# Service difficulty reports: N845AX, cancelled Jan 26, 2018 A list on [N845AX, cancelled Jan 26, 2018](https://openairdocs.org/deregistered/N845AX-2018-01-26.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ABXA000481](https://openairdocs.org/sdr/ABXA000481.md): Latch · failed · Oct 28, 2000 · N845AX · Doug DC861 · Fixed Inner Doors > COCKPIT DOOR KNOB WOULD NOT OPEN DOOR FROM OUTSIDE COCKPIT. REPAIRED AND LUBED DOOR LATCH MECHANISM IAW DC8 MM. OPS CHECKED GOOD AT THIS TIME. - [SDR ABXA000472](https://openairdocs.org/sdr/ABXA000472.md): Doubler · cracked · Oct 19, 2000 · N845AX · Doug DC861 · Nacelle/Pylon, Plate/Skin > FOUND 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. - [SDR ABXA000363](https://openairdocs.org/sdr/ABXA000363.md): Wire · broken · Aug 3, 2000 · N845AX · Doug DC861 · Engine Oil System Wiring > DURING 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. - [SDR ABXA000153](https://openairdocs.org/sdr/ABXA000153.md): Floorbeam · corroded · Mar 20, 2000 · N845AX · Doug DC861 · Fuselage Main, Floor Beam > FLOORBEAM AT FUSELAGE STATION 920, RIGHT SIDE BETWEEN SEAT TRACK A AND B AT CUSPWAS CORRODED. REPAIRED FLOORBEAM IAW ABX REA D853-35008. - [SDR ABXA000145](https://openairdocs.org/sdr/ABXA000145.md): Frame · corroded · Mar 13, 2000 · N845AX · Doug DC861 · Fuselage Main, Frame > STATION 1140 FRAME CORRODED UNDER UPPER FLANGE. REPAIRED IAW ABX REA D853-34995MR. - [SDR ABXA000144](https://openairdocs.org/sdr/ABXA000144.md): Keelbeam · corroded · Mar 13, 2000 · N845AX · Doug DC861 · Fuselage Main, Keel > KEEL BEAM CORRODED, CENTER ASSY COMPARTMENT AT FS 665. REPAIRED IAW ABX REA D853-34991MR. - [SDR ABXA99000143](https://openairdocs.org/sdr/ABXA99000143.md): Skin · corroded · Mar 7, 2000 · N845AX · Doug DC861 · Fuselage Main, Plate/Skin > DURING C-CHECK, FOUND SKIN PANEL CORRODED AT STATION 690. REPAIRED IAW ABX REA D853-34983MR. - [SDR ABXA9900035](https://openairdocs.org/sdr/ABXA9900035.md): Rod · broken · Jan 22, 1999 · N845AX · Doug DC861 · Flight Compartment Windows > CAPTAIN'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. - [SDR ABXA9800838](https://openairdocs.org/sdr/ABXA9800838.md): Ctc · seized · Sep 16, 1998 · N845AX · Doug DC861 · Cabin Compressor System > AFTER 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 - [SDR ABXA9800479](https://openairdocs.org/sdr/ABXA9800479.md): Engine · failed · Jun 2, 1998 · N845AX · Doug DC861 · Engine (Turbine/Turboprop) > DURING 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 - [SDR ABXA00454](https://openairdocs.org/sdr/ABXA00454.md): Retract Mech · lack of lube · May 19, 1998 · N845AX · Doug DC861 · Landing Gear Retraction/Extension System > AFTER 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 OPE - [SDR ABXA9800422](https://openairdocs.org/sdr/ABXA9800422.md): Vane · corroded · Mar 25, 1998 · N845AX · Doug DC861 · Trailing Edge Flaps > RIGHT VANE HAD WIDESPREAD DELAMINATION AND CORROSION. REPLACED ALL HONEYCOMB CORE DOUBLERS AND SKIN. - [SDR ABXA00035](https://openairdocs.org/sdr/ABXA00035.md): Rod · broken · Jan 26, 1998 · N845AX · Doug DC861 · Flight Compartment Windows > CAPTAIN'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. - [SDR ABXA9600632](https://openairdocs.org/sdr/ABXA9600632.md): Engine · failed · Oct 2, 1996 · N845AX · Doug DC861 · Engine (Turbine/Turboprop) > NR 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 EN - [SDR ABXA9600618](https://openairdocs.org/sdr/ABXA9600618.md): Battery Pack · discharged · Aug 30, 1996 · N845AX · Doug DC861 · Emergency Lighting > EMERGENCY LIGHTING FAILED A2 CHECK INSPECTION. REPLACED EMERGENCY LIGHTING BATTERY PACK. OPS CHECKED NORMAL I/A/W DC-8 M.M. 33-50-0. - [SDR ABXA9600612](https://openairdocs.org/sdr/ABXA9600612.md): Rudder Pump · leaking · Aug 18, 1996 · N845AX · Doug DC861 · Rudder Control System > ONE 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, QUANT - [SDR ABXA9600611](https://openairdocs.org/sdr/ABXA9600611.md): O-Ring · cut · Aug 18, 1996 · N845AX · Doug DC861 · Hydraulic System, Main > LOST 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 PUMP - [SDR ABXA9600600](https://openairdocs.org/sdr/ABXA9600600.md): Lamp · defective · Jul 19, 1996 · N845AX · Doug DC861 · Emergency Lighting > EMERGENCY EXIT LIGHT DOES NOT INDICATE DISARMED. RELAMPED EMERGENCY EXIT LIGHT, OPS CHECK GOOD. - [SDR ABXA9600597](https://openairdocs.org/sdr/ABXA9600597.md): Boost Pump · defective · Jul 16, 1996 · N845AX · Doug DC861 · Fuel Boost Pump > NR 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. GRO - [SDR ABXA9600497](https://openairdocs.org/sdr/ABXA9600497.md): O-Ring Seal · defective · May 24, 1996 · N845AX · Doug DC861 · Hydraulic Pump (Electric/Engine), Main > DURING 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 SY - [SDR ABXA9500656](https://openairdocs.org/sdr/ABXA9500656.md): Engine · failed · Aug 8, 1995 · N845AX · Doug DC861 · Engine (Turbine/Turboprop) > NR 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. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N845AX-2018-01-26/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.