Boeing 737-322
Service difficulty reports · 4,751
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 = '737322' 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 = '737322' 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 2001UALA00290Skin · dentedAFT CARGO DOOR EXTERNAL SKIN DENTED ABOVE THE HANDLE AREA. REPAIRED DENTS ON AFT CARGO DOOR. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00289Bulkhead · crackedBS 178 BULKHEAD CRACKED AT LBL 5.7 WL 218. REPAIRED CRACKED BULKHEAD. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00281Battery · dischargedBOTH DC LIGHTS ILLUMINATED. SUPPLEMENTAL DATA UPDATE THE M6 AIRCRAFT BATTERY (MR24349-445), AND M5 BATTERY CHARGER (MR24315-011) WERE REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 2001UALA00266Switch · failedAUDIO CYCLING BETWEEN ALL CHANNELS. SUPPLEMENTAL DATA UPDATE REPLACED AUDIO REPRODUCER AND RESET SWITCH. OPS CHECKED NORMAL.SDR 2001UALA00265Selector Switch · failedUNABLE TO PRESSURIZE THE AIRCRAFT AFTER DEPARTURE. SUPPLEMENTAL DATA UPDATE CABIN PRESSURE SELECTOR FAILED. REPLACED THE CABIN PRESSURE SELECTOR PANEL.SDR 2001UALA00272Tee Chord · crackedFORWARD CARGO DOOR CROSSBEAM AFT END OUTER TEE CHORD CRACKED. REPAIRED CRACKED TEE CHORD. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00271Beam · crackedAFT CARGO DOOR LOWER CROSS BEAM CRACKED. REPAIRED CRACKED CROSS BEAM. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00270Stop Fitting · crackedFORWARD GALLEY DOOR LOWER AFT STOP FITTING FRAME CRACKED. REPAIRED CRACKED FRAME. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00259Floorbeam · corrodedFLOORBEAM HAS 27 PERCENT MATERIAL LOSS AT STA 294. REPAIRED FLOORBEAM. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00256Actuator · failedLEADING EDGE FLAP EXTENSION PROBLEM. SUPPLEMENTAL DATA UPDATE REPLACED THE NR 3 LEADING EDGE FLAP ACTUATOR. OPS CHECKED NORMAL.SDR 2001UALA00230O-Ring · leakingFUEL WAS NOTICED LEAKING FROM THE TOP OF THE LEFT WING. *S/D* FOUND FUEL LEAKING FROM LEADING EDGE SPAR INBOARD OF NR 2 ENG. REPLACED O-RING ON LOWER JET PUMP. NO LEAKS WITH BOOST PUMPS PRESSURIZED.SDR 2001UALA00220Connector · dirtyEMERGENCY EXIT LIGHTING FROM ROW 17 TO ROW 22 IS INOPERATIVE. CLEANED CONNECTORS. OPS CHECKED GOOD.SDR 2001UALA00255Frame · crackedLEFT HAND OVERWING FRAME BS 616L IS CRACKED. REPAIRED OVERWING FRAME BS 616L. ACCOMPLISHED MAJOR REPAIR.SDR 2001UALA00240Skin · dentedDENT ON FUSELAGE AFT OF DOOR 1L AT STA 392, WL 210, AND STRINGER 16L NEEDS PERMANENT REPAIR. THIS IS CONSIDERED A MAJOR REPAIR. ACCOMPLISHED NON-DESTRUCTIVE TESTING, NO CRACKS FOUND. ALODINED, PRIMED, AND INSTALLED DOUBLER TO AFFECTED AREA. ACCOMPLISHED MASDR 2001UALA00280Bulkhead · crackedBS 178 BULKHEAD WEB CRACKED. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00274Skin · damagedFUSELAGE UPPER CROWN SKIN HAS A MATERIAL LOSS UNDER THE VHF ANTENNA. INSTALLED A DOUBLER TO THE AFFECTED AREA. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00285Bulkhead · crackedBS 178 BULKHEAD VERTICAL CHORD AT LBL 5.7 IS CRACKED. REPAIRED VERTICAL CHORD. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00191Bolt · improper partFUEL SEEPING FROM THE TOP OF THE RIGHT WING. *S/D* FOUND THE FUEL LEAK TO BE RESULTING FROM BOLTS BOTTOMING OUT IN THE DOME NUTS IN THE SUSPECTED PANEL. REPLACED THE PANEL. THE BOLTS HAVE BEEN SWITCHED OUT WITH SHORTER ONES IN ORDER TO ELIMINATE THE PROBLESDR 2001UALA00286Frame · crackedBS 178 BULKHEAD AFT SIDE LBL 5.7 INBOARD CHORD CRACKED. REPAIRED CRACKED CHORD. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00278Skin · dentedDENT LOCATED AT STA 960 LOWER FUSELAGE CENTERLINE. REPAIRED DENT. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00239Mount · crackedSTATION 178 IS CRACKED AT THE RADAR ANTENNA MOUNT. THIS IS CONSIDERED A MAJOR REPAIR. INSTALLED DOUBLER TO AFFECTED AREA. ACCOMPLISHED MAJOR REPAIR.SDR 2001UALA00177Circuit Breaker · malfunctionedNOSE GEAR UNSAFE LIGHT ON WHEN THE GEAR WAS EXTENDED FOR LANDING. SUPPLEMENTAL DATA UPDATE RESET BREAKER C404 AND NORMAL GEAR INDICATION RETURNED. REPLACED THE BREAKER AS A PRECAUTION.SDR 2001UALA00161Screw · missingDIVERTED DUE TO A PASSENGER SEEING A SCREW FALL OUT OF THE ENGINE MOUNT AREA. *S/D* FOUND FAIRING WITH MISSING SCREW. REPLACED SCREW.SDR 2001UALA00139Panel · crackedNR 1 NACELLE STRUT PLUME SUPPRESSOR AFT PANEL CRACKED. *S/D* FOUND PLUME PANEL CRACKED. REPAIRED PANEL.SDR 2001UALA00120Filter · leakingLOSS OF THE B-SYSTEM HYDRAULICS. *S/D* REPLACED B-SYSTEM ACOUSTIC FILTER AND ASSOCIATED O-RING, AND SERVICED B-SYSTEM HYDRAULICS. NO FURTHER LEAKS EVIDENT.SDR 2001UALA00116Circuit Breaker · poppedLANDING GEAR WARNING INDICATION. *S/D* ACCOMPLISHED CHECK OF LEVER LOCK SOLENOID. FOUND LANDING GEAR LATCH AND PRESS WARNING CIRCUIT BREAKER OPEN. RESET CIRCUIT BREAKER. SYSTEM CHECKED NORMAL.SDR 2001UALA00084Computer · malfunctionedAUTOPILOT A WOULD NOT ENGAGE. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED BOTH A & B FLIGHT CONTROL COMPUTERS AND AUTOPILOT STABILIZER TRIM SERVOS. ALL OPERATIONAL CHECKS WERE GOOD.SDR 2001UALA00085Switch · failedNR 2 PACK TRIPPED AFTER TAKEOFF AND WOULD NOT RESET. *S/D* FOUND THE COMPRESSOR DISCHARGE SWITCH FAILED. REPLACED THE COMPRESSOR DISCHARGE SWITCH.SDR 2001UALA00083Seal · tornCABIN PRESSURIZATION PROBLEM. *S/D* FOUND FORWARD ENTRY SEAL TORN, AFT CARGO DOOR REN MISSING, AND FORWARD DRAIN VALVES LEAKING. REPLACED FORWARD ENTRY DOOR SEAL, AFT CARGO DOOR REN, AND 12 DRAIN PLUGS.SDR 2001UALA00637Control Rod · chafedRUDDER POWER CONTROL UNIT CONTROL ROD AFT END OUTBOARD SIDE CHAFED, WORN AND KINKED. *S/D* CONTROL ROD REPLACED WITH SERVICEABLE CONTROL ROD. OFF UNIT FOUND TO BE WITHIN LIMITS PER BOEING SERVICE LETTER 737-SL-27-098 WHICH WAS WRITTEN TO ADDRESS THIS ISSUE SDR 2001UALA00633Control Rod · chafedRUDDER POWER CONTROL UNIT CONTROL ROD AFT END OUTBOARD SIDE CHAFED, WORN AND KINKED. *S/D* CONTROL ROD REPLACED WITH SERVICEABLE CONTROL ROD. OFF UNIT SCRAPPED PER BOEING SERVICE LETTER 737-SL-27-098 WHICH WAS WRITTEN TO ADDRESS THIS ISSUE IN APRIL 1995. SDR 2001UALA00073Blade · damagedNR 2 ENGINE VIBRATION. *S/D* FOUND TWO FAN BLADES SHINGLED. REPLACED THE TWO FAN BLADES. A SUBSEQUENT TRIM RUN REVEALED NO VIBRATION.SDR 2001UALA00065Loop · damagedWING-BODY OVERHEAT LIGHT ILLUMINATED. *S/D* FOUND LOOP M487 LOCATED IN LEFT ENGINE STRUT CAVITY SHORTED TO GROUND. REPLACED LOOP M487.SDR 2001UALA00060Csd · failedNR 2 GENERATOR FAILED DURING CLIMBOUT. *S/D* ISOLATED SOURCE OF FAILURE TO NR 2 ENGINE GENERATOR CONSTANT SPEED DRIVE UNIT. THE CSD WAS REPLACED. THE NR 2 AC GENERATOR UNIT AND NR 2 GENERATOR CONTROL UNIT WERE REPLACED AS PRECAUTIONARY. AIRCRAFT WAS RETURSDR 2001UALA00047Bellcrank · brokenLEFT SIDE INBOARD LEADING EDGE FLAP STUCK IN DOWN POSITION AFTER TAKEOFF. *S/D* FOUND BROKEN BELLCRANK. REPLACED THE BELLCRANK.SDR 2001UALA00046Receiver · inoperativeNR 1 NAVIGATION RECEIVER IS INOPERATIVE. *S/D* REPLACED NR 1 NAVIGATION RECEIVER. OPS CHECKED OK.SDR 2001UALA00024Valve · failedFUEL TRANSFER PROBLEMS. *S/D* REPLACED THE CROSSFEED VALVE, NR 2 FUEL TANK FORWARD AND AFT BOOST PUMP CHECK VALVES, RIGHT HAND CENTER TANK BOOST PUMP CHECK VALVE, AND RIGHT CENTER TANK BOOST PUMP. ACCOMPLISHED CENTER TANK OVERRIDE CHECK. SYSTEM OP''S CHECKSDR 2001UALA00020Lanyard · brokenAFT CARGO DOOR LIGHT CAME ON AFTER TAKEOFF. *S/D* FOUND AFT CARGO DOOR RELEASE HANDLE BUNGEE CORD BROKEN AND INTERFERING WITH DOORSWITCH. REPLACED BROKEN BUNGEE CORD.SDR 2001UALA00644Control Rod · chafedRUDDER POWER CONTROL UNIT CONTROL ROD AFT END OUTBOARD SIDE CHAFED, WORN AND KINKED. *S/D* CONTROL ROD REPLACED WITH SERVICEABLE CONTROL ROD. BOEING RELEASED SERVICE LETTER 737-SL-27-098 TO ADDRESS THIS ISSUE BACK IN APRIL 1995. HEAVY MAINTENANCE JOB INSTRSDR 2000UALA00804Controller · failedCABIN ALTITUDE CLIMBED TOO HIGH ON CLIMBOUT. IN CRUISE, COULD NOT CONTROL CABIN ALTITUDE IN AUTO STANDBY OR MANUAL MODES. *S/D* THE CABIN PRESSURE CONTROLLER FAILED. REPLACED THE CABIN PRESSURE CONTROLLER.SDR 2000UALA00785Actuator · failedAFTER NORMAL GEAR RETRACTION, NOSE LANDING GEAR FELL OUT OF GEAR WELL. *S/D* FOUND NOSE LANDING GEAR LOCK ACTUATOR NOT ALLOWING GEAR TO FULLY LOCK. REPLACED NOSE LANDING GEAR LOCK ACTUATOR. CHECKED OPERATION OF NOSE LANDING GEAR ASSEMBLY. OPERATED NORMALLSDR 2000UALA00780Controller · lack of lubeABORTED TAKE-OFF AT 110 KNOTS DUE TO A TAKE-OFF WARNING HORN. SUPPLEMENTAL DATA UPDATE THE S651 SWITCH WAS CLEANED AND THE SPEED BRAKE CONTROL LEVER WAS LUBRICATED. OPS CHECKS NORMAL.SDR 2000UALA00779Seal · failedUNABLE TO MAINTAIN CABIN PRESSURE. SUPPLEMENTAL DATA UPDATE REPLACED GROUND AIR CONNECTOR AND REPAIRED GATE SEAL.SDR 2000UALA00768Warning System · activatedAFT BODY OVERHEAT INDICATION FOLLOWED BY AN ABNORMAL ODOR IN THE COCKPIT. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED ENGINE RUN-UP ON BOTH ENGINES, AND PERFORMED PNEUMATIC SYSTEM TEST. NO BURNING SMELL AND NO AFT BODY OVERHEAT LIGHT ILLUMINATED.SDR 2000UALA00771Light · inoperativeEMERGENCY EXIT LIGHTING INOPERATIVE FROM ROW 20 AFT. SUPPLEMENTAL DATA UPDATE REPLACED CUT FEEDER STRIP, INSTALLED NEW INCAPSULATED LIGHT IN AFT GALLEY, AND COMPLETED INSTALLATION OF AFT EEL FLOOR LIGHTING. OPS CHECKS GOOD.SDR 2000UALA00713Line · chafedLOSS OF THE 'A' SYSTEM HYDRAULICS. SUPPLEMENTAL DATA UPDATE FOUND BRAIDED FLEX LINE FROM 'A' SYSTEM PRESSURE MODULE TO 'A' SYSTEM ELECTRIC MOTOR DRIVEN PUMP CHAFED THRU. REPLACED DAMAGE FLEX LINE.SDR 2000UALA00694Pressure Switch · malfunctionedFUEL BOOST PUMP LIGHTS FLICKERED. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED NR 2 AFT LOW PRESSURE SWITCH.SDR 2000UALA00683Plate · out of adjREAR CARGO DOOR WARNING LIGHT. SUPPLEMENTAL DATA UPDATE ADJUSTED STRIKER PLATE.SDR 2000UALA00670Switch · failedANTISKID INDICATION. SUPPLEMENTAL DATA UPDATE THE S303 LANDING GEAR SWITCH FAILED. THE SWITCH WAS REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 2000UALA00666Engine · malfunctionedPARTIAL LOSS OF POWER IN THE NR 1 ENGINE. *S/D* THE ENGINE WAS REPLACED.
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