N851AM, cancelled Sep 21, 2018

Service difficulty reports · 41

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 = 'N851AM' AND deregistration_id = 'N851AM-2018-09-21'
  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 ASMF20180821002Computer · failedDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE HYDRAULIC SYSTEM B ON THE FEEL ELEVATOR COMPUTER. MAINTENANCE PERFORMED A REVISION, DETECTING A HYDRAULIC LEAK AT HYDRAULIC SYSTEM B FEEL ELEVATOR COMPUTER REDUCER. THE FEEL ELEVATOR COMPUTER WAS REPJun 3, 2018 · N851AM · Boeing 737752 · Elevator Control SystemSDR ASMF201706003Tire · puncturedAIRCRAFT RETURNED TO PLATFORM DURING PUSH BACK, THE NLG WHEEL NUMBER 2 WAS PUNCTURED. MAINTENANCE PERFORMED REVISION IAW AMM 32-45-00, DETECTING NLG WHEEL NUMBER 1 PUNCTURED BY FOD. THEREFORE RIGHT NLG WHEELS ASSY WAS REPLACED IAW AMM 32-45-21, TESTED CORRECTJun 11, 2017 · N851AM · Boeing 737752 · TireSDR ASMF201611013Fuel Heater · leakingAIRCRAFT RETURNED TO PLATFORM DURING TAXING, A FUEL LEAK WAS DETECTED IN THE LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE FUEL SERVO HEATER DAMAGED; SO THE LEFT FUEL SERVO HEATER WAS REPLACED IAW AMM 73-11-07 AND LEFT ENGINE WAS RUN IAWSep 18, 2016 · N851AM · Boeing 737752 · Fuel HeaterSDR ASMF201610022Fuel Heater · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, A FUEL LEAK WAS DETECTED IN THE LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE FUEL SERVO HEATER DAMAGED; SO THE LEFT FUEL SERVO HEATER WAS REPLACED IAW AMM 73-11-07 AND LEFT ENGINE WAS Sep 18, 2016 · N851AM · Boeing 737752 · Engine Fuel DistributionSDR ASMF2016072600001Actuator · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYDRAULIC LEAK IN THE SPOILER ACTUATOR NUMBER 12. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT SPOILER ACTUATOR RESTRICTOR PACKING NUMBER 12; SO THE SPOILER ACTUATOR RESTRICTOR PACKING CONNECTOR NMay 8, 2016 · N851AM · Boeing 737752 · Hydraulic System, MainSDR ASMF201602002Warning System · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO AFTER START ENGS, THE ELEC LIGHT TURNED ON. PERFORMED ELEC SYS AUTO TEST IAW FIM 34-31 TASK 801, CONFIRMING THE FAILURE, SO THE RESET TO RUPTURES & BITE TO SPCU MODULE WERE PERFORMED IAW FIM 24-34 TASK 802, NO FAILURES WERDec 23, 2015 · N851AM · Boeing 737752 · DC Indicating SystemSDR ASMF201510025Warning System · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE ELEC LIGHT TURNED ON. PERFORMED RESEAT TO STANDBY POWER IAW AMM 24-21-00, NO CONFIRMING FAILURE, TESTED CORRECT.Sep 30, 2015 · N851AM · Boeing 737752 · AC Indicating SystemSDR ASMF201510003Warning System · false activationDURING APPROACH WITH FLAPS & LANDING GEARS UP, THE RED LIGHT OF NLG TURNED ON BRIEFLY & ALARM WAS ACTIVE RETURNED TO NORMAL CONDITION AFTER THE EVENTS. PERFORMED THE FIM 32-30 TASK 811 PROCEDURE, NO CONFIRMING FAILURE, TESTED CORRECT.Aug 5, 2015 · N851AM · Boeing 737752 · Landing Gear Position and WarningSDR ASMF201509008Windshield · crackedDURING TRANSIT CHECK, IT WAS DETECTED THE RT WINDSHIELD NR 1 CRACKED. PERFORMED REVISION, DETECTING CRACKS OUT OF LIMITS IAW AMM 56-11-00-210-007. THE RT WINDSHIELD NR 1 WAS REPLACED IAW AMM 56-11-11-000 400-801 & WINDOW HEAT CONTROL MODULE WAS REPLACED AMM Jul 29, 2015 · N851AM · Boeing 737752 · Flight Compartment WindowsSDR ASMF201507013Hydraulic Line · leakingDURING TRANSIT CHECK, A HYD LEAK WAS DETECTED IN THE HYD SYS B OF THE ENG DRIVEN PUMP. PERFORMED REVISION DETECTING HYD LEAK AT HYD SYS B OF THE ENG DRIVEN PUMP HYD PRESS LINE. THE HYD PRESS LINE WAS CLEANED & TIGHTENED IAW AMM 29-11-11. AS PRECAUTIONARY ACJun 21, 2015 · N851AM · Boeing 737752 · Hydraulic System, MainSDR ASMF201503004Heat Exchanger · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START, AN OIL LEAK WAS DETECTED. PERFORMED REVISION, DETECTING OIL LEAK IN THE OIL & FUEL HEAT EXCHANGER DRAIN. THE RT HEAT EXCHANGER WAS REPLACED IAW AMM 79-21-02, TESTED CORRECT.Jan 18, 2015 · N851AM · Boeing 737752 · Engine Oil CoolerSDR ASMF2014061706014Pump · leakingDURING OVERNIGHT CHECK, A FUEL LEAK WAS DETECTED IN RT ENG FUEL PUMP OF 40 DROPS PER MINUTE. THE FUEL PUMP WAS REPLACED IAW AMM 73-11-01, TESTED CORRECT.May 10, 2014 · N851AM · Boeing 737752 · Engine Fuel PumpSDR ASMF201308017Warning Light · false activationACFT RETURNED DUE TO DURING CLIMB THE "EQUIP" LIGHT TURNED ON CROSSING OF 12,000 FT TO 13,000 FT. MX PERSONNEL PERFORMED REVISION TO ELECTRONIC EQUIPMENT ACCESS DOOR IAW AMM 52-48-41; BITE WAS PERFORMED TO BOTH CABIN PRESSURE CONTROLLERS IAW MM 21-32-00, THE Jul 27, 2013 · N851AM · Boeing 737752 · Air Distribution SystemSDR ASMF201306005Apu · damagedDURING TRANSIT CHECK, DETECTED SMOKE AND STRONG NOISE WAS HEARD IN THE APU. MX PERSONNEL PERFORMED REVISION DETECTING INTERNAL DAMAGES IN THE APU; SO THE REPORT WAS DEFERRED IAW MEL 49-1 CAT C. MX PERSONNEL REPLACED THE APU IAW AMM 49-11-00, TESTED CORRECT.Jun 12, 2013 · N851AM · Boeing 737752 · APU Core EngineSDR ASMF201210001Actuator · damagedCAPTAIN REPORTED THAT DURING APPROACH, THE AILERONS CONTROL FELT HARD. MX PERSONNEL PERFORMED FLIGHT CONTROL TEST, DETECTING THAT THE AILERONS CONTROL DID NOT RETURN TO NEUTRAL POSITION IAW MM 27-11-00. THE LT WING FLIGHT SPOILER ACTUATOR NR 4 WAS REPLACED ISep 11, 2012 · N851AM · Boeing 737752 · Drag Control ActuatorSDR ASMF201207008Engine · making metalCAPTAIN REPORTED THAT DURING DESCENT, THE RT ENGINE OIL FILTER BYPASS LIGHT TURNED ON. MX PERSONNEL REMOVED THE FILTER ASSY AND CHIP DETECTOR ABG/TGB, DETECTED METAL PARTICLES. RT ENGINE NR 2 WAS REPLACED AND TESTED IAW AMM 71-00-02 AND IAW AMM 71-00-00, ALLJul 26, 2012 · N851AM · Boeing 737752 · Engine (Turbine/Turboprop)SDR ASMF201111010Slide · unwanted deployDURING TRANSIT CHECK, A F/A ACTIVATED THE RT DOOR SLIDE. MX REPLACED THE RT DOOR SLIDE IAW MM 25-66-01, ALL CORRECT.Nov 14, 2011 · N851AM · Boeing 737752 · Escape SlideSDR ASMF201111001Carbon Seal · leakingDURING TRANSIT CHECK,DETECTED AN OIL LEAK IN THE RT ENGINE HYD PUMP SEAL WITH 118 DROPS PER MINUTE. ACFT WAS SENT TO THE HANGAR AND THE RT ENGINE HYD PUMP CARBON SEAL WAS REPLACED IAW MM 72-60-00, TESTED CORRECT.Oct 23, 2011 · N851AM · Boeing 737752 · Turbine Engine Oil SystemSDR ASMF201107004Skin · dentedDURING TRANSIT CHECK, MX DETECTED ONE DENT IN THE RT HORIZ STABILIZER L/E AT STATION 233.30 OF 5.50 X 2.00 INCHES WITH 0.208 INCH DEPTH. INSPECTION PERSONNEL CONFIRMED THAT THE DENT WAS WITHIN LIMITS IAW SRM 55-10-01 ALLOWABLE DAMAGE 1 PAGE 106, SO IT WAS TEMJun 27, 2011 · N851AM · Boeing 737705 · Horizontal Stabilizer, Plate/SkinSDR ASMF201012007Brake · damagedDURING TRANSIT CHECK, TECH DETECTED THE MLG BRAKE NR 2 WITH THE INNER BEARING SEPARATED OF THEIR RETAINING RING AND HUBCAP; ALSO, MLG BRAKE BUSHING DID OUT OF POSITION, SO TECH REPLACED THE MLG BRAKE NR 2 IAW MM 32-45-11, ALL CORRECT.Dec 6, 2010 · N851AM · Boeing 737752 · Landing Gear Brake SystemSDR ASMF201012002Shutoff Valve · leakingDURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN RT FUELING SHUTOFF VALVE; SO MX CLOSED THE VALVE. MX REPLACED THE RT FUELING SHUTOFF VALVE IAW MM 28-21-51-000-801 AND 28-21-00-700-801, TESTED CORRECT.Nov 28, 2010 · N851AM · Boeing 737705 · Aircraft Fuel Distribution SystemSDR ASMF201010006Actuator · leakingCAPTAIN REPORTED THAT DURING CRUISE AND DESCENT, THE CONTROL COLUMN WITH AFT AND FWD MOVEMENT ABOUT 2 INCHES. ACFT WAS SENT TO THE HANGAR AND MX PERFORMED A CONTROL COLUMN POWER FORCE TEST AND ELEVATOR MECHANISM CONDITION INSP IAW 27-31-00; ELEVATOR PITOT SYS Oct 19, 2010 · N851AM · Boeing 737705 · Elevator Control SystemSDR ASMF 20081101Windshield · crackedAIRCRAFT RETURNED DUE TO THE LT WINDOW NR 1 CRACKED. MAINT REPLACED THE LT WINDSHIELD ASSY NR 1 AND WINDOW HEAT CONTROL UNIT IAW AMM 56-11-11 AND AMM 30-41-11, TESTED CORRECT. THE OVERWEIGHT INSPECTION WAS NOT NECESSARY DUE TO THE ACFT LANDED WITH 52,961 KG ANNov 17, 2008 · N851AM · Boeing 737* · Flight Compartment WindowsSDR ASMF200804004Control Module · failedCAPTAIN REPORTED THAT LANDING GEAR LEVER DID NOT MOVE UP AFTER TAKE OFF, SO HE PERFORMED ABNORMAL PROCEDURE QRH PAGE 14.4. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER MODULE IAW MM 32-31-11, TESTED CORRECT IAW 32-3Apr 22, 2008 · N851AM · Boeing 737* · Landing Gear Door Retract SectionSDR ASMF200804002Module · failedDURING TAKEOFF, THE (3) LIGHTS OF LANDING GEAR TURNED ON; CAPTAIN PERFORMED AN ADDITIONAL LANDING GEAR CYCLE AND LIGHTS TURNED OFF. MAINT PERFORMED FIM 32-61 TASK 809, FOUNDING INTERMITTENT FAILURE OF THE LANDING GEAR MODULE, SO IT WAS REPLACED AND TESTED IAW Apr 17, 2008 · N851AM · Boeing 737 · Landing Gear Retraction/Extension SystemSDR ASMF200803002Windshield · scratchedCAPTAIN REPORTED SEVERAL SCRATCHES ON RT WINDSHIELD NR 1. RT WINDSHIELD NR 1 WAS REPLACED IAW MM 56-11-11, TESTED CORRECT.Mar 14, 2008 · N851AM · Boeing 737* · Flight Compartment WindowsSDR ASMF200712003Skin · damagedDURING TRANSIT CHECK THE AIRCRAFT WAS HIT BY A BAGGAGE CONVEYOR IN THE LOWER FUSELAGE SKIN AT STATION 807 BETWEEN STRINGER 26R AND 27R; CAUSING A DAMAGE OUT OF LIMITS OF 1INCH DIAMETER AND 0.066 INCH DEPTH IAW SRM 53-00-01. MAINTENANCE PERSONNEL REPAIRED THE Dec 18, 2007 · N851AM · Boeing 737* · Fuselage Main, Plate/SkinSDR ASMF200712001Window · crackedCAPTAIN REPORTED THAT LT WINDOW NR 4, CRACKED DURING DESCENT. MAINTENANCE PERSONNEL REPLACED THE WINDOW IAW MM 56-11-31, TESTED CORRECT.Dec 9, 2007 · N851AM · Boeing 737* · Flight Compartment WindowsSDR ASMF200609001Control Box · failedAIRCRAFT RETURNED TO PLATFORM DURING TAXING ANTISKID INOP LIGHTS TURNED ON. ANTISKID CONTROL BOX DELETED PROCEDURE WAS PERFORMED BUT FAIL CONTINUED AND VALVES CONNECTORS WERE CHECKED, BEING CORRECT. ANTISKID CONTROL BOX WAS REPLACED IAW MM 32-42-21, TESTED CORSep 1, 2006 · N851AM · Boeing 737724 · Brake Anti-Skid SectionSDR ASMF200608010Radome · damagedDURING FINAL APPROACH, A HAIL STORM WAS REPORTED BY CAPTAIN AND A MISSED APPROACH WAS PERFORMED. DURING MAINTENANCE REVIEW, THE RADOME WAS DETECTED DAMAGED AND OUT OF LIMITS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK DENTS WERE DETECTED IN HAug 13, 2006 · N851AM · Boeing 737* · Aerodynamic FairingsSDR ASMF200607013Structure · ground damageDURING OVERNIGHT CHECK, AIRCRAFT WAS HIT BY A CARGO CONTAINER, BETWEEN LT LONGERONS 25 AND 26 PRODUCING A DENT OF 5 INCHES OF DIAMETER AND CRACK IN THE CENTER OF 2 INCHES BETWEEN STATIONS 303 AND 312. PENDING FINAL WORKS.Jul 18, 2006 · N851AM · Boeing 737 · Aircraft StructuresSDR ASMF20060508Sensor · faultyAIRCRAFT RETURNED TO PLATFORM, APU WITH LOW PRESSURE. ENGINES WERE STARTED WITH GROUND EQUIPMENT. DURING OVERNIGHT SERVICE, SENSORS P2, PT AND DP WERE REPLACED IAW MM 49-52-31, 49-52-32 AND 49-52-33, RESPECTIVELY, TESTED CORRECT.May 17, 2006 · N851AM · Boeing 737* · APU Engine Fuel and ControlSDR ASMF200604018Blades · brokenCAPTAIN REPORTED THAT DURING FINAL APPROACH AT VSA IT WAS A BIRD STRIKE ON THE RIGHT SIDE OF THE AIRCRAFT. THE RT ENGINE WAS INSPECTED, CLEANED AND OPERATIONAL TESTED IAW FIM 71-05 TASK 801, ALL CORRECT. AT ARRIVING TO MEX THE RT ENGINE WAS INSPECTED BY BIRDApr 27, 2006 · N851AM · Boeing 737* · Engine (Turbine/Turboprop)SDR ASMF200603004Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXI, PSEU LIGHT TURNED ON. BREAKERS P6-3, D1 AND D2 WERE RESEATED AND LIGHT TURNED OFF. DURING RIGHT ENGINE START, PSEU LIGHT TURNED ON AGAIN, THEREFORE, ENGINES WERE SHUTDOWN AND FIM 32-09 PROCEDURE Mar 9, 2006 · N851AM · Boeing 737* · Landing Gear SystemSDR ASMF200601013Bleed Air Sys · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING PUSH BACK, THE BLEED APU WITH 12 PSI INDICATION. THE ENGINES WERE STARTED WITH EXTERNAL PNEUMATIC PLANT IAW MM 49-50-00 AND THE APU REPORT WAS DEFERRED IAW MEL 49-7. AT MEX, THE CDU TEST WAS PERFORMED. Jan 19, 2006 · N851AM · Boeing 737724 · APU Bleed Air SystemSDR ASMF200601005Apu · failedAIRCRAFT RETURNED TO PLATFORM DURING ENGINES STARTING, LOW PNEUMATIC INDICATION PRESSURE IN THE APU. THE ENGINES WERE STARTED WITH EXTERNAL PNEUMATIC PLANT IAW MM 49-50-00 AND THE FAULT CODE 495 031 00 WAS SHOWN. AT MEX, THE FIM PROCEDURE WAS PERFORMED IAW FJan 12, 2006 · N851AM · Boeing 737724 · APU Bleed Air SystemSDR ASMF200601002Hydraulic System · leakingCAPTAIN REPORTED THAT DURING TAKE OFF WHEN THE LANDING GEARS WAS RETRACTED, THE LT HYDRAULIC QUANTITY INDICATION FELT FROM 105 PERCENT TO 74 PERCENT; REDUCING DURING FLIGHT TO 67 AND REESTABLISHED IN GROUND TO 89 PERCENT; ADDITIONALLY, THE RF LIGHT TURNED ON AJan 4, 2006 · N851AM · Boeing 737* · Hydraulic System, MainSDR ASMF200511004Apu · failedDURING ENGINES STARTING, THE PNEUMATIC AUXILIARY POWER UNIT FAILED. THE ENGINES WERE STARTED WITH EXTERNAL PNEUMATIC PLANT IAW MM 49-11-00, TESTED CORRECT. THE FIM PROCEDURE WAS PERFORMED IAW FIM 49-55 TASK 804, ALL CORRECT.Nov 5, 2005 · N851AM · Boeing 737* · APU Core EngineSDR ASMF200510014Pump · failedCAPTAIN REPORTED LOSS OF HYDRAULIC FLUID IN LT SIDE. DURING REVISION DETECTED A LEAK IN LT MAIN PUMP, SO IT WAS REPLACED IAW MM 29-11-11 AC WAS DISPATCHED. AC RETURNED TO PLATFORM, DURING TAXING PSEU AND LT HYDRAULIC SYS LIGHTS TURNED ON. BREAKERS D1 AND D2 WEOct 29, 2005 · N851AM · Boeing 737* · Hydraulic Pump (Electric/Engine), MainSDR ASMF200506018Eec · failedACFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RT ENGINE STARTING, ENGINE SHUT OFF BY ITSELF AT 20 PERCENT, STAR VALVE INDICATION FLASHING AND LOW OIL PRESS INDICATED ON 7 PSI (RED ZONE). EEC TEST PERFORMED AND 72-30102 INTERNAL EEC FAULT MESSAGE SHOWN IJun 17, 2005 · N851AM · Boeing 737* · Fuel Controlling SystemSDR ASMF200506008Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM, RT ENGINE LOW OIL PRESSURE INDICATION DURING TAXING. RAN ENG CONNECTOR AND SWAP / CHANGE TRANSMITTER CHANNEL WERE CLEANED IAW MM 72-00-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE NON ROUTINE CARD A0077753 WAS ISSUED FOR PERJun 5, 2005 · N851AM · Boeing 737* · Engine Oil Indicating System
Back to N851AM, cancelled Sep 21, 2018