N441J, cancelled Jul 14, 2017
Service difficulty reports · 169
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 = 'N441J' AND deregistration_id = 'N441J-2017-07-14' 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 = 'N441J' AND deregistration_id = 'N441J-2017-07-14' 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 ARWA20070901Engine · power lossABORT TAKEOFF DUE TO NR 1 ENGINE UNABLE TO MAKE MAXIMUM TAKEOFF POWER EPR I-68 AT FIREWALL. ABORTED PRIOR REACHING 80 KNOTS. OPERATIONAL CHECKED NR 1 ENGINE AT ENGINE RUN-UP IN ACCORDANCE TO M/M 71-00; NOTED NR 1 EPR READING 0.1 LOW. ALL OTHER INDICATION NOSDR ARWA20070802Indicator · malfunctionedPOWER REDUCTION REQUIRED ON NR 2 ENGINE AFTER TAKEOFF IN ORDER TO MAINTAIN EGT LIMIT. 09-04-07 REMOVED AND REPLACED NR 2 EGT INDICATOR IN ACCORDANCE WITH MM 77-20-1. REMOVED AND REPLACED FCU IN ACCORDANCE WITH DC-8 M/M 7320-1; ACCOMPLISHED ENGINE RUN-UP INSDR ARWA20070702Brake Assy · damagedWHILE TAXING TO RAMP, AFTER LANDING, BRAKES LOCKED UP. NR 5 BRAKE ASSEMBLY LOCKED UP ON TAXI WAY. REMOVED AND REPLACED NR 5 ANTI-SKID WHEEL SPEED TRANSDUCER IAW MM 32-43-2. NR 5 MAIN WHEEL ANTI-SKID TRANSDUCER DAMAGED. REMOVED AND REPLACED NR 5 BRAKE ASSEMBLYSDR ARWA20070701Brake Assy · lockedAFTER LANDING, ON TAXI TO RAMP, BRAKES "LOCKED UP". REMOVED AND REPLACED BRAKE ASSEMBLY NR 2 IN ACCORDANCE WITH DC-8 M/M 32-42-1. OPERATIONAL CHECK FOR LEAKS OK.SDR ARWA20070606Transducer · inoperativePRIOR TO TAKEOFF ANTI-SKID INOPERATIVE LIGHT REMAINED ILLUMINATED; RETURN TO BLOCK. REMOVED AND REPLACED NR 8 MAIN LANDING GEAR WHEEL SPEED TRANSDUCER IN ACCORDANCE WITH M/M 32-43-02; GROUND TEST NORMAL IN ACCORDANCE WITH M/M 32-43-00.SDR ARWA20070604Unknown · unknownBEFORE TAKEOFF ANTI-SKID INOPERATIVE LIGHT PLUS RAI (F/W) LIGHTS BOTH ILLUMINATED.SDR ARWA20070602Bypass Valve · brokenAILERON MANUAL REVERSER LIGHT STAYS ON WHILE AILERON IS POWERED AND CONTROL CHECK UNSATISFACTORY. REMOVED AND REPLACED BROKEN BYPASS VALVE TURNBUCKLE AND ADJUSTED AILERON POWER TO MANUAL REVERSION MECHANISM IN ACCORDANCE WITH DC-8 M/M 27-11-8; OPERATIONAL CHESDR ARWA20070306Hose · leakingIN FLIGHT EN COUNTER A LOSS OF HYDRAULIC PRESSURE; PERFORMED EMERGENCY CHECKLIST. T/S AND FOUND RT MAIN LANDING GEAR BOGIE TRIM CYLINDER HYDRAULIC HOSE LEAKING; REMOVED AND REPLACED IN ACCORDANCE WITH DC8 M/M 32-33-1. SERVICE HYDRAULIC RESERVOIR IN ACCORDANCSDR ARWA20060701Skin · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LEFT ELEVATOR XE 195-313 T/E LOWER SKIN WITH CORROSION.SDR ARWA20060702Panel · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LT HORIZONTAL STABILIZER BETWEEN XE 312.500 AND XE 149.000 T/E UPPER PANELS WITH CORROSION.SDR ARWA20060703Skin · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STATION 25, L-33R SKIN WITH CORROSION.SDR ARWA20060303Pin · unknownFIRST OFFICER'S COURSE DEVIATION INDICATOR (CDI) DOES NOT CORRESPOND TO OMNI BEARING SELECTOR (OBS) IN FLIGHT. FIRST OFFICER'S HEADING "BUG" DOES NOT CORRESPOND TO SELECTED HEADING. REMOVED AND REPLACED PIN NR 1 AT PTO-117 IN ACCORDANCE WITH M/M 20-50-1 AND SDR ARWA20051202Actuator · leakingLOG PAGE NR 116558. ON POST FLIGHT FOUND LEAKING BY EMPANAGE LOWER SIDE REAR STRIKE PAD REAR ACCESS PANEL. REMOVED AND REPLACED RUDDER PACK ACTUATOR IAW MM 27-21-6. LEAK CHECK AND OPERATIONAL CHECK IAW MM 27-20-0 FOUND NORMAL, NO LEAKS NOTICE.SDR ARWA20051002Line · leakingLOST HYD FLUID FROM MAIN HYD RESERVOIR AFTER LANDING. UPON INSPECTION; FOUND FLEX LINE LEAKING ON RT MAIN GEAR TRUCK O/B HYD MANIFOLD NEXT TO BOGGIE TRIM ACTUATOR. REMOVED & REPLACED LINE WITH E EACH FLEX LINE FROM FAK. REPLACED DAMAGE LINE IN HYD SYSTEM ONSDR ARWA20050803Link Assy · vibrationAFTER TAKEOFF AND GEAR RETRACTION, EXPERIENCED CONTINUOUS VIBRATION AND NOISE FROM NOSE WHEEL WELL AREA. RETURNED AND LANDED TO INVESTIGATE. REMOVED AND REPLACED RT NOSE DOOR LINK ASSEMBLY IAW MM. PERFORMED ADJUSTMENT TEST SYSTEM IAW M/M. TEST GOOD.SDR ARWA20050507Wire · openAFTER TAKEOFF, ZNS ON NR 2 GENERATOR WITH LEFT EMERGENCY BUS POWER FAIL LIGHT ON. PERFORMED ABNORMAL CHECKLIST TO NO AVAIL; PERFORMED FUEL DUMP AS PER CHECKLIST. TRANSFERRED TO DMI 19258 AS PER MEL 24-1 CAT-C (ON T/S FOUND NR 2 GENERATOR CAUSING FAIL ZNS). SDR ARWA20050504Generator · failedDURING CLIMB-OUT, NR 2 GEN SYSTEM DEVELOPED A ZNS. AFTER PERFORMING ABNORMAL CHECK-LIST ONLY LT EMERGENCY BUSS WAS RESTORED. REMOVED AND REPLACED CSD AND AC GENERATOR IN ACCORDANCE WITH DC-8 M/M 24-10-1 AND 24-20-1. LEAKS CHECKED; NO LEAKS NOTED; GENERATOR SDR ARWA20050404Connector · dirtyDURING TAXI, ELEVATOR POSITION INDICATOR (EPI) FAILED DURING FLIGHT CONTROL CHECK. TRANSFERRED TO DMI NR 19171 AS PER MEL 27-9 CAT "C". CLEANED AND SECURED ELEVATOR EPI INDICATOR IN ACCORDANCE WITH M/M 31-10-30. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/SDR ARWA20041203Amplifier · malfunctionedAFTER TAKEOFF NR 4 ENGINE FIRE WARNING ILLUMINATED INTERMITTENTLY, SHUT DOWN ENGINE AND RETURNED TO KMIA AFTER FUEL DUMPING. OVERWEIGHT LANDING IN KMIA, SMOOTH LANDING. REMOVED AND REPLACED AMPLIFIER (POSITION NR 4) IN ACCORDANCE WITH MM 26-10-4 AND REMOVEDSDR ARWA20041005Fire Loop · shortedON CLIMBOUT THROUGH 15,000 FT MASTER FIRE WARNING SOUNDED WITH LIGHT INDICATION ON NR 4 ENGINE. PERFORMED EMERGENCY CHECKLIST (RETARDED POWER LEVER, FIRE SHUTOFF LEVER FORWARD, LIGHT CONTINUED ON, FIRE EXT AGENT, LIGHT WENT OUT). COMPLETED CHECKLIST, ALL OTHSDR ARWA20040904Pin · damagedDURING UP-LATCH CHECK THE GEAR NOT LATCHED, LIGHT ILLUMINATED AND PERFORMED ABNORMAL CHECKLIST, THEN BOTH GEAR NOT LATCHED AND DOOR NOT LATCHED REMAINED ILLUMINATED. REMOVED RT GEAR ASSY SENT TO AAR LANDING GEAR; REPAIRED STUD ASS PART NR 5759145508 ON RT GEASDR ARWA20040804Indicator · failedDURING TAXI, FIRST OFFICER'S VERTICAL SPEED INDICATOR (VSI) DISPLAY SHOWS REPEATER ANNUNCIATOR. FAILURE AND NO NEEDLE. REMOVED AND REPLACED TCAS/VSI AT FIRST OFFICER'S SIDE. CHECK SYSTEM ON GROUND OK IN ACCORDANCE WITH MM 34-12-0 AND 34-11-1.SDR ARWA20040802Indicator · inoperativeWEATHER RADAR DOES NOT PAINT WEATHER NOR DOES IT WORK IN MAPPING MODE. TEST FUNCTION IS NORMAL; AIRCRAFT RETURNED. REMOVED AND REPLACED WHEATHER INDICATOR IN ACCORDANCE WITH MM 34-00; OPERATIONAL CHECK DUE; REMOVED AND REPLACED RADAR R/T IN ACCORDANCE WITH MSDR ARWA20040801Transceiver · failedCLIMBING WEATHER RADAR DOES NOT PAINT WEATHER; AIRCRAFT RETURNED. REMOVED AND REPLACED WEATHER RT AND ANTENNA IAW MM 34-41-0 AND 34-41-1 GROUND TEST NORMAL.SDR ARWA20040703Unknown · unknownAFTER APP TAKEOFF POWER HEARD BANG ON LEFT HAND SIDE WING. INSPECTED LEFT HAND WING IN ACCORDANCE WITH MM 57-00; NO OBVIOUS DEFECTS NOTED. ALSO INSPECTED LEFT HAND MAIN LANDING GEAR AND DOORS IN ACCORDANCE WITH MM 32-10-0, NO OBVIOUS DEFECTS NOTED. PERFORMESDR ARWA20040301Fitting · crackedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 3 PYLON STATION YN 300 APPROX. FOOT STOOL FITTING LEFT SIDE WITH CRACK. REMOVED AND REPLACED FOOT STOOL FITTING FROM NR 3 PYLON IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-000084, DATED 22-MAR-04, DOUGLASSDR ARWA20040202Web · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE INTERIOR BETWEEN STA 1060.000 AND STA 1080.000 LT CUSP WITH CORROSION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH BOEING ROD SKETCH 04-05-18-001. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR.SDR ARWA20040201Cargo Track · corrodedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT BETWEEN STA 940.000 AND STA 1500.000, RBL 58.5 INCHES TRACK WR SECTION WITH CORROSION. REMOVED CORROSION IN ACCORDANCE WITH DC-8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IN ACCORDANCE SDR ARWA20040104Keelbeam · crackedDURING A C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LT MAIN LANDING GEAR W/W STATION 920, KEELBEAM LT TEE EXTRUSION WITH 3 INCH CRACK. REPAIRED KEEL WEB STIFFENER AT STA 920 IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-00005H, DATED 02 MARCH 04, DC8 SRM 51-2SDR ARWA20031207Bulkhead · corrodedNR 970. DURING (C) CHECK INSPECTION, NLG WW RT TUNNEL STATION 8.000 PRESSURE BULKHEAD FORWARD FACE. NOSE LANDING GEAR RT FITTING WITH CORROSION AT L-31.SDR ARWA20031003Warning Light · false activationLANDING GEAR DOOR NOT LATCH LIGHT ILLUMINATED AFTER TAKEOFF; PERFORMED ABNORMAL CHECKLIST, LIGHT WENT OUT. CLEANED, INSPECTED & LUBRICATED LANDING GEARS AND DOORS IAW DC8 MM 12-81-1. ACCOMPLISHED GEARS SWING IAW DC8 MM 32-30-0. NO DEFECTS NOTED.SDR ARWA20030914Bleed Valve · stuckUNABLE TO OBTAIN MAX POWER INDICATION WITH NR 1 TROTTLE AT IT'S FULL FORWARD STOP POSITION. FOUND NR 1 ENGINE SURGE BLEED VALVE STUCK OPEN; REMOVED AND REPLACED NR 1 ENGINE SURGE BLEED VALVE IAW DC-8 MM 75-30-3; OPERATIONAL CHECK NORMAL IAW MM 71-00.SDR ARWA20030901Cylinder · brokenAFTER TAKE-OFF, WHEN GEAR WAS RETRACTED; NOT LATCHED AND DOORS NOT LATCHED. LIGHT REMAINED ILLUMINATED. PERFORMED LANDING GEAR SYSTEM ABNORMAL CHECK LIST AND RETURNED TO MNMG. FOUND RT GEAR BOGIE TRIM CYLINDER BROKEN AT FORWARD ATTACH POINT; REMOVED AND RESDR ARWA20030807Door Frame · crackedDURING ROUTINE INSPECTION THE FOLLOWING WAS FOUND; AFT SERVICE DOOR JAMB, AFT TOP CORNER WITH CRACK OF 1.125 INCH. REPAIRED THE AFT SERVICE DOOR JAMB AFT TOP CORNER IAW SRM 53-2-0 FIG 16, SHEETS 4, 5, 6, 7 & 8 TEMPORARY REVISION 53-156, DATED 12/20/02. (EA 10SDR ARWA20030806Door Frame · crackedDURING ROUTINE INSPECTION THE FOLLOWING WAS FOUND; AFT ENTRANCE DOOR JAMB AFT BOTTOM CORNER WITH CRACKS OF 0.625 & 0.437 INCH. REPAIRED THE AFT ENTRANCE DOOR JAMB AFT BOTTOM CORNER IAW SRM 53-2-0 FIG 18, SHEETS 1, 5, 6, 7 & 8, TEMPORARY REVISION 53-134 & TEMPSDR ARWA20030801Bleed Valve · inoperativeCOMPRESSOR STALL NR 2 ENGINE COMMENCING THE TAKE OFF ROLL. REJECTED TAKE OFF (RTO). REMOVED AND REPLACED NR 2 PRESSURE RATIO SURGE BLEED VALVE IAW MM 75-30-3. OPERATIONAL CHECK ON RUN UP IAW MM 71-0 FOUND NORMAL.SDR ARWA20030602Transmitter · inoperativeAFTER BRAKE RELEASE, WHILE SETTING MAX POWER, NUMBER ONE ENGINE OIL PRESSURE ROSE TO 60 PSI. REMOVED AND REPLACED PRESSURE TRANSMITTER IAW MM 79-32-1. ACCOMPLISHED ENGINE RUN UP IAW ARROW AIR J/C 72-000-30-02SDR ARWA20030302Wire · damagedON FINAL ANTI-SKID LIGHT STAYED ON WITH LFI INDICATION. CHECKED ANTI-SKID WIRING IAW W/D 32-3-0. FOUND BROKEN WIRE GOING TO LT IN-BOUND VALVE, REPAIRED WIRE IN ACCORDANCE WITH MM 20-50-1, OPERATIONAL CHECKED ANTI-SKID SYSTEM IAW MM 32-43-0. OPERATIONAL CHECKSDR ARWA20030105Line · leakingNR 2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO FLUCTUATING OIL PRESSURE AND INTERMITTENT PRESSURE WARNING LIGHT AT 1555Z WINDMILLING OIL PRESSURE 15-25 PSI. INSPECTED NR 2 ENGINE, FOUND RIGID LINE BETWEEN MAIN OIL FILTER AND DIFFERENTIAL PRESSURE SWITCH DAMAGED (LSDR ARWA20030101Spar CapLOG PAGE # 503179. DISCREPANCY: DURING 1A CHECK THE FOLLOWING WAS FOUND; ITEM # 128M: L/H WING AUXILIARY SPAR INBD. UPPER LOG WITH CRACK. GENERATED BY J/C # 51-020-04-06-1. CORRECTIVE ACTION: ACCOMPLISHED TEMPORARY REPAIR IN ACCORDANCE WITH BOEING MESSAGE ISDR ARWA20021103Gyro · failedFIRST OFFICER'S COMPASS FLAG IN VIEW; FIRST OFFICER'S HORIZONTAL INDICATOR (HSI) CAPTAIN'S RADIO MAGNETIC INDICATOR (RMI). REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO IAW MM 34-21-1. ALSO REMOVED AND REPLACED CIRCUIT BREAKER 2 AMP IAW MM 20-50-1. PERFORMED OSDR ARWA20021007Cap · looseNR 4 ENGINE OIL QUANTITY DROPPED TO ZERO. PRECAUTIONARY SHUT DOWN: N1 26 PERCENT, N2 35 PERCENT, OIL TEMP 90C. INSPECTED NR 4 ENGINE AND FOUND CSD SPLINE STAND PIPE CAP LOOSE, RE-TIGHTENED CAP IAW MM 79-20-6. SERVICED ENGINE OIL IAW 12-20-1 RAN ENGINE PER SDR ARWA20021001Fire Detector · malfunctionedNR 4 ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. OVERWEIGHT LANDING AT 277.0 LBS PERFORMED. REMOVED AND REPLACED NR 4 FIRE SENSOR ON BURNED SECTION OF THE ENGINE IAW MM 26-10-1. ALSO REWIRED FROM PL-1341 CONNECTOR TO PL- 1368, PL-1367 CONNECTOR AND REPLACESDR ARWA20020916Line · leakingCLIMB FL 270 NR 2 ENGINE OIL PRESSURE FLUCTUATED BELOW 35 PSI, OIL PRESS LIGHT CAME ON, OIL TEMPERATURE WENT UP. FOLLOWED ENGINE SHUT DOWN PROCEDURES. 15 PSI OIL PRESS FOR 30 MINUTES. AIRCRAFT LANDED OVERWEIGHT WITHOUT INCIDENT. INSPECTED NR 2 ENGINE FOR EVIDESDR ARWA20020904Computer · malfunctionedDURING DESCEND PITCH TRIM COMPENSATOR FAILED IN EXTENDED POSITION, PERFORMED EMERGENCY CHECKLIST PHASE 1 AND 2 ITEMS; INITIATED A FLAP 50 LANDING AND DECLARED AN EMERGENCY IAW PHASE 2 EMERGENCY ABNORMAL CHECKLIST. REMOVED AND REPLACED PITCH COMPUTER IAW MM 27SDR ARWA20020809Oil System · lack of lubeNR 3 ENGINE OIL QUANTITY INDICATING ZERO; WITH OIL PRESSURE FLUCTUATING AND LOW OIL PRESSURE, LIGHT ILLUMINATED. PERFORMED IN-FLIGHT ENGINE SHUTDOWN AT 1920Z. NOTE WINDMILLING OIL PRESSURE 20 PSI TURNED ON START LEVER AT 2020Z AS PER AFM. SERVICED NR 3 ENGISDR ARWA20020803Engine · power lossAFTER BRAKE RELEASE, LOST PARTIAL POWER ON NR 4 ENGINE. ABORTED TAKEOFF AND RETURNED TO RAMP. REMOVED AND REPLACED NR 4 ENGINE, OPS CHECK AND LEAK CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR ARWA20020801Hydraulic Line · blownLOST ALL HYDRAULIC ON LANDING. CHECK HYDRAULIC QUANTITY AND TO BOC AT STANDARD PIPE. REPLACED BLOWN BRAKE HYDRAULIC LINE AT LT GEAR, SERVICED MAIN HYDRAULIC SYSTEM; RUN UP ENGINES AND CHECK HYDRAULIC PUMPS OFR OPS AND FOUND NORMAL. OPERATED ALL FLIGHT CONTRSDR ARWA20020601B-Nut · looseABORTED TAKEOFF DUE TO NR 4 ENGINE WOULD NOT GO TO MAX POWER. FOUND COMPRESSOR BLEED ACTUATOR TO CONTROL CLOSED TUBE B-NUT LOOSE; TIGHTENED B-NUT IAW MM 75-30-2; PERFORMED FLAG CHECK ENGINE RUN UP OPS CHECKED NORMAL IAW MM 75-30-3 AND 71-00 MAX TAKEOFF POWER SDR ARWA20020310Hydraulic Line · leakingWHEN READY TO TAXI, HYDRAULIC QUANTITY GAUGE INDICATED LOSS OF FLUID, HYDRAULIC PRESSURE GAUGE INDICATED LOSS OF PRESS. ACCOMPLISHED APPROPRIATE CHECKLIST, RETURNED TO RAMP. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE FROM NR 3 ENGINE HYDRAULIC PUMP, OPS CH
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