Boeing 737-401
Service difficulty reports · 2,961
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 = '737401' 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 = '737401' 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 USAA030164Fitting · corrodedFOUND FITTING CORRODED .125 INCH AREA, 2 INCHES AROUND FITTING, BOTH SIDES, BS 685 LT MLG SIDE STRUT FITTING. REMOVED BUSHINGS, MACHINED FACES AND BORE OF LUG AND INSTALLED NEW BUSHINGS PER EA 76728. (M)SDR USAA030159Attach Angle · crackedFOUND ATTACH ANGLE CRACKED .5 INCH, BS 328 LBBL 45 CABIN FLOOR. MANUFACTURED NEW ANGLE AND INSTALLED PER DWG NR BAC-65-45812 AND SRM 51-10-02. (M)SDR USAA030158Intercostal · crackedFOUND INTERCOSTAL CRACKED 1 INCH, BS 328 LBBL 45 CABIN FLOOR. REPLACED INTERCOSTAL PER SRM 51-10-02. (M)SDR USAA030146Skin · crackedPIT - FOUND SKIN CRACKED 1 INCH, NACELLE STRUT SKIN CRACK AROUND PANEL 57271, LEFT PYLON. DOUBLER INSTALLED PER TR 54-30-07 AND EA 56543B. (M)SDR USAA030149Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, FS 500C BELOW S26L. FABRICATED REPAIR PARTS PER EA 94532. (M)SDR USAA030110Skin · crackedINTERIOR DOOR SKIN CRACKED .5 INCH LONG, 3RD DOOR STOP ADJUSTMENT SCREW FROM BOTTOM AT AFT SIDE MED. FABRICATED REPAIR DOUBLER AND INSTALLED PER EA 76156, SRM 51-40-03, 52-10-01, 51-70-13. (M)SDR USAA030165Angle · corrodedFOUND ZEE ANGLE CORRODED 2 INCHES BY 3 INCHES, AFT ENTRY DOOR ZEE ANGLE, STATION 907 TO 1006. REPLACED ZEE ANGLE PER SRM 51-10-02 AND BOEING REPAIR DWG NR 65-52878. CORROSION LEVEL 1, TASK NR C53-67-01. (M)SDR USAA030098Skin · crackedPIT - FOUND ENTRY DOOR CUTOUT CRACKED .25 INCH, STATION 947, STRINGER 11L, LEFT AFT ENTRY DOOR CUTOUT. INSTALLED DOUBLER PER SRM 53-60-01. (M)SDR USAA030102Floorbeam · corrodedFOUND FLOORBEAM CORRODED .5 INCH BY 1 INCH AREA, FLOORBEAM STATION 947 LBL 24.75 TO RBL 24.75. REPAIR FLANGE PER TYPICAL REPAIR 53-60-02 REV A, PART B. (M)SDR USAA030144Channel · corrodedPIT - FOUND CHANNEL CORRODED 4 INCHES BY 6 INCHES, AFT CARGO Z-CHANNEL STATION 727D TO 867 JUST ABOVE STRINGER 24L. NEW CHANNEL SPLICED IN PER TYPICAL REPAIR 53-40-01 AND SRM 51-70-11, SRM 53-60-53. (M)SDR USAASB03088Battery Pack · inoperativeMAINTENANCE REPORTED THE EMERGENCY LIGHTS AT THE LAST TWO SEAT ROWS, THE AFT RT SERVICE DOOR AND THE RIGHT EMERGENCY EXIT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 6 BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB03076Servo · malfunctionedON CLIMB-OUT FROM CLT, EN ROUTE TO BOS, CAPTAIN LOST HIS AUTO PILOT AND VOR. HE SWITCHED TO THE FIRST OFFICERS AUTO PILOT AND LOST THAT AS WELL. AT THE SAME TIME, SEVERAL INSTRUMETNS WERE GIVING ERRONEOUS DATA ALONG WITH THE MACH TRIM FAIL LIGHT AND SPEED TRSDR USAA030097Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCH, RIGHT HORIZONTAL STAB LOWER SKIN APPROX STATION 115. DAMAGE CUTOUT AND EXTERNAL SKIN DOUBLER INSTALLED PER SRM 55-10-01 FIG 204. (M)SDR USAASB03073Seal · leakingMCO - FLT 553 - EN ROUTE FROM RSW TO CLT, CAPTAIN REPORTED THE ALTITUDE WARNING HORN BEGAN SOUNDING AND THAT THE CABIN PRESSURE WAS CLIMBING. CREW WAS UNABLE TO CONTROL CABIN PRESSURE AT ALTITUDE. FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. SDR USAA030103Seat Track · corrodedFOUND SEAT TRACK CORRODED .5 INCH BY 1 INCH OF CORROSION, RIGHT INBOARD SEAT TRACK STATION 907. CORROSION LEVEL 1. REMOVED CORROSION, BLEND OUT, PER SRM 51-10-02. (M)SDR USAA030085Sill · corrodedFOUND SILL ASSEMBLY CORRODED 1.5 INCH AREA, AFT ENTRY DOOR LOWER SILL ASSEMBLY FROM STATON 907 PLUS 6 INCHES, STATION 1006. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. (M)SDR USAASB03071Sensor · malfunctionedAFTER TAKEOFF FROM CLT, CREW WAS UNABLE TO RETRACT THE LANDING GEAR AS GEAR LEVER WOULD NOT MOVE TO THE UP POSITION. QUICK REFERENCE HANDBOOK PROCEDURES WERE FOLLOWED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLSDR USAA030071Stringer Clip · crackedFOUND CLIP CRACKED 1 INCH, STRINGER CLIP 11R STATION 360. INSTALLED FABRICATED CLIP PER SRM 51-40-02. (M)SDR USAA030058Splice · crackedPIT - FOUND STRINGER SPLICE WITH TWO CRACKS .25 IN LENGTH, BS 907 STRINGER 4 LEFT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-30-01. (M)SDR USAA030088Skin · crackedCLT - FOUND CRACK IN SKIN 3.5 INCHES, STATION L 495, L STRINGER 17, SKIN. INSTALLED DOUBLER AND TRIPLER PER EA 87256. (M)SDR USAA030084Bearing · failedFOUND FAILURE IN TERMINAL OF ROLLER BEARING, AFT CARGO DOOR AND DEEP GOUGES IN LATCHING FITTING AND COVER PLATE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)SDR USAA030072Stringer Clip · crackedPIT - FOUND CLIP CRACKED 1 INCH, STATION 360 STRIGNER 11R. INSTALLED FABRICATED CLIP PER SRM 51-40-02. (M)SDR USAA030070Angle · crackedPIT - FOUND ANGLE CRACKED .5 INCH, UPPER SIDE OF 13R STATION 291.5. DEFECTIVE PART REPLACED WITH IDENTICAL PART N/R. (M)SDR USAA030069Angle · crackedPIT - FOUND ANGLE WITH .5 INCH CRACK, UPPER SIDE S9R AT STATION 291.5. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)SDR USAA030067Striker · crackedPIT - FOUND SEAL DEPRESSOR CRACKED 2 INCHES, UPPER FORWARD CORNER FORWARD SERVICE DOOR SEAL DEPRESSOR. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)SDR USAA030068Angle · crackedPIT - FOUND ANGLE CRACKED .5 INCH, ABOVE STRINGER 11R STATION 291.5. DEFECTIVE PART REPLACED WTH IDENTICAL PART NR. (M)SDR USAA030051Intercostal · crackedPIT - FOUND WEB INTERCOSTAL CRACKED .5 INCH, FS 277-294.5 AT S-14R. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-02. (M)SDR USAA030049Clip · crackedPIT - FOUND STRINGER ATTACH CLIP CRACKED .25 INCH, STATION 578, S4R. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-00-03. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-00-03. (M)SDR USAASB03062Circuit Breaker · trippedCLT - FLT 859 - ON APPROACH INTO CLT, THE FLAP INDICATION DID NOT GO BEYOND 10 DEGREES. CREW COMMENCED WITH A MISSED APPROACH AND DECLARED AN EMERGENCY. ALTERNATE FLAP EXTENSION PROCEDURE WAS INITIATED AND A NORMAL FLAP LANDING WAS MADE WITH FLAP INDICATION SDR USAA030047Flange · brokenFOUND HINGE COVER ATTACH FLANGE BROKEN OFF, LOWER RIGHT SIDE OF RUDDER 23 INCHES FROM BOTTOM. MANUFACTURED REPAIR STRAP AND FILLERS PER EA 76261. (M)SDR USAA030045Stringer · crackedPIT - FOUND STRINGER CRACKED .5 INCH, HAT CHANNEL STRINGER AT STATION 380 S2R. COMPLETED REPAIR SPLICES, SECTION AND SHEAR CLIP PER SRM 53-00-03. (M)SDR USAA030044Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, FS 480 S8R S9R. COMPLETED REPAIRS FOR TYPICAL REPAIR 53-10-20A. (M)SDR USAA030073Support · crackedPIT - FOUND ANGLE SUPPORT CRACKED .5 INCH, AT UPPER SIDE OF STRINGER 13R AT STATION 291.5. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)SDR USAASB03055Warning Light · malfunctionedON GEAR EXTENSION INTO PHL, CREW RECEIVED A RED NOSE GEAR UNSAFE LIGHT WITH NO GREEN GEAR INDICATION LIGHTS. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND FOUND A CIRCUIT BREAKER FOR THE AIR GROUND SENSOR HAD TO BE RESET. CREW RESET CIRCUIT BREAKSDR USAASB03050Charger · inoperativeMAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT SEAT ROW 11DEF INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AT STATION 634L. OPERATIONAL CHECK GOOD. (M)SDR USAASB03047Battery Pack · inoperativeTPA - MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK, AT THE FORWARD RIGHT CABIN, WILL NOT HOLD A CHARGE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB03046Charger · inoperativePIT - DUIRNG OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 12 THROUGH 19, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1136 BATTERY CHARGER ASSEMBLY AND THE BATTEYR PACK, P/N 20SDR USAA030031Spar · crackedPIT - FOUND UPPER REAR SPAR CRACKED 1 INCH IN LENGTH TWO EACH, RIGHT WING UPPER REAR SPAR AT RSS 224.14. ACCOMPLISHED OVERSIZE OF HOLES AND INSTALLATION OF REPAIR DOUBLER PER EA 75898. (M)SDR USAASB03041Gcu · failedCLT - FLT 799 - SHORTLY AFTER TAKEOFF FROM ORD, EN ROUTE TO CLT, THE NR 1 GENERATOR BUS OFF LIGHT ILLUMINATED. CREW PLACED THE NR 1 GENERATOR BACK ON LINE, WHERE IT STAYED FOR A COUPLE OF MINUTES, BEFORE DROPPING OFF LINE AGAIN. FREQUENCY AND VOLTS WERE NORMSDR USAASB03023Module · failedCLT - FLT 1132 - ON DESCENT INTO CLT, PASSING THROUGH FL190 AT 310 KNOTS, THE AMBER LEADING EDGE TRANSIT LIGHT ILLUMINATED. CREW SLOWED AIRCRAFT DOWN TO 230 KNOTS AND FELT AN AIRCRAFT VIBRATION WITH A SLIGHT RIGHT HAND ROLL TENDENCY. A FLAPS 15 LANDING WAS ASDR USAA030014Skin · crackedCLT - FOUND SKIN CRACKED 2.2 INCH, BELOW S23R AT STATION 727D. INSTALLED DOUBLER PER T/R 53-60-03. (M)SDR USAASB03016Warning Light · illuminatedALB - FLT 1057 - ON APPROACH INTO ALB, FROM CLT, CREW RECEIVED A TWO DEGREE FLAP ASYMMETRY INDICATION. CREW DECLARED AN EMERGENCY AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ON TAXI TO THE GATE, THE FLAP PROBLEM CORRECTED ITSELF. MAINTENANCE OPERATED FLSDR USAASB02015ABattery Pack · dischargedPIT - MAINTENANCE REPORTED THE FORWARD GALLEY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAA030011Stiffener · crackedPIT - FOUND STIFFENER CRACKED .5 INCH, RT STIFFENER RBBL 6.15 STATION 663.75 WL 170.4. INSTALLED REPAIR ANGLES PER EA 75661 AND EA 75658. (M)SDR USAA020010AStiffener · crackedPIT - FOUND STIFFENER CRACKED .5 INCH, LEFT STRINGER LBBL 6.15 STATION 663.75 WL 170.4. INSTALLED REPAIR ANGLES PER EA 75658. (M)SDR USAA030009Skin · crackedPIT - FOUND DURING MAINTENANCE, LOWER SKIN CRACKED 1.5 INCH, RIGHT HORIZ STAB LOWER SKIN AFT OF SPAR CHORD STATION 125. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TR 55-10-07. (M)SDR USAA020001ASkin · crackedPIT - FOUND SKIN CRACKED 2 INCHES, STATION 727D AT OVERWING EXIT LIGHT RIGHT SIDE. INSTALLED REPAIR DOUBLER PER TR 53-60-03. (M)SDR USAASB04005Pump · overheatedCLT - FLT 1456 - EN ROUTE FROM DCA TO FLL, THE B-SYSTEM ELECTRIC HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE B-SYSTEM ELECTRIC HYDRAULSDR USAASB02222Battery Pack · dischargedPHL - MAINTENANCE FOUND THE AFT EMERGENCY LIGHTS INOPERATIVE/WON'T TEST. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT AND RIGHT EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. (M)SDR USAASB02216Sensor · failedUPON NORMAL DESCENT, CREW REPORTED A THUMPING NOISE COMING FROM THE NR 1 ENGINE, SOUNDING LIKE COMPRESSOR STALLS. COMPRESSOR STALLS BECAME PROGRESSIVELY WORSE AS RPM BECAME LOWER ON THE ENGINE. FLIGHT LANDED WITHOUT INCIDENT. THE ENGINE WAS NOT SHUT DOWN AN
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