N861AM
Service difficulty reports not matched to an aircraft · 40
They name N861AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.
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 n_number = 'N861AM' AND registry_match IS NULL 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 n_number = 'N861AM' AND registry_match IS NULL 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 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 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 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 SDR ASMF201611008Hinge 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 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 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 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 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 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 ASMF201506011Warning System · false activationAIRCRAFT REJECTED TAKEOFF AT 30 KNOTS, DUE TO PSEU LIGHT TURNED ON. ACCOMPLISHED THE QRH 15.4 PROCEDURE & RETURNED TO PLATFORM. PERFORMED RESEAT PSEU TEST IAW AMM 32-06-10, NO CONFIRMING FAILURE & PSEU LIGHT TURNED OFF, TESTED CORRECT.SDR 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 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 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 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 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 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 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 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 ASMF201203001Switch · out of adjustACFT RETURNED TO DEPARTURE, DURING CLIMB, THE MLG DID NOT RETRACT; SO FLIGHT CREW ACCOMPLISHED THE QRH 14.16 PROCEDURE, CONFIRMING THE FAILURE. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED A REVISION DETECTING THE MANUAL EXTENSION ACCESS DOOR SWITCHSDR ASMF201202005Bellcrank · brokenCAPTAIN REPORTED THAT DURING TAKEOFF, THE ACFT REQUIRED 3 UNITS TO THE LEFT OF RUDDER TRIM. DURING MX REVIEW, THE RT OTBD FLAP, INBD BELLCRANK WAS FOUND BROKEN. THE RT OTBD FLAP, INBD BELLCRANK WAS REPLACED IAW MM 27-51-24, TESTED CORRECT.SDR ASMF201202004Fseu · damagedCAPTAIN REPORTED THAT DURING APPROACH, FLAPS DID NOT EXTEND, FLIGHT CREW ACCOMPLISHED QRH 9.4 PROCEDURE, CONFIRMING THE FAILURE. MX REPLACED THE FLAP SLAT ELECTRONIC UNIT IAW MM 27-51-01, TESTED CORRECT.SDR ASMF201109006Pump · damagedCAPTAIN REPORTED THAT DURING APPROACH LANDING GEAR HANDLE HAD NOT MOVED EVEN THROUGH LOCK OVERRIDE HANDLE WAS MOVED; FLIGHT CREW ACCOMPLISHED THE QRH 14.10 PROCEDURE AND MANUAL GEAR EXTENSION WAS PERFORMED. MX REPLACED THE EMDP SYS A IAW M 29-11-21 AND EXTENSSDR ASMF201109003Actuator · leakingDURING OVERNIGHT CHECK, A HYD LEAK WAS DETECTED IN THE LT ELEVATOR TAB LOCK ACTUATOR. THE LT ELEVATOR TAB LOCK ACTUATOR WAS REPLACED IAW MM 27-31-34 AND OPS TEST WAS PERFORMED IAW MM 27-31-00-700-815, ALL CORRECT.SDR ASMF201107011Structure · damagedDURING TRANSIT CHECK, THE LT AFT CABIN DOOR WAS DAMAGED. MX PERFORMED VISUAL INSPECTION TO LT AFT ENTRY STRUCTURE DOOR IAW MM 52-13-00 DETECTING DAMAGES OUT OF LIMIT IN THE DOOR COVER AND THE LATERAL STRIPS OF THE COVER DOOR WERE BENT. TECH REPAIRED THE DOORSDR ASMF201107009Pump · damagedACFT REJECTED TAKEOFF AT LESS THAN 70 KNOTS WITH GROSS WEIGHT OF 58764 KG DUE TO LEFT ENGINE NOT REACHING THRUST, 101PERCENT REQUIRED, ONLY IT REACHED 90 PERCENT THRUST WITH ATS SET AND OFF. MX PERFORMED BITE IN EEC IAW MM 73-21-00 AND BITE TO THE ATS WAS PERFSDR ASMF201107008Engine · malfunctionedACFT REJECTED TAKEOFF AT 80 KNOTS AND GROSS WEIGHT OF 67 870 KG DUE TO THRUST ASYMMETRY OF 97 PERCENT N2 ON LT ENGINE AND 103 PERCENT N2 ON RT ENGINE AND LT THRUST LEVEL CUT BACK AUTOMATICALLY AFTER TRYING TO EQUAL POWER. MX PERFORMED BITE IN EEC IAW MM 73-21
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