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 CALA9901692Seat Track · corrodedINSPECTION FOUND RT O/B SEAT TRACKS CORRODED AT STA 990-1030 AND 950B-970. THE SEAT TRACK SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9901691Panel · corrodedINSPECTION FOUND LEFT TRANSITION PANEL CORRODED AT FS 1110-1166 IN AFT PIT. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9901690Angle · corrodedINSPECTION FOUND TRANSITION PANEL ATTACH ANGLE AT STA 1148-1166 IN AFT PIT. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9901689Fitting · corrodedINSPECTION FOUND NR 6 SPOILER CENTER HINGE POINT LEFT AND RIGHT FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-20-3, PAGE 5.SDR CALA9901688Frame · bentINSPECTION FOUND FRAME UPPER FLANGE BENT AT STA 560, LONGERON 25L. THE BENT AREA WAS REMOVED AND AN ANGLE WAS INSTALLED IAW SRM 53-10-4, 51-10-2, AND 51-30-2.SDR CALA9901687Fitting · corrodedINSPECTION FOUND C1 CARGO DOOR LOWER FORWARD SILL FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9901686Stringer · corrodedINSPECTION FOUND STRINGER 26R CORRODED FROM STA 700-750. A REPAIR WAS INSTALLED IAW SRM 51-30-2.SDR CALA9901685Battery · dischargedINSPECTION FOUND EMERGENCY EXIT SIGNS AT L2 AND R2 DOORS INOPERATIVE. THE BATTERY WAS REMOVED AND REPLACED IAW MM 33-50-22.SDR CALA9901684Battery Pack · dischargedINSPECTION FOUND EMERGENCY LIGHTS FROM ROW 23-30 INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-50-01, PAGE 501.SDR CALA9901683Wire · brokenINSPECTION FOUND THE LT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. A BROKEN WIRE AT CONNECTOR ON POWER SUPPLY WAS REPAIRED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-22, PAGE 401.SDR CALA9901682Power Supply · inoperativeINSPECTION FOUND THE RT AND LT SERVICE DOOR EMERGENCY SLIDE LIGHTS INOPERATIVE. THE POWER SUPPLY HAD FAILED AND A SHORTED WIRE WAS FOUND. THE POWER SUPPLY WAS REPLACED AND THE WIRE WAS REPAIRED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-00, PAGE 401.SDR CALA9901681Skin · wornINSPECTION FOUND THE RT I/B FOREFLAP UPPER SKIN WORN THROUGH. THE FOREFLAP WAS REPAIRED IAW SRM 51-40-6.SDR CALA9901680Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN LEFT MLG O/B DOOR SKIN INNER SURFACE. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-2.SDR CALA9901679Panel · corrodedINSPECTION FOUND VERTICAL STABILIZER RT ACCESS PANEL NR 5216 AND STIFFENER CORRODED. A NEW PANEL AND NUT PLATES WERE INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-30-2, 51-10-2, AND MM 51-20-0.SDR CALA9901678Web · corrodedINSPECTION FOUND WEB CORRODED AT WING CENTER SECTION, FS 770 LOWER TORQUE BOX AT KEEL AREA. THE CORRODED SECTION OF WEB WAS CUT OUT AND A NEW WEB SECTION WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-40-2, AND MM 51-20-0.SDR CALA9901677Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN ATTACH ANGLE AT FS 1193, RBL 20. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.SDR CALA9901675Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 1050-1070, LONGERON 27L. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE WAS INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-30-2.SDR CALA9901674Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT STA 480, LONGERON 27R-27L. THE SHEAR TIE WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-4, FIGURE 12.SDR CALA9901673Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1110-1130, LBL 15. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-0, PAGE 3.SDR CALA9901672Web · crackedINSPECTION FOUND RT WING ROOT L/E TO BODY LOWER SUPPORT WEB CRACKED AT NUT PLATE HOLE, FS 720E, STRINGER 21R. THE CRACK WAS 1 INCH LONG. THE CRACKED AREA WAS CUT OUT, FILLER AND DOUBLER WAS INSTALLED IAW SRM 51-40-2 AND 51-30-2.SDR CALA9901671Support · corrodedINSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 420, RBL 12-25. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.SDR CALA9901670Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL ATTACH ANGLE AT STA 720F, BL 0. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.SDR CALA9901669Angle · brokenINSPECTION FOUND ATTACH ANGLE FOR RT TRANSITION WEB AT FS 560, LONGERON 27R BELOW TORQUE BOX BROKEN OFF. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2.SDR CALA9901668Web · corrodedINSPECTION FOUND WEB CORRODED AT AFT CARGO DOOR JAMB. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-20-1.SDR CALA9901667Pan · crackedINSPECTION FOUND A 4 INCH CRACK IN L-1 DOOR INNER PAN FORWARD LOWER CORNER. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5265-01005.SDR CALA9901666Frame · crackedINSPECTION FOUND A 1.25 INCH CRACK IN RT FUSELAGE FRAME AT STA 312, LONGERON 13R. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-4, FIGURE 1. REPAIR ANGLES WERE INSTALLED IAW SRM 53-10-4, 51-10-2, AND 51-30-0.SDR CALA9901665Support · corrodedINSPECTION FOUND RT LOWER BODY FAIRING SUPPORT NR 10 CORRODED. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.SDR CALA9901664Skin · corrodedINSPECTION FOUND SKIN OF RT ACCESS PANEL AT FUSELAGE BELLY BETWEEN HEAT EXCHANGERS CORRODED WITH PULLED RIVETS. THE SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-2.SDR CALA9901663Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 380, LONGERON 8R. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-4. A REPAIR WAS INSTALLED IAW SRM 53-10-4, FIGURE 1.SDR CALA9901662Stiffener · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 3 ENGINE COWL NR 10 STIFFENER. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-20-1 AND 51-30-2.SDR CALA9901661Web · crackedINSPECTION FOUND A 3 INCH CRACK IN AFT CARGO DOOR JAMB UPPER AFT WEB. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-20-1.SDR CALA9901660Angle · corrodedINSPECTION FOUND WEB SUPPORT ANGLE CORRODED WING CENTER SECTION FS 790 LOWER TORQUE BOX AT KEEL AREA. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, PAGE 7.SDR CALA9901659Angle · corrodedINSPECTION FOUND WEB SUPPORT ANGLE CORRODED AT WING CENTER SECTION LOWER TORQUE BOX AT KEEL AREA, FS 810. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-1, PAGE 4 AND 51-10-2.SDR CALA9901658Frame · crackedINSPECTION FOUND A .75 INCH CRACK IN LT FORWARD NLG DOOR SIXTH FRAME. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.SDR CALA9901657Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES AT STA 344, LBL 20 TO LBL 60. A REPAIR WAS INSTALLED IAW SRM 53-10-8, FIGURE 9.SDR CALA9901656Support · crackedINSPECTION FOUND A 1 INCH CRACK ON EACH END OF FLOOR SUPPORT AT STA 848, BL 0 AND LBL 25. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.SDR CALA9901655Skin · dentedINSPECTION FOUND BOTTOM OF NR 3 ENGINE COWL SKIN DENTED AND SCRATCHED BETWEEN STIFFENERS 9 & 10. THE DAMAGED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 54-30-3.SDR CALA9901654Fitting · corrodedINSPECTION FOUND CENTER CARGO DOOR FORWARD PRESSURE RELIEF DOOR SKIN FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9901653Seat Track · corrodedINSPECTION FOUND LT O/B SEAT TRACK CORRODED FROM STA 950-1038. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-2, 51-30-2.SDR CALA9901647Skin · delaminatedINSPECTION FOUND THE LT INBOARD T/E FLAP DELAMINATED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-2, PAGE 405.SDR DL72S992769Battery Pack · dischargedON MTC LAYOVER, LT OUTSIDE EMERGENCY EGRESS LIGHTING INOP. REPLACED FWD LIGHT POWER SUPPLY. REPLACED BULBS FOR MID LIGHT AND REPLACED BATTERY PACK ON AFT LIGHT, OPER NOW NORMAL.SDR DL72S992761Skin · crackA .75 INCH LONG CRACK WAS FOUND EMANATING FROM A FASTENER HOLE NEAR THE UPPER FORWARD CORNER OF THE R1 DOOR CUTOUT (FS 380). THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 368954-14, SDR DL72L992760Web · dentTHE NR 4 RIB OF THE VERTICAL STABILIZER HAS A DENT IN THE WEB THAT RESULTED IN A 1 INCH DIAMETER CUTOUT. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333924-14.SDR DL72K992768Battery · dischargedFORWARD OUTBOARD FLIGHT ATTENDANT FLASHLIGHT NO TEST. REPLACED BATTERY. FLASHLIGHT NOW OPS NORMAL.SDR CALA9901644Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM UPPER CHORDS CORRODED AT FS 1030 FROM LBL 12 TO RBL 40. A REPAIR WAS INSTALLED IAW SRM 53-10-8, 51-10-2, 51-30-1, AND MM 51-20-0.SDR CALA9901643Floorbeam · gougedINSPECTION FOUND FLOORBEAM GOUGED AT STA 344, RBL 45. A REPAIR WAS INSTALLED IAW SRM 51-10-2, 51-20-4, 51-30-2, MM 51-20-0, ECRA 5310-03955, AND EA 27-5310-2-A0532.SDR CALA9901641Panel · corrodedINSPECTION FOUND LT TRANSITION PANELS AT FS 1030-1065 AND FS 1065-1090 CORRODED. THE PANELS WERE REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9901640Panel · corrodedINSPECTION FOUND LT AND RT TRANSITION PANELS AT FS 990-1030, S27L AND RT TRANSITION PANEL AT FS 1030-1070 CORRODED. THE PANELS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-01.SDR CALA9901638Panel · corrodedINSPECTION FOUND TRANSITION PANELS AT FS 620-660, S24R AND AT STA 660-800, S23L CORRODED. THE PANELS WERE REMOVED AND NEW PANELS WERE INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9901637Support · crackedINSPECTION FOUND A 1 INCH CRACK IN SECOND FRAME SUPPORT FROM AFT OF LT FORWARD NR 2 ENGINE COWL. THE FRAME SUPPORT WAS REMOVED AND A NEW FRAME SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30-1, AND 51-10-1.
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