Boeing 727-224
Service difficulty reports · 2,252
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 = '727224' 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 = '727224' 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 CALA9801736Track · corrodedINSPECTION FOUND NR 4 FLAP TRACK FORWARD CLEVIS CORRODED ON BOTH SIDES. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.SDR CALA9801705Angle · crackedINSPECTION FOUND A 4 INCH CRACK IN ANGLE AND DOUBLER AT RT WING FIXED LEADING EDGE RIB AT SLAT STA 0. THE DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND 51-40-3, FSDR CALA9801704Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN BRACKET WHERE RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-40-3, 51-30-2, AND 51-10-2.SDR CALA9801703Doubler · crackedINSPECTION FOUND A .5 INCH CRACK IN DOUBLER INSIDE LT INBOARD FLAP AT AFT END OF INBOARD FLAP TRACK CARRIAGE SPINDLE CUTOUT. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-1 AND 51-30-2.SDR CALA9801702Rib · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT O/B MIDFLAP O/B END RIB FORWARD OF MID SPAR. THE CRACK WAS STOP DRILLED. A DOUBLER ANGLE WAS INSTALLED IAW SRM 51-30-2, PAGE 4.SDR CALA9801701Skin · dentedINSPECTION FOUND FUSELAGE SKIN AND RIB DENTED JUST AFT OF NLG AFT DOOR. THE RIB AND SKIN WERE REMOVED AND REPLACED IAW SRM 51-10-1.SDR CALA9801700Pad · corrodedINSPECTION FOUND BOTTOM SURFACE OF SPOILER BEAM PAD CORRODED WHERE NR 3 FLAP TRACK MOUNTS. THE FLAP TRACK MOUNT PAD WAS REMOVED AND REPLACED IAW SRM 51-10-2, PAGE 1 AND 51-30-2, PAGE 14.SDR CALA9801699Track · corrodedINSPECTION FOUND RT WING NR 5 FLAP TRACK FORWARD LUG AREA CORRODED. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.SDR CALA9801695Track · corrodedINSPECTION FOUND RT WING NR 8 FLAP TRACK FORWARD ATTACH LUG AREA CORRODED. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.SDR CALA9801694Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN OUTBOARD BRACKET WHERE RT WING NR 5 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9801693Hat Channel · corrodedINSPECTION FOUND HAT CHANNEL CORRODED AT FS 1150, LBL 24. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.SDR CALA9801692Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1034, RBL 45-65. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.SDR CALA9801691Skin · corrodedINSPECTION FOUND RT ELEVATOR SKIN LOWER SURFACE CORRODED. THE CORRODED AREA WAS CUT OUT AND A NEW FITTING AND DOUBLER WERE INSTALLED IAW SRM 55-20-3, FIGURE 2, PAGE 2, 51-10-2, AND 51-40-5.SDR CALA9801690Carriage · corrodedINSPECTION FOUND NR 7 FLAP OUTBOARD FLAP INBOARD CARRIAGE CORRODED. THE FLAP CARRIAGE WAS REMOVED AND REPLACED IAW MM 57-53-2.SDR CALA9801679Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 22.5 TO 24.5. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-8 AND 51-30-2.SDR CALA9801678Angle · crackedINSPECTION FOUND A .375 CRACK IN ANGLE AT INTERCOSTAL AT BS 950A-950B, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.SDR CALA9801677Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 1067, RBL 12-24 AND RBL 45-65. THE FLOOR SUPPORTS WERE REMOVED AND A NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-1AND 51-10-2.SDR CALA9801676Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1034, RBL 24-45. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2.SDR CALA9801675Web · corrodedINSPECTION FOUND RT WEB CORRODED AT FS 1122, RBL 65. THE CORRODED AREA WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-2, 51-10-1, PAGE 4, AND 51-30-2.SDR CALA9801674Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT TOP FLANGE SCREW HOLE FS 1050, RBL 35. THE CORRODED AREA WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 51-10-1, 51-10-2, AND 53-10-5, FIGURE 7.SDR CALA9801673Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1140, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-10-1, AND 51-30-2.SDR CALA9801672Mount · corrodedINSPECTION FOUND FORWARD LAV FLOORBOARD MOUNT FRAME AT STA 312-344 HAD CORROSION AROUND MOUNTING HOLES. THE MOUNT FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 53-10-8.SDR CALA9801669Spindle · corrodedINSPECTION FOUND NR 8 FLAP CARRIAGE AFT SPINDLE CORRODED. THE NR 8 FLAP CARRIAGE ASSEMBLY WAS REMOVED AND REPLACED IAW MM 57-50-00.SDR CALA9801668Pressure Panel · crackedINSPECTION FOUND A .9375 INCH CRACK IN LT MLG WHEEL WELL CEILING PRESSURE PANEL JUST FORWARD OF WHEEL WELL LIGHT AT STA 930, LBL 48. THE CRACK WAS STOP DRILLED IAW BOEING DRAWING 65-89360. A DOUBLER WAS INSTALLED IAW BOEING DRAWING 65-89360.SDR CALA9801667Track · corrodedINSPECTION FOUND CORROSION IN BORE WHERE BUSHINGS MOUNT ON LT AND RT SIDES OF NR 3 FLAP TRACK FORWARD CLEVIS. THE FLAP TRACK ASSEMBLY WAS REMOVED AND REPLACED IAW MM 57-40-00.SDR CALA9801666Track · corrodedINSPECTION FOUND NR 1 FLAP TRACK PAD MOUNT CENTER HOLE CORRODED. THE FLAP TRACK ASSEMBLY WAS REMOVED AND REPLACED IAW MM 57-40-00.SDR CALA9801665Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN STRINGER 15L AND 15R AT STA 720B. REPAIRS WERE INSTALLED IAW SRM 53-10-3 AND 51-10-2.SDR CALA9801664Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1130-1150, RBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-6 AND 51-10-2.SDR CALA9801663Floor · corrodedINSPECTION FOUND FLOOR WEB WITH CORROSION RUNNING INTO SPLICE AT FS 1178-1183, RBL 16. THE CORRODED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-2, FIGURE 1, 51-10-2, AND 51-30-2, PARAGRAPH 7.SDR CALA9801662Skin · dentedINSPECTION FOUND LT OUTBOARD AILERON TAB DENTED ON UPPER SURFACE WITH THE TRAILING EDGE BENT. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41.SDR CALA9801661Flap Track · corrodedINSPECTION FOUND RT WING NR 6 FLAP TRACK CORRODED AROUND FORWARD MOUNT HOLES. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.SDR CALA9801658Track · corrodedINSPECTION FOUND RT WING NR 7 FLAP TRACK ROLLER SURFACES CORRODED. THE FLAP TRACK ASSEMBLY WAS REMOVED AND REPLACED IAW MM 57-40-00.SDR CALA9801657Skin · corrodedINSPECTION FOUND CORROSION IN RT ELEVATOR SKIN UNDER OUTBOARD MOST STATIC WICK BASE. THE CORRODED AREA WAS CUT OUT. A NEW DOUBLER AND FITTING WERE INSTALLED IAW SRM 55-20-3, FIGURE 2, PAGE 2.SDR CALA9801656Support · corrodedINSPECTION FOUND FORWARD LAV INBOARD WALL FLOOR SUPPORT CORRODED. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-1, PAGE 4.SDR CALA9801655Rib · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT WING TIP RIB UPPER FLANGE BY INBOARD AFT CORNER OF FUEL VENT OUTLET. THE CRACK WAS STOP DRILLED IAW SRM 51-30-2. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, FIGURE 1.SDR CALA9801644Carriage · corrodedINSPECTION FOUND NR 2 FLAP CARRIAGE AFT SPINDLE BUSHING CORRODED. THE NR 2 FLAP CARRIAGE ASSEMBLY WAS REMOVED AND REPLACED IAW MM 57-50-00.SDR CALA9801643Carriage · corrodedINSPECTION FOUND RT WING NR 5 FLAP CARRIAGE SPINDLE CORRODED AT FORWARD AREA. THE NR 5 FLAP CARRIAGE ASSEMBLY WAS REPLACED IAW MM 57-50-00.SDR CALA9801642Skin · corrodedINSPECTION FOUND CORROSION IN RT ELEVATOR SKIN UNDER OUTBOARD CENTER STATIC WICK BASE. THE CORRODED AREA WAS CUT OUT, A DOUBLER AND FITTING WERE INSTALLED IAW SRM 55-20-3 FIGURE 2 PAGE 2.SDR CALA9801641Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD MIDFLAP RIB OUTBOARD OF INBOARD CARRIAGE SPINDLE MOUNT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-10-5, FIGURE 1.SDR CALA9801640Rib · crackedINSPECTION FOUND A 2.75 AND 1 INCH CRACK IN RIB INSIDE RT WINGTIP, ACCESSED THROUGH PANEL NR 8811. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. ANGLE REPAIRS WERE INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.SDR 98ZZZM863Skin · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION ON EXT FUSELAGE SKIN ABOVE R2 SERVICE DOOR UPPER HINGE AND BELOW R2 SERVICE DOOR BELOW LOWER HINGE. CORROSION WAS REPAIRED PER BOEING LETTER AND DRAWING HAE-TUS-98-014RR DATED 8/7/98 AND SRM 51-10-6, 53-30-1, 53-30-2, DSDR 98ZZZM862Floorbeam · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON STATION 1130 FLOORBEAM, CORROSION REMOVAL BLENDOUT WAS BEYOND SRM LIMITS. CORROSION WAS REPAIRED PER BOEING LETTER AND DRAWING HAE-TUS-98-0166TR AND SRM 53-10-8. AUTHORIZATION PER FAA FORM 8110-3 DATED 8/27/98, FSDR CALA9801578Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN SUPPORT BRACKET FOR LT WING NR 2 LEADING EDGE FLAP ACTUATOR. A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2.SDR CALA9801577Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 5 SLAT ACTUATOR INBOARD ATTACH RIB. THE CRACK WAS STOP DRILLED, A REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 51-10-1.SDR CALA9801576Channel · crackedINSPECTION FOUND A 1.25 INCH CRACK IN CHANNEL INSIDE TRAILING EDGE AT UPPER SKIN OUTBOARD END OF AFT FALSE SPAR ABOVE NR 3 FLAP TRANSMISSION. A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2.SDR CALA9801575Bracket · crackedINSPECTION FOUND A .375 INCH CRACK IN SUPPORT BRACKET FOR LT WING NR 1 LEADING EDGE FLAP ACTUATOR. A NEW BRACKET WAS INSTALLED IAW SRM 51-10-1 AND 51-30-2.SDR CALA9801574Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT CARGO STIFFENER AT STA 950A, LONGERON 29R. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2, 51-10-1, 51-10-2.SDR CALA9801573Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT LT SIDE, STA 1166, TWO INCHES ABOVE TOP OF FLOORBEAM. THE CORRODED AREA WAS CUT OUT, A DOUBLER WAS INSTALLED IAW ECRA 5330-02699.SDR CALA9801558Bottle Pin · corrodedINSPECTION FOUND RT AFT BOTTLE PIN CORRODED. THE BOTTLE PIN AND FORWARD AND AFT BUSHINGS WERE REMOVED AND REPLACED, THEN SAFETIED AND SEALED IAW MM 57-41-1.SDR CALA9801557Fitting · corrodedINSPECTION FOUND LT AND RT HORIZONTAL STABILIZER ATTACH FITTING CORRODED. THE CORROSION WAS REMOVED BY BORING HOLES. NEW BUSHINGS AND BEARINGS WERE INSTALLED. THE BEARINGS WERE TORQUED AND SAFETIED IAW ECRA 5550-01033.
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