N825AX, cancelled Apr 25, 2007

Service difficulty reports · 155

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 = 'N825AX' AND deregistration_id = 'N825AX-2007-04-25'
  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 ABXA060079Landing Gear · malfunctionedAFTER TAKEOFF AT ILN, UNABLE TO RAISE LANDING GEAR HANDLE. DID NOT USE FLIGHT HANDLE RELEASE, AIRCRAFT WAS IN FLIGHT MODE. CREW FLEW AIRCRAFT WITH ALL THREE GEAR DOWN, DID A FLY BY TO VERIFY NOSE GEAR WAS STRAIGHT DOWN. COMPLIED WITH NOSE LANDING GEAR REPACFeb 2, 2006 · N825AX · Doug DC863 · Landing Gear SystemSDR ABXA060041Stringer · crackedLEFT WING (AFT SIDE) STRINGER LONGERON 58 WS 428 - 463 END FITTING CRACKED. REMOVED DAMAGED STRINGER END FITTING TWO CRACKS, ONE 4.5" AND ONE 12.0". FABRICATED NEW FITTING IAW DAC DWG 5644972. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2. PERFORMED DJan 15, 2006 · N825AX · Doug DC863 · Wing, Longeron/StringerSDR ABXA060045Spar Cap · corrodedWING CENTER SECTION UPPER SURFACE HAD TWO AREAS OF CORROSION WITH PITTING BS 851, RIGHT BUTT LINE 12, BS 851, RIGHT BUTT LINE 17. CUT OUT DAMAGED AREA AND REPAIRED WITH NEW PART IAW DC8 SRM 53-2-5. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SJan 14, 2006 · N825AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA060043Fitting · corrodedBATHTUB FITTING HAD CORROSION AT LONGERON 34, ATTACH POINT BS 879. CORROSION FOUND OUT OF LIMITS OF DC8 SRM 53-2-0. REMOVED FITTING IAW DC8 SRM 51-1-20D. INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-20D, 51-3-1, AND 51-1-8.Jan 14, 2006 · N825AX · Doug DC863 · Fuselage Main, Attach FittingsSDR ABXA060044Fitting · corrodedBATHTUB FITTING HAD CORROSION AT LONGERON 24, ATTACH POINT BS 940. CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-20. INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-20D, 51-3-0, AND 51-1-8.Jan 13, 2006 · N825AX · Doug DC863 · Fuselage Main, Attach FittingsSDR ABXA060042Skin · corrodedDEFOLIATED SKIN ON BELLY OF PLANE JUST AFT OF SKIN DOUBLER AT APPROXIMATELY STA 1420, LONGERON 36. REPAIRED AREA IAW ABX REA D853-51398-MR.Jan 12, 2006 · N825AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA060046Strap · corrodedCORROSION ON ANGLE STRAP ON TOP OF MAIN LANDING GEAR WHEEL WELL BOX FORWARD OF FLOORBEAM STA 902, LEFT BUTT LINE 65. REMOVED CORROSION IAW DC8 SRM 51-1-8. DETERMINED TO BE OUT OF ACCEPTABLE LIMITS IAW DC8 SRM 53-2-0. REMOVED AND REPLACED WITH NEW FABRICATEDDec 23, 2005 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA050263Cabin Pressure · unknownDURING CLIMB AT FL310, CABIN RATE OF CLIMB WENT FROM 500 FPM TO 6,000 FPM. COULD NOT STOP THE CABIN FROM CLIMBING USING AUTO OR MANUAL LEVER. CABIN WENT TO 11,000 FT. DONNED OXYGEN AND STARTED DESCENT. AT ABOUT FL290, REGAINED CONTROL OF BOTH AUTO AND MANUNov 4, 2005 · N825AX · Doug DC863 · Cabin Pressure Control SystemSDR ABXA050179Transmitter · defectiveNR 3 ENGINE OIL PRESSURE PEGGED OFF SCALE HIGH. ENGINE WAS SECURED AND FLIGHT CONTINUED ON TO IAD. OIL PRESSURE REMAINED PEGGED OUT HIGH. PERFORMED ENGINE INSPECTION IAW P&W JT3D MM 72-00. OIL FILTER FOUND CLEAN. REMOVED AND REPLACED OIL PRESSURE TRANSMITJul 28, 2005 · N825AX · Doug DC863 · Engine Oil PressureSDR ABXA040351Outflow Valve · malfunctionedDURING DESCENT, CABIN PRESS WENT TO 2000 FT/MIN. RATE OF CLIMB UP TO 9500 CABIN ALT WITH NO CONTROL EITHER MANUALLY OR AUTOMATICALLY. RECOVERED AT FL 19000. COULD NOT DUPLICATE. CREW VERBAL, HEAVY RAINS LEAVING ILN. SUSPECT ICE BUILD-UP. INSPECTED OUTFLOOct 15, 2004 · N825AX · Doug DC863 · Pressure Regulator/Outflow ValveSDR ABXA040155Control Box · defectiveAFTER TAKEOFF, GEAR WARNING LIGHT REMAINED ON. LANDING GEAR AND DOOR INDICATOR PANEL SHOWED NOSE GEAR. RECYCLED, SAME RESULT. CONSULTED ABNORMAL AND PROCEEDED TO DESTINATION. MAINTENANCE AT ILN: DURING SELF TEST OF PROX SWITCH CONTROL BOX, NOSE GEAR UP LIMIT FApr 27, 2004 · N825AX · Doug DC863 · Landing Gear Position and WarningSDR ABXA040058Angle · gougedLEFT WING OUTBOARD FLAP STA 219 FOLD HINGE COVER WELL OUTBOARD LOWER SIDE GOUGED. REPAIRED AREA IAW REA D827-48510MR.Jan 30, 2004 · N825AX · Doug DC863 · Trailing Edge FlapsSDR ABXA040054Longeron · corrodedFORWARD ACCESSORY AT STA 25, LONGERON 31 LEFT WAS CORRODED. REPAIRED AREA IAW REA D853-48515MR.Jan 30, 2004 · N825AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA040057Spar · crackedRIGHT WING REAR SPAR XRS 139 JACKPAD TO REAR SPAR FITTING CRACKED. REPAIRED AREA IAW REA D857-48845MR.Jan 30, 2004 · N825AX · Doug DC863 · Wing SparSDR ABXA040056Finger Doubler · corrodedFORWARD CARGO LOWER LEFT SKIN FINGER DOUBLER CORRODED UNDERNEATH FROM STA 200 TO 220, LONGERON 35 LEFT TO 33 LEFT, BUTTLINE 7 TO BUTTLINE 20. REPAIRED AREA IAW REA D853-48505MR.Jan 30, 2004 · N825AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA040053Longeron · crackedRIGHT WHEEL WELL LONGERON 24 FITTING WAS CRACKED JUST UNDER BOTTLE BOLT. REMOVED AND REPLACED LONGERON 24 RIGHT IAW ABX REA D853-48504MR.Jan 30, 2004 · N825AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA040055Longeron · corrodedAFT ACCESSORY COMPARTMENT CORROSION AT FUSELAGE SKIN AND DOUBLER LONGERON 33 RIGHT, FS 1620 - 1628, ADJACENT TO OUTFLOW VALVE. REPAIRED AREA IAW REA D853-48508MR.Jan 30, 2004 · N825AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA030435Battery Pack · dischargedDURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHT BATTERY DEAD. REPLACED EMERGENCY BATTERY PACK. SYSTEM CHECKED GOOD IAW DC8 MM 33.Nov 7, 2003 · N825AX · Doug DC863 · Emergency LightingSDR ABXA030394Transmitter · defectiveNR 4 ENGINE OIL PRESSURE INDICATED + 100 PSI AT TOP OF CLIMB. SECURED ENGINE AT 0325Z, RETURNED TO 22 PSI AT 0345. REPLACED NR 4 OIL PRESSURE TRANSMITTER, NR 4 OIL PRESSURE RELIEF VALVE AND MAIN ENGINE OIL FILTER. RAN NR 4 ENGINE, OIL PRESSURE AT IDLE 41 PSOct 23, 2003 · N825AX · Doug DC863 · Engine Oil PressureSDR ABXA030096Longeron · corrodedDURING LINE OPERATIONS AT ILN, LONGERON 36 WAS FOUND TO HAVE INTERGRANULAR CORROSION IN THE LOWER FLANGE AT STA 1420. REPAIRED LONGERON IAW ABX REA D853-46872MR.Mar 3, 2003 · N825AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA030066Threshold · bentMAIN CABIN DOOR THRESHOLD LIP WAS RAISED PREVENTING DOOR FROM OPENING. REPAIRED RAISED LIP ON THRESHOLD OF MAIN CABIN DOOR AS REQUIRED IAW DC-8 MM.Feb 6, 2003 · N825AX · Doug DC863 · Fuselage Main, StructureSDR ABXA020347Control Arm · defectiveWITH GEAR HANDLE DOWN, GREEN LIGHTS NOT ON, RED LIGHTS NOT ON EITHER. ACCOMPLISHED ABNORMAL PROCEDURE, STILL NO LIGHTS. OTHER CHECKLIST ITEMS INDICATED ALL GEAR WAS DOWN AND LOCKED. FOUND GEAR WARNING INTERLOCK CIRCUIT BREAKER INTERMITTENT (D-3). REPLACED CIRCDec 6, 2002 · N825AX · Doug DC863 · Landing Gear Position and WarningSDR ABXA010802Longeron · crackedFORWARD CARGO, STATION 300 - 320, LONGERON 35 LEFT, ATTACH ANGLE CRACKED. REPAIRED AREA AND INSTALLED NEW SECTION OF LONGERON, NEW -Z- FITTINGS, SPLICES AND NEW WEB IAW DC-8 SRM 51-1-20D, 53-2-0, 51-1-8, 51-1-24 AND REA D853-43046MR.Mar 1, 2002 · N825AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010806Fitting · damagedDURING C-CHECK, THE FITTING (P/N 9755584-508) WAS DAMAGED. R&R IAW REA D853-43051-MR AND FAA FORM 8110-3.Feb 25, 2002 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010654Light · inoperativeON CLIMBOUT, UPPER CARGO SMOKE LIGHT CAME ON. NO SMOKE OR UNUSUAL SMELLS NOTED. NR 3 SMOKE DETECTOR APPEARED TO GIVE FALSE INDICATION. RELAMPED THE NR 3 UPPER CARGO SMOKE DETECTOR. OPS CHECKED GOOD IAW DC-8 MM 26-10-00.Dec 27, 2001 · N825AX · Doug DC863 · Smoke DetectionSDR ABXA010450Control Box · defectiveRED GEAR UNSAFE LIGHT ILLUMINATED. LANDING GEAR AND DOOR LATCHING SELECTOR INDICATED RIGHT MAIN DOOR UNLATCHED. FOLLOWED ABNORMAL PROCEDURE AND ALL INDICATIONS RETURNED TO NORMAL. REPLACED THE GEAR PROXIMITY CONTROL BOX IAW DC-8 MM 32-10-00. OPS CHECKED GOAug 20, 2001 · N825AX · Doug DC863 · Landing Gear Position and WarningSDR ABXA010420Proximity Switch · malfunctionedAFTER GEAR RETRACTION RECEIVED RED GEAR UNSAFE LIGHT ILLUMINATION WITH UNSAFE LIGHT ILLUMINATED WITH GEAR UP. RAN ABNORMAL PROCEDURES AND RECEIVED RIGHT MAIN LANDING GEAR DOOR NOT LATCHED LIGHT MOMENTARILY THEN RIGHT MAIN LANDING GEAR DOOR LIGHT WENT OUT ACCOAug 1, 2001 · N825AX · Doug DC863 · Landing Gear Position and WarningSDR ABXA010410Uplock · out of adjRED GEAR UNSAFE LIGHT CAME ON AT CRUISE AND THE RIGHT GEAR DOOR LANDING GEAR AND LIGHT WENT OUT. PERFORMED LANDING GEAR DOOR SWITCH TEST AND ADJ/TEST MAIN GEAR DOOR. CLOSED PROXIMITY SWITCH. BOTH CHECKED GOOD. ADJUSTED DOOR UPLATCH TURNBUCKLES IAW DC-8 MM Jul 25, 2001 · N825AX · Doug DC863 · Landing Gear Retraction/Extension SystemSDR ABXA010065Valve · defectiveTHE LEFT MAIN LANDING GEAR WHEEL BRAKES WOULD NOT OPERATE. MAINTENANCE INSPECTED AND FOUND THE BRAKE HYDRAULIC POWER VALVE ASSY TO HAVE A BROKEN FORK. THE POWER VALVE WAS REPLACED IAW DC-8 MM 32-42-02.Feb 27, 2001 · N825AX · Doug DC863 · Master Cylinder/Brake ValveSDR ABXA010004Window · stuckFIRST OFFICERS CLEARVIEW WINDOW DID NOT OPEN ALL THE WAY. MAINTENANCE INSPECTED AND REPLACED LOWER AFT HOOK SPRING AND ADJUSTED IAW DC-8 MM 56-10-03. PRESSURIZATION AND WINDOW OPERATION CHECKED GOOD.Jan 9, 2001 · N825AX · Doug DC863 · Flight Compartment WindowsSDR ABXA010002Window · stuckFIRST OFFICERS CLEARVIEW WINDOW WOULD NOT OPEN COMPLETELY. MAINTENANCE INSPECTED AND OPERATED THE FIRST OFFICERS CLEARVIEW WINDOW SEVERAL TIMES. THE WINDOW OPERATED NORMALLY IAW DC-8 MM 56-10.Jan 9, 2001 · N825AX · Doug DC863 · Flight Compartment WindowsSDR ABXA000360Window · out of adjFIRST OFFICER''S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED SERRATED HOOK STOP ON AFT OF FIRST OFFICER''S CLEARVIEW WINDOW. OPS CHECKED GOOD PER DC8 MM.Aug 3, 2000 · N825AX · Doug DC863 · Flight Compartment WindowsSDR ABXA000158Rack · malfunctionedEMERGENCY LIGHTS BLINKED ON/OFF EVERY 2.5 MINUTES. REPLACED EMERGENCY LIGHT RACK ASSEMBLY IAW DC8 MM, OPS CHECKED GOOD.Mar 21, 2000 · N825AX · Doug DC863 · Emergency LightingSDR ABXA000155Battery Pack · inoperativeEMERGENCY BATTERY CHARGING CIRCUIT BREAKER WOULD NOT RESET. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC9 MM, OPS CHECKED GOOD.Mar 20, 2000 · N825AX · Doug DC863 · Emergency LightingSDR ABXA9900079Spring · out of adjustAFTER GEAR RETRACTION, RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR TWICE, UNSAFE LIGHT REMAINED. USED ABNORMAL PROCEDURES TO DETERMINE RIGHT GEAR DOOR UNSAFE AND SECURED DOOR TO NORMAL. ADJUSTED CABLE TENSION AND REPLACED OVERCENTER SPRING.Feb 5, 1999 · N825AX · Doug DC863 · Landing Gear Door Retract SectionSDR ABXA9900126Fitting · corrodedBATHTUB FITTING CORRODED AT STATION 1220, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-20D AND ABX REA D853-24927-1MR.Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900124Fitting · corrodedCORRODED BATHTUB FITTING AT LONGERON 28 LEFT, STATION 1260. REPLACED FITTING IAW DWG 3755842, ABX REA D853-24928 AND DC8 SRM 53-2-0.Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900089Fitting · corrodedBATHTUB FITTING AT STATION 1260, LONGERON 30 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-21D, DWG 3755842 AND ABX REA D853-249271.Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900088Fitting · corrodedEXFOLIATED BATHTUB FITTING AT LONGERON 29 LEFT, STATION 1220. REPLACED FITTING IAW ABX REA D853-24927 AND DC8 SRM 51-1-21D.Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900087Fitting · corrodedCORRODED BATHTUB FITTING AT STATION 1200, LONGERON 29 LEFT. REPLACED FITTING IAW ABX REA D853-249279 AND DWG 93755842.Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900086Fitting · corrodedEXFOLIATED BATHTUB FITTING AT STATION 1260, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 53-2-0 AND ABX REA D853-24921.Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900085Fitting · corrodedEXFOLIATED BATHTUB FITTING AT STATION 1240, LONGERON 31 LEFT. REPLACED FITTING IAW DC8 SRM 53-2-0 AND ABX REA D853-24927MR.Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900083Fitting · corrodedCORRODED BATHTUB FITTING AT LONGERON 28 LEFT, STATION 1260. REPLACED FITTING IAW DWG 3755842, ABX REA D85324928MR AND DC8 SRM 53-2-0.Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900082Fitting · corrodedBATH TUB FITTING CORRODED AT STATION 1220, LONGERON 31 LEFT. REPLACED FITTING IAW DWG 3755844, ABX REA D853-219271MR AND DC8 SRM 51-1-20D.Jan 27, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900125Fitting · crackedLEFT CUSP LOWER ATTACH FITTING CRACKED AT STATION 1080. REPAIRED IAW DC8 SRM 51-1-20D.Jan 26, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900084Fitting · crackedLEFT CUSP LOWER FITTING CRACKED AT STATION 1080. REPAIRED IAW DC8 SRM 51-1-20D.Jan 26, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900128Bulkhead · crackedCRACKED INTERCOSTAL ON AFT BULKHEAD, STATION 1540 RIGHT. REPAIRED IAW DC8 SRM AND DWG 5646608.Jan 23, 1999 · N825AX · Doug DC863 · Fuselage Main, BulkheadSDR ABXA9900118Gusset · corrodedGUSSET PLATE HAD EXFOLIATED CORROSION AT STATION 1240 LONGERON 24 LEFT. REPLACED GUSSETT IAW DWG 9755849 AND DC8 SRM 51-01-20D AND ABX RE AND 853-24930.Jan 23, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900117Gusset · corrodedGUSSET HAD EXFOLIATED CORROSION AT STATION 1220 LONGERON 24 LEFT. REPLACED GUSSET IAW DC8 SRM 51-01-20D AND ABX REA D853-24930.Jan 23, 1999 · N825AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA9900116Channel · crackedLEFT MAIN LANDING GEAR SUPPORT STRUCTURE CRACKED AT AFT SIDE OF LANDING GEAR CUT-OUT. REPLACED CHANNEL IAW DWG 5611020 AND DC8 SRM 51-01-21.Jan 23, 1999 · N825AX · Doug DC863 · Wing Miscellaneous Structure
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