Boeing 737-322

Service difficulty reports · 4,751

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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.

SDR 2004UALA00770Skin · gougedFUSE SKIN PANEL IS GOUGED AT BS 294, 12 INCHES BELOW LT ENTRY DOOR UPPER HINGE. MAJOR REPAIR ACCOMPLISHED. REPLACED SKIN PANEL.Aug 12, 2004 · N395UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00769Bear Strap · damagedAFT CARGO DOOR AT STA 795 STR 23 - 24 RT TO THE BEAR STRAP REQUIRES REPLACEMENT OF LWR SKIN SECTION DAMAGED FROM A PREVIOUS REPAIR. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER.Aug 11, 2004 · N395UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00768Link Assy · failedRIGHT MLG WAS DAMAGED BY IMPROPER CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. REPLACED LINK.Aug 8, 2004 · N395UA · Boeing 737322 · Main Landing Gear Attach SectionSDR 2004UALA00782Generator · malfunctionedAPU GEN ON LINE, FOUND VOLTAGE TO INDICATE 127VAC, WITH COCKPIT PANEL LIGHTS DIM, E&E LIGHTS VERY DIM AND FLUCTUATING, EXHAUST FAN NORMAL CB POPS. APU POWER IS NO GOOD. APU GEN C-B (C899) CONTACT B2 TERMINAL LUG & 3EA WIRES INSULATION BURNT 8 INCHES FROM B2 LAug 8, 2004 · N362UA · Boeing 737322 · AC Generation SystemSDR 2004UALA00764Skin · dentedFUSELAGE SKIN HAS TWO DENTS AT STA 393 AND STR 16L. CUT-OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER.Aug 8, 2004 · N395UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00765Trunnion · damagedLEFT MLG TRUNNION LINK WAS DAMAGED BY IMPROPER CORROSION REMOVAL. REPLACED LINK.Aug 8, 2004 · N395UA · Boeing 737322 · Main Landing Gear Attach SectionSDR 2004UALA00733Csd · failedRETURNED TO ORD DUE TO A NR 1 ENGINE GENERATOR DRIVE LIGHT. NR 1 CSD FAILED. OIL LOSS EVIDENT ON COWL, CSD EXTREMELY HOT ON ARRIVAL, SUSPECT INTERNAL FAILURE. REPLACED THE NR 1 CSD, EXCESSIVE METAL FOUND ON CHIP DETECTOR. SHOP FOUND EXTENSIVE INTERNAL CSD FAILAug 7, 2004 · N352UA · Boeing 737322 · AC Generation SystemSDR 2004UALA00745Light · inoperativeFWD GALLEY EEL FLOOR LIGHT INOPERATIVE. REPLACED EEL GALLEY FLOOR STRIP.Aug 6, 2004 · N343UA · Boeing 737322 · Emergency LightingSDR 2004UALA00719Warning Light · illuminatedDIVERTED TO JFK DUE TO NOSE GEAR RED LIGHT INDICATION. PERFORMED GEAR SWING AND NOTED NOSE GEAR LOCK ACTUATOR WOULD NOT LOCK IN RETRACT POSITION WITH GEAR LEVER IN OFF POSITION. REPLACED NOSE GEAR LOCK ACTUATOR AND ACCOMPLISHED SEVERAL GEAR SWING AND MANUAL EAug 3, 2004 · N350UA · Boeing 737322 · Landing Gear Position and WarningSDR 2004UALA00763Skin · dentedFUSELAGE SKIN IS DENTED AT STA 357, 3 INCHES BELOW STR 20R AND NEXT TO A BUTT JOINT. INSTALLED DOUBLER AND TRIPLER.Aug 2, 2004 · N395UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00717Warning Light · illuminatedABORTED TAKEOFF AT 110 KNOTS DUE TO A WING BODY OVERHEAT MESSAGE. LEFT WING BODY OVERHEAT LIGHT COME ON AT TAKE-OFF ROLL. MAINTENACE CHECKED LEFT PACK AREA FOR PNEUMATIC LEAK. NO LEAKS WERE FOUND. REPOSITIONED OVERHEAT SENSING ELEMENT GROMMETS. RAN LEFT PACKAug 2, 2004 · N329UA · Boeing 737322 · Overheat DetectionSDR 2004UALA00716Seal · misinstalledABORTED TAKEOFF AT VERY LOW SPEED DUE TO A REPORT OF FLAMES COMING FROM THE TAILPIPE OF THE NR 2 ENGINE. FLT RETURNED TO THE GATE UNDER IT'S OWN POWER. TEARDOWN OF THE ENGINE REVEALED THAT AN HPC STAGE 6 HONEYCOMB HAD FAILED. THIS FAILURE MODE IS AN INDUSTRAug 2, 2004 · N393UA · Boeing 737322 · Engine (Turbine/Turboprop)SDR 2004UALA00762Clip · crackedSTA 500D STR 8R HAS CRACKED CLIP. REPLACED STRINGER CLIP.Aug 1, 2004 · N395UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2004UALA00715Cable · damagedLAST 18 FEET OF EEL LIGHTING INOP. REPLACED FEEDER CABLE.Aug 1, 2004 · N351UA · Boeing 737322 · Light System WiringSDR 2004UALA00761Frame · crackedCABIN OVERWING FRAME BODY STA 616L CRACKED AT BOTTOM FASTENER BELOW FLOOR LEVEL. REMOVED CRACKED AREA, FABRICATED AND INSTALLED ANGLE.Jul 31, 2004 · N395UA · Boeing 737322 · Fuselage Main, FrameSDR 2004UALA00760Intercostal · crackedMID CABIN HAS A CRACKED INTERCOSTAL AT STA 540 RBL 2 AND LBL 2. REPAIRED THE FLOOR INTERCOSTALS.Jul 30, 2004 · N395UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2004UALA00759Frame · crackedR1 DOOR CUT-OUT FWD FRAME CRACKED JUST ABOVE STR 17R AT STA 294. MAJOR REPAIR ACCOMPLISHED. REMOVED THE CRACKED FRAME AND FABRICATED A REPAIR.Jul 30, 2004 · N395UA · Boeing 737322 · Fuselage Main, FrameSDR 2004UALA00703Fitting · brokenNR 5 GROUND SPOILER OB ACTUATOR ATTACH LUG BROKEN. NR 5 GROUND SPOILER ACTUATOR WAS FOUND FRACTURED AT THE BEARING END DURING ROUTINE HMV MAINTENANCE INSPECTION. THE ACTUATOR WAS SENT TO THE SHOP FOR INITIAL EVALUATION BEFORE BEING SENT TO BOEING FOR A FULL FJul 29, 2004 · N395UA · Boeing 737322 · Wing, Attach FittingsSDR 2004UALA00676Stringer Clip · crackedSTRINGER 23R CLIP AT STA 727C CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP.Jul 19, 2004 · N394UA · Boeing 737322 · Fuselage Main, Attach FittingsSDR 2004UALA00675Skin · dentedRIGHT HORIZONTAL STABILIZER DENTED ON THE FIXED LEADING EDGE TWELVE INCHES FROM INBOARD EDGE. *S/D* DURING AIRCRAFT MAINTENANCE VISIT, AN INTERIM REPAIR WAS FOUND ON THE RIGHT HORIZONTAL STABILIZER LEADING EDGE AT STA 75. THE INTERIM REPAIR WAS CHANGED TO AJul 19, 2004 · N394UA · Boeing 737322 · Horizontal Stabilizer, Plate/SkinSDR 2004UALA00694Skin · damagedON SKIN DAMAGE AT STA 360, A DENT IN STRINGER 20R SKIN FLANGE. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED. REPLACED STRINGER SPLICE FITTING.Jul 18, 2004 · N367UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00674Lamp · inoperativeAFT GALLEY EEL STRIP INOPERATIVE. REPLACED EEL STRIP.Jul 18, 2004 · N323UA · Boeing 737322 · Emergency LightingSDR 2004UALA00704Bear Strap · damagedPREVIOUS BEAR STRAP REPAIR NEEDED TO BE REPLACED DUE TO SIDE SKIN REPLACEMENT FOR AFT CARGO. THE PREVIOUS REPAIR IS LOCATED ON THE AFT PIT DOOR CUT OUT ON THE AFT SIDE. INSTALLED QUADRUPLER.Jul 17, 2004 · N394UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00639Sensor · failedRETURNED TO DEN DUE TO OVERHEATED EXHAUST COOLING FAN. THE EQUIPMENT COOLING LOW FLOW SENSOR FAILED. REPLACED THE LOW FLOW SENSOR WITH A NEW AND IMPROVED ONE. PERFORMED EQUIPMENT COOLING EXHAUST SYSTEM TEST. NO FAULTS NOTED.Jul 3, 2004 · N311UA · Boeing 737322 · Cabin Cooling SystemSDR 2004UALA00626Warning Light · illuminatedABORTED TAKEOFF AT 80 KNOTS DUE TO ELECTRICAL SIX PACK ALERT. COULD NOT DUPLICATE. REPLACED WORN LAMPS IN SIX PACK, CHECKS NORMAL.Jun 28, 2004 · N365UA · Boeing 737322 · Central WarningSDR 2004UALA00600Frame · crackedSTA 663 FRAME HAS 4 CRACKS, 2 EACH AT THE STR 3 RT LIGHTENING HOLE, AND 1 EACH AT THE STR 1 AND 2 RT LIGHTENING HOLE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND REMOVED STRINGER SPLICES FOR ACCESS, INSTALLED REPAIR ANGLE DOUBLER AND STRINGER SPLICES.Jun 21, 2004 · N391UA · Boeing 737322 · Fuselage Main, FrameSDR 2004UALA00695Skin · dentedDENT IN FUSELAGE JUST FWD AND ABOVE AFT LAV SERVICE PANEL. DENT MEASURES 6 INCH LONG X 5 INCH VERTICAL AT 0.250 INCH DEEP. FRAME HAS DISTORTION. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER/TRIPLER REPAIR.Jun 18, 2004 · N330UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00593Indicator · inaccurateDIVERTED TO COS DUE TO INOP FUEL GAUGE. CREW REPORTED UNEVEN FUEL LOAD WITH EQUAL FUEL FLOW. FOUND 340 LBS DIFFERENCE BETWEEN THE DRIP STICK VALUE AND THE LEFT MAIN FUEL QUANTITY INDICATION SYSTEM. CALIBRATED NR 1 AND NR 2 FUEL QUANTITY INDICATION SYSTEMS.Jun 17, 2004 · N399UA · Boeing 737322 · Fuel Quantity IndicatorSDR 2004UALA00589Skin · dentedFOUND A 3.5 X 1.5 X 0.1875 DEEP DENT ON RIGHT HORIZONTAL STABILIZER LEADING EDGE APPROX 15 FEET FROM THE FUSELAGE. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED FLUSH REPAIR.Jun 16, 2004 · N391UA · Boeing 737322 · Horizontal Stabilizer, Plate/SkinSDR 2004UALA00588Circuit Breaker · trippedDIVERTED TO IAD DUE TO CIRCUIT BREAKER PROBLEMS. GROUND SERVICE CB P6-11 D8 POPPED 2 TIMES ON TAXI. CYCLED BATTERY CHARGER C-B'S AFTER 20 MINUTES. RESET GROUND C-B WITH NORMAL FAN SELECTED FOR 5 MINUTES AND ALT EXHAUST FOR 20 MINUTES, GROUND C-B HELD AND STJun 16, 2004 · N306UA · Boeing 737322 · External Power SystemSDR 2004UALA00585Engine · fluctuatesABORTED TAKEOFF AT 110 KNOTS DUE TO FUEL FLOW FLUCTUATION ON NUMBER 2 ENGINE. *S/D* ACCOMPLISHED POWER ASSURANCE CHECK, PMC CHECK, AND ACCELERATION CHECK. ALL CHECKS OK. NO FAULTS FOUND.Jun 15, 2004 · N375UA · Boeing 737322 · Engine (Turbine/Turboprop)SDR 2004UALA00584Light · contaminatedEMERGENCY EXIT PATH LIGHTS ARE INOP FROM ROW 15 AFT. REMOVED COFFEE AND CLEANED EEL TRACKS. OPS CHECKED NORMAL.Jun 15, 2004 · N347UA · Boeing 737322 · Emergency LightingSDR 2004UALA00583Lap Joint · damagedREPLACEMENT OF REPAIRS AT STA 887 STR 20R LAP JOINT AND AT STA 907 SKIN SPLICE DURING THE REPLACEMENT OF RIGHT AFT LOWER SKIN. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER, TRIPLER AND QUADRUPLER RUNNING FROM STA 874 TO STA 921, AND FROM STR 19R TO 21R.Jun 14, 2004 · N391UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00582Rib · dentedRT HORIZONTAL O/B LEADING EDGE SKIN IS DENTED AT THE 7TH RIB. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED INTERNAL DOUBLER AND FILLER.Jun 13, 2004 · N391UA · Boeing 737322 · Horizontal Stabilizer, Spar/RibSDR 2004UALA00578Sensing Element · failedDIVERTED TO DENVER WITH NR 1 ENGINE OVERHEAT LIGHT ON. LANDED ON AMBER ALERT WITH ENGINE SHUTDOWN. CREW REPORTED CRUISING AT FL350, NR 1 ENGINE OVERHEAT LIGHT FLICKERED TWICE AND THEN CAME ON STEADY. ACCOMPLISHED ENGINE OVERHEAT CHECK LIST, LIGHT STAYED ON.Jun 13, 2004 · N368UA · Boeing 737322 · Overheat DetectionSDR 2004UALA00565Angle · crackedANGLE ON AFT OF INTERCOSTAL STA 294 STR 23L CRACKED. FABRICATED AND INSTALLED ANGLE.Jun 9, 2004 · N391UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2004UALA00553Actuator · failedRETURNED TO FIELD DUE TO NR 3 LEADING EDGE FLAP PROBLEM. REPLACEMENT OF THE LEADING EDGE FLAP ACTUATOR CORRECTED THE DISCREPANCY. THE LEADING EDGE FLAP ACTUATOR WAS FOUND WITH A SEVERELY DETERIORATED PISTON HEAD SEAL. THE CONDITION OF THIS SEAL SUPPORTS THE REJun 7, 2004 · N386UA · Boeing 737322 · Leading Edge Slat ActuatorSDR 2004UALA00538Shear Tie · damagedSHEAR TIES WERE FOUND DAMAGED OR HAD EXCESSIVE GAP BETWEEN SKIN AND SHEAR TIE AT STA 727 S24L-S25L, 727D S24L-S25L, 727C S25R-S26R, 727D S25R-S26R, 727E S24L-S25L AND 767 S24L-S25L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED SHEAR TIES.Jun 2, 2004 · N399UA · Boeing 737322 · Fuselage Main, StructureSDR 2004UALA00540Warning Light · illuminatedEQUIPMENT COOLING EXHAUST OFF LIGHT ILLUMINATED IN BOTH NORMAL AND ALTERNATE MODES. THE EQUIPMENT COOLING LOW FLOW SENSOR FAILED. REPLACED THE LOW FLOW SENSOR WITH A NEW AND IMPROVED ONE. PERFORMED EQUIPMENT COOLING EXHAUST SYSTEM TEST. NO FAULTS NOTED.Jun 2, 2004 · N329UA · Boeing 737322 · Cabin Cooling SystemSDR 2004UALA00533Beam · corrodedAFT PIT SILL BEAM HAD CORROSION. REPLACED LOWER SILL BEAM WEB.Jun 2, 2004 · N399UA · Boeing 737322 · Fuselage Main, StructureSDR 2004UALA00532Splice · misinstalledTWO EA STRINGER SPLICES WERE FOUND WITH INADEQUATE EDGE DISTANCE AT FASTENER LOCATIONS STA 907 STR 26R AND 25R. REPLACED STRINGER SPLICES.Jun 2, 2004 · N399UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2004UALA00528Skin · misinstalledBOTTOM BELLY SKIN HAS INSUFFICIENT ED ON THE LT SKIN LAP FASTENER HOLES FROM STA 727-907. REPLACED LOWER BELLY SKIN.Jun 2, 2004 · N399UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00527Bear Strap · cutAFT CARGO DOOR CUTOUT AFT EDGE BEAR STRAP REPAIR DOUBLER IS INSUFFICIENT. REPLACED BEAR STRAP DOUBLER.Jun 2, 2004 · N399UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00525Wire · inoperativeEMERGENCY ESCAPE LIGHTING INOP FROM ROWS 15-21. REPLACED FEEDER CABLE ROWS 14-21.Jun 1, 2004 · N343UA · Boeing 737322 · Light System WiringSDR 2004UALA00523Doubler · cutSTRAP DOUBLERS ARE CUT AT STR 26R, BETWEEN STA 727C AND 727D. REPLACED STRAP DOUBLERS.Jun 1, 2004 · N399UA · Boeing 737322 · Fuselage Main, StructureSDR 2004UALA00521Shear Tie · misrepairedSTATION 787 SHEAR TIE BETWEEN STR 2L AND 27R HAS NO EDGE DISTANCE ON PREVIOUS REPAIR. REPAIRED SHEAR TIE.Jun 1, 2004 · N399UA · Boeing 737322 · Fuselage Main, StructureSDR 2004UALA00520Splice · damagedSTATION 727A STRINGER SPLICE HAS ELONGATED HOLE. REPLACED STRINGER SPLICE.Jun 1, 2004 · N399UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2004UALA00519Shear Tie · damagedSTATION 727A INBOARD OF STRINGER 27L SHEAR TIE HAD EXCESSIVE MATERIAL LOSS. REPLACED SHEAR TIE.Jun 1, 2004 · N399UA · Boeing 737322 · Fuselage Main, StructureSDR 2004UALA00518Stringer Clip · crackedSTATION 277 STRINGER 15R STRINGER CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP.Jun 1, 2004 · N399UA · Boeing 737322 · Fuselage Main, Longeron/StringerSDR 2004UALA00517Wire · failedFLIGHT DIVERTED DUE TO A STUCK FUEL CROSS-FEED VALVE CAUSING A FUEL IMBALANCE. CREW REPORTED FUEL CROSSFEED LIGHT REMAINS BRIGHT (INDICATING VALVE IS IN TRANSIT) NO MATTER WHAT POSITION THE CROSSFEED SWITCH IS IN. AND FUEL CROSS FEED VALVE POSITION LIGHT DOES Jun 1, 2004 · N328UA · Boeing 737322 · Fuel System Wiring
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