Boeing 727-232
Service difficulty reports · 6,539
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 = '727232' 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 aircraft_model_key = '727232' 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 CALA9901742Floorbeam · corrodedINSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 380-400, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.SDR DL72S992840Beam · crackedB727 AFT CARGO DOOR, NR 5 PRESSURE STOP BEAM WAS FOUND DAMAGED. THE OUTER T-CHORD OF THE STOP BEAM WAS FOUND CRACKED AT ATA 1095. REPAIRED PER ER/A 372942-14AD.SDR CALA9901735Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 420-440, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.SDR CALA9901734Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN UPPER FORWARD CORNER SKIN OF LT AFT NR 2 ENGINE COWL. THE CRACKED AREA WAS CUT OUT, A DOUBLER AND FILLER WERE INSTALLED IAW SRM 54-30-3, 51-10-2, AND 51-30-2.SDR CALA9901733Frame · corrodedINSPECTION FOUND FRAME CORRODED ON TOP LEG IN AFT CARGO AREA AT STA 1070, S27R. THE CORRODED DOUBLER, GUSSET, AND STIFFENER WERE REMOVED IAW SRM 51-30-2. A NEW DOUBLER, GUSSET, AND STIFFENER WERE INSTALLED IAW SRM 51-30-2.SDR CALA9901732Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1130, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-10-1, 51-10-2, 51-30-2, AND MM 51-20-2.SDR CALA9901731Support · corrodedINSPECTION FOUND AFT CARGO FLOOR SUPPORT CORRODED AT FS 1075, RBL 12. THE CORRODED AREA WAS CUT OUT, NEW PARTS AND NUT PLATES WERE INSTALLED IAW SRM 51-40-4, 51-30-1, 51-10-2, 51-20-0, AND 51-20-4.SDR CALA9901730Longeron · corrodedINSPECTION FOUND LONGERON 20L CORRODED AT FS 560-600. REPAIR ANGLES WERE INSTALLED IAW SRM 53-10-3, FIGURE 2, 51-10-2, AND 51-20-3.SDR CALA9901729Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 312-344, LBL 30. THE UPPER STRAP OF FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT STRAP WAS INSTALLED IAW SRM 51-30-2 AND 53-10-2.SDR CALA9901728Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT FS 600, LBL 12. THE CRACK WAS STOP DRILLED AND REPAIR PARTS WERE INSTALLED IAW SRM 51-40-4.SDR CALA9901727Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN RADIUS OF RIB AT RT FORWARD NLG DOOR FORWARD UPPER EDGE, SIX INCHES BELOW THE DOOR LATCH. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 51-10, FIGURE 1, 52-10-2, 51-30-1, AND MM 51-20-0.SDR CALA9901726Skin · gougedINSPECTION FOUND FUSELAGE SKIN GOUGED AT FS 348, S26L. THE GOUGED AREA WAS CUT OUT, REPAIR FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-30-3, FIGURE 24, 51-30-2, 51-20-4.SDR CALA9901725Floor Panel · corrodedINSPECTION FOUND BLUE WATER STAINS AND CORROSION ON FLOOR PANEL AT STA 290-300. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-4, PAGE 4, 51-10-2, AND MM 51-20-0.SDR CALA9901724Hinge · crackedINSPECTION FOUND A .5 INCH CRACK IN CENTER HINGE BRACKET OF RT WING I/B AILERON TAB. THE HINGE WAS REMOVED AND REPLACED IAW SRM 57-50-01.SDR CALA9901723Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1148, BL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-1 AND 51-10-2.SDR MZZA99239Housing · crackedGUM - FLT 988 - EN ROUTE TO SPN, STARTED NOTICING A LOSS OF A-SYSTEM HYDRAULIC QUANTITY. REMOVED AND REPLACED MLG SEQUENCE VALVE PER MM 32-32-31. (X)SDR CALA9901721Doubler · gougedINSPECTION FOUND DOUBLER GOUGED AT FS 259-303, S24L. THE GOUGED AREA WAS CUT OUT AND FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5330-02912 AND BOEING DRAWING 65-18420.SDR CALA9901720Stiffener · crackedINSPECTION FOUND A 1 INCH CRACK AT EACH END OF PANEL 1104 STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.SDR DL72S992823Floorbeam · crackedTHE FS 294.5 FLOORBEAM WEB AT LBL 40 WAS FOUND WITH A 7 INCH LONG CRACK RUNNING FROM A CABLE PASS THROUGH HOLE TO THE LOWER EDGE OF THE WEB AND THROUGH THE LOWER CHORD. THE LOWER CHORD WAS REPLACED. THE DAMAGED SECTION OF WEB WAS REPAIRED WITH AN SDR DL72S992817Stiffener · crackedNR 2 SLAT O/B TRACK I/B SPAR STIFFENER CRACKED. REPLACED STIFFENER PER M/M 57-20-21 PG 813.SDR DL72S992816Stringer · crackedSTR 18A CRACKED AT STA 940 AFT SIDE OF RADIUS BLOCK AT AFT LOWER BOLT. REPAIRED PER M/M 53-12-0 PG 816, LEVEL II TIME LIMITED REPAIR.SDR DL72K992815Accessory Unit · malfuncitonedAFTER GEAR EXT, NOSE GEAR GREEN DOWN AND LOCK FAILED TO ILLUM. DIVERTED INTO JFK. REPLACED LANDING GEAR ACCESSORY UNIT.SDR DL72S992822Frame · crackedTHE FWD JAMB FRAME OF THE C1 DOOR CUTOUT FS 560 WAS FOUND WITH A 1 INCH CRACK IN THE FRAME WEB JUST BELOW THE NR 6 DOOR STOP FITTING. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH A DOUBLER PER ER/A 368895-14AD.SDR DL72S992805Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 740 REVEALED CRACK INDICATIONS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION OF THE SKIN PANEL BETWEEN FS 480 & 680 CONFIRMED CRACKS IN CONSECUTIVE FRAME BAYS. THE ENSDR DL72S992804Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 740 REVEALED CRACK INDICATIONS IN THE LOWER SKIN OF THE LOWER FASTENER ROW. INTERNAL MFEC INSPECTION OF THE SKIN PANEL BETWEEN FS 360 & 480 CONFIRMED A TOTAL OF 4 CRACKS IN ALONG THE SKIN LENSDR DL72S992803Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 740 REVEALED CRACK INDICATIONS. INTERNAL MFEC INSPECTION OF THE 4R LAP SPLICE BETWEEN FS 680 & 740 CONFIRMED 7 CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN ALONG THE LENGTH OF THE PANSDR CALA9901717Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 950D-990, BL 0. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A REPAIR WAS INSTALLED IAW SRM 51-10-4, FIGURE 3.SDR CALA9901716Support · bentINSPECTION FOUND FLOOR SUPPORT CORRODED AND BENT AT FS 660-800, BL 0. THE CORROSION WAS REMOVED IAW SRM 53-10-1. THE BENT SECTION OF FLOOR SUPPORT WAS REMOVED AND REPLACED USING SPLICES IAW SRM 51-40-2 AND 51-30-1.SDR CALA9901715Support · crackedINSPECTION FOUND A 3 INCH CRACK IN FLOOR SUPPORT AT FS 760, RBL 3. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30, 51-10-2, AND MM 51-20-0.SDR CALA9901714Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 420, RBL 20-40 AND AT STA 400-420, RBL 10. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9901713Angle · corrodedINSPECTION FOUND R-1 DOOR THRESHOLD ATTACH ANGLES CORRODED AT STA 380-420. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE ATTACH ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2, 51-10-2, 51-20-1, 51-40-3, FIGURE 1, AND MM 51-20-0.SDR CALA9901712Angle · corrodedINSPECTION FOUND TWO ATTACH ANGLES CORRODED FROM FS 216-219, RBL 15, L27R. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.SDR CALA9901711Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN NUT PLATE STRIP ANGLE AT STA 623, LONGERON 23R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 53-10-2.SDR CALA9901710Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT FS 277, RBL 12. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED USING SUPPORT ANGLES AND STIFFENERS IAW SRM 51-30-2 AND 51-40-4, FIGURE 1.SDR CALA9901709Seat Track · corrodedINSPECTION FOUND SEAT TRACK SECTIONS CORRODED AT STA 380-420, RBL 40 AND STA 990-1030, RBL 48. THE SEAT TRACK SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.SDR CALA9901708Skin · corrodedINSPECTION FOUND RT BODY FAIRING 3441 INNER SKIN AND SUPPORT NR 22 CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0. THE SUPPORT WAS REMOVED AND A DOUBLER AND BRACKET WERE INSTALLED SDR CALA9901706Skin · corrodedINSPECTION FOUND LEFT LOWER BODY FAIRING 3341 SKIN AND NR 7 SUPPORT CORRODED. THE SKIN WAS REMOVED AND NEW SKIN, DOUBLER, AND STRAPS WERE INSTALLED IAW SRM 53-30-3 AND 51-20-4. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9901705Frame · crackedINSPECTION FOUND A .75 INCH CRACK IN LT FRAME AT FS 930 BELOW WINDOW. REPAIRED IAW ECRA 5310-01397.SDR CALA9901704Skin · gougedINSPECTION FOUND LEFT O/B AILERON LOWER EDGE GOUGED. THE GOUGED AREA WAS REPAIRED IAW SRM 57-50-5, FIGURE 2 AND 51-20-0.SDR CALA9901703Beam · crackedINSPECTION FOUND A 2 INCH CRACK IN BEAM BEHIND WEB AFTER REMOVAL OF NR 8 SPOILER FITTING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6A. A REPAIR WAS INSTALLED IAW SRM 51-30-2.SDR CALA9901702Frame · crackedINSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 540, S27R. THE CRACKED SECTION OF FRAME WAS REMOVED AND A REPAIR DOUBLER, FRAME, AND ANGLE WERE INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.SDR CALA9901701Web · crackedINSPECTION FOUND A 2 INCH CRACK IN LEFT WING SLAT NR 1 O/B TRACK TO SLAT WEB. THE SLAT AND TRACK WERE REMOVED IAW MM 27-81-11. A NEW WEB, TRACK FITTING, AND LOWER SKIN WERE INSTALLED IAW SRM 51-30-2. THE SLAT AND TRACK WERE INSTALLED IAW MM 27-81-11.SDR CALA9901700Web · corrodedINSPECTION FOUND AFT CARGO C-3 DOOR CUTOUT FORWARD WEB LOWER SURFACE CORRODED AROUND NUT PLATES FROM STRINGER 27R TO 19R AT FS 1090. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 53-10-1, 51-20-1, AND 51-30-2.SDR CALA9901699Stringer · corrodedINSPECTION FOUND STRINGER 28L CORRODED AT STA 480. THE STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-10-2, 51-30-2, AND MM 51-20-0.SDR CALA9901698Panel · corrodedINSPECTION FOUND LT TRANSITION PANEL AT FS 540-670 CORRODED. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9901697Panel · corrodedINSPECTION FOUND RT TRANSITION PANEL CORRODED AT STA 950E. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2, 51-10-6, AND 51-40-3.SDR CALA9901696Panel · corrodedINSPECTION FOUND RT TRANSITION PANELS AT FS 480-560 AND FS 1070-1090 CORRODED. THE PANELS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-20-1, 51-10-2, AND MM 51-20-0.SDR CALA9901695Angle · crackedINSPECTION FOUND A 1 INCH IN COCKPIT FLOOR SUPPORT ANGLE AT FS 303, LBL 5. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-20-1.SDR CALA9901694Seat Track · corrodedINSPECTION FOUND RT O/B SEAT TRACK CORRODED FROM STA 1030-1070. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9901693Support · crackedINSPECTION FOUND A 3 INCH CRACK IN FLOOR SUPPORT AT FS 760, RBL 56. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-2, AND 51-20-0.
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