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 2005UALA01141Frame · crackedFWD GALLEY DOOR AFT SIDE CLOSURE FRAME IS CRACKED AT 1EA FASTENER HOLE AT LOWER CORNER. REPAIR ACP'D TO CRACKED FRAME WITH SPLICE IN NEW FRAME SECTION PER SRM 51-40-02.SDR 2005UALA01137Landing Gear · malfunctionedUNABLE TO RAISE GEAR AFTER DEPARTURE. SAFETY SENSORS (AIR & GROUND) FOUND OUT OF ADJUSTMENT . (SENSORS STUCK IN GROUND MODE). REPLACED S106 SENSOR AND ADJUSTED THE CLEARANCE PER MM 32-09-01 AND PERFORMED OPS CHECK GOOD.SDR 2005UALA01112Elevator · malfunctionedABORTED TAKE OFF AT 140 KNOTS DUE TO NO ELEVATOR MOVEMENT. UNSECURED ELEVATOR BALANCE WEIGHT BECAME LODGED BETWEEN LOWER SURFACE OF BALANCE BAY & ANGLE USED TO SUPPORT ACCESS PANEL AT STABILIZER BS 94.07. SUBJECT BALANCE WEIGHT BECAME DISLODGED FROM BALANCE STSDR 2005UALA01076Transformer · overheatedNR 1 TRANSFORMER, RECTIFIER WAS FOUND TO HAVE OVERHEAT DAMAGE. FOUND GRND PWR CB-S BURNT. COVER OVER ALL THREE TRANSFORMER-RECTIFIER UNITS WAS BURNED, DUE TO SUSPECTED OVERHEAT IN ONE OR MORE TRS. ALL THREE TRS REPLACED, AS WAS THE BATTERY, BATTERY CHARGER,SDR 2005UALA01072Window · crackedCAPT WINDSCREEN CRACKED AT 11000 FT. EXTERIOR PANE ONLY. WINDOW REPLACED WITH MM 56-11-21.SDR 2005UALA01043Cabin Pressure · malfunctionedUNABLE TO HOLD PRESSURIZATION. REPLACED OVERHEAD CABIN PRESSURE SELECTOR REF MM21-31-25 AND CABIN PRESSURE CONTROLLER REF MM21-31-21 AND ACCOMPLISHED SYSTEM OPS TEST PER MM21-31-00 ALL CK OK. ALSO PRESSURIZED A-C MANUALLY UP TO 3.5 DIFFERENTIAL ALL CK OK.SDR 2005UALA01040Fire Warning · will not testDURING PREFLT TEST, FIRE BELL DOES NOT RING ON ENG APU TEST OR CARGO TEST.SDR 2005UALA01038Light · tornEMERGENCY EXIT LIGHTING STRIP TORN NEAR AFT GALLEY. SUPPLEMENTAL DATA UPDATE, REPLACED LIGHT STRIP.SDR 2005UALA01021Bleed Air Sys · malfunctionedFLIGHT DIVERTED DUE TO NR 1 BLEED WILL NOT SHUT OFF. NR 1 ENGINE BLEED AIR REGULATOR FAILED. REPLACED BLEED AIR REGULATOR PER MM 36-11-16 AND PERFORMED OPERATIONAL CHECK GOOD.SDR 2005UALA01003Light · dirtyEEL LIGHTS INOP FROM ROW 12C TO 21C. CLEANED AND DRIED EEL LIGHTS BY SEAT 19A.SDR 2005UALA00999Power Supply · inoperativeEMERGENCY EXIT LIGHTS AFT OF SEAT ROW 12 ARE INOP. REPLACED BATTERY PACKSDR 2005UALA00998Light · inoperativeEEL LIGHTS INOP FROM ROW 16 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. REPLACED FEEDER CABLE, PCN 560-0809, AND REPLACED EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMP, PCN 560-0857.SDR 2005UALA01008Connector · corrodedFOUND RIGHT FLAP POSITION TRANSMITTER CONNECTOR D229 HAD CORROSION DAMAGE. PIN 9 OF FLAP TRANSMITTER CONNECTOR WAS CORRODED. CAPTAIN'S STALL WARNING SYSTEM WOULD NOT TEST DUE TO A CORRODED WIRE DISCONNECT PLUG (D229). THE SUBJECT DISCONNECT PLUG WAS REPLACSDR 2005UALA00977Rod · out of adjustDOOR 1R HANDLE MOVES IN FLIGHT. *S/D* ADJUSTED COCKING ROD AND LATCH FITTINGS AND STOP PINS. REF MM 52- 00-96-0100A AND MM 52-41-00.SDR 2005UALA00962Skin · dentedLWR FUSELAGE EXTERNAL SKIN HAS A DENT AT BS 1020.5 AT STRINGER 25L. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLERS PER SRM 53-80-01.SDR 2005UALA00960Lamp · burned outEEL LAMPS AFT OF ROW 15 INOP. REPLACED SHORTED LAMP AT ROW 21.SDR 2005UALA00956Light · inoperativeAFT GALLEY FLOOR EEL LIGHTS INOP. REPLACED LAMP STRIP AT AFT GALLEY.SDR 2005UALA00948Skin · damagedEXTERNAL FUSELAGE SKIN HAS LIGHTNING STRIKE DAMAGE AT STA 747 STR 24R.SDR 2005UALA00932Floorbeam · corrodedCABIN FLOOR BS 312 LBL 1 AND LBL 6 SMALL AREA OF CORROSION ON UPPER SURFACE OF FLOORBEAM.SDR 2005UALA00931Bulkhead · gougedAFT PRESSURE BULKHEAD HAS SEVERAL GOUGES AND SCRATCHES AT UPPER ELECTRICAL CONDUIT THROUGH LT SIDE LBL 5 TO LBL 3 WL 84.SDR 2005UALA00914Shear Tie · dentedEXTERNAL FUSELAGE STA 807 BETWEEN 28L AND 28R HAS A DENT AND SHEAR TIE BENT AT RADIUS.SDR 2005UALA00913Door Frame · corrodedR1 DOOR FRAME STA 296 RBL 54 CORRODED, S17R, WL 208.SDR 2005UALA00893Door Frame · corrodedFWD GALLEY DOOR STUB FRAME AT STA 296 AND RBL 54 CORRODED AT STRINGER S-17R AND WL 208.SDR 2005UALA00885Frame · crackedFWD GALLEY DOOR FRAME CRACKED AFT SIDE LOWER STOP FITTING.SDR 2005UALA00884Frame · crackedFWD GALLEY DOOR AFT FRAME IS CRACKED AT 3RD AND 4TH STOP FITTING CUTOUTS.SDR 2006UALA00135Skin · damagedCUTOUT FOR DOOR 2R LOWER HINGE COVER AT STA 955 IS DAMAGED. THE DAMAGE WAS TRIMMED FROM THE -82 SKIN ASSY (-86 SKIN AND -87 DOUBLER) IN ACCORDANCE WITH 737-300 SRM 53-00-01 FIGURE 101, ALLOWABLE DAMAGE NR 1, DETAIL 1 AND 737-300 SRM 51-10-02.SDR 2005UALA00881Inverter · inoperativeEMERGENCY EXIT FLOOR LIGHTS INOP HALF WAY BACK. REPLACED AFT INVERTER.SDR 2005UALA00876Skin · bentEXTERNAL FUSELAGE SKIN BENT & DAMAGED AT AFT GALLEY DOOR LOWER HINGE CUTOUT.SDR 2005UALA00875Skin · dentedEXTERNAL FUSELAGE SKIN DENTED ABOVE STR 10R AT STA 377.SDR 2005UALA00878Light · damagedEMERGENCY EXIT LIGHTS, FLOOR LIGHT DAMAGED AT AFT CABIN. REPLACED EEL LIGHT ASSY.SDR 2005UALA00873Trim System · malfunctionedEXCESSIVE RUDDER AND TRIM, NEEDED 4 UNITS LT RUDDER TRIM AND 3 UNITS LWD TRIM PLUS YOKE INPUT, TO MAINTAIN WINGS LEVEL. EMERGENCY EQUIPMENT REQUESTED. A BROKEN NR 6 SPOILER CONTROL CABLE (WSB2-4) INHIBITED FLIGHT SPOILER MOVEMENT OF THE NR 6 SPOILER CREATING SDR 2005UALA00869Floorbeam · corrodedCABIN FLOOR, STA 294.5 LBL 7, FLOORBEAM UPPER SURFACE, CORROSION.SDR 2005UALA00868Support · wornEE ACCESS DOOR CUTOUT, RT DOOR CUTOUT, SUPPORT FRAME STR 27R STA 338 IS WORN ABOVE DOOR LATCH FITTING.SDR 2005UALA00867Floorbeam · corrodedCABIN FLOORBEAM TOP CORRODED IN SEVERAL PLACES.SDR 2005UALA01007Odor · detectedELECTRICAL SMELL OCCURRED IN COCKPIT AND CABIN AFTER 1ST ATTEMPT TO CONNECT GROUND POWER. REMOVED SPEED SENSOR ACC PNL FOUND APU INLET OIL SOAKED, RAN APU UNABLE TO FIND SOURCE 22SEP SFO: PER AMM 49-00-00-0101 PG 180M FIG 140 LK 21. REPLACE SPEED SENSOR PACKINSDR 2005UALA00852Skin · dentedEXT FUSELAGE SKIN IS DENTED 0.75 INCH FWD OF STA 1006 & IMMEDIATELY BELOW SKIN LAP AT S14L.SDR 2005UALA00848Skin · damagedEXTERNAL FUSELAGE STA 434 STR 2R BLENDED SKIN AROUND A FASTENER IS DAMAGED.SDR 2005UALA00851Warning Light · illuminatedFLT SHOWED LE FLAPS IN TRANSIT LIGHT. AMBER ALERT CALLED IN. A FAILED LEADING EDGE (LE) FLAP AND SLAT CONTROL VALVE INHIBITED FULL EXTENTION OF THE LE FLAPS AND SLATS. SUBJECT FAILURE CONSIDERED AN ISOLATED INCIDENTCORRECTIVE ACTION: REPLACED AND TESTED SUBSDR 2005UALA00850Light · inoperativeLEFT AND RIGHT EMERGENCY EXIT LIGHTS INOP (EXTERIOR). REPLACED LIGHT ASSEMBLY.SDR 2005UALA00847Structure · dentedAFT CARGO DOOR HAS SEVERAL OVERLAPPING DENTS AND SKIN IS DAMAGED ON FWD SIDE. INSTALLED A REPAIR DOUBLER 53 BY 48 INCHES REF SRM 52-00-01 AND SRM 51-00-01 FIG 202.SDR 2005UALA00846Angle · corrodedAFT GALLEY DOOR THRESHOLD ZEE ANGLE CORRODED STA 978 TO 984 RBL 62.5 STR 17 WL 208.SDR 2005UALA00845Floor Support · corrodedCABIN FLOOR SUPPORT AT AFT ENTRY DOOR HAS CORROSION STA 957-986 LBL 62.5 WL 208 AND LBL 63.0 WL 208.SDR 2005UALA00838Skin · crackedDENT FWD AND BELOW DOOR 2L.SDR 2005UALA00834Structure · bird strikeBIRD STRIKE AROUND THE RADOME, VERY LOUD, ALSO, ODOR IN COCKPIT. ON CLIMB, THE AIRCRAFT ENCOUNTERD A BIRDSTRIKE. THE AIRCRAFT RETURNED TO FIELD AND MAINTENANCE PERFORMED A BID STRIKE INSPECTION PER AMM. THERE WAS EVIDENCE OF BIRD INGESTION IN THE NR 1 ENG HSDR 2005UALA00815Stringer Clip · crackedAFT PIT STA 907 STR 24R STRINGER CLIP BENT AND CRACKED. REMOVED AND REPLACED STRINGER CLIP.SDR 2005UALA00814Stringer Clip · bentAFT PIT STA 727D STR 20L STRINGER CLIP BENT AND CRACKED. REMOVED AND REPLACED STRINGER CLIP.SDR 2005UALA00817Switch · failedAIRCRAFT PRESSURIZATION PROBLEM. AFTER T/O, CREW REPORTED LOSS OF LNAV, VNAV, AUTOTHROTTLE, TCAS AND ENGINE LOW IDLE LIGHT WAS ON. THROUGH 25,000 FT, ALTITUDE WARNING HORN SOUNDED AND THE CABIN ALTITUDE MAXED OUT AT 11,000 FT. AFTER T/O, CREW REPORTED LOST LSDR 2005UALA00756Light · inoperativeEEL LIGHTS INOPERATIVE ON FLOOR AT AFT CABIN. CLEANED AND DRIED RACEWAY, PWR CABLE AND LIGHTS.SDR 2005UALA00754Skin · crackedAFT CARGO DOOR HAS A VERTICAL CRACK APPROX 2 INCHES LONG, 6 T0 8 INCHES DOWN FROM DOOR HANDLE. REMOVED EXISTING DOUBLERS AND INSTALLED NEW DOUBLER APPROX 48" BY 48" PER SRM 52-30-01 AND SRM 52-00-01.SDR 2005UALA00749Light · inoperativeEEL FLOOR LIGHTING ROWS 15-21 INOPERATIVE. REPLACED CABLE AND SECURED TRACKS. REPLACED CABLE AND SECURED TRACKS.
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