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 SWAA2017013011531Wedge · damagedRT WING NR 7 SLAT WEDGE OUTBOARD LOWER SURFACE MISSING DOUBLER. R & R THE NR 7 SLAT IAW AMM.SDR SWAA2017012611496Battery · dischargedRT EMERGENCY AISLE LIGHT INOP AT ROW 8. R&R BATTERY PER AMM.SDR SWAA2017012611480Battery · dischargedLT EMERGENCY AISLE LIGHT INOP BETWEEN ROW 7 TO ROW 13. R&R BATTERY PER AMM.SDR ASMF201702005Pcu · failedAIRCRAFT RETURNED TO PLATFORM AFTER START OF ENGINES, THE THRUST REVERSER UNIT LIGHT TURNED ON. PERFORMED BITE TO SPCU MODULE IAW FIM 24-31 TASK 801 PROCEDURE, CONFIRMING THE FAILURE. THE SPCU MODULE WAS REPLACED IAW AMM 24-34-11, TESTED CORRECT.SDR SWAA2017012511457Web · damagedAFT CARGO DOOR SUB THRESHOLD WEB DAMAGED. R&R WEB IAW SRM AND DWG.SDR SWAA2017011811244Intercostal · crackedINTERCOSTAL CRACKED BETWEEN BS 277 TO 294.5, BL 0. R & R INTERCOSTAL IAW SRM AND DWG.SDR SWAA2017012611479Skin · erodedVERTICAL STABILIZER LEADING EDGE ERODED AT COMPOSITE PANEL. R&R VERTICAL STABILIZER PER WO.SDR SWAA2017012511456Strap · corrodedAFT CARGO DOOR STRAP CORRODED AT BS 809, RBL 19. R&R STRAP IAW SRM AND DWG.SDR SWAA2017012511455Fitting · crackedFLOOR SUPPORT CLIP CRACKED AT BS 867, LBL 10. R&R CLIP PER SRM AND DWG.SDR SWAA2017011811259Web · corrodedSUB THRESHOLD WEB CORRODED UPPER AND LOWER SURFACE. R & R THE WEB IAW SRM AND DWG.SDR SWAA2017011811249Support Angle · crackedSUPPORT ANGLE CRACKED AT BS 948, LBL 11. R & R THE SUPPORT ANGLE IAW SRM AND DWG.SDR SWAA2017010410949Cover · detachedRIGHT OVERWING EXIT SIGN COVER DETACHED. SECURED THE SIGN IAW AMM.SDR SWAA2016120910345Battery Pack · failedAFT RT EMERGENCY BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.SDR SWAA2016120910344Flap Track · looseRT WING OUTBOARD AFT FLAP OUTBOARD FLAP TRACK LOOSE AT AFT ATTACH POINT. R&R TRACK IAW AMM.SDR SCNA20161201329Sensor · faultyFLAP ASYMMETRY ON TAKEOFF. FLAPS LOCKED AT 2 DEGREES FLAP POSITION INDICATION SPLIT AT 2 DEGREES. REMOVED AND REPLACED NR 3 FLAP SKEW SENSOR. ACCOMPLISHED FLAP SENSOR FUNCTIONAL CHECK. ALL FLAP SENSOR WITHIN LIMITS. OK FOR SERVICE.SDR SWAA2016120110096Girt Bar · looseL2 DOOR EMERGENCY EVAC SLIDE GIRT LOOSE. SECURED GIRT PER MT.SDR SWAA2016120110095Girt Bar · looseR1 DOOR EMERGENCY EVAC SLIDE GIRT LOOSE. SECURED GIRT PER MT.SDR SWAA2016111609762Light · inoperativeRT OVERWING EMERGENCY LIGHT INOP. RELAMPED BULB PER AMM.SDR ASMF20161216007Window · crackedAIRCRAFT RETURNED FROM FLIGHT DUE TO DURING CRUISE THE PASSENGER WINDOW 1A GOT CRACKED. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL REPLACED THE PASSENGER WINDOW 1A IAW AMM 56-21-00, TESTED CORRECT. THE GROUND HANDLING EQUIPMENT HITS AIRPLANE OR SDR ASMF20161216006Coupling · brokenAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE CREW OXYGEN CYLINDER WAS LEAKING WITH STRONG NOISE AND OXYGEN LOW LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED AN OXYGEN CREW INSPECTION IAW MM 35-12-85, DETECTING OXYGEN CYLINDER MANOMETER WITH 0 PSI ANSDR SWAA2016110309347Sign · missingL1 DOOR FRAME BULKHEAD LOWER EXIT SIGN MISSING RED ARROW. R&R SIGN PER AMM.SDR ASMF201612002Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM DUE TO HIGH PASSENGER CABIN TEMPERATURE WITHOUT LIGHT INDICATION. MAINTENANCE PERSONNEL PERFORMED THE FIM 21-61 TASK 801 PROCEDURE, NO CONFIRMING FAILURE.SDR ASMF201611022Bleed Valve · leakingDURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK IN THE RIGHT ENGINE. THE PLATFORM WAS CLEANED AND MAINTENANCE PERFORMED REVISION, DETECTING FUEL LEAK IN THE TRANSIENT BLEED VALVE WITH 4 DROPS PER MINUTE WITHIN OPERATION LIMITS IAW AMM 71-71-00 PAGE 6, DISPASDR SWAA2016093008310Slide · out of positionR1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.SDR ASMF201611016Sensor · failedCAPTAIN REPORTED THAT DURING CRUISE AT 400 FL, LE FLAPS TRANSIT AND FULL EXTEND SLAT NUMBER 1 LIGHTS ILLUMINATED. MAINTENANCE PERFORMED BITE TO FSEU IAW FIM 27-51 TASK 801 PROCEDURE, SHOWING FAILURE AT POSITION SENSOR OF SLAT NUMBER 1; SO THE PROXIMITY INBOARDSDR SWAA2016092608175Wire · disconnectedEMERGENCY LIGHT BATTERY PACK DISCONNECTED AT BS 727C+13. CONNECTED BATTERY PACK IAW AMM.SDR SWAA2016092608174Lens · dirtyR2 DOOR AFT EMERGENCY LIGHT LENS DIRTY. CLEANED LENS IAW AMM.SDR SWAA2016092608173Lens · dirtyRIGHT WING TO BODY FAIRING AFT EMERGENCY LIGHT LENS DIRTY. CLEANED LENS IAW AMM.SDR SWAA2016092608172Lens · dirtyLEFT WING TO BODY FAIRING AFT EMERGENCY LIGHT LENS DIRTY. CLEANED LENS IAW AMM.SDR ASMF201611013Fuel Heater · leakingAIRCRAFT RETURNED TO PLATFORM DURING TAXING, A FUEL LEAK WAS DETECTED IN THE LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE FUEL SERVO HEATER DAMAGED; SO THE LEFT FUEL SERVO HEATER WAS REPLACED IAW AMM 73-11-07 AND LEFT ENGINE WAS RUN IAWSDR ASMF201610022Fuel Heater · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, A FUEL LEAK WAS DETECTED IN THE LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE FUEL SERVO HEATER DAMAGED; SO THE LEFT FUEL SERVO HEATER WAS REPLACED IAW AMM 73-11-07 AND LEFT ENGINE WAS SDR ASMF201611010Screw · out of positionCAPTAIN REPORTED THAT BEFORE TAXING, THE LEFT RUDDER WAS NOT MOVED FREELY. MAINTENANCE PERSONNEL PERFORMED THE FIM 27-21 TASK 806 PROCEDURE, DETECTING A SCREW OUT OF POSITION JAMMING THE PEDAL FROM THE BOTTOM UP TO THE CAPTAIN LEFT PEDAL COVER; SO THE SCREW WASDR ASMF201610019Rudder Pedal · bindingCAPTAIN REPORTED THAT BEFORE TAXING, THE LEFT RUDDER WAS NOT MOVED FREELY. MAINTENANCE PERSONNEL PERFORMED THE FIM 27-21 TASK 806 PROCEDURE, DETECTING A SCREW OUT OF POSITION JAMMING THE PEDAL FROM THE BOTTOM UP TO THE CAPTAIN LEFT PEDAL COVER; SO THE SCREW WASDR SWAA2016090855608Battery Pack · inoperativeFORWARD ENTRY EMERGENCY LIGHT BATTERY PACK INOPERATIVE. R & R BATTERY PACK IAW MM.SDR ASMF201611007Line · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN ALTERNATE BRAKE SELECTOR VALVE LINE. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT ALTERNATE BRAKE SELECTOR VALVE LINE; SO THE LINE WAS REPLACED IAW AMM 32-41-93, TESTED CORRECT.SDR ASMF201610016Line · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN ALTERNATE BRAKE SELECTOR VALVE LINE. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT ALTERNATE BRAKE SELECTOR VALVE LINE; SO THE LINE WAS REPLACED IAW AMM 32-41-93, TESTED CORRECT.SDR SWAA2016090655513Window Frame · crackedFLIGHT DECK L1 WINDOW FRAME UPPER OUTBOARD CORNER CRACKED. REPAIRED THE WINDOW FRAME IAW ACO.SDR SWAA2016090655512Window Frame · crackedFLIGHT DECK L1 WINDOW FRAME CRACKED. REPAIRED THE WINDOW FRAME IAW ACO.SDR SWAA2016092608171Light · brokenFORWARD ENTRY LOWERED CEILING EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT IAW SOPM.SDR SWAA2016090155352Lens · dirtyLEFT EXTERNAL EMERGENCY LIGHT LENS DIRTY, JUST FORWARD OF WING TO BODY FAIRINGS. CLEANED LENS IAW SOPM.SDR SWAA2016090155348Lens · dirtyLEFT EXTERNAL EMERGENCY LIGHT LENS DIRTY, JUST AFT OF WING TO BODY FAIRINGS. CLEANED LENS IAW SOPM.SDR SWAA2016092608170Window Frame · crackedFLIGHT DECK R1 WINDOW FRAME INNER CORNER CRACKED. REPAIRED THE WINDOW FRAME IAW ACO.SDR SWAA2016082255049Slide · out of positionR1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITON. REPOSITIONED THE SLIDE IAW MT AND MM.SDR SWAA2016090955643Pin · looseRT EMERGENCY EXIT DOOR OPENING AFT UPPER DOOR STOP FITTING PIN LOOSE. SECURED PIN IAW AMM.SDR ASMF201610008Pulley · stuckAIRCRAFT RETURNED TO PLATFORM DURING FLIGHT CONTROL CHECK, THE LEFT FLIGHT SPOILER WAS DEPLOYED PARTIALLY AFTER BOTH ENGINES START. MAINTENANCE PERSONNEL CHECKED LEFT SPOILER CONTROL SYSTEM, CABLE GUARDS, CONTROL CABLE PULLEYS AND BRACKETS IAW AMM 27-61-00/601SDR SWAA2016082255030Lens · missingR1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. R & R LIGHT ASSEMBLY IAW AMM.SDR SWAA2016090955642Slide · frayedR2 DOOR EMERGENCY EVAC SLIDE GIRT FRAYED. R & R SLIDE IAW MAINTENANCE.SDR SWAA2016083055279Beam · crackedR1 DOOR CUTOUT FWD STUB BEAM CRACKED AT BS 294.5, WL 210. R & R STUB BEAM IAW SRM.SDR ASMF201610006Speed Brake · out of alignmentDURING TRANSIT CHECK, THE LEFT WING SPEED BRAKE DOOR NUMBERS 3, 4 AND 5 WERE OUT OF ALIGNMENT. MAINTENANCE PERSONNEL PERFORMED THE SPOILERS CONTROL SYSTEM CABLE LUBRICATING AND SPEED BRAKE CONTROL SYSTEM OPERATIONAL TEST IAW AMM 12-26-00 AND AMM 27-62-00, ALL SDR SWAA2016083055278Web · corrodedWEB CORRODED BETWEEN BS 947 TO BS 967, STR 20L. R & R WEB IAW DWG AND SRM.
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