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 95UAL900246Sensor · intermittentCREW REPORTS, AFT CARGO DOOR LIGHT FLICKERED AND THEN REMAINED ON. REPLACED PROXIMITY SENSOR AND ADJUSTED GAP PER MM CHECKS OK.SDR 95UAL900245Skin · crackedFOUND TWO-INCH CRACK IN FUSELAGE ON AFT SIDE OF E AND E COOLING FAN EXHAUST PORT. ACCOMPLISHED PERMANENT SKIN REPAIR PER STRUCTURAL REPAIR MANUAL 53-30-3 USING .10 INCH THICK 2024-T3 CIRCULAR EXTERNAL REPAIR DOUBLER WITH THREE FASTENER ROWS.SDR 95UAL900232Eel · inoperativeEMERGENCY ESCAPE PATH LIGHTING INOP IN AFT CABIN. REPAIRED LIGHT, CHECKS OK.SDR CAL950970Battery Pack · dischargedGSO - EXIT LIGHT INOP. REPLACED RIGHT EXTERNAL EMERGENCY EXIT LIGHT BATTERY PACK AND BATTERY. (M)SDR CAL950969Battery Pack · dischargedGSO - AIRCRAFT IN 1/2 D-CHECK, FOUND LEFT EXTERNAL EMERGENCY LIGHT INOP. REPLACED LEFT EXTERNAL EMERGENCY EXIT LIGHT BATTERY PACK AND BATTERY. (M)SDR CAL950968Battery Pack · dischargedGSO - AIRCRAFT IN 1/2 D-CHECK, FOUND BATTERY PACK INOP. REPLACED BATTERY PACK FOR L-1 SLIDE. (M)SDR CAL950967Frame · crackedGSO - AIRCRAFT IN D-CHECK, FOUND CRACK IN FRAME SEGMENT APPROXIMATLY .75 INCH AT BS 500A BETWEEN S20L, S21L, AND ABOVE S23L, REMOVED AND REPLACED. (M0SDR CAL950966Frame · crackedGSO - AIRCRAFT IN 1/2 D-CHECK, FOUND CRACK APPROXIMATELY .75 INCH IN FRAME SEGMENT AT BS 400 BETWEEN S21L AND S22L, REMOVED AND REPLACED. (M)SDR CAL950965Frame · crackedGSO - AIRCRAFT IN 1/2 D-CHECK, FOUND CRACK IN FRAME SEGMENT APPROXIMATELY .75 INCH AT BS 500A BETWEEN S20R AND S21R, REMOVED AND REPLACED. (M)SDR CAL950964Frame · crackedGSO - AIRCRAFT IN ONE-HALF D-CHECK. DURING INSPECTION, FOUND CRACK APPROXIMATELY .75 INCH AT BS 420 BETWEEN S21L, S22L, S23L. STOP DRILLED CRACK AND INSTALLED DOUBLER. (X)SDR CAL950963Frame · crackedGSO - AIRCRAFT IN ONE-HALF D-CHECK DURING INSPECTION, FOUND CRACK FRAME SEGMENT APPROXIMATELY .05 INCH AT BS 480 BETWEEN S20L AND S21L. REMOVED AND REPLACED. (X)SDR CAL950962Frame · crackedGSO - AIRCRAFT IN 1/2 D-CHECK DURING INSPECTION, FOUND CRACK IN FRAME SEGMENT AT BS 460 APPROXIMATELY .75 INCH, BETWEEN S20L AND S21L. REMOVED AND REPAIRED. (X)SDR CAL950960Frame · crackedGSO - INSPECTION FOUND CRACKS IN FRAME AT BS 500B BETWEEN STR 19L AND STR 20L, AND BETWEEN STR 25L AND STR 27L. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .33 INCH LONG. THE CRACKED SEGMENT OF FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (XSDR CAL950959Frame · crackedGSO - INSPECTION FOUND CRACKS IN FRAME AT BS 500 BETWEEN STR 21L AND STR 22L AND STR 22L AND STR 23L. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .75 INCH LONG. THE CRACKED SEGMENT OF FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (X)SDR CAL950958Frame · crackedGSO - INSPECTION FOUND A CRACK IN FRAME AT BS 420 BETWEEN S22R AND S21R AND BETWEEN S21R AND S20R. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .75 INCH LONG. THE CRACKED FRAME SEGMENT WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (X)SDR CAL950956Skin · crackedGSO - INSPECTION FOUND A .50 INCH CRACK AT FORWARD LOWER CORNER OF AFT CARGO DOOR CUT-OUT, EXTERNAL SKIN. THE CRACKED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW TIMCO ENGINEERING ORDER RFO-01655. (X)SDR 95UAL900224Brake Flange · crackedNR 4 WHEEL, BRAKE AND PART OF AXLE, DEPARTED FROM AIRCRAFT. REPLACED GEAR. CRACK WAS FOUND EMANATING FROM BRAKE ATTACH FLANGE, PER BOEING SERVICE BULLETIN 737-32-1068.SDR 95UAL900215Transmission · inopEXECUTED MISSED APPROACH AT ORD, TRAILING EDGE FLAPS DID NOT EXTEND BEYOND 5 DEGREES. REPLACED NR 7 TRAILING EDGE FLAP TRANSMISSION, CHECKS OK.SDR 95UAL900211Socket · burnedBURNING ELECTRICAL SMELL FROM AFT GALLEY AREA. SMELL DISSIPATED WHEN FLUORESCENT OVERHEAD LIGHTS AT GALLEY TURNED OFF. REPLACED LAMP HOLDER SOCKET, WIRES AND LAMPS. CHECKS O.K.SDR 95UAL900176Eel · inoperativeFIRST CLASS EEL LIGHTS INOP. REPLACED EEL LIGHTS.SDR 95UAL900155Eel Battery Pack · dischargedEMERGENCY LIGHTS INOP ON LEFT SIDE EXTERIOR OF AIRCRAFT. REPLACED BATTERY PACK.SDR 95UAL900154Latches · out of rigA/C RETURNED TO FIELD WITH AFT CARGO DOOR LIGHT, UNABLE TO PRESSURIZE A/C. AFT CARGO DOOR WAS FOUND OPEN. THE LATCHES APPEARED SECURE, BUT THE DOOR WAS OUT RIG.SDR AWXA9500641Door Frame · crackedPHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L2 DOOR FRAME CRACKED IN TWO AREAS, UPPER FORWARD CORNER OF FRAME AT BS 951, AND FORWARD NR 2 DOOR STOP CASTING, P/N 65558741, AT STOP BASE, FORWARD SIDE INNER SKIN WEB. REPAIRS COMPLIED WITH PER ER 2-53-16-41. (SDR 95UAL900109Fire Loop · malfunctionedAFTER TAXI OUT, THE NR 2 FIRE WARNING LIGHT CAME ON AND TWO FIRE BOTTLES WERE DISCHARGED. LIGHT REMAINED ON, PASSENGERS EVACUATED BY SLIDES. FOUND FIRE LOOP M337 HAS A SHORT BETWEEN PINS 4 AND 6 IN CONNECTOR D992. REPLACED LOOP SYSTEM, OPS CHECKS OK.SDR 95UAL900108Door · not latchedAFT CARGO DOOR LIGHT CAME ON AFTER TAKEOFF AND AIRCRAFT WOULD NOT PRESSURIZE. FOUND DOOR OPEN ON ARRIVAL, CHECKED LATCHES AND THEY OPERATED NORMAL, OVER CENTERED GOOD. NO PREVIOUS HISTORY.SDR P2EA95005Beam · corrosionFLT NR 119 - MCI - DURING NOSE WHEEL WELL INSPECTION PER EO 953753A010, MAINTENANCE FOUND CORROSION ABOVE NOSE WHEEL WELL APPROXIMATLEY STATION 227.8. MAINTENANCE REMOVED AND REPLACED STRUCTURAL BEAM. LEVEL 2 REPORT WILL BE FILED WITH BOEING AND FAA WILL ALSSDR 95UAL900067Uplock Act · malfunctionedAFTER GEAR RETRACTION, RT MAIN GEAR INTRANSIT RED LIGHT REMAINED ON. PLACED GEAR HANDLE OFF AND GEAR FELL OUT. TOOK 3 ATTEMPTS TO GET GEAR TO LOCK UP. REPLACED RT UPLOCK ACTUATOR. OPS CHECKS OK.SDR 95UAL900056Eel Batteries · dischargedONE COACH EMERGENCY FLASH LIGHT DOES NOT WORK. REPLACED BATTERIES.SDR 95UAL900050Eel Battery Pack · dischargedRT EXT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY.SDR 95UAL900048Eel Cable · failedTHREE SECTIONS OF EEL LIGHTING INOP MIDDLE OF ACFT. REPLACED EEL LIGHT POWER CABLE, CHECKS NORMAL.SDR 95UAL900041Eel Battery Pack · dischargedEXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACKS.SDR CAL950527Hyd Line · wornFLT NR 1728 - CLE - THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IND. BOTH THE RED AND GREEN LIGHTS REMAINED ON. WHEN THE GEAR HANDLE WAS PLACED DOWN, THE RED LIGHT EXTINGUISHED. THE HYDRAULIC QUANTITY GAUGE DROPPED TO .8 GALS. THE AIRCRAFT WSDR 95UAL900022Eel Battery Pack · dischargedRIGHT OW EMERGENCY LIGHTS STAYED ON. REPLACED OW BATTERIES.SDR 95UAL900004Hyd Hose · failedRETURNED TO FIELD UNDER AN AMBER ALERT DUE TO LOSS OF HYDRAULIC PRESSURE. RIGHT UPLOCK ACTUATOR HOSE FAILED AT THE B-NUT. REPLACED HOSE SYSTEM OP CHECKS OK.SDR 95UAL900000Oil Press Sw · malfunctionedA/C RETURNED TO ICT, WITH NR 2 OIL BYPASS LIGHT ON AND ENGINE POWER REDUCED TO IDLE. REPLACED OIL PRESSURE DIFFERENTIAL SWITCH.SDR 95UAL737079Eel Battery Pack · dischargedFOUND LEFT OVER WING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK.SDR 95UAL737078Yaw Damper · malfunctionedAUTOPILOT ENGAGED WITH ALTITUDE HOLD, HEADING HOLD AND YAW DAMPER ON. RECEIVED ONE JOLT IN RUDDER PEDALS FOR LEFT RUDDER INPUT. DISENGAGED YAW DAMPER AND AUTOPILOT.SDR 95UAL737077Fire Contl Unit · malfunctionedLANDED UNDER AMBER ALERT, DUE TO A FIRE WARNING INDICATION ON THE NUMBER 1 ENGINE. REPLACED ENGINE FIRE CONTROL UNIT.SDR 95UAL737073C-6 Blade · failedIN CRUISE, FLIGHT LEVEL 290, NUMBER TWO ENGINE EXHAUST GAS TEMPERATURE PEAKED AND EXPERIENCED SEVERE VIBRATION. PULLED THROTTLE BACK TO IDLE AND DIVERTED TO CLE. FAILED C-6 BLADE DAMAGED HIGH AND LOW COMPRESSORS. BLADE FAILED DUE TO TRAILING EDGE IMPACT DAMSDR 95UAL737071Uplock Switch · malfunctionedON GEAR RETRACTION THE RIGHT GEAR RED LIGHT ILLUMINATED WITH GEAR HANDLE UP OR OFF. CYCLED GEAR DOWN AND GOT THREE GREEN LIGHTS. RETRACTED GEAR AGAIN AND GOT RED LIGHT CONDITION, RETURNED TO ORD. REPLACED RIGHT MLG UPLOCK SENSORS. ALSO, REPLACED THE A8 RISDR AWXA9500287Eel Batt Charger · inoperativePHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY, OPS CHECK GOOD. (M)SDR 95UAL737064Connector · unmodifiedNUMBER ONE ENGINE SLOW TO SPOOL UP, ABORTED TAKEOFF. THE BACKSCHELL OF THE FILTER BYPASS SWITCH CONNECTOR WAS INTERFERING WITH THE THROTTLE LEVER ARM. MODIFIED FILTER BYPASS SWITCH CONNECTOR PER COA 9-9198. CHECKS OK.SDR 95UAL737057Fire Loop · shortedAT 17,000 FEET IN CLIMB, NUMBER 2 FIRE HANDLE FLICKERED INTERMITTENTLY AND EMITTED AN ARCING SOUND. SEEMED TO FLICKER MORE WITH THROTTLE MOVEMENT. FOUND M337 FIRE LOOP DETECTOR SHORTED INTERNALLY. REPLACED DETECTOR AND CORRODED CONNECTOR. CHECKS OK.SDR CAL950292Skin · crackedGSO - INSPECTION FOUND A 1 INCH CRACK EXTENDING BEYOND STOP HOLE IN RT WING UPPER SURFACE FIXED LEADING EDGE. THE ADJACENT SKIN AT O/B TRACK FOR NR 5 SLAT WAS WARPED. THE DAMAGED AREA WAS ROUTED OUT IAW SRM 57-30-4. REPAIR DOUBLER AND FILTER WERE FABRICATESDR 95UAL737053Hose · failed'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHT CAME ON AND HYDRAULIC QUANTITY READS ZERO. REPLACED FAILED 'A' SYSTEM HYDRAULIC HOSE. SERVICED RESERVOIR AND LEAKS CHECKS OK.SDR CAL950291Skin · crackedGSO - INSPECTION FOUND SEVERAL FASTENER HOLES CRACKED IN RT FUSELAGE SKIN AT BS 188 TO 251 BETWEEN WL 207 AND WL 234. THE CRACKS WERE ALL APPROXIMATELY .1 INCH LONG. THE CRACKED SKIN SECTIONS WERE CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSSDR 95UAL737052Wheel · failedON DEPARTURE, MAIN GEAR WHEEL AND TIRE ASSEMBLY SEPARATED FROM THE AIRCRAFT, RETURNED TO ORD. REPLACED MAIN GEAR INNER CYLINDER DUE TO POSSIBLE HEAT DAMAGE. REPLACED NUMBER ONE ANTI-SKID TRANSDUCER, NUMBER ONE AND TWO TIRE AND BRAKE ASSEMBLY. GEAR SWING CHESDR 95UAL737023Hyd Module · crackedAFTER TAKEOFF WITH GEAR AND FLAPS UP, FLIGHT CONTROL WARNING LIGHT AND STANDBY HYDRAULIC SYSTEM LOW QUANTITY LIGHT CAME ON. 'A' SYSTEM QUANTITY READ ONE GALLON. REPLACED HYDRAULIC STANDBY MODULAR PACKAGE DUE TO A CRACKED HOUSING. ALSO, REPLACED STANDBY PUMPSDR AWXA9400550Nr 5 Carbon Seal · deterioratedPHX - FLT 45 - CORRECTION TO SUPPLEMENTAL/CLOSED SDR DATED 95-02-09; ORIGINAL SDR DATED 94-08-24. LAS/LAX - ON CLIMB-OUT, NR 1 ENGINE HIGH OIL TEMP AND APU GENERATOR WENT OFF LINE. NR 1 GENERATOR PLACARDED INOPERATIVE. ACFT RETURNED TO GATE WITHOUT FURTHER SDR 95UAL737011Fire Light · illuminatedCREW REPORTS THAT DURING FLIGHT, NUMBER TWO ENGINE FIRE WARNING SOUNDED FOR TWO SECONDS AND WENT OFF. SOUNDED A SECOND TIME, SHUT DOWN ENGINE AND DISCHARGED THE BOTTLE. LANDED UNDER AMBER ALERT.
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