Boeing 737-377
Service difficulty reports · 223
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 = '737377' 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 = '737377' 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 AU980801Link · worn(AUS) PASSENGER SEAT 8A RECLINE LIMIT LINK WORN.SDR AU981300Harness · faulty(AUS) NR 2 ENGINE EGT WIRING HARNESS FAULTY. HARNESS FAILED THE `WET INSULATION' TEST IN THE WORKSHOP AFTER REMOVAL.SDR AU980602Connector · shorted(AUS) APU FIRE DETECTOR LOOP CONNECTOR SHORT CIRCUITED BETWEEN THE CENTER PIN AND THE OUTER SHELL. FALSE APU FIRE WARNING RESULTED IN THE FIRE BOTTLE BEING DISCHARGED.SDR AU980984Stud · fractured(AUS) LT OUTBOARD NR 1 LEADING EDGE SLAT ACTUATOR STUD LOCKING ASSEMBLY END FITTING FRACTURED AND JAMMED UNDER THE HEAD OF THE INNER PISTON P\N 65-44757-1 AND THE END OF THE TRANSFER TUBE P\N 65-44768-1 PREVENTING CORRECT OPERATION OF THE ACTUATOR. PART TC: SDR AU980668Press Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB FORWARD FACE CONTAINED A TOTAL OF FIVE CRACKS. A CRACK WAS ALSO FOUND IN THE RADIUS OF THE VERTICAL CHORD OF THE BULKHEAD AT LBL 5.7 LEVEL WITH THE HORIZONTAL STIFFENER AT WL 184. FOUND DURING EDDY CURRENT INSPECTION IAW ESDR AU980986Valve · leaking(AUS) FORWARD TOILET DRAIN VALVE LEAKING DURING VACUUM TEST IAW ERB73-38-11 PT2. PART TC: 3,325.SDR AU980716Connector · contaminated(AUS) APU FIRE DETECTOR FAULTY. INVESTIGATION FOUND OIL IN THE CONNECTOR BODY.SDR AU980537Window · cracked(AUS) RT EMERGENCY EXIT HATCH WINDOW OUTER PANEL DELAMINATED AND CRACKED FROM THE LOWER FORWARD CORNER VERTICALLY UP THE REAR EDGE TO THE TOP REAR CORNER.SDR AU980576Bearing · failed(AUS) LT AIR CONDITIONING SYSTEM AIR CYCLE MACHINE FAILED. SUSPECT CAUSED BY FAILURE OF THE AIR CYCLE MACHINE COMPRESSOR BEARING CAUSING THE ACM TO SEIZE. THE RT RAM AIR CONTROL MODULE P\N 607518-2 FAILED SHORTLY AFTER DUE TO BREAKING DOWN OF THE THRISTOR CRSDR AU980533Control Cable · frayed(AUS) WING FLIGHT SPOILER CABLES CONTAINED BROKEN STRANDS IN THE AREA ADJACENT TO PULLEY AT STN 230: LT WS B1-3, P/N BACC2A3A02794EG. WS B2-3, P/N BACC2A3A03216FG. WS A2-3, P/N BACC2A3A01853FG. WS A1-3, P/N BACC2A3A02428EG. RT WS B1-4, P/N BACC2A3A02625FGSDR AU980179Control Cable · frayed(AUS) WING FLIGHT SPOILER CABLES FRAYED AT WING STN 230:- 1. CABLE PNO BACC2A3A03216FG LOCATED AT LH WSB2-3 2. CABLE PNO BACC2A3A02794EG LOCATED AT LH WSB1-3 3. CABLE PNO BACC2A3A03051FG LOCATED AT RH WSB2-4 FOUND DURING SPECIAL INSPECTION IAW B737-3-97A.SDR AU980171Control Cable · worn(AUS) WING FLIGHT SPOILER CABLE LOCATED RH SIDE AT WSB2-4 AT WS136 PULLEY WORN BEYOND LIMITS. FOUND DURING SPECIAL INSPECTIONB737-3-97A.SDR AU980052Control Cable · frayed(AUS) FLIGHT SPOILER CABLES (3OFF) LOCATED IN RH WING ADJACENT TO STN 230 CONTAINED BROKEN STRANDS. FOUND DURING INSPECTION IAW SPECIAL INSPECTION B737/3/97A.SDR AU980170Control Cable · damaged(AUS) WING FLIGHT SPOILER CABLES FRAYED. CABLES LOCATED IN THE FOLLOWING POSITIONS:- 1. CABLE PNO BACC2A3A02794EG AT LH WSB1-3 2. CABLE PNO BACC2A3A03216FG AT LH WSB2-3 3. CABLE PNO BACC2A3A03051FG AT RH WSB2-4 4. CABLE PNO BACC2A3A02652FG AT RH WSB1-3 FOUND DSDR AU980180Control Cable · frayed(AUS) WING FLIGHT SPOILER CABLES FRAYED AT WING STN 230 IN THE FOLLOWING LOCATIONS:- 1. CABLE PNO BACC2A3A02794EG LOCATED AT LH WSB1-32. CABLE PNO BACC2A3A02625FG LOCATED AT RH WSB1-43. CABLE PNO BACC2A3A03051FG LOCATED AT RH WSB2-4FOUND DURING SPECIAL INSPECTSDR AU980172Control Cable · worn(AUS) FLIGHT SPOILER CABLES WORN BEYOND LIMITS. CABLES LOCATED IN THE FOLLOWING POSITIONS AT LH WING REAR SPAR STN 210:-1. CABLE PNO BACC2C3D02428EG AT WSA1-32. CABLE PNO BACC2C3D01853FG AT WSA2-3FOUND DURING SPECIAL INSPECTION MSI-B737-3-97A.SDR AU980062Control Cable · frayed(AUS) LH AND RH WING SPOILER CABLES FRAYED. CABLES AFFECTED, PNO WSB1-4 AND PNO WSB2-4 IN RH WING AND PNO WSB2-3 AND PNO WSB1-3 IN LH WING.SDR AU980010Seat · worn(AUS) SEAT 8G WORN. THE SEAT WAS OBSTRUCTING THE OVERWING EXIT WHEN INTHE UPRIGHT POSITION.SDR AU971640Control Cable · broken(AUS) NO6 FLIGHT SPOILER CABLE WSB2-4 FAILED ADJACENT TO THE PULLEYS AT RH WING STN 230 AT WBL157.0. EVIDENCE OF ADVANCED INTERNALCORROSION.SDR AU971611Cable · broken(AUS) AFT ENTRY DOOR ESCAPE SLIDE COVER RELEASE CABLE BROKEN IN LOOP AT THE GIRT BAT ATTACHMENT END.SDR AU971612Skin · cracked(AUS) RH C-D FLIGHT COMPARTMENT WINDOW POST UPPER GUSSET SKIN CRACKED.CRACK LENGTH 3.175MM (0.125IN). FOUND DURING EDDY CURRENT INSPECTION.SDR AU971604Lock · faulty(AUS) LH INBOARD THRUST REVERSER SYNCH LOCK FAULTY. WORKSHOP TESTING COULD FIND NO MALFUNCTION.SDR AU971363Engine · failed(AUS) NO2 ENGINE HAD HIGH VIBRATION AND HIGH EGT. FORWARD SUMP CHIP DETECTOR CONTAINED A SMALL AMOUNT OF METAL AND STATIONARY BEARING MATERIAL.SDR AU971540Sensor · failed(AUS) RH AIR CONDITIONING PACK RAM AIR TEMPERATURE SENSOR OPEN CIRCUITED CAUSING THE RAM AIR DOOR AND OUTLET LOUVRES TO CLOSE AND LIMIT COOLING AIR OVER PRIMARY AND SECONDARY HEAT EXCHANGERS.SDR AU971603Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING LOCATIONS:-1. THREE CRACKS IN THE BULKHEAD WEB BETWEEN LBL 5.7 AND RBL 5.7 LOCATED UNDER THE RADAR SCANNER MOUNTING BRACKETS - CRACK LENGTHS 24MM (0.944IN) - 14MM (0.551IN) - 13MM (0.511IN) 2. CRACK IN SDR AU971425Tire · failed(AUS) BOTH LH MAIN WHEEL TYRES FAILED. SUSPECT NO1 OUTBOARD TYRE FAILED FIRST DUE TO FOD. NO2 TYRE THEN FAILED DUE TO HIGH ENERGY BRAKING COMBINED WITH RAPID DECELERATION. DAMAGE TO FLAPS, MLG DOORS AND BRAKE LINES. SMALL AMOUNTS OF TYRE DEBRIS ALSO ENTERED THSDR AU971539Web · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB CRACKED IN SEVEN PLACES:- A. AREA UNDER THE RADAR SCANNING MOUNTING BRACKETS CONTAINED FOUR CRACKS BETWEEN LBL 5.5 AND RBL 5.7 - CRACK LENGTHS 27MM (1.06IN), 13MM (0.5IN) AND TWO CRACKS OF 16MM (0.630IN)B. TWO CRACKS EITHERSDR AU971237Tire · separated(AUS) LH NOSEWHEEL TYRE TREAD SEPARATED. DAMAGE TO LH FRONT CORNER OF E & E BAY DOOR.SDR AU970941Frame · cracked(AUS) FORWARD CARGO DOOR FRAME CRACKED AT DOOR FRAME RADIUS FROM LOWERAFT CORNER AND RUNNING UP THE AFT SIDE OF THE DOOR - CRACK LENGTH APPROXIMATELY 210MM (9IN) - INVESTIGATION FOUND FURTHER CRACKING IN THE FOLLOWING LOCATIONS:-1. HORIZONTAL CROSS BEAM ATTACHSDR AU970717Chord · cracked(AUS) FORWARD PRESSURE BULKHEAD LH SIDE CHORD CRACKED IN RADIUS AT WL 207 - CRACK LENGTH 40MM (1.574IN) AND WL 195 - CRACK LENGTH 51.5MM (2.027IN) - FOUND DURING INSPECTION IAW ER B73-53-10-39SDR AU970715Arm · cracked(AUS) LH FOREFLAP SUPPORT ARM CRACKED THROUGH BOLT HOLESDR AU970826Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD AT STATION 178 CRACKED IN SIXPLACES - FOUND USING EDDY CURRENT AND ULTRASONIC INSPECTIONS IAWER B73-53-10-39ASDR AU970937Computer · malfunctioned(AUS) ELEVATOR FEEL COMPUTER SUSPECT FAULTY - WORKSHOP INVESTIGATIONCOULD FIND NO DEFECTSSDR AU970829Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD WEB CRACKED IN FIVE PLACES - FOUND DURING EDDY CURRENT AND ULTRASONIC INSPECTION IAW ERB73-53-10-39ASDR AU970828Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING AREAS:-1. LH FORWARD PRESSURE BULKHEAD SIDE CHORD RADIUS AT WL 195 - CRACK LENGTH 63.5MM (2.5IN)2. LH INTERCOSTAL ADJACENT TO BULKHEAD AT WL 1953. RH INTERCOSTAL ADJACENT TO BULKHEAD AT WL 195SDR AU970718Post · cracked(AUS) LH AND RH C-D WINDOW POSTS CRACKED IN UPPER CORNERS - FOUND DURING EDDY CURRENT INSPECTIONSDR AU970714Post · cracked(AUS) WINDOW POSTS C-D CRACKED IN THE FOLLOWING AREAS:- 1. LH SIDE - CRACK LENGTH 20MM (0.787IN)2. RH SIDE - CRACK LENGTH 40MM (1.574IN)FOUND DURING EDDY CURRENT INSPECTIONSDR AU971224Fire Detector · faulty(AUS) APU FALSE FIRE WARNING. SUSPECT CAUSED BY MOISTURE IN FIREDETECTOR SYSTEM.SDR AU970638Seal · damaged(AUS) APU PNEUMATIC DUCT SEAL IN AFT PRESSURE BULKHEAD TORN.SDR AU970642Cable · frayed(AUS) FORWARD ENTRY DOOR ESCAPE SLIDE LATCH CABLE FRAYED IN AREA OF SWAGED BALL END TERMINALSDR AU970544Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED AT SIDE CHORD RADIUS LH SIDE AT WL207 - CRACK LENGTH APPROXIMATELY 76.2MM (3IN)SDR AU970641Web · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB CONTAINED THREE CRACKS IN AREA BELOW THE RADAR SCANNING MOUNTING BRACKETS - TWO CRACKS LOCATED AT LBL 5.7 - ONE CRACK LOCATED AT RBL 5.7 - CRACK LENGTHS 10MM(0.393IN) - FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-10-3SDR AU970825Post · cracked(AUS) LH NO1 WINDOW POST CRACKED IN OUTBOARD UPPER CORNER - FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-10-36SDR AU970499Bearing · failed(AUS) HYDRAULIC `B' SYSTEM ELECTRIC PUMP TRUNNION BEARINGS FAILED.DAMAGE CAUSED TO PUMP ROTATING GROUP, PUMP HOUSING AND ELECTRIC MOTOR.SDR AU970411Seat · worn(AUS) SEATS 8A AND 8G BLOCKING OFF EMERGENCY EXIT WHEN IN UPRIGHT POSITION DUE TO WEARSDR AU970637Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING AREAS:-1. FORWARD FACE OF BULKHEAD WEB CONTAINED THREE CRACKS IN AREA BELOW RADAR SCANNING MOUNTING BRACKETS AT RBL 5.7 - CRACK LENGTHS 15MM (0.59IN) - 14MM (0.55IN) AND 3MM (0.118IN) - FOUND USING ULTRASDR AU970498Coalescer Bag · dirty(AUS) LH AIRCONDITIONING PACK WATER SEPARATOR COALESCER BAG DIRTYSDR AU970302Diode · shorted(AUS) GENERATOR CONTROL UNIT FAULTY - INVESTIGATION FOUND DIODE CR907 SHORT CIRCUITED ALLOWING TRANSFORMER T901 TO OVERHEATSDR AU970186Turbine · damaged(AUS) APU TURBINE BUCKLED AND WHEEL PROTRUDED THROUGH ENGINE CASING - DAMAGE TO GEARBOX AREA - RH ENGINE MOUNT SHATTEREDSDR AU970187Control Valve · seized(AUS) RH AIR CONDITIONING PACK, SINGLE PACK OPERATION MARGINAL - LH AIR CONDITIONING SYSTEM FAULTY DUE TO 35 DEGREE CONTROL VALVE PNO321942-1-1 BEING SEIZED IN CLOSED POSITION WITH SHAFT SHEARED AND LH TEMPERATURE CONTROL VALVE PNO 398116-1-1 HAVING LIMITED M
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