Boeing 737-222
Service difficulty reports · 657
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 = '737222' 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 = '737222' 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 96UAL900475Fire Module · malfunctionedCREW REPORTED NUMBER TWO ENGINE HAD FIRE WARNING ON TAXI IN. LIGHT REMAINED ON AFTER BOTH BOTTLES WERE SEQUENTIALLY DISCHARGED. *S/D* ACCOMPLISHED VISUAL CHECK OF ENGINE, FOUND OK. CHECKED INLET AND EXHAUST, ALSO OK. REPLACED ENGINE MODULE AND RAN ENGINE,SDR 96UAL900473Fan · failedFLIGHT CREW REPORTED THAT EN ROUTE HAD AN ELECTRICAL SMOKE AND SMELL THROUGHOUT THE CABIN. GALLEY POWER AND GASPER FAN SHUT OFF. SUPPLEMENTAL DATA UPDATE: TROUBLESHOT SYSTEM AND FOUND BURNT BEARINGS ON THE GASPER FAN. REPLACED GASPER FAN. CHECKS O.K.SDR 96UAL900434Position Ind · malfunctionedTRAILING EDGE FLAPS LOCKED OUT HYDRAULICALLY AT 2.5 DEGREES, NEEDLES WERE MATCHED. CREW SELECTED ALTERNATE FLAPS TO TRY TO GET TO 15 DEGREES. ALTERNATE FLAPS CAUSED BOTH NEEDLES TO INCREASE 1 TO 2 DEGREES. CREW WAS NOT SURE IF FLAPS MOVED OR IF IT WAS A INDSDR CALA9600773Adc · inoperativeTHE CAPTAIN'S ALTIMETER, COMPASS FLAG IN HSI, OFF FLAG IN ALT SELECT WINDOW, AUTO PILOT, MACH TRIM, GPWS, MODE-C AND CAPTAIN'S DME INSTRUMENTATION ALL WENT INOPERATIVE INTERMITTENTLY WHILE EN ROUTE. THE USABILITY OF THE INSTRUMENTATION WOULD RETURN EVERY 10 SDR 96UAL900417Computer · corrodedYAW DAMPER ABRUPTLY MOVES RUDDER INTERMITTENTLY FOR NO APPARENT REASON. *S/D* REPLACED YAW COUPLER AND VERTICAL GYRO. FOUND CORROSION ON COMPUTER CONTACTS. REPLACED ROLL COMPUTER, CHECKS OK.SDR 96UAL900408Skin · crackedTHREE RIVETS IN A ROW WITH CRACKS IN FUSELAGE SKIN COMING FROM RIVET HOLES. LOCATION IS APPROXIMATELY ONE FOOT FORWARD AND THREE FEET ABOVE AFT CARGO DOOR.SDR 96UAL900401Light · failedEMERGENCY EXIT LIGHT ABOVE AFT GALLEY DOOR FAILS A-CHECK TEST. REPLACED EMERGENCY LIGHT ASSEMBLY, OPERATION CHECKS NORMAL.SDR CALA9600820Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN EXTERNAL SKIN AT FORWARD LOWER CORNER OF L-2 DOOR CUTOUT. THE CRACKED AREA WAS CUT OUT, REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-30-2 AND 51-10-2.SDR CALA9600822Doubler · crackedINSPECTION FOUND THREE EACH CRACKS IN T-CHORD AND WEB DOUBLER AT STA 675, RBL 24.8. THE CRACKS WERE .25 INCH OR SMALLER. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2. THE EDGE CRACKS ON T-CHORD WERE TRIMMED OUT AND THE REPAIR WAS SDR 96UAL900377Coffee Warmer · dirtyCREW REPORT, AN ELECTRIC OVERHEAT SMELL IN THE COCKPIT WITH BOTH PACKS ON, STARTED EIGHT MINUTES AFTER TAKEOFF. *S/D* REPLACED COALESCER BAGS. FOUND PLASTIC ON FORWARD COFFEE WARMER, REMOVED PLASTIC. RAN PACKS WITH ENGINE AND APU, NO SMELLS NOTED.SDR 96UAL900376Tire · blow outLEFT OUTBOARD IN TIRE BLEW ON TAKEOFF, DID NOT RETRACT GEAR. REPLACED NUMBER ONE AND NUMBER TWO MAIN TIRES, CHECKS OK.SDR CALA9600821Floorbeam · crackedINSPECTION FOUND A .5 INCH CRACK IN FLOORBEAM WEB AT STA 665, BBL 0. THE AREA WAS REPAIRED IAW EA 5710-01322, SRM 51-30-09 AND SRM 51-30-02.SDR P2EA96002Circuit Breaker · trippedFLT NR 204 - SLC - AT 5 KNOTS, TAKEOFF CONFIGURATION WARNING HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND LEADING EDGE POSITION ANNUNCIATOR DC CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. ACCOMPLISHED TAKEOFF WARNING SYSTEM CHECSDR 96UAL900340Line · leakingCREW REPORTS LOSS OF A-SYSTEM HYDRAULIC FLUID WHEN GEAR LOWERED ON APPROACH. DECLARED AN AMBER ALERT. *S/D* FOUND HYDRAULIC LINE TO A-SYSTEM LEAKING. INSTALLED NEW LINE, CHECKS OK.SDR 96UAL900305Light Strip · inoperativeEMERGENCY ESCAPE PATH LIGHTING AT ROW 12 INOPERABLE. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP. CHECKS O.K.SDR 96UAL900256Switch · inoperativeWHEN GEAR EXTENDED FOR LANDING GOT A RED UNSAFE LIGHT FOR NOSE LANDING GEAR. RECYCLED GEAR AND SECOND EXTENSION GOT NO LIGHTS AT ALL. VISUALLY CONFIRMED NOSE GEAR WAS DOWN. MAIN GEAR INDICATIONS WERE NORMAL. *S/D* REPLACED NOSE LANDING GEAR INDICATION SWISDR 96UAL900240Turbine Wheel · failedAPU DISCHARGED METAL FRAGMENTS ONTO RAMP. SUPPLEMENTAL DATA UPDATE: FOUND TURBINE WHEEL FAILED. CAUSE UNDER INVESTIGATION. PART TOTAL CYCLES, 6,673.SDR 96UAL900232Battery · dischargedRIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, CHECKS OK.SDR 96UAL900231Duct · damagedHEARD LOUD NOISE AFTER TURNING ON RIGHT PACK AFTER TAKEOFF. *S/D* FOUND RIGHT AIR CONDITIONING DISTRIBUTION DUCT IN CENTER BAY AFT OF FORWARD CARGO PIT DAMAGED. REPLACED DUCT, CHECKS OK.SDR 96UAL900217Qty Transmitter · shortedAFTER TAKEOFF ON GEAR RETRACTION, "A" SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/2 GALLON. AFTER LOWERING GEAR, QUANTITY SHOWED FULL, THEN WENT BACK TO 1/2 GALLON. GAUGE JUMPED AROUND AFTER LANDING AND WENT TO FULL. SUPPLEMENTAL DATA UPDATE: REPLACED "A" SYSTESDR 96UAL900204Windshield · failedNR 1 LEFT WINDSHIELD OUTER PANE SHATTERED. WINDOW HEAT TURNED OFF AND OPERATED AT REDUCED PRESSURIZATION. SUPPLEMENTAL DATA UPDATE: MOISTURE AT THE POWER BUS CAUSED SHORT AND CRACKED THE OUTER PANE. REPLACED WINDSHIELD. CHECKS O.K.SDR 96ZZZX1692Boost Pump · malfunctionedMCO - FLT 570 - DEPARTED MCO TO ROCHESTER, NY. DURING FLIGHT, CREW REPORTED A FUEL IMBALANCE OCCURRED OUT OF RT MAIN TANK. AIRCRAFT WAS DIVERTED TO GSP. MAINTENANCE AND FLT CREW WERE DISPATCHED TO GSP TO RECOVER A/C. SYSTEM WAS CHECKED BY MAINTENANCE. ALLSDR 96UAL900188Csd Hose · leakingABORTED TAKEOFF DUE TO LOW OIL PRESSURE LIGHT CAME ON AT 90 KNOTS. SUPPLEMENTAL DATA UPDATE: CONSTANT SPEED DRIVE OIL SERVICE LINE WAS LEAKING. REPLACED TWO SHORT HOSES ON THE ELBOW FITTING AND ASSOCIATED "O" RINGS. CHECKS O.K.SDR 96UAL900187Tire · separatedRIGHT OUTBOARD MAIN TIRE SEPARATED AND DAMAGED THE FLAP AND NUMBER ONE SPOILER. *S/D* REPLACED NUMBER THREE AND FOUR MAIN TIRE. REPAIRED FLAP AND SPOILER. TIRE CAP COMPLETELY GONE.SDR 96UAL900185Light Strip · damagedEMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 15 TO ROW 18. REPLACED DAMAGED LIGHT STRIP AND CHECKS OK.SDR 96UAL900184Toggle · brokenDURING INSPECTION OF FLAPS FOR A AIRCRAFT ROLLING PROBLEM WITH FLAPS AT 10 DEGREES, FOUND LEFT SIDE FOREFLAP LOOSE FROM MIDFLAP. LEFT OUTBOARD TOGGLES WERE FOUND BROKEN. AIRCRAFT HAD BEEN DE-ICED WITH TYPE II FLUID 55 HOURS PREVIOUS TO THE INCIDENT. TOGGLE SDR 96UAL900166Light · disconnectedNR ONE LEFT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REINSTALLED EXIT LIGHT AT DOOR ONE LEFT. CHECKS O.K.SDR 96UAL900158Gland Nut · fracturedON GEAR RETRACTION LEFT MAIN GEAR RED LIGHT STAYED ON WITH GEAR HANDLE IN THE UP POSITION. RECYCLED GEAR AND GOT 3 GREEN LIGHTS IN DOWN POSITION. RED LIGHT REMAINED ON WITH GEAR HANDLE IN THE UP POSITION, HAD HEAVY DRAG IN CRUISE. *S/D* LEFT MAIN GEAR GLANSDR 96UAL900150Air Distr · odorELECTRIC SMOKE SMELL IN COCKPIT AND CABIN SWITCHING BLEEDS. CEILING IN FORWARD GALLEY HOT TO TOUCH. EMERGENCY EQUIPMENT REQUESTED. SUPPLEMENTAL DATA UPDATE: ACCOMPLISHED POWER RUN, CHECKED ALL SYSTEMS, COULD NOT DUPLICATE. REMOVED CEILING PANELS AND CHECKSDR 96UAL900138Coalescer Bag · contaminatedCREW REPORTS, HEAVY SMOKE IN COCKPIT AND CABIN. TURNED RIGHT PACK OFF AND THEN LEFT PACK, NO HELP. CREW TURNED OFF SOME ELECTRICAL FUNCTIONS AND SMOKE WAS SOMEWHAT BETTER ON APPROACH. SOURCE OF SMOKE MAYBE OIL OR ELECTRICAL. OIL WAS FOUND IN THE LEFT PACK SDR 96UAL900130Coalescer · contaminatedDURING CLIMB, KEROSENE LIKE SMELL IN PASSENGER CABIN. BOTH PACKS AND BLEEDS ON AT THE TIME. FUEL SMELL ORIGINATED FROM THE GROUND PNEUMATIC CONNECTOR, WHICH WAS CONTAMINATED FROM A GROUND TRUCK USED FOR STARTING THE ENGINES. THE DUCTING WAS CLEANED, COALESCSDR 96UAL900111Regulator · leakingSMOKE IN CABIN, THE RIGHT PACK WAS OFF AND THE OVERHEAT LIGHT CAME ON. THE TURBOFAN WAS RUNNING ALL THE TIME. REPLACED THE PRESSURE REGULATOR, CHECKS OK. THE SHOP FOUND AN INTERNAL DIAPHRAGM WAS LEAKING.SDR 96UAL900090Prox Card · badAFTER TAKEOFF, GEAR LEVER WOULD NOT GO PAST NEUTRAL POSITION, RETURNED TO ORD. *S/D* THE A-1 AND A-2 LANDING GEAR POSITION INDICATING SYSTEM PROXIMITY CARDS IN THE LANDING GEAR ACCESSORY UNIT WERE FOUND BAD. REPLACED CARDS, SYSTEM CHECKS OK.SDR 96UAL900082Out Flow Valve · failedCREW REPORTS, UNABLE TO PRESSURIZE AIRPLANE AFTER TAKEOFF. CAN CONTROL OUTFLOW VALVE OPEN AND CLOSE. THE RIGHT FLOW CONTROL VALVE WOULD NOT TURN ON. REPLACED FLOW CONTROL VALVE AND CONNECTOR PINS. THE SHOP FOUND THE FLOW CONTROL VALVE HAD LOW AIR FLOW CAUSSDR 96UAL900066Seal · leakingCREW REPORTS, UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. MAINTENANCE FOUND AIR LEAKING FROM FORWARD AIRSTAIRS DOOR SEAL. STOPPED LEAK BY PUTTING ALUMINUM FILLED EPOXY RESIN UNDERNEATH AIRSTAIRS DOOR SEAL. AIRCRAFT PRESSURIZES NORMALLY.SDR 96UAL900054Strip · inoperativeEMERGENCY ESCAPE PATH LIGHTING IN FIRST CLASS INOP. REPLACED LIGHT STRIP.SDR 96UAL900029Lamp · failedEMERGENCY ESCAPE PATH LIGHTING INOP AT ROW 12. RELAMPED AND REPLACED COVER, CHECKS OK.SDR 96UAL900022Battery · dischargedAFT GALLEY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES AND CHECKS OK.SDR 96UAL900019Battery · dischargedFLIGHT DECK EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY AND CHECKS OK.SDR 96UAL900003Fire Loop · inoperativeEXPERIENCED NUMBER ONE ENGINE FIRE WARNING, ENGINE WAS SHUTDOWN AND FIRE BOTTLE DISCHARGED. REPLACED NUMBER ONE ENGINE LOWER FIRE DETECTION LOOP, BOTH FIRE BOTTLES AND SQUIBS.SDR 95UAL900370Compressor · stalledON TAKEOFF AT 90 KNOTS, NR ONE ENGINE HAD A COMPRESSOR STALL. A BRIGHT FLASH WAS OBSERVED ON TAKEOFF, ABORTED TAKEOFF. SUPPLEMENTAL DATA UPDATE: ENGINE WAS BORESCOPED AT THE C-6, C-7, AND C-13 BLADES. BORESCOPE REVEALED EVIDENCE OF SMALL BIRD INGESTION WITHSDR 95UAL900360Sensing Element · inoperativeCREW REPORTED, NR 2 ENGINE FIRE WARNING INDICATION ILLUMINATED IN FLIGHT. DISCHARGED BOTTLES AND SHUTDOWN ENGINE. REPLACED NUMBER TWO ENGINE FIRE DETECTION SENSING ELEMENT, CHECKS OK.SDR 95UAL900358Csd · failedIN CRUISE WHEN THROTTLES WERE RETARDED, NR1 CSD LOW OIL PRESSURE LIGHT CAME ON AND THEN WENT OFF, OCCURRED REPEATEDLY. ALSO, AUTOPILOT DISENGAGED MANY TIMES FOR NO REASON. REPLACED NUMBER ONE ENGINE CONSTANT SPEED DRIVE, OIL COOLER AND OIL FILTER. RAN ENGINESDR 95UAL900357Anti-Skid Module · inoperativeOUTBOARD ANTI-SKID WARNING LIGHT ILLUMINATED AT 100 KNOTS ON TAKEOFF ROLL. TAKEOFF WAS ABORTED WITH VERY LITTLE BRAKING USED. REPLACED ANTI-SKID CONTROL MODULE, CHECKS OK.SDR 95UAL900356Latch Mech · out of adjustHANDLE AT DOOR 2 LEFT KEEPS MOVING TOWARD THE OPEN POSITION IN-FLIGHT. SUPPLEMENTAL DATA UPDATE: CHECKED LATCH TORQUE TUBES FOR PROPER ADJUSTMENT PER MM. DOOR CHECKS O.K.SDR 95UAL900354Nr 3 Bearing · failedAT 29,000 FEET HEARD A BANG FROM RIGHT HAND SIDE OF AIRCRAFT. EPR DROPPED AND CAPTAIN REDUCED ENGINE TO FLIGHT IDLE. FOUND NUMBER THREE BEARING CAGE FAILURE. SUSPECT IT WAS DUE TO EXCESSIVE POCKET WEAR. FAILURE OCCURRED MIDWAY BETWEEN THE CAGE RIVET HOLES.SDR 95UAL900280Flex Line · cloggedBOTH LOW PRESSURE LIGHTS FOR 'A' SYSTEM HYDRAULIC PUMPS CAME ON FOLLOWED BY LOW PRESSURE LIGHT FOR NUMBER ONE 'B' PUMP AND FEEL DIFFERENTIAL PRESSURE LIGHT. FOUND OBSTRUCTION IN ENGINE FLEX LINE CAUSING LOW PRESSURE INDICATION. REPLACED RESERVOIR AIR PRESSURSDR 95UAL900276Cabin Press Ind · leakingPASSING THROUGH 25,000 FEET, CABIN ALTITUDE WAS 6,500 FEET AND CLIMBING AT 700 FEET. THE DIFFERENTIAL PRESSURE WAS 2.1 AT 29,000 FEET, CABIN WAS AT 6,500 FEET AND DIFFERENTIAL PRESSURE WAS 2.8, STANDBY NO HELP. CAPTAIN WENT ON OXYGEN BECAUSE NOT FEELING WELLSDR 95UAL900260Indicator Wire · failedNR THREE LEADING EDGE DEVICE FAILED TO RETRACT AFTER TAKEOFF. THIS WAS FOUND TO BE AN INDICATION PROBLEM. THE NR THREE LEADING EDGE SLAT ACTUATOR ROD END WIRE ASSEMBLY WAS REPLACED. CHECKS O.K.SDR 95UAL900250Strut · crackedNR THREE MAIN LANDING GEAR INNER CYLINDER BRAKE FLANGE HAS TWO CRACKS. CRACKS START FROM THE INSIDE OF THE MOUNT BOLT HOLES AT THE 2 O'CLOCK AND 10 O'CLOCK POSITIONS AND EXTEND INWARD TOWARD FLANGE RADIUS. CRACKS CONFIRMED BY EDDY CURRENT INSPECTION. REPLA
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