N1409A
Service difficulty reports · 458
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 = 'N1409A' 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 = 'N1409A' 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 UIEA2021060701284Circuit Card · faultedL ENG ANALOG N2 STATUS MESSAGE 2+10 IN FLIGHT(<P>PERFORMED FIM 73-21 FT901 RESISTANCE CHECK GOOD B/W PINS 3&4 ON N2 SPEED SENSOR.PERFORMED ENG RUN IAW AMM 71-00-00 MSG REMAINED.REMOVED AND REPLACED L ENG N2 SPEED CARD IAW WDM 77-12-12.AFTER MULTIPLE ENG RUNS SSDR UIEA2021060701283Circuit Card · faultedR ENG ANALOG N2 STATUS MESSAGE 0+30 IN FLIGHT(<P>PREFORMED FIM 73-21 FT 901 RESISTANCE BETWEEN PIN 3 AND 4 ON N2 SPEED SENSOR RESISTANCE CHECK GOOD, PERFORMED ENGINE RUN IAW AMM 71-00-00 STATUS MESSAGE REMAINED. REMOVED AD REPLACED RIGHT ENGINE N2 ENGINE SPEEDSDR UIEA2021050101049Filter · not reportedPER MDDR 145973 REPLACE APU FUEL FILTER.(<P>REMOVED AND REPLACED APU FUEL FILTER ELEMENT IAW AMM 49-31-04, PENDING LEAK CHECK. </P><P>PERFORMED APU OPS. CHECK IAW AMM 49-11-00. NO LEAKS FOUND.</P>)SDR UIEA2021050101048Indicator · leaking#1 PYLON DIFFERENTIAL PRESSURE INDICATOR LEAKING(<P>REMOVED AND REPLACED #1 PYLON DIFF PRESS IND PER AMM -29-11-17. NO LEAKS NOTED.</P>)SDR UIEA2021050101047Seal · damagedCOCKPIT ELT AUTO RELEASE SEAL DAMAGE. PIN 1151324-1 S/N 1151324-07195(<DIV>REMOVED AND REPLACED COCKPIT ELT AS REQUIRED PER AMM 25-64-00 CK'D OK HEX CODE ADCC4060EC00161.</DIV>)SDR UIEA2021050101046Wire · chafedENG 1 LOWER FIRE LOOP ELECTRICAL WIRE WITH CHAFFING LOCATED AT 6 O'CLOCK POSITION .(<P>REPAIRED ENG #1 FIRE LOOP WIRING INSULATION PER SWPM 20-10-13: ENG 1 FIRE DETECTION SYS TEST OK IAW AMM 26-11-00 REV132<BR /></P>)SDR UIEA2021050101045Unknown · leaking#2 ENG THRUST REV OPEN/CLOSE ACTUATOR HAS EVIDENCE OF HYD LEAK(<P>CLEANED #2 ENG T/R ACTUATOR ON BOTH SIDES PENDING OPS CHECK. PERFORMED OPS CHECK PER AMM 78-31-00, NO LEAKS NOTED. <BR /></P>)SDR UIEA2021050101043Safety Wire · missing#1 ENG (ECU) MOUNT BOLTS ARE NOT SAFETIED.(<P>VERIFIED #1 ENGINE ECU BOLTS TO FAN CASE TORQUE CHECK IAW AMM 73-21-15 AND SAFETIED BOLTS WITH LOCKWIRE IAW AMM 20-10-23.<BR /></P>)SDR UIEA2021050101042Fastener · worn#1 ENG INLET CASE O/B ANTI - ICE PANELS HAS (2 EA) HOLES THAT FASTENERS HAS WORN THRU. REQUIRES DIMPLE WASHER ON FASTENERS.(<P>REMOVED AND REPLACED WORN FASTENERS AT #1 ENG BY INLET CASE O/B ANTI-ICE ACCESS PANEL PER B767-300 AMM 20-11-00-910-802.<BR /></P>)SDR UIEA2021050101041Fastener · worn#1 ENG PYLON HAS HYD RESERVOIR ACCESS PANELS WITH SMOKING RIVETS AT CLOSING LATCH POSITIONS ON I/B AND O/B SIDES (SAIL BOATS)(<DIV>REPLACED LOSSE FASTENERS AT #1 ENG PYLON BY ACCESS PANELS I/B AND O/B SIDE OF SAILBOATS PER B767-300 SRM 51-40-02-06-0.</DIV>)SDR UIEA2021050101040Fastener · worn#2 ENG I/B NACELLE STRUT ACCESS PANELS FOR HYD RESERVOIR (SAILBOATS) HAVE SMOKING RIVETS AT LATCH POSITIONS ON I/B SIDE.(<DIV>REMOVED AND REPLACED LOOSE FASTENERS AT #2 ENG I/B NACELLE STRUT ACCESS PANEL PER B767-300 SRM 51-40-02-06-0.</DIV>)SDR UIEA2021050101039Depressor · damagedMAIN CARGO DOOR AFT SEAL DEPRESSOR DAMAGED.(<P>REMOVED DAMAGED SEAL DEPRESSOR. LOCATED, DRILLED, DEBURRED, INSTALLED AND PAINTED NEW SEAL DEPRESSOR AT MAIN DECK CARGO DOOR CUT OUT AFT SIDE PER B767-300 AMM 20-11-0-910-802.<BR /></P>)SDR UIEA2021050101038Window · looseCOCKPIT LIFE RAFT COMPARTMENT VIEWING WINDOW LOOSE(<P>CLEANED AND RE-GLUE LOOSE WINDOW VIEWING AT COCKPIT LIFE RAFT COMPT PER B767-300 AMM 20-30-01-992-001.SDR UIEA2021050101037Battery · not reportedCOCKPIT FLASHLIGHT BATTERIES NEED TO BE REPLACED 2 EACH P/N P4-01-0021(<P>REMOVED AND REPLACED COCKPIT FLASHLIGHT BATTERIES 2 EA AS REQUIRED PER AMM 25-64-00. CK'D OK.<BR /></P>)SDR UIEA2021050101036Sensor · no testFUEL QUANTITY INDICATING SYSTEM "DRY CAPACITANCE TEST FOR THE RIGHT SURGE TANK FUEL LEVEL SENSOR FAIL TEST AT 4.8 PICOFARADS". NOTE: SENSOR TS196(<P>T/S F/M 28-21-F/T806; REMOVED & REPLACED TS196 RH SURGE TANK FUEL LEVEL SENSOR PER AMM 28-21-03. REV 132.SDR UIEA2021050101035Sensor · no testFUEL TANK OPENING REQUIRED DUE TO THE RIGHT SURGE TANK FUEL LEVEL SENSOR FAIL TEST. NOTE: PANEL TO BE OPEN 642AB(<P>R/H SURGE TANK PLATE 642AB REMOVED FOR TANK ACCESS. REF M/M 28-11-03-004-001. APU BATTERY AND MAIN BATTERIES DISCONNECTED. OK TO REINSTALL R/H SSDR UIEA2021050101034Solenoid · damaged#1 ENG HYD PUMP DEPRESSURIZATION SOLENOID IS DAMAGED(<P>REMOVED AND REPLACED #1 ENGINE HYD. PUMP DEPRESSURIZATION VALVE IAW AMM 29-11-05, PENDING LEAK AND OPS CHECK. </P><P>PERFORMED OPS CHECK AND LEAK CHECK PER AMM 71-00-00 AND AMM 29-11-05. OPS CHECK GOOD ANSDR UIEA2021050101033Seal · brokenCOCKPIT AVSAX CONTAINMENT BAG VACUUM SEAL IS BROKEN P/N AS-002-1(<P>REMOVED AND REPLACED COCKPIT AVSAX REF EO 6725A212<BR /></P>)SDR UIEA2021050101032Depressor · dentedDENT FOUND ON FWD M/C DOOR DEPRESSOR SEAL AT STA 492 BTW S4L AND S13L DENT FOUND TO BE WITHIN LIMITS PER REF SRM 53-00-15-1A DETAIL 12(<P>REMOVED DAMAGED SEAL DEPRESSOR, LOCATED DRILLED AND INSTALLED NEW SEAL DEPRESSOR AT MAIN CARGO DOOR CUT OUT FWD SIDE PER BSDR UIEA2021042701007Filter · failed"L ENG FUEL FILTER" EICAS MESSAGE, QRH COMPLETE, ENGINE INDICATIONS NORMAL(<P>PERF FUEL FILTER ELEMENT INSPECTION, FOUND PARTICULATE < 0.25MM IN SIZE BOTH L AND R FUEL FILTERS. REPLACED BOTH FUEL FILTERS AMM TASK 73-11-02-216-001-H00. LEAK CHECKS GOOD. TRANSFESDR UIEA2021042100950Oxygen Mask · inoperative#1 SUPERNUMERARY OXY MASK INOP ( SUPERNUMERARY SEAT / (ALL CARGO CONFIG) )(<P>ITEM TRANSFERED TO MDDR# 145648 PER MEL 25-25-03, CAT D, DUE DATE 19-AUG-21. SP@0116Z.</P><P>21APR21 - LP1188600 - M4 -ONT - PERFORMED OPS CHECK OF # 1 SUPERNUMERARY O2 MASK IAW AMM SDR UIEA2021021700332Pressure Switch · faultedRIGHT ENG PRV STATUS MSG.(T/S IAW FIM 36-10 FAULT TREE 847. SUSPECT PRESSURE SWITCH TO BE AT FAULT. REMOVED AND REPLACED PRV PRESSURE SWITCH IAW AMM 36-21-03. REF LOG PAGE 1253834 ITEM NR 8 FOR OPS CK 14FEB21 LOG PG 1253834 ITM 8 CVG: PERFORMED LEAK CHECK OSDR UIEA2021021200287Valve · malfunctionedAPU WILL NOT DELIVER PNEUMATIC AIR VALVE APU VALVE CYCLED TWICE.(<P>PERFORMED OPS TEST OF PNEUMATIC SYSTEM, NO DEFECTS NOTED IAW AMM 36-00-00. SYSTEM OPS CHECK NORMAL.</P>)SDR UIEA2021020900259Indicator · false indicationNO MANIFOLD DUCT PRESSURE WITH APU OPERATING & APU BLEED VALVE INDICATING.(<P>CYCLED BLEED SWITCH PER AMM 36-11-00. OPS CHK GOOD.<BR /></P>)SDR UIEA2021020700238Radar · malfunctionedNO CONVECTIVE ACTIVITY AT FL320, GROUND RETURNS ON RADAR APPEAR WITH TILT SELECTED AT 0 DEGREES AND RANGE SELECTED TO 160 MILES, GAIN SELECTED TO AUTO AND WX OR WX/TURB SELECTED.(<P>PERFORMED SYSTEM TEST OF WXR IAW AMM 34-43-00-715-026. OPS CHECK GOD. NO FAULSDR UIEA2021012100096Isolator · wornLEFT AFT APU VIBRATION ISOLATOR WORN TO LIMITS. REMOVED AND REPLACED LEFT AFT VIBRATION ISOLATOR, IAW AMM 49-13-01. OPERATIONS CHECK GOOD AT THIS TIME.SDR UIEA2021011300042Warning Message · false activationCABIN ALT AUTO 2 STATUS MESSAGE ILLUMINATED. PERFORMED BITE TEST ON NR 2 CABIN PRESSURE CONTROLLER. NO DEFECTS OR FAULTS NOTED. MESSAGE CLEARED, IAW AMM 21-31-00.SDR UIEA2021011100034Fitting · leakingAPU INOP(<P>FOUND BROKEN THREADED FITTING TO APU BEARING. OIL LEAKING. TRANSFERRED TO MDDR # 140687 IAW MEL 49-11-01A, CAT C, DUE 19 JAN 21. PLACARDS INSTALLED.</P><P>19JAN, CVG, LP 1239488, ITEM M5: REMOVED AND REPLACED APU IAW AMM 49-11-01. OPS CHECK OF APUSDR UIEA2021010700018Radar · malfunctionedLEFT WXR SYSTEM, WXR FAIL. PERFORMED GROUND TEST OF BOTH WEATHER RADAR SYSTEMS, REF AMM 34-43-00-715-001-001. BOTH OPERATIONS CHECK NORMAL.SDR UIEA2020122202610Unknown · unknownNUMBER 1 ENGINE START VALVE LIGHT FAILED TO ILLUMINATE, ENGINE START VALVE LIGHTS, -200/-300. TRANSFERRED TO MDDR 139877, IAW MEL 80-00-01-01, CAT C. PERFORMED ENGINE START 2X, START VALVE LIGHT ILLUMINATES & EXTINGUISHES AT START AND AT 50% N2 EACH ATTEMPT.SDR UIEA2020122002596Warning Light · false activationITEM 3-APU FAULT ON LANDING/TAXI IN. RE-START OK. PERFORMED BITE CHECK OF THE APU ECU, IAW 49-61-05, NO FAULTS FOUND. OK FOR SERVICE.SDR UIEA2020122102604Panel · openON POST FLIGHT INSPECTION, PANEL WAS FOUND OPEN. PERFORMED PNEUMATIC LEAK TEST, IAW BOEING 767 AMM 71-00-00. NO LEAK DETECTED. CLOSED PANEL, IAW BOEING 767 AMM 78-31-14.SDR UIEA2020113002475Fault Message · false activationAPU FAULT AFTER LANDING. REPEAT WRITE UP. PERFORMED BITE TEST OF APU ECU 49-11 FT 987, NO FAULTS NOTED. APU START TEST 49-11-00-201 NORMAL AT THIS TIME.SDR UIEA2020112002430Indication Sys · failedITEM 1-FUEL CONFIG EICAS. TOTALIZER VS. CALCULATED=3.1 THOUSAND POUNDS. TOTALIZER 3.1 THOUSAND LESS THAN CALCULATED INDICATION=SUSPECTED FUEL LEAK. PERFORMED BITE TEST ON FQIS, FOUND LM DENS CONTAM OR RESISTOR G AND LM COMPENSATOR CONTAMINATED G. STUCK LMSDR UIEA2020111902425Fire Detector · malfunctionedITEM 02-RT ENGINE FIRE LP 2 STATUS MESSAGE. R & R UPPER AFT ENGINE FIREWALL DETECTOR LOOP 2, IAW AMM 26-11-02. FAULT NO LONGER IN VIEW. PERFORMED ENGINE RUN RIGHT ENGINE, IAW AMM 72-00-00, NO DEFECTS NOTED.SDR UIEA2020111602401O-Ring · leakingDUE TO SUSPECTED FUEL LEAK PERFORMED GVI OF WINGS AND LT & RT ENGINE. FOUND LEAK ON RT ENGINE FUEL FILTER DP SWITCH. REMOVED AND REPLACED FUEL FILTER DP SWITCH O-RING, IAW 73-34-01. PERFORMED DRY MOTOR, IAW AMM 71-00-00, NO LEAKS NOTED. OPERATIONS CHECK NOSDR UIEA2020110902367None · noneINFO ONLY: RT ENGINE NO START FIRST ATTEMPT ON SINGLE IGNITOR. START OK ON BOTH. PERFORMED RT ENGINE IGNITION SYSTEM AUDIBLE TEST, IAW AMM 74-00-00. OPERATIONS CHECK GOOD, IGNITORS OPERATE NORMAL.SDR UIEA2020110602359Warning Message · false activation"APU FAULT" EICAS UPON ATTEMPTING APU START ON GROUND. PERFORMED ECU BITE, IAW B767 FIM 49-11 FT 987. NO FAULTS THEN PERFORMED APU START, IAW B767 AMM 49-11-00, NO FAULTS. APU OPERATIONS NORMAL, APU STARTED FIRST ATTEMPT.SDR UIEA2020110402345Apu · sparksDURING GROUND OPERATIONS MAINTENANCE WITNESSED SPARKS COMING OUT OF APU TAIL PIPE. MAINTENANCE SHUT DOWN APU AND PLACED ON DEFERRAL 49-11-01, MDDR 137202, CAT C. RAN APU IAW BITE TEST, PER FIM 49-11 FT 987, NO FAULTS NOTED. RAN BOTH PACKS, PER AMM 21-00-00.SDR UIEA2020102402293Ecu · malfunctionedRT ENGINE CONTROL EICAS MESSAGE AFTER ENGINE START. REMOVED AND REPLACED ECU. OPERATIONS CHECKS NORMAL, IAW AMM 73-21-15. PERFORMED ENGINE RUN-UP, OPERATIONS CHECKS NORMAL. NO FAULTS NOTED, IAW AMM 71-00-00.SDR UIEA2020101302235Bleed Valve · unknownDUCT PRESSURE 2500 PSI WITH APU ON AND APU BLEED VALVE OPEN. PERFORMED OPERATIONS CHECK OF PNEUMATIC SYSTEM, IAW AMM 36-00-00. OPERATIONS CHECKS GOOD, SYSTEM IS OK.SDR UIEA2020101002208Gasket · leakingNR 2 ENGINE SHOWS SIGN OF OIL LEAK. REMOVED AND REPLACED FUEL TO/OIL HEAT EXCHANGE TUBE GASKET, IAW B767 AMM 79-21-01.SDR UIEA2020100392133Transformer · shortedREPEAT WRITE-UP: DESCENDING THROUGH FL 180 AFTER TURNING WING AND LOGO LIGHTS ON, "RT AC BUS OFF" EICAS MESSAGE. RAN QRH, RT AC BUS RESTORED. ON FINAL APPROACH TURNED WING AND LOGO LIGHTS ON AGAIN ANOTHER RT AC BUS FAILURE. FOUND NUMEROUS WIRES CHAFED AT RTSDR UIEA2020100132138Buss · malfunctionedPASSING 18,000 AND AFTER SELECTING LANDING LIGHTS RECEIVED "RT AC BUS "OFF" EICAS. AFTER QRH, WE COULD NOT RESTORE RT AC BUS AND ACCEPTED LANDING CLEARANCE DUE TO LAND AT NEAREST SUITABLE AIRCRAFT CONFIGURED WITHOUT PROBLEM AND LANDING ROLLOUT AND TAXI UNEVENSDR UIEA2020092982121Apu · malfunctionedDURING TAXI-IN APU FAULT EICAS MESSAGE DURING APU START, SECOND START ATTEMPT WAS NORMAL START. OPERATIONS TESTED APU, REF 49-11-00, NO FAULTS NOTED AT THIS TIME. OK FOR CONTINUED SERVICE.SDR UIEA2020092802119Buss · failedRIGHT BUS FAILED, RESET VIA QRH, FAILED A SECOND TIME. PER CREW WHILE DESCENDING FROM 180 WHEN TURNING ON THE LANDING LIGHTS THE RT BUS FAILED. WHEN MX WENT TO DEBREIF THE CREW FOUND BOTH LT & RT BUSES OFF AND AC WAS ON STANDBY POWER, PER FIM 24-41 FT 805. SDR UIEA2020092952068Fault Message · malfunctionedAPU FAULT MSG. TRANSFERED TO MDDR 134960, CAT C, DUE 05AUG20 PER MEL 49-11-01A. RAN APU, PER AMM 49-00-00, NO FAULTS NOTED. BITE THE APU, PER FIM 49-11, NO FAULTS NOTED. RAN BOTH PACKS, PER AMM 21-00-00, NO FAULTS NOTED. RAN BOTH ENGINES, PER AMM 71-00-00SDR UIEA2020092532059Gcu · malfunctionedRT GEN OFF EICAS MSG. RAN QRH AND MESSAGE DID NOT CLEAR. LANDED UNEVENTFULLY. PERFORMED FIM 24-20 FAULT TREE 801 THRU STEP 11. RT GEN CONTROL UNIT REMOVED & REPLACED, IAW 24-22-02. PERFORMED TEST OF GCU & BPCU, IAW 24-22-02. OPS CHECK GOOD AT THIS TIME. SDR UIEA2020092532060Gcu · malfunctionedRT AC BUS OFF EICAS MSG COM QRH AND MESSAGE WAS CLEARED. PERFORMED BPCU BIT, IAW 24-22-02. NO FAULTS FOUND. PERFORMED FIM 24-20 FT 801 THROUGH STEP 11. RT GEN CONTROL UNIT R & R, IAW 24-22-02 AND PERFORMED TEST OF GCU AND BPCU, IAW 24-22-02. OPS CHK GOOD.SDR UIEA2020092512025Fault Light · false activationREPEAT WRITEUP APU FAULT ON 1 ATTEMPT, 2ND APU ATTEMPT SUCCESSFUL. PERFORMED APU CONTROL UNIT, IAW AMM 49-61-05. BITE TEST OPS CHECK AND TEST OK.
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