Boeing 737-301
Service difficulty reports · 4,797
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 = '737301' 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 = '737301' 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 USAA991450Door Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5I NCH CRACK DOOR FRAME CUTOUT UPPER FORWARD STOP FITTING DOOR FRAME WEB. REMOVED AND REPLACED PER SRM 51-10-02. (M)SDR USAA991451Seat Track · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT FORWARD END OF SEAT TRACK STATION 345, LBL 20. REPLACED SEAT TRACK PER SRM 53-00-02. (M)SDR USAA991452Angle · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 4 INCH AREA OF CORROSION AT STATION 294.6 UPPER CHORD AFT FLANGE RBL 50.5, CORROSION LEVEL 1. INSTALLED ANGLE PER SRM 53-10-51 FIG 101. (M)SDR USAA991467Skin · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TWO 1.9 INCH CRACKS BS 328 FORWARD SERVICE DOORWAY, DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN. INSTALLED OUTER DOUBLER AND 2 MIDDLE DOUBLERS PER SRM 53-10-01 FIG 202. (M)SDR USAA991468Skin · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FIVE 1 INCH CRACKS ALONG ACTUATOR LOWER SKIN NR 1 SLAT. INSTALLED FILLER AND DOUBLER PER TR 57-50-01. (M)SDR USAA991475Window Post · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK L-1 WINDOW AFT UPPER POST. INSTALLED DOUBLER PER EA 66274. (M)SDR USAA991476Frame · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION AFT CARGO BS 793 STRINGER 25R FRAME, CORROSION LEVEL 1. REPAIRED PER SRM 51-20-01 AND SRM 51-10-02. (M)SDR USAA991477Angle · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 36 INCH BY 2 INCH AREA OF CORROSION FORWARD SERVICE DOOR Z-ANGLE STATION 289-325, RBL 61. CORROSION LEVEL 1. REPLACED Z-ANGLE PER SRM 51-10-02. (M)SDR USAA991494Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT BS 311.9, STRINGER 5L CORNER OF FRAME. INSTALLED DOUBLER PER EA 66257 AND TR 53-10-14. (M)SDR USAA991495Web · crackedCLT - DURIGN Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 294.5, STRINGER 7L, IN CORNER MOUNT POINT WEB. REMOVED AND REPLACED PER SRM 51-10-02 AND BOEING DWG 65-17684. (M)SDR USAA991496Web · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT BS 306.0, STRINGER 4L MIDDLE LOWER LEG WEB. REMOVED AND REPLACED PER SRM 53-00-03. (M)SDR USAA991497Stringer · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STATION 726, STRINGER 18A SHELF, RBL 61, WL 188. REPAIRED PER SERM 51-10-02. (M)SDR USAA991498Web · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT N/G UPPER DRAG HRM WEB. INSTALLED NEW WEB PER REPAIR DOCUMENT 51-10-02. (M)SDR USAA991506Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION ON FLOORBEAM STATION 344, BL 0 UPPER CHORD, CORROSION LEVEL 2. SPLICED IN NEW T-CPA PER SRM 53-10-51 FIG 205. (M)SDR USAA991499Frame · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 6 INCH BY 1.5 INCH AREA OF CORROSION ON FRAME STATION 927 BETWEEN STRINGER 27L AND STRINGER 7R. CORROSION LEVEL 2. INSTALLED REPAIR DOUBLER PER SRM 53-00-07 AND SRM 51-40-01. (M)SDR USAA991373Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 887, STRINGER 9L TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991417Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 663, STRINGER 10R TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991418Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 807, STRINGER 6R TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M)SDR USAA991419Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 847, STRINGER 8R AND 9R FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991420Frame · crackedCLT - DURIGN Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480, STRINGER 8R AND 9R FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991421Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK BS 847 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA991423Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH AT 3 AREAS UPPER CHORD TOP SURFACE BS 312, LBL 12 - RBL 24. FLOORBEAM CORROSION LEVEL 2. INSTALLED T-CAP PER SRM 53-10-51. (M)SDR USAA991440Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK BS 480 BETWEEN STRINGER 8 AND 9 LEFT FRAME. INSTALLED DOUBLER AND FILLER PER TR 53-10-14. (M)SDR USAA991439Stringer · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS STRINGER 4L AT BS 908 AND 909 STRINGER. INSTALLED STRINGER PER SRM 51-40-00. (M)SDR USAA991438Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 827 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66285. (M)SDR USAA991437Splice · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK STRINGER 4R STATION 908 SPLICE. INSTALLED STRINGER PER SRM 51-40-00. (M)SDR USAA991436Stringer · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY .5 INCH, AREA OF CORROSION ON STRINGER 10R, STATION 337. CORROSION LEVEL 1. INSTALLED NEW STRINGER PER SRM 51-10-02. (M)SDR USAA991431Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY .05 INCH AREA OF CORROSION ON FLOORBEAM STATION 344, LBL 9.5 UPPER CHORD OF T-CAP. CORROSION LEVEL 1. SPLICED IN NEW T-CAP PER SRM 53-10-51 FIG 205. (M)SDR USAA991430Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY .05 INCH AREA OF CORROSION ON FLOORBEAM STATION 344, RBL 2.5 AFT EDGE OF T-CAP. CORROSION LEVEL 1. SPLICED IN NEW T-CAP PER SRM 53-10-51 FIG 205. (M)SDR USAA991424Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 663, STRINGER 10L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)SDR AWXA0000001Actuator · malfunctionedWITH GEAR UP, RT MAIN RED GEAR UNSAFE LIGHT IS ILLUMINATED, THRUST AT CLIMB, NO YAW. REPLACED RT MLG UPLOCK ACTUATOR AND SENSOR. OPS AND RETRACT CK GOOD. TT 0028847 M+E 03-3232-9-0003CURERENT HISTORY: NONERECOMMENDATION: REMAIN OPEN PENDING REVIEW OF TEASDR USAASB99309Selector · lack of lubePIT - FLT705 - ON APPROACH INTO PIT, AS LANDING GEAR WAS SELECTED DOWN, ALL THREE GEAR SHOWED SIMULTANEOUS RED AND GREEN INDICATIONS. CREW BROKE OFF APPROACH AND ACCOMPLISHED CHECKLIST PROCEDURES. GEAR WAS VISUALLY OBSERVED DOWN THROUGH VIEWPORTS AND BY TOWESDR USAASB99305Fire Loop · failedMCI - FLT 328 - AFTER TAKEOFF FROM MCI, THE RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. THREE MINUTES LATER, THE LEFT WING TO BODY OVERHEAT LIGHT ILLUMINATED AND A STRONG BURNING SMELL WAS PRESENT IN THE COCKPIT. FLIGHT RETURNED TO FIELD AT MCI AND LANDEDSDR USAASB99301Unknown · odorMCO - FLT 2152 - 20 MINUTES AFTER T/O FROM RSW, UNIDENTIFIED FUMES WERE RECOGNIZED IN THE AFT GALLEY. CREW TURNED OFF GALLEY POWER SWITCH AND PULLED ALL CIRCUIT BREAKERS IN THE GALLEY. NO SMOKE WAS PRESENT BUT FUMES BECAME STRONGER. CREW DECLARED EMERGENCY SDR AWXA9900487Light · inoperativeEMERGENCY EXIT LIGHT ASSY AT SEATS 12 AND 22 LT SIDE INOP. REPLACED LIGHT ASSY AT SEAT 12, REPAIRED BROKEN WIRE AT SEAT 22 AND OPS CHECKED GOOD. WIRE (P/N BMS 13-13-1/1-22)SDR USAASB99296Mec · faultyCLT - FLT 299 - ON CLIMB-OUT FROM CLT, AT FL210, THE NR 1 ENGINE N1 INDICATOR BEGAN FLUCTUATING IN ALL PARAMETERS OF FLIGHT. THE N1 WOULD SURGE PLUS OR MINUS 7 PERCENT EVERY 7 TO 10 SECONDS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENTSDR USAASB99293Engine · vibrationCLT - FLT 8052 - ON CLIMB-OUT FROM CLT, THE NR1 ENGINE VIBRATION MONITOR INDICATED 2 UNITS ACCELERATING THROUGH 210 KNOTS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCYWAS DECLARED. MAINTENACNE ACCOMPLISHED TROUBLESHOOTISDR DL733992709Slide · deployedWHILE REPOSITIONING A/C TO GATE FOR FIRST FLIGHT DEPARTURE, R1 SLIDE WAS INADVERTENTLY DEPLOYED DUE TO GIRT BAR APPARENTLY SHIFTED AND WHEN OPS ATTEMPTED TO BOARD A/C GIRT BAR GOT CAUGHT ON DOOR FRAME AND DEPLOYED WHEN DOOR WAS OPENED FULLY. MTC FERRY A/C TO SDR USAA991435Skin · crackedPIT - DURING RON VISIT, FOUND 1.0625 INCH LONG CRACK ON FUSELAGE SKIN AT RT SIDE, STATION 767 STRINGER 22 TO 23 RT. REMOVED CRACK WITH CUTOUT. INSTALLING EXTERNAL DOUBLER PER SRM 53-00-00-01, FIG 201, EA 53528. (M)SDR USAASB99290Cabin Pressure · failedPIT - FLT 2380 - DURING CLIMB-OUT FROM PIT, THE AUTO PRESSURIZATION SYSTEM FAILED TO STANDBY. CREW WAS UNABLE TO CONTROL CABIN IN STANDBY OR MANUAL MODE. CABIN CONTINUED TO CLIMB WITH OUTFLOW VALVE CLOSED. DECISION WAS MADE TO RETURN TO FIELD AT PIT. FLIGHSDR USAASB99289Handle · malfunctionedPIT - FLT 705 - DURING LOWERING OF LANDING GEAR, INBOUND TO PIT, CREW RECEIVED ALL 6 GEAR INDICATION LIGHTS (3 RED AND 3 GREEN). CREW RECYCLED GEAR AND INDICATION WAS NORMAL. FLIGHT LANDED AT PIT WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENSDR USAASB99283Door · openMCO - FLT 1232 - A/C FAILED TO PRESSURIZE IMMEDIATELY AFTER T/O FROM FLL. CAPT ASKED F/A TO CHECK THE DOORS AND FOUND THE AFT RIGHT SERVICE DOOR CLOSED WITH HANDLE DOWN BUT THE DOOR DID NOT APPEAR TO BE SEALING PROPERLY. NO DOOR WARNING LIGHTS WERE ILLUMINATSDR USAASB99279Controller · failedPHL - FLT 435 - EN ROUTE FROM BTV TO PHL, AT FL260, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW VERIFIED CABIN ALTITUDE READING AT 10,000 FT. CREW COMPLIED WITH ABNORMAL PROCEDURES AND ACCOMPLISHED A STEEP DESCENT TO FL120. NO OXYGEN MASKS WERE DEPLOYED. SDR USAASB99278Indicator · failedCLT - FLT 2202 - DURING CLIMB-OUT FROM CLT, THE FLAPS FAILED TO RETRACT AS FLAP INDICATOR FAILED AT 5 DEGREES FLAPS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FLAP POSDR USAASB99277Coalescer Bag · contaminatedLGA - FLT 6461 - EN ROUTE FROM BOS TO IAD, THE F/A REPORTED THAT COCKPIT CREW SMELLED BURNING ELECT ODOR IN CABIN. CAPT DECIDED TO DIVERT TO LGA. FLT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX ACCOMP GROUND ENG RUN WITH PACKS ISOLATED ASDR AWXA9900428Controller · malfunctionedIN AUTO PRESS, SYSTEM FAILED TO MAINTAIN CABIN PRESS, STANDBY AND MANUAL MODE FAILED, DUCT PRESS NML AT ALL PWR SETTINGS. INSPECTED DOOR SEALS AND PRESSURIZED CABIN WITH NO DEFECTS NOTED. REPLACED CABIN PRESS CONTROLLER AS PRECAUTION DUE TO PREVIOUS HISTORY SDR DL733992563Controller · malfunctionedPRESSURIZATION LOST AFTER T/O FROM COS. UNABLE TO REGAIN PRESSURATION ANY CONFIGURATION. CHECKED ALL DOORS, RAN ENGS AND PACKS ON GROUND. ACFT PRESSURIZATION NORMAL.SDR USAASB99275Garlock Seal · leakingDEN - FLT 624 - EN ROUTE FROM LAS TO PIT, AT APPROXIMATELY FL330, THE RIGHT ENGINE OIL QTY DROPPED TO .25 GALLON. OIL PRESSURE REMAINED NORMAL. FLIGHT DIVERTED TO DEN AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND NO ENGINE SHUTDOWN OCCUSDR USAA991218Antenna Base · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 12 INCH AREA OF CORROSION BETWEEN STRINGER 28 LT AND RT AFT OF STATION 500 ANTENNA BASE, CORROSION LEVEL 2. REPLACED ANTENNA BASE PER SRM 51-10-02. (M)SDR USAA991215Shear Tie · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 420 STRINGER 4 LEFT SHEAR TIE. REMOVED AND REPLACED PER SRM 51-10-2. (M)
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