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 UPS03240919Buss Tie · corrodedINSPECTION TYPE: C&SI, RT I/B AILERON BUS QUADRANT CORRODED IN CABLE GROOVE. RIGHT I/B AILERON BUS QUADRANT REPLACED AS REQUIRED UP TO STEP D6 INCLUSIVE IAW MM 27-10-56.Jun 11, 2003 · N940UP · Boeing 727185C · Aileron Control SystemSDR UPS03240920Hinge · crackedINSPECTION TYPE: C, LT O/B AILERON I/B BALANCE BAY FWD PANEL IDLER HINGE CRACKED & BROKEN. REPLACED LT O/B AILERON I/B BALANCE BAY FWD PANEL IDLER HINGE IAW MM 27-10-04 & ON REMOVAL OF HINGE, PIN FOUND TO BE DAMAGED, PIN REPLACED IAW MM 27-10-04.Jun 9, 2003 · N940UP · Boeing 727185C · AileronsSDR UPS03240966Stiffener · corrodedINSPECTION TYPE:C CORROSION ON LT 870 MID SECTION ATTACHMENT TO BULKHEAD STIFFENER REPAIR CARRIED OUT IAW SRMO EO 2003-038-006 SRM 51-30-02, UPS EO B72 7-5310-3056 AND DRAWING 65C23231 UPS ENG. FILE NO. 727-53-20118Jun 7, 2003 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS03240948Sill · crackedINSPECTION TYPE: C CRACKS ON LT SILL IN NLG WHEEL WELL AT FWD END AND THE 6TH RIVET FROM FWD. HFEC TO CONFIRM CRACK. CUTOUT MADE AND STOP DRILLED, REPAIRED IAW SRM 51-40-02.Jun 7, 2003 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS03240922Skin · crackedINSPECTION TYPE: C, CRACKS IN SKIN FROM FASTENER HOLES AROUND NR 3 RT WINDOW CUTOUT FWD OF BS 259.5 AT S10R AREA. FASTENERS REMOVED AND DAMAGED AREA TRIMMED OUT IAW SRM 53-30-3 FIGUR E 29. REPAIR PARTS FABRICATED IAW SRM 53-30-3 FIG 29. REPAIR PARTS PARTIALJun 7, 2003 · N940UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS03240964Skin · crackedINSPECTION TYPE:C SUSPECT CRACK AT MID GALLEY DOOR UPPER HINGE CUT OUT REPAIR CARRIED OUT IAW SRM 51-10-2. SKIN REPAIR CARRIED OUT IAW SMRO EO 2003-038-004 UPS ENGINEERING FILE NO. B727-5330-18961.Jun 6, 2003 · N940UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS03240962Stringer · corrodedINSPECTION TYPE: C SUSPECTED CORROSION AT BS 1180 STR. 20R REPAIR CARRIED OUT IAW SRM 51-10-06, SRM 53-30-01 & 53-30-02. NEW STRINGER ENDS INSTALLED, FASTENERS INSTALLED IAW SRM 51-30-02. LAP REFASTENED IAW UPS EO.Jun 6, 2003 · N940UP · Boeing 727185C · Fuselage Main, Longeron/StringerSDR UPS03240949Skin · corrodedINSPECTION TYPE: C SUSPECT CORROSION BS 605 STR 4R LFEC + HFEC CARRIED OUT, NDF. VISUAL INSPECTION SHOWS CORROSION AT STR 4 BS 521-BS740. DAMAGE REMOVED IAW SRM 53 30 03. REPAIR PARTS FABRICATED IAW SRM 53 30 03. REPAIR INSTALLED IAW SRM 53 30 03. REPAIJun 6, 2003 · N940UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS03240965Skin · corrodedINSPECTION TYPE:C SUSPECT CORROSION ON FIXED L-EDGE SKIN UPPER AFT SURFACE AT 2 LOCATIONS LE STA 345 AND 340 APPROX RT. REPAIR CARRIED OUT IAW SMRO EO 2003-038-007. UPS ENGINEERING FILE NO. 727-57-20106Jun 5, 2003 · N940UP · Boeing 727185C · Wing, Plate/SkinSDR UPS03240921Hinge · crackedINSPECTION TYPE: C, RT MLG BODY DOOR HINGE UNDER SAFETY BAR HAS SUSPECT CRACK. HFEC INSP CARRIED OUT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT: CRACK CONFIRMED. HINGE HALF REMOVED IAW SRM 51-30-02. NEW HINGE HALF FITTED IAW SRM 51-30-02.Jun 5, 2003 · N940UP · Boeing 727185C · Landing Gear DoorsSDR UPS03240753Stringer · crackedINSPECTION TYPE: C, ON REMOVAL OF BLIND FASTENER STRINGER FOUND DAMAGED (CRACKED) AT FUSELAGE HOLE STRINGER 26L AT BS 320. CRACK CONTAINED IAW SRM 53-10-3. HFEC INSP CARRIED OUT ON THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 FIG 4 &16 RESULT. NO DEFECTS FOUMay 26, 2003 · N954UP · Boeing 727185C · Fuselage Main, Longeron/StringerSDR UPS03240747Shear Tie · crackedINSPECTION TYPE: C, 2 SUSPECT CRACKS AT SHEAR STRAPS AT LBBL 20 BETWEEN BS 294 & BS 328 2 REPAIRS. FABRICATED NEW SHEAR TIES IAW SRM 51-20-1. REPAIRED SHEAR TIES IAW SRM 51-40-3. INSTALLED NEW SHEAR TIES IAW SRM 51-30-2.May 23, 2003 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS03240752Angle · crackedINSPECTION TYPE: C, NR 6 SLAT, O/B TRACK TO SLAT ATTACH ANGLE IS CRACKED. ANGLE FABRICATED IAW SRM 51-20-01. ANGLE INSTALLED IAW SRM 51-20-02.May 20, 2003 · N954UP · Boeing 727185C · Leading Edge DevicesSDR UPS03240751Skin · crackedINSPECTION TYPE:C SUSPECT CRACK AT FWD ENTRY DOOR CUTOUT AT FWD UPPER CORNER AS MARKED. HFEC INSP CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT CRACK CONFIRMED. REPAIR CARRIED OUT IAW UPS EO B727-5330-1460-D. REPAIR AT FWD ENTRY DOOR REPAINTED IAW May 19, 2003 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS03240746Bracket · crackedINSPECTION TYPE: C, NR 3 SLAT, STRUCTURE SUPPORT ANGLE IS CRACKED JUST I/B OF WHERE ACTUATOR EYE END ATTACHES TO SLAT. BRACKET REMOVED IAW SRM 51-30-02. BRACKET FABRICATED IAW SRM 51-20-01. BRACKET INSTALLED IAW SRM 57-50-03 & SRM 51-30-02.May 19, 2003 · N954UP · Boeing 727185C · Leading Edge DevicesSDR UPS03240748Support Bracket · crackedINSPECTION TYPE: C, WEATHER RADAR TX MOUNTING PLATE, SUPPORT BRACKET AFT LEFT SIDE IS CRACKED. REPAIR CARRIED OUT IAW SRM 51-40-2 FIG 1 SHEET 1.May 17, 2003 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS03240754Skin · corrodedINSPECTION TYPE: C, LT ELEV UPPER SURFACE, CORROSION BENEATH I/B & 2ND FROM I/B STATIC DISCHARGE BASES. DISCHARGE BASE REMOVED IAW SRM 51-30-02 ON 2ND FROM I/B STATIC BASE. CORROSION REMOVED AND FOUND TO BE OUTSIDE OF LIMITS IAW SRM 55-20-1. REPAIRS CARRIEMay 16, 2003 · N954UP · Boeing 727185C · Elevator, Plate/SkinSDR UPS03240750Stop · crackedINSPECTION TYPE: C, AFT NR 1 DOOR STOP ON FWD DOOR HAS A SUSPECT CRACK. HFEC INSP CARRIED OUT ON AFT NR 1 DOOR STOP ON FWD DOOR IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT - CRACK CONFIRMED. AFT NR 1 DOOR STOP FITTING REPAIRED IAW EO B727-5230-0032-N APPX C May 16, 2003 · N954UP · Boeing 727185C · Fuselage Main, StructureSDR UPS03240749Washer · missingINSPECTION TYPE: C, AIR LEAK AT NWW PRESSURE PANEL, RT FWD PANEL. PANEL REMOVED IAW MM 20-80-01. FIBRE WASHERS FOUND TO BE MISSING & REPLACED IAW IPC 25-53-00. ON FURTHER INVESTIGATION CRACK FOUND ON NWW SIDE WALL. AREA CUT OUT IAW SRM 51-40-2. REPAIRED May 15, 2003 · N954UP · Boeing 727185C · Fuselage Main, BulkheadSDR UPS03240661Light · inoperativeEMERGENCY EXIT LIGHT AT CREW ENTRY DOOR INOPERATIVE. PERFORMED ADJ/TEST OF EMERGENCY LIGHTS IAW MM 33-50-01. OPS CHECK GOOD. NO DEFECTS NOTED.May 9, 2003 · N954UP · Boeing 727185C · Emergency LightingSDR UPS03240675Frame · corrodedINSPECTION TYPE: C&SI, FUSELAGE FAIRING NR 3431, AFT FORMED SECTION HAS HEAVY CORROSION UNDER FLOATING ANCHOR NUTS REMOVED FASTENERS ON FRAME IAW SRM 51-30-02. CORRODED SECTION OF FRAME FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-01 FIG 1 & CORRODED SECT ION OF Apr 22, 2003 · N954UP · Boeing 727185C · Aerodynamic FairingsSDR UPS03240677Angle · crackedINSPECTION TYPE: C&SI, CRACK ON ANGLE AFT CARGO DOOR INTERIOR, JUST ABOVE FWD DOOR STOP FITTING REMOVED CRACKED ANGLE, AFTER DE-RIVETING AREA IAW SRM 51-30-2 FABRIC ATED NEW ANGLE IAW SRM 51-20-1 FIG 7. INSTALLED NEW ANGLE & REPAIRED IAW SRM 51-40-3Apr 17, 2003 · N954UP · Boeing 727185C · Cargo/Baggage DoorsSDR UPS03240681Flap Track · corrodedINSPECTION TYPE: C&SI, NR 7 FLAP TRACK - LIGHT SURFACE CORROSION IN HORIZ. HOLES I & J. NR 2 FLAP TRACK INSTALLED IN NR 7 FLAP TRACK POS. IAW MM 27-51-31Apr 16, 2003 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS03240679Seat Track · crackedINSPECTION TYPE: C&SI, SEAT TRACK CRACKED AT O/B FLANGE, RBL 45.5 BETWEEN BS 780 - BS 804 REPLACED SEAT TRACK IAW DRAWING NR 65-41980Apr 16, 2003 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS03240674Support · corrodedINSPECTION TYPE: C&SI, SUSPECT CORROSION UNDER 2 STRIP PANELS EITHER SIDE OF FEEL COMPUTER BOTH PANELS HAVE SUSPECT BULGES IN AREAS AROUND FASTENERS TO FACILITATE ACCESS LT & RT PANELS NT 9703 & 9704 REMOVED IAW SR M 51-30-5 REMOVED LT & RT TEE SUPPORTS IAW SRApr 15, 2003 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS02237588Wire · damagedINSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT ABOVE FORWARD ENTRY DOOR INOP. NO POWER TO PINS 1 AND 5 FOR CHARGING, CORRECTED WIRING PER WDM 33-5 1-01. REPLACED BATTERIES PER MM 33-51-01 PAGE 201.Feb 8, 2002 · N954UP · Boeing 727185C · Light System WiringSDR UPS02237553Channel · crackedINSPECTION TYPE:C+SI CHANNEL ON LT WING REAR SPAR O/B OF NR 1 SPOILER CRACKED.Jan 15, 2002 · N940UP · Boeing 727185C · Wing Miscellaneous StructureSDR UPS02237587Housing · crackedINSPECTION TYPE:C+SI ON CLEANING OF 9G NET FITTINGS, FLOOR MOUNTED HOUSINGS X2 WERE FOUND TO BE CRACKED. HOUSING REPLACED IAW SRM 51-30-02 AND DWG 65-49366.Jan 14, 2002 · N940UP · Boeing 727185C · Cargo CompartmentsSDR UPS02237448Pin · corrodedINSPECTION TYPE:C+SI LEFT BS 740 TERMINAL PIN IS CORRODED IN AREA UNDERNEATH HEAD, AND PIN RETAINING BOLT HAS PITTING CORROSION. LEFT BS 740 TERMINAL PIN AND RETAINING BOLT REPLACED IAW MM 57-41-04.Jan 12, 2002 · N940UP · Boeing 727185C · Wing, Attach FittingsSDR UPS02237521Skin · corrodedINSPECTION TYPE:C CIRCUMFERENTIAL 259.5 EXHIBIT MATERIAL LOSS OF 10% AT STR 10RT. REMOVED FASTENERS & CUT OUT DAMAGE SKIN AS PER DRW 69-62161, SIVE OF CUT OUT 3.5" X 4.25". INSTALLED DOUBLER REPAIR AS PER EO B727-5310 -1371 APPENDIX E. DOUBLER SIZE 8" XJan 10, 2002 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS02237520Skin · corrodedINSPECTION TYPE:C FUSELAGE CIRCUMFERENTIAL 441 EXHIBIT 10% MATERIAL LOSS STINGER 20R THRU STRINGER 22R. REMOVED FASTENERS FROM REPAIR AREA, CUT OUT CORROSION ON FUSELAGE SK IN BS 441 FROM STR 18R TO STR 22R IAW EO B727-5310-1371. SIZE OF CUT OUT 4.5" X 34Jan 10, 2002 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS02237535Floor Support · crackedINSPECTION TYPE:C+SI FLOOR SUPPORT UNDER THIRD CREW MANS TABLE IS CRACKED AT ANCHOR NUT HOLE AND HAS NUMEROUS AREAS OF LIGHT SURFACE CORROSION, FLOOR SUPPORT IS LOCATED JUST AFT OF F/O O2 MASK STORAGE BOX. FLOOR SUPPORT Z-BRACKET LOCATED BETWEEN BS 258-277 LJan 8, 2002 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS02237522Skin · corrodedINSPECTION TYPE:C FUSELAGE SKIN MISSING RIVET HEAD AT LAP JOINT 6LT AND SOME OTHER RIV ETS ARE DISHED BS 640 TO 660. REMOVED RIVETS AT FUSELAGE SKIN LAP JOINT 6LT FROM FS640 TO 660 AND FOUND CORROSION ON LOWER SKIN FS 650 OUT OF LIMITS. CUT OUT DAMAGED AREJan 8, 2002 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS02237546Sill · corrodedINSPECTION TYPE:C EVIDENCE OF CORROSION ON R3 WINDOW SILL IN CONTROL CABIN (IE) LWR EXTRUDED ANGLE.Jan 7, 2002 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS02237544Attach Fitting · corrodedINSPECTION TYPE:C+SI ON REMOVAL OF NR 5 FLAP TRACK FWD ATTACH FITTING, PITTING CORROSION FOUND IN UPPER HOLE COMMON TO SPECIAL STUD ON TRUNNION SUPPORT FITTING.Jan 7, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237541Casting · crackedINSPECTION TYPE:C+SI LT ELEPHANTS EAR FWD CASTING CRACKED ON MOUNT LUG. CASTING REPLACED IAW DWG NO65-26786.Jan 7, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237533Floorbeam · corrodedINSPECTION TYPE:C+SI EXFOLIATION CORROSION ON THE UPPER CHORD FLANGE OF FLOORBEAM AT BS 480 LBL 25 TO 45.Jan 7, 2002 · N940UP · Boeing 727185C · Fuselage Main, Floor BeamSDR UPS02237466Lap Joint · corrodedINSPECTION TYPE:C+SI SURFACE CORROSION ON UPPER SKIN AT LAP JOINT BS 210 STR 24L IN LOWER NOSE COMPT. LAP JOINT DE-RIVETED, CORROSION REMOVED, AREA OUTSIDE LIMITS CUT OUT, REPAIR PARTS FAB'D, HFEC C/W AND NDF, REPAIR INSTALLED IAW SRM 53-30-3 FIG 14 AND SRM 5Jan 7, 2002 · N940UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS02237532Fitting · corrodedINSPECTION TYPE:C+SI EVIDENCE OF CORROSION ON SEAT TRACK SECTION BS 868 LBL 45.5, SEAT TRACK SUPPORT LINK. FITTING REMOVED SRM 51-30-02, NEW FITTING INSTALLED IAW SRM 51-30-02.Jan 6, 2002 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS02237478Fitting · corrodedINSPECTION TYPE:C+SI FRAME TO STRINGER CLEAT CORRODED AT BS 420 STR 18L IN THE E+E BAY. AREA OF CORROSION APPROX .75 INCH BY .5 INCH AND EXTENDED THROUGH THE CLEAT. R&R IAW SRM.Jan 5, 2002 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS02237503Intercostal · crackedINSPECTION TYPE:C+SI INTERCOSTAL BETWEEN FLOORBEAMS AT BS 320 RBL 55 APPROX IN THE E/E BAY IS CRACKED.Jan 3, 2002 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS02237477Support · crackedINSPECTION TYPE:C+SI SUPPORT TANG CRACKED ON DELTA BEAM BS 760 LT. CRACKED TANG TRIMMED FLUSH WITH DELTA BEAM LOWER CHORD. HFEC CARRIED OUT NDF. REPAIR CARRIED OUT IAW SMRO EO 2001-057-011.Jan 3, 2002 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS02237540Support Bracket · corrodedINSPECTION TYPE:C+SI SUPPORT BRACKET FOR LT FWD END OF NR 4 FLAP TRACK HAS PITTING CORROSION IN BORE OF HOLE.Jan 2, 2002 · N940UP · Boeing 727185C · Wing Miscellaneous StructureSDR UPS02237531Web · crackedINSPECTION TYPE:C+SI VERTICAL LT WEB CRACKED OVER ENGINE NR 2 HORIZONTAL FIREWALL AT BS 1376 APPROX. WEB REPLACED IAW DWG 65-17555.Jan 2, 2002 · N940UP · Boeing 727185C · Nacelle/Pylon, Main FrameSDR UPS02237530Web · crackedINSPECTION TYPE:C+SI VERTICAL RT WEB CRACKED OVER ENGINE 2 HORIZONTAL FIREWALL AT BS 137 6 APPROX. WEB REPLACED IAW DWG 65-17555.Jan 2, 2002 · N940UP · Boeing 727185C · Nacelle/Pylon, Main FrameSDR UPS02237514Door Frame · crackedINSPECTION TYPE:C+SI ON REMOVAL OF DAMAGED BRACKET, FWD LWR DOOR STOP FITTING FOUND DAMAGED AND DOOR CUTOUT FRAME CRACKED AT LWR FWD FASTENER FITTING HOLE AFT CARGO DOOR CUTOUT FWD FRAME.Jan 2, 2002 · N940UP · Boeing 727185C · Fuselage Main, StructureSDR UPS02237513Seat Track · corrodedINSPECTION TYPE:C+SI SURFACE CORROSION ON THE LWR SURFACE OF SEAT TRACK UPPER FLANGE AT BS 350 LBL 45.Jan 2, 2002 · N940UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS02237512Flap Track · corrodedINSPECTION TYPE:C+SI NR 2 FLAP TRACK PITTING CORROSION ON FACE OF FWD MOUNT PAD.Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237502Flap Track · corrodedINSPECTION TYPE:C+SI NR 5 FLAP TRACK, PITTING CORROSION IN BORE AND COUNTER BORE OF AFT LT HOLE ON FWD PAD. TRACK REPLACED IAW MM 27-51-31.Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS02237501Flap Track · corrodedINSPECTION TYPE:C+CI NR 5 FLAP TRACK PITTING CORROSION IN BORE AND COUTERBORE OF AFT RT HOLE ON FWD MOUNT PAD. TRACK REPLACED IAW MM 27-51-31.Jan 2, 2002 · N940UP · Boeing 727185C · Trailing Edge Flaps
Back to Boeing 727-185C