Boeing 737-3B7
Service difficulty reports · 4,722
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 = '7373B7' 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 = '7373B7' 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 DL733000960Connector · looseFAULT LIGHT CAME ON IN FLIGHT INTERMITTENTLY. DIVERTED TO LAX. FOUND FIRE WALL CONNECTOR D406 LOOSE. CLEANED AND SECURED. RAN ENG, ALL CHECKS NORMAL.SDR USAASB00140Battery Pack · dischargedCLE - MAINTENANCE FOUND THE CENTER CABIN OVERHEAD EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)SDR USAASB00135Apu · overspeedCHA - FLT 657 - EN ROUTE FROM CLT TO DFW, AT FL350, THE APU OVERSPEED LIGHT ILLUMINATED FOLLOWED BY AN AUTO SHUTDOWN. APU WAS POWERING THE NR 1 GENERATOR BUS DUE TO A MEL ON THE NR 1 ENGINE CSD FOR LEAKING. JUST PRIOR TO OVERSPPED, CREW OBSERVED APU GENERATOSDR DL733000888Skin · crackedTHE UPPER AFT CORNER OF THE LOWER HINGE CUTOUT ON THE R1 DOOR WAS FOUND WITH A .25 INCH CRACK. THE CRACK IS TYPICAL OF BAC S/B 737-52-1096. THE CRACK WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER THE S/B AND PER ER/A 377233-14.SDR USAA000663Skin · crackedPIT - FOUND SKIN CRACKED 1.75 INCH, RIGHT SIDE STATION 727D TO STATION 727E AT STRINGER 24R. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01 FIG 201. (M)SDR USAASB00129Engine · surgesPHL - FLT 1545 - DURING CLIMB-OUT FROM PHL, AT FL160, THE NR 1 ENGINE BEGAN TO SURGE FROM 95 T0 97 PERCENT N1 AND WOULD RETREAT TO THE PRESET 87 PERCENT N1. CAPTAIN NOTED THAT THIS SURGE OCCURRED THREE TIMES WITH AN ACCOMPANYING YAW EACH TIME. DECISION WAS MSDR DL733000854Engine · overtempJUST AFTER ROTATION, NR 1 EGT 970 DEG WITH WARNING HORN FOR APPROX 10 SECONDS. REPLACED NR 1 ENG PER ROUTINE CARD DECK.SDR USAASB00127Adc · failedCLT - FLT 463 - CLIMB-OUT FROM CLT, AT FL 230, OFF FLAGS APPEARED ON CAPTAIN''S AIRSPEED INDICATOR AND ALTIMETER. CREW WAS UNABLE TO ENGAGE A-SYSTEM AUTOPILOT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. SDR USAA000595Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 4 INCHES, LOWER AFT CORNER OF FORWARD GALLEY DOOR CUTOUT. INSTALLED DOUBLER PER SRM 51-30-01. (M)SDR USAASB00119Tube · crackedBWI - FLT 988 - UPON LIFTOFF, JUST AFTER GEAR RETRACTION, CAPTAIN RECEIVED INDICATION OF SYSTEM A HYDRAULIC LOSS. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND SHUTDOWN BOTH SYSTEM A PUMPS WITHIN TWO MINUTES. FLIGHT DIVERTED TO BWI AND LANDED WITSDR USAA000578Panel · crackedPIT - FOUND PANEL CRACKED .375 INCH PAST EXISTING STOP DRILL, KEEL BEAM PANEL BETWEEN WHEEL WELLS. INSTALLED TEMP REPAIR DOUBLER INCORPORATING BOTH CRACKED AREAS PER SRM 53-60-12 FIG 202/EA 53683D. (M)SDR USAASB00115Controller · failedPBI-FLT 1681 - AFTER TAKEOFF FROM PBI, AIRCRAFT PRESSURIZATION APPEARED TO OPERATE NORMAL UNTIL ABOUT 5,500 FEET. THE AUTO FAIL LIGHT ILLUMINATED AND PRESSURIZATION SWITCHED TO STANDBY. AIRCRAFT DIFFERENTIAL CONTINUED TO CLIMB. SWITCHED OVER TO MANUAL AND HSDR USAASB00112Door · not closedPHL - FLT 725 - AFTER TAKEOFF FROM PHL, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT. OUTFLOW VALVE WAS FULL CLOSED WITH NORMAL DUCT PRESSURE. AFT FLIGHT ATTENDANT REPORTED A LOUD NOISE FROM THE AFT RIGHT SERVICE DOOR. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WSDR USAASB00110Indicator · failedBOS - FLT 663 - AFTER TAKEOFF FROM BOS, DURING FLAP RETRACTION, THE FLAP INDICATOR SHOWED A FLAP ASYMMETRY. CAPTAIN DECLARED AN EMERGENCY AND ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCIDENSDR USAASB00109Valve · failedCLT - FLT 1930 - EN ROUTE FROM PHL TO PBI, CREW NOTIFIED DISPATCH VIA ACARS THATY THEY WERE LOSING CABIN PRESSURE ALTITUDE AND UNABLE TO CONTROL THE PRESSURE LOSS. FLIGHT DESCENDED TO FL140 AND WAS MAINTAINING PRESSURE FOR AWHILE, BUT CABIN BEGAN LOSING PRESSSDR USAASB00101Clamp · looseCHS - FLT 1452 - ON CLIMB-OUT FROM RSW, AT FL270, CAPTAIN RECEIVED A RIGHT WING BODY OVERHEAT INDICATION. LIGHT EXTINGUISHED IMMEDIATELY AFTER BLEED SWITCH WAS TURNED OFF. CAPTAIN DESCENDED FLIGHT TO FL250, AND AT THIS POINT, THE ALTITUDE WARNING HORN SOUNDEDSDR USAASB00099Accessory Unit · failedPHL - FLT 1077 - EN ROUTE TO JAX, SUPPLY DUCT TEMPERATURE WENT TO 51 DEGREES CELSIUS AND CAIBN GOT VERY HOT. CABIN TEMPERATURE WAS UNCONTROLLABLE. A HOT SMELL WAS ALSO NOTED. FLIGHT DIVERTED TO PHL. ON DESCENT, CREW HAD TO SWITCH TO STANDBY PRESSURIZATION SDR USAASB00098Light · shortedIAH - FLT 2231 - ON CLIMB-OUT FROM IAH, AT APPROXIMATELY 9,000 FEET, CAPTAIN REPORTED THERE WAS A LOUD POP AND SPARKS THAT DROPPED DOWN ON THE FIRST OFFICER FROM THE OVERHEAD PANEL. AT 18,000 FEET, ALL APPEARED TO BE OPERATING NORMAL. NO SMOKE OR SMELL OF ANSDR USAASB00097Light · failedCLT - PILOT REPORTED THE EMERGENCY EXIT LIGHT IN SEAT ROW 10ABC IS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY IN SEAT ROW 10ABC. OPERATIONAL CHECK GOOD. (X)SDR USAASB00095Module · malfunctionedGSO - FLT 1409 - FLIGHT DEPARTED PIT WITH THE NR 2 GENERATOR ON MEL. EN ROUTE TO TPA, THE APU OVERSPEED LIGHT ILLUMINATED WITH APU AUTO SHUTDOWN. FLIGHT DIVERTED TO GOS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RESET AND RSDR USAASB00092Arm · failedCLT - FLT 682 - ON CLIMB-OUT FROM CLT, AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD ENTRY DOOR LEAKING. REMOVED AND REPLACED THE FORWARD ENTRY DSDR USAASB00085Battery Pack · dischargedALB - MAINTENANCE FOUND THE BULLNOSE EMERGENCY EVACUATION LIGHTS AT SEAT ROWS 3, 7 AND 9 INOPERATIVE AND THE LEFT CEILING EXIT SIGN AND RIGHT OVERWING EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB00082Seal · dislodgedPHL - FLT 1797 - AFTER TAKEOFF FROM PHL, CAPTAIN RECEIVED A DOOR WARNING INDICATION THAT THE AFT ENTRY DOOR WAS AJAR. WITH HANDLE IN LOCKED POSITION, FLIGHT ATTENDANT REPORTED THE LANYARD WAS STUCK IN THE DOOR. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHSDR USAASB00083Element · failedMCO - FLT 1640 - ON CLIMB-OUT FROM PBI, CAPTAIN RECEIVED A RIGHT WING BODY OVERHEAT INDICATION. AFTER CHECKING ALL THE SPECIAL PROCEDURES, CAPTAIN ELECTED TO DIVERT TO MCO. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOSDR USAA000451Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 2.125 INCHES, STRINGER 24L JUST FORWARD OF BS 727E. INSTALLED EXTERNAL DOUBLER PER EA 66901. (M)SDR USAASB00077Battery Pack · failedMIA - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMVOED AND REPLACED THE BATTERY PACK (P/N 2013-1ALP) AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAA000386Frame · corrodedCLT - FOUND FRAME CORRODED 2 INCHES, FRAME BETWEEN STRINGER 27L AND 27R BS 867. INSTALLED REPAIR DOUBLER PER SRM 53-00-07. (M)SDR USAA000371Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 2 INCHES BY 3 INCHES, LEFT SIDE Z-ANGLE PER SRM 53-10-02 AND 51-40-02. (M)SDR USAA000367Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, FORWARD SERVICE DOOR CUTOUT STRINGER 14R STATION 277. REMOVED DAMAGED PER SRM 51-10-2. (M)SDR USAA000368Angle · crackedCLT - FOUND ANGLE CRACKED 1.500 INCH, ON SUPPORT FITTING 695. INSTALLED FABRICATED ANGLE PER SRM 51-70-11. (M)SDR USAA000369Fitting · crackedCLT - FOUND FITTING CRACKED .5 INCH, RIGHT PACK INTAKE STATION 540. INSTALLED DOUBLER AND FILLER PER TR 53-50-03. (M)SDR USAA000370Angle · crackedCLT - FOUND ANGLE CRACKED 2 INCHES, LEFT HORIZ STAB CUTOUT S5A. INSTALLED REPAIR ANGLE PER SRM 53-00-01 FIG 221 AND EA 66811. (M)SDR USAASB00074Uplock Sensor · malfunctionedMIA - FLT 1830, AFTER TAKEOFF AND GEAR SELECTOR IN UP POSITION, THE LEFT MAIN LANDING GEAR RED LIGHT REMAINED ILLUMINATED. CREW RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. FLIGHT CONTINUED ONTO PHL WHERE IT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMSDR USAASB00072Arm · out of adjPHL - FLT 308 - ON CLIMB-OUT FROM PHL, AT APPROXIMATELY 10,000 FEET, A LOUD AIR RUSHING NOISE WAS HEARD FROM THE FORWARD ENTRY DOOR. AIRCRAFT WAS UNABLE TO PRESSURIZE. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECSDR USAA000363Skin · crackedPIT - FOUND SKIN AND SUPPORT CHANNEL CRACKED, 1 INCH, 1.875 INCH AND 15 INCH CRACK, FS 500 AND 500A VHF NR 2 ANTENNA. CUT OUT SKIN DAMAGE AND INSTALLED FILLER AND DOUBLER PER EA 54375-A. (M)SDR USAA000350Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .5 INCH, STATION 178, WL 200.01, LBL 4.50 BULKHEAD. INSTALLED DOUBLER AND FILLER PER TR 53-10A. (M)SDR USAA000351Stringer · corrodedCLT - FOUND STRINGER CORRODED 4 INCHES, STATION 1006, STRINGER 26R AFT LAV SERVICE PANEL. REPLACED STRINGER SECTION PER SRM 51-10-2. (M)SDR USAA000348Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, AFT CARGO FLOOR STRINGER, STATION 747, RBL 13. REPAIRED PER SRM 53-00-53 FIG 202. (M)SDR USAA000349Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .400 INCH, STATION 178, WL 197.50, LBL 4.50 BULKHEAD. INSTALLED DOUBLER AND FILLER PER TR 53-10-07A. INSTALLED DOUBLER AND FILLER PER TR 53-10-07A. (M)SDR USAA000347Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 2 INCHES, COOLING DUCT MOUNT AFT OF E/E BAY FUSELAGE SKIN. REPAIRED PER EA 66803 AND TR 53-30-04. (M)SDR USAA000312Stiffener · corrodedCLT - FOUND STIFFENER CORRODED 1 INCH BY 4 INCH, LOWER FRAME AFT STATION 1016 1 INCH RBL. INSTALLED REPAIR ANGLE AND FILLER PER SRM 51-70-11. (M)SDR USAA000313Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .75 INCH BY .75 INCH, STATION 967, LBL 44 INCH. INSTALLED UPPER CHORD PER TR 53-10-05 REV A. (M)SDR USAA000314Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH BY 1 INCH, STATION 344, LBL 42. REPLACED T-CAP PER SRM 53-10-51. (M)SDR USAA000315Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, STATION 847 BETWEEN STRINGER 8R AND STRINGER 9R. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66768. (M)SDR USAA000316Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, STATION 827 BETWEEN STRINGER 8L AND STRINGER 9L. INSTALLED FILLER AND DOUBLER PER TR 53-10-14 AND EA 66768. (M)SDR USAA000317Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, STATION 807 BETWEEN STRINGER 8L AND STRINGER 9L. INSTALLED DOUBLER AND FILLER PER TR 53-10-14. (M)SDR USAA000318Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, STATION 787 BETWEEN STRINGER 8L AND STRINGER 9L. INSTALLED FILLER AND DOUBLER PER TR 53-10-14 AND EA 66768. (M)SDR USAA000319Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, STATION 867 BETWEEN STRINGER 8L AND STRINGER 9L. INSTALLED FILLER AND DOUBLER PER TR 53-10-14. (M)SDR USAA000320Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, STATION 480 BETWEEN STRINGER 8L AND STRINGER 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA000321Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, STATION 480 STRINGER 8R AND STRINGER 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)
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