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 AU990397Apu · fire(AUS) APU FIRE. DAMAGE WAS FOUND AROUND THE EGT THERMOCOUPLE AND WIRING AND EVIDENCE OF DAMAGE IN THE LOWER EXHAUST SHROUD AREA ADJACENT TO THE EGT HARNESS.SDR AU990527Stringer · cracked(AUS) STRINGER 18A WEB LOCATED AT BS 727 CRACKED FROM THE LT AND RT SIDE AFT INBOARD FASTENER HOLES. FOUND DURING EDDY CURRENT INSPECTION.SDR AU990502Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING LOCATIONS: 1. VERTICAL CHORD AT LBL 5.7 WL 184 - CRACK LENGTH 35 MM (1.377 INCH) IN INBOARD RADIUS AND 14 MM (0.551 INCH) IN OUTBOARD RADIUS. 2. WEB ON FORWARD FACE AT WL 218 LOCATED 90 MM (3.543 INCSDR AU990462Stringer · cracked(AUS) FUSELAGE STRINGER 18A WEB LOCATED AT BS 727 CRACKED AT THE AFT INBOARD FASTENER HOLES ON THE LT AND RT SIDES. FOUND DURING EDDY CURRENT INSPECTION.SDR AU990406Window · cracked(AUS) CAPTAIN'S NR 1 WINDOW OUTER PANE CRACKED IN NUMEROUS LOCATIONS. CRACKING ORIGINATED FROM LIGHT BURN MARKS NEAR THE UPPER EDGE OF THE WINDOW.SDR AU990506Frame · cracked(AUS) LT FUSELAGE FRAME INNER CHORD LOCATED AT STS 639 CRACKED DOWNWARDS FROM THE LOWER FASTENER HOLE. FOUND DURING EDDY CURRENT INSPECTION.SDR AU990486Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD LOCATED AT STA 178 CRACKED IN THE FOLLOWING LOCATIONS: 1. CRACK LOCATED ON THE INBOARD SIDE RADIUS OF THE LT VERTICAL CHORD (LBL 5.7) AND WL184 ON THE AFT SIDE OF THE BULKHEAD - CRACK LENGTH 9.525 MM (0.375 INCH). 2. CRACKSDR AU990436Stringer · cracked(AUS) STRINGER 18A WEB CRACKED FROM THE INBOARD HOLE AT BULKHEAD ATTACHMENT LOCATED AT BS 727 RT SIDE. FOUND DURING EDDY CURRENT INSPECTION.SDR AU990489Structure · damaged(AUS) AIRCRAFT SUFFERED HAIL DAMAGE IN THE FOLLOWING LOCATIONS: 1. LT AILERON AND LT AND RT AILERON TAB. 2. LT AND RT ELEVATOR. 3. SPOILERS. 4. RUDDER.SDR AU990452Structure · damaged(AUS) AIRCRAFT SUFFERED HAIL DAMAGE TO THE FOLLOWING AREAS: 1. LT AND RT AILERONS. 2. RT AILERON TRIM TAB. 3. LT AND RT ELEVATORS. 4. LT AND RT HORIZONTAL STABILIZERS. 5. SPOILERS. 6. RUDDER.SDR AU990435Frame · cracked(AUS) FUSELAGE INNER CHORD LOCATED AT BS 616 LT CRACKED THROUGH THE LOWER FASTENER HOLE. FOUND DURING EDDY CURRENT INSPECTION.SDR AU990370Cable · frayed(AUS) BOTH AFT DOOR ESCAPE SLIDE COVER RELEASE CABLES FRAYED AND CORRODED. FOUND DURING INSPECTION IAW AD/B737/042.SDR AU990356Valve · sticking(AUS) FORWARD CABIN OUTFLOW VALVE STICKING IN THE `OPEN' POSITION.SDR AU990389Bearing · contaminated(AUS) AILERON FEEL, CENTERING AND TRIM MECHANISM SUPPORT BEARINGS CONTAMINATED WITH DIRT AND GRIT.SDR AU990551Connector · damaged(AUS) NR 2 OVEN CONTROLLER CONNECTOR SOCKET AND PINS HAD ARCING DAMAGE. SEE ALSO MDR AU990550.SDR AU990550Connector · damaged(AUS) NR 2 OVEN CONNECTOR SOCKETS AND CONTROLLER CONNECTOR PINS HAD ARCING DAMAGE.SDR AU990409Connector · damaged(AUS) NR 2 ENGINE GENERATOR LEAD PHASE `B' PIN AND SOCKET ON CONNECTOR D5126P/J FAULTY. PHASE `B' PIN CABLE W144-002-06 DAMAGED FOR APPROXIMATELY 50.8 MM (2 INCHES).SDR AU990300Bulkhead · cracked(AUS) FORWARD FUSELAGE BULKHEAD CRACKED IN THE FOLLOWING AREAS: 1. BULKHEAD WEB LOCATED ADJACENT TO THE RIGHT LOWER RADAR ANTENNA MOUNT INBOARD UPPER CORNER - CRACK LENGTH 6 MM (0.236 INCH). 2. SIDE CHORD ANGLE LOCATED AT WL 207 LT SIDE AND WL 195 LT SIDE SDR AU990102Connector · faulty(AUS) NR 2 ENGINE EGT HARNESS CONNECTOR D1208 SUSPECT FAULTY. LOWER EGT HARNESS P/N TC174-00 AND ELECTRICAL INTERFACE COUPLING P/N CA150-00 ALSO REPLACED.SDR AU990135Bearing · failed(AUS) RT TRIM WHEEL OUTBOARD SHAFT SUPPORT BEARING COLLAPSED. ALL BEARING BALLS MISSING. PART TC: 34,858.SDR AU990066Bracket · broken(AUS) RIGHT NOSE LANDING GEAR DOOR AFT HINGE BRACKET BROKEN INTO TWO PIECES. PART TC: 34,874.SDR AU990705Web · cracked(AUS) STRINGER 18A WEB LOCATED AT BS 727 CRACKED ON LT AND RT SIDES RUNNING AFT FROM FASTENER. FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-10-40A.SDR AU990528Frame · corroded(AUS) FUSELAGE FRAME LOCATED IN THE AFT CARGO COMPARTMENT AT BS 842 RT SEVERELY CORRODED BETWEEN STRINGERS S25R AND S26R AT AFT CARGO DOOR APERTURE.SDR AU990118Stringer · cracked(AUS) FUSELAGE STRINGER WEB 18A LOCATED AT BS 727 CRACKED ON BOTH LT AND RT SIDES RUNNING AFT FROM FASTENERS. FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-10-40A.SDR AU990089Frame · cracked(AUS) FUSELAGE FRAME INNER CHORD LOCATED AT LHS BS 639 CONTAINED A CRACK EMANATING FROM THE FASTENER. FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-10-41A.SDR AU990065Frame · corroded(AUS) FUSELAGE FRAME LOCATED IN THE AFT CARGO COMPARTMENT AT STN 847 BETWEEN STRINGERS S25R AND S26R CONTAINED SEVERE CORROSION.SDR AU990039Frame · cracked(AUS) LEFT AND RIGHT FORWARD PRESSURE BULKHEAD SIDE CHORDS CRACKED. TWO CRACKS WERE ALSO FOUND IN THE BULKHEAD WEB AND ONE IN THE VERTICAL CHORD LOCATED AT LBL 5.7.SDR AU981602Compressor · leaking(AUS) NR 1 ENGINE LEAKING OIL FROM THE LP COMPRESSOR. OIL CONTAMINATION OF NR 1 AIR CONDITIONING SYSTEM.SDR AU981474Housing · cracked(AUS) NR 5 RT INBOARD GROUND SPOILER OUTBOARD ACTUATOR HOUSING PIVOT LUG BROKEN. CAUSED BY TWO FATIGUE CRACKS ORIGINATING FROM CORROSION PITTING IN THE HOUSING PIVOT BEARING BORE. PART TC: 34,921.SDR AU981473Housing · cracked(AUS) LEFT INBOARD GROUND SPOILER OUTBOARD ACTUATOR HOUSING PIVOT LUG BROKEN. SUBMITTER SUSPECTS CAUSED BY FATIGUE CRACKING ORIGINATING FROM CORROSION PITTING IN THE HOUSING PIVOT BEARING BORE. PART TC: 34,043.SDR AU981472Housing · cracked(AUS) RIGHT INBOARD SPOILER OUTBOARD ACTUATOR HOUSING PIVOT LUG BROKEN. SUBMITTER SUSPECTS CAUSED BY FATIGUE CRACKING ORIGINATING FROM CORROSION PITTING OF THE HOUSING PIVOT BEARING BORE. PART TC: 33,875.SDR AU981440Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD FORWARD FACE LOCATED AT STA 178 CRACKED IN THE FOLLOWING AREAS: 1. FORWARD PRESSURE BULKHEAD WEBS CRACKED IN FOUR PLACES IN THE AREA BELOW THE RADAR ANTENNA MOUNT POINTS. 2. VERTICAL CHORD RADIUS ON THE REAR FACE OF THE BULKHSDR AU981301Seal · damaged(AUS) FLEET INSPECTION FOUND NUMEROUS TOILET WASTE BIN ENCLOSURE DOOR SEALS WORN AND/OR DAMAGED.SDR AU981291Cable · worn(AUS) RIGHT THRUST CABLE WORN AND FRAYED IN AREA OF LEADING EDGE STN 219 WHERE THE CABLE PASSES THROUGH THE SEAL.SDR AU981290Cable · worn(AUS) LEFT FUEL CUT-OFF CABLE WORN AND FRAYED IN AREA OF WING LEADING EDGE AT STN 219 WHERE THE CABLE PASSES THOUGH THE SEAL.SDR AU981477Housing · cracked(AUS) LT INBOARD GROUND SPOILER ACTUATOR HOUSING PIVOT LUG BROKEN. CRACK WAS CAUSED BY FATIGUE ORIGINATING FROM CORROSION PITTING IN THE PIVOT LUG BEARING BORE. PART TC: 34,028.SDR AU981617Fitting · cracked(AUS) DURING 4C CHECK, TWO CRACKS WERE FOUND AT LT LOWER SUPPORT ANGLE WHERE HORIZONTAL STABILIZER JACK SCREW PRIMARY SUPPORT BEAM ATTACHES TO STAR TRUSS. IN ADDITION, FOUR ATTACH BOLTS WERE SHOWING SIGNS OF LOOSENESS. CRACKS RAN UPWARD IN RADIUS OF ANGLE, CSDR AU981535Skin · corroded(AUS) LOWER WING SKIN CRACKED AND CORRODED IN THE AREA OF THE REAR SPAR ATTACHMENT POINT FOR THE NR 1 TRAILING EDGE FLAP TRACK.SDR AU981370Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD LEFT SIDE CHORD LOCATED AT WL 207 CRACKED AT FLOOR LEVEL. CRACK LENGTH 12.7 MM (0.5 INCH). FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-10-39D.SDR AU981160Lanyard · frayed(AUS) L2 PASSENGER DOOR ESCAPE SLIDE COVER RELEASE CABLE FRAYED. FOUND DURING INSPECTION IAW AD/B737/42.SDR AU981349Bolt · out of adjust(AUS) FORWARD DOOR L1 STOP BOLTS SLIGHTLY OUT OF ADJUSTMENT.SDR AU981336Rod · fractured(AUS) NR 1 LEADING EDGE SLAT ACTUATOR EYE END FRACTURED. DAMAGE CAUSED TO NR 1 SLAT. INVESTIGATION FOUND THAT THE FAILURE WAS INITIATED BY STRESS CORROSION CRACKING AT AN AREA OF FRETTING AND CORROSION ON BORE SURFACE. PART TC: 28,098.SDR AU981467Stringer · cracked(AUS) FUSELAGE STRUCTURE CONTAINED FIVE CRACKS IN AN AREA LOCATED FORWARD OF THE FORWARD SERVICE DOOR IN THE FOLLOWING LOCATIONS: ONE CRACK IN STRINGER 14R AT THE FORWARD END OF THE WEB IMMEDIATELY AFT OF THE FRAME AT STA 2772. ONE CRACK IN STRINGER 15R TO FSDR AU981048Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD LOCATED AT STN 178 CRACKED IN THE FOLLOWING AREAS: 1. FORWARD FACE WEB CRACKED IN FIVE POSITIONS ADJACENT TO THE RADAR MOUNT POINTS. 2. WL217 CONTAINED TWO CRACKS IN THE AREA BETWEEN LBL 5.7 AND LBL 17 3. LT SIDE CHORD LSDR AU981151Lanyard · frayed(AUS) ESCAPE SLIDE COVER RELEASE CABLES FRAYED AT BOTH AFT DOORS. FOUND DURING INSPECTION IAW AD/B737/42.SDR AU981256Actuator · leaking(AUS) RIGHT KRUEGER FLAP ACTUATOR LEAKING DUE TO EXCESS SEALANT ON THE SEAL PLATE BETWEEN THE ACTUATOR VALVE AND THE BLOCKING VALVE. LOSS OF HYDRAULIC FLUID. PART TC: 23,138.SDR AU981416Warning Light · illuminated(AUS) LT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED AND STAYED ON FOR APPROXIMATELY 1.5 HOURS. EXTENSIVE INVESTIGATION OF THE ELECTRICAL SYSTEM COULD FIND NO FAULTS.SDR AU981095Bulkhead · cracked(AUS) FORWARD FUSELAGE BULKHEAD FORWARD FACE CONTAINED SIX WEB CRACKS. FOUND DURING ULTRASONIC INSPECTION.SDR AU981287Web · corroded(AUS) LEFT AND RIGHT KEEL BEAM WEBS CORRODED IN THE AREA JUST FORWARD OF STN 727A. FURTHER INVESTIGATION FOUND THE CORROSION RAN UNDER THE SEALANT BETWEEN THE KEEL BEAM LOWER CHORDS AND THE FUSELAGE SKIN. FOUND DURING INSPECTION IAW ER B73-53-20-5.SDR AU981094Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING AREAS: SIDE CHORDS AT WL 207 LT AND WL 207 RT (2 CRACKS). VERTICAL CHORD AT LBL 5.7 AFT FACE 3. INTERCOSTALS AT WL 197 LT AND WL 195 RT (2 CRACKS). FOUND DURING EDDY CURRENT INSPECTION.
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