Boeing 737-83N
Service difficulty reports · 1,087
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 = '73783N' 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 = '73783N' 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 SCNA20230206062Intercostal · corrodedDEFECT TC 203350000 NR 00129: CORROSION ON FWD CARGO BAFFLE BS 500A - 500B RBL 25 WL 156. RESOLUTION. R/R BAFFLE BS 500A - 500B RBL 25 WL 156 IAW B737 SRM 51-40-02-0G-0 DWG 143A7505.SDR SCNA20230206060Not Reported · crackedDEFECT TC 203350000 NR00138: FWD CARGO COMPARTMENT BAFFLE CLIP AT BS 500H LBL 25 WL 156 FWD SIDE OF FRAME CRAKCED. RESOLUTION: R/R BAFFLE CLIP AT BS 500H LBL 25 WL 156 FWD SIDE OF FRAME IAW SRM 51-40-02-0G-0 AND DWG 143A7505SDR SCNA20221229152Girt Bar · out of adjustL1 GIRT BAR ON SLIDE DIFFICULT TO ARM/DISARM. ADJUSTED GIRT BAR REF AMM 25-66-01. OK FOR SERVICE.SDR 2022F00468Windshield · arcedQRF TO GRU AIRPORT. AT 15000FT WE HAD L1 WINDSHIELD ELECTRICAL ARCSDR SCNA20221017131Girt Bar · damagedFOUND RELEASE STOP ASSY ON R1 GIRT BAR MISSING. INSTALLED GIRT BAR RELEASE STOP ASSY REF AMM 25-66-01 THIS CLEARS MEL 25-10 MDDR#114432SDR SCNA20221012128IStop Fitting · missingDEFECT 716420: FOUND RELEASE STOP ASSY ON R1 GIRT BAR MISSING RESOLUTION: (IN PROGRESS)SDR SCNA20221011126Autothrottle Sys · failedDEFECT : LEFT AUTO THROTTLE FAILS TO ADVANCE DURING TAKEOFF. RESOLUTION: REF LOGPAGE 71649 ITEM #2 R&R GEARBOX ASSY IAW AMM 22-31-00. THIS CLEARS MEL 22-4 MDDR# 114373.SDR UIEA2022100801100Processor · unbalancedFUEL IMBAL (QRH 12-15). LH ENGINE SHUTDOWN (QRH R 6). SINGLE ENGINE EMERGENCY LANDING(PERFORMED INITIAL VISUAL INSPECTION FOR LEAKS IN THE SYSTEM, OPERATED BOTH ENGINES & INSPECTED FUEL LINES & NOZZLE FOR EVIDENCE OF LEAKS. PERFORMED FQIS BITE, FOUND FAULTS 28SDR SCNA20221005123Flap System · warning lightDEFECT 724694: AFTER FLAPS WERE SET T 5 WITH A LE FLAPS EXT GREEN LIGHT LE FLAPS INTRANSIT AMBER LIGHT COMES ON WITH #2 AMBER LIGHT OVERHEAD PANEL THEN EXTINGISHED FLAPS WERE RAISED TO UP AND INTRANSIT AND #2 COMES ON AGAIN. RESOLUTION: PERFORMED FIM TASSDR SCNA20220920108None · noneDEFECT 725253: LOSS OF SYSTEM B HYDRAULIS IN FLIGHT. RESOLUTION: FOUND PLUG ON B SYSTEM HYD MODULE TO BE LOOSE TIGHTENED PLUG R& R # 2 ENG ENGINE DRIVE PUMP PER AMM 29-11-11 OPS & LEAK CHECK GOOD OK FOR SERVICESDR SCNA20220715080Girt Bar · stiffDEFECT: 2L GIRT BAR DIFFCULT TO REMOVE FROM CLIPS WHEN ARMING. RESOLUTION: GIRT BAR WITHIN LIMITS. REF AMM 25-66-01SDR SCNA20220715079Girt Bar · looseDEFECT: 2L GIRT BAR DOOR BRACKET DOESNT HOLD GIRT BAR SECURELY. RESOLUTION: INSPECTED L2 DOOR GIRT BAR BRACKET. NO DEFECTS NOTED. GIRT BAR IS HELD SECURELY IN BRACKET. WORK PERFORMED IAW AMM 25-66-00SDR SCNA20221003116SUBattery Pack · inoperativeSUPPLEMENT SCNA20221003116: WORK ORDER NR-00183: FWD LH & RH EMER LIGHT BATTERY PACKS INOP. RESOLUTION: PERFORMED INSTALLATION POWER SUPPLY BATTERY PACK FWD LH AND RH ZONE IAW AMM TASK 33-51-06-960-805. OPERATYIONL TEST GOOD IAW AMM SUBTASK 33-51-06-710-004SDR SCNA20221003116Battery Pack · inoperativeDEFECT 690301: FWD LH & RH EMER LIGHT BATTERY PACKS INOP. RESOLUTION: PERFORMED INSTALLATION POWER SUPPLY BATTERY PACK FWD LH AND RH ZONE IAW AMM TASK 33-51-06-960-805. OPERATYIONL TEST GOOD IAW AMM SUBTASK 33-51-06-710-004.SDR SCNA20220634074Battery Pack · inoperativeWORK ORDER 61170: FWD LH & RH EMER LIGHT BATTERY PACKS INOP. RESOLUTION: (IN PROGRESS)SDR UIEA2022032900252Window · shortedL1 WINDOW SHORTED OUT DURING DESCENT(<P>REMOVED AND REPLACED L1 WINDOW IAW AMM 56-11-11, OPS CK GOOD.</P>)SDR SCNA20220124002Brake · damagedAT GATE, NUMBER TWO TIRE BRAKE OVERHEAT. RIGHT BRAKE 5.0 AT GATE, RAMP PERSON CAME TO FLIGHT DECK AND REPORTED SMALL FIRE AND FLAMES BUT WENT OUT QUICKLY. PERFORMED FIM 32-46 TASK 808 FOR BRAKE TEMP LIGHT. FOUND LOWER BRAKE PISTION DAMAGED. PERFORMED HEAT SDR Q2SA20210918456Switch · inoperativeDUE TO LANDING GEAR NOT RETRACTING AFTER TAKEOFF, AN ATB WAS ACCOMPLISHED INTO AUS. AIRCRAFT WAS FERRIED TO IAH FROM AUS DUE TO A/C JACKS AVAILABILITY IN IAH. MANUAL EXTENSION ACCESS DOOR SWITCH WAS REMOVED AND REPLACED IN COMPLIANCE WITH AMM 32-34-11. THE SWISDR Q2SA20210909455Transmitter · faultedWHEN COMPLETING BEFORE LANDING CHECKLIST, FLAP HANDLE SELECTED TO 30, FLAP INDICATOR NEEDLE INDICATED 8 + 10 DEGREES. ON THE GO AROUND, THE FLAP NEEDLES MATCHED AT 10 DEGREE. COMPLETED THE QRH PROCEDURE, USING ALTERNATE FLAP MASTER SWITCH AND ELECTRICALLY MOVESDR Q2SA20210808453Proximity Sensor · inoperativeAIRCRAFT GROUNDED. LE FLAP TRANSIT LIGHT CAME ON AT FLIGHT LEVEL 400. RAN QRH AND LIGHT WENT OUT. REMOVED AND REPLACED LE FLAP 1 PROXIMITY SENSOR IAW B737 AMM 27-88-11-000-802/27-88-400-802. OPS CHECK GOOD.SDR Q2SA20210804450Inlet · contaminatedON DESCENT, PASSING THROUGH 11,000 FEET, SMELLED CHLORINE. PUT ON OXYGEN MASK. INSPECTED PACKS WITH APU BLEED AND ALSO WITH BOTH ENGINES RUNNING. COULD NOT DUPLICATE CHLORINE SMELL IN THE CABIN. FURTHER INSPECTION FOUND PETROLEUM JELLY RESIDUAL UNDERNEATH PANESDR Q2SA20210712448Flap System · malfunctionedAIRCRAFT LANDED WITHOUT INCIDENT. CREW REPORTED ON APPROACH SELECTED FLAP 30 AND THEY REMAINED AT FLAP 15. CYCLED FLAP LEVER TO 15 THEN BACK TO 30, FLAPS WOULD NOT MOVE FROM FLAP 15. MAINTENANCE VISUALLY INSPECTED FLAPS AND SLATS AND CYCLED FLAPS FULL UP AND DSDR Q2SA20210418446Line · crackedAIRCRAFT GROUNDED. #2 ENGINE OIL QUANTITY INDICATION WENT TO ZERO INFLIGHT. OIL PRESSURE DROP TO RED LINE. SHUT DOWN ENGINE #2, DIVERTED TO ATL. FOUND SCAVENGE RETURN LINE CRACKED. REMOVED AND REPLACED SCAVENGE RETURN LINE PN 340-015-302-01 IAW 79-21-01. PERFOSDR Q2SA20210331445Switch · out of adjustAIRCRAFT GROUNDED. GEAR WOULD NOT RETRACT AFTER TAKE-OFF. RAN QRH, GEAR WOULD NOT RETRACT. RETURNED TO AFW. INSPECTED AND FOUND MANUAL RELEASE EXTENSION DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH AS PER AMM 32-34-00 TASK 820-802. PERFORMED OPERATIONAL AND SDR SCNA20210302012Tire · failedBLEW 2 MAIN LEFT TIRES ON LANDING TAXI OFF RUNWAY. TRANSFERRED LOG PAGE 644446 ITEM 1 TO W-O 58267. [REMOVED AND REPLACED #1 MAIN TIRE AND WHEEL ASSYS. REF. AMM 32-45-11. REMOVED AND REPLACED #2 MAIN TIRE AND WHEEL ASSY. REF AMM 32-45-11. THESE TIRES WERE CHANSDR Q2SA20210224443Wire · damagedAIRCRAFT GROUNDED. SELECTED FLAPS 1 WITH NO MOVEMENT. RAN VARIOUS FLAP QRH PROCEDURES AND EVENTUALLY ENDED WITH ALL FLAPS UP LANDING QRH PROCEDURE. NO ABNORMALLY HARD LANDING. AUTO BRAKES MAX. TROUBLESHOOT PER WDM 27-53-21. REPAIRED WIRES W1024-2008R, W1024-20SDR SCNA20210112001Controller · malfunctionedON DEPARTURE AUTOFAIL LIGHT ILLUMINATED NNC COMPLETED. IN CRUISE FLIGHT OFF SCHEDULE DESCENT LIGHT ILLUMINATED FOLLOWED BY AUTO FAIL LIGHT ILL AGAIN AND THEN PANEL WENT BLANK. INFORMED OVER ACARS LOSS OF CABIN PRESSURE, DECLARED EMERGENCY. DIVERSION TO DEN SDR SCNA20200728050Slat System · warning light#8 LED DID NOT EXTEND FULLY LE TRANSIT ILLUMINATED. PERFORMED FSEU BITE PER FIM 27-51 TASK 801. NO EXISTING FAULTS . PERFORMED FIM 27-88 TASK 804, NO FAULTS FOUND. VISUALLY INSPECTED SENSOR, OPERATED FLAPS SEVERAL TIMES. ALL OPS AND INDICATIONS NORMAL.SDR SCNA20200701047Shutoff Valve · malfunctionedPARKING BRAKE ILLUMINATED AFTER TAKE OFF. CREW DECLARED EMERGENCY AS PRECAUTION. REPLACED PARKING BRAKE SHUT OFF VALVE IAW AMM 32-44-21 INSTALLATION TEST GOOD, NO LEAKS NOTED.SDR SCNA20200612045Sensor · faultyFLAP TRAILING EDGE ASSYMETRY PRIOR TO FLAPS 1. FOUND FLAP NR 2 SKEW FAULT CODE 27-53251 PERFORMED FIM 27-59 TASK 802. REMOVED AND REPLACED NR 2 FLAP SKEW SENSOR REF AMM 27-59-01 OPS CHECK GOOD.SDR Q2SA202002065426Electronic Unit · malfunctionedAIRCRAFT GROUNDED. ON APPROACH, FLAPS EXTENDED TO 5 DEGREES BUT NOT BEYOND. ALTERNATE FLAP IS GOOD TO 15 DEGREES. CREW DECLARED EMERGENCY. REMOVED AND REPLACED FLAP SLAT ELECTRONICS UNIT IAW B737-800 AMM 27-51-01. OPS CHECK GOOD AT THIS TIME. A/C OK FOR SERVISDR Q2SA202002054425Circuit Board · failedAIRCRAFT GROUNDED. SOURCE OFF LT ON #1 GEN @ FL 380. RAN QRH - GEN WOULD NOT RESET. DIVERTED ON APU GEN ONLY. #2 GEN ON DEFFERRAL. CREW DECLARED EMERGENCY. REMOVED AND REPLACED #1 GCB (C801) PER AMM B737-800 AMM 24-21-41. OPERATIONAL CHECKS GOOD.SDR 2020F00279Sensor · failedQRF TO THE ORIGIN AIRPORT DUE TO BLEED TRIP OFF ENGINE NUMBER ONE LIGHT ILLUMINATES. QRH APPLIED BY CREW AND FAIL RECURRENT AGAIN. RETURN REQUIRED.CORRECTIVE ACTION: WAS REPLACED PRECOOLER CONTROL VALVE SENSOR IAW AMM 36-12-03/401 AND REPLACED 450 THERMOSTAT ISDR 2020F00084Bellcrank · brokenUPON LANDING LH OUTBOARD AFTER FLAP, INBOARD BELLCRANK BROKEN. CORRECTIVE ACTION: BELLCRANCK MECHANISM OUTBOARD AFT FLAP LH REMOVED AND REPLACEDSDR Q2SA20190702423Gcu · malfunctionedAIRCRAFT GROUNDED. DURING THE "BEFORE START CHECKLIST", THE APU GEN TRIPPED OFF AND A STRONG ELECTRICAL SMELL FILLED THE COCKPIT. RESET APU GCU IAW AMM 24-21-81. VERIFIED ALL SYSTEMS OP CHECK GOOD.SDR Q2SA20190518417Connector · looseAIRCRAFT GROUNDED. TRAILING EDGE FLAPS WOULD NOT EXTEND PAST 2 IN NORMAL; WOULD EXTEND TO 15 USING ALTERNATE FLAPS. C/W INSPECTION OF ALL RELATED FLAP COMPONENTS FOR DEFECTS. UPON INSPECTION, FOUND LH FLAP POSITION TRANSMITTER CONNECTOR LOOSE WITH RED BAND SHOSDR ASMF20180918007Starter · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RIGHT ENGINE START, N2 REACHED 10% OF N2 AND DECREASED TO 0%. MAINTENANCE PERSONNEL PERFORMED AN INSPECTION IAW AMM 73-21-00 DETECTING THE STARTER DAMAGED. SO THE RIGHT ENGINE STARTER WAS REPLACED IAW AMM 80-11-01, TSDR ASMF20180625003Circuit Breaker · failedCAPTAIN REPORTED THAT DURING APPROACH, FLAPS DISAGREE DISPLAYED WHEN SELECTING FLAPS 1, FLAPS STAYS IN UP POSITION, USING ALTERNATE FLAPS FOR LANDING WITH FLAPS 30. MAINTENANCE PERFORMED A BITE OF THE FSEU IAW FIM 27-51, TASK 801. FAILURE CODE 27-53280 DISPLSDR ASMF20180515012Circuit Breaker · defectiveCAPTAIN REPORTED THAT DURING APPROACH FLAPS DISAGREE WAS SHOWN WHEN SELECTING FLAPS 1, FLAPS STAYS IN UP POSITION, USING ALTERNATE FLAPS FOR LANDING WITH FLAPS 30. MAINTENANCE PERSONNEL PERFORMED BITE TO FSEU IAW FIM 27-51, TASK 801 PROCEDURE, SHOWING FAILURE SDR ASMF20180327001Sensor · failedDURING A TRANSIT CHECK, DETECTED AN LE SLAT NR 6 LIGHT TURNED ON. MAINTENANCE PERFORMED A BITE TO FSEU IAW FIM 27-51 / 801, SHOWING FAILURE CODES 27-81211, FIM 27-88 TASK 805 WAS PERFORMED, DETECTING LE SLAT NR 6 INBOARD SENSOR S1005 FAILURE; LE SLAT NR 6 ISDR ASMF201802001Connector · corrodedCAPTAIN REPORTED THAT DURING INITIAL APPROACH LE FLAP TRANSIT LIGHT WHEN LOWERING LEVER DOWN TO FLAP 1, THE INDICATION STAYED AT POSITION 1 MAKING LE FLAP TRANSIT AND SUBSEQUENTLY PROCEDURES FOR LANDING ALTERNATE FLAP PROCEDURE NO SATISFACTORY. MAINTENANCE PERSDR ASMF201801018Fuel Heater · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO A FUEL LEAK IN THE RIGHT ENGINE, AFTER ENGINE START. MAINTENANCE DETECTED THE FUEL SERVO HEATER LEAKING. THE RIGHT FUEL SERVO HEATER WAS REPLACED IAW AMM 73-11-07 AND LEFT ENGINE WAS RUN IAW MM 71-00-00, TEST 3A IDLE-POWERSDR ASMF201801014Transmitter · malfunctionedCAPTAIN REPORTED THAT DURING APPROACH, THE FLAPS, SLATS AND LEADING EDGE DID NOT EXTEND DURING NORMAL SYSTEM OPERATION, SO FLIGHT CREW ACCOMPLISHED THE QRH 9.28 PROCEDURE, BEING NECESSARY A MISSED APPROACH DUE TO VHF WITH FAILURE. MAINTENANCE PERSONNEL PERFORMSDR ASMF20170531004Pressure Switch · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGINE START, THE LEFT ENGINE FUEL FILTER BY PASS LIGHT TURNED ON. MAINTENANCE PERSONNEL REPLACED THE LEFT ENGINE DIFFERENTIAL PRESSURE SWITCH AND FUEL FILTER IAW AMM 73-34-01, TESTED CORRECT.SDR ASMF201704019Brake · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED FROM THE RIGHT MAIN LANDING GEAR. MAINTENANCE PERFORMED AN INSPECTION IAW AMM 32-11-21, LEAKAGE WAS OUT OF LIMITS. AIRCRAFT WAS SENT TO THE HANGAR, DETECTING THE MAIN LANDING GEAR BRAKE POSITION 3 WITH CORROTSDR ASMF201704008Reservoir · low quantityDURING TRANSIT CHECK, IT WAS DETECTED EVIDENCE OF HYDRAULIC LEAKAGE IN THE LEFT MAIN LANDING GEAR AND AN INDICATION IN COCKPIT OF LOW LEVEL OF HYDRAULIC IN THE RESERVOIR. THEREFORE HYDRAULIC SYSTEM WAS SERVICED IAW AMM 12-12-00. ADDITIONALLY AN EXTERNAL LEAKAGSDR ASMF201703007Fire Detector · failedAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE LEFT FIRE DETECTION SYSTEM FAULT LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED LEFT ENGINE FIRE DETECTION TEST IAW AMM 26-10-00, DETECTING LOOP B OF LEFT ENGINE WITH FAULT; SO THE CIRCUIT BREAKERS A24, A2SDR ASMF201703001Fire Detector · no testCAPTAIN REPORTED DURING A TRANSIT CHECK, THE FIRE DETECTOR OF LOOPS A & B WITH FAULT LIGHT ON LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED AN INSPECTION IAW AMM 26-11-00 CONFIRMING FAILURE. THE FIRE DETECTOR ASSY UPPER WAS REPLACED IAW AMM 26-11-01, TESTED CSDR ASMF20170301001Gland Nut · corrodedDURING TRANSIT CHECK, IT WAS DETECTED CORROSION ON THE SHOCK STRUT GLAND NUT AND CYLINDER OF THE LEFT MAIN LANDING GEAR; THEREFORE THE LEFT MAIN LANDING ASSY WAS REPLACED IAW AMM 32-11-00, ADDITIONALLY LEFT MLG TEST WAS PERFORMED IAW AMM TASK 32-32-00-710-801,SDR ASMF20170301002Warning System · activatedAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CRUISE, THE RIGHT SIDE WING BODY OVERHEATS LIGHT TURNED ON AND RIGHT PACK AIR CONDITIONED WAS DEFERRED, SHOWING BETWEEN 12 PSI AND 15 PSI. MAINTENANCE PERSONNEL PERFORMED REVISION, CONFIRMING THE FAILURE; SO THE RIGHT
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