N92874, cancelled Mar 21, 2013

Service difficulty reports · 100

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 = 'N92874' AND deregistration_id = 'N92874-2013-03-21'
  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 CALA0300589Doubler · corrodedINSPECTION FOUND INTERNAL DOUBLER FOR OUTFLOW VALVE CORRODED AT STA 1325 BETWEEN L21L AND L22L. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-02.Oct 12, 2003 · N92874 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0300333Battery Pack · inoperativeINSPECTION FOUND THE OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-53-00, PAGE 407.Jun 23, 2003 · N92874 · Doug DC982 · Emergency LightingSDR CALA0300270Slide · dischargedINSPECTION FOUND THE R-1 DOOR SLIDE PRESSURE LOW. THE EMERGENCY DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-62-00.May 28, 2003 · N92874 · Doug DC982 · Escape SlideSDR CALA0200430Skin · crackedINSPECTION FOUND A 1/4" CRACK AT RIVET IN L-1 DOOR SKIN AND THE CORNER WAS BENT. THE CRACK WAS LOCATED AT THE UPPER AFT CORNER OF DOOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 32 AND 51-10-3B.Jul 25, 2002 · N92874 · Doug DC982 · Passenger/Crew DoorsSDR CALA0200421Seat Track · corrodedINSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 200-228. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-05, FIGURE 4F, SHEET 1.Jul 19, 2002 · N92874 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200405Seat Track · corrodedINSPECTION FOUND L/H CENTER SEAT TRACK CORRODED AROUND FLOOR PANEL MOUNT HOLES BETWEEN STA 1136 AND 1174. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-05.Jul 17, 2002 · N92874 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200401Seat Track · corrodedINSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 200-228. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F, SHEET 1.Jul 15, 2002 · N92874 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0200141Fan · overheatedTHE FLIGHT ATTENDANT REPORTED AN ELECTRICAL SMOKE ODOR APPARENTLY COMING FROM THE RIGHT AFT LAV AREA AFTER TAKEOFF FROM MIA. THE AIRCRAFT WAS RETURNED TO MIA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE CABIN AIR RECIRCULATION FAN HAD OVERHEAMar 19, 2002 · N92874 · Doug DC982 · Air Distribution FanSDR CALA0100655Charger · inoperativeINSPECTION FOUND EMERGENCY AISLE PATH LIGHTING IN CENTER OF AIRCRAFT INOPERATIVE. THE EMERGENCY BATTERY CHARGER NEAR TOP BEACON WAS REMOVED AND REPLACED AND OPERATION OF AISLE PATH LIGHTING CHECKED GOOD.Jul 14, 2001 · N92874 · Doug DC982 · Emergency LightingSDR CALA0100566Intercostal · corrodedINSPECTION FOUND FIVE INTERCOSTALS CORRODED INSIDE TORQUE BOX AT AFT CARGO PIT AREA, FS 1165 - 1203. THE INTERCOSTALS WERE REMOVED AND NEW INTERCOSTALS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-1, AND 51-30-5.Jun 21, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100565Skin · gougedINSPECTION FOUND EXTERNAL FUSELAGE SKIN GOUGED AFT OF R-1 DOOR GUST LOCK. THE GOUGED AREA WAS REMOVED. SKIN FILLER AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-34-0, 51-10-4, 51-10-3, AND 53-04, FIGURE 24.Jun 21, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100540Skin · dentedINSPECTION FOUND LEFT I/B FLAP LOWER SKIN SURFACE DENTED. THE LEFT I/B FLAP PANEL WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-50-14, 51-10-3, 51-50-20, AND 57-52-14. THE PANEL WAS INSTALLED IAW SRM 51-30-1.Jun 12, 2001 · N92874 · Doug DC982 · Trailing Edge FlapsSDR CALA0100539Intercostal · corrodedINSPECTION FOUND MID CARGO INTERCOSTAL CORRODED AT FS 769-788 BETWEEN LONGERONS 27R AND 28R. PANEL 2214C WAS REMOVED IAW SRM 51-30-01. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-05. PANEL 2214C WAS REINSTALLED IAW SRM 51-30-01.Jun 12, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100537Web · corrodedINSPECTION FOUND AFT CARGO PIT TORQUE BOX WEB CORRODED. THE TORQUE BOX WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.Jun 10, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100536Door Frame · corrodedINSPECTION FOUND FORWARD CARGO DOOR FORWARD JAMB UPPER WEB CORRODED. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-5.Jun 7, 2001 · N92874 · Doug DC982 · Fuselage Main, StructureSDR CALA0100534Angle · corrodedINSPECTION FOUND CUSP ANGLE CORRODED AT FS 200, RBL 54. THE R-1 DOOR, FRAME FITTING, AND CUSP ANGLE WERE REMOVED IAW MM 52-41-00, SRM 51-30-05, AND 53-05, FIGURE 55. A NEW ANGLE AND REPAIR SPLICE ANGLES WERE INSTALLED IAW SRM 51-30-01. THE R-1 DOOR WAS REINJun 6, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100533Frame · corrodedINSPECTION FOUND TAIL COMPARTMENT LT SIDE CANTED FRAME GOUGED AT FS 1463. THE CORROSION WAS REMOVED AND REPAIR ANGLES WERE INSTALLED IAW SRM 51-30-5, 53-01, FIGURE 1, 51-10-3, AND EA 9-5311-2-A0888, FIGURE 2.Jun 3, 2001 · N92874 · Doug DC982 · Fuselage Main, FrameSDR CALA0100532Web · crackedINSPECTION FOUND A 1 INCH CRACK IN L1 DOOR TORQUE BOX WEB AFT OF TANG AT LONGERON 15L. THE FASTENERS WERE REMOVED, TANGS TRIMMED, AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-30-2, 51-10-4, AND EA 9-5314-2-A0884.Jun 3, 2001 · N92874 · Doug DC982 · Passenger/Crew DoorsSDR CALA0100531Floorbeam · corrodedINSPECTION FOUND AFT CARGO FLOORBEAM AND NUT PLATES CORRODED AT FS 1338. THE UPPER L-ANGLE ON FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-05, 51-30-01, 51-30-02, 51-30-05, AND 51-10-4.Jun 3, 2001 · N92874 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0100530Skin · dentedINSPECTION FOUND RT WING EXTERNAL SURFACE OF ZERO SLAT SKIN DENTED I/B OF THE DRIVE TRACK. THE SLAT WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-80-01, EA 9-5740-2-A0890, AND ECRA 5740-01040.Jun 3, 2001 · N92874 · Doug DC982 · Leading Edge DevicesSDR CALA0100529Strap · corrodedINSPECTION FOUND AFT CARGO DOOR JAMB TORQUE BOX FWD STRAP CORRODED. THE FORWARD STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-10-4, 51-10-3, AND 51-30-5.Jun 2, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100528Floorbeam · corrodedINSPECTION FOUND AFT CARGO CABIN FLOORBEAM AND NUT PLATES CORRODED AT FS 1322. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05 AND 53-05, FIGURE 20A.Jun 2, 2001 · N92874 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0100527Beam · corrodedINSPECTION FOUND AFT CARGO DOOR JAMB BEAM CORRODED. THE LOWER DOOR JAMB BEAM WAS REMOVED AND A NEW LOWER DOOR JAMB BEAM WAS INSTALLED USING A DOUBLER AND SPACER IAW SRM 51-30-5 AND 51-30-2.Jun 2, 2001 · N92874 · Doug DC982 · Fuselage Main, StructureSDR CALA0100524Frame · corrodedINSPECTION FOUND MID CARGO FRAME CORRODED AT FS 541 BETWEEN LONGERONS 26R AND 26L. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 2A, 51-10-4, 51-10-3, 53-05, FIGURE 2A, AND 51-30-5.May 31, 2001 · N92874 · Doug DC982 · Fuselage Main, FrameSDR CALA0100523Frame · corrodedINSPECTION FOUND MID CARGO FRAME CORRODED AT FS 560 BETWEEN LONGERONS 26R AND 26L. THE CORRODED SECTION OF FRAME WAS REMOVED AND A Z-FRAME REPAIR SPLICE WAS INSTALLED IAW SRM 53-03, FIGURE 2A AND 51-10-3.May 30, 2001 · N92874 · Doug DC982 · Fuselage Main, FrameSDR CALA0100522Support · crackedINSPECTION FOUND AFT CARGO FALSE BULKHEAD LOWER SUPPORTS CORRODED AND CRACKED AT FS 1007, LONGERON 28L AND 28R. BOTH SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-10-5, 51-10-4, AND 51-10-3.May 30, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100521Skin · damagedINSPECTION FOUND EXTERNAL FUSELAGE SKIN CREASED AT FS 230 BETWEEN LONGERON 17L AND 18L. THE SKIN WAS REPAIRED IAW ECRA 5330-02445.May 30, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100520Floorbeam · corrodedINSPECTION FOUND AFT CARGO OVERHEAD FLOORBEAM CORRODED ON NUT PLATES AND EXFOLIATION CORROSION ON RT SIDE AT FS 1309. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.May 29, 2001 · N92874 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0100519Support · corrodedINSPECTION FOUND MID CARGO SUPPORT CORRODED AT FS 750 BETWEEN LONGERONS 29L AND 29R. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW 51-30-5, 51-10-4, AND 51-30-2.May 29, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100518Frame · corrodedINSPECTION FOUND AFT CARGO FRAME CORRODED AT FS 1117, LONGERON 30. THE CORRODED SECTION OF FRAME WAS REMOVED AND A NEW FRAME SECTION WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.May 29, 2001 · N92874 · Doug DC982 · Fuselage Main, FrameSDR CALA0100517Cargo Track · corrodedINSPECTION FOUND MID CARGO RT TIE DOWN TRACK CORRODED BETWEEN FS 693 AND 788. THE CARGO TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-01, 51-10-4, AND 51-10-3.May 29, 2001 · N92874 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0100516Door Frame · corrodedINSPECTION FOUND MID CARGO DOOR LOWER JAMB BEAM CORRODED AROUND RIVNUTS. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-03027.May 29, 2001 · N92874 · Doug DC982 · Fuselage Main, StructureSDR CALA0100512Web · corrodedINSPECTION FOUND CUSP WEB CORRODED AT FS 200 - 207, RBL 56. THE CUSP WEB WAS REMOVED AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 1, 51-30-02, 51-30-08, AND 51-10-3.May 26, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100511Web · crackedINSPECTION FOUND MAIN CABIN CUSP WEB CRACKED IN SEVERAL PLACES AT FS 1280, RBL 54. THE CRACKS WERE APPROXIMATELY 1 INCH LONG. FLOOR PANELS WERE REMOVED TO GAIN ACCESS. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 96, 51-10-3, AND 51-30-2. THE FLOORMay 26, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100510Web · corrodedINSPECTION FOUND MAIN CABIN CUSP WEB CORRODED AT FS 160 - 200, RBL 56. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01, FIGURE 3. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-14-1, FIGURE 11, 51-30-02, 51-10-3, AND 53-01, FIGURE 3.May 26, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100509Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED ON UPPER AND LOWER SURFACE IN MID CARGO AREA AT FS 636, LONGERON 28R-29R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1.May 26, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100508Support · corrodedINSPECTION FOUND SUPPORT CORRODED AT AFT LT SIDE OF WEB AT CUSP AREA, STA 1309. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4.May 26, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100506Skin · dentedINSPECTION FOUND LT EXTERNAL FUSELAGE SKIN DENTED AT FS 195, LONGERON 23L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.May 25, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100505Floor Support · corrodedINSPECTION FOUND MAIN CABIN FLOOR SUPPORT CORRODED AT FS 160-200, RBL 56. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-30-3, 51-30-4, AND 51-30-2.May 25, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100504Skin · gougedINSPECTION FOUND RT INTERNAL FUSELAGE SKIN GOUGED AT FS 1429. THE AREA WAS BLENDED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-3, 51-10-4, AND 51-30-2.May 25, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100503Skin · dentedINSPECTION FOUND RT MLG DOOR EXTERNAL SKIN DENTED IN TWO PLACES 7 INCHES APART I/B OF DOOR SKID. A REPAIR PATCH WAS INSTALLED IAW SRM 52-01, FIGURE 2 AND 51-30-3.May 24, 2001 · N92874 · Doug DC982 · Landing Gear DoorsSDR CALA0100502Skin · dentedINSPECTION FOUND RT EXTERNAL FUSELAGE SKIN DENTED BETWEEN FS 313 - 332, LONGERON 20-21R. THE EXISTING DOUBLER WAS REMOVED IAW SRM 51-30-05 AND 51-30-02. THE DENTED SKIN WAS REMOVED IAW SRM 53-04, FIGURE 12 & 13. REPAIR DOUBLERS AND FINGER DOUBLERS WERE INSTMay 24, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100501Skin · dentedINSPECTION FOUND LT EXTERNAL FUSELAGE SKIN DENTED AT FS 233, LONGERON 23L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2.May 24, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100493Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AND CREASED AT FS 322, LONGERON 25R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-4, AND 51-10-3.May 22, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100492Skin · dentedINSPECTION FOUND THE EXTERNAL FUSELAGE SKIN DENTED AT FS 340, LONGERON 24L. THE DENTED AREA WAS REFORMED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.May 22, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100491Skin · damagedINSPECTION FOUND EXTERNAL FUSELAGE SKIN CREASED AT FS 312, LONGERON 24L. THE SKIN WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2, 53-04, FIGURE 38, 51-10-3, AND 51-30-2.May 22, 2001 · N92874 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100489Floor Panel · delaminatedINSPECTION FOUND CABIN CENTER FLOOR PANEL DELAMINATED AT FS 905 - 946. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW ECRA 5100-01844.May 21, 2001 · N92874 · Doug DC982 · Fuselage Floor PanelSDR CALA0100486Floor Panel · crackedINSPECTION FOUND CABIN CENTER FLOOR PANEL CRACKED AT FS 905-946. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2 AND 51-30-8.May 21, 2001 · N92874 · Doug DC982 · Fuselage Floor PanelSDR CALA0100484Web · crackedINSPECTION FOUND A 2 INCH CRACK IN CUSP WEB AT FS 237, RBL 56. THE CUSP WEB WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-2 AND 53-01, FIGURE 2. A REPAIR DOUBLER AND THE CUSP WEB WERE INSTALLED IAW SRM 53-01, FIGURE 4, 51-30-2, AND 51-30-1.May 20, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100482Floor Support · crackedINSPECTION FOUND CABIN RT I/B FLOOR SUPPORT CORRODED WITH A 1.5 INCH EDGE CRACK AT FS 210. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-3.May 20, 2001 · N92874 · Doug DC982 · Fuselage Miscellaneous Structure
Back to N92874, cancelled Mar 21, 2013