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 AUS20030902Skin · corroded(AUS) RT WING VENT TANK UPPER SKIN LOWER SURFACE CORRODED. LOWER CHORD OF REAR SPAR AND WEBS OF STIFFENERS NR 9 AND NR 10 ALSO CORRODED.SDR AUS20030872Spar · corroded(AUS) LT WING VENT TANK SKIN ATTACHMENT FLANGES AND WEBS OF STIFFENERSNO9, NR 10 AND NR 11 CORRODED BEYOND LIMITS. LOWER SECTION OF REAR SPAR ALSO CORRODED.SDR AUS20030828Spar · corroded(AUS) LT WING VENT BOX NR 10 STIFFENER CORRODED ON AFT FACE BETWEEN STN 557 & 583. CORROSION WAS FOUND IN 4 AREAS. 3 AREAS WERE LOCATED BETWEEN 100MM & 177.8MM OUTBOARD OF WS 557 & WERE APPROX 25.4MM INDIAMETER. ONE AREA LOCATED BETWEEN 304.8MM & 381MM OUTBOARSDR AUS20030564Skin · cracked(AUS) FORWARD GALLEY DOOR CUTOUT SKIN FORWARD AND AFT UPPER CORNERS CRACKED. THE AFT UPPER CORNER OF THE CUTOUT WAS CRACKED FROM ONEHOLE IN THE BEARSTRAP ONLY. TWO HOLES AT THE FORWARD UPPER CORNER OF THE CUTOUT WERE CRACKED IN THE STUBFRAME ONLY AND ATHIRD HOSDR AUS20030237Stiffener · corroded(AUS) LT WING CENTER SECTION SUPPORT BEAM STIFFENER CONTAINED LEVEL 2 CORROSION. FOUND DURING INSPECTION IAW J3-CA53-0129.SDR AUS20030238Web · corroded(AUS) LT WING CENTRE SECTION SUPPORT BEAM WEB CONTAINED LEVEL 2 CORROSION IN AREA BETWEEN THE HEAT EXCHANGER CUTOUTS. AREA OF CORROSION 6.3MM (0.250IN) IN DIAMETER BY 0.508MM (0.020IN) DEEP.FOUND DURING INSPECTION IAW J3-CA53-0129.SDR AUS20030018Nut · cracked(AUS) TRAILING EDGE FLAP TRACK RETAINING BOLTS LOCATED AT THE LT OUTBOARD FLAP, INBOARD TRACK, INBOARD RETAINING BOLT THREADS WERE NOT IN SAFETY. BOLT AND BARREL NUT WERE REMOVED AND INSPECTED WITH THE NUT FOUND TO BE CRACKED.SDR AUS20021447Spar · cracked(AUS) RT WING REAR SPAR CRACKED AROUND FASTENER HOLE. FOUND DURING INSPECTION IAW ER B73-57-40-17 AND BOEING SB 737-57-1216.SDR AUS20021433Bulkhead · damaged(AUS) REAR PRESSURE BULKHEAD DAMAGED ON LT SIDE. A GOUGE WAS FOUND ON A LAP JOINT OF A WEB DOME CLOSE TO S-15L.SDR AUS20021428Frame · cracked(AUS) FORWARD CARGO DOOR CRACKED IN TWO PLACES. ONE CRACK WAS LOCATED IN THE FORWARD FRAME RADIUS IN LINE WITH THE LOWER FITTING PROPAGATING UPWARDS. THE OTHER CRACK WAS FOUND IN THE AFT FRAME IN THE SAME POSITION. CRACK LENGTH 38.1MM (1.5IN). FOUND DURING INSSDR AUS20021045Skin · corroded(AUS) RT WING UPPER SURFACE CORRODED IN AREA LOCATED FORWARD OF THE FILLER CAP AT APPROXIMATELY WING STN 440. AN AREA OF 6.35MM (0.250IN) BY 25.4MM (1IN) WAS REMOVED AT THE FORWARD EDGE OF THE FILLER CAP HOUSING.SDR AUS20010967Cable · frayed(AUS) AFT SERVICE DOOR RELEASE CABLES FRAYED. FOUND DURING INSPECTION IAW AD/B737/042.SDR AUS20010966Cable · frayed(AUS) FORWARD SERVICE DOOR RELEASE CABLES FRAYED. FOUND DURINGINSPECTION IAW AD/B737/042.SDR AUS20010988Cable · stiff(AUS) NOSE LANDING GEAR EXTENSION SYSTEM CABLE STIFF TO OPERATE. AFORCE IN EXCESS OF 50 POUNDS WAS NEEDED TO OPERATE THE CABLE. THE MAXIMUM LIMIT IS 28 POUNDS.SDR AUS20010710Hose · ruptured(AUS) NOSE LANDING GEAR EXTENSION FLEXIBLE HOSE RUPTURED. LOSS OF SYSTEM A' HYDRAULIC FLUID.SDR AUS20010709Valve · broken(AUS) FORWARD TOILET DRAIN VALVE POPPET BROKEN. INNER POPPET WASMISSING.SDR AUS20010706Cable · frayed(AUS) FORWARD GALLEY DOOR ESCAPE SLIDE RELEASE CABLE FRAYED. FOUNDDURING INSPECTION IAW AD/B737/042.SDR AUS20010584Hose · leaking(AUS) LH MAIN LANDING GEAR UPLOCK ACTUATOR HOSE LEAKING. METALCONTAMINATION OF NO1 HYDRAULIC PUMP FILTERS.SDR AUS20010551Generator · misinstalled(AUS) NR 3 TOILET AND PSU 21L OXYGEN GENERATORS HAD THE RELEASE PINS INCORRECTLY INSTALLED IN THE SAFETY PIN HOLES.PERSONNEL/MAINTENANCE ERROR.SDR AUS20010495Apu · faulty(AUS) APU FAILED PERFORMANCE MONITORING TEST. EGT ROSE TO 800 DEGREES.SDR AUS20010615Fcu · faulty(AUS) APU FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND PISTON ANDSHAFT SET IN TIMER WORN. THE GOVERNOR SHAFT WAS WORN. FLYWEIGHT TOES WORN. PACKINGS AND SEALS FLAT AND WORN.SDR AUS20010518Fcu · faulty(AUS) APU FUEL CONTROL UNIT FAULTY.SDR AUS20010560Pcu · leaking(AUS) RUDDER POWER CONTROL UNIT (PCU) LEAKING INTERNALLY.SDR AUS20010529Pcu · faulty(AUS) RUDDER POWER CONTROL UNIT (PCU) INTERNAL LEAK. FOUND DURING INSPECTION IAW ER B73-27-20-15 AND BOEING SL 737-SL-27-119. WORKSHOP INSPECTION FOUND THE LEAK WITHIN LIMITS.SDR AUS20010659Fitting · fractured(AUS) LT INBOARD GROUND SPOILER CENTRE OUTBOARD HINGE FITTING HAD A MISSING PIECE ALLOWING THE HINGE BEARING TO LOOSEN IN THE FITTING.SDR AUS20010398Generator · misinstalled(AUS) OXYGEN GENERATORS LOCATED IN THE FLIGHT ATTENDANT SERVICE UNITADJACENT TO CABIN DOORS L1 AND L2 HAD THE RELASE PINS LOCATED INTHE SAFETY PIN HOLES. PERSONNEL/MAINTENANCE ERROR.SDR AUS20010396Sensor · failed(AUS) AIR SENSING TEST CARD FAILED.SDR AU010381Compass · faulty(AUS) AIR BUBBLE IN STANDBY COMPASS. FOUND DURING INSPECTION IAWAD/INST/9.SDR AU010380Compass · faulty(AUS) BUBBLE IN COMPASS FLUID. FOUND DURING INSPECTION IAW AD/INST/9.SDR AUS20010563Jackscrew · corroded(AUS) NR 3 TRAILING EDGE FLAP JACKSCREW CORRODED. SPALLING ON SCREWJACKBALL AND NUT. SUSPECT INCORRECT LUBRICANT USED.SDR AU010376Controller · faulty(AUS) FLAPS FAILED TO MOVE PAST 15 DEGREES.SDR AU010375Hydraulic System · low(AUS) HYDRAULIC A SYSTEM QUANTITY AND PRESSURE LOST.SDR AUS20010443Door · misinstalled(AUS) FORWARD TOILET OXYGEN SYSTEM DROP-DOWN DOOR HAD WHITE SILASTICMATERIAL ACROSS THE FORWARD OUTBOARD CORNER PREVENTING IT FORM OPENING. THE SILASTIC HAD BEEN USED ON THE TOILET CEILING PANEL AND HAD BEEN SMEARED ACROSS THE OXYGEN PANEL DOOR.SDR AU010331Generator · failed(AUS) OXYGEN GENERATORS LOCATED ABOVE SEATS 9LT, 11LT, 13LT, 15LT AND 17LT HAD THE RELEASE PIN LOCATED IN THE SAFETY PIN HOLE.SDR AU010346Motor · failed(AUS) AIRCRAFT PRESSURISATION SYSTEM OUTFLOW VALVE ELECTRIC MOTOR FAILED. OUTFLOW VALVE FAILED TO OPEN.SDR AUS20010581Circuit Breaker · failed(AUS) NR 1 GENERATOR BREAKER FAILED.SDR AU010305Placard · missing(AUS) TIRE INFLATION PLACARD MISSING.SDR AUS20010941Structure · corroded(AUS) CORROSION CONTROL INSPECTION FOUND AREAS OF LEVEL 2 CORROSION.FOUND DURING INSPECTION IAW AD/B737/52 AMDT2.SDR AU010311Bungee Cord · broken(AUS) AFT CARGO DOOR RELEASE LANYARD HANDLE JAMMED UNDER DOOR SEAL. INVESTIGATION FOUND THE LANYARD BUNGEE CORD BROKEN.SDR AUS20010867Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD LOCATED AT BS178 CRACKED IN TWO LOCATIONS. ONE CRACK FOUND IN LBL 5.7 LOCATED THROUGH INSULATIONBLANKET HOLE. CRACK LENGTH 15.875MM (0.625IN). ONE CRACK FOUND IN RBL 17.1 LOCATED THROUGH INSULATION BLANKET HOLE. CRACK LENGTH15.8SDR AUS20010605Valve · faulty(AUS) TOILET DRAIN VALVE FAULTY. FOUND DURING TESTING IAW ER B73-30-11.SDR AUS20010768Hose · ruptured(AUS) LT MAIN LANDING GEAR ACTUATOR UP HOSE BURST. LOSS OF SYSTEM A' HYDRAULIC FLUID.SDR AU010107Bolt · loose(AUS) SEAT BELT ATTACHMENT BOLT LOOSE AT SEAT 11E. FOUND DURING INSPECTION IAW ER B73-25-20-246.SDR AUS20010886Bearing · seized(AUS) NOSE LANDING GEAR MANUAL EXTENSION RELEASE MECHANISM TORQUE SHAFT BEARINGS SEIZED.SDR AU010064Wire · damaged(AUS) KAPTON WIRES LOCATED IN REFUEL PANEL HAVE DAMAGED INSULATION ALLOWING THE WIRES TO BE EXPOSED.SDR AU010063Cable · frayed(AUS) L2 DOOR SLIDE ATTACHMENT CABLE FRAYED IN LOOP AREA.SDR AU001262Transmitter · out of adj(AUS) LT TRAILING EDGE FLAP TRANSMITTER OUT OF ADJUSTMENT.SDR AU001284Wire · damaged(AUS) KAPTON WIRES LOCATED IN REFUEL PANEL HAVE DAMAGED INSULATION ALLOWING THE WIRES TO BE EXPOSED.SDR AU001287Hose · leaking(AUS) NOSE LANDING GEAR RETRACTION ACTUATOR DOWN LINE HYDRAULIC HOSE RUPTURED. LOSS OF SYSTEM A'' HYDRAULIC FLUID.SDR AU001074Brake · corroded(AUS) NR 2 BRAKE ATTACHMENT FLANGE BOLT HOLES CORRODED. PITTING CORROSION ALSO FOUND IN THE BOLT HOLE AT THE 10 O CLOCK POSITION. FOUND DURING INSPECTION IAW AD/B737/140.
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