Boeing 737-247
Service difficulty reports · 1,009
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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 = '737247' 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 = '737247' 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 DL73S031111Tab · flutterON CLIMB FROM CVG AT 250 - 280 KTS. F/A REPORTED VIBRATION IN AFT OF AIRCRAFT. VERIFIED BY F/O. NO CHANGE WITH CHANGE IN AIRSPEED, ON DESCENT F/A NOTICED VIBES, SIGNIFICANTLY REDUCED AIRSPEED BELOW 250 KTS. REPLACED LEFT AND RIGHT ELEVATOR TABS.SDR DL73S031046Fire Detector · malfunctionedPRIOR TO TIME OF DESCENT, APU FIRE WARNING. ACCOMPLISHED EMERGENCY PROCEDURES. BOTTLED DISCHARGED. LIGHT REMAINED ILLUMINATED. INSPECTED APU EXHAUST AND APU COMPARTMENT FOR DAMAGE OR EVIDENCE OF FIRE, NONE FOUND. APU WAS NOT RUNNING AT TIME OF FIRE WARNINSDR DL73S030927Web · wornFOUND ON R1 LETTER CK,OUTBOARD BALANCE BAY I/B WEB CHAFED THRU AT LT HORIZ STAB. REPAIRED PER SRM 51-40-20 FIG 11.SDR DL73S030920Actuator · leakingLOST A-SYSTEM HYD PRESSURE AND QTY WHILE PASSING THROUGH 18,500. FOUND NR 3 SPOILER ACTUATOR LEAKING. REPLACED SAME.SDR DL73S030910Autothrottle Sys · failedON T/O ROLL AFTER TOGA THROTTLES REQUIRED MANUAL SET WITH NORMAL FD/AP/AT. F/O TURNED THROTTLE OVER TO CAPT NR 1 AND 2 THROTTLES SPLIT WITH AN INCREASE ON 1. EGT WENT UP TO 630 ON NR 1 WITH A 2.12 SETTING 2.1 AT SET. NR 2 WAS AT 2.04. EVENED THROTTLES AT 2SDR DL73S030815Adc · failedAFTER LIFTOFF F/O ALT AND AIRSPEED FAILED. CONTACTED ATL MTC RTN TO CVG. REPLACED NR 2 DADC.SDR DL73S030794Adc · failedON T/O LOST BOTH CAPT AND F/O AIRSPEED AND ALTIMETER. CAPTS FROZE, NO FLAGS. F/O HAD FLAGS IN VIEW. FOUND HOSES OFF NR 1 ADC. RECONNECTED HOSES, BOTH WERE SECURE. PERFORMED TEST ON ADC CHECKS OK. F/O ADC HAD FAILED. REPLACED SAME, TEST OK.SDR DL73S030788Wire · shortedNR 2 ENG SHUTDOWN INFLT DUE TO OIL TEMP PEGGED HIGH. FOUND TO BE INDICATION PROBLEM (SHORTED WIRE). REPAIRED WIRE.SDR DL73K030782Wire · chafedDURING PREFLIGHT, FOUND EMERGENCY EXIT LIGHTS INOP AT ROWS 5 TO 9. FOUND BROKEN WIRE CHAFING AT SEAT 5D. REPAIRED WIRE IAW MM. REPLACED FUSES IN FWD AND AFT BATTERY PACKS. LIGHTS NOW OPS NORMAL.SDR DL73K030625Power Supply · dischargedLEFT OVER WING DOOR EXIT SIGN INOP DURING TEST. REPLACED POWER SUPPLYSDR DL73S030618Sense Line · looseA/C WOULD NOT PRESSURIZE DURING CLIMBOUT. POM PROCEDURE WERE FOLLOWED AS WELL AS MULTIPLE BLEED CONFIGURATIONS WERE TRIED INCLUDING USING APU BLEED AND STBY AND MANUAL AC/DC MODES ON CONTROLLER. MAIN AND FWD OUTFLOW VLVS WERE CLOSED. SECURED LOOSE SENSE LINSDR DL73S030554Duct · damagedNR 2 ENGINE OVERHEAT LIGHT ILLUM SHORTLY AFTER T/O EGT APPROX 620 FULL T/O POWER SETTING. RETARDED THROTTLE, LIGHT WENT OUT APPROACHING IDLE. REPLACED FLEX DUCT AND TWO LOWER FIRE LOOPS.SDR DL73K030539Strap · buckledFS 1016 PRESSURE BULKHEAD / OUTER CIRCUMFERENTIAL TEAR STRAP / STR5L TO 7L - BUCKLING: THE SUBJECT STRAP WAS FOUND BUCKLED BETWEEN FASTENERS FROM THE BULKHEAD WEB SPLICE AT S-7L TO APPROXIMATELY S-6L. THERE IS NO BUCKLING OR OIL CANNING OF THE BULKHEAD WEB. SDR DL73K030501Tube · crackedSLOW LEAK IN FLT RESULTED IN A-SYSTEM RESERVOIR GOING TO ZERO AND SUBSEQUENT LOW PRESSURE LIGHTS ILLUMINATED. FOUND NR 1 ENG TO PYLON PRESSURE LINE CRACKED AT BEND. REPLACED HYD LINE. RAN ENGINES/FLIGHT CONTROLS, NO FURTHER LEAKS NOTED.SDR DL73K030460Power Supply · inoperativeEMERGENCY FLOOR LIGHTING INOP AT ROWS 1 THRU 4. REPLACED POWER SUPPLYSDR DL73S030404Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK JUST BELOW STRINGER 18R AT FS 750. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737-200 SRM AND PER ER/A 384987-14.SDR DL73K030336Element · malfunctionedNR 1 ENGINE OVERHEAT ON CLIMBOUT.PERFORMED PROCEDURES IAW POM. LIGHT STAYED ON UNTIL AFTER SE LANDING - REPLACED LOWER LOOP AND FIRE DETECTOR ACCESSORY UNITSDR DL73K030310Door Frame · crackedTHE UPPER STUB SECTION OF THE R1 DOOR OPENING FWD FRAME WAS FOUND WITH A 1.1 INCH CRACK IN THE BEND RADIUS EMANATING FROM THE FRAME CUTOUT FOR THE UPPER DOOR STOP FITTING. THE CRACK WAS REMOVED WITH A TRIM OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE PER ERSDR DL73K030295Line · damagedCAPT'S A/S INDICATOR FAILED ABOVE 110K ON TAKEOFF. ON T/O IT WENT TO 45K, AFTER AIRBORNE TO 360K, LATER DECREASED TO 45K PRIOR TO LANDING. REPLACED PITOT FLEX LINE ON FRONT OF NR 1 ADC, PERFORMED LEAK CK PER MM AND FOUND NO LEAKS. ALL INST TEST OK PER MM.SDR DL73K030274Actuator · brokenON APPROACH INTO MCO NOSE LANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. OK ON SECOND ATTEMP AND LANDED WITH OUT INCIDENT. AMT FOUND LOCK ACTUATOR FAILED CAUSING 1 INCH DIAMETER HOLE IN FWD PRESS BULKHEAD NOSE WHEEL WELL.SDR DL73K030207Controller · inoperativeNR 1 CSD HIGH OIL TEMP LIGHT ILLUM CLIMBING THRU 15000 FT. DISCONNECTED CSD PER POM. STARTED APU AT 19000 FT THEN AT FL250 THE APU GEN DROPPED OFF LINE. DIVERTED TO MCO. FOUND CSD OVERSERVICED. SERVICED TO CORRECT LEVEL. CHECKS NORMAL ON ENGINE RUN. FWDSDR DL73K030177Duct · rupturedSHORTLY AFTER LIFT OFF, NR 2 ENGINE OVERHEAT LIGHT CAME ON ACCOMPANIED BY A BLEED TRIP LIGHT. OVERHEAT LIGHT EXTINGUISHED WHEN THRUST LEVERS RETARDED TO IDLE. FOUND SENSE LINE LEAKING AT PRBC AND COWL ANTI-ICE DUCT BLOWN. REPLACED SENSE LINE, COWL DUCT, ANDSDR DL73K030117Skin · crackedTHE FUSELAGE SKIN AT FS 480 WAS GOUGED AND CRACKED BY GROUND EQUIPMENT JUST BELOW THE STRINGER 26R SKIN LAP JOINT. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN. THE SKIN CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384498-14.SDR DL73K030038Floorbeam · corrodedCORROSION DAMAGE ON STA 986.5 FLOORBEAM UPPER CHORD AT LBL 6 AND RBL 6. REPAIRED PER SRM DRD 53-20-1D FIG 803D, UPPER CHORD REPLACEMENT.SDR DL73K030007Blade · damagedON CLIMBOUT FROM BDL PASSING THROUGH FL6000 HEARD AND FELT A LOUD EXPLOSION FROM AREA OF THE FORWARD CARGO NR 2 ENG. DIVERTED TO JFK, THE STALL NOISE WAS AUDIBLE FROM COCKPIT BUT ENGINE INST WERE NORMAL ON BOTH ENGINES. FOUND 5 FAN BLADES CURLED AT TIP. BLESDR DL73K021468Transceiver · failedWX RADAR INOP. ANT FAULT MSG DISPLAYED. REPLACED RADAR TRANSCEIVER. RADAR TEST NORMAL.SDR DL73K021443Skin · dentedFUSELAGE / SKIN / FS 370-400 / STRG. 17L-18L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED AT FS FS 395 BETWEEN STRINGERS 17L & 18L. THERE WAS AN ADJACENT SKIN REPAIR WITHIN 10" OF THE DENT. THE EXISISDR DL73K021406Regulator Valve · leakingAIR TURNBACK FROM FLL TO BDL, RETURNED TO FLL. BLEED TRIP OFF NR 1 ENG ON TAKEOFF ROLL. REPLACED PRESSURE REGULATOR BLEED LINES FOR LEAKING.SDR DL73K021341Check Valve · leakingON ARRIVAL FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE DENTED. SUSPECT DAMAGE FROM BLUE ICE CAUSED BY LEAKING FWD LAV SERVICE PANEL. REPLACED STAB L/E ASSY AND REPLACED LAV SERVICE LINE CHECK VALVE.SDR DL73K021333Hydraulic System · lowSYSTEM A HYD QTY INDICATOR DROPPED TO 1.5 GALLONS FOLLOWED BY ILLUMINATION OF SYSTEM B LOW QTY LIGHT. ABNORMAL PROCEDURES FOLLOWED. A/C ARRIVED WITH A SYSTEM AT 2.5 GAL. SERVICED TO FULL EXERCISED FLAPS/SLATS AND SPOILERS OPERATED GEAR HANDLE. PERFORMED YASDR DL73K021315Tire · separatedON WALK AROUND FOUND TIRE TREAD MISSING ON NR 4 MAIN TIRE. TREAD SEPARATION CAUSED DAMAGE TO THE RT INBD UNDERWING FIXED PANEL, RT TRAILING EDGE MID FLAP AND BROKE THE INNER AND CENTER RT GEAR DOORS. REPLACED WHEEL ASSY AND REPAIRED DAMAGE.SDR DL73K021245Clamp · looseON T/O ROLL RECEIVED A PACK TRIP OFF INDICATION. CONTINUED TAKEOFF. ONCE AIRBORNE PERFORMED PROCEDURE PER POM. WHEN THE PACK WAS RESET THE PRESSURE PEGGED TO TOP OF SCALE. WING BODY OVERHEAT ILLUMINATED FOLLOWED BY A BLEED TRIP OFF INDICATION. ALL INDICATSDR DL73K021229Wire · brokenRED TRACK LIGHTING INOP AT FWD COAT CLOSET, REPAIRED WIRE.SDR DL73K021206Web · chafedFOUND ON Q1 LETTER CK RT AND LT INBD BALANCE BOARD PANELS CHAFING THROUGH THE INBD WEBS. REPAIRED PER SRM 51-40-20 AND OPERATION 1000SDR DL73K021205Skin · gougedUPPER SKIN WORN THROUGH AT NO 2 T/E FOREFLAP REPAIRED PER SRM 51-40-20 FIG 12SDR DL73K021187Drain · failedON CLIMBOUT NOTICED EXCESSIVE CABIN CLIMB RATE. LEVELED OFF AT 10000 FT. CABIN CONTINUED TO CLIMB TO 10000 FT. OUTFLOW VALVE SHOWED FULL CLOSED. FORWARD OUTFLOW VALVE SHOWS FULL CLOSED. COULD NOT CONTROL CABIN ALTITUDE AT ALL IN DESCENT. REPLACED SEVERALSDR DL73K021178Gasper Fan · failedON ARRIVAL PBI CREW OFF FLT 2309 REPORTED UNIDENTIFIABLE ODOR THROUGHOUT THE AIRCRAFT. AIRCRAFT WAS CARRYING HUMAN REMAINS, AND CREW SUSPECTED THIS TO BE THE SOURCE OF THE ODOR. BOTH MTC AND GROUND CREW INSPECTED CARGO COMPARTMENTS AND FOUND CLEAN. GRD CREWSDR DL73K021167Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 1.375 CRACK ALONG THE MILL LINE JUST ABOVE STRINGER 16L AT FS 525, AFT OF THE WING SCANNING LIGHT CUTOUT. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM AND ERSDR DL73K021165Skin · crackedTHE SKIN AT THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR (R2) CUTOUT WAS FOUND WITH A .375 INCH TYPICAL CRACK. THE CRACK WAS CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL DOUBLER PER ER/A 383941-14, REV A.SDR DL73K021150Tire · separatedNR 4 TIRE TREAD SEPARATION ON T/O FROM FLL. OUTBOARD GEAR DOOR MISSING WITH DAMAGE TO NR 2 ENGINE NACELLE AND RIGHT FLAP ASSEMBLY ONLY MINOR BUMP FELT ON T/O ROLL PRIOR TO ROTATION. REPLACED BOTH RIGHT MAIN WHEEL ASSY, REPLACED DOOR, RPD NACELLE.SDR DL73K021109Power Supply · dischargedEMERGENCY EXIT LIGHTS POWER SUPPLY FAILED ON L/O INSP. REPLACED POWER SUPPLY.SDR DL73K020934Battery · dischargedAFT MEGAPHONE INOP. REPLACED BATTERIES.SDR DL73K020922Hydraulic Line · leakingNR 2 ENGINE HYD PUMP RUPTURED THE PRESS LINE AND LOST ALL HYD QTY. FOUND RIGHT ENGINE HYD PUMP PRESS LINE LEAKING. REPLACED LINE. PULLED AND INSPECTED ALL SYSTEM AND CASE DRAIN FILTERS, NO TROUBLE FOUND. SERVICED HYD TO FULL. RAN ENGINE AND ELEC PUMPS. CSDR DL73K020868Frame · crackedFUSELAGE FRAME AT STA 616 LH/RH WERE CRACKED IN IN BD/OUTBD FLANGEAT LOCATION ATTACHING TO FLOOR STUB BEAM. D AMAGE WAS FOUND DURING INSPECTION PER SI 3-85751-12. CORRECTIVE ACTION: DAMAGE WAS REPAIRED PER ER/A 383607-14.SDR DL73K020648Wire · chafedON ARRIVAL FOUND RIGHT OVERWING EMERGENCY EXIT SIGN INOP. REPLACED EXIT SIGN OVERHEAD BATTERY AND BATTERY POWER SUPPLY, REPAIRED CANNON PLUG WIRING AT POWER SUPPLY DUE TO CHAFED WIRING. ALL CHECK NORMAL.SDR DL73K020636Garlock Seal · leakingNR 1 ENG OIL QTY SHOWED A STEADY DECREASE AS FLIGHT PROGRESSED. ULTIMATELY QUANTITY WENT TO ZERO INDICATION. OIL TEMP AND PRESSURE REMAINED STEADY IN THE NORMAL RANGE AT ALL TIMES. FOUND NR 1 ENG GARLOCK SEAL AT STARTER LEAKING. REPLACED STARTER GARLOCK SSDR DL73K020617Door Frame · crackedDOORS / C2 CARGO DOOR / FWD FRAME / LAP SPLICE : CRACK REPAIR THE FWD FRAME OF THE C2 CARGO DOOR WAS FOUND WITH 2" CRACK IN THE UPPER FRAME AND A FASTENER HOLE CRACK IN THE LOWER FRAME AT FRAME LAP JSDR DL73K020598Ballast · failedCOCKPIT CENTER FLORESCENT LIGHTS INOP CA RPLD BALLAST, OP CKS GOOD.SDR DL73K020519Cap · splitHYDRAULIC SYSTEM A FAILURE IMMEDIATELY FOLLOWING TAKEOFF. FOUND CAP ON NR 7 SPOILER HAD SPLIT. REPLACED CAP AND O-RING. INSPECTED AND REPLACED CASE DRAIN AND PRESSURE FILTERS. SERVICED HYDS TO FULL. LEAK AND OPS CHECKS OK.SDR DL73K020432Skin · crackedTHE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR (R2) CUTOUT WAS FOUND WITH A .5 INCH TYPICAL CRACK IN THE BONDED SKIN ASSY. THE CRACK WAS REMOVED. THE SKIN WAS REPAIRED WITH AN EXTERNAL DOUBLER INSTALLED PER ER/A 382883-14 REV A.
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