N16815, cancelled Sep 17, 2002
Service difficulty reports · 86
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 = 'N16815' AND deregistration_id = 'N16815-2002-09-17' 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.
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 = 'N16815' AND deregistration_id = 'N16815-2002-09-17' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA0200001Fuse · blownINSPECTION FOUND SEAT MOUNTED EMERGENCY LIGHTS AT ROW 5-12 INOPERATIVE. MAINTENANCE FOUND FUSE BLOWN IN BATTERY CHARGER AND WIRING AT ROW 5 SHORTED TO THE SEAT TRACK. REPAIRED WIRING IAW STANDARD WIRING PRACTICES. REPLACED FUSE IAW MM 33-51-00.SDR CALA0100764Floor Panel · delaminatedINSPECTION FOUND MAIN CABIN CENTER FLOOR PANEL DELAMINATED AT FS 1117-1174. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.SDR CALA0100761Floor Panel · puncturedINSPECTION FOUND CABIN FLOOR PANEL PUNCTURED AT FS 256-313. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1 AND ECRA 5320-01265.SDR CALA0100746Intercostal · crackedINSPECTION FOUND A 7" CRACK IN R-1 DOOR INNER INTERCOSTA UNDER HINGE ATTACH POINT. THE R-1 DOOR WAS REMOVED IAW MM 52-41-00. THE CRACK WAS STOP DRILLED AND A REPAIR CAP AND FITTING WERE INSTALLED IAW SRM 52-05, FIGURE 5. REINSTALLED R-1 DOOR IAW MM 52-41-00.SDR CALA0100745Pan · gougedINSPECTION FOUND R-1 DOOR LOWER PAN GOUGED AT RIVNUTS. THE PAN SUPPORT WAS REMOVED FOR ACCESS IAW SRM 51-30-02. A REPAIR ANGLE AND DOUBLER WAS INSTALLED IAW ECRA 5240-01386. THE SUPPORT PAN WAS REINSTALLED IAW SRM 51-30-2.SDR CALA0100744Skin · dentedINSPECTION FOUND RT WING O/B FLAP O/B TRAILING EDGE SKIN LOWER SURFACE DENTED. THE SKIN WAS REMOVED IAW SRM 51-30-2 AND THE SUPPORT RIBS WERE FOUND DAMAGED. NEW RIBS AND A REPAIR DOUBLER WERE INSTALLED AND THE SKIN WAS REINSTALLED IAW SRM 51-10-4, 51-10-3, 5SDR CALA0100742Mount · corrodedINSPECTION FOUND R/H WING I/B FLAP HINGE #2 CORRODED IN BOTTOM MOUNT HOLE. THE HOLE WAS REAMED AND TWO BUSHINGS WERE INSTALLED IAW EA 9-2750-2-A0914 AND ECRA 2750-01333.SDR CALA0100741Frame · corrodedINSPECTION FOUND FRAME CORRODED AT FS 1271 FROM LONGERON 27L TO 27R. THE CORRODED AREA OF FRAME WAS CUT OUT IAW SRM 53-03, FIGURE 2A. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 2A, 53-10-3, AND 53-03, FIGURE 2A.SDR CALA0100739Skin · gougedINSPECTION FOUND R/H ELEVATOR LOWER SKIN SURFACE O/B OF TRIM TAB PUSH ROD FAIRING GOUGED. THE SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-2 AND 55-03.SDR CALA0100738Bracket · crackedINSPECTION FOUND A 1" CRACK IN T-BRACKET OF FORWARD CARGO DOOR UPPER INTERNAL PAN FORWARD OF AFT HINGES. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5.SDR CALA0100737Web · corrodedINSPECTION FOUND FORWARD CARGO TORQUE BOX WEB CORRODED AROUND FASTENER HOLES AT STA 370. THE TORQUE BOX WEB AND SUPPORT ANGLE WERE REMOVED IAW SRM 51-10-4 AND 51-30-2. A REPAIR WEB AND SUPPORT ANGLE WERE INSTALLED IAW SRM51-30-2.SDR CALA0100736Web · crackedINSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR TORQUE BOX WEB TANG. THE CRACKED AREA OF WEB TANG WAS TRIMMED OUT AND A DOUBLER AND FILLER WERE INSTALLED IAW EA 9-5314-2-A0905 AND ECRA 5310-04170.SDR CALA0100734Angle · crackedINSPECTION FOUND A 1" CRACK IN T-ANGLE AT FORWARD CARGO DOOR UPPER INTERNAL PAN AFT OF FORWARD HINGE. THE T-ANGLE WAS REMOVED AND A NEW T-ANGLE WAS INSTALLED IAW SRM 51-30-5.SDR CALA0100733Channel · crackedINSPECTION FOUND A 1" CRACK IN L/H MLG DOOR CHANNEL AT FORWARD END OF DOOR JUST ABOVE DOOR SEAL. A REPAIR DOUBLER WAS INSTALLED IAW EA 9-5281-2-A0904 AND ECRA 5280-01267.SDR CALA0100731Splice · corrodedINSPECTION FOUND LONGERON 29L SPLICE CORRODED IN FORWARD CARGO AREA AT FS 225. THE LONGERON SPLICE WAS REMOVED AND A NEW SPLICE WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-30-2, 51-10-4, AND 51-30-5.SDR CALA0100730Frame · corrodedINSPECTION FOUND MID CARGO FRAME CORRODED AT FS 522 BETWEEN LONGERONS 28L AND 28R. THE CORRODED AREA OF FRAME WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-03 AND 51-30-5.SDR CALA0100728Skin · gougedINSPECTION FOUND R/H ELEVATOR SKIN LOWER SURFACE JUST OUTBOARD OF #2 HINGE MOUNTING PAD GOUGED. THE SKIN PANEL WAS REMOVED AND A NEW SKIN PANEL WAS INSTALLED IAW SRM 51-30-2.SDR CALA0100725Skin · dentedINSPECTION FOUND RUDDER CONTROL TAB SKIN DENTED IN THE LOWER LEFT SIDE. THE RUDDER TAB WAS REMOVED IAW MM 27-20-02. THE TAB WAS REPAIRED, WEIGHED, AND BALANCED IAW SRM 55-40-1. THE TAB WAS INSTALLED AND THROW CHECKS WERE COMPLETED IAW MM 27-20-02.SDR CALA0100718Skin · dentedINSPECTION FOUND L/H "0" SLAT EXTERNAL SKIN DENTED. THE SKIN AND ATTACHING PARTS WERE REMOVED IAW SRM 51-30-6 AND 51-30-1. A DOUBLER WAS INSTALLED IAW SRM 57-09, FIGURE 10A. THE SKIN AND ATTACHING PARTS WERE REINSTALLED IAW SRM 51-30-6 AND 51-30-1.SDR CALA0100717Web · corrodedINSPECTION FOUND CUSP WEB CORRODED AT FS 160 - 200, RBL 35 TO RBL 50. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 53-10-1.SDR CALA0100716Spacer · corrodedINSPECTION FOUND MID CARGO DOOR LOWER JAMB BEAM SPACER CORRODED AROUND RIVNUTS. THE SPACER WAS REMOVED AND A NEW SPACER WAS INSTALLED IAW SRM 51-30-4 AND 51-10-4.SDR CALA0100715Seat Track · corrodedINSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT FS 845-1032. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED WITH SPLICES IAW SRM 53-05, FIGURE 4F AND 51-10-3.SDR CALA0100714Skin · dentedINSPECTION FOUND L/H EXTERIOR FUSELAGE SKIN DENTED AT FS 522 ABOVE L25 AND AT FS 494 ABOVE L25. THE DENTS WERE COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-4, AND 51-30-2.SDR CALA0100713Seat Track · corrodedINSPECTION FOUND CABIN L/H CENTER SEAT TRACK CORRODED AT FS 1032-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4, 51-10-3, AND 53-05, FIGURE 4F.SDR CALA0100711Floor Panel · brokenINSPECTION FOUND CABIN L/H O/B FLOOR PANELS BROKEN OFF AT FASTENER HOLES AT FS 1079-1155 AND FS 1155-1250. THE PANELS WERE REPAIRED IAW SRM 51-70-1.SDR CALA0100710Seat Track · corrodedINSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT FS 1174-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-10-3.SDR CALA0100709Floor Panel · puncturedINSPECTION FOUND CABIN R/H I/B FLOOR PANEL PUNCTURED AT FS 389-408. A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265 AND SRM 51-30-1.SDR CALA0100708Floor Panel · delaminatedINSPECTION FOUND COPILOT'S I/B FLOOR PANEL DELAMINATED. THE FLOOR PANEL WAS REMOVED AND A NEW FLOOR PANEL WAS INSTALLED IAW SRM 53-30-01, 53-21-0, SHEET 23, 51-30-1, AND 51-30-2.SDR CALA0100705Web · corrodedINSPECTION FOUND CUSP WEB CORRODED AT FS 200-237, RBL 44 TO RBL 56. THE CORRODED SECTION OF CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-02.SDR CALA0100704Angle · corrodedINSPECTION FOUND R-1 DOOR CUSP ANGLE CORRODED AT FS 203. THE CORRODED SECTION OF CUSP ANGLE WAS CUT OUT IAW SRM 51-30-1. A CUSP ANGLE AND SPLICE WERE INSTALLED IAW SRM 53-05, FIGURE 55, SHEET 2.SDR CALA0100702Seat Track · corrodedINSPECTION FOUND L/H SEAT TRACK CORRODED AT STA 1108-1309. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-1.SDR CALA0100701Pan · crackedINSPECTION FOUND DOOR PAN CRACKED AROUND BOTTOM STOP AT AFT CARGO DOOR AFT SIDE. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 1 & 4 AND ECRA 5230-01540.SDR CALA0100700Web · crackedINSPECTION FOUND CUSP WEB CRACKED AFT OF L-2 DOOR AT STA 1174, LBL 60. THE CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1.SDR CALA0100699Seat Track · corrodedINSPECTION FOUND CABIN SEAT TRACK CORRODED AT STA 798-1108. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1.SDR CALA0100698Skin · dentedINSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT STA 218, LONGERON 16L AND 18L. THE DENTS WERE COLD WORKED IAW SRM 53-04, FIGURE 38. DOUBLERS WERE INSTALLED IAW SRM 53-10, FIGURE 38 AND 51-10-4.SDR CALA0100697Skin · gougedINSPECTION FOUND RT FUSELAGE EXTERNAL SKIN DENTED AND GOUGED BELOW NR 2 ENGINE APRON AT STA 1309. THE DAMAGED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A REPAIR DOUBLER AND SKIN PLUG WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-30-2.SDR CALA0100696Skin · gougedINSPECTION FOUND FORWARD CARGO DOOR EXTERNAL SKIN GOUGED BELOW HANDLES. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 1 AND 52-05.SDR CALA0100692Seat Track · corrodedINSPECTION FOUND R/H CENTER SEAT TRACK CORRODED AT FS 798-874. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-30-3.SDR CALA0100690Floor Panel · delaminatedINSPECTION FOUND CABIN FLOOR PANELS M-P DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.SDR CALA0100689Floor Panel · delaminatedINSPECTION FOUND CABIN FLOOR PANELS B-K DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.SDR CALA0100688Floor Panel · delaminatedINSPECTION FOUND CABIN L/H I/B FLOOR PANEL DELAMINATED AT FS 1079-1155 AND R/H I/B FLOOR PANEL WAS DELAMINATED AT FS 927-1003. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.SDR CALA0100687Floor Panel · delaminatedINSPECTION FOUND MAIN CABIN CENTER FLOOR PANELS DELAMINATED AT FS 1174-1250 AND FS 1309-1361. A R/H I/B FLOOR PANEL WAS DELAMINATED AT FS 1250-1309. A NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.SDR CALA0100686Floor Panel · delaminatedINSPECTION FOUND CABIN R/H I/B AND CENTER FLOOR PANELS AT FS 1117-1174 DELAMINATED AND CENTER PANEL AT FS 1079-1117 DELAMINATED. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.SDR CALA0100685Floor Panel · delaminatedINSPECTION FOUND CABIN CENTER FLOOR PANELS DELAMINATED AT FS 826-886 AND AT FS 945-1003. NEW FLOOR PANELS WERE INSTALLED IAW ECRA 5320-01265.SDR CALA0100684Floor Panel · delaminatedINSPECTION FOUND L/H I/B FLOOR PANEL PUNCTURED AT FS 769-826 AND L/H I/B FLOOR PANEL AT FS 864-886 WAS DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265.SDR CALA0100683Floor Panel · delaminatedINSPECTION FOUND R/H I/B FLOOR PANELS DELAMINATED AT FS 826-927. A CENTER PANEL AT FS 886-946 AND CENTER & RIGHT CENTER PANELS AT FS 807-826 WERE FOUND DELAMINATED. NEW PANELS WERE INSTALLED IAW ECRA 5320-01265.SDR CALA0100682Floor Panel · delaminatedINSPECTION FOUND MAIN CABIN R/H CENTER AND L/H CENTER FLOOR PANELS DELAMINATED AT FS 693-769. NEW PANELS WERE INSTALLED IAW ECRA 5320-01265.SDR CALA0100677Skin · dentedINSPECTION FOUND L/H LOWER EXTERNAL FUSELAGE SKIN DENTED AT STA 389, LONGERON 29L. THE DENT WAS COLD FORMED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-3 AND 53-05, FIGURE 38.SDR CALA0100676Skin · dentedINSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT FS 275, LONGERON 17L. THE DENTED AREA OF SKIN WAS REMOVED IAW SRM 51-30-2. NEW SKIN WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND ECRA 5330-02445.SDR CALA0100675Skin · damagedINSPECTION FOUND FUSELAGE SKIN CREASED AT STA 180, LONGERON 23R. THE CREASED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 12, PAGE 35. A REPAIR DOUBLER AND FINGER DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12, PAGE 35, 51-10-4, 53-30-5, AND 51-30-2.
Back to N16815, cancelled Sep 17, 2002