Boeing 737-752
Service difficulty reports · 2,590
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 = '737752' 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 = '737752' 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 ASMF201109010Seal · damagedDURING TRANSIT CHECK IT WAS DETECTED AN OIL LEAK IN THE RT ENGINE IDG DRAIN SEAL; SO THE RT ENGINE IDG GEARBOX MAGNETIC CARBON SEAL WAS REPLACED IAW MM 72-60-00 AND DRY MOTOR LEAK TEST WAS PERFORMED IAW MM 71-00-00, TESTED CORRECT.SDR ASMF201109007Skin · damagedDURING TRANSIT CHECK, MX PERSONNEL DETECTED 1 DENT WITH NICK ON FWD CARGO DOOR SKIN AT STA 467 BETWEEN LONGERONS 19 AND 20 OF 1.562 LONG, 1" WIDE AND 0.047" DEPTH. MX PERSONNEL CONFIRMED THAT THE DENT WAS OUT OF LIMITS IAW SRM 52-30-01. ACFT WAS SENT TO THE SDR ASMF201108011Seal · damagedDURING TRANSIT CHECK, A HYD LEAK WAS DETECTED IN THE RT THRUST REVERSER WITH 20 DROPS PER MINUTE; SO THE REPORT WAS DEFERRED IAW MEL 78-1 CAT C. DURING OVERNIGHT CHECK, THE SUPPLY HYD LINE SEALS OF ACTUATOR WERE REPLACED IAW MM 78-31-03, TESTED CORRECT AND THSDR ASMF201108010Door · out of adjustACFT RETURNED TO DEPARTURE DURING CLIMB, THE ACFT DID NOT PRESSURIZE WITH DOOR TOTALLY CLOSED AND PRESSURE LIGHT REMAINING OFF. DURING MX REVISION, THE FORWARD ENTRY DOOR WAS DETECTED .5" MISADJUSTED, BEING NECESSARY TO PERFORM SEVERAL CYCLES UNTIL CLOSE, AS SDR ASMF201108006Windshield · brokenACT PERFORMED AN UNSCHEDULED LANDING, DUE TO L1 WINDSHIELD BROKEN. THE FLIGHT CREW PERFORMED THE QRH 1.14 PROCEDURE, CONFIRMING THE FAILURE. MX REPLACED THE L1 WINDSHIELD ASSY IAW MM 56-11-11 AND WINDOW HEAT SYS TEST WAS PERFORMED IAW MM 30-41-00, ALL CORRECTSDR ASMF201108004Radome · damagedCAPTAIN REPORTED THAT DURING TAKEOFF, ACFT FLEW INTO A HAIL RAIN. A HAIL STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-18-212-801 DETECTING LT AND RT RETRACTABLE LANDING LIGHTS WITH CRACKS, NOSE RADOME WITH DAMAGES OUT OF LIMITS; VHF COMMUNICATION SDR ASMF201108001Carbon Seal · damagedDURING TRANSIT CHECK IT WAS DETECTED AN OIL LEAK THROUGH THE LT ENGINE IDG, MX REPLACED THE LT ENGINE IDG CARBON SEAL AND TEST WAS PERFORMED IAW AMM 72-60-00 AND AMM 79-00-00, ALL CORRECT.SDR ASMF201107006Access Panel · damagedDURING OVERNIGHT CHECK, TECH DETECTED A FUEL LEAK IN LEFT WING MAIN TANK ACCESS DOOR NR 532AB; MX TIGHTEN THE SCREWS NOT CORRECTING THE LEAK, SO THEY REMOVED THE ACCESS DOOR FINDING THE RUBBER SEAL AND THE ALUMINUM GASKET DAMAGED. ACCESS DOOR, RUBBER SEAL ANDSDR ASMF201107005Regulator · damagedACFT RETURNED TO DEPARTURE, DUE TO THE RIGHT PACK BLEED TRIP OFF LIGHT TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE. MX REPLACED THE RT ENGINE BLEED AIR REGULATOR IAW MM 36-11-03 AND FIM 36-10 TASK 801 PROCEDURE WAS PERFSDR ASMF201106003Shimmy Dampener · leakingDURING TRANSIT CHECK, A HYD LEAK WAS DETECTED IN THE RT SHIMMY DAMPER MLG HYD; SO THE RT SHIMMY DAMPER MLG HYD WAS REPLACED IAW MM 32-11-81, TESTED CORRECT.SDR ASMF201106002Guide Arm · deformedDURING TRANSIT CHECK, THE MAIN DOOR WAS HIT BY A JETWAY PROMOTING A DEFORMED GUIDE ARM OF THE UPPER HINGE ARM AND 2 NICKS AT AFT EDGE OF THE LT FORWARD ENTRY DOOR. MX ISSUED THE NON ROUTINE CARD A0176793, A0176794 AND A0176795. THE GUIDE ARM OF THE LT FWD ENTSDR ASMF201105017Nose Cowl · crackedDURING OVERNIGHT CHECK, DETECTED A CRACK OF 3.5 INCH LENGTH NEAR FORWARD L/E AT 6 HOURS POSITION IN LT ENGINE NOSE COWLING. MX REPLACED THE LT ENGINE NOSE COWLING IAW MM 71-11-02, ALL CORRECT.SDR ASMF201105015Battery · damagedCAPTAIN REPORTED THAT DURING CRUISE STRONG FUMES WERE PERCEIVED IN BOTH GALLEY AREAS WITH NO EVIDENCE OF SMOKE, DISAPPEARING AFTER TRIPPING OFF GALLEYS CIRCUIT BREAKERS. MX PERFORMED A REVISION DETECTING THE MAIN BATTERY WITH HIGH TEMPERATURE AND FUMES; SO THSDR ASMF201105009Oil System · leakingDURING TRANSIT CHECK WAS DETECTED AN OIL LEAK IN THE RT ENGINE. MX PERFORMED INSP IAW AMM 71-00-00 PAGES 12 AND 14, NO LEAKS WERE DETECTED.SDR ASMF201105005Structure · dentedDURING TRANSIT CHECK A BIRD STRIKE WAS ON THE RT WINDSHIELD AND RT HORIZONTAL STABILIZER L/E. MX PERSONNEL PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING A DENT OF 20.0 X 6.0 INCHES, WITH 1.125 INCH BETWEEN STA 81.5 TO 101.5; IT WAS CONFIRMED THAT DENT WSDR ASMF201101004Target · out of adjustACFT REJECTED TAKEOFF AT LESS THAN 80 KNOTS DUE ELECTRONIC EQUIPMENT ACCESS DOOR LIGHT TURNED ON. DURING MX REVISION, THE ELECTRONIC EQUIPMENT ACCESS DOOR WAS DETECTED CLOSED AND ENSURED; ACFT WAS DISPATCHED IN SUCH CONDITION. THE HIGH ENERGY STOP INSP WAS NOSDR ASMF201101003Strut · damagedDURING TRANSIT CHECK, A HYD SLIP WAS DETECTED IN THE LT MLG SHOCK ABSORBER. DURING MX REVISION, THE MLG SHOCK ABSORBERS WERE COMPRESSED; SO ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED A MLG SERVICE IAW MM 12-15-31, ALL CORRECT AND THE MLG SHOCK STRUSDR ASMF201101002Carbon Seal · damagedCAPTAIN REPORTED THAT DURING CRUISE, THE RT ENGINE OIL QUANTITY DECREASED AND THE OIL QUANTITY REACHED 1 QUARTER DURING DESCENT, SO FLIGHT CREW ACCOMPLISHED THE QRH 7.21 AND 7.14 PROCEDURES AND SHUT DOWN THE ENGINE. ACFT WAS SENT TO THE HANGAR AND DURING OVERSDR ASMF201101001Control Cable · out of adjustCAPTAIN REPORTED THAT DURING CRUISE, ACFT REQUIRED 10 UNITS OF RT OF RUDDER AND AILERON COMPENSATOR TO MAINTAIN STRAIGHT AND LEVELED FLIGHT. ACFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK MX ADJUSTED THE RUDDER AND AILERON CONTROL CABLES IAW MM 27-21-SDR ASMF201012010Wheel · damagedACFT RETURNED TO PLATFORM DURING TAXING, BOTH NLG TIRES WERE PASSED ON TAXI LIGHT. MX PERFORMED THE NLG INSP IAW MM 32-21-00 DETECTING DAMAGE SCRATCHED THE RT NOSE LANDING WHEEL; SO RT NOSE LANDING WHEEL WAS REPLACED IAW MM 32-45-21, ALL CORRECT.SDR ASMF201012008Skin · crackedCRACK OF 0.5 INCHES ON EDGE OF AFT CARGO COMPARTMENT DOOR SCUFFS PLATE AND DENTS ON FUSELAGE SKIN NEAR AFT CARGO COMPARTMENT DOOR OF 3.0 X 0.102 INCHES AND 4.0 X 0.126 INCHES FROM STA 807 TO 827 BETWEEN S-25R AND S-27L. MX ISSUED THE NON ROUTINE CARD A0169176SDR ASMF201012007Brake · damagedDURING TRANSIT CHECK, TECH DETECTED THE MLG BRAKE NR 2 WITH THE INNER BEARING SEPARATED OF THEIR RETAINING RING AND HUBCAP; ALSO, MLG BRAKE BUSHING DID OUT OF POSITION, SO TECH REPLACED THE MLG BRAKE NR 2 IAW MM 32-45-11, ALL CORRECT.SDR ASMF201012003Skin · crackedCAPTAIN REPORTED A BIRD STRIKE IN RT WING DURING LANDING. ACFT WAS SENT TO THE HANGAR AND MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING CRACK IN THE L/E SLAT NR 6; SO IT WAS REPLACED IAW MM 27-81-54, TESTED CORRECT.SDR ASMF201011003Wheel · damagedMX PERSONNEL DETECTED SMOKE IN THE WHEEL AND TIRE ASSY NR 4, SO THEY PERFORMED A BRAKE SEIZURE CONDITIONAL INSP IAW MM 05-51-15, DETECTING THE BEARING CUPS AND CONES OF THE WHEEL AND TIRE ASSY NR 4 MELTED AND STUCK WITH THE AXLE. MX REPLACED THE MAIN WHEEL ANSDR ASMF201010004Seal · damagedDURING TRANSIT CHECK, TECH ADDED 4 QTS OF OIL IN THE RT ENGINE AND PERFORMED A REVISION DETECTING WET THE IDG GEARBOX WITHOUT EXTERNAL LEAK. ACFT WAS SENT TO THE HANGAR AND THE RT ENGINE GEARBOX IDG COUPLING CARBON SEAL WAS REPLACED IAW MM 72-60-00 TASK 72-60SDR ASMF201010003Carbon Seal · damagedDURING TRANSIT CHECK, TECH DETECTED AN OIL LACK IN THE IDG GEARBOX CARBON SEAL IN THE LT ENGINE. ACFT WAS SENT; SO IT WAS REPLACED AND LEAK TEST WAS PERFORMED IAW MM 72-60-00 AND MM 24-11-11, ALL CORRECT.SDR ASMF20101002Access Panel · crackedDURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN RT WING MAIN TANK DUE TO A CRACK AT DRIP STICK NR 4 OF THE FUEL TANK ACCESS DOOR PANEL NR 632FB. MX PERFORMED FUEL LEAK INSP DETECTING FUEL LEAK IN LIMITS IAW MM 28-11-00 PAGE 604. AT MEX, THE FUEL TANK ACCESSDR ASMF201009007Warning Light · illuminatedACFT REJECTED TAKEOFF AT LESS THAN 80 KNOTS AND GROSS WEIGHT 61267 KG DUE AFT SERVICE DOOR LIGHT TURNED ON. DURING MX REVISION, THE PSEU AND AFT SERVICE DOOR WERE CHECKED IAW FIM PROCEDURE 52-10 TASK 801 AND MM 52-13-00, THE LIGHT TURNED OFF. THE HIGH ENERGYSDR ASMF201009005Skin · dentedDURING TRANSIT CHECK A BIRD STRIKE WAS DETECTED ON THE RT SIDE HORIZONTAL STABILIZER L/E. MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING DENT OF 12.00 X 3.50 INCHES, WITH 0.400 INCH DEPTH LOCATED IN STA 78.5. THE RT SIDE HORIZONTAL STABILIZER L/E WAS SDR ASMF201009004Gasket · failedDURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN LT WING MAIN TANK DUE TO A CRACK IN THE GASKET AND SEAL OF THE FUEL TANK ACCESS DOOR PANEL NR 532CB, SO THEY WERE REPLACED AND LEAK TEST WAS PERFORMED IAW AMM 28-11-11, ALL CORRECT.SDR ASMF201009003Structure · crackedDURING TRANSIT CHECK A BIRD STRIKE WAS DETECTED ON THE RT SIDE HORIZONTAL STABILIZER L/E. MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING DENT WITH CRACK AND HOLE OF 6 X 3 INCHES LOCATED IN STA 321.67. THE RT SIDE HORIZONTAL STABILIZER L/E WAS REPLACED SDR ASMF201009002Sleeve · out of limitsDURING OVERNIGHT CHECK WAS DETECTED A LIGHTNING STRIKE IN THE RT ENGINE OTBD SLEEVE REVERSER. TECH PERFORMED A LIGHTNING STRIKE INSP IAW MM 05-51-19 DETECTING LOOSE MATERIAL IN THE MENTIONED REVERSER, OUT OF OPERATION LIMITS. TECH REPLACED RT ENGINE THRUST REVSDR ASMF201007007Seal · damagedDURING OVERNIGHT CHECK, TECH PERSONNEL DETECTED A OIL LEAK IN SEAL OF THE IDG OF THE RT ENGINE, SO IT WAS REPLACED AND LEAK TEST WAS PERFORMED IAW AMM 72-60-00, ALL CORRECT.SDR ASMF201007005Sleeve · out of limitsDURING OVERNIGHT CHECK, WAS DETECTED A LIGHTNING STRIKE IN THE LT ENGINE REVERSER. TECH PERFORMED A LIGHTNING STRIKE INSP IAW MM 05-51-19 DETECTING MATERIAL LOOSE OUT LIMITS OF OPERATION. TECH REPLACED LEFT ENGINE THRUST REVERSER SLEEVE IAW MM 78-31-02, ALL CSDR ASMF100109001Retaining Ring · damagedACFT PERFORMED AN UNSCHEDULED LANDING, DURING CLIMB AT 18,500 FEET, THE LT ENG WAS SHUTDOWN SUDDENLY. MX PERSONNEL REVIEWED THE ENGINE AND CHIP DETECTORS AND NO DAMAGES WERE FOUND, SO BOROSCOPE INSPECTION WAS PERFORMED ON COMPRESSOR AND TURBINE, DETECTING HPTSDR ASMF200910005Pump · leakingDURING FLIGHT, THE ENG 2 LOW PRESSURE LIGHT TURNED ON WITH CODE 293 210 52. MX DETECTED A HYD LEAK ON RT HYD PUMP, SO HYD PUMP WAS REPLACED IAW MM 29-11-11, TESTED CORRECT.SDR ASMF200910004Carbon Seal · leakingDURING OVERNIGHT CHECK, A FUEL AND OIL LEAKS WERE DETECTED ON HPTACC VALVE DRAIN AND ON HYD PUMP DRAIN. MX REPLACED THE FUEL PUMP AND THE HYD PUMP CARBON SEAL IAW MM 75-21-01 AND 72-60-00, TESTED CORRECT.SDR ASMF200910001Valve · leakingACFT RETURNED TO PLATFORM DUE TO A RT ENGINE FUEL LEAK. MX DETECTED A FUEL LEAK OUT OF LIMITS IAW MM 71-71-00 PAGE 606, PROCEEDING FROM THE HPTACC VALVE. ACFT WAS SENT TO THE HANGAR AND HPTACC VALVE WAS REPLACED AND TESTED IAW MM 75-21-01 AND TASK 71-00-00-7SDR ASMF200907003Control Module · burnedACFT RETURNED DUE TO OVERHEAT LIGHT TURNED ON AND RT WINDSHIELD ASSY BROKEN AT 17,000 FEET. MX REPLACED THE WINDOW HEAT CONTROL MODULE AND RT WINDSHIELD ASSY IAW MM 30-41-11 AND 56-11-11, TESTED CORRECT. OVERWEIGHT INSP WAS NOT NECESSARY DUE TO THE ACFT LANDESDR ASMF200907001Fuel Tank · leakingDURING TRANSIT CHECK A FUEL LEAK WAS DETECTED ON LT WING. MX PERSONNEL REPLACED THE LT WING FUEL TANK ACCESS PANEL IAW MM 28-11-11 PAGE 401, TESTED CORRECT.
Back to Boeing 737-752