Boeing 737-4B7
Service difficulty reports · 5,757
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 = '7374B7' 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 = '7374B7' 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 USAA001130Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 727B RIGHT SIDE FUSELAGE BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA001129Frame · crackedCLT - FOUND FRAME CRACKED .75 INCH, LOWER END OF 601 LT FRAME INNER CHORD ANGLE. INSTALLED DOUBLER PER TR 53-62-01 AND EA 67675. (M)SDR USAA001128Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 480 LT SIDE FUSELAGE BETWEEN 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA001127Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 440 LT SIDE FUSELAGE BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA001126Stiffener · crackedFOUND VERTICAL STIFFENER WITH A .375 INCH CRACK, STAB STATION 101.90 BETWEEN RIVETS. REPLACED STIFFENER AND INSTALLED PER SRM 51-10-02 AND 55-10-01. (M)SDR USAA001101Angle · crackedCLT - FOUND Z-ANGLE CRACKED 1 INCH BY 1 INCH, STATION 995.5 LBL 41. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. (M)SDR USAA001100Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 747 RT SIDE FUSE BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA001099Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 747 LT SIDE FUSELAGE BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA001098Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 867 RT SIDE FUSELAGE, BETWEEN STRINGER 8R AND 9R. DRILLED OUT AND INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA001097Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 867 LT SIDE FUSELAGE BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA001096Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 727D RT SIDE FUSELAGE BETWEEN STRINGER 8R AND 9R. DRILLED OUT AND INSTALLED PER TR 53-10-14A. (M)SDR USAA001095Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 727D LT SIDE FUSELAGE BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA001094Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .375 INCH, TIE CLIP AT RT FUSELAGE STATION 907 STRINGER 8R. FABRICATED TIE CILP PER DWG 69-35352-15. (M)SDR USAA001093Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FRAME STATION 907 RT SIDE FUSELAGE, BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA001092Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FRAME STATION 400 LT SIDE FUSELAGE, BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA001091Skin · crackedCLT - FOUND PYLON SKIN CRACKED 1 INCH, LOWER AFT CORNER OF 5724L. INSTALLED DOUBLER PER TR 54-50-07. (M)SDR USAASB00200Adc · failedCLT - FLT 1929 - EN ROUTE PIT/SJU, CAPTAIN'S AIRSPEED INDICATOR, ALTIMETER, A-SYSTEM AUTOPILOT, GPWS AND VHF COMMUNICATION HAD FAILED OR WERE WORKING INTERMITTENTLY. CREW OBSERVED NO CIRCUIT BREAKERS WERE TRIPPED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FUSDR USAASB00196Light · failedDCA - PILOT REPORTED THE EMERGENCY EXIT LIGHTS ON SEAT 11C INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. (X)SDR USAA001031Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 827 RIGHT SIDE BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER ANGLE PER TR 53-10-14A. (M)SDR USAA001030Angle · crackedCLT - FOUND VERTICAL ANGLE CRACKED .5 INCH, STATION 294, WL 208, RBL 54. INSTALLED DOUBLER PER 51-70-11. (M)SDR USAA001011Frame · crackedCLT - FOUND FRAME SUPPORT CRACKED .25 INCH, STATION 380 FRAME LT SIDE BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER SRM 53-10-14. (M)SDR USAA001014Angle · corrodedCLT - FOUND Z-ANGLE CHORD CORRODED 3 INCHES BY 24 INCHES, AFT ENTRY DOOR SILL. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. (M)SDR USAA001023Floorbeam · corrodedCLT - FOUND T-CAP FLOORBEAM CORRODED 120 INCHES BY 2 INCHES, STATION 986.5 FULL LENGTH OF FLOORBEAM. CORROSION LEVEL 1. FABRICATED NEW T-CAP PER TR 53-60-01. (M)SDR USAA001029Frame · crackedCLT - FOUND FRAME CRACKED 1.5 INCHES, LOWER END OF FRAME 616 RT INNER CHORD ANGLE. MADE NEW FILLER AND ANGLE PER TR 53-62-01. (M)SDR USAA001028Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, FS 380 RIGHT SIDE FUSELAGE BETWEEN STRINGER 8R AND 9R. INSTALLED HI-LOCK PER SRM 51-10-02. (M)SDR USAA001027Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 1 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 201. FABRICATED DOUBLER AND FILLERS AND INSTALLED PER SRM 53-10-08. (M)SDR USAA001026Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 1 INCH, STATION 178 BULKHEAD WEB RBL 4.75, WL 201. FABRICATED DOUBLER AND FILLER AND INSTALLED PER SRM 53-10-08. (M)SDR USAA001025Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 1 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 198. FABRICATED DOUBLER AND FILLER AND INSTALLED PER SRM 53-10-08. (M)SDR USAA001024Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 1 INCH, STATION 178, BULKHEAD WEB, RBL 4.75, WL 198. FABRICATED DOUBLER AND FILLER AND INSTALLED PER SRM 53-10-08. (M)SDR USAA001013Frame · crackedCLT - FOUND FRAME SUPPORT CRACKED .25 INCH, STATION 500A FRAME LT SIDE BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER SRM 53-10-14. (M)SDR USAA001012Frame · crackedCLT - FOUND FRAME SUPPORT CRACKED .5 INCH, STATION 440 FRAME RT SIDE BETWEEN STRINGER 8R AND 9R. REPAIRED DOUBLER PER SRM 53-10-14 AND 53-10-02. (M)SDR USAASB00191Door Seal · blownTPA - FLT 1080 - CLIMBING THROUGH FL190 OUT OF TPA, THE CABIN ALTITUDE WARNING HORN SOUNDED AS AIRCRAFT FAILED TO PRESSURIZE IN AUTO OR STANDBY MODE. OUTFLOW VALVE INDICATED CLOSED. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITHOUT FURTHER INCIDENT. NO EMESDR USAASB00167Control Panel · failedLGA - FLT 2382 - EN ROUTE FROM BUF-LGA, AT FL270, THE AUTO PRESSURIZATION SYSTEM FAILED. THE AURAL WARNING HORN SOUNDED AS THE CABIN ALTITUDE CLIMBED ABOVE 10,000 FEET. CREW DECLARED AN EMERGENCY AND DESCENDED TO 8,000 FEET. FLIGHT CONTINUED ONTO LGA AND LANSDR USAASB00165Sensor · failedMCO - FLT 2019 - FLIGHT DEPARTED MCO WITH THE LEFT PACK ON MEL. DURING CLIMB-OUT, THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO FIELD AT MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT SDR USAASB00164Light · faultyGSO - MAINTENANCE FOUND THE AFT LEFT ENTRY DOOR EMERGENCY EGRESS LIGHT ASSEMBLY INOPERATIVE. MAINTENANCE ACCOMPLISHED TEMPORARY REPAIR TO LIGHT FIXTURE AND PROGRAMMED FOR REPLACEMENT AT THE NEXT HEAVY MAINTENANCE CHECK. OPS CHECK GOOD. (M)SDR USAA000781Skin · crackedTPA - FOUND CARGO DOOR SKIN CRACKED .25 INCH, UPPER AFT CORNER FORWARD CARGO DOOR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER PER TR 52-30-03 AND SRM 52-00-03. (M)SDR USAASB00151Valve · failedSJU - FLT 2296 - FLIGHT DEPARTED SJU WITH THE RIGHT PACK ON MEL. AFTER TAKEOFF, THE LEFT ENGINE BLEED TRIPPED OFF. CREW SWITCHED TO APU AND THEN BACK TO LEFT ENGINE BLEED BUT THE BLEED TRIPPED OFF AGAIN. CAPTAIN ELECTED TO RETURN TO FIELD AT SJU. FLIGHT LASDR USAA000738Skin · crackedCLT - FOUND SKIN CRACKED, STATION 727D AT STRINGER 23R. INSTALLED DOUBLER PER SRM 53-60-03. (M)SDR USAASB00149Light · inoperativeTPA - FOUND EMERGENCY LIGHT AT 9C INOPERATIVE. MAINTENANCE REPLACED THE ASSEMBLY. (M)SDR USAA000712Skin · crackedCLT - FOUND SKIN CRACKED .250 INCH, EXT SKIN AFT ENTRANCE DOOR LOWER HINGE UPPER CUTOUT. INSTALLED DOUBLER PER SRM 52-00-01. (M)SDR USAA000701Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 440, STRINGER 8L. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA000699Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 787, STRINGER 8L. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA000698Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 440, STRINGER 8R. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA000697Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 296, STRINGER 17R FORWARD SERVICE DOOR CUTOUT. INSTALLED DOUBLER AND FILLER ANGLE PER SRM 51-70-11. (M)SDR USAA000696Frame · crackedCLT - FOUND FRAME CRACKED 2 INCHES, BS 601 RT, WL 202. INSTALLED STIFFENER AND FILLER PER EA 67119. (M)SDR USAA000703Floor Support · corrodedCLT - FOUND FLOOR SUPPORT BEAM CORRODED 1 INCH BY 2 INCH, 9 INCHES INBOARD OF AFT ENTRY DOOR STATION 986.5. INSTALLED NEW T-CAP PER TR 53-60-01. CORROSION LEVEL 2. (M)SDR USAA000700Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 747, STRINGER 8L. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)SDR USAA000695Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 70 INCHES, FS 328 BETWEEN RBL 56 AND RBL 14. INSTALLED NEW T-CAP PER SRM 53-10-51. CORROSION LEVEL 2. (M)SDR USAA000668Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, OUTBOARD EDGE OF PANEL 5727L CUTOUT. INSTALLED DOUBLER PER TR 54-30-07. (M)SDR USAA000655Floor Support · corrodedCLT - FOUND FLOOR SUPPORT CORRODED, RIGHT AFT DOOR Z-ANGLE. LEVEL 1 CORROSION. INSTALLED DOUBLER PER SRM 51-70-11. (M)
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