Boeing 737-291
Service difficulty reports · 408
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 = '737291' 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 = '737291' 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 2001UALA00394Skin · damagedRT FUSELAGE HAS EXISTING INTERIM REPAIR FROM BS 178 TO BS 191 AND FROM WL 190 TO WL 199. ACCOMPLISHED FINAL REPAIR. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00380Generator · failedNR 2 GENERATOR DROPPED OFF LINE. DRAINED THE CSD OIL TO PROPER LEVEL, AND CHECKED THE MAGNETIC OIL PLUG / FOUND CLEAN OF DEBRIS. FUNCTIONAL TEST ACCOMPLISHED. AIRCARFT RETURNED TO SERVICE.SDR 2001UALA00369Keelbeam · damagedDAMAGED AREAS AT KEEL BEAM STA 680 AND STA 708. REPLACES FASTENERS AT DAMAGED AREAS. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00321Floor Support · corrodedFLOOR SUPPORT HAS CORROSION AROUND FASTENER HOLES AT RBL 20 AND BETWEEN STA 967 AND STA 986. REMOVED CORRODED FLOOR SUPPORT. FABRICATED, ALODINED, PRIMED, AND INSTALLED NEW FLOOR SUPPORT. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00231Collar · out of adjLEFT GEAR UNSAFE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE FOUND UPLOCK BELL CRANK RETAINING COLLAR OUT OF ALIGNMENT AND CONTACTING MANUAL RELEASE LEVER. RE-ALIGNED AND SECURED COLLAR. OPERATIONAL CHECK AND MANUAL EXTENSION OF LANDING GEAR CHECKED NORMAL.SDR 2001UALA00229Collar · out of adjLEFT GEAR UNSAFE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE FOUND UPLOCK BELLCRANK RETAINING COLLAR OUT OF ALIGNMENT AND CONTACTING MANUAL RELEASE LEVER. RE-ALIGNED AND SECURED COLLAR. OPERATIONAL CHECK AND MANUAL EXTENSION OF LANDING GEAR CHECKED NORMAL.SDR 2001UALA00158Skin · crackedSEVERAL FATIGUE CRACKS WERE FOUND IN THE FUSELAGE SKIN JUST AFT OF THE FORWARD GALLEY DOOR AND FORWARD OF THE STA 360 PRODUCTION JOINT. *S/U* FASTENER HOLE CRACKED AT STR 15R WAS REPAIRED PER SRM 53-30-3, FIGURE 43. FASTENER HOLES CRACKED AT STR 16R WERE RESDR 2001UALA00131Check Valve · restrictedRETURNED TO FIELD DUE TO LOSS OF THE B-SYSTEM HYDRAULICS. *S/D* FOUND B-SYSTEM RESERVOIR CHECK VALVE FAILED AND RESTRICTING FLOW. REPLACED BOTH RESERVOIR CHECK VALVES. SERVICED HYDRAULICS TO FULL AND LEAKED CHECKED GOOD.SDR 2001UALA00082Smoke · detectedSMOKE IN THE COCKPIT. *S/D* THREE WIRE SOCKETS IN CONNECTOR D96 BROKE OFF AND SHORTED TOGETHER. REPLACED THE SOCKETS.SDR 2001UALA00018Engine · malfunctionedUNCOMMANDED POWER LOSS IN ENGINE NR 2. *S/D* REPLACED THE NR 2 ENGINE.SDR 2001UALA00004Gyro · failedPROBLEM WITH THE CAPTAINS HORIZONTAL SITUATION INDICATOR. *S/D* REPLACED THE NR 1 DIRECTIONAL GYRO. OPS CHECKED NORMAL.SDR 2000UALA00806Bullet · separatedENGINE COMPRESSOR STALL ON TAKEOFF. *S/D* THE STALL WAS CAUSED BY THE NR 2 ENGINE NOSE DOME BEING LIBERATED FROM THE FRONT ACCESSORY SUPPORT. THE ACCESSORY SUPPORT AND NOSE DOME WERE REPLACED.SDR 2000UALA00803Battery Pack · inoperativeEXTERIOR LIGHTS FOR FORWARD LEFT AND RIGHT ESCAPE SLIDES INOPERATIVE DURING EMERGENCY LIGHTS TEST. SUPPLEMENTAL DATA UPDATE REPLACED BATTERY PACK.SDR 2000UALA00680Coalescer Bag · contaminatedSMOKE SMELL IN THE PASSENGER CABIN. SUPPLEMENTAL DATA UPDATE NO FAULT FOUND. REPLACED COALESCER BAG AS PRECAUTION.SDR 2000UALA00657Buss Tie · shortedBURNING SMELL NOTICED THROUGHOUT THE CABIN. *S/D* REPAIRED, RE-TERMINATED B-PHASE WIRING, AND REPLACED C805 NR 2 BUS TIE BREAKER. ALL SYSTEMS CHECKED GOOD.SDR 2000UALA00752Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-11.SDR 2000UALA00634Compressor · stalledCOMPRESSOR STALL ON NR 1 ENGINE AT CLIMBOUT. *S/D* BORESCOPED 6TH AND 7TH STAGES. NO LIMITING CONDITIONS FOUND.SDR 2000UALA00631Battery · dischargedELECTRICAL SMELL IN CABIN. *S/D* FOUND EMERGENCY LIGHT BATTERY AND CHARGER M1050 BURNT. REPLACED CHARGER AND BATTERY. SYSTEM CHECKS NORMAL. ELECTRICAL SMELL GONE.SDR 2000UALA00616Indicator · malfunctionedAFTER TAKEOFF A-SYSTEM PRESSURE DROPPED TO 800 PSI AND QUANTITY TO 2.8 GAL. NO A-PUMP LOW PRESSURE LIGHTS OR FLIGHT CONTROL LIGHTS. ON APPROACH WHEN FLAPS EXTENDED TO 5, PRESSURE RETURNED TO 3000. *S/D* REPLACED A-SYSTEM PRESSURE TRANSMITTER, A-SYSTEM PRESSDR 2000UALA00570Engine · failedA PASSENGER REPORTED A TORCH COMING FROM THE NR 2 ENGINE DURING DESCENT. *S/D* THE NR 2 ENGINE WAS REPLACED.SDR 2000UALA00559Regulator · failedNR 1 ENGINE LOW OIL PRESSURE INDICATION. *S/D* REPLACED OIL PRESSURE REGULATOR, OPERATIONAL CHECKS GOOD.SDR 2000UALA00475Bottle · dischargedEVACUATION SLIDE BOTTLE PRESSURE INDICATES ZERO. *S/D* SLIDE 2L WAS REPLACED, DISCREPANCY WAS FOUND TO BE A BURST DISC ON THE SLIDE BOTTLE PRESSURE REGULATOR.SDR 2000UALA00508Compressor · stalledNR 2 ENGINE COMPRESSOR STALL. *S/D* NR 2 ENGINE WAS REPLACED.SDR 2000UALA00507Computer · failedELEVATOR FEEL LIGHT INDICATION. *S/D* REPLACED ELEVATOR FEEL COMPUTER AND 2 FILTERS. TESTED ELEVATOR FEEL SYSTEM, SYSTEM FUNCTIONS NORMALLY.SDR 2000UALA00490Connector · damagedAPU FIRE WARNING IN FLIGHT. *S/D* REPLACED APU FIRE DETECTOR PLUG (CONNECTOR) D984, APU FIRE DETECTION TEST NORMAL. REPLACED APU FIRE BOTTLE.SDR 2000UALA00488Light · inoperativeSERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. FOUND EMERGENCY LIGHT ASSEMBLY DETACHED. RE-INSTALLED EMERGENCY LIGHT.SDR 2000UALA00422Actuator · bypassingNR 5 SLAT NOT RETRACTING TO FULL UP. *S/D* FOUND NR 5 SLAT ACTUATOR BYPASSING. REPLACED THE NUMBER 5 SLAT ACTUATOR.SDR 2000UALA00408Fire Loop · damagedNR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. *S/D* FOUND LOWER LOOP M337 (LOOP A) SHORTED. REPLACED LOWER LOOP AND SYSTEM TESTED NORMAL. REPLACED ENGINE FIRE BOTTLES PER MM 26-21-01.SDR 2000UALA00391Battery Pack · inoperativeRIGHT HAND EMERGENCY EXIT LIGHTS INOPERATIVE AT FORWARD AND AFT OF EMERGENCY EXIT. *S/D* REPLACED THE BATTERY PACK.SDR 2000UALA00755Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-11.SDR 2000UALA00375Fire Loop · damagedOVERHEAT WARNING LIGHT ON. *S/D* REPLACED LOWER OVERHEAT SENSING LOOP ON NR 1 ENGINE PER MM 26-11-04. SYSTEM WAS TESTED NORMAL PER MM 26-12-02.SDR 2000UALA00305Generator · failedCREW REPORTS, NR 1 GENERATOR FAILED IN CRUISE WITH ZERO VOLTS AND ZERO FREQUENCIES. *S/D* THE NR 1 ENGINE GENERATOR WAS REPLACED AS WELL AS THE NR 1 CONSTANT SPEED DRIVE TRANSMISSION AS PRECAUTIONARY.SDR 2000UALA00228Panel · failedUNABLE TO CONTROL CABIN PRESSURATION IN AUTO OR STANDBY. *S/D* A FAILURE OF THE CABIN PRESSURE SELECTOR PANEL. REPLACED CABIN PRESSURE SELECTOR.SDR 2000UALA00226Rod End · brokenRIGHT MAIN LANDING GEAR WOULD NOT EXTEND HYDRAULICALLY. MANUAL EXTENSION WAS SUCCESSFUL. *S/D* DURING MAINTENANCE EVALUATION OF RT MLG ASSSEMBLY DUE TO USE OF MANUAL EXTENSION TO LOWER GEAR, FOUND RT MLG UPLOCK ACTUATOR ROD END BROKEN.SDR 2000UALA00227Fire Detector · failedCREW REPORTS APU FIRE WARNING SOUNDED AFTER TAKEOFF. *S/D* FOUND APU FIRE DETECTOR M717 BAD.SDR 2000UALA00754Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-11.SDR 2000UALA00282Sensor · out of adjAFT CARGO LIGHT INDICATION. *S/D* ADJUSTED DOOR SENSOR TARGET. DOOR INDICATION SYSTEM HAS PERFORMED NORMAL SINCE THE ADJUSTMENT.SDR 2000UALA00753Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-11.SDR 2000UALA00188Blanket · wornELECTRICAL SMELL REPORTED AT ROW 11 SIDEWALL NEAR FLOOR. *S/D* FOUND INSULATION BLANKET ON APU DUCT DETERIORATED. REPLACED INSULATION BLANKET ON APU BLEED DUCT.SDR 2000UALA00153Line · leakingLOST OF SYSTEM ''A'' HYDRAULICS DUE TO A HYDRAULIC LEAK FROM A FLEX LINE. *S/D* LEAK WAS FOUND COMING FROM LEFT HAND MAIN LANDING GEAR LOCK ACTUATOR. REPLACED DAMAGED HYDRAULIC FLEX LINE.SDR 2000UALA00147Transceiver · malfunctionedNUMBERS 1 AND 2 VERY HIGH FREQUENCY COMMUNICATIONS SYSTEMS FAILED FOR FIVE MINUTES. *S/D* REPLACED THE NUMBER 1 VERY HIGH FREQUENCY COMMUNICATIONS TRANSCEIVER (P/N 6221181003) AND THE NUMBER 1 AUDIO CONTROL PANEL (P/N G283304).SDR 2000UALA00130Skin · crackedTHE FUSELAGE SKIN CRACKED ALONG STRINGER S-25L AT BODY STATION 935. REMOVED THE EXISTING ADJACENT DOUBLER. FABRICATED AND INSTALLED THE NEW EXTENDED DOUBLER.SDR 2000UALA00039Fire Loop · shortedTHE AIRCRAFT DIVERTED DUE TO AN AMBER ALERT ON THE AUXILIARY POWER UNIT FIRE INDICATION. *S/D* THE LOWER LOOP M334 SHORTED TO GROUND. REPLACED THE LOWER LOOP M334 AND AUXILIARY POWER UNIT FIRE BOTTLE.SDR 2000UALA00005Detector · shortedTHE AUXILIARY POWER UNIT FIRE BOTTLE DISCHARGED BY THE FLIGHT CREW . *S/D* THE SHORTED M717 DETECTOR CAUSED A FALSE FIRE INDICATION. REPLACED THE M717 LOOP AND THE AUXILIARY POWER UNIT FIRE BOTTLE. REPLACED THE M515 LOOP AS A PRECAUTION.SDR 99UAL900652Warning Light · illuminatedTHE CREW REPORTED THE 'A' HYDRAULIC SYSTEM QUANTITY INDICATION OF 1.9 GALLONS ALONG WITH THE ILLUMINATION OF THE LOW QUANTITY LIGHT FOR THE STANDBY HYDRAULIC SYSTEM.SDR 99UAL900540Engine · leakingFLIGHT CREW SUSPECTED FLUID LEAK ON NUMBER ONE ENGINE.SDR 99UAL900526Coupler · failedDURING TAKEOFF AT 120 KNOTS, AIRCRAFT YAWED TO THE RIGHT. AT THE TIME, NUMBER 1 AND 2 ENGINE OUTPUTS WERE EQUAL. *S/D* REPLACED THE YAW DAMPER COUPLER. REPLACED THE BEARINGS AS A PRECAUTION.SDR 99UAL900505Hsi · flaggedTHE CAPTAIN'S HSI AND THE FIRST OFFICER'S RMI FLAGS INTERMITTENTLY CAME IN VIEW.SDR 99UAL900485Outflow Valve · failedAT APPROXIMATELY 12K, THE CABIN PRESSURE CONTROL WENT FROM AUTO TO STANDBY. FIVE MINUTES LATER AND AT 23K, RATE OF CLIMB PRESSURE OF AIRCRAFT INCREASED TO APPROXIMATELY 1000 FEET BELOW SEA LEVEL. CABIN DIFFERENTIAL PRESSURE WAS IN YELLOW BAND BUT DID NOT EXCSDR 99UAL900484Beam · fracturedDURING ROUTINE GEAR SWINGS, THE RIGHT MAIN GEAR WAS PINNED WHEN THE RIGHT MAIN GEAR WALKING BEAM (BOEING P/N 65-46108-X) FRACTURED TWO INCHES FROM THE OUTSIDE DIAMETER OF THE SLOTTED BEARING RACE. *S/D* THE RIGHT MAIN LANDING GEAR ACTUATOR WALKING BEAM FRACT
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