N745AM, cancelled Apr 6, 2018

Service difficulty reports · 20

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 = 'N745AM' AND deregistration_id = 'N745AM-2018-04-06'
  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 ASMF20170531005Monitor · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAKE OFF, CONFIGURATION STABILIZER ALARM WAS ACTIVED. MAINTENANCE PERSONNEL PERFORMED INSPECTION IAW FIM 31-43 TASK 867, CONFIRMING FAILURE IN IOM 003 RH OF INVALID DATA, THEREFORE THE IOM M003 RIGHT WAS REPLACED IAWMay 27, 2017 · N745AM · Boeing 7772Q8 · Flight Control SystemSDR ASMF201705002Pump · failedCAPTAIN REPORTED THAT DURING CRUISE, THE FUEL QUANTITY INDICATION WAS WRONG, FUEL QUANTITY WAS VERIFIED USING FUEL DIPSTICK. OPS TESTED FOR THE SYSTEM FUEL QUANTITY INDICATOR PERFORMED IAW AMM 28-24-00, FUEL TRANSFER WHEN NOT COMMANDED WAS PERFORMED IAW FIM 2May 16, 2017 · N745AM · Boeing 7772Q8 · Aircraft Fuel Distribution SystemSDR ASMF201602007Hydraulic Line · leakingCAPTAIN REPORTED THAT DURING APPROACH, THE HYD CENTRAL SYS QTY DECREASED TO 0.14 GAL & THE MSG IN EICAS & STATUS OF AUTO BRAKE SOL VLV WAS SHOWN. PERFORMED ACFT TURN AROUND, DETECTING HYD LEAK IN LT MLG HOSE. THE HOSE WAS REPLACED IAW AMM 20-10-14 & AMM 32-3Jan 24, 2016 · N745AM · Boeing 7772Q8 · Hydraulic System, MainSDR ASMF201503012Valve · looseDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE WHEEL NR 4. DURING MX REVISION, THE WHEEL NR 4 WAS DETECTED LEAKING WITHIN LIMITS. THE BRAKES BLEED PORT OF THE WHEEL NR 4 WAS TIGHTENED & CLEANED IAW AMM 32-45-00, TESTED CORRECT.Feb 6, 2015 · N745AM · Boeing 7772Q8 · Landing Gear Brake SystemSDR ASMF201407008Bracket · brokenAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO URGENT ATTENTION OF A SICK PAX. PERFORMED AN OVERWEIGHT LANDING INSPECTION IAW MM 05-51-35 PHASE 1, DETECTING A RT MLG HYD TRUCK BRACKET BROKEN. EVALUATED THE DAMAGE & FOUND IT WITHIN LIMITS IAW AMM 32-10-01. Jul 1, 2014 · N745AM · Boeing 7772Q8 · Main Landing Gear Strut/Axle/TruckSDR ASMF2014061706010Slide Raft · out of positionDURING TRANSIT CHECK, THE LT DOOR SLIDE RAFT NR 2 WAS FOUND OUT OF POSITION ON THE ACFT FLOOR & WITH METAL SEAMS LOOSEN. ACFT WAS SENT TO THE HANGAR & SENT THE LT DOOR SLIDE RAFT TO SURVIVAL SHOP FOR ASSEMBLY CORRECTLY IAW CMM 25-61-52. INSTALLED THE RT DOORApr 27, 2014 · N745AM · Boeing 7772Q8 · Escape SlideSDR ASMF201308008Fairing · damagedDURING TRANSIT CHECK, A BIRD STRIKE WAS DETECTED IN RT ENGINE. BIRD STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-18, DETECTING 6 FAIRING DAMAGES AND 2 PANELS WITH 4 IMPACT, BEING WITHIN LIMITS OF OPERATION IAW AMM 71-00-00. PANELS WERE REPAIRED IJul 12, 2013 · N745AM · Boeing 7772Q8 · Wing StructureSDR ASMF201211007Probe · malfunctionedACFT RETURNED TO PLATFORM DUE TO AFTER RT ENGINE START, IT WAS HAD OSCILLATIONS BETWEEN 540 AND 580 CELSIUS DEGREES OF EGT. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED THE LOWER AND UPPER EGT PROBES AND HARNESS T-49 IAW MM 77-21-01 AND 77-21-05, TESNov 18, 2012 · N745AM · Boeing 7772Q8 · Engine EGT/TIT Indicating SystemSDR ASMF201106001Sensor · damagedAIRCRAFT RETURNED DURING CLIMB, THE EICAS MESSAGE LT PACK WAS SHOWN AND IT WAS NOT AIR ON LT DUCT. DURING MX REVISION, THE MESSAGES 21-23041 WAS SHOWN, THE FIM 21-51 TASK 803 PROCEDURE WAS PERFORMED; SO THE LT PACK SENSOR WAS REPLACED IAW MM 21-51-03, TESTED CJun 1, 2011 · N745AM · Boeing 7772Q8 · Cabin Cooling SystemSDR ASMF201010007Sensor · damagedACFT PERFORMED AN UNSCHEDULED LANDING, DUE TO DURING CLIMB THE ENG OIL FILTER SENSOR AND ENG OIL FILTER LIGHTS TURNED ON AND DURING CRUISE THE EICAS MESSAGE ENG OIL FILTER WAS SHOWN. THE FLIGHT CREW PERFORMED THE QRH 7.20 PROCEDURE, CONFIRMING THE FAILURE. DUROct 20, 2010 · N745AM · Boeing 777222 · Turbine Engine Oil SystemSDR ASMF201008001Tire · detachedDURING TAKEOFF RUN; A STRONG NOISE WAS HEARD, IECAS MESSAGE OF TIRE PRESS WAS SHOWN AND TIRE PRESS LIGHT TURNED ON, THE TIRE NR 1 WAS DEFLATED AND THE FLIGHT CONTINUED TO MAD IAW FCT 777 (TM) 8.18 (32-40-72-00 PROCEDURE). MX DETECTED MAIN TIRE NR 1 FLOOR DETAAug 19, 2010 · N745AM · Boeing 7772Q8 · TireSDR ASMF201004002Blades · damagedDURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENGINE WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES IN THE 1ST, 2ND, 3RD AND 4TH STAGES IAW AMM 72-00-00, PARAGRAPH 5H. THE FINAL REPAIR DETAILS OR ENGIMar 21, 2010 · N745AM · Boeing 7772Q8 · Turbine Engine Compressor SectionSDR ASMF20100321001Blade · damagedDURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENG WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES IN THE 1ST, 2ND, 3RD AND 4TH STAGES IAW AMM 72-00-00, PARAGRAPH 5H. THE FINAL REPAIR DETAILS OR ENGINE Mar 21, 2010 · N745AM · Boeing 7772Q8 · Turbine Engine Compressor SectionSDR ASMF200911001Brake Assy · leakingDURING TRANSIT CHECK, A HYD LEAK WAS DETECTED ON THE RT MLG BRAKE NR 8. MX REPLACED THE BRAKE ASSY NR 8 IAW MM 32-45-07, TESTED CORRECT.Nov 11, 2009 · N745AM · Boeing 7772Q8 · Landing Gear Brake SystemSDR MAS2008F00062Thrust Reverser · damagedDURING TRANSIT CHECK WAS DETECTED THE OUTBOARD REVERSER OF THE RT ENGINE WITH EXTENDED DAMAGE ON FAN DUCT INNER WALL WITH MATERIAL MISSING OF 70 X 60 INCH BY IMPACT OF THE BOROSCOPE L PLUG, THE ACFT WAS SENT TO HANGAR FOR REVERSER REPLACEMENT WHICH WILL BE SENAug 21, 2008 · N745AM · Boeing 7772Q8 · Engine Thrust ReverserSDR 2008FA0000472Engine · failedDURING TRANSIT CHECK, THE RT ENGINE WAS DETECTED WITH DAMAGES. MAINT PERFORMED BOROSCOPIC INSPECTION, DETECTING DAMAGES OUT OF LIMITS, SO RT ENGINE WAS REPLACED AND TESTED IAW MM 71-00-02 AND 71-00-00, ALL CORRECT. (K)Jun 6, 2008 · N745AM · Boeing 7772Q8 · Engine (Turbine/Turboprop)SDR 2008FA0000471Sensor · failedAC RETURNED TO DEPARTURE DUT TO RT ENGINE STALLED. MAINT PERFORMED FIM 75-21 TASK 822 AND STALL INSPECTION IN 1ST, 5TH AND 9TH HPC STAGES. NO DAMAGES WERE DETECTED IAW MM 71-00-00. RT PT25 SENSOR WAS REPLACED IAW MM 73-21-63, TESTED CORRECT. THE OVERWEIGHTJun 1, 2008 · N745AM · Boeing 7772Q8 · Engine Indicating SystemSDR ASMF200806001Sensor · failedAIRCRAFT RETURNED OF FLIGHT DUE TO RIGHT ENGINE STALLED. MAINTENANCE PERSONNEL PERFORMED FIM 75-21 TASK 822 AND STALL INSPECTION IN 1ST, 5TH AND 9TH HPC STAGES, NO DAMAGES WERE DETECTED IAW MM 71-00-00. RIGHT PT25 SENSOR WAS REPLACED IAW MM 73-21-63, TESTED Jun 1, 2008 · N745AM · Boeing 7772Q8 · Fuel Controlling SystemSDR ASMF200710004Engine · overtempAIRCRAFT REJECTED TAKEOFF AT 101 KNOTS DUE TO HIGH TEMPERATURE INDICATION ON THE LT ENGINE, REACHING 1035 CELSIUS DEGREES MOMENTARY AND 1015 DURING 11 SECONDS. MAINTENANCE PERSONNEL PERFORMED FIM PROCEDURE 73-22 TASK 819 FOUND ALL CORRECT, ADDITIONALLY HIGH ENOct 18, 2007 · N745AM · Boeing 777* · Engine (Turbine/Turboprop)SDR ASMF200607003Scuff Plate · ground damageDURING TRANSIT CHECK, AIRCRAFT WAS HIT BY A BAGGAGE CONVEYOR PROMOTING A DENT OF 3 INCHES LONG, 1 INCH WIDE AND .2500 INCH DEPTH IN THE SCUFF PLATE OF THE ACCESS BULK CARGO, SO IT WAS REPAIRED IAW SRM 51-10-01. DURING OVERNIGHT CHECK SCUFF PLATE WAS REMOVED TOJul 2, 2006 · N745AM · Boeing 777* · Standard Practices/Structures
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