · Boeing 727185C · Fuselage Main, Floor BeamSDR UPS00233136Intercostal · corrodedINSPECTION TYPE:C+SI INTERCOSTAL UNDER LAVATORY DOOR AND PARTITION CORRODED (FWD TOILET) INTERCOSTAL REPLACED IAW SRM 53-10-02 AND SRM 51-10-1Jun 14, 2000 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS00233130Floor Support · crackedINSPECTION TYPE:C+SI FLOOR SUPPORT IN E/E BAY AT BS 380 ABOVE STR 25R IS CRACKED. REPAIRED SUPPORT IAW SRM.51-20-1,SRM.51-30-1Jun 14, 2000 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS00233129Stringer · corrodedINSPECTION TYPE:C+SI CORROSION ON STRINGER 21R AT BS 390 IN E/E BAY. CORROSION REMOVED IAW SRM 51-10-6 AND STRINER REPAIRED IAW SRM 53-10-3 F IG2.Jun 14, 2000 · N954UP · Boeing 727185C · Fuselage Main, Longeron/StringerSDR UPS00233214Floorbeam · corrodedINSPECTION TYPE: C+SI, CORROSION ON FLOORBEAM BS 680 BETWEEN BL 0 & RBL 24.75. HFEC C/O IAW B727 NDT MANUAL PT6,51-00-00FIG4 AROUND TRIM AREA. NDF. FLOORBEAM REPAIR IAW SRM 53-10-08 FIG5.Jun 13, 2000 · N954UP · Boeing 727185C · Fuselage Main, Floor BeamSDR UPS00233177Skin · crackedINSPECTION TYPE: C+SI. ENGINE NR 1 THRUST REVERSER LOWER DOOR INNER SKIN CRACKED AT MID SECTION . DYE PENETRANT INSPECTION CARRIED OUT TO LOCATE ENDS IAW B727 SOP D6- 51702, SECTION 20-20-02. RESULTS; ENDS MARKED & STOP DRILLED. CRACK FOUND TO BE CONTAINEDJun 13, 2000 · N954UP · Boeing 727185C · Engine Thrust ReverserSDR UPS00233147Spar · crackedINSPECTION TYPE:C+SI LT HOROZONTAL STAB, FRONT SPAR LOWER CHORD CRACKED @ LE STA 236 - 248. HFEC C/O IAW B727 NDT MANUAL, PT6, 51-00-00, FIG 4. CRACK ENDS MARKED BEFORE REPAIR AND POST DAMAGE REMOVAL. NO DEFECTS FOUND. REPAIR C/O IAW SRM 55-10-5Jun 13, 2000 · N954UP · Boeing 727185C · Horizontal Stabilizer, Spar/RibSDR UPS00233141Bulkhead · crackedINSPECTION TYPE:C+SI SUSPECT CRACK ON BS 178 BULKHEAD LT STR 17L. HFEC INSPECTION CARRIED OUT IAW B727-NDT MANUAL, PT6,51-00-00,FIG4. CRACK CONFIRMED ON BS 178 BULKHEAD LT ANGLE, AT STR 17L. CRACK CUT OUT IAW SRM 51-40-3 FIG1 .HFEC INSP C/O IAW B727 Jun 13, 2000 · N954UP · Boeing 727185C · Fuselage Main, BulkheadSDR UPS00233120Pin · corrodedINSPECTION TYPE:C+SI RT BS 740 BOTTLE PIN CORRODED. BOTTLE PIN REMOVED AND REPLACED ***CPCP***Jun 13, 2000 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS00233116Sleeve · corrodedINSPECTION TYPE:C+SI BS 740 RT FITTING SLEEVE CORRODED. RT BS 740 FITTING SLEEVE REPLACED IAW.DRW 65C13724 ***CPCP***Jun 13, 2000 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS00233233Structure · crackedINSPECTION TYPE: C&SI, CRACK ON CLEAT BETWEEN MAIN CARGO DOOR SILL & FRAME IN LWR FWD CARGO HOLD AT STA BS 500 REPAIRED PER SRM 51-40-2 FIG 1Jun 12, 2000 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS00233162Door Frame · crackedINSPECTION TYPE: C+SI. LOWER FWD CARGO HOLD CRACKED ON CARGO DOOR FRAME AT BS 570 BETWEEN STR 21 RT & 22 RT. HFEC INSP CARRIED OUT IAW B727 NDT MANUAL, PT6, 51-00-00, FIG 4. TOTAL OF 6 CRACKS FOUND. CRACK ENDS MARKED. FRAME REPAIRED IAW SRM 53-10-4 FIG 1Jun 12, 2000 · N954UP · Boeing 727185C · Fuselage Main, StructureSDR UPS00233161Spoiler Panel · contaminatedINSPECTION TYPE: C+SI. X-RAY INSPECTION HAS SHOWN THAT NR 13 SPOILER PANEL HAS SOME MOISTURE CONTAMINATION. NR 13 SPOILER PANEL REMOVED IAW MM 27-61-01. NR 13 SPOILER PANEL INSTALLED IAW MM 27-61-01.Jun 12, 2000 · N954UP · Boeing 727185C · SpoilersSDR UPS00233148Frame · tornINSPECTION TYPE:C+SI. SMALL TEAR IN FRAME BS620 @ STR 5 & 6 RT (CABIN). HFEC INSP CARRIED OUT IAW B727 NDT MANUAL, PT6, 51-00-00, FIG4. POST DAMAGE REMOVAL. NDF. DAMAGED AREA BLENDED OUT IAW SRM 51-10-01 AND FRAME REPAIRED IAW SRM 53-10-04.FIG2.Jun 12, 2000 · N954UP · Boeing 727185C · Fuselage Main, FrameSDR UPS00233157Beam · crackedINSPECTION TYPE: C+SI. RT WING CRACKED ON SPOILER NR 8 SUPPORT BEAM AT IB HINGE. HFEC INSP C/O ON NR 8 SPOILER IB SUPPORT BEAM & HINGE IAW B727-NDT MANUAL PT6 SUBJECT 51-00-00 FIG16 & 4.RESULT NDF. REPAIR C/O IAW EO 2000-022-005 UPS FILE NR 727-57-2163.Jun 10, 2000 · N954UP · Boeing 727185C · SpoilersSDR UPS00233230Attach Angle · corrodedINSPECTION TYPE: C+SI, NR 5 FLAP TRACK FWD ATTACH FLANGE UPPER SURFACE CORRODED. MACHINED FWD ATTACH FLANGE UPPER SURFACE IAW SOPM 20-10-02 AND OHM 57 -40-01. SMRO EO.2000-022-007.UPS FILE NO.5740-2167.Jun 9, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00233229Attach Angle · corrodedINSPECTION TYPE: C+SI, NR 5 FLAP TRACK AFT ATTACH FLANGE UPPER SURFACE CORRODED. MACHINED AFT ATTACH FLANGE UPPER SURFACE IAW SOPM 20-10-02. REF SMRO EO2000-022-007 FOR REPAIR .UPS FILE NO.5740-2167.Jun 9, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00233213Flap Track · corrodedINSPECTION TYPE: C+SI, NR 3 FLAP TRACK AFT FLANGE UPPER SURFACE & HOLES CORRODED INSIDE BORES & LWR SURFACES. MACHINED AREA TO REMOVE CORROSION. REPAIR CARRIED OUT IAW SMRO EO.200 022-004.UPS FILE NO727-57-2165.Jun 9, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00233212Flap Track · corrodedINSPECTION TYPE: C+SI, NR 3 FLAP TRACK FWD ATTACH LUG CORRODED. MACHINED AREA TO REMOVE CORROSION. MPI C/O ON THE FWD ATTACH LUGS IAW B727 SOP D6-51702 CHP 20-20-01.NDF. REF SMRO EO.2000-022-006 FOR REP AIR UPS FILE NR .727-57-2164.Jun 9, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00233181Skin · crackedINSPECTION TYPE: C+SI. FASTENER HEAD MISSING & TWO OTHER FASTENERS HEADS DISHED AT BS 730 STR 14RT. REMOVED ALL FASTENERS ALONG LAP JOINT IAW SRM 52-30-2. HFEC ON COUNTER SINK IAW B727 MANUAL D6-48875. PT6. SUB 53-30-00 FIG 3 ON STR 14 RT BETWEEN BS 677Jun 9, 2000 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS00233159Spar · puncturedINSPECTION TYPE: C+SI. LT IB AILERON REAR SPAR IS PUNCTURED. REMOVED AILERON AND TAB IAW MM 27-10-01. REPAIR CARRIED OUT IAW SRM 5 1-40-2 FIG 1.Jun 9, 2000 · N954UP · Boeing 727185C · AileronsSDR UPS00233156Fitting · corrodedINSPECTION TYPE: C+SI. LT OB AILERON, IB END FITTING IS BADLY CORRODED AROUND ATTACH LUG FOR AILERON OPERATING ROD. REPLACED AILERON CASTING IAW DRW 65-21766.Jun 9, 2000 · N954UP · Boeing 727185C · AileronsSDR UPS00233153Fitting · corrodedINSPECTION TYPE:C+SI. LT OB AILERON 2 ND HINGE SUPPORT FITTING FROM IB IS BADLY CORRODED REPLACED FITTING IAW DRW NR 65-21708Jun 9, 2000 · N954UP · Boeing 727185C · AileronsSDR UPS00233144Skin · corrodedINSPECTION TYPE:C+SI SUSPECTED CORROSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER BS 1140, BETWEEN STR 3 AND 4 RT. LFEC FOUND CORROSION. AREA DERIVETED IAW SRM 51-30-2 BS 1183 & 1110. EO.B727-5330-0509.APPX8.3 C/OJun 9, 2000 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS00233118Skin · crackedINSPECTION TYPE:C+SI DURING HFEC INSP. OF SECTION 41 FUSELAGE SKIN, 2 FASTENER HOLES CRACKED, FOUND AT BS.203.8 BETWEEN WL207.5 AND WL234 RT. REPAIRED IAW SRM 53-30-3 FIG3 PER EO B727-5330-0795 BS203.8 WL207.5 TO WL234 RT.Jun 9, 2000 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS00233175Skin · chafedINSPECTION TYPE: C+SI. ENGINE NR 3 TRUST REVERSER LOWER DOOR INNER SKIN WORN DUE CHAFING OF SEAL. REPAIR CARRIED OUT IAW SRM CHP.78-30-01 FIG 202.Jun 8, 2000 · N954UP · Boeing 727185C · Engine Thrust ReverserSDR UPS00233174Skin · chafedINSPECTION TYPE: C+SI. ENGINE NR 1 TRUST REVERSER LOWER DOOR INNER SKIN WORN DUE CHAFING OF SEAL. REPAIR CARRIED OUT IAW SRM CHP 78-30-01 FIG202Jun 8, 2000 · N954UP · Boeing 727185C · Engine Thrust ReverserSDR UPS00233152Fitting · crackedINSPECTION TYPE:C+SI. NR 3 FLAP TRANSMISSION MOUNT FITTING IS CRACKED NR 3 FLAP TRANSMISSION REMOVED IAW MM 27-51-41. CASTING REPLACED BOEING DRAWING 65-16201. REFITTED NR 3 FLAP TRANSMISSION ASSY IAW MM.27-51-41.Jun 8, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00233113Angle · crackedINSPECTION TYPE:C+SI ENGINE NR 2 AFT MOUNT SUPPORT RIB RIGHT CHORD INSIDE THE VERTICAL FIN HAS CRACKED SUPPORT ANGLE APPROX 17 INCHS FROM TOP OF CHORD. REPLACED CRACKED ANGLE IAW DRAWING NO.65-17553Jun 8, 2000 · N954UP · Boeing 727185C · Nacelle/Pylon StructureSDR UPS00233180Support Bracket · crackedINSPECTION TYPE: C+SI. ENGINE NR 3 THRUST REVERSER OUTBOARD FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACED IAW MM.78-30-00Jun 7, 2000 · N954UP · Boeing 727185C · Engine Thrust ReverserSDR UPS00233179Support Bracket · crackedINSPECTION TYPE: C+SI. ENGINE NR 1 THRUST REVERSER FAIRING MID SUPPORT BRACKET CRACKED. REPLACE BRACKET.Jun 7, 2000 · N954UP · Boeing 727185C · Engine Thrust ReverserSDR UPS00233143Stringer · crackedINSPECTION TYPE:C+SI LT 18A HAS SUSPECTED CRACK AT BS940 LOWER FWD ATTACHMENT BOLT. HFEC INSP CARRIED OUT IAW B727 NDT MANUAL,PT6,51-00-00,FIG4. CRACK CONFIRMED ON S18A LT BS 940 LT AND FUSELAGE SKIN FOUND CRACKED IN TWO PLACES AT THIS POSITION (BS940 LT Jun 7, 2000 · N954UP · Boeing 727185C · Fuselage Main, Longeron/StringerSDR UPS00233128Carriage · corrodedINSPECTION TYPE:C+SI NR 3 FLAPTRACK CARRIAGE SPINDLE BORE CORRODED (INTERNALLY) CARRAGE REPLACED. ***CPCP***Jun 7, 2000 · N954UP · Boeing 727185C · Wing, Control SurfacesSDR UPS00233125Carriage · corrodedINSPECTION TYPE:C+SI NR 6 FLAP CARRIAGE SPINDLE BORE CORRODED (INTERNALLY) REPLACE NR 6 FLAP CARRIAGE.Jun 7, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00232947Flap Track · crackedINSPECTION TYPE:C+SI, NR 1 FLAP TRACK SUSPECT CRACK AT SPACER BLOCK FAIRING GUIDE BLOCK FWD HOLE. HFEC INSP CARRIED OUT IAW B727 NDT MANUAL, PART 6,51-00-00, FIG 4. CRACK CONFIRMED ON NR 1 FLAP TRACK SPACER BLOCK FAIRING GUIDE BLOCK FWD HOLE. TRACK REPLACEDJun 7, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00232946Carriage · corrodedINSPECTION TYPE:C+SI, NR 8 FLAP CARRIAGE SPINDLE BORE CORRODED. REPLACED CARRIAGE ASSY IAW MM 27-51-13.Jun 7, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00232945Carriage · corrodedINSPECTION TYPE:C+SI, NR 7 FLAP CARRIAGE SPINDLE BORE CORRODED (INTERNALLY). REPLACED FLAP TRACK CARRIAGE IAW MM 27-51-13+OHMJ57-52-11.Jun 7, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00232944Carriage · corrodedINSPECTION TYPE:C+SI, NR 5 FLAP CARRIAGE SPINDLE OUTER SURFACE CORRODED UNDER FWD THRUST WASHER. REPLACED CARRIAGE.Jun 7, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00232942Carriage · corrodedINSPECTION TYPE:C+SI, NR 4 FLAP TRACK CARRIAGE SPINDLE BORE CORRODED. REPLACED CARRIAGE.Jun 7, 2000 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS00233226Angle · corrodedINSPECTION TYPE: C+SI, CORROSION ON PULLEY SUPPORT BRACKET FOR NLG STEERING CABLES. WEB ANGLE FOUND CORRODED. ON REMOVAL OF PULLEY SUPPORT BRACKET, BRACKET FOUND TO BE O.K. AT BS 312L. PRESSURE WEB ANGLE FOUND TO BE CORRODED BEYOND LIMITS. REPLACED ANGLE Jun 6, 2000 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS00233041Skin · crackedINSPECTION TYPE:C+SI SUSPECT CRACK IN MAIN CARGO DOOR SKIN AT FORWARD PRESSURE RELIEF DOOR UPPER FORWARD CUTOUT. HFEC INSP C/O IAW B727 NDT MANUAL,PT6,51-00-00,FIG4. CRACK CONFIRMED ON MAIN CARGO DDOOR AT FWD PRESSURE RELIEF DOOR FWD UPPER CORNER.REPAIRJun 6, 2000 · N954UP · Boeing 727185C · Cargo/Baggage DoorsSDR UPS00233040Jackscrew · corrodedINSPECTION TYPE:C+SI NLG MANUAL EXTENSION JACK CORRODED JACKSCREW REMOVED AND REPLACED IAW MM 32-34-11. NLG MANUAL EXTENSION ADJUSTED IAW MM 3234-00Jun 6, 2000 · N954UP · Boeing 727185C · Landing Gear Retraction/Extension SystemSDR UPS00233206Outflow Valve · leakingINSPECTION TYPE: C+SI, LT OUTFLOW VALVE LEAKING ON PRESSURIZATION. BOTH OUTFLOW VALVES REPLACED DUE PRESSURIZATION PROBLEM. REMOVED VALVE IAW MM21-30-52.Jun 3, 2000 · N954UP · Boeing 727185C · Pressure Regulator/Outflow ValveSDR UPS00232424Battery Pack · inoperativeINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS (2) NEED NEW BATTERIES. INSTALLED NEW BATTERIES IN BOTH EMERGENCY EXIT LIGHTS, OPS CHECK GOOD.Apr 24, 2000 · N940UP · Boeing 727185C · Emergency Lighting
Back to Boeing 727-185C