N342AM, cancelled Jul 18, 2023

Service difficulty reports · 32

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 = 'N342AM' AND deregistration_id = 'N342AM-2023-07-18'
  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.

SDR ASMF2021120700315Transmitter · failedAILERONS FLIGHT CONTROL TEST WITH RIGHT MOVEMENT SLOWER. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING AILERONS FLIGHT CONTROL TEST WITH RIGHT MOVEMENT SLOWER. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING BITE TO PSEU IAW FIM 27-11 TASK 8081 PROCEDURE, NOOct 13, 2021 · N342AM · Boeing 7378Z9 · Aileron Control SystemSDR ASMF20211026025Transmitter · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING AILERONS FLIGHT CONTROL TEST WITH RIGHT MOVEMENT SLOWER. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING BITE TO PSEU IAW FIM 27-11 TASK 8081 PROCEDURE, NO CONFIRMING FAILURE; AS A PRECAUTIONARY ACTION; THE FLAPSOct 13, 2021 · N342AM · Boeing 7378Z9 · Aileron Control SystemSDR ASMF202106015Control Cable · out of adjustDURING TRANSIT CHECK, IT WAS DETECTED THE FLIGHT CONTROL TEST WITH SLOW RESPONSE OF AILERON MOVING RIGHT TO NEUTRAL. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING SLOW AILERON RESPONSE; SO THE SLOW AILERON RESPONSE TO CONTROL WHEEL INPUT WITH HYDRAULIC PMay 25, 2021 · N342AM · Boeing 7378Z9 · Aileron Control SystemSDR 2021F00162Aileron Sys · lack of lube26.05.2021 18:43 DURING TRANSIT CHECK THE FLIGHT CONTROL TEST SLOW DURING TRANSIT CHECK, IT WAS DETECTED THE FLIGHT CONTROL TEST WITH SLOW RESPONSE OF AILERON MOVING RIGHT TO NEUTRAL. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING SLOW AILERON RESPONSE; SMay 25, 2021 · N342AM · Boeing 7378Z9 · Aileron Control SystemSDR ASMF202101021Structure · crackedDURING 8A-P CHECK IN TASK CARD J3770-818-02-01 (21) AT MEX STATION, IT WAS DETECTED SEVERAL CRACKS AT RIGHT ENGINE INNER THRUST REVERSER. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A CRACK ON UPPER FIREWALL STA 247.40 AND WL 100; A CRACK ON UPPER FJan 16, 2021 · N342AM · Boeing 7378Z9 · Engine Thrust ReverserSDR ASMF202011013Acoustic Panel · dentedDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED A SEVERAL DENTS AND A NICK ON LEFT ENGINE INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A SEVERAL DENTS WITH 2.875" AND 1.500"OF SEPARATION; A DENT OF 0.500Sep 30, 2020 · N342AM · Boeing 7378Z9 · Nacelle/Pylon, Main FrameSDR ASMF202011007Switch · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXIING, WHEN PRESS TOGA FOR TAKEOFF SOUNDS THE ALARM OF TAKEOFF CONFIGURE WITH FLAPS 1 AND STAB TRIM 6.1. MAINTENANCE PERSONNEL PERFORMED BITE TO PSEU, IAW FIM 32-09 TASK 801 PROCEDURE AND FIM 27-62 TASK 808 PROCEDSep 23, 2020 · N342AM · Boeing 7378Z9 · Drag Control SystemSDR ASMF202011005Packing · damagedDURING TRANSIT CHECK, A HYDRAULIC LEAKAGE WAS DETECTED ON FLAP CONTROL VALVE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING PACKING´S OF HYDRAULIC LINES OF FLAP CONTROL VALVE WITH LEAKAGE. SO THE PACKING´S OF HYDRAULIC LINES P/N NAS1612-8A, MANUFACTURESep 21, 2020 · N342AM · Boeing 7378Z9 · Hydraulic System, MainSDR ASMF20200603022Skin · damagedDURING TRANSIT CHECK, IT WAS DETECTED A DISBONDED AND ERODED OF LT OUTBOARD AFTER FLAP. MAINTENANCE PERSONNEL PERFORMED REVISION TO DISBONDED AND ERODED 2 AT UPPER AND LOWER SKIN ON TRAILING EDGE INBOARD CORNER OF LT OUTBOARD AFTER FLAP, FROM OTEF STA 88.2 TOMar 23, 2020 · N342AM · Boeing 7378Z9 · Trailing Edge FlapsSDR ASMF20190712004Window · crackedAIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF THE RT WINDOW NR 2 WAS CRACKED FRM 56102042; SO MAINTENANCE PERSONNEL REPLACED THE RT WINDOW P/N: 141A4810-39, S/N: 01269H9011 NR 2 IAW AMM56-12-11-400-801; IT WAS PERFORMED CABIN PRESSURE LEAK TEST IAW AMM 05-51Jul 3, 2019 · N342AM · Boeing 7378Z9 · Flight Compartment WindowsSDR 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 PROTECTIVMar 16, 2019 · N342AM · Boeing 737800* · AC Generator-AlternatorSDR 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 PMar 8, 2019 · N342AM · Boeing 737800* · Hydraulic System, MainSDR 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-0Nov 20, 2018 · N342AM · Boeing 737800* · Weather Radar SystemSDR 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 TAKEOFOct 29, 2018 · N342AM · Boeing 737800* · Central WarningSDR 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 SESep 7, 2018 · N342AM · Boeing 737800* · Turbine Engine Oil SystemSDR 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 REGMar 8, 2018 · N342AM · Boeing 737800* · Pneumatic Distribution SystemSDR ASMF201704010Connector · looseDURING TRANSIT CHECK, IT WAS DETECTED THE STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING THE CONNECTOR D381 LOOSE, THEREFORE THE CONNECTOR WAS TIGHTENED IAW AMM 27-41-00,TESTED CORRECT. AS A PRECAUTIONARY ACTION, THE STAB Apr 12, 2017 · N342AM · Boeing 737800* · Flight Control System WiringSDR ASMF201700301003Slide · out of limitsDURING THE TRANSIT CHECK, THE ESCAPE SLIDE PACK FROM FWD ENTRY DOOR WAS FOUND OUT OF RANGE OF PRESSURE. MAINTENANCE PERSONNEL REPLACED THE ESCAPE SLIDE PACK IAW AMM 25-65-01, TESTED CORRECT.Feb 4, 2017 · N342AM · Boeing 737800* · Escape SlideSDR ASMF201612015B-Nut · looseDURING TRANSIT CHECK, DETECTED A HYDRAULIC LEAK IN THE RIGHT MAIN LANDING GEAR WW. MAINTENANCE PERFORMED FOUND THE HYDRAULIC LEAK IN THE HYDRAULIC SYSTEM B OF THE ENGINE DRIVEN PUMP HYDRAULIC PRESSURE LINE NUT. THE HYDRAULIC PRESSURE LINE WAS TIGHTENED IAW ADec 4, 2016 · N342AM · Boeing 737800* · Hydraulic System, MainSDR ASMF201612011Shutoff Valve · malfunctionedDURING FUELING, A FUEL SPILLAGE IN THE LEFT TANK WAS DETECTED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. THE PLATFORM WAS CLEANED BY FIREMEN AND MAINTENANCE PERSONNEL CLOSED THE VALVE MANUALLY AND THE REFUELING SHUTOFF VALVE WAS DEFERRED BY MEL 28-10-2 CAT C. AT Nov 16, 2016 · N342AM · Boeing 737800* · Fuel StorageSDR ASMF201611005Pump · failedAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB AT FL 170´, THE LEFT ENGINE EXPERIENCED THRUST DETERIORATION AT A SHOW RATE, THE LEFT ENGINE THRUST LEVER WAS ADVANCED TO THE FULL THRUST POSITION WITHIN INDICATION OF THRUST INCREASING AT ALL PARAMETERS. AIRCRAFAug 27, 2016 · N342AM · Boeing 737800* · Engine Fuel PumpSDR ASMF201610014Pump · failedAIRCRAFT RETURNED DURING CLIMB AT FL 170´, THE LEFT ENGINE EXPERIENCED THRUST DETERIORATION AT A SHOW RATE, THE LEFT ENGINE THRUST LEVER WAS ADVANCED TO THE FULL THRUST POSITION WITHIN INDICATION OF THRUST INCREASING AT ALL PARAMETERS. AIRCRAFT WAS SENT TO THAug 27, 2016 · N342AM · Boeing 737800* · Engine Fuel PumpSDR ASMF2016072600014Actuator · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGINES START, THE LEFT ENGINE CONTROL LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO LEFT EEC IAW FIM 73-10 TASK 801 PROCEDURE, SHOWING THE MESSAGES L REVERSER SLEEVE POSITION SIGNAL OUT OF RANGE; SO THE LJun 5, 2016 · N342AM · Boeing 737800* · Engine Fuel DistributionSDR ASMF2015030400001Relay · failedAIRCRAFT REJECTED TAKE OFF AT 80 KNOTS DUE TO MASTER CAUTION & RT AFT OVERWING DOOR LIGHTS TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 1.8 PROCEDURE, CONFIRMING THE FAILURE. PERFORMED REMOVAL & INSTALLATION OF THE RT EMER EXIT DOOR IAW AMM 52-22-00 & IT PERFeb 1, 2015 · N342AM · Boeing 737800* · Emergency ExitsSDR ASMF201503008Warning System · false activationAIRCRAFT REJECTED TAKE OFF AT 60 KNOTS DUE TO MASTER CAUTION & RT AFT OVERWING DOOR LIGHTS TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 1.8 PROCEDURE, CONFIRMING THE FAILURE. PERFORMED BITE TO PSEU & THE CB`S WERE RESEATED IAW FIM 32-09 TASK 801 PROCEDURE, NJan 30, 2015 · N342AM · Boeing 737800* · Central ComputersSDR ASMF201501028Battery Pack · damagedAIRCRAFT RETURNED FROM FLIGHT DUE TO DURING CLIMB, ALL EMER LIGHTS TURNED ON & BURNED ODOR WITH NO EVIDENCE OF SMOKE WAS DETECTED. PERFORMED REVISION DETECTING IN THE M1671 BATTERY PACK THE CB P18-3 B-10 POPPED. O THE BATTERY PACK NR M1671 WAS DEFERRED IAW MJan 5, 2015 · N342AM · Boeing 737800* · Emergency LightingSDR ASMF201501022Solenoid · malfunctionedAIRCRAFT REJECTED TAKE OFF AT 60 KNOTS, DUE TO RT AFT OVERWING LIGHT TURNED ON. PERFORMED A REVISION AT THE AFT OVERWING DOOR IAW AMM 52-20-00 & BITE TO PSEU IAW FIM 52-20 TASK 801 PROCEDURE, SHOWING FAILURE MSG. R FL SW FAULT, & DETECTING FAILURE OF FLIGHT LDec 28, 2014 · N342AM · Boeing 737800* · Emergency ExitsSDR ASMF201501012Wire Harness · damagedCAPTAIN REPORTED THAT DURING CRUISE, THE BLEED TRIP OFF LIGHT TURNED ON. ACCOMPLISHED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE & CONTINUING TO DESTINATION. PERFORMED THE FIM 36-10 TASK 801 DETECTING WIRING HARNESS DAMAGE. MW0311 LT ENG WIRING HARNESS WNov 10, 2014 · N342AM · Boeing 737890 · Pneumatic System WiringSDR ASMF2015010500002Brake Assy · damagedAIRCRAFT REJECTED TAKEOFF AT 120 KNOTS, DUE TO AN ABNORMAL VIBRATION IN THE LT MLG. PERFORMED HIGH ENERGY STOP INSPECTION & AIRFRAME VIBRATION CONDITION INSPECTION IAW AMM 05-51-07 & AMM 05-51-67, DETECTED LT MLG BRAKES & WHEELS NRS 1 & 2 DAMAGED, LT MLG AXLEOct 4, 2014 · N342AM · Boeing 737800* · Landing Gear Brake SystemSDR ASMF201310002Oven · contaminatedACFT RETURNED TO PLATFORM, F/A REPORTED THAT A WIRE BURNED ODOR AFTER AFT GALLEY OVENS TURNED ON. MAINTENANCE PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-56, DETECTING PAPER BURNED PROPERTY OF CATERING; THE PAPER WAS REMOVED AND AFTSep 15, 2013 · N342AM · Boeing 737832 · Buffet/GalleysSDR ASMF201309009Unknown · unknownCAPTAIN REPORTED THAT DURING DESCENT, A STRONG NOISE IN COCKPIT FWD COMPARTMENT WAS HEARD. MX PERFORMED A PRESSURIZATION VALVE AND OUTFLOW VALVE EXTERIOR VISUAL INSPECTION AND BITE TO CONTROLLER NR 2 IAW AMM 21-31-00, ALL CORRECT.Sep 4, 2013 · N342AM · Boeing 737832 · Standard Practices/StructuresSDR ASMF20130531013Skin · damagedCAPTAIN REPORTED A LIGHTNING STRIKE DURING APPROACH IN THE FUSELAGE SKIN. MX PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19 DETECTING A PERFORATION OUT OF LIMITS OF .1250" DIAMETER AT BS 480. FUSELAGE SKIN AT BS 480 WAS REPAIRED IAW SRM 53May 19, 2013 · N342AM · Boeing 737800* · Fuselage Main, Plate/Skin
Back to N342AM, cancelled Jul 18, 2023