N18833, cancelled Jun 1, 2007

Service difficulty reports · 61

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 = 'N18833' AND deregistration_id = 'N18833-2007-06-01'
  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 CALA0400426Wire Harness · defectivePOSITION LIGHTS CIRCUIT BREAKER POPPED AND WILL NOT RESET. REPLACED R5-1051 WIRE BUNDLE PER STD WIRE PRACTICE MANUAL 20-31-15.Apr 26, 2004 · N18833 · Doug DC982 · Light System WiringSDR CALA0400203Thrust Reverser · crackedINSPECTION FOUND A 10 INCH CRACK IN NR 2 ENGINE UPPER THRUST REVERSER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW 7830-01872.Mar 2, 2004 · N18833 · Doug DC982 · Engine Thrust ReverserSDR CALA0400197Web · crackedINSPECTION FOUND AFT BAGGAGE BIN THRESHOLD WEB CRACKED IN TWO PLACES AT STA 1155 FORWARD SIDE OF DOOR CUTOUT. THE CRACKS WERE THREE INCHES LONG. REPAIRED WEB IAW ECRA 5310-04403.Mar 1, 2004 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0300011Longeron · corrodedINSPECTION FOUND LONGERON 30 CORRODED IN E&E COMPARTMENT AT STA 160-170. THE CORRODED SECTION OF LONGERON WAS REPLACED IAW SRM 53-02 AND 53-10-01.Jan 15, 2003 · N18833 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0200440Strut · leakingTHE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF FROM MCO. THE GEAR WAS CYCLED, BUT THE HANDLE WOULD NOT RAISE PAST HALF WAY. THE AIRCRAFT WAS RETURNED TO MCO. MAINTENANCE FOUND THE NOSE STRUT DEFLATED DUE TO AN INTERNAL LEAK. A FULL NOSE Aug 18, 2002 · N18833 · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR CALA0200439Valve · defectiveTHE NOSE GEAR DID NOT RETRACT AND WAS ACCOMPANIED BY THE RED GEAR UNSAFE LIGHT REMAINING ILLUMINATED AFTER TAKEOFF FROM MIA. THE GEAR WAS CYCLED, BUT THE HANDLE WOULD NOT COME UP. THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FAug 18, 2002 · N18833 · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR CALA0200200Longeron · corrodedINSPECTION FOUND LONGERON 29R CORRODED AT STA 1287. THE CORRODED AREA OF LONGERON WAS REMOVED AND A NEW SECTION AND SPLICES WERE INSTALLED IAW SRM 53-02, FIGURE 18.Apr 13, 2002 · N18833 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0001065Seat Track · gougedINSPECTION FOUND SEAT TRACK GOUGED AT FS 1000 - 1025, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 4F.Jul 13, 2000 · N18833 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001064Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 1031 - 1136, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 4F.Jul 13, 2000 · N18833 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001038Channel · corrodedINSPECTION FOUND FWD LAV FWD BULKHEAD LOWER SECTION WHERE IT TIES INTO FLOOR DELAMINATED AND CHANNEL HAD CORROSION. THE DELAMINATED AREA WAS REPAIRED BY APPLYING A FIBERGLASS OVERLAY REPAIR IAW SRM 51-70-1, PAGE 5. THE CORRODED CHANNEL WAS REMOVED AND REPLACJul 11, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001037Skin · crackedINSPECTION FOUND A .5 INCH AND .375 INCH CRACK IN FUSELAGE SKIN AT STA 168, RBL 15 FORWARD OF R-1 SERVICE DOOR. THE INNER SKIN ACCESS PANEL FORWARD OF R-1 DOOR WAS REMOVED IAW SRM 51-30-1. THE CRACKED AREA WAS REMOVED. FILLER AND DOUBLER WERE INSTALLED IAW Jul 11, 2000 · N18833 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001036Cable · out of rigTHE FORCE REQUIRED TO RELEASE TAIL CONE EXCEEDED ALLOWABLE LIMIT. THE CABLES WERE CLEANED, LUBRICATED, AND ADJUSTED AND A FUNCTIONAL TEST CHECKED GOOD IAW MM 53-53-00 AND WORK CARD NR EA 5350-01063.Jul 11, 2000 · N18833 · Doug DC982 · Aerodynamic FairingsSDR CALA0001019Skin · dentedINSPECTION FOUND AFT FUSELAGE EXTERNAL SKIN JUST FORWARD OF VENTRAL AIRSTAIR DENTED WITH A CREASE RUNNING HORIZONTAL AT STA 1361. THE DAMAGED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4 AND 51-30-2.Jul 10, 2000 · N18833 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001002Floorboard · corrodedINSPECTION FOUND RT FLOOR WEB OB OF OUTBOARD SEAT TRACK. CORRODED AT FS 900. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-30-2, AND 51-10-3.Jul 1, 2000 · N18833 · Doug DC982 · Fuselage Floor PanelSDR CALA0001001Web · corrodedINSPECTION FOUND LT CUSP WEB CORRODED AT FS 1022-1041. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4 AND 51-30-2.Jul 1, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000999Floor Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AROUND FASTENER HOLES AT STA 218, LBL 16 TO RBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-01, FIGURE 11, AND 51-10-3.Jun 30, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000998Floor Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 212, RBL 14. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-33-5, 53-14-1, AND 51-30-5.Jun 30, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000997Floor Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AROUND FASTENER HOLES AT STA 160-200, RBL 42. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1 AND 53-14-1, FIGURE 11.Jun 30, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000974Longeron · corrodedINSPECTION FOUND LONGERON 29L CORRODED IN AFT CARGO AREA AT STA 1287. THE CORRODED AREA WAS CUT OUT IAW SRM 53-02, FIGURE 18. REPAIR PARTS WERE INSTALLED IAW SRM 53-02, FIGURE 18, 51-30-1, AND 51-30-2.Jun 25, 2000 · N18833 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0000973Web · corrodedINSPECTION FOUND FORWARD CABIN SUBFLOOR WEB CORRODED AT STA 160 - 200, LBL 50. THE CORRODED AREA WAS REMOVED IAW SRM 51-30-2 AND 53-01, FIGURE 2. A FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-12-1, FIGURE 11 AND 51-30-2.Jun 25, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000984Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 860, RBL 54. THE CORRODED SECTION OF SEAT TRACK WAS CUT OUT AND A REPLACEMENT SEAT TRACK AND AFT SPLICE WERE INSTALLED IAW SRM 53-05, FIGURE 4F.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000983Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 1136, LBL 22. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 4F.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000982Seat Track · corrodedINSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 1174 - 1236, LBL 56. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK AND SPLICE REPAIR WERE INSTALLED IAW SRM 53-05, FIGURE 4 AND 51-30-1.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000980Seat Track · corrodedINSPECTION FOUND CABIN SEAT TRACKS CORRODED AT STA 1180, RBL 22 AND AT STA 1220, RBL 22. THE SEAT TRACKS WERE REMOVED AND NEW SEAT TRACKS WERE INSTALLED IAW SRM 51-30-2, 51-30-1, 53-05, FIGURE 4, AND 51-10-3.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000979Seat Track · corrodedINSPECTION FOUND CABIN SEAT TRACKS CORRODED AT FS 1136 - 1174, LBL 44 AND AT FS 1174 - 1190, LBL 22. THE SEAT TRACKS WERE REMOVED AND NEW SEAT TRACKS WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 53-05, FIGURE 4, AND 51-60-0.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000978Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 200, LBL 4 - RBL 4 AND AT STA 224, RBL 14. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-03-5, 51-30-5, 53-14-1, AND 51-30-2.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000977Floor Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORTS CORRODED AT STA 160 - 168, LBL 52 AND AT STA 165, LBL 8. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 53-14-1, 51-10-1, 51-30-2, AND 51-30-1.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000976Floor Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORTS CORRODED AT STA 180, RBL 10 - RBL 46 AND AT STA 200, RBL 10 - RBL 52. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-2 AND 53-14-1, FIGURE 11.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000975Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AROUND SEVERAL FASTENER HOLES AT STA 160 - 200, RBL 8. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-30-5, 53-14-1, FIGURE 27.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000972Web · corrodedINSPECTION FOUND UPPER SURFACE OF O/B LEFT CABIN FLOOR WEB LIGHTENING HOLE CORRODED AT FS 1231-1236. THE CORRODED AREA WAS REMOVED, A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-14-3, 51-10-2, AND 51-30-2.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000971Flange · corrodedINSPECTION FOUND AFT CARGO DOOR SUPPORT UPPER FLANGE CORRODED AT STA 1211, RBL 6. THE SUPPORT WAS REMOVED AND A SUPPORT ANGLE WAS INSTALLED IAW SRM 51-3-0 AND DRAWING 69936660.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000970Web · corrodedINSPECTION FOUND UPPER SURFACE OF WEB CORRODED AT STA 201, RBL 48, JUST AFT OF RT SERVICE DOOR. A SPLICE DOUBLER WAS INSTALLED IAW SRM 51-04-2, FIGURE 5, 53-10-3, AND 51-30-2.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000969Floor Support · corrodedINSPECTION FOUND CABIN THRESHOLD FLOOR SUPPORT CORRODED AT L-1 DOOR. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 53-14-1, FIGURE 11.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000968Attach Fitting · corrodedINSPECTION FOUND AFT CARGO SEAT TRACK ATTACH FITTING CORRODED AT STA 1174, LBL 54. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-03.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage Main, Attach FittingsSDR CALA0000967Cargo Track · corrodedINSPECTION FOUND CARGO TRACK IN AFT CARGO PIT CORRODED AT STA 1322, LBL 26-28. REPAIR DOUBLERS WERE INSTALLED IAW 53-01 AND 51-10-0.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000966Cargo Track · corrodedINSPECTION FOUND CARGO TRACK IN AFT CARGO PIT CORRODED AT STA 1003 - 1155, RBL 24. THE CARGO TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-24.Jun 24, 2000 · N18833 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9800896Feeder Cable · shortedINSPECTION FOUND APU POWER FEEDER CABLE NR 2 SHORTED ON STANDOFF ANGLE CLIP LOCATED IN TAIL COMPARTMENT AT SUPPORT CLAMP BETWEEN AFT PRESSURE BULKHEAD AND TERMINAL BLOCK. THE APU POWER FEEDER CABLE WAS REPLACED FROM T-STRIP STA 218 TO APU T-STRIP IN TAIL COMPMay 20, 1998 · N18833 · Doug DC982 · AC Power Distribution SystemSDR CALA9800895Angle · crackedINSPECTION FOUND SEVERAL .75 INCH CRACKS IN LT VERTICAL STABILIZER ATTACH ANGLE ABOVE CANTED STA 1463. THE CRACKED AREAS WERE CUT OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 23.May 19, 1998 · N18833 · Doug DC982 · Vertical StabilizerSDR CALA9800886Tiedown Rail · corrodedINSPECTION FOUND RIGHT TIE DOWN RAIL CORRODED IN AFT CARGO BIN AT STA 1007 TO 1155. THE TIE DOWN RAIL WAS REMOVED AND THE CORROSION WAS REMOVED IAW SRM 51-30-3. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5320-01519.May 19, 1998 · N18833 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9800885Longeron · corrodedINSPECTION FOUND LONGERON 29R CORRODED AT STA 580. A SPLICE WAS INSTALLED IAW SRM 51-10-5.May 18, 1998 · N18833 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA9800884Skin · crackedINSPECTION FOUND A .5 INCH CRACK WITH DENT AT LOWER AFT CORNER OF FORWARD MAIN CABIN DOOR SKIN. A REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 37.May 18, 1998 · N18833 · Doug DC982 · Cargo/Baggage DoorsSDR CALA9800883Cables · out of adjustEXCESSIVE FORCE WAS REQUIRED TO RELEASE TAILCONE USING AFT CABIN DOOR AND THE INTERIOR RELEASE HANDLE. THE CABLES AND LATCHES WERE ADJUSTED IAW MM 53-53-00.May 18, 1998 · N18833 · Doug DC982 · Aerodynamic FairingsSDR CALA9800872Beam · crackedINSPECTION FOUND A .5 INCH CRACK AT FORWARD END OF FORWARD SERVICE DOOR NR 1 BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2.May 16, 1998 · N18833 · Doug DC982 · Service DoorsSDR CALA9800871Beam · crackedINSPECTION FOUND A 1 CRACK AT BOTH ENDS OF MAIN CABIN DOOR NR 1 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-10-3.May 16, 1998 · N18833 · Doug DC982 · Passenger/Crew DoorsSDR CALA9800870Tiedown Rail · corrodedINSPECTION FOUND CORROSION ON LT TIE DOWN RAILS AT STA 1007-1174 AND STA 1212-1231. NEW TIE DOWN RAILS WERE INSTALLED IAW SRM 51-30-01.May 15, 1998 · N18833 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9800869Jamb · corrodedINSPECTION FOUND FORWARD BAGGAGE BIN DOOR JAMB PAN CORRODED. THE CORRODED AREA OF DOOR PAN WAS CUT OUT. A REPAIR PAN WAS INSTALLED IAW SRM 53-05, FIGURE 44, SHEET 1.May 15, 1998 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9800868Angle · corrodedINSPECTION FOUND CORROSION ON FORWARD FACE OF MAIN BAGGAGE BIN LOWER DOOR JAMB Z-ANGLE. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63.May 15, 1998 · N18833 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9800866Skin · dentedFUSELAGE DENTED STA 256 L 18. INSTALLED DOUBLER REPAIR PER EC/RA 5330-02664.May 14, 1998 · N18833 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9800862Skin · damagedTEMP AIRPHONE REPAIR AT STA 383 BETWEEN L 30 AND L 29. INSTALLED DOUBLER PER SRM 53-04 FIG 38.May 14, 1998 · N18833 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9800861Skin · damagedTEMP AIRPHONE REPAIR AT STA 237 BETWEEN L30 AND L29. INSTALLED DOUBLER PER SRM 53-04 FIG 38.May 14, 1998 · N18833 · Doug DC982 · Fuselage Main, Plate/Skin
Back to N18833, cancelled Jun 1, 2007