Boeing 737-130
Service difficulty reports · 287
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 = '737130' 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 = '737130' 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 CAL950518Pressure Panel · corroded31J - THE NOSE WHEEL WELL PRESSURE BULKHEAD WAS FOUND WITH A CORROSION BULGE 1 INCH IN DIAMETER, AT THE AFT FORWARD OUTBOARD CORNER OF THE LEFT ACCESS PANEL BETWEEN THE SKIN AND INVERTED 'T'. THE PRESSURE PANEL WAS REPAIRED IAW ECRA 5310-03128, REV IR. (M)SDR CAL950423Carriage Spindle · shearedIAH - INSPECTION FOUND THE RIGHT OUTBOARD FLAP OUTBOARD CARRIAGE SPINDLE SHEARED AT FORWARD RETAINING NUT. THE CARRIAGE ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (M)SDR CAL950440Lap Seam · corroded31J - INSPECTION FOUND CORROSION IN THE LAP SEAM AT BS 420, STR 27R. THE CORRODED AREA WAS REMOVED. A DOUBLER AND FILLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 53-30-03. (X)SDR CAL950405Skin · crackedGSO - INSPECTION FOUND FUSELAGE SKIN FASTENER HOLES CRACKED IN SEVERAL PLACES BETWEEN WL 207.5 AND 234.35, SECTION 41. THE CRACKS WERE APPROXIMATELY .25 INCH LONG. THE CRACKED AREA WAS REMOVED. DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW EA 5310-0SDR CAL950404Skin · crackedGSO - INSPECTION FOUND FUSELAGE SKIN FASTENER HOLES CRACKED IN SEVERAL LOCATIONS BETWEEN BS 188-251.6 RIGHT SIDE. THE CRACKS WERE APPROXIMATELY .25 INCH LONG. THE CRACKED SECTION OF SKIN WAS REMOVED. REPAIR DOUBLER S AND FILLERS WERE FABRICATED AND INSTALLESDR CAL950403Skin · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN EXTERNAL SKIN AT STRINGER 4L, STATION 908. THE CRACKED AREA WAS CUTOUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. (W)SDR CAL950402Frame · corrodedGSO - INSPECTION FOUND CORROSION ON FRAME ABOVE STRINGER 26R AT STATION 529. A NEW FRAME AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. (W)SDR CAL950401Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME BETWEEN S20L AND S21L AT STATION 440. THE FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING NR 65C25113 AND EA 5310-01211. (W)SDR CAL950400Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME BETWEEN S20L AND S21L AT STATION 500. THE CRACKED SECTION OF FRAME WAS CUTOUT. A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW BOEING BLUE PRINT NR 65C25113 AND EA 5310-01211. (W)SDR CAL950399Frame · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME BETWEEN S20L AND S21L AT STATION 480. THE CRACKED SECTION OF FRAME WAS CUOTUT. A NEW SECTION OF FRAME WAS INSTALLED IAW BOEING DRAWING NR 65C25113 AND EA 5310-01211. (W)SDR CAL950398Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME BETWEEN S22L AND S23L AT STATION 460. THE CRACKED FRAME WAS REMOVED AND A NEW FRAME AND DOUBLERS WERE INSTALLED IAW BOEING PRINT NR 65C25113. (W)SDR CAL950437Fitting · cracked31J - INSPECTION FOUND A .3750 INCH CRACK IN THE RT BS 695 FRAME AFT LOWER FITTING AT THE OUTBOARD FASTENERS IN THE AFT HORIZONTAL FLANGE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SB 737-53-1080, REV. 2 AND BOEING DRAWING 65C34490. (X)SDR CAL950439Shear Beam · cracked3LJ - A .3750 INCH CRACK WAS FOUND IN THE RADIUS OF THE INBOARD FLANGE AT THE FORWARD END OF THE LT S18A SHEAR BEAM, AFT SIDE OF BS 664 BULKHEAD. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, SRM 51-40-3, SRM 51-10-2, SRM SDR CAL950438Frame · cracked31J - A 1 INCH CRACK WAS FOUND IN THE AFT LOWER CORNER OF THE L-2 DOOR FRAME. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5210-01224. (X)SDR CAL950294Hyd Line · leakingEWR - FLT 1477 - THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE ON DESCENT INTO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE A-SYSTEM HYDRAULIC PRESSURE LINE IN LEFT WING ABOVE LEFT GEAR LEAKING. THE LINE WAS REPLACED USSDR CAL950253Combustor Unit · inoperativeDTW - FLT 1851 - A RUMBLING NOISE FOLLOWED BY A SERIES OF BANGS WAS HEARD IN THE AFT SECTION OF AIRCRAFT WHILE IN FLIGHT. INSPECTION BY MAINTENANCE FOUND THAT THE NOISE WAS CAUSED BY SURGING OF THE APU. THE APU COMBUSTOR UNIT WAS FOUND AT FAULT. THE APU COMSDR CAL950261Intercostal · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN INTERCOSTAL UPPER FLANGE AT BS 984, LBL 37. THE INTERCOSTAL WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-0. (X)SDR CAL950260Angle · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN FRAME TO STRINGER ATTACH ANGLE AT STR 26R, STA 333. THE CRACKED ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, SRM 51-30-2, AND SRM 53-10-3. (X)SDR CAL950259Stringer · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN STR 28R, LOCATED IN THE FORWARD PIT AT STA 420 - STA 440. THE DAMAGED AREA WAS CUT OUT AND CHANNEL FILLER AND SHIMS WERE INSTALLED IAW SRM 53-10-3, SRM 51-10-2, AND SRM 51-30-2. (X)SDR CAL950258Stringer · corrodedGSO - INSPECTION FOUND CORROSION ON STR 27R AT STA 446. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X)SDR CAL950257Angle · corrodedGSO - INSPECTION FOUND CORROSION INSIDE WEB OF DOOR SILL ANGLE AND NUT PLATES AT STA 440, STR 25R. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND SRM 51-1-21A. (X)SDR CAL950256Web · corrodedGSO - NOSE WHEELWELL, LEFT UPPER PANEL WEB, WAS FOUND BULGED AT FORWARD EDGE AND THERE WAS CORROSION ON UPPER SURFACE AND INSIDE FASTENER HOLES. AN INTECOSTAL WAS FABRICATED AND INSTALLED IAW SRM 54-10-3 AND SRM 51-30-2. (X)SDR CAL950255Web · corrodedGSO - THE NOSE WHEELWELL, RT UPPER PANEL WEB, WAS FOUND BULGED AT FORWARD EDGE AND THERE WAS CORROSION INSIDE FASTENER HOLE. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 54-10-3 AND SRM 51-30-2. (X)SDR CAL950254Skin · crackedGSO - INSPECTION FOUND CRACK INDICATIONS IN SKIN AT LEFT FS BS 188-253, WL 208.1 TO WL 234.35. THE CRACKS WERE APPROXIMATELY .50 INCH LONG. THE CRACKED AREAS OF SKIN WERE CUT OUT AND DOUBLERS AND FILLERS WERE INSTALLED IAW EA 5310-01188. (X)SDR CAL950241Hydraulic Line · chafedEWR - FLT 1204 - THE B-SYSTEM HYDRAULIC QUANTITY WAS LOST WHILE EN ROUTE TO EWR. THE A-SYSTEM QUANTITY GAUGE DECREASED TO ONE GALLON. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND A B-SYSTEM HYDRAULIC PRESSURE LINE CHAFED THROUGH. THE HYDRSDR CAL950152Hyd Line · chafedFLT NR 1484 - EWR - THE 'A' HYDRAULIC SYSTEM WAS LOST APPROXIMATELY 20 MINUTES BEFORE ARRIVING IN EWR. THE HYDRAULIC QUANTITY INDICATED ZERO. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE 'A' SYSTEM AILERON PCU HYDRAULIC PRESSURE LINE CSDR CALA950158Skin · corrodedGSO - INSPECTION FOUND THE FUSELAGE SKIN BULGED OVER STRINGER 20L AT STA 970, BELOW REAR ENTRY. THE DAMAGED AREA WAS CUT OUT AND A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-2 FIG 15 SRM 51-20-4 AND SRM 51-30-2. (W)SDR CAL950160Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN O/B RIB AT RT WING NR 4 SLAT O/B TRACK. THE CRACK WAS STOP DRILLED AND REPAIR FITTINGS WERE INSTALLED IAW EC 5710-01660. (W)SDR CAL950159Skin · corrodedGSO - INSPECTION FOUND THE SKIN BULGED AT LAP JOINT STRINGER 19L STA 940 TO 950. THE DAMAGED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-6, 53-30-3 AND 51-30-2. (W)SDR CAL950137Hyd Line · leakingCLE - FLT 1475 - THE A-SYSTEM HYDRAULIC FLUID QUANTITY BEGAN TO DECREASE AFTER TAKEOFF FROM CLE. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 ENGINE A-HYDRAULIC SYSTEM PRESSURE LINE UNION IN THE RT WHEELWELL LEAKISDR CAL950101Battery Charger · inoperativeTPA - FLT 1790 - THE FLIGHT ATTENDANT REPORTED A SMOKY ODOR IN CABIN DURING CLIMB-OUT. THE BATTERY CHARGER CIRCUIT BREAKER WAS PULLED AND THE ODOR SUBSIDED. THE AIRCRAFT WAS RETURNED TO TPA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE BATTERY CHASDR CAL950199Slat · cracked31J - INSPECTION FOUND A 1 INCH CRACK IN THE LEFT LEADING EDGE NR 3 SLAT NR 1 HINGE DOOR AREA. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-10-2, 57-30-4, AND 51-30-2. (X)SDR CAL950198Floor Beam · cracked31J - A 2 INCH CRACK WAS FOUND IN THE FLOOR BEAM AND RUNNING UNDER THE RADIUS AT BS 716.0 AND BL 0. A REPAIR WAS FABRICATD AND INSTALLED IAW SRM 53-10-9. (X)SDR CAL950197Skin · cracked31J - A 1 INCH CRACK WAS FOUND ON THE OUTER SKIN OF THE LEFT FORWARD EMERGENCY EXIT DOOR. THE CRACK WAS STOP DRILLED, ROUGH EDGES WERE BLENDED OUT, AND A REPAIR WAS INSTALLED IAW SRM 52-00-2. (X)SDR CAL950196Web · corroded31J - CORROSION WAS FOUND ON THE LT OUTBOARD MID-FLAP WEB AND DOUBLER AT THE FOREFLAP ATTACH POINT. THE CORRODED AREA WAS REMOVED AND REPAIR WAS INSTALLED IAW SRM 51-10-6, 51-40-6, 51-10-3, AND 57-52-00. (X)SDR CAL950072Dnlock Sensor · inoperativeEWR - FLT 1881 - THE RT MLG GREEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GREEN LIGHT WOULD EXTINGUISH BY MOVING THE GEAR HANDLE TO UP, BUT WOULD COME BACK ON WITH THE GEAR HANDLE IN OFF. THE ACFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCSDR CAL950001Hyd Line · chafedFLT NR 1680 - ORD - THE 'A' SYSTEM HYDRAULIC QUANTITY INDICATION SLOWLY DROPPED TO ZERO WHILE EN ROUTE FROM MCI TO MKE. THE AIRCRAFT WAS DIVERTED TO ORD. THE 'A' SYSTEM LOW PRESSURE LIGHTS BEGAN TO FLICKER ON AND OFF WHILE ON FINAL APPROACH. THE AIRCRAFT LA
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