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.

SDR 2005UALA01478Engine · bird ingestionRETURN TO FIELD DUE TO BIRD STRIKE TO NR 2 ENGINE & ASSOCIATED HIGH VIBRATIONS. AFTER FAN BLADE SET REPLACEMENT HIGH ENGINE VIBRATION CONTINUED AND ENGINE WAS REPLACED. THE ENGINE SHOP VERIFIED CORRECT FAN BLADE SPACER, SHIM, RETAINER AND PROPER FAN BLADE WEIDec 18, 2005 · N329UA · Boeing 737322 · Engine (Turbine/Turboprop)SDR 2005UALA01461Target · looseSHORTLY AFTER TAKEOFF AFT CARGO DOOR WARNING LIGHT ILLUMINATED. RETURNED TO DEN WITH AFT CARGO DOOR LIGHT PROBLEM. DOORS CHECKED, FLIGHT DEPARTED WITH 92 PASSENGERS 1:05 LATE. FOUND AFT CARGO DOOR WARNING SWITCH TARGET LOOSE AND OUT OF POSITION. SECURED TARDec 13, 2005 · N375UA · Boeing 737322 · Door Warning SystemSDR 2005UALA01460Warning System · activatedAT FL330, CABIN ALT WARNING HORN SOUNDED. PRESSURIZATION WAS IN AUTO AND OUTFLOW VALVE INDICATED FULL CLOSED. SWITCHED BOTH PACKS TO HIGH AND STARTED DESCENT. AT FL280, CABIN RATE SLOWED. DURING TROUBLESHOOTING OF CBN PRESSUR IZATION PROBLEM, FOUND RT PACKDec 13, 2005 · N315UA · Boeing 737322 · Cabin Compressor SystemSDR 2005UALA01443Wire · arcedCAPT UPPER LT PITOT HEAT CB AT P13-3 C1 INSIDE WIRE ARCED TO GROUND WHEN OPENING PANEL FOR INSPECTION. WIRES BURNT THRU AND SEPERATED AT P18-3 C1 CIRCUIT BREAKER DUE TO WIRE W18-217 BEING ROUTED INCORRECTLY AND CHAFING THRU PROTECTIVE COVER OVER TIME ON THEDec 9, 2005 · N308UA · Boeing 737322 · Ice/Rain Protection System WiringSDR 2005UALA01446Landing Gear · malfunctionedNO INDICATION OF NOSE GEAR COMING UP. CREW SPOKE WITH SAMC, NO POSITIVE RESULT WITH GEAR. SWITCH S845 "NOSE GR DOWN SENSOR" FAILED. REPLACED SWITCH AND PERFORMED OPERATIONAL CHECK (SWUNG GEAR) OF THE GEAR, CHECKS GOOD.Dec 8, 2005 · N314UA · Boeing 737322 · Landing Gear Retraction/Extension SystemSDR 2005UALA01417Skin · puncturedPUNCTURE JUST FWD OF RT NOSE GEAR DOOR AND 1 FT FWD OF EXT PWR PANEL DOOR. ACCOMPLISHED INSTALLATION OF REPAIR DOUBLERS AND TRIPLERS PER SRM 53-00-01 REPAIR 31.Dec 7, 2005 · N332UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA01396Wire · inoperativeEEL LIGHT INOP AT AFT GALLEY CART STOWAGE. REPLACED RIBBON CABLE.Dec 4, 2005 · N347UA · Boeing 737322 · Light System WiringSDR 2005UALA01386Wire · damagedFIRST CLASS FLOOR EEL AND GALLEY STRIP EEL LIGHT IS INOP. REPLACED FEEDER CABLE.Dec 2, 2005 · N305UA · Boeing 737322 · Light System WiringSDR 2005UALA01392Inverter · inoperativeCREW REPORTS ROW 15 TO AFT CABIN ESCAPE PATH LIGHTING INOPERATIVE. INVERTER REPLACED.Dec 1, 2005 · N365UA · Boeing 737322 · Light System WiringSDR 2005UALA01381Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT. RESET CIRCUIT BREAKER FOR "'LANDING GEAR LATCH AND PRESSURE WARNING'" ON P6-3 PANEL. PERFORMED OPERATIONAL CHECK PER 7-11-11, 32-32=00 AND 32-34-00 (SWUNG) . NO FAULT FOUND.Nov 30, 2005 · N331UA · Boeing 737322 · Main Landing GearSDR 2005UALA01374Skin · corrodedLT WING ROOT AREA UPPER SKIN SURFACE CORRODED AT FUSELAGE STA 616 TO 617.5 AT WBL 85.0 TO 87.0. REMOVED CORROSION DAMAGE PER SRM 57-20-01, ROTO PEENED, ALODINED & RESTO RED PAINT PER SRM 51-20-01.THE REPAIR IS APPROVED BY FAA 8100-9 DATED NOV 27TH 2005.Nov 29, 2005 · N349UA · Boeing 737322 · Wing, Plate/SkinSDR 2005UALA01373Skin · corrodedLT WING ROOT AREA UPPER SKIN SURFACE CORRODED AT FUSELAGE STA 616 TO 626 AT WBL 108 10 112. REMOVED CORROSION DAMAGE PER SRM 57-20-01, ROTO PEENED, ALODINED & RESTO RED PAINT PER SRM 51-20-01.THE REPAIR IS APPROVED BY FAA 8100-9 DATED NOV 27TH 2005.Nov 29, 2005 · N349UA · Boeing 737322 · Wing, Plate/SkinSDR 2005UALA01372Skin · corrodedLT WING ROOT AREA UPPER SKIN SURFACE CORRODED AT FUSELAGE STA 626 TO 663.7 AT WBL 108 10 112. REMOVED CORROSION DAMAGE PER SRM 57-20-01, ROTO PEENED, ALODINED & RESTORED PAINT PER SRM 51-20-01.THE REPAIR IS APPROVED BY FAA 8100-9 DATED NOV 27TH 2005.Nov 29, 2005 · N349UA · Boeing 737322 · Wing, Plate/SkinSDR 2005UALA01336Window · arcedARCING AND SMOKE FROM CAPTAIN'S SLIDING WINDOW. REPLACED BROKEN LUG ON WIRE W504-404-20W AT T266 AND SECURED WIRING. WINDOW HEAT OPS CHKS OK.Nov 27, 2005 · N370UA · Boeing 737322 · Flight Compartment WindowsSDR 2005UALA01353Window · arcedCAPTAINS SLIDING WINDOW IS ARCING NEAR THE WINDOW FRAME. REPLACED CAPTS SLIDING WINDOW HEAT PIGTAIL WIRES OP TEST OK OVHT TEST OK.Nov 26, 2005 · N381UA · Boeing 737322 · Flight Compartment WindowsSDR 2005UALA01355Light · inoperativeEEL LIGHTS FROM ROW 15 AFT TO GALLEY INOPERATIVE. REPLACED EEL STRIP AT AFT SEATS.Nov 25, 2005 · N311UA · Boeing 737322 · Emergency LightingSDR 2005UALA01339Snubber · misinstalledFLIGHT DIVERTED DUE TO CABIN PRESSURIZATION PROBLEM. FOUND DOOR 1LT SNUBBER INSTALLED INCORRECTLY AND DOOR PRESSURE SEAL DAMAGED. REINSTALLED SNUBBER PER MM52-11-96 PG 401 AND REPAIRED SEAL.Nov 25, 2005 · N202UA · Boeing 737322 · Passenger/Crew DoorsSDR 2005UALA01331Window · crackedL4 WINDOW CRACKED EN ROUTE. L4 WINDOW MIDDLE PANE SHATTERED, REPLACED WINDOW PER MM 56-11-31.Nov 22, 2005 · N327UA · Boeing 737322 · Flight Compartment WindowsSDR 2005UALA01521Window · unknownRETURNED TO THE FIELD DUE TO A FLIGHT DECK WINDOW PROBLEM.Nov 20, 2005 · N383UA · Boeing 737322 · Passenger/Crew DoorsSDR 2005UALA01319Engine · flamed outRIGHT ENGINE FLAMED OUT AFTER STALL. ACCOMPLISHED ENGINE TROUBLESHOOTING PER AMM71-00-02 WITH NO FAULTS FOUND. REPLACED MAIN ENGINE CONTROL (MEC) AND FUEL PUMP AS PRECAUTION. SHOP FINDINGS ON FUEL PUMP AND MEC FUEL PUMP BENCH TEST FOUND NO FAULTS. MEC BENCH TNov 20, 2005 · N312UA · Boeing 737322 · Engine (Turbine/Turboprop)SDR 2005UALA01304Skin · crackedPOSSIBLE LONGITUDINAL CRACK BELOW STRINGER AFT OF RIGHT WING BODY FAIRING BELOW EMERGENCY EXIT LIGHT. INSTALLED REPAIR DOUBLER PER UA-EVA-50778.Nov 20, 2005 · N374UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA01500Seal · damagedRT FL DUE TO DOOR 1 LT AIR LEAK. DOOR SEAL DAMAGED. REPLACED DOOR SEAL.Nov 19, 2005 · N383UA · Boeing 737322 · Passenger/Crew DoorsSDR 2005UALA01312Light · looseEMERGENCY EXIT LIGHT STRIP NOT ATTACHED FIRST 6 INCHES. EEL STRIP REINSTALLED.Nov 19, 2005 · N373UA · Boeing 737322 · Emergency LightingSDR 2005UALA01313Sign · inoperativeEMERGENCY EXIT SIGN ABOVE FLIGHT DECK DOOR IS INOP. BATTERY PACK REPLACED.Nov 18, 2005 · N348UA · Boeing 737322 · Emergency LightingSDR 2005UALA01293Lamp · inoperativeEEL LIGHTS INOP FROM ROW 17 AFT. REPLACED EEL CABLE AND MOST AFT LAMP.Nov 17, 2005 · N314UA · Boeing 737322 · Emergency LightingSDR 2005UALA01282Light · inoperativeEMERGENCY EEL STRIP LIGHTING INOP FROM ROW 15 AFT. STRIP REPLACED.Nov 15, 2005 · N335UA · Boeing 737322 · Emergency LightingSDR 2005UALA01272Skin · crackedDOOR 2R DOOR CUTOUT HAS POSSIBLE CRACK APPROX 3.5 INCH LOWER FWD CORNER. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED HFEC AND CONFIRMED CRACK THREE AND ONE HALF INCH LONG. MAJOR REPAIR PER SRM 53-00-01 DETAIL IV, DOUBLER-TRIPLER REPAIR SCHEME USED AT FWD LWR CORNENov 14, 2005 · N315UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA01320Sill · crackedAFT PIT HAS DENT IN LOWER SILL. AREA OF DENT IS ON DOOR SILL. REPAIRED SILL AND REINSTALLED.Nov 13, 2005 · N349UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2005UALA01265Frame · misdrilledFWD GALLEY DOOR AFT FRAME UPPER HOLE AT STOP FITTING HAS NO ED. SUPPLEMENTAL DATA UPDATE FABRICATED DOUBLER AND FILLER AND INSTALLED REF AAR EO 50267 AND SRM 51-40-02.Nov 12, 2005 · N328UA · Boeing 737322 · Galley DoorsSDR 2005UALA01264Skin · crackedAFT GALLEY DOOR LWR HINGE CUTOUT IN FUSELAGE LWR FWD EDGE CRACKED. DATA REMOVED CRACK FABRICATED DOUBLER AND TRIPLER PER SRM 53-60-01.Nov 12, 2005 · N328UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA01234Relief Valve · failedEXPERIENCED A RAPID DECOMPRESSION. ACCOMPLISHED SAFETY RELIEF VALVE TEST PER MM 21-32-21 AND TEST FAILED. REPLACED VALVE AND PERFORMED CABIN DEPRESSURIZATION AND ALTITUDE WARNING CHECKS PER MM 05-51-81, SYSTEM OPS GOOD.Nov 7, 2005 · N340UA · Boeing 737322 · Cabin Pressure Control SystemSDR 2005UALA01232Relay · failedBOTH IRS ON DC LIGHTS ILLUM JUST AFTER LIFTOFF. SUA IRS POWER FAULT HAS NOT REOCCURRED.Nov 5, 2005 · N326UA · Boeing 737322 · Navigation SystemSDR 2005UALA01231Skin · crackedDOOR OPENING AT 2R HAS A CRACK AT THE UPPER HINGE CUT-OUT. VERIFID LENGTH AND LOCATION OF CRACK. CUT OUT DAMAGED AREA AND MFG DOUBLER SKIN REPAIR PER SRM 53-60-01.Nov 5, 2005 · N379UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA01233Odor · detectedELEC ODOR DETECTED NEAR ROW 18. SUPPLEMENTAL DATA UPDATE, AIRCRAFT WAS CHECKED WITH NO DISCREPANCIES FOUND, AND NO FURTHER COMPLAINTS OF ELECTRICAL ODOR. AS A PRECAUTION, A CALLOUT HAS BEEN ENTERED TO LOWER THE PSUS BETWEEN ROWS 16 AND 20 TO CHECK FOR DAMAGENov 4, 2005 · N304UA · Boeing 737322 · Air Distribution SystemSDR 2005UALA01230Angle · crackedHORIZONTAL STABILIZER CUTOUT UPPER CHORD ANGLE CRACKED LOCATED BETWEEN STA 1138 & 1156 AT STRINGER 5A. *S/D* REMOVED CRACKED AREA OF CHORD ANGLE. ACP NDT FOR CRACKS. NO CRACKS FOUND. FABRICATED AND INSTALLED NESTED ANGLE REPAIR AND FILLER. PER SRM 51-70-Nov 4, 2005 · N328UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2005UALA01229Skin · dentedLOWER FUSELAGE DENT AT STA 204 & STR 22 LEFT. *S/D* REMOVED DAMAGE & ACP NDT FOR CRACKS. NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER & FILLER PER SRM 53-10-01 REPAIR NR 11.Nov 4, 2005 · N328UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA01209Generator · malfunctionedLOST NR 2 GENERATOR AND THEN RECEIVED A NR 2 ENGINE OVERHEAT MESSAGE. LOSS OF GENERATOR CAUSED BY APPARENT CSD FAILURE. GENERATOR, CSD, AND CSD OIL COOLER WERE REPLACED. GENERATOR RECEIVED ROUTINE SHOP MAINTENANCE, BUT HAD NOT FAILED. CSD AND CSD OILER COOOct 30, 2005 · N374UA · Boeing 737322 · AC Generator-AlternatorSDR 2005UALA01207Light · burned outEMERGENCY AISLE LIGHT INOP AT ROW 21. RELAMPED WITH NR 1317 LAMP.Oct 29, 2005 · N318UA · Boeing 737322 · Emergency LightingSDR 2005UALA01241Door Frame · crackedAFT CARGO DOOR FWD FRAME IS CRACKED AT BOLT HOLE ABOVE THE NR 3 FWD DOOR STOP FITTING. *S/D* REPLACED FORWARD UPPER AND LOWER DOOR FRAMES PER SRM 51-40-02.Oct 27, 2005 · N336UA · Boeing 737322 · Fuselage Main, StructureSDR 2005UALA01204Light · inoperativeEEL FLOOR LIGHTS INOPERATIVE FROM ROW 13 AFT. REPLACED INVERTER AT ROW 19.Oct 27, 2005 · N315UA · Boeing 737322 · Emergency LightingSDR 2005UALA01195Skin · gougedFUSELAGE SKIN APPROXIMATE STA 807 AND STR 18R ABOVE AFT CARGO DOOR HAS A DEEP GOUGE APPROX .025 INCH LONG. BLENDED GOUGE, REPAIRED SKIN PER SRM 53-00-01 REPAIR 32 BY INSTALLING DOUBLER AND TRIPLER.Oct 26, 2005 · N336UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA01194Skin · dentedSMALL SHARP DENT IN RIGHT FUSELAGE APPROXIMATELY 15 INCHES AFT OF AND 6 INCHES BELOW DOOR 1R CUTOUT. REMOVED DAMAGE REF SRM 53-00-01, MANUFACTURED A DOUBLER AND TRIPLER PER SRM 53-00-01 REPAIR 31.Oct 26, 2005 · N336UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA01187Light · inoperativeEMERGENCY FLOOR PATH EXIT LIGHTING INOP AT ROW 15 AFT. REPLACED EEL POWER STRIP AND MOST AFT LIGHT ASSY.Oct 25, 2005 · N315UA · Boeing 737322 · Emergency LightingSDR 2005UALA01173Door Frame · crackedFWD SIDE GALLEY DOOR FRAME LOWER END IS CRACKED AT TWO EACH FASTENER LOCATION. REMOVED THE CRACKS, INSTALLED FRAME REPAIR AND INNER SKIN REF JD SM90-52-40-14JD AND BOEING DRAWING 69-69430.Oct 20, 2005 · N336UA · Boeing 737322 · Fuselage Main, StructureSDR 2005UALA01172Floor Panel · corrodedFWD CABIN FLOOR RT INNER CORD UNDER FLOOR PANEL IS CORRODED, FROM BS 280 TO 348 WL 208.1 RBL 54. REMOVED AND REPLACED CREASE BEAM AND DRAIN PAN REF SRM 51-40-02.Oct 20, 2005 · N336UA · Boeing 737322 · Fuselage Floor PanelSDR 2005UALA01171Frame · crackedMID CABIN RT FRAME IS CRACKED AT STUB BEAM AT STA. 616 LOWER FASTENER HOLE. ACCOMPLISHED A REPAIR REF MM53-11-89, INSTALLED A FILLER AND DOUBLER ANGLE.Oct 20, 2005 · N336UA · Boeing 737322 · Fuselage Main, FrameSDR 2005UALA01170Frame · crackedMID CABIN LT FRAME IS CRACKED AT STUB BEAM AT STA 616 LOWER FASTENER HOLE. REPAIRED LT FRAME STA 616 REF MM 53-11-89 ,INSTALLED FILLER AND ANGLE DOUBLER.Oct 20, 2005 · N336UA · Boeing 737322 · Fuselage Main, FrameSDR 2005UALA01166Skin · crackedEXTERNAL FUSELAGE SKIN STA 363 TO 365 ABOVE STR 4R AT CHEM MILL STEP HAS A CRACK INDICATION. MAJOR REPAIR ACP'D - DOUBLER-TRIPLER REPAIR INSTALLED PER SRM 53-00-01 REPAIR 31 FIG 210Oct 19, 2005 · N336UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA01165Skin · crackedFUSELAGE HAS THREE INCH CRACK BEHIND LT WING EMERGENCY EXIT LIGHT AREA. ACCOMPLISHED CATEGORY B REPAIR REF. SRM 53-00-01. CRITICAL FASTNER ROW WILL NEED INSPECTION AT 60,000 CYCLES AFTERINSTALLATION OF REPAIR. ** MF5633 CREATED TO MONITOR **Oct 19, 2005 · N371UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2005UALA01159Skin · delaminatedNR 6 SLAT LEADING EDGE HAS DELAMINATION ON UPPER SURFACE. HONEYCOMB EXPOSED. REINSTALLED NEW SLAT.Oct 16, 2005 · N311UA · Boeing 737322 · Leading Edge Devices
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