N849AX, cancelled Mar 4, 2005

Service difficulty reports · 118

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 = 'N849AX' AND deregistration_id = 'N849AX-2005-03-04'
  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 ABXA030130Controller · defectiveWINDSHIELD HEAT, SPARKS CAME FROM FORWARD RIGHT WINDSHIELD. SPARKS WERE COMING FROM LOWER RIGHT. CIRCUIT BREAKERS WERE PULLED. REPLACED RIGHT WINDSHIELD TEMP. CONTROL DUE TO WINDOW REPLACEMENT IAW DC-8 AMM 30-41-0-1-2-0001. OPS CHECKED GOOD. REPLACED RIGApr 3, 2003 · N849AX · Doug DC861 · Windshield/Door Rain/Ice RemovalSDR ABXA030061Control Cable · out of adjustGEAR RETRACTION RED GEAR LIGHT STAYED ON. LANDING GEAR RT DOOR LATCHING SELECTOR ON FLT ENGINEER'S PANEL SHOWED RT DOOR. CYCLED GEAR, LIGHTS WENT OUT. ADJUSTED RT MLG DOOR FOLLOW UP MECHANISM AND CABLES 135A & 134A IAW DC-8 MM 32-31-05. CHECKED RT MLG DOOR UPJan 29, 2003 · N849AX · Doug DC861 · Landing Gear Door Retract SectionSDR ABXA030057Actuator · defectiveWHEN GEAR WAS RETRACTED AFTER TAKE-OFF, LANDING GEAR UNSAFE LIGHT REMAINED ON. RT MLG DOOR INDICATED NOT LATCHED. CYCLED GEAR PER ILN MAINTENANCE REQUEST. NO CHANGE IN PROBLEM. REPLACED RT MLG DOOR ACTUATOR IAW DC-8 MM 32-31-05. ADJUSTED FOLLOW-UP HITCH IAJan 27, 2003 · N849AX · Doug DC861 · Landing Gear Door ActuatorSDR ABXA030058Roller · out of adjustGEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RT DOOR INDICATED NOT LATCHED ON FLIGHT ENGINEERS PANEL. CYCLED GEAR ONCE AND ALL CHECKED GOOD. SHIMMED RT MLG DOOR UPLATCH ROLLER IAW DC-8 MM 32-31-04. PULL CHECK OF RT MLG DOOR IAW DC-8 MM 32-31-04. PERFOJan 24, 2003 · N849AX · Doug DC861 · Landing Gear Door Retract SectionSDR ABXA030046Torque Tube · out of adjustGEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED WITH RT MLG DOOR SHOWING UNSAFE. CYCLED LANDING GEAR, LIGHTS REMAINED ON. PLACED GEAR HANDLE TO UPLATCH POSITION. LIGHT WENT OUT. EXCESSIVE INBOARD AND OUTBOARD GAPS WERE FOUND ON THE RT MLG TORQUE TUBE. Jan 22, 2003 · N849AX · Doug DC861 · Landing Gear Retraction/Extension SystemSDR ABXA020069Battery Pack · dischargedLOST EXTERNAL POWER AND NO EMERGENCY EXIT LIGHT ILLUMINATED WITH SWITCH IN ARMED POSITION. REPLACED THE EMERGENCY BATTERY PACK. OPS CHECKED GOOD IAW DC-8 MM.Jul 29, 2002 · N849AX · Doug DC861 · Emergency LightingSDR ABXA020002Switch · defective# 1 engine low oil pressure light on in flight. Oil pressure was 46 psi. Engine was shut down at 0905 Z. Windmilling oil pressure on secured engine was 12 psi for 19 minutes. Replaced low pressure switch IAW DC-8 MM 79-30. Ran # 1 engine, no leaks noted. EngiJun 24, 2002 · N849AX · Doug DC861 · Engine Oil PressureSDR ABXA010831Doubler · crackedLEFT WING 505F PANEL HAD 10 EACH CRACK INDICATIONS AT FASTENER HOLES. REPAIRED AREA IAW REA D857-43069MR.Mar 29, 2002 · N849AX · Doug DC861 · Wing StructureSDR ABXA010832Fitting · corrodedSURFACE CORROSION FOUND IN CARGO DOOR TORQUE BOX AT STA. 345, LONGERON 35 RIGHT, LOWER CARGO COMPARTMENT. REPLACED 'Z' FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-24, REA D853-43-83MR AND REA D853-43076MR.Mar 28, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010833Doubler · corrodedAFT CARGO, LONGERON 32 RIGHT, B/S 1200, WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21 AND REA D853-43071MR.Mar 27, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010801Fitting · cracked#3 PYLON V-BLOCK SUPPORT FITTING HAD A CRACK IN IT. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-3-0, 51-1-23 AND 56-3-0.Mar 23, 2002 · N849AX · Doug DC861 · Nacelle/Pylon StructureSDR ABXA010800Strap · corroded#1 PYLON "T" CAP STRAP HAD CORROSION AT WING STATION 485.00, LOWER SPAR CAP, FORWARD SPAR. REMOVED AND REPLACED THE FORWARD SPAR STRAP, REMOVED AND REINSTALLED THE #1 PYLON "T" DOUBLER IAW DC-8 SRM 51-1-20D, 51-1-8.Mar 22, 2002 · N849AX · Doug DC861 · Nacelle/Pylon StructureSDR ABXA010789Seat Track · crackedFORWARD CARGO AT F.S. 340 - 360, LEFT BUTT LINE 50, SEAT TRACK WAS CRACKED. REPLACED SEAT TRACK IAW DC-8 SRM 51-1-8, 51-3-0, 51-1-21 AND ZANTOP DWG. #86302.Mar 20, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010788Fitting · crackedFORWARD CARGO AT F.S. 200 - 220, LONGERON 31 LEFT, SPLICE FITTING WAS CRACKED. REPLACED FITTING IAW DC-8 SRM 51-1-20D.Mar 19, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010787Frame · crackedFORWARD CARGO AT F.S. 180, ABOVE LONGERON 36 FRAME, UPPER CHORD WAS CRACKED AND BENT. REPAIRED AREA IAW DC-8 SRM STD-5310-002 AND SRM 51-1-8.Mar 19, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010786Seat Track · crackedFORWARD CARGO AT F.S. 580 - 600, LEFT BUTT LINE 50, SEAT TRACK WAS CRACKED. REPLACED SEAT TRACK IAW DC-9 SRM 51-3-0, 51-1-8 AND ZANTOP DWG. #86302.Mar 19, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010830Longeron · corrodedFORWARD ACCESSORY COMPARTMENT AT F.S. 640 - 660, LONGERON 31 RIGHT, WAS CRACKED. FABBED REPAIR STRAP AND REPAIRED AREA IAW DC-8 SRM 53-2-0, 53-4-1, 51-1-20D AND REA D853-43068MR.Mar 18, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010785Fitting · crackedFORWARD CARGO, F.S. 380 - 400, LONGERON 31 LEFT, SPLICE FITTING WAS CRACKED. REMOVED AND REPLACED FITTING AT STA. 390, LONGERON 31 LEFT IAW DC-8 SRM 51-1-24 AND 51-1-20D.Mar 16, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010791Strap · crackedT-CAP DOUBLER STRAP AT WS 485.00, FORWARD SPAR, LOWER CRACKED NR 4 ALT. REMOVED AND REPLACED DOUBLER STRAP IAW DC-8 SRM 51-1-20D, 51-1-24 AND DAC DWG 5803958.Mar 15, 2002 · N849AX · Doug DC861 · Wing Miscellaneous StructureSDR ABXA010790Fitting · crackedFORWARD LOWER CARGO, STATION 272, FITTING WAS CRACKED FORWARD OF C1 DOOR. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-3-1 AND 51-1-24.Mar 15, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010784Fitting · crackedSPLICE FITTING CRACKED AT LONGERON 27 RIGHT, STATION 450, FORWARD LOWER CARGO. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-1-21.Mar 15, 2002 · N849AX · Doug DC861 · Fuselage Main, StructureSDR ABXA010834Spar Cap · crackedRIGHT WING, FORWARD LOWER SPAR CAP HAD 9 EACH FASTENERS HOLES SHOWING CRACK INDICATIONS. REPAIRED DAMAGED HOLES IAW REA D857-43058.Mar 12, 2002 · N849AX · Doug DC861 · Wing StructureSDR ABXA010792Seat Track · crackedFORWARD CARGO AT F.S. 580 - 600, AT LEFT BUTT LINE 55, SEAT TRACK WAS CRACKED. REMOVED AND REPLACED SEAT TRACK IAW DC-8 SRM 51-3-0, 51-1-24 AND 51-1-8.Mar 10, 2002 · N849AX · Doug DC861 · Fuselage Structure (General)SDR ABXA010777Splice · crackedAFT LOWER CARGO COMPARTMENT, LONGERON SPLICE TIE CRACKED BETWEEN B.S. 1300 - 1320, LONGERON 31 LEFT. REPLACED SPLICE IAW DC-8 SRM 51-1-20D AND 51-3-2.Mar 10, 2002 · N849AX · Doug DC861 · Fuselage Main, StructureSDR ABXA010472Indicator · defectiveDURING GEAR DOWN EXTENTION INTO LAX, THE HYDRAULIC QUANTITY BEGAN TO RAPIDLY DECREASE. CREW DECLARED AN EMERGENCY INTO LAX. FOUND THE HYDRAULIC INDICATOR INTERMITTENTLY INOPERATIVE. REPLACED THE INDICATOR. BLED THE HYRDRAULIC SYSTEM AND CYCLED ALL FLIGHT CONTRSep 12, 2001 · N849AX · Doug DC861 · Hydraulic Quantity IndicatorSDR ABXA010471Tire · defectiveDURING DEPARTURE FROM ILN, UPON GEAR RETRACTION, WHEN THE NOSE GEAR ENTERED THE WELL, A VIBRATION WAS FELT IN THE THROTTLE QUADRANT AREA. CREW RECYCLED GEAR AND DID A TOWER FLYBY THEN CONTINUED ON TO LAX. FOUND THE LEFT NOSE TIRE DEFORMED AND OUT OF ROUND. REPSep 12, 2001 · N849AX · Doug DC861 · Landing Gear Retraction/Extension SystemSDR ABXA010458Switch · malfunctionedMAIN CARGO DOOR, NON-DOUGLAS, SYSTEM A-LIGHT CAME ON IN FLIGHT WITH PRESSURIZATION HOLDING. PER ABNORMALS, CREW DESCENDED TO 10,000 FEET. DEPRESSURIZED AIRCRAFT AND INSPECTED DOOR. LIGHT WENT OUT BELOW 6.0 PSID. DOOR INSPECTION, ALL LATCHED APPEARED LOCKEDAug 30, 2001 · N849AX · Doug DC861 · Door Warning SystemSDR ABXA010445Seal · leakingLOSS OF HYDRAULICS DURING CLIMB, HAPPENED ABOUT WHEN GEAR UPLATCH CHECK WAS ACCOMPLISHED. DURING HYDRAULIC PRESSURE CHECK (TERMINAL AREA) HYDRAULIC QUANTITY DECREASED. FOUND SLOT CONTROL VALVE SEALS LEAKING. REPACKED VALVE. SERVICED HYDRAULIC SYSTEM. SYSTAug 17, 2001 · N849AX · Doug DC861 · Leading Edge Slat Control SystemSDR ABXA010225Seal · damagedAN EXTREMELY LOUD NOISE WAS NOTED IN THE MAIN CARGO COMPARTMENT AROUND THE MAIN CARGO DOOR. THE CREW REPORTED HEARING A THUMP AND PRESSURIZATION INCREASED TO 1000 FPM RATE OF CLIMB. PRESSURIZATION COULD NOT BE CONTROLLED MANUALY AT FL21. THE CREW DONNED O2 May 13, 2001 · N849AX · Doug DC861 · Cargo/Baggage DoorsSDR ABXA010123Rod · brokenTHE RIGHT MAIN LANDING GEAR FLYING DOOR CONNECTING ROD WAS BROKEN. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN LANDING GEAR FLYING DOOR CONNECTING ROD, IAW DC-8 MM 32-12-01.Apr 7, 2001 · N849AX · Doug DC861 · Landing Gear Door Retract SectionSDR ABXA000333Door · out of adjON GEAR RETRACTION RED LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH RIGHT MAIN GEAR DOOR NOT LATCHED LIGHT ON. ACCOMPLISHED GEAR RECYCLE AND LOWERED FLAPS. LIGHTEXTINGUISHED. RERIGGED RIGHT MAIN LANDING GEAR DOOR FOLLOW-UP MECHANISM IAW DC8 MM. OPSCHECKJul 16, 2000 · N849AX · Doug DC861 · Landing Gear Door Retract SectionSDR ABXA000332Actuator · out of adjON GEAR RETRACTION, GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RIGHT MAIN DOOR INDICATED NOT LATCHED. RECYCLED GEAR, NO HELP. ADJUSTED RIGHT MAIN GEAR DOOR FOLLOW-UP MECHANISM IAW DC8 MM 32-31-05.Jul 14, 2000 · N849AX · Doug DC861 · Landing Gear Door ActuatorSDR ABXA000190Window · lack of lubeCAPTAIN''S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. INSPECTED AND LUBRICATEDWINDOW MECHANISM. OPS CHECKED GOOD.Apr 12, 2000 · N849AX · Doug DC861 · Flight Compartment WindowsSDR ABXA000018Window · stickingDURING PREFLIGHT, CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN INTERMITTENTLY. CLEANED AND LUBRICATED MECHANISM. OPS CHECKED GOOD.Jan 19, 2000 · N849AX · Doug DC861 · Flight Compartment WindowsSDR ABXA9900865Window · lack of lubeCAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED UPPER GUIDE PIN. OPS CHECKED GOOD.Dec 28, 1999 · N849AX · Doug DC861 · Flight Compartment WindowsSDR ABXA9900107Controller · defectiveDURING ENGINE START FOR REPOSITIONING FLIGHT, CREW REPORTED SMELL OF SMOKE IN COCKPIT. REPLACED LEFT AND CENTER WINDSHIELD TEMPERATURE CONTROLLERS. DETERMINED BAD FILTER WAS CAUSING ODOR.Feb 16, 1999 · N849AX · Doug DC861 · Windshield/Door Rain/Ice RemovalSDR ABXA9900010Switch · damagedAFTER CLIMB-OUT, AFTER TURNING LAST CTC ON, CARGO DOOR WARNING LIGHT ILLUMINATED. DUMPED 20,000 POUNDS OF FUEL AND RETURNED TO ILN. FOUND LOWER DOOR JAMB SWITCH ARM BENT. REPLACED SWITCH. PRESSURIZED AIRCRAFT. DOOR INDICATION LIGHT, OPS CHECKED GOOD.Jan 14, 1999 · N849AX · Doug DC861 · Door Warning SystemSDR ABXA9900003Retract Mech · lack of lubeON GEAR RETRACTION, GEAR HANDLE APPEARED TO BE HITTING STOP. RECYCLED HANDLE TWICE. GEAR CAME UP. LUBRICATED LANDING GEAR HANDLE LINKAGE. INSPECTED HANDLE AND CONTROL VALVE. NO DEFECTS NOTED. OPS CHECKED GOOD.Jan 4, 1999 · N849AX · Doug DC861 · Landing Gear Retraction/Extension SystemSDR ABXA9800889Window · lack of lubeCAPTAIN'S SLIDING WINDOW (EMERG EXIT) VERY DIFFICULT TO OPEN. CLEANED AND LUBRICATED MECHANISM, OPS CHECKED GOOD.Oct 9, 1998 · N849AX · Doug DC861 · Flight Compartment WindowsSDR ABXA9800714Fitting · crackedSTATION 980-1000 STRINGER 22R END FITTING WAS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-8 AND DWG 37532351.Jul 12, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous StructureSDR ABXA9800670Strap · crackedRIGHT WING LEADING EDGE AT STATION XFS 610.000, UPPER RIB TRAILING EDGE STRAP IS CRACKED. REPLACED STRAP IAW DWG 5655441 AND DC8 SRM 51-1-21A.Jun 27, 1998 · N849AX · Doug DC861F · Wing Miscellaneous StructureSDR ABXA9800712Angle · cracked680 BULKHEAD UPPER ATTACH FITTING TO FLOOR BOARD FRAME CRACKED AT RBL24. REPLACED FLOOR SUPPORT ANGLE IAW DWG 4645517 AND DC8 SRM 51-1-20D.Jun 26, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous StructureSDR ABXA9800669Web · corrosionHEAVY CORROSION ON TORQUE BOX WEB AT STATION 1210-1250. REPAIRED WEB IAW DWG 9754945, DC8 SRM 53-2-0 AND 51-1-21.Jun 24, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous StructureSDR ABXA9800717Rib · crackedLEFT WING LEADING EDGE LOWER RIB ARM CRACKED BY AFT FASTENER AT STATION XFS 816.250. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-21.Jun 23, 1998 · N849AX · Doug DC861F · Wing, Rib/BulkheadSDR ABXA9800716Angle · crackedRIGHT WING LEADING EDGE AT STATION XFS 766.250, THE INTERNAL DOUBLER ANGLE FORWARD OF ACCESS HOLE HAS A 5 CRACK. REPAIRED IAW DC8 SRM 51-1-8 AND 51-1-20D.Jun 23, 1998 · N849AX · Doug DC861F · Wing Miscellaneous StructureSDR ABXA9800703Rib · crackedRIGHT WING LEADING EDGE AT STATION XOLDI 6.225, UPPER LEADING EDGE RIB HAS A 4 CRACK. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-21.Jun 23, 1998 · N849AX · Doug DC861F · Wing, Rib/BulkheadSDR ABXA9800702Fitting · crackedFLOORBOARD ATTACH ANGLE CRACKED AT STATION 1140, RBL 55. REPAIRED IAW ABX REA NR D853-22888 AND DC8 SRM 51-3-0.Jun 23, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous StructureSDR ABXA9800706Fitting · crackedSPLICE FITTING CRACKED AT STATION 1300 - 1320 STRINGER 31L. REPLACED FITTING IAW DC8 SRM 51-1-20D.Jun 21, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous StructureSDR ABXA9800705Web · crackedLEFT WHEEL WELL AFT TORQUE BOX WEB CRACKED. REPAIRED IAW DC8 SRM 53-2-0, 51-1-8 AND 51-1-21.Jun 21, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous StructureSDR ABXA9800704Fitting · crackedLEFT LOWER FRAME TO CUSP FITTING CRACKED AT STATION 1070. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 9755584.Jun 21, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous Structure
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