Boeing 737-800
Service difficulty reports · 843
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 = '737800' 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 = '737800' 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 SWAA2021092320148Fitting · cracked#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23.COMPLIED WITH E.A 21-154-02194. PERFORM REPETITIVE INSPECTIONS EVERY 8 DAYS AND PERMANENT REPAIR WITHIN 60 DAYS PER EA 21-154-02194.PERFORM SDR SWAA2021092321045Fitting · cracked#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23.C/W EA 21-154-02194 PREFORM REPETITIVE INSPECTION EVERY 8 DAYS AND PERMANENT REPAIR IN 60 DAYS. PREFORM GVI ON END OF CRACK FOR ANY PRSDR SWAA2021092321047Fitting · cracked#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23.COMPLIED WITH E.A 21-154-02194. PERFORM REPETITIVE INSPECTIONS EVERY 8 DAYS AND PERMANENT REPAIR WITHIN 60 DAYS PER EA 21-154-02194.PERFORM SDR 2021F00240Skin · dentedDENT ON LH WING FIXED LEADING EDGE UPPER SKIN, DURING TRANSIT CHECK, IT WAS DETECTED A DENT ON LH WING FIXED LEADING EDGE UPPER SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT ON LH WING FIXED LEADING EDGE UPPER SKIN STA 150.75; HFEC INSPECTSDR 2021F00238Acoustic Panel · damagedCRACK ON RH ENGINE OUTBD THRUST REVERSER INNER ACUSTIC PANEL, DURING TRANSIT CHECK, IT WAS DETECTED A CRACK ON RH ENGINE OUTBOARD THRUST REVERSER INNER ACOUSTIC PANEL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING 2 CRACKS OF 0.750" AND 0.500" ON RH ENSDR 2021F00204Blade · damagedNICKS ON RIGHT ENGINE LEADING EDGE FAN BLADES, DURING TRANSIT CHECK, IT WAS DETECTED A SEVERAL NICKS ON RIGHT ENGINE LEADING EDGE FAN BLADES. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING SEVERAL NICKS ON RIGHT ENGINE LEADING EDGE FAN BLADES NUMBERS 2,SDR 2021F00205Skin · dentedDENT ON RH HORIZONTAL STABILIZER LEADING EDGE. DURING TRANSIT CHECK, IT WAS DETECTED A DENT ON RH HORIZONTAL STABILIZER. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT ON RH HORIZONTAL STABILIZER LEADING EDGE LOCATED BETWEEN LE STA 74.93 AND LE SSDR 2021F00202Sensor · malfunctionedRETURNED TO PLATFORM BY RIGHT ENGINE OIL HIGH PRESSURE. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXYING RIGHT ENGINE OIL HIGH PRESSURE SHOWED. MAINTENANCE PERSONNEL PERFORMED REVISION TO RIGHT ENGINE, DETECTING EXCEEDANCE ALERT ABOUT OIL-PRESS-HIGH; SO THESDR 2021F00199Controller · failedRETURN TO FLIGHT DUE DURING CLIMB HAD PRESSURIZATION FAILURE. AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, IT WAS HAD A PRESSURIZATION FAILURE. MAINTENANCE PERSONNEL PERFORMED REVISION TO LEFT PRESSURIZATION CONTROLLERS, NO SHOWING FAILURE CODE; COPY FLIGHSDR 2021F00198Pump · damagedLEFT ENGINE WITH FUEL LEAK AT FUEL PUMP PACKAGE. DURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK AT LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE LEFT ENGINE WITH FUEL LEAK AT FUEL PUMP PACKAGE; SO THE FUEL PUMP WAS REPLACED IAW AMM 73SDR 2021F00197Structure · crackedCRACK ON LH ENGINE THRUST REVERSER AT LOWER INSULATION. DURING TRANSIT CHECK, IT WAS DETECTED A CRACK ON LH ENGINE THRUST REVERSER. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING A CRACK OF 1.00" LENGTH, 0.828" WIDE ON LOWER INSULATION BLANKET, ZONE 2, STSDR 2021F00211Skin · warpedWEAR ON RH WING TRAILING EDGE OUTBOARD AFT FLAP. DURING 12A CHECK AT MEX STATION, IT WAS DETECTED, IT WAS DETECTED A WEAR ON RH WING TRAILING EDGE OUTBOARD AFT FLAP. MAINTENANCE PERSONNEL PERFORMED REVISION, WEAR ON UPPER SKIN ON RH WING TRAILING EDGE OUTBOARDSDR 2021F00260Line · leakingHYDRAULIC LEAK IN THE LINE TUBE SYSTEM B, DURING TRANSIT CHECK, THE HYDRAULIC SYSTEM B WAS SHOWED WITH QUANTITY OF CERO. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING LINE TUBE HYDRAULIC SYSTEM B MAIN BAY MLG RIGHT SIDE REAR LEAKAGE; SO THE REFILL HYDRAULSDR Q2SA20210808452Sensor · out of adjustAIRCRAFT GROUNDED. LE FLAP TRANSIT ILLUMINATED AFTER TAKEOFF WITH FLAPS 1 SELECTED. COMPLIED WITH FIM 27-88 TASK 804. FOUND "L1" INBOARD SENSOR OUT OF RANGE FOR TARGET. ADJUSTED WITH SHIMS PER AMM 27-88-11-400-801. COMPLIED WITH LEADING EDGE FLAP AND PROX SENSSDR Q2SA20210807451Fseu · faultedAIRCRAFT GROUNDED. AMBER LE FLAP TRANSIT LIGHT AT FLAPS 15. FLIGHT CREWS ACCOMPLISHED QRH FOR LEADING EDGE FLAPS TRANSIT. REPLACED FLAP/SLAT ELECTRONICS UNIT (FSEU) IAW AMM 27-51-01/401. BITE AND OPS CHECK GOOD. NO DEFECTS NOTED. FURTHER TROUBLESHOOTING REMOVESDR 2021F00224Priority Valve · leaking27.07.2021 15:40 HYDRAULIC LEAK IN THE RIGHT MAIN LANDING GEAR PIT. DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RIGHT MAIN LANDING GEAR PIT. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT FLAP PRIORITY VALVE; SO THE FLAP PSDR 2021F00218Engine · damaged26.07.2021 01:39 AIRCRAFT DURING CLIMB HAD LEFT ENGINE SHUTDOWN, AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE LEFT ENGINE SHUTDOWN. MAINTENANCE PERSONNEL PERFORMED REVISION TO LEFT ENGINE CHIP DETECTOR, DETECTING METAL PARTICLE WASTE AND DURING PRELIMISDR 2021F00233Cowling · damaged22.07.2021 17:54 NICK ON LEFT ENGINE NOSE COWLING
DURING TRANSIT CHECK, IT WAS DETECTED A NICK ON LEFT ENGINE NOSE COWLING. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A NICK ON
LEFT ENGINE NOSE COWLING BETWEEN 11 AND 12 HRS POSITION; A NICK WAS RSDR 2021F00237Accumulator · leaking12.07.2021 14:26 HYDRAULIC LEAK IN THE MAIN LANDING GEAR PIT. DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE MAIN LANDING GEAR PIT. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT BRAKE ACCUMULATOR LINE AT HYDRAULIC SYSTEM B ISDR 2021F00236Hydraulic System · leaking09.07.2021 01:43 A HYDRAULIC LEAK IN THE ELEVATOR FEEL COMPUTER. DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE EMPENNAGE AREA AND FEEL DIFFERENTIAL PRESSURE LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED REVISION AT ELEVATOR, DETECTING A HYDRAUSDR Q2SA20210629447Warning Message · false activationAIRCRAFT LANDED WITHOUT INCIDENT. CREW REPORTED FLAP TRAILING EDGE DISAGREE DURING LANDING, WITH SELECTOR LEVER AT 15, INDICATION 25. FOUND FSEU BITE 830 FAULT 27 51351. PERFORMED BOEING FIM 27-50, TASK 803. NO FAULTS FOUND. REMOVED AND REPLACED FSEU IAW B737 SDR ASMF2021F00108Lubrication Unit · faulted28.06.2021 14:32 ENG 2 SHUTDOWN ON FLIGHT DUE LOW OIL PRESSURE AND QUANTITY. AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE RIGHT ENGINE PRESENTED LOW OIL PRESSURE AND QUANTITY; SO FLIGHT CREW IMMEDIATELY PERFORMED THE RIGHT ENGINE SHUTDOWN. MAINTENANCESDR ASMF2021071400107Line · leaking21.06.2021 15:30 HYDRAULIC LEAK IN TAIL CONE. DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN TAIL CONE. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT ELEVATOR FEEL COMPUTER LINE; SO THE ELEVATOR FEEL COMPUTER LINE WAS TIGHTENED SDR 2021F00165Door · bulged01.06.2021 17:11 A BULGE IN RIGHT COUNTER FRAME APU ACCESS DOOR. DURING TRANSIT CHECK, IT WAS DETECTED A BULGE IN FUSELAGE SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A BULGE OF 1.395" LENGTH, 0.156" WIDTH AND 0.010" DEPTH AT FUSELAGE SKIN SECSDR 2021F00164Packing · failed28.05.2021 20:16 RIGHT ENGINE FAN BLADE ULTRASONIC INSPECTION WITH FUEL LEAK DURING OVERNIGHT CHECK IN EO 3772031 AT MEX STATION, AFTER RIGHT ENGINE FAN BLADE ULTRASONIC INSPECTION, IT WAS DETECTED RIGHT ENGINE FUEL LEAK MAINTENANCE PERSONNEL PERFORMED REVISIOSDR 2021F00133Module · false indicationCARGO FIRE INDICATION IN FLIGHT AT CRUISE ALTITUDE. LIGHT EXTINGUISHED AFTER 5 SECONDS. NO OTHER INDICATION OF FIRE FWD COMPARTMENTSDR 2021F00160Motor · failed24.05.2021 12:00 DURING TRANSIT CHECK THE STABILIZER TRIM WITHOUT MOVEMENT DURING TRANSIT CHECK, IT WAS DETECTED THE HORIZONTAL STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING HORIZONTAL STABILIZER FAIL TO TRIM NOSE UP ANDSDR 2021F00110Acoustic Panel · damaged23.04.2021 17:35 NICK ON RIGHT ENGINE INNER BARRIER ACOUSTIC PANEL. DURING TRANSIT CHECK, IT WAS DETECTED A NICK ON RIGHT ENGINE INNER BARRIER ACOUSTIC PANEL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A NICK FROM 10.5" ON RIGHT ENGINE FWR EDGE INNESDR 2021F00048Transmitter · damagedDURING TAXIING THE STABILIZER TRIM WITHOUT MOVEMENT. AIRCRAFT RETURNED TO PLATFORM DUE TO TAXYING THE HORIZONTAL STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING BITE TO PSEU IAW FIM 22-11 TASK 801 PROCEDURE, SHOWING FAILSDR OZIA2021082300366None · damagedLARGE BIRD STRIKE LOWER NUM 1 ENG COWL. NO EXCESSIVE ENG VIBRTIO N PARAMETERS NORMAL ENG NBR 1 NOSE COWL IN PROCESS FOR REMOVAL DUE TO PARTS NEED TO BE CLEAR FROM CUSTOMS. THIS LOG PAGE IS OPEN AND THE AIRCRAF IS OUT OF SERVICE. MORE DETAILS AWAITED.SDR SWAA2021021748769Plate · crackedAFT CARGO COMPARTMENT SILL AFT CORNER PLATE CRACKED. REF SA-M 326 A1102331 FROM NRC D406118. PERFORMED W.O. INSTRUCTION NR 21-153-00322 TIME LIMITED SCUFF PLATE CRACK REPAIR SPEED TAPE APPLIED. REQUIRES RE- INSPECTION EVERY 8 DAYS MUST BE PERMANENTLY REPAIRSDR Q2SA20201017438Fmc · inoperativeAIRCRAFT GROUNDED. CLIMBING THR FL320 IAS + ALT DISAGREE ILLUMINATED. CAPT AND STANDBY AGREED F/O'S SPEED 90 KTS LOWER AND 500' HIGHER AT FL 340 DESCENDED TO FL 280 (NON RVSM) AND RETURNED TO CVG F/O'S AIRSPEED AND ALTITUDE AGREED DESCENDING THRU FL 210. SESDR SCNA20201005054Proximity Sensor · malfunctionedNOSE GEAR DISAGREED WITH LANDING GEAR LEVER (RED GEAR LIGHT) OVERHEAD GEAR INDICATED GEAR DOWN (GREEN LIGHT). AIR RETURN. EMERGENCY DECLARED. R & R PROX SENSOR S0845, REF AMM 32-61-51. OPERATIONS CHECK GOOD.SDR Q2SA20200924436Adc · malfunctionedAIRCRAFT GROUNDED. APPROX 31000-31700 W/ AUTOPILOT ENGAGED, AUTOPILOT STARTED A DECENT. WE HAD ALTITUDE DISAGREE AND AIRSPEED DISAGREE. COMPLIED W/QRH FOR ALTITUDE UNRELIABLE AIRSPEED DISAGREE 80 KT DIFFERENCE. INSPECTED LT & RT PITOT AND STATIC DRAINS FORSDR 2020F00043Connector · inoperativeSEAT MOUNTED EMERGENCY LIGHT INOP.SDR SCNA2019080023111Structure · crackedNUMBER 3 KRUGER FLAP, OTBD BULL NOSE, INBD HINGE POINT IS CRACKED. INSTALLED NEW BULL NOSE, STILL NEEDS TO HAVE BONDING WIRE SEALED WITH SEALANT. APPLIED SELANT AS NEEDED.SDR CA190524025Tire · failed(CAN) RH NOSEWHEEL SN B8045/B8045 HAD TREAD SEPARATE DURING TAKEOFF ROLL OUT. RH AND LH NOSEWHEELS REPLACED IAW AMM 32-45-11 (TC# 20190524025)SDR ASMF2019042320Idg · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT MID DUE TO DURING CRUISE, THE APU SHUTDOWN AND RIGHT IDG WAS PREVIOUS DEFERRED. MAINTENANCE PERSONNEL PERFORMED REVIEW TO SYSTEM, DETECTING APU LOW OIL PRESSURE LIGHT TURNED ON WITH LIGHTEN AND APU WAS HAD PROTECTIVSDR ASMF2019042318Line · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE HYDRAULIC SYSTEM B OF THE ENGINE DRIVEN PUMP. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT HYDRAULIC SYSTEM B IN PLUG OF RETURN FILTER MODULE; SO THE RETURN FILTER MODULE PLUG PSDR 2018FA0000538Intercostal · corrodedCORROSION FOUND IN THE BOTH FORWARD AND AFT LEFT OVERWING EMERGENCY EXITS UPPER SILL INTERCOASTAL. THE ITEM WAS GIVEN A TEMPORARY REPAIR AS PER BOEING 8100-9, EA# PD37-53-2453.SDR DALA2018112986910Skin · damaged(LOG 0843144) DURING INSPECTION FOUND EXISTING RE-WORK EXTERNAL SKIN AFT LOWER CORNER LOC. AT AFT GALLEY DOOR AT UPPER FUSELAGE. MAINTENANCE REPAIRED EXTERNAL SKIN AFT LOWER CORNER LOC. AT AFT GALLEY DOOR AT UPPER FUSELAGE ASPER ER/A 573312-14 REV. ORIGINAL ANSDR ASMF20190109010Mount · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE EICAS MESSAGE WXR FAIL WAS SHOWN; MAINTENANCE PERSONNEL PERFORMED INSPECTION DETECTING MBA 4A MOUNTING TRAY FAILED IAW AMM 34-42; SO THE WEATHER RADAR R/T MOUNT WAS REPLACED P/N: 2041213-0413 S/N: MBA4A-0SDR ASMF20190109005Warning System · false activationAIRCRAFT RETURN TO PLATFORM DUE TO BEFORE TO TAKEOFF, THE TAKEOFF CONFIGURATION ALARM AND LIGHT, PSEU LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO PSEU IAW AMM 31-51-00, SHOWING MESSAGES AND FAILURE CODES STAB TRM NOT GRN, STAB TRM GREEN AND TAKEOFSDR SCNA201809143107Flap System · malfunctionedENCOUNTERED A FLAP DISAGREEMENT. FLAP HANDLE WAS IN THE 30 DEGREE DETENT AND FLAPS INDICATED 25 ON FLAP INDICATOR. ACCOMPLISHED NNC. LAX FIRE DEPARTMENT REPORTED SMOKE COMING FROM NR 1 BRAKE AREA. PERFORMED FSEU BITE. NO FAULTS FOUND. OPERATED FLAPS 0-40, OPS SDR ASMF20180902717Seal · leakingDURING OVERNIGHT CHECK, IT WAS DETECTED AN OIL LEAK IN THE LH ENGINE. MAINTENANCE PERSONNEL PERFORMED ENGINE 3A IDLE-POWER LEAKING TEST, DETECTING AN OIL LEAK ON N2 PAD DRAIN SEAL OF 60 DROPS PER MINUTE, BEING OUT OF LIMITS IAW AMM 71-71-00; SO THE MAGNETIC SESDR ASMF20180625013Flex Hose · leakingDURING A TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED FROM FEED LINE OF SPOILER NUMBER 8 ACTUATOR, MAINTENANCE REPLACED THE FLEX HYDRAULIC LINE AT THE SPOILER ACTUATOR IAW AMM 20-10-52.SDR DALA201804262834Seat Track · wornDURING INSPECTION, FOUND THE FIRST OFFICER`S INBD SEAT TRACK WORN. MAINTENANCE REPLACED THE WORN TRACK SECTION IAW AMM 25-11.SDR DALA2018042652833Seat Track · wornDURING INSPECTIONM FOUND THE CAPTAIN`S AFT INBOARD SEAT TRACK WORN. MAINTENANCE REPLACED THE SEAT TRACK SECTION IAW AMM 25-11.SDR ASMF201803002Shutoff Valve · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DUCT PRESSURE LOW INDICATION IN THE RIGHT ENGINE, SHOWING 18 PSI. MAINTENANCE PERFORMED REVISION IAW 36-11-00, DETECTING A PNEUMATIC LEAK IN THE RIGHT ENGINE PRSOV. THE RIGHT ENGINE PRSOV AND THE RIGHT ENGINE BLEED AIR REGSDR SWAA2018012419293Control Module · faultyLAVATORYIES STOPPED WORKING IN FLIGHT. R & R THE LOGIC CONTROL MODULE IAW AMM.
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