N967AM
Service difficulty reports · 24
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N967AM' AND registry_match = 'registration' 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 = 'N967AM' AND registry_match = 'registration' 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 M17F20230808104Actuator · failed- FLAPS DRIVE - ROLL/YAW ASYMETRY - GND PROX SYS - GPWS FLAP OVRD - SPOILER- NO AUTO LAND - HYD SPOILERS SYS - ELEC SPOILERS SYSSDR 2023F00045Module · unserviceableMAINTENACE MSG OF FLIGHT CONTROL SYS (RUDDER, AILERON, ELEVATOR FLAP) AND HYD PRESSSDR 2023F00095Unknown · unknownDURING STARTING THE MESSAGE "ENG FUEL SPAR VALVEL" APPEARS, THE ENGINE STARTS NORMALSDR 2022F00220None · noneACTUADOR DE FRENOS 8 EN ESTATUS, FRM 324 143 08SDR 2022F00215None · noneACTUADOR DE FRENOS 8 EN ESTATUS FRM 324 143 08,SDR 2022FA0000060Slat · damagedDURING TRANSIT CHECK, IT WAS DETECTED THREE DENTS ON SLAT NUMBER 1 SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING 3 DENTS ON SLAT 1 WITH MULTIPLE DAMAGES ON LE FRONTAL AREA LOCALIZED BETWEEN STA 1151.75 AND STA 1160; A DENT AT STA 1152.75 WITH 1.7SDR ASMF2021120800324Skin · damagedTHREE DENTS ON SLAT NUMBER 1 SKIN. DURING TRANSIT CHECK, IT WAS DETECTED THREE DENTS ON SLAT NUMBER 1 SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING 3 DENTS ON SLAT 1 WITH MULTIPLE DAMAGES ON LE FRONTAL AREA LOCALIZED BETWEEN STA 1151.75 AND STA 1SDR ASMF202106007Depressor · damagedDURING OVERNIGHT AND APPLICATION OF TASK CARD J8778-025-02-01(13) AT MEX, IT WAS DETECTED WORN WELDMENT ASSY ON BOTH SIDES OF RIGHT DEPRESSOR PYLON ENGINE. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING WORN WELDMENT ASSY ON BOTH SIDES OF RIGHT DEPRESSOSDR ASMF202101016Acoustic Panel · dentedDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED DENT ON LEFT T/R IFS INNER WALL ACOUSTIC PANEL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT OF 1.125" DIAMETER, 0.021" DEPTH ON LEFT T/R IFS INNER WALL ACOUSTIC PANEL, AT LOWER BIFURCATIOSDR ASMF20200603020Door · nickedDURING TRANSIT CHECK, IT WAS DETECTED NICKS AT RT SIDE FWD ELECTRONICS EQUIPMENT ACCESS DOOR. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING FIVE NICKS, THREE NICKS WITH DIMENSIONS APPROXIMATELY OF 0.312" LENGTH AND 0.250" WIDE BETWEEN STA 305 & 307 AND TWSDR ASMF2019061304Fan · failedDURING TRANSIT CHECK, IT WAS DETECTED EICAS MESSAGE LIQUID COOLING 21-81013. MAINTENANCE PERSONNEL PERFORMED A REVIEW TO COOLING SYSTEM, DETECTING THE LEFT POWER ELECTRONICS COOLING (PECS) FAILED; SO THE LEFT POWER ELECTRONICS COOLING WAS REPLACED IAW AMM DMCSDR ASMF201901090006Warning Message · false activationAIRCRAFT RETURNS TO PLATFORM DUE TO SPOILER LIGHT IN EICAS AND STATUS FLAP GROUND INHIBIT MESSAGE. MAINTENANCES PERSONNEL PERFORMED REVIEW, DETECTING FAILURE CODES 27-12303 AND 27-17752; SO THE FIM DMC-B787-A-27-60-F1-DMA-421A-A PROCEDURE WAS PERFORMED, NO CONSDR ASMF2019010900003Autothrottle Sys · malfunctionedAIRCRAFT RETURNED TO PLATFORM DUE TO AUTOTHROTTLES DID NOT ENGAGE. MAINTENANCE PERSONNEL PERFORMED AUTOTHROTTLE SYSTEM OPERATIONAL TEST IAW FIM DMC-B787-A-31-90-F8-01A-421B-A PROCEDURE, SHOWING FAILURE CODES 22-20060 AND 22-20050; SO THE FIM DMC-B787-A-31-90-FSDR ASMF201809021Not Reported · malfunctionedAIRCRAFT RETURNED TO PLATFORM, DUE TO AFTER STARTS ENGINES THE FLAP/SLAT PRIMARY SYSTEM INDICATION WAS SHOWN WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED FLAP/SLAT PRIMARY SYSTEM TEST WAS IAW DMC-B787-A-27-51-00-01B-300B-A, TESTED SATISFACTORY.SDR ASMF20180902718Battery Pack · failedDURING TRANSIT CHECK, THE CENTER EMERGENCY LIGHTS ROWS 29 TO 33 TURNED OFF. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING THE BATTERY PACK FAILED; SO THE BATTERY PACK WAS REPLACED IAW AMM DMC-B787-A-33-51-07-02B-520A-A / 720A-A AND EMERGENCY LIGHT TEST WASDR ASMF20170202001Actuator · damagedCAPTAIN REPORTED THAT DURING APPROACH, THE MESSAGE IN EICAS AND STATUS SLAT DRIVE. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERFORMED THE FIM PROCEDURE IAW DMC-B787-A-27-80-F1-33A-421A-A, DETECTING GEAR ROTATORY ACTUATORS ON SLAT 11, LANYARD SKEW AND BLSDR ASMF20161216004Seal · leakingDURING OVERNIGHT CHECK AND THE EO 8772004 ISSUED TO REPLACE THE TRANSFER GEARBOX (TGB) ON BOTH ENGINES, MAINTENANCE PERSONNEL DETECTED OIL LEAK IN RIGHT TGB SLEEVE; SO THE RIGHT TGB SLEEVE SEALS WERE REPLACED IAW AMM DMC-B787-A-G72-01-00A-520A-A AND TEST 4 PARSDR ASMF20161216003Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM DUE TO AFTER START ENGINES, THE RIGHT ENGINE CONTROL LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO CMCF IAW FIM DMC-B787-A-G13-20-F1-52A-421A-A, SHOWING FAILURE CODE 73-11152 AND DURING CHANGE OF THE CONFIGURATION TYPE SDR ASMF201611002Actuator · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR. FOUND TO BE OUT OF LIMITS IAW A-A-29-11-00-00C-364-A. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL REPLACED THE RIGHT MAIN LANDING GEAR RETRACT ACSDR ASMF201610011Actuator · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYDRAULIC LEAK IN THE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR OUT OF LIMIT IAW DMC B787A-A-29-11-00-00C-364-A. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL REPLACED THE RIGHT MAIN LANDING GEAR RETRACT ACTUASDR ASMF201510012Actuator · failedDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE HORIZONTAL STABILIZER TRIM ACTUATOR. ACFT WAS SENT TO THE HANGAR. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR IAW DMC-B787-A-27-41-07-00B-520A-A, TESTED CORRECT.SDR ASMF201510007Heat Exchanger · failedDURING TRANSIT CHECK, IT WAS DETECTED A FLUID LEAK IN THE AFT GALLEY. THE AFT GALLEY WAS CLEANED. PERFORMED REVISION & CLEANING IAW AMM DMC-B7878-A-12-25-01-02A-258A-A, NO CONFIRMING FLUID LEAK. AS PRECAUTIONARY ACTION, THE AFT GALLEY WAS DEFERRED IAW MEL 2SDR ASMF201408001Ram Air Turb · deployedAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE EICAS MESSAGE RAT EXTEND & RAT UNLOCKED LIGHT TURNED ON, WITH THE LANDING GEAR LEVER IN UP POSITION. DURING MAINTENANCE REVISION, THE RAM AIR TURBINE WAS FOUND EXTENDED. ACFT WAS SENT TO THE HANGAR & THE NSDR ASMF201407002Warning System · false activationCAPTAIN REPORTED THAT DURING APPROACH, THE AHM EICAS MSG OF OVERSPEED WAS REACHED WITH MORE 15 KNOTS. PERFORMED FLAP & SLAT DOWN OVERSPEED OR ABOVE 20,000 FEET CONDITION INSPECTION IAW AMM DMC-B787-A-05-51-08-00B-280B-A, PHASE I, NO DAMAGES WERE FOUND.
Back to N967AM