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 ASMF201612014Warning Light · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO DURING BOTH ENGINES START, THE ALT MODE AND CDS FAULT LIGHTS TURNED ON AT BOTH DISPLAYS. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE FAILURE CODES 31-68081 IN THE DEU. THE BITE TO BOTH EEC WAS PERFORMED IAW FIM SDR ASMF201611018Slide · out of positionDURING TRANSIT CHECK, THE RIGHT DOOR SLIDE NUMBER 1 WAS FOUND OUT OF POSITION. MAINTENANCE PERSONNEL REMOVED AND INSTALLED THE LEFT DOOR SLIDE RAFT NUMBER 1 IAW AMM 25-66-01, TESTED CORRECT.SDR ASMF201611014Sensor · failedAIRCRAFT RETURNED TO PLATFORM DUE TO AFTER STARTING THE ENGINES, THE PSEU LIGHT ILLUMINATED. MAINTENANCE PERFORMED BITE TO PSEU IAW FIM 32-61 TASK 804 PROCEDURE, SHOWING FAILURE CODES 32-61006 AND S0074 UP TO LKD. THE MAIN LANDING GEAR UP LOCK SENSOR S0074 WASSDR ASMF201610023Sensor · failedAIRCRAFT RETURNED TO PLATFORM DUE TO AFTER START ENGINES, THE PSEU LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO PSEU IAW FIM 32-61 TASK 804 PROCEDURE, SHOWING FAILURE CODES 32-61006 AND S0074 RIGHT UP LKD; SO THE MAIN LANDING GEAR UP LOCK SENSOR S0SDR ASMF201610017Hinge Fitting · damagedCAPTAIN REPORTED THAT DURING CRUISE, A STRONG NOISE IN THE FWD ENTRY DOOR WAS LISTENED; AT THE GATE THE FLIGHT ATTENDANT DETECTED THAT THE HINGE OF THE DOOR WAS FALL DOWN. MAINTENANCE PERSONNEL PERFORMED A REVISION TO FWD ENTRY DOOR IAW SRM 52-10-00, DETECTINGSDR ASMF201610007Actuator · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING FUEL LEAK IN THE TRANSIENT BLEED VALVE DRAIN PORT. THE RIGHT ENGINE WAS MOTORING, AFTER IT WAS STARTED AND ENGINE OPERATIONAL TEST WAS PERFOSDR ASMF201610002Module · intermittentAIRCRAFT RETURNED TO PLATFORM DURING TAXING, THE RIGHT SIDE WING BODY OVERHEATS LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO WHEEL WELL FIRE, WING AND BODY OVERHEAT DETECTION CONTROL MODULE IAW FIM 26-18 TASKS 801 AND 802, SHOWING FAILURE CODE 64 “SDR ASMF201610001Engine · vibrationCAPTAIN REPORTED THAT DURING CLIMB, THE RIGHT ENGINE REACHED 4.0 UNITS OF VIBRATION AND DURING CRUISE THE VIBRATION WAS STABILIZED IN 2.9 UNITS MAINTENANCE PERSONNEL PERFORMED A RIGHT ENGINE VIBRATION, VIBRATION HIGH SYSTEM CHECK IAW FIM 71-05 TASK 808 PROCESDR ASMF2016072600017Tire · failedCAPTAIN REPORTED THAT DURING TAKEOFF AND LANDING A VIBRATION IN MAIN LANDING GEAR. MAINTENANCE PERSONNEL PERFORMED THE TIRE BURST CONDITIONAL INSPECTION, THE FLAT SPOTTED TIRES CONDITIONAL INSPECTION AND HIGH ENERGY STOP INSPECTION IAW AMM 05-51-54, AMM 05-51SDR ASMF201605013Pressure Valve · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DUCT PRESS LOW INDICATION IN THE LT ENG, SHOWING 5 PSI. PERFORMED REVISION IAW 36-11-00, DETECTING A PNEUMATIC LEAK IN THE LT ENG PRSOV, DEFERRED IAW MEL 36-5-1 CAT C. THE LT ENG PRSOV, BAR & SENSOR 390 WERE REPLACED IAW SDR ASMF201605009Drain Line · damagedDURING TRANSIT CHECK, IT WAS DETECTED A WATER SPILLAGE IN THE FWD GALLEY, E & E COMPARTMENT. ACFT WAS SENT TO THE HANGAR & PERFORMED CLEANING IAW AMM 25-71-00. GALLEY SPILLAGE CONDITIONAL INSPECTION WAS PERFORMED IAW AMM 05-51-13, DETECTING THE DRAIN WATER LSDR ASMF201605001Valve · stuckAIRCRAFT REJECTED TAKE OFF AT 40 KNOTS, DUE TO DURING TAKEOFF ROLL THE RT BLEED TRIP OFF LIGHT TURNED ON. THE FLIGHT CREW ACCOMPLISHED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE. PERFORMED REVISION DETECTING THE RT ENG HIGH STAGE VLV STUCK IN OPEN. THE HSDR ASMF201511002Pitot Tube · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE LT PITOT LIGHT TURNED ON. PERFORMED BITE TO PSEU IAW FIM 30-31-TASK 802 PROCEDURE, DETECTING THE PROBE PITOT WITH DAMAGE. THE PROBE PITOT WAS REPLACED IAW AMM 34-11-01 & LT PITOT SYS LEAK TEST WAS PERFOSDR ASMF201510016Transmitter · failedAIRCRAFT RETURNED TO PLATFORM DUE TO, AFTER START ENGINES & DURING FLAPS EXTENSION, THE LT & RT FLAP INDICATION SHOWN ASYMMETRY WITH LEVER DID NOT COMMAND. PERFORMED THE FIM 27-51 TASK 801 PROCEDURE, SHOWING FAILURE CODE 27-52260 & THE FIM 27-51 TASK 820 PROCSDR ASMF201510015Indication Sys · malfunctionedAIRCRAFT RETURNED TO PLATFORM DUE TO AFTER START ENGINES, THE LE FLAP EXTEND INDICATION WAS SHOWN WITHOUT MOVEMENT. PERFORMED THE FIM 27-51 TASK 820 PROCEDURE, NO FAILURE WAS DETECTED. AS A PRECAUTIONARY ACTION, THE FLAPS POSITION TRANSMITTER T428 WAS REPLACSDR ASMF201509011Sensor · damagedDURING TRANSIT CHECK, IT WAS DETECTED A LIGHTNING STRIKES IN THE FUSELAGE SKIN. PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, DETECTING SMALL BURNED MARKS IN THE FUSELAGE SKIN AT STATION 479, BETWEEN STRINGER 25L & 26L, STATION 494.5, & LT HORIZ STSDR ASMF201509009Line · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE MAIN BRAKE NR 1. PERFORMED REVISION IAW AMM 31-40-00, DETECTING A HYD LEAK IN QUICK CONNECTION LINE OF THE CHECK VLV OF THE MAIN BRAKE NR 1. THE QUICK CONNECTION LINE & NIPPLE WERE REPLACED IAW AMM 32-4SDR ASMF201509006Cap · looseAIRCRAFT RETURNED TO PLATFORM, DUE TO DURING TAXING, IT WAS DETECTED AN ELEC CABLE BURNED ODOR WITH EVIDENCE OF WHITE SMOKE. PERFORMED FIM 21-00 TASK 806 PROCEDURE & SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-56. BOTH AIR CONDITIONED PACKS &SDR ASMF201509005Heat Exchanger · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE EECS ALT MODE & RT WINDOW HEAT PANEL LIGHTS TURNED ON. PERFORMED BITE TO BOTH EEC IAW AMM 73-21-00, NO FAILURE DETECTED & RT WINDOW HEAT CONTROLLER WAS VERIFIED IAW AMM 30-41-11, NO FAILURE DETECTED. PESDR ASMF201509003Line · leakingDURING TRANSIT CHECK, TECHNICAL PERSONNEL DETECTED SMOKE IN THE LT MLG. PERFORMED REVISION, DETECTING HYD LEAK IN THE LINE MAIN TO BRAKE NR 1. LINE MAIN TO BRAKE NR 1 WAS TIGHTENED & CLEANED IAW AMM 32-45-00. THE MAIN WHEEL NR 1 WAS REPLACED IAW AMM 32-45-1SDR ASMF201509001Line · looseDURING TRANSIT CHECK, TECHNICAL PERSONNEL DETECTED SMOKE IN THE LT MLG. PERFORMED REVISION, DETECTING HYD LEAK IN THE LINE MAIN TO BRAKE NR 1. LINE MAIN TO BRAKE NR 1 WAS TIGHTENED & CLEANED IAW AMM 32-45-00. THE MAIN WHEEL NR 1 WAS REPLACED IAW AMM 32-45-1SDR ASMF201506008Warning System · false activationDURING TRANSIT CHECK, AFTER CLOSE THE DOORS, THE RT WING BODY OVERHEATS LIGHT TURNED ON, SO THE FLIGHT CREW ACCOMPLISHED THE QRH 2.23 PROCEDURE, NO CONFIRMING FAILURE & CONTINUING TO DESTINATION. AFTER ACFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE ANTI-SDR ASMF201503030Indication Sys · faultyAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO LOW FUEL INDICATION. DETECTED FUEL LEAKS IN BOTH ENGS WITHIN LIMITS IAW MM71-71-00. DURING OVERNIGHT CHECK, PERFORMED FUEL QTY INDICATING SYS INSPECTION IAW MM 28-41-00, ALL CORRECT.SDR ASMF201503014Shutoff Valve · failedDURING FUELING, A FUEL SPILLAGE IN THE RT TANK WAS DETECTED DUE TO THE SOV DID NOT CLOSE. THE PLATFORM WAS CLEANED BY FIREMEN & MX CLOSED THE VLV MANUALLY & THE REFUELING SOV WAS DEFERRED BY MEL 28-10-2 CAT C. THE FIM 28-21 TASK 809 PROCEDURE WAS PERFORMED CSDR ASMF201501016Processor · failedDURING FUELING, A FUEL SPILLAGE IN THE LT TANK WAS DETECTED DUE TO THE SOV FAILURE. THE PLATFORM WAS CLEANED BY FIREMEN & MX PERSONNEL. CLOSED THE VLV MANUALLY & THE REFUELING SOV WAS DEFERRED BY MEL 28-10-2 CAT C. DURING OVERNIGHT CHECK, THE PRESSURE FUELISDR ASMF201501003Tip Cap · damagedDURING TRANSIT CHECK DETECTED DAMAGE IN LE OF THE HORIZONTAL STABILIZER & RETRACTABLE LANDING LIGHT RIGHT, THE ACFT WAS SENT TO HANGAR, REPLACED THE LE OF THE HORIZONTAL STABILIZER & RIGHT RETRACTABLE LANDING LIGHT IAW AMM 27-41-21 & AMM 33-42-02 RESPECTIVELY,SDR ASMF201409001Warning System · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGS START, THE LT PACK CONTROLLER LIGHT TURNED ON. PERFORMED REVISION, DETECTING RAM AIR ACTUATOR WITH FAILURE, SO THE RAM AIR ACTUATOR WAS DEFERRED IAW MEL 21-5 CAT C. THE FIM 21-61-801 PROCEDURE WAS PERFORMED, TSDR ASMF201407006Filter · failedDURING TRANSIT CHECK, CAPTAIN REPORTED AN ABNORMAL SMOKE FROM LT WING. PERFORMED REVISION DETECTING CONTAMINATED WITH HYD LIQUID THE LT ENG AIR PURGE SYS PNEUMATIC DUCT. ACFT WAS SENT TO THE HANGAR. THE FIM 21-00 TASK 806 PROCEDURE WAS PERFORMED, THE RECIRCSDR ASMF201407005Relief Valve · leakingDURING TRANSIT CHECK, CAPTAIN REPORTED AN ABNORMAL FUME & ODOR WITH NO EVIDENCE OF SMOKE IN CABIN CREW. PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-56, DETECTING THE LT PRESS RELIEF VLV WITH HYD LEAK. THE LT PRESS RELIEF VLV WAS REPLSDR ASMF2014061706008Rivet · burnedLIGHTNING STRIKE DURING CLIMB IN THE LT SIDE FUSELAGE SKIN. PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION IAW MM 05-51-19, DETECTING SMALL BURNED MARKS & A LIGHT SCRATCH IN THE FUSELAGE SKIN AT STATIONS 195.5, 310, 330.62 & 429 BETWEEN STRINGERS 22L, 23SDR ASMF2014061706007Monitor · burnedDURING TRANSIT CHECK, BURNING ODOR WITH NO EVIDENCE OF SMOKE WAS DETECTED IN PAX CABIN. PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-56 & FIM 21-00 TASK 806 PROCEDURE, DETECTING MONITOR BURNED, SO THE ENTERTAINMENT SYS WAS DEFERRED IASDR ASMF201403009Valve · damagedAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB AT 6000 FEET, THE RT PNEUMATIC DUCT PRESS WAS PROPPED 10 PSI WITH PRESS INDICATION OF 10 PSI IN THE RT SIDE & 5 PSI IN THE LT SIDE. THE FLIGHT CREW ACCOMPLISHED THE QRH 2.1 PROCEDURE, CONFIRMING THE FAILURE. MXSDR ASMF201402004Apu · overtempDURING TRANSIT CHECK, THE APU WAS SHUT OFF AUTOMATICALLY BY OVER TEMP. MX PERSONNEL PERFORMED FIM 49-30 TASK 802 PROCEDURE, CONFIRMING THE FAILURE, SO THE REPORT WAS DEFERRED IAW MEL 49-1, CAT C. AT MEX, MX PERSONNEL PERFORMED THE FIM 49-30 TASK 803 & OPERATSDR ASMF201312008Shutoff Valve · failedAIRCRAFT REJECTED TAKE OFF AT 50 KNOTS, DUE TO DURING TAKEOFF ROLL THE LT BLEED TRIP OFF LIGHT TURNED ON, SO THE FLIGHT CREW ACCOMPLISHED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE. REPLACED THE LT ENG PRSOV IAW AMM 36-11-04, CONTINUING THE FAILURE, SO THESDR ASMF20131108004Battery Pack · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO EMERGENCY EXIT LIGHTS TURNED ON WITH SWITCH IN ARM POSITION AND CIRCUIT BREAKER A-11 TRIPPED. DURING MAINTENANCE REVISION, THE BATTERY PACK M2335 WAS DETECTED DAMAGE. BATTERY PACK WAS REPLACED IAW AMM 33-51-06, TESTED CORRSDR ASMF201310007Tire · failedDURING TRANSIT CHECK, FOUND LT NOSE WHEEL WITH A THROWN TREAD AND LOW PRESSURE. LT NOSE WHEEL REPLACED IAW AMM 32-45-00.SDR ASMF201308005Autopilot Sys · unknownDURING CRUISE, BOTH AUTOPILOTS WERE OUT OF SERVICE. AIRCRAFT RETURNED. MX PERSONNEL PERFORMED DISENGAGE BAR RESET TEST AND AUTOPILOT SYSTEM CMD A AND B CHECK IAW AMM 22-11-00, TESTED CORRECT.SDR ASMF201308002Shutoff Valve · damagedDURING CLIMB, AIRCRAFT RETURNED, THE LEFT AIR CONDITIONING PACK AND ALL TOILETS OUT OF SERVICE, FLIGHT CREW ACCOMPLISHED THE QRH 2.10 PROCEDURE. MX PERSONNEL REPLACED THE SHUTOFF VALVE AND BLEED AIR REGULATOR OF THE LEFT ENGINE PNEUMATIC SYS IAW AMM 30-11-04SDR ASMF201306009Warning Light · false activationACFT REJECTED TAKEOFF AT 40 KNOTS WITH A GROSS WEIGHT OF 67,900 KG, FORWARD ENTRY DOOR LIGHT TURNED ON. DURING MX REVISION, THE FORWARD ENTRY DOOR WAS DETECTED CLOSED AND SECURED.SDR ASMF201306007Skin · dentedDURING TRANSIT CHECK, THE RT FWD SERVICE DOOR WAS DAMAGED, PROMOTING A DENT OF 1.5" LENGTH, 0.020" DEPTH, AT BS 343.2, ON STRINGER 13R. MX PERSONNEL ISSUED THE NON ROUTINE CARD A0206436. , THE RT AFT SERVICE DOOR WAS REWORKED IAW SRM 53-00-01, PARA 4B (3), FISDR ASMF201306002Line · leakingDURING PUSH BACK, DETECTED A HYDRAULIC LEAK IN THE RT MLG LINE, THE LINE WAS TIGHTENED IAW MM 20-10-51, ALL CORRECT.SDR ASMF201303004Target · out of adjustACFT REJECTED TAKEOFF AT 90 KNOTS DUE TO THE RT ENGINE REVERSE LIGHT TURNED ON. MX PERSONNEL PERFORMED A BITE TO EAU IAW MM 78-34-00, DETECTING FAILURE IN THE STOW TARGETS S835 AND S830. STOW TARGETS S835 AND S830 WERE ADJUSTED IAW MM 78-34-02 PAGE 501, TESSDR ASMF201303001Sensor · out of limitsACFT RETURNED TO PLATFORM DUE TO FLAPS WITHOUT MOVEMENT WITH INDICATION LEVER OF 5 UNITS. MX PERSONNEL PERFORMED BITE TO FSEU IAW FIM 27-51 TASK 801 PROCEDURE, SHOWING FAILURE CODE 27-53252 AND THE SENSOR T527 OUT OF LIMITS; SO THE SENSOR T527 WAS REPLACED IASDR ASMF201301001Valve · leakingDURING TRANSIT CHECK, MX DETECTED A WATER LEAK IN THE FORWARD LAVATORY FOR RINSE VALVE. FORWARD RINSE VALVE WAS REPLACED IAW MM 38-32-01, TESTED CORRECT.SDR ASMF201212007Engine · smokeDURING ENGINE START, SMOKE WAS DETECTED FROM RT ENGINE. MX PERFORMED ENGINE LEAKING INSPECTION IAW MM 72-00-00, DETECTED OIL LEAK IN THE RT ENGINE FUEL PUMP DRAIN. RT ENGINE WAS RUN IAW MM 71-71-00, TESTS NR 3A/3B AND MM 79-00-00, NO LEAKS WERE DETECTED. ASSDR ASMF201212005Slat System · failedACFT RETURNED TO PLATFORM, AFTER ENGINES START, THE FLAP L/E TRANSIT LIGHT TURNED ON. MX PERSONNEL PERFORMED A BITE ON FSEU IAW MM 27-11-00, DETECTING THE SLAT 7 WITH FAILURE, FIM 27-88 TASK 803 PROCEDURE WAS PERFORMED, CONFIRMING THE FAILURE. DURING MX REVISDR ASMF201211008Seal · leakingDURING TRANSIT CHECK, TECH PERSONNEL DETECTED A NLG SHOCK STRUT HYD LEAK; SEALS REPLACED IAW MM 32-21-11, TESTED CORRECT.SDR ASMF201211002Engine · vibrationCAPTAIN REPORTED THAT DURING ENGINES START, LT ENGINE VIBRATION REACHED 5.01. MX PERSONNEL PERFORMED BITE TO AIRBORNE VIBRATION MONITORING SYSTEM; THE LT ENGINE WAS INSPECTED IAW MM 71-00-00; THE FIM 71-05 TASK 808 PROCEDURE WAS PERFORMED; THE N1 CONNECTOR DSDR ASMF201208007Restrictor Valve · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYDRAULIC SPILLAGE IN THE RT PIT. DETECTED A LEAK IN THE PRESSURIZATION MODULE RESTRICTOR VALVE; SO IT WAS REPLACED IAW MM 29-11-02, TESTED CORRECT.SDR ASMF201205006Skin · burnedCAPTAIN REPORTED A POSSIBLE LIGHTNING STRIKE DURING DESCENT IN LT WINGLET T/E. MX PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19. DETECTED BURN WITH EXPOSED FIBERS OF 2" DIAMETER OUT OF LIMITS IN LT WINGLET T/E; SO IT WAS REPAIRED IAW SRM
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