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 AU001065Connector · damaged(AUS) NR 1 GENERATOR HARNESS CONNECTOR D5124J AND WIRES W142-001-6,W142-002-6 AND W142-003-6 LOCATED AT WING DISCONNECT BURNT ANDDAMAGED DUE TO ARCING. SUSPECT CAUSED BY LOOSE CONTACTS DUE TOFAULTY MANUFACTURE AND POOR RELIABILITY OF CONNECTORS.SDR AU001086Structure · corroded(AUS) LEVEL 2 CORROSION INSPECTION CARRIED OUT IAW AD/B737/52 AMDT2.SDR AU000732Skin · cracked(AUS) FORWARD SERVICE DOOR CUTOUT CONTAINED SEVEN CRACKS PROPAGATING FROM RIVET HOLES IN THE FORWARD UPPER CORNER AND SIX OUT OF ROUND HOLES IN THE UPPER AFT CORNER. FOUND DURING EDDY CURRENTINSPECTION.SDR AU000704Skin · cracked(AUS) LT HORIZONTAL STABILISER LOWER SKIN CRACKED IN AREA OF CHEMICALLY MILLED EDGE BETWEEN STN 147.9 AND STN157.1 JUST FORWARD OF THE REAR SPAR. CRACK LENGTH 38.1MM (1.5IN). FOUND DURING EDDY CURRENT INSPECTION.SDR AU000703Skin · cracked(AUS) RT FORWARD SERVICE DOOR AFT LOWER CORNER OUTER SKIN CRACKED. CRACK LENGTH 13MM (0.51IN). FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-30-18B.SDR AU000762Control Cable · frayed(AUS) HORIZONTAL STABILISER TRIM CABLE HAD AN EXCESSIVE AMOUNT OF BROKEN STRANDS. APPROXIMATELY THIRTY STRANDS BROKEN IN A 609.6MM(24IN) LENGTH LOCATED IN THE EMPENNAGE AREA.SDR AU001021Skin · cracked(AUS) LT HORIZONTAL STABILISER LOWER SKIN CRACKED AT THE CHEMICALLY MILLED EDGE BETWEEN STN 156.00 AND STN 158.00. CRACK LENGTH 50.8MM(2IN).SDR AU001000Switch · faulty(AUS) AC POWER SELECTOR SWITCH (S3) ARCING INTERNALLY.SDR AU001022Bracket · cracked(AUS) RT NOSE LANDING GEAR DOOR FORWARD HINGE BRACKET CRACKED ACROSS WEB. CRACK LENGTH 23MM (0.905IN).SDR AU000763Bearing · failed(AUS) TRAILING EDGE HYDRAULIC FLAP DRIVE MOTOR DRIVE SHAFT BEARING FAILED.SDR AU000773Skin · cracked(AUS) FUSELAGE SKIN CRACKED ON THE LT SIDE JUST AFT OF THE WING LIGHT ASSEMBLY BETWEEN STN 500C AND STN 500D LOCATED ABOVE STRINGER NR 15. CRACK LENGTH APPROXIMATELY 50MM (1.96IN).SDR AU000768Intercostal · cracked(AUS) FUSELAGE INTERCOSTAL / STRINGER LOCATED AT S5L AT BS 303.9 CRACKED BOTH LONGITUDINALLY AND VERTICALLY.SDR AU001283Wire · damaged(AUS) KAPTON WIRES LOCATED IN REFUEL PANEL HAVE DAMAGED INSULATION ALLOWING THE WIRES TO BE EXPOSED.SDR AU000515Housing · cracked(AUS) LT INBOARD GROUND SPOILER OUTBOARD ACTUATOR HOUSING CRACKED.SDR WP012000B1305Stud · crackedFATIGUE CRACKS IN HOLE DETECTED DURING MAGNETIC INSPECTION.SDR AU000547Skin · corroded(AUS) LT WING LOWER SKIN CONTAINED INTERGRANNULAR CORROSION IN AN AREAADJACENT TO ACCESS PANEL 7204L. CORROSION EXTENDED FROM THE EDGEOF THE PANEL CUTOUT IN TWO LOCATIONS FOR APPROXIMATELY 25MM (1IN).SDR AU000546Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD WEB CRACKED AT RIGHT BUTTOCK LINE 5.7 AND WATERLINE 8.3. FOUND DURING EDDY CURRENT INSPECTION.SDR AU000348Bearing · failed(AUS) SYSTEM A HYDRAULIC PUMP FAILED INTERNALLY. SUSPECT CAUSED BY FAILED TRUNNION BEARINGS. METAL CONTAMINATION OF HYDRAULIC FILTERS.SDR AU000369Skin · cracked(AUS) RT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STABILISER STN 120.3 AND STN 129.5 LOCATED 38.1MM (1.5IN) FORWARD OF THE REAR SPAR. CRACK LENGTH 57.15MM (2.25IN).SDR AU000598Structure · corroded(AUS) LEVEL 2 CORROSION FOUND IN FUSELAGE STRUCTURE AS A RESULT OFAD/B737/52 AMDT 2.SDR AU000597Structure · corroded(AUS) LEVEL 2 CORROSION FOUND IN THE FUSELAGE STRUCTURE AS A RESULT OFAD/B737/52 AMDT 2.SDR AU000347Wire Rope · frayed(AUS) AFT SERVICE DOOR SLIDE RELEASE CABLE FRAYED IN THE LOOP WHERE ITATTACHES TO THE LATCH. FOUND DURING INSPECTION IAW AD/B737/42.SDR AU000382Fitting · cracked(AUS) RT MAIN LANDING GEAR BEAM OUTBOARD SUPPORT FITTING CRACKED. FOUND DURING EDDY CURRENT INSPECTION IAW SB B737-57-1216.SDR AU000975Connector · damaged(AUS) NR 2 PYLON HARNESS FIREWALL CONNECTOR DAMAGED DUE TO ARCING.SDR AU000596Nut · undertorqued(AUS) DURING PREFLIGHT INSPECTION, THE NR 4 BLOCKER DOOR WAS FOUND NOT FULLY STOWED ON THE NR 1 ENGINE I/B REVERSER COWL. INVESTIGATION THEN FOUND THE BLOCKER DOORS LOWER HINGE BOLT WAS MISSING ANDTHE UPPER BOLT WAS LOOSE. FURTHER INVESTIGATION FOUNDTHE NR 2 SDR AU000144Structure · corroded(AUS) LEVEL 2 CORROSION FOUND AS A RESULT OF AD/B737/52 AMDT6.SDR AU000942Plug · burned(AUS) AFT GALLEY NR 3 OVEN TIMER POWER PINS BURNT AT TIMER MODULE PLUG.SDR AU000059Housing · cracked(AUS) LH GROUND SPOILER OUTBOARD ACTUATOR HOUSING CRACKED.SDR AU000034Support Bracket · cracked(AUS) RIG AFT FLAP NR 2 ROLLER SUPPORT UPPER FLANGE CRACKED. CRACK LENGTH 76.2MM (3 INCHES).SDR AU990952Cable · frayed(AUS) CABIN DOOR ESCAPE SLIDE COVER LATCH RELEASE CABLES FRAYED. THE ESCAPE SLIDES AFFECTED WERE LOCATED AT DOORS R1, R2, AND L2.SDR AU990938Frame · cracked(AUS) FUSELAGE FRAME INNER CHORDS LOCATED AT FR 616 AND FR 639 LEFT CRACKED AT THE LOWER RIVET HOLES. FOUND DURING EDDY CURRENT INSPECTION.SDR AU991054Connector · loose(AUS) NR 2 ENGINE FIRE DETECTOR SYSTEM CONNECTOR PLUG D1208 LOOSE. FALSE FIRE WARNING RESULTED IN DISCHARGE OF BOTH FIRE BOTTLES.SDR AU990886Wire · failed(AUS) SYSTEM 'B' ELECTRIC HYDRAULIC PUMP OUTPUT PRESSURE LINE CHAFING ON POWER CABLE W0334 WIRE BUNDLE CAUSING SHORT CIRCUIT.SDR AU990680Hose · failed(AUS) RIGHT MAIN LANDING GEAR UPLOCK ACTUATOR HYDRAULIC HOSE FAILED ADJACENT TO THE END FITTING. LOSS OF SYSTEM 'A' HYDRAULIC FLUID. DRY RUNNING OF ELECTRICAL AND ENGINE DRIVEN HYDRAULIC PUMPS DAMAGED THE PUMPS.SDR AU990747Frame · cracked(AUS) LEFT FRAME INNER CHORD LOCATED AT FS 616 ABOVE THE CENTER FUEL TANK CRACKED IN LOWER RIVET HOLE. FOUND DURING EDDY CURRENT INSPECTION.SDR AU990961Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD RT SIDE CHORD RADIUS CRACKED AT FLOOR LEVEL. FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-10-39.SDR AU990738Piston Ring · cracked(AUS) RIGHT PRESSURE REGULATING AND SHUTOFF VALVE FAULTY. WORKSHOP INSPECTION FOUND THAT THE CONTROL PISTON RING SET WAS CRACKED AND THE ACTUATOR COVER PACKING WAS TORN.SDR AU990746Bearing · failed(AUS) NR 2 ENGINE NR 4 BEARING FAILED. SECONDARY DAMAGE TO HPC, HPT AND LPT MODULES. AFT SUMP CHIP DETECTOR HAD HEAVY CONTAMINATION.SDR AU990584Engine · malfunctioned(AUS) NR 2 ENGINE VIBRATION. INVESTIGATION FOUND OIL CONTAMINATION IN THE TAILPIPE AND METAL CONTAMINATION OF THE AFT SUMP CHIP DETECTOR.SDR AU991066Skin · cracked(AUS) RIGHT SERVICE DOOR AFT LOWER CORNER RADIUS CRACKED. CRACK LENGTH APPROXIMATELY 25.4 MM (1 INCH) RUNNING THROUGH TWO THICKNESSES OF SKIN. CRACK FOUND AFTER THE DOOR SCUFF PLATE WAS REMOVED.SDR AU990885Bearing · seized(AUS) NOSE LANDING GEAR MANUAL EXTENSION SYSTEM LEFT AND RIGHT TORQUE TUBE SUPPORT BEARINGS SEIZED. SUBMITTER SUSPECTED CAUSED BY LACK OF LUBRICATION CAUSED BY WASHING.SDR AU990960Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING AREAS: 1. FORWARD SIDE WEB - TWO CRACKS. 2. LOWER AFT SIDE WEB - TWO CRACKS. 3. VERTICAL CHORD AFT SIDE - ONE CRACK. 4. RT SIDE CHORD RADIUS - ONE CRACK FOUND DURING ULTRASONIC AND EDDY CURRESDR AU990555Door Sill · cracked(AUS) FORWARD SERVICE DOOR SILL LOWER AFT CORNER RADIUS CRACKED FROM EDGE CUTOUT THROUGH A FASTENER AND SCREW HOLE INTO ANOTHER FASTENER HOLE. CRACK LENGTH 69.85 MM (2.75 INCH).SDR AU990470Controller · malfunctioned(AUS) EXCESS CABIN ALTITUDE WARNING HORN ACTIVATED. SUSPECT FAULTY CABIN PRESSURE CONTROLLER.SDR AU990544Warning Light · illuminated(AUS) APU FIRE WARNING LIGHT ILLUMINATED. FIRE BOTTLE DISCHARGED AND WARNING LIGHT EXTINGUISHED. SEVERAL MINUTES LATER, THE WARNING LIGHT ACTIVATED AGAIN AND INTERMITTENTLY ACTIVATED FOR THE REMAINDER OF THE FLIGHT. INVESTIGATION COULD FIND NO CAUSE FOR THESDR AU990484Stringer · cracked(AUS) FUSELAGE STRINGER 18A LOCATED AT BS 727, LT AND RT SIDES CRACKED AT THE INBOARD HOLES. FOUND DURING EDDY CURRENT INSPECTION.SDR AU990463Stringer · cracked(AUS) FUSELAGE STRINGER 18A LOCATED ON BOTH LT AND RT SIDES AT BS 727 CRACKED AT THE INBOARD HOLES. FOUND DURING EDDY CURRENT INSPECTION.SDR AU990673Bulkhead · cracked(AUS) FWD PRESSURE BULKHEAD FWD AND AFT FACES CRACKED IN FOLLOWING AREAS: 1. 2 CRACKS IN BULKHEAD WEB ON FWD SIDE OF BULKHEAD. A. ONE CRACK BENEATH HORIZ STRAP IN WEB AT WL 218 OUTBOARD OF RBL 5.7. CRACK LENGTH 9.525 MM (0.375 INCH). B. CRACK UNDER INBOSDR AU990755Beam · cracked(AUS) STABILIZER CUT-OUT BEAMS IN FUSELAGE CONTAINED TWO CRACKS ON THE LT SIDE AND ONE CRACK ON THE RT SIDE. FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-30-10D.SDR AU990674Frame · cracked(AUS) FUSELAGE FRAME INNER CHORD LOCATED AT STN 616 LEFT CRACKED IN LOWER FASTENER HOLE AFT FACE. FOUND DURING EDDY CURRENT INSPECTION.
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