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 2000UALA00326Blade · vibrationCREW REPORTS EXCESSIVE VIBRATION. *S/D* FULL SET OF FAN BLADES WERE REPLACED.SDR 2000UALA00322Blade · vibrationEXCESSIVE ENGINE VIBRATION (NR 2 ENGINE). *S/D* FAN TRIM BALANCE WAS ATTEMPTED. REPLACED FAN BLADE SET. NO FURTHER EVENTS REPORTED.SDR 2000UALA00318Sensor · dirtyFORWARD CARGO LIGHT ILLUMINATED 100 FEET AFTER TAKEOFF. *S/D* ADJUSTED STRIKER PLATE ON FWD CARGO DOOR. CLEANED SENSOR. PERFORMED OPERATIONAL CHECKS SEVERAL TIMES ON GROUND, FOUND NORMAL.SDR 2000UALA00316Light · will not testEMERGENCY LIGHT FROM ROW 17 TO THE BACK OF THE CABIN IS SHOWING NO LIGHT WHEN DOING THE TESTING. *S/D* INSTALLED NEW GALLEY LAMP STRIP.SDR 2000UALA00308Latch · out of rigON DEPARTURE FROM DEN, AFT SERVICE DOOR LIGHT ILLUMINATED. *S/D* DOOR SOFT LATCH - OUT OF RIG. ADJUSTED DOOR STOPS PER MAINTENANCE MANUAL. NO ADDITIONAL OCCURRENCES.SDR 2000UALA00729Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00309Regulator · failedBLEED VALVE MALFUNCTION PREVENTING ANTI-ICING ON ONE WING AND ENGINE. *S/D* FOUND FAILED PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV). REPLACED PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV).SDR 2000UALA00223Accessory Unit · malfunctionedTHE NR 3 FLAP IN TRANSIT LIGHT ON THE OVERHEAD PANEL FLICKERS ALONG WITH THE FORWARD PANEL FLAPS IN TRANSIT LIGHT WITH FLAPS UP. *S/D* REPLACED THE FLAP SLAT ACCESSORY UNIT, (M229). THE LEADING EDGE INDICATION SYSTEM HAS OPERATED NORMAL SINCE THE REPLACEMENSDR 2000UALA00220Relay · malfunctionedCOCKPIT WARNING LIGHTS CAME ON IN FLIGHT. *S/D* REPLACED RELAYS R33, R34, R87 AND MASTER DIM MODULE.SDR 2000UALA00287Squat Switch · inoperativeTCAS FAIL LIGHT ILLUMINATED, LNAV AND VNAV WOULD NOT ENGAGE, ACARS STUCK IN GROUND MODE, AUTO THROTTLES REMAINED IN THROTTLE HOLD. *S/D* REPLACED M990 GROUND SENSING SQUAT SWITCH. SYSTEM CHECKED OK.SDR 2000UALA00267Blade · bird strikeRETURNED TO TUS DUE TO A NR 1 ENGINE BIRD STRIKE. *S/D* INSPECTION REVEALED 3 DAMAGED FAN BLADES AND MIDSPAN SHROUD OVERLAP ON THE FAN BLADES. BORESCOPE INSPECTION OF HIGH PRESSURE COMPRESSOR WITH NO LIMITING DEFECTS. THREE FAN BLADE PAIRS WERE REPLACED ANDSDR 2000UALA00744Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00258Relay · failedRETURNED TO THE FIELD AT DEN WHEN BOTH EQUIPMENT COOLING FANS WERE INOPERATIVE. *S/D* FOUND THE EQUIPMENT COOLING EXHAUST LOW FLOW INDICATION RELAY FAILED. REPLACED THE EQUIPMENT COOLING EXHAUST LOW FLOW INDICATION RELAY.SDR 2000UALA00249Packing · wornDIVERTED TO SMF DUE TO A NR 1 ANTI ICE VALVE LIGHT ILLUMINATION. *S/D* REPLACED LT COWL ANTI ICE VALVE. OPS CHECK OK.SDR 2000UALA00739Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00244Module · inoperativeRETURNED TO THE FIELD AT IAD DUE TO NUMEROUS WARNING LIGHTS ON. *S/D* DIMMING AND TEST MODULE INOPERATIVE. REPLACED THE DIMMING AND TEST MODULE.SDR 2000UALA00216Indicator · malfunctionedNR 1 ENGINE LOST 9 - 10 PERCENT OF THRUST FROM TARGET CLIMB N1. *S/D* REPLACED THE NR 1 N1 INDICATOR.SDR 2000UALA00215Controller · failedALTITUDE WARNING HORN SOUNDED AT FL290. *S/D* THE CABIN PRESSURE CONTROLLER FAILED. REPLACED THE CABIN PRESSURE CONTROLLER.SDR 2000UALA00738Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00200Gcu · failedONE ENGINE GENERATOR OFF BUS WOULD NOT RESET. *S/D* REPLACED GENERATOR CONTROL UNIT. OPS CHECK GOOD.SDR 2000UALA00187Wire · inoperativeAFT GALLEY ELECTRONIC EGRESS LIGHT STRIP INOPERABLE. REPLACED FEEDER CABLE.SDR 2000UALA00186Wire · arcedWING SCAN LIGHT WIRES ARCHING AT ELEVATOR CONTROL CABLE. *S/D* DURING TROUBLESHOOTING OF THE WING SCAN LIGHT, IT WAS DISCOVERED THAT THE POWER WIRE FOR THE FORWARD WING SCAN LIGHT (W282-001-18) WAS CHAFING AGAINST THE LEFT HAND ELEVATOR CABLE EB. THE CHAFISDR 2000UALA00180Relay · intermittentINTERMITTENT STANDBY POWER LIGHT IN FLIGHT. LIGHT WOULD COME ON AND STAY ON REGARDLESS OF SWITCH POSITION. *S/D* REPLACED RELAY R330. OPS CHECK GOOD.SDR 2000UALA00737Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00168Probe · looseCREW NOTICED FUEL IMBALANCE AND COULD NOT MONITOR FUEL AMOUNT IN LEFT TANK DUE TO INOP FUEL GAUGE. *S/D* PERFORMED NR 2 FUEL QUANTITY INDICATING SYSTEM DRY CALIBRATION AND RESISTANCE, CAPACITANCE CHECKS OF TANK AND COMPENSATOR UNITS. FOUND PROBE F8 BAD. RESDR 2000UALA00166Duct · damagedEQUIPMENT SUPPLY COOLING ALTERNATE LIGHT CAME ON IN FLIGHT AND EFIS SCREENS WENT BLANK (LOST COLOR). COLOR CAME BACK (LIGHT WENT OUT), FOLLOWING RETURN TO THE AIRPORT. *S/D* FOUND ORIFICE ASSEMBLY MISSING FROM EFIS COOLING SUPPLY DUCT. INSTALLED MISSING ORSDR 2000UALA00728Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2001UALA00643Control 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. HESDR 2000UALA00150Housing · fodTHE CONTROL WHEELS STUCK IN THE FULL RIGHT AILERON POSITION. THE RIGHT AILERON AND FLIGHT SPOILERS WERE FULLY EXTENDED. *S/D* THE TRANSFER MECHANISM (P/N: 65-54200-15) WAS FOUND TO HAVE RECENT WITNESS MARKS ON THE LOWER BEARING HOUSING WHICH SUGGESTS THE JASDR 2000UALA00736Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00136Sensor · contaminatedTHE NOSE LANDING GEAR AMBER LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. *S/D* FOUND LANDING GEAR HAD HEAVY ACCUMULATION OF ICE. CLEANED GEAR AND SENSOR. JACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES. NOSE GEAR INDICATION NORMAL. THIS AIRCRAFT HAS NOT HAD ASDR 2000UALA00743Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00105Fire Detector · shortedTHE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. THE INDICATION EXTINGUISHED AND ILLUMINATED INTERMITTENTLY. *S/D* THE CORE DETECTION LOOP (M1122) SHORTED TO BOTH A AND B LOOPS. REPLACED BOTH LOOPS, CONTROL MODULE (M279) AND FIRE BOTTLES. PERFORMED HIGH POWERSDR 2000UALA00735Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00733Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00765Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00734Bulkhead · crackedCRACK FOUND ON THE BODY STATION 178 BULKHEAD WEB. SUPPLEMENTAL DATA UPDATE CRACKS REPAIRED PER BOEING SRM 53-10-08.SDR 2000UALA00085Module · malfunctionedTHE FLIGHT CREW DIVERTED DUE TO A LEADING EDGE SLAT INDICATION PROBLEM. *S/D* REPLACED THE LEADING EDGE SLAT/FLAP POSITION INDICATION MODULE AND PERFORMED OPERATIONAL TEST. ALL POSITION INDICATING LIGHTS OPERATED NORMAL.SDR 2000UALA00084Pulley Bracket · wornTHE SPOILER CABLE PULLEY ASSEMBLY LOWER BRACKET COMPLETELY WORE THROUGH DUE TO A MISROUTED LEFT HAND AILERON CABLE. *S/D* THE AILERON CABLE WAS DEFLECTED APPROXIMATELY 2.25 INCH. REPLACED THE PULLEY BRACKET ASSEMBLY, PULLEY AND AILERON CABLE.SDR 2000UALA00060Sensor · out of adjTHE NR 3 LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED DURING FLIGHT. *S/D* FOUND THE NR 3 LEADING EDGE FLAP FULL UP PROXIMITY SENSOR GAP OUT OF ADJUSTMENT. ADDED SHIMS TO BRING THE GAP INTO CORRECT TOLERANCE.SDR 2000UALA00056Controller · failedDURING DESCENT THE AIRCRAFT CABIN RAPIDLY DEPRESSURIZED. *S/D* THE CABIN PRESSURE CONTROLLER FAILED TO OPERATE. REPLACED THE CABIN PRESSURE CONTROLLER.SDR 2000UALA00002Actuator · failedTHE NOSE LANDING GEAR RED LIGHT WOULD NOT EXTINGUISH WITH THE LANDING GEAR HANDLE IN THE RETRACTED POSITION. *S/D* REPLACED THE NOSE LANDING GEAR ACTUATOR. TESTED THE NOSE LANDING GEAR LOGIC, POSITION AND WARNING SYSTEM.SDR 2000UALA00001Indicator · malfunctionedTHE FLIGHT CREW REPORTED THAT THE CREW OXYGEN DROPPED FROM 1800 LBS TO 600 LBS IN TWO HOURS. *S/D* REPLACED THE FLIGHT DECK CREW INDICATOR LOCATED ON THE AFT OVERHEAD PANEL.SDR 99UAL900653Tire · failedON TAKEOFF, THE CREW SUSPECTED THAT THE NOSE TIRES WERE BLOWN. REPLACED BOTH NOSE TIRES. INSPECTED ALL GEAR STRUTS, WING LOWER SURFACES AND FLAPS, NO DAMAGES NOTED.SDR 99UAL900651Structure · damagedWHILE TAXIING THE AIRCRAFT FOR MAINTENANCE, THE LEFT-HAND WING HIT A BLAST FENCE, SHEARING OFF THE WING TIP ASSEMBLY AND DAMAGING THE FRONT SPAR LOWER CHORD, LOWER WING SKIN AND THE OUTBOARD FIXED LEADING EDGE SKIN. *S/D* REPLACED THE WING TIP ASSEMBLY AND FSDR 99UAL900645Line · leakingTHE NR 1 GENERATOR TRIPPED OFF LINE TWICE. *S/D* LEAK FOUND ON OIL RETURN LINE. REPLACED O-RING.SDR 99UAL900639Odor · detectedFLIGHT CREW REPORTED KEROSENE ODOR. EXECUTED SMOKE-FUMES-ODOR PROCEDURE IN FLIGHT MANUAL. OPERATED BOTH ENGINES AND PACKS. NO FUMES OR ODOR NOTED.SDR 99UAL900638Blower · failedTHE EQUIPMENT COOLING EXHAUST FAN CIRCUIT BREAKER POPPED, CAUSING AN ELECTRICAL SMELL. *S/D* THE EQUIPMENT BLOWER MOTOR MAIN BEARING FAILED. REPLACED THE EQUIPMENT BLOWER MOTOR AND RESET THE EQUIPMENT COOLING EXHAUST FAN CIRCUIT BREAKER.SDR 99UAL900626Harness · chafedAT 120 KNOTS THE AIRCRAFT ABORTED AT TAKEOFF DUE TO NR 1 ENGINE LOW OIL PRESSURE INDICATION. *S/D* DURING TROUBLESHOOTING, THE LOW OIL PRESSURE CONNECTOR WIRES WERE SHORTED. REPAIRED EACH WIRE AND RAN THE ENGINE. THE ENGINE LOW OIL PRESSURE INDICATION SYSTSDR 99UAL900663Floorbeam · crackedDISCOVERED A CRACK OF APPROXIMATELY 1.0 INCH AT RBL 46 ON THE FLOORBEAM AT BS 927. THE CRACK LOCATED IN THE RADIUS OF THE WEB AND THE UPPER CAP OF THE I-BEAM. REPAIRED THE CRACK BY STANDARD FLOORBEAM SHEET METAL REPAIRS PER 737 SRM.
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