Boeing 737-322
Service difficulty reports · 4,751
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 = '737322' 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 = '737322' 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 2000UALA00660Pin · misinstalledDURING A ROUTINE MAINTENANCE VISIT, AS A RESULT OF BOEING TELEX M-7200-00-02474 REPORTING IMPROPER OXYGEN GENERATOR RELEASE PIN INSTALLATIONS. MECHANICS FOUND MULTIPLE GENERATORS WITH RELEASE PINS INSTALLED INCORRECTLY. CORRECTED RELEASE PIN INSTALLATIONS.SDR 2000UALA00732Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00630Altimeter · failedCABIN PRESSURE CAN NOT BE MAINTAINED. *S/D* FOUND FAILED CAPTAINS ALTIMETER. REPLACED CAPTAINS ALTIMETER.SDR 2000UALA00620Landing Gear · malfunctionedRED NOSE GEAR UNSAFE LIGHT ON AFTER GEAR EXTENSION. *S/D* THE FLIGHT CREW RESET CIRCUIT BREAKER C404 AND ALL NOSE GEAR INDICATIONS RETURNED TO NORMAL. MAINTENANCE PERSONNEL IN DENVER JACKED THE NOSE OF AIRCRAFT AND PERFORMED SEVERAL GEAR SWINGS AND A MANUALSDR 2000UALA00617Altimeter · failedUNCONTROLLED CABIN PRESS CLIMB AT 28K FT, DESCENDED TO 11K AND CONTROL RETURNED. *S/D* FOUND FAILED CAPTAINS ALTIMETER. REPLACED THE CAPTAINS ALTIMETER.SDR 2000UALA00621Fuel Cell · leakingSUSPECTED FUEL LOSS FROM NUMBER 2 MAIN TANK. *S/D* FOUND CENTER SHIELDED CONNECTOR SHIELD BROKEN ON NR 2 MAIN FUEL GAUGE. REPLACED SHIELDED SOCKET AND CENTER PIN. REPLACED FUEL BOOST PUMP AND LOW PRESSURE SWITCH. AIRCRAFT OPS CHECKED GOOD. FUEL PUMP P/N:SDR 2000UALA00614Engine · malfunctionedLOW FUEL FLOW INDICATION FOR THE NR 1 ENGINE. *S/D* THE ENGINE WAS REPLACED.SDR 2000UALA00597Engine · malfunctionedABNORMAL INDICATION ON NR 1 ENGINE. *S/D* THE ENGINE WAS REPLACED.SDR 2000UALA00769Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00767Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00582Indicator · failedLEADING EDGE AND TRAILING EDGE FLAPS WOULD NOT RETRACT. *S/D* REPLACED R123 FLAP ASYMMETRY SHUTOFF RELAY AND TRAILING EDGE FLAP POSITION INDICATOR. FLAP SLAT SYSTEM, OPS CHECKS NORMAL.SDR 2000UALA00764Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00742Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00556Loop · damagedRIGHT WING BODY OVERHEAT INDICATION. *S/D* REPLACED RIGHT HAND PYLON OVERHEAT LOOP M1204. SYSTEM OPERATION CHECKED NORMAL.SDR 2000UALA00766Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00731Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00552Control Unit · failedNR 1 ENGINE FLAME-OUT. *S/D* TROUBLESHOOTING ON THE GROUND SUGGESTED THAT THE AUTOTHROTTLE WAS THE CAUSE AND IT WAS REPLACED. THE FUEL PUMP AND MAIN ENGINE CONTROL WERE ALSO CHANGED AS A PRECAUTION. SUBSEQUENT ENGINE RUNS SHOWED ALL PARAMETERS WITHIN LIMITSDR 2000UALA00543Csd · failedNR 2 GENERATOR HAD LOW OIL PRESSURE AND WAS DISCONNECTED IN FLIGHT. *S/D* THE CONSTANT SPEED DRIVE AND FILTER WERE REPLACED AND BACKFLUSHED. THE OIL COOLER WAS ALSO REPLACED AS A PRECAUTION.SDR 2001UALA00638Control Rod · chafedRUDDER POWER CONTROL UNIT CONTROL ROD AFT END OUTBOARD SIDE CHAFED, WORN AND KINKED. *S/D* CONTROL ROD REPLACED WITH SERVICEABLE CONTROL ROD. OFF UNIT FOUND TO BE WITHIN LIMITS PER BOEING SERVICE LETTER 737-SL-27-098 WHICH WAS WRITTEN TO ADDRESS THIS ISSUE SDR 2000UALA00537Computer · malfunctionedGROUND PROXIMITY WARNING SYSTEM INDICATION. *S/D* REPLACED GROUND PROXIMITY WARNING SYSTEM COMPUTER (P/N: 965-0976-003-104-104) AND TESTED. PASSES WITH NO FAULTS.SDR 2000UALA00536Controller · failedCABIN PRESSURE LOSS. *S/D* REPLACED THE CABIN PRESSURE CONTROLLER.SDR 2000UALA00528Sensor · failedEQUIPMENT COOLING EXHAUST OFF LIGHT ILLUMINATED. *S/D* REPLACED EQUIPMENT COOLING EXHAUST LOW FLOW SENSOR.SDR 2000UALA00522Window · crackedCAPTAINS NR 1 WINDOW IS CRACKED. *S/D* REPLACED CRACKED WINDOW.SDR 2000UALA00516Circuit Breaker · failedLANDING GEAR INDICATION LIGHT INOPERATIVE. *S/D* REPLACED CIRCUIT BREAKER MASTER DIM SECTION 5.SDR 2000UALA00509Bushing · wornAIRFRAME VIBRATION. *S/D* LEFT ELEVATOR TAB INBOARD HINGE FITTING BEARING AND HARDWARE HAVE EXCESSIVE WEAR. REMOVED TAB, REPLACED MOST INBOARD HINGE BUSHINGS AND BOLT.SDR 2000UALA00506Control Box · failedRIGHT WING-BODY OVERHEAT DETECTION SYSTEM INOPERATIVE. *S/D* REPLACED COMPARTMENT OVERHEAT CONTROL UNIT, WING-BODY OVERHEAT DETECTION SYSTEM TEST NORMAL.SDR 2000UALA00478Ballast · odorELECTRICAL SMELL IN MIDDLE OF COACH CABIN. *S/D* REPLACED BALLAST AND BULB, OPS OK AND NO SMELL NOTED.SDR 2000UALA00468Pump · malfunctionedENGINE INDICATION PROBLEM. *S/D* REPLACED FUEL PUMP AND MAIN ENGINE CONTROL (MEC), PERFORMED ACCELERATION CHECK WITH ALL PARAMETERS NORMAL.SDR 2000UALA00466Circuit Breaker · pulledAUTOPILOT WILL NOT HOLD ALTITUDE AND SPEED TRIM FAIL LIGHT ILLUMINATED. *S/D* FOUND STAB TRIM CIRCUIT BREAKER PULLED. RESET STAB TRIM BREAKER AND ACCOMPLISHED DIGITAL FLIGHT CONTROL SYSTEM TESTS, ALL TESTS CHECKED NORMAL.SDR 2000UALA00462Blade · bird strikeABORTED TAKEOFF AT 120 KNOTS DUE TO A BIRD STRIKE IN THE NR 2 ENGINE. *S/D* REPLACED FAN BLADES.SDR 2000UALA00458Light · inoperativeEMERGENCY EXIT LIGHTING STRIP INOPERATIVE. REPLACED POWER SUPPLY.SDR 2000UALA00741Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00740Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00454Control Panel · failedAUTOPILOT MASTER CONTROL PANEL FAILED. *S/D* REPLACED AUTOPILOT MODE CONTROL PANEL. NO FURTHER FAILURES HAVE BEEN EXPERIENCED.SDR 2000UALA00452Safety Switch · failedLANDING GEAR WOULD NOT RETRACT. *S/D* FOUND SAFTEY SWITCH-AIR SENSING (S106) OPEN. REPLACED S106 SAFETY SWITCH, OPERATIONAL CHECK OK.SDR 2000UALA00431Iru · failedLOSS OF THE CAPTAINS INERTIAL REFERENCE SYSTEM. *S/D* REPLACED NR 1 DIGITAL TO ANALOG ADAPTER AND NR 1 INERTIAL REFERENCE UNIT. OPS CHECKED SYSTEM. DAA, P/N DG1035AB03. IRU, P/N HG1050AD05/AD04.SDR 2000UALA00416Sensor · failedNORMAL AND ALTERNATE EQUIPMENT COOLING WARNING LIGHTS ILLUMINATED. *S/D* M100 LOW FLOW INSTRUMENT COOLING SENSOR FAILED. REPLACED M100 LOW FLOW INSTRUMENT COOLING SENSOR.SDR 2000UALA00414Connector · damagedENGINE FIRE WARNING. *S/D* REPLACED CONNECTOR ON NR 1 ENGINE LT FAN COWL FIRE LOOP. FOUND CORE WIRING LOOSE AND CHAFING ON NR 2 ENGINE. REPAIRED AND SECURED WIRING ON NR 2 ENGINE.SDR 2000UALA00392Light · damagedEMERGENCY EXIT LIGHTING DAMAGE. SECURED EMERGENCY EXIT LIGHT STRIP.SDR 2000UALA00390Warning Light · illuminatedABORTED TAKEOFF AT 100 KNOTS AFTER THE PACK MASTER CAUTION LIGHT ILLUMINATED.SDR 2000UALA00399Connector · dirtyNR 1 THRUST REVERSER WOULD NOT DEPLOY. *S/D* CLEANED CANNON PLUGS ON HYDRAULIC MODULE. OPERATIONAL CHECKS OK.SDR 2000UALA00397Light · inoperativeFORWARD MAIN ENTRY DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. *S/D* THE TRAILING EDGE FLAP POSITION INDICATOR WAS REPLACED.SDR 2000UALA00389Rod · out of adjLANDING GEAR INDICATION PROBLEM. *S/D* ADJUSTED RIGHT HAND GEAR DOOR ACTUATION ROD. OPERATIONS CHECK GOOD.SDR 2000UALA00409Skin · tornA 36 X 4 INCH TEAR, 3 FEET BELOW DOOR 1 RIGHT. *S/D* FUSELAGE SKIN WAS DAMAGED BY GROUND SERVICE EQUIPMENT. REPAIRED SHEAR TIE AT BS 312, REFERENCE STRUCTURAL REPAIR MANUAL (SRM) 53-00-07. INSTALLED NEW FRAME SPLICE AT BS 328, REFERENCE SRM 51-70-11. REPASDR 2000UALA00355Indicator · failedFLAPS LOCKED UP AT POSITION ONE. *S/D* THE TRAILING EDGE FLAPS POSITION INDICATOR WAS REPLACED. THE AIRCRAFT HAS NOT HAD ANY FLAP PROBLEMS SINCE THE REPLACEMENT OF THE INDICATOR.SDR 2000UALA00354Panel · failedTHE MASTER CONTROL PANEL WENT INOPERATIVE, ALL WINDOWS SHOW 8''S. BOTH AUTOPILOTS, FLIGHT DIRECTORS, AND NR 1 VOR COURSE INFORMATION IS INOPERATIVE. *S/D* REPLACED MODE CONTROL PANEL. OPERATIONAL TESTS NORMAL.SDR 2000UALA00353Bearing · failedNUMBER 2 ENGINE STALLING AT CRUISE POWER SETTING OF 88 PERCENT N1. NUMBER 2 ENGINE CONTINUED TO STALL UNTIL POWER SETTING WAS RETURNED TO IDLE. *S/D* REPLACED NR 2 ENGINE. SHOP FINDINGS CONFIRMED A NR 4 BEARING FAILURE.SDR 2000UALA00347Coupling · malfunctionedSIDE TO SIDE MOTION OCCURRED AFTER TAKEOFF. MOTION CONTINUED DURING TURN, CLIMB AND CRUISE PHASES OF FLIGHT. *S/D* REPLACED YAW DAMPER COUPLER AND THE NR 2 MAIN ENGINE CONTROL.SDR 2000UALA00343Sensor · out of adjFORWARD CARGO DOOR OPEN LIGHT CAME ON AT ROTATION. *S/D* FOUND TARGET NOT MAKING CORRECT CONTACT. ADJUSTED TARGET. NO HISTORY, NO ADDITIONAL OCCURRENCES AFTER TARGET ADJUSTED.SDR 2000UALA00328Sensor · malfunctionedYELLOW LEADING EDGE FLAP TRANSIT LIGHT REMAINED ON AND LEFT INBOARD FLAP INDICATOR GREEN LIGHT ON. EXCEEDED 230KTS BY 5-10 KTS. *S/D* REPLACED LEADING EDGE FLAP NUMBER 2 EXTEND SENSOR, S171, PER AMM 27-8 8-11.
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