N845AX, cancelled Jan 26, 2018

Service difficulty reports · 21

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 = 'N845AX' AND deregistration_id = 'N845AX-2018-01-26'
  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 ABXA000481Latch · failedCOCKPIT DOOR KNOB WOULD NOT OPEN DOOR FROM OUTSIDE COCKPIT. REPAIRED AND LUBED DOOR LATCH MECHANISM IAW DC8 MM. OPS CHECKED GOOD AT THIS TIME.Oct 28, 2000 · N845AX · Doug DC861 · Fixed Inner DoorsSDR ABXA000472Doubler · crackedFOUND 12 INCH CRACK ON NR 4 INBOARD SIDE OF PYLON SKIN STATION YOP 220. *S/D* REPAIRED IAW DC8 SRM 54-2-1 AND REA D854-38893-MR.Oct 19, 2000 · N845AX · Doug DC861 · Nacelle/Pylon, Plate/SkinSDR ABXA000363Wire · brokenDURING CLIMBOUT, NR 4 ENGINE OIL TEMPERATURE WENT TO 155 DEGREES. PERFORMED ABNORMAL CHECKLIST. TEMPERATURE DID NOT CHANGE. SHUT NR 4 ENGINE DOWN. OIL TEMPERATURE REMAINED AT 155 DEGREES FOR ENTIRE FLIGHT. FOUND GROUND WIRE E-355 BROKEN AT GROUND LUG 941.Aug 3, 2000 · N845AX · Doug DC861 · Engine Oil System WiringSDR ABXA000153Floorbeam · corrodedFLOORBEAM AT FUSELAGE STATION 920, RIGHT SIDE BETWEEN SEAT TRACK A AND B AT CUSPWAS CORRODED. REPAIRED FLOORBEAM IAW ABX REA D853-35008.Mar 20, 2000 · N845AX · Doug DC861 · Fuselage Main, Floor BeamSDR ABXA000145Frame · corrodedSTATION 1140 FRAME CORRODED UNDER UPPER FLANGE. REPAIRED IAW ABX REA D853-34995MR.Mar 13, 2000 · N845AX · Doug DC861 · Fuselage Main, FrameSDR ABXA000144Keelbeam · corrodedKEEL BEAM CORRODED, CENTER ASSY COMPARTMENT AT FS 665. REPAIRED IAW ABX REA D853-34991MR.Mar 13, 2000 · N845AX · Doug DC861 · Fuselage Main, KeelSDR ABXA99000143Skin · corrodedDURING C-CHECK, FOUND SKIN PANEL CORRODED AT STATION 690. REPAIRED IAW ABX REA D853-34983MR.Mar 7, 2000 · N845AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA9900035Rod · brokenCAPTAIN'S WINDOW (EMERG EXIT) LATCH PIN WAS FOUND BROKEN DURING PREFLIGHT. REPLACED LOWER FORWARD LINKAGE ROD IAW DC8 MM 56-10-3, OPS CHECKED GOOD.Jan 22, 1999 · N845AX · Doug DC861 · Flight Compartment WindowsSDR ABXA9800838Ctc · seizedAFTER TAKEOFF WHILE CLIMBING THRU FL200, A LOUD CTC HOWL WAS HEARD WITH A STRONG SMELL OF SOMETHING BURNING. OBSERVED NR 1 CTC SURGING. SHUT OFF NR 1 CTC AND BURNING ODOR DISAPPEARED IN APPROXIMATELY 5 MINUTES. NO ADDITIONAL PROBLEMS NOTED. FOUND NR 1 CTC Sep 16, 1998 · N845AX · Doug DC861 · Cabin Compressor SystemSDR ABXA9800479Engine · failedDURING CRUISE FLIGHT AT FL 280, MACH.82, A SUDDEN VIBRATION WAS FELT. NR 2 ENGINE INDICATED; EGT 540, N2 80 PERCENT, OIL TEMP 125 DEG. OIL QUANTITY WAS ZERO AND EPR WAS 1.0. NR 2 ENGINE WAS SHUTDOWN AND EMERG CHECKLIST WAS ACCOMPLISHED. ENGINE WINDMILLED Jun 2, 1998 · N845AX · Doug DC861 · Engine (Turbine/Turboprop)SDR ABXA00454Retract Mech · lack of lubeAFTER TAKEOFF WHEN LANDING GEAR RETRACTED, HEARD LOUD RUMBLING NOISE FROM NOSE GEAR AREA. ALL RETRACTION INDICATIONS WERE NORMAL. RECYCLED GEAR THREE TIMES WITH SAME RESULT. GEAR FAILED UPLATCH CHECK. AIR TURNED BACK TO ONT. NOSE LANDING GEAR DOOR WAS OPEMay 19, 1998 · N845AX · Doug DC861 · Landing Gear Retraction/Extension SystemSDR ABXA9800422Vane · corrodedRIGHT VANE HAD WIDESPREAD DELAMINATION AND CORROSION. REPLACED ALL HONEYCOMB CORE DOUBLERS AND SKIN.Mar 25, 1998 · N845AX · Doug DC861 · Trailing Edge FlapsSDR ABXA00035Rod · brokenCAPTAIN'S WINDOW (EMERG EXIT) LATCH PIN WAS FOUND BROKEN DURING PREFLIGHT. REPLACED LOWER FORWARD LINKAGE ROD IAW DC8 MM 56-10-3, OPS CHECKED GOOD.Jan 26, 1998 · N845AX · Doug DC861 · Flight Compartment WindowsSDR ABXA9600632Engine · failedNR 2 OIL PRESSURE LIGHT ILLUMINATED, OIL PRESSURE FLUCTUATED BELOW 35 PSI TO 20 PSI. SECURED ENGINE AT 1243 Z, RPM NEVER FELL BELOW 24 PERCENT N-2 UNTIL TOUCHDOWN. HIGHEST WAS 35 PERCNET N-2, APPROXIMATELY 5 PSI OIL PRESSURE. REPLACED NR 2 ENGINE IAW ABX ENOct 2, 1996 · N845AX · Doug DC861 · Engine (Turbine/Turboprop)SDR ABXA9600618Battery Pack · dischargedEMERGENCY LIGHTING FAILED A2 CHECK INSPECTION. REPLACED EMERGENCY LIGHTING BATTERY PACK. OPS CHECKED NORMAL I/A/W DC-8 M.M. 33-50-0.Aug 30, 1996 · N845AX · Doug DC861 · Emergency LightingSDR ABXA9600612Rudder Pump · leakingONE HOUR INTO FLIGHT NOTICED HYDRAULIC QUANTITY SLOWLY DECREASING. MARKED GAUGE AND CONTINUED TO DECREASE VERY SLOWLY. APPROXIMATELY ONE NEEDLE WIDTH ABOVE STANDPIPE PERFORMED HYDRAULIC FLUID LOSS CHECKLIST. ONCE HYDRAULICS DEPRESSURIZED AND ISOLATED, QUANTAug 18, 1996 · N845AX · Doug DC861 · Rudder Control SystemSDR ABXA9600611O-Ring · cutLOST HYDRAULIC QUANTITY DOWN TO THE N, RAN HYDRAULIC PRESS/LOSS CHECKLIST. THE QUANTITY STAYED AT THE N. VISUALLY INSPECTED AIRCRAFT, NO LEAKS NOTED. SERVICED HYDRAULIC SYSTEM, RAN NR 2 AND NR 3 ENGINES, CYCLED ALL SYSTEMS, FOUND NR 3 ENGINE HYDRAULIC PUMPAug 18, 1996 · N845AX · Doug DC861 · Hydraulic System, MainSDR ABXA9600600Lamp · defectiveEMERGENCY EXIT LIGHT DOES NOT INDICATE DISARMED. RELAMPED EMERGENCY EXIT LIGHT, OPS CHECK GOOD.Jul 19, 1996 · N845AX · Doug DC861 · Emergency LightingSDR ABXA9600597Boost Pump · defectiveNR 4 ENGINE FEED PUMP PRESSURE LIGHT ILLUMINATED WHILE CLIMBING THROUGH 24,000 FEET AND ENGINE FLAMED OUT. CHECKLIST PROCEDURES WERE ACCOMPLISHED AND THE ENGINE HAD RELIGHT. REPLACED BOOST AND FEED PUMPS FOR THE NR 4 ENGINE IAW DC8 MM, CHAPTER 28-20-00. GROJul 16, 1996 · N845AX · Doug DC861 · Fuel Boost PumpSDR ABXA9600497O-Ring Seal · defectiveDURING APPROACH, HYDRAULIC FLUID QUANTITY DROPPED TO THE STANDPIPE LEVEL AND THE HYDRAULIC PRESSURE DECREASED AFTER THE LANDING GEAR WAS EXTENDED. REPLACED DEFECTIVE O-RING SEAL ON THE NR 3 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE FITTING. OPERATED HYDRAULIC SYMay 24, 1996 · N845AX · Doug DC861 · Hydraulic Pump (Electric/Engine), MainSDR ABXA9500656Engine · failedNR 4 ENGINE SHUTDOWN IN FLIGHT DUE TO ENGINE FAILURE. EGT MAXIMUM TEMPERATURE WAS 760 DEGREES CELSIUS. NR 4 ENGINE WAS SECURED IAW EMERGENCY PROCEDURE CHECKLIST. AIRCRAFT RETURNED TO ILN. REMOVED AND REPLACED ENGINE. TRIMMED DURING GROUND RUN IAW DC 8 MM.Aug 8, 1995 · N845AX · Doug DC861 · Engine (Turbine/Turboprop)
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