Boeing 737-476
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 = '737476' 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 = '737476' 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 AUS20040086Actuator · faulty(AUS) STABILIZER TRIM ACTUATOR FAULTY.SDR AUS20040028Trim Tab · loose(AUS) ELEVATOR TAB FREE PLAY EXCEEDED MAXIMUM LIMIT OF 0.9144MM (0.036IN). FREE PLAY MEASURED 1.143MM (0.045IN). FOUND DURING INSPECTION IAW AD/B737/175 AND EI 737-55-12R5.SDR AUS20040014Proximity Switch · faulty(AUS) NR 3 LEADING EDGE SLAT PROXIMITY SWITCH FAULTY.SDR AUS20040004Control Panel · failed(AUS) AUTOPILOT MODE CONTROL PANEL FAILED.SDR AUS20031306Windshield · cracked(AUS) FIRST OFFICERS NR 1 WINDOW CRACKED IN OUTER PANE. CRACKING APPEARS TO ORIGINATE FROM DELAMINATION AT TOP LT AREA OF WINDOW.SDR AUS20031339Bolt · sheared(AUS) RT MAIN LANDING GEAR OUTBOARD WHEEL TIE BOLT SHEARED IN THREADED SECTION.SDR AUS20031226Check Valve · cracked(AUS) CENTER FUEL TANK RT BOOST PUMP DISCHARGE CHECK VALVE BODY CRACKED. CRACK LENGTH APPROXIMATELY 31.75MM (1.25IN).SDR AUS20031237Frame · cracked(AUS) FUSELAGE FRAME AFT CHORD HOLES (3OFF) CRACKED. AFT WEB HOLE CRACKED. FOUND DURING EDDY CURRENT INSPECTION IAW MFG DRAWING737R53-154-01.SDR AUS20031128Slide · twisted(AUS) DOOR R1 ESCAPE SLIDE TWISTED DURING DEPLOYMENT.SDR AUS20031065Warning System · overheated(AUS) RT WING BODY OVERHEAT LIGHT ILLUMINATED. LIMITED INFORMATION PROVIDED.SDR AUS20031058Engine · erratic(AUS) NR 1 ENGINE EGT REACHED AT LEAST 1100 TO 1200 DEGREES AND WAS ERRATIC. ALL OTHER INDICATIONS NORMAL.SDR AUS20031075Cable · wrong part(AUS) RT ENGINE THRUST LEVER STIFF IN OPERATION. INVESTIGATION FOUND INCORRECT CABLE FITTED. CABLE WAS APPROXIMATELY 120MM (4.72IN)LONGER THAN THE CORRECT CABLE. FURTHER INSPECTION ALSO FOUND CABLE JAMMING ON THE INTERNAL TEFLON SURFACE. UNAPPROVED PART. PESDR AUS20031041Structure · damaged(AUS) LT MAIN LANDING GEAR DOOR DAMAGED. FURTHER INVESTIGATION FOUND LT MAIN LANDING GEAR BRAKE SWIVEL BRACKET AND OUTER DOOR ATTACHMENT FITTING LOOSE WITH TWO BOLTS SHEARED AND ANOTHER TWO BOLTS LOOSE.SDR AUS20031040Plate · separated(AUS) RT INBOARD FLAP INBOARD SEAL PLATE SEPARATED.SDR AUS20031161Rib · cracked(AUS) WING RIB LOCATED AT WBL 135.5 CRACKED AT LOWER CUT-OUT FOR STR 1 ON RT SIDE. CRACK LENGTH 25.4MM (1IN). FOUND DURING EDDY CURRENT INSPECTION.SDR AUS20031160Stringer · cracked(AUS) STRINGER CRACKED AT RIVET HOLE LOCATED FORWARD OF FRAME 328. CRACK LENGTH APPROXIMATELY 0.0254MM (0.1IN). FOUND DURING EDDY CURRENT INSPECTION.SDR AUS20031027Turbine Blades · cracked(AUS) NUMEROUS HPT BLADE CRACKS (RADIAL TIP CRACK TURNING AXIAL) WERE FOUND WITH THE POTENTIAL FOR BLADE TIP CORNER SEPARATION. FOUND DURING ROUTINE BOROSCOPE INSPECTION.SDR AUS20031009Roller · faulty(AUS) DOOR L1 HAD THE LATCHING ROLLERS OUTSIDE OF THE LATCHING CAM WITH THE DOOR CLOSED.SDR AUS20031005Connector · burned(AUS) NR 1 GENERATOR DISCONNECT PLUG CONNECTOR BURNT.SDR AUS20031004Gcu · faulty(AUS) APU GENERATOR CONTROL UNIT (GCU) FAULTY.SDR AUS20031002Hose · damaged(AUS) PASSENGER SERVICE UNIT (PSU) OXYGEN HOSE SEVERED AT OXYGEN GENERATOR FITTING ON THE PSU.SDR AUS20031001Anti-Ice System · faulty(AUS) RT WING ANTI-ICE SYSTEM OPERATING WITH ANTI-ICE SWITCH IN THE OFF POSITION.SDR AUS20031057Bolt · cracked(AUS) NR 2 ENGINE MOUNTING SYSTEM FORWARD MOUNT CONE BOLT CRACKED. FOUND DURING NDT INSPECTION.SDR AUS20030991Fitting · split(AUS) NR 2 ENGINE HYDRAULIC PUMP PRESSURE LINE QUICK DISCONNECT FITTING SPLIT.SDR AUS20030989Line · leaking(AUS) NR 1 ENGINE FUEL FEED LINE FROM FRONT SPAR TO PYLON LEAKING. LINE WAS WORN IN AREA OF O RING SEAL.SDR AUS20030988Control Unit · faulty(AUS) ELEVATOR FEEL AND CENTERING UNIT SPRING BROKEN.SDR AUS20030986Fan Blade · cracked(AUS) NR 2 ENGINE FAN BLADE FRACTURE SURFACE CONTAINED EVIDENCE OF FATIGUE CRACKING. ENGINE AND FAN BLADE HAD BEEN INVOLVED IN A BAT STRIKE AND THE ENGINE HAD BEEN REMOVED FOR WORKSHOP INSPECTION.SDR AUS20030916Plug · loose(AUS) FUEL CROSSFEED VALVE PLUG LOOSE.SDR AUS20030899Tire · failed(AUS) RT NOSE WHEEL TIRE BLOWN OUT. LT TIRE FAILED DUE TO OVERLOAD.SDR AUS20030878Control Panel · faulty(AUS) ATC TRANSPONDER CONTROL PANEL FAULTY. PANEL WAS FOUND TO BE EXCESSIVELY HOT TO TOUCH.SDR AUS20030780Latch · unlocked(AUS) DOOR L1 HANDLE MOVED UP CAUSING AIR NOISE DURING FLIGHT. HANDLE MOVED ON SEVERAL OCCASIONS. SUSPECT CAUSED BY INCORRECT RIGGING/ADJUSTMENT.SDR AUS20030771Window · faulty(AUS) FLIGHT DECK SLIDING WINDOW 2R FAILED THE EMERGENCY RELEASE TEST. INVESTIGATION FOUND THE CAUSE OF THE PROBLEM WAS EITHER LACK OF LUBRICANT OR ADJUSTMENT OF THE WINDOW.SDR AUS20030746Controller · faulty(AUS) LT SIDE WINDOW OVERHEAT INDICATION. WINDOW HEAT TURNED OFF, BUT LIGHT STAYED ON. SUSPECT FAULTY & INTERMITTENT WINDOW HEAT CONTROLLER.SDR AUS20030712Fitting · cracked(AUS) NR 1 ENGINE HYDRAULIC SYSTEM FIREWALL QUICK DISCONNECT FITTING CRACKED. LOSS OF A-SYSTEM HYDRAULIC FLUID.SDR AUS20030762Actuator · faulty(AUS) HORIZONTAL STABILISER TRIM ACTUATOR FAULTY.SDR AUS20030619Throttle · faulty(AUS) NR 1 ENGINE AUTO-THROTTLE DISENGAGED AND SUBSEQUENTLY RE-ENGAGED. ENGINE PARAMETERS FLUCTUATED FROM 70 PERCENT N1 TO APPROXIMATELY 107 PERCENT N1 WITH WARNING LIGHT ILLUMINATION.SDR AUS20030639Symbol Generator · failed(AUS) NR 1 SYMBOL GENERATOR FAILED.SDR AUS20030534Connector · dirty(AUS) NR 1 ENGINE FIRE DETECTION SYSTEM FAULTY. SUSPECT CAUSED BY DIRTY CONNECTOR.SDR AUS20030507Seat · loose(AUS) PASSENGER SEAT 1A-C OUTBOARD LEG ADRIFT FROM SEAT TRACK.SDR AUS20030424Trim Panel · faulty(AUS) STABILISER TRIM SYSTEM FAULTY. HORIZONTAL STABILISER MAIN TRIMACTUATOR AND HORIZONTAL STABILISER TRIM RELAY R64 REPLACED.SDR AUS20030388Lever · jammed(AUS) NR 2 ENGINE THRUST REVERSER LEVER JAMMED.SDR AUS20030339Engine · failed(AUS) NR 2 ENGINE FAILED. DURING CLIMB A LOUD THUD WAS HEARD AND A PASSENGER REPORTED A LARGE FIREBALL. ENGINE INDICATIONS WERE NORMAL.SDR AUS20030316Csd · failed(AUS) NR 1 ENGINE CONSTANT SPEED DRIVE (CSD) INPUT DRIVESHAFT SPLINE DISENGAGED DUE TO RETAINING RING AND SPACER COMING ADRIFT.SDR AUS20021443Door · cracked(AUS) FORWARD CARGO DOOR CRACKED IN FORWARD AND AFT LOWER CORNERS ASWELL AS THE LOWER CORNER OUTER T' CHORD. FOUND DURING EDDY CURRENT INSPECTION IAW AD/B737/142 AND EI 737-52-3.SDR AUS20021353Pushrod · broken(AUS) CABIN DOOR R2 JAMMED CLOSED. INVESTIGATION FOUND THE LOWER DOOR PUSHROD BROKEN.SDR AUS20021346Warning Light · false activation(AUS) APU FIRE WARNING. FIRE BOTTLE DISCHARGED. INSPECTION FOUND NO EVIDENCE OF FIRE.SDR AUS20021318Seat · misinstalled(AUS) SEATS LOCATED AT ROW 10A AND 10F PARTIALLY BLOCKING EMERGENCY EXITS. PERSONNEL/MAINTENANCE ERROR.SDR AUS20021282Flap · damaged(AUS) LH INBOARD MID FLAP UPPER SKIN DAMAGED. A SECTION OF METAL SKIN MEASURING APPROXIMATELY 150MM (5.9IN) BY 250MM (9.84IN) WAS MISSING.SDR AUS20021245Charger · faulty(AUS) BATTERY CHARGER HOT AND EMITTING ELECTRICAL ODOURS.SDR AUS20021281Valve · faulty(AUS) FUEL TRANSFER SYSTEM CHECK VALVE FAULTY.
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