N14075, cancelled May 21, 2013

Service difficulty reports · 108

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 = 'N14075' AND deregistration_id = 'N14075-2013-05-21'
  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 WRLA2006044Support Channel · corrodedITEM: DURING "C" CHECK IN GSO FOUND LAV SUPPORT CHANNEL CORRODED ON UPPER SURFACE STA 859 LBL70. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED & REPLACED SUPPORT CHANNEL IAW DC10 SRM.Jul 23, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006027Fitting · corrodedDURING C3 CK, FOUND CORROSION ON LT WHEEL WELL AT STA 1509 INBOARD FITTING. REMOVE AND REPLACE FITTING.Jul 21, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006023Tee Fitting · corrodedDURING C3 CK, FOUND CORROSION ON TEE CHORD AT L43 LT WHEEL WELL, STA 1521. REMOVE CORROSION AND REEVALUATE, AND GENERATE RFTS FOR REPAIR. FASTENERS REQ'D REMOVAL.Jul 20, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006069Floorbeam · corrodedDURING C-CK IN GSO FOUND FLOORBEAM CORRODED IN MAIN CABIN AT STA 495 AT APPROX RBL 56. REPLACED FLOOR SUPPORT IAW CAB DWG ACA 7364 AND DC10 SRM 51-31-01 VOL II AND DC10 SRM 51-33-01 VOL II.Jul 18, 2006 · N14075 · Doug DC1030 · Fuselage Main, Floor BeamSDR WRLA2006068Floorbeam · corrodedDURING C-CK IN GSO FOUND FLOORBOARD ATTACH ANGLE CORRODED IN MAIN CABIN AT STA 395 BELOW THE COCKPIT DOOR. FLOORBOARD ATTACH ANGLE REMOVED AND REPLACED WITH NEW P/N BAC1503-4162 EXTRUSION 7075-T6105111 (PO 541368.1) IAW DC 10 SRM 51-31-01 VOL II.Jul 18, 2006 · N14075 · Doug DC1030 · Fuselage Main, Floor BeamSDR WRLA2006067Floor Support · corrodedDURING C-CHECK IN GSO FOUND MAIN CABIN AT APPROX STA 430, AT RBL 10, FLOOR SUPPORT CORRODED. RECEIVED FLOOR SUPPORT P/N ABA8225-503 PO 541338, REMOVED OLD SUPPORT. LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-31-01 VOL II. INSTALLED FLOOR SUPPORT AND DOOR JAMJul 18, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006070Floor Support · corrodedDURING C-CK IN GSO FOUND FLOOR SUPPORT CORRODED IN MAIN CABIN B/N STA 879-755 AT APPROX LBL 46. RECEIVED NEW PART P/N ADA 7327-1 PO 540808-12; INSTALLED NEW FLOOR SUPPORT AIW DC10 SRM 51-31-01 VOL II.Jul 16, 2006 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WRLA2006066Seat Track · corrodedDURING C-CK IN GSO FOUND RIGHT O/B SEAT TRACK AND LAV MOUNT CORRODED AT STA 1909-1913. BLENDED AREA IN ELECTRIC SEAT TRACK. FABRICATED STRAP.Jul 14, 2006 · N14075 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2006065Seat Track · corrodedDURING C-CK IN GSO AT STA 1960, FOUND RT O/B TRACK AND LAV MOUNT CORRODED. BLEND OUT CORROSION IN SEAT TRACK.Jul 14, 2006 · N14075 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2006024Stiffener · corrodedDURING C3 CK, FOUND CORROSION IN LT MAIN GEAR WELL AFT PRESSURE BULKHEAD, STA 1521, ON THE VERTICAL STIFFENER (LWR AFT AREA). REMOVED CORROSION AND REPLACED STIFFENER.Jul 9, 2006 · N14075 · Doug DC1030 · Fuselage Main, BulkheadSDR WRLA2006020Bulkhead · corrodedDURING C3 CHECK, FOUND CORROSION IN LT MAIN GEAR WHEEL WELL AFT PRESSURE BULKHEAD, STA 1521, VERTICAL STIFFENER LOWER SUPPORT WEB AND ASSOCIATED ANGLES. REMOVED CORROSION AND REPLACED STIFFENER, WEB, AND ANGLES PER SRM PROCEDURES.Jul 9, 2006 · N14075 · Doug DC1030 · Fuselage Main, BulkheadSDR WRLA2006009Fire Warning · false activationAPU AUTOSHUTDOWN WITH A FIRE WARNING ALERT. FIRE AGENT CYLINDER 1 DISCHARGED. REPLACED NR 1 REAR FIRE BOTTLE PER MM CHAP 26. INSPECTED APU AREA FOR LEAK AND POSSIBLE FIRE DAMAGE, NONE FOUND. OK FOR CONTINUED SERVICE.Mar 8, 2006 · N14075 · Doug DC1030 · Fire DetectionSDR WRLA2005084Fuel Sys · leakingDIVERSION DUE TO 1+20HR INTO FLIGHT NR 3 FUEL FLOW STARTED TO INDICATE 15,000 LBS PER HOUR ON THE NEEDLE, 29,320 ON DIGITAL. FUEL USED ON NR 3 ROSE TO OVER 5,000 LBS MORE THAN 1 AND 2. ENGINE SHUTDOWN PER PROCEDURES. FUEL PRESSURE ON NR 3 STILL INDICATES 80Apr 7, 2005 · N14075 · Doug DC1030 · Engine Fuel and ControlSDR WLDA200496Lever · stuckON APPROACH, LANDING GEAR HANDLE WOULD NOT RELEASE. COMPLIED WITH ALTERNATE GEAR EXTENSION PROCEDURE AND COMPLETED NORMAL LANDING. CLEANED AND LUBED CABLES, CLEANED CANNON PLUG ON HOLDING COIL AND CHECKED FOR BINDING ON GROUND. NO BINDING OR BROKEN CABLES, Oct 9, 2004 · N14075 · Doug DC1030 · Landing Gear SelectorSDR WLDA200493Floor Panel · corrodedDURING "B4" CHECK IN BYH, FOUND FLOOR PANEL FWD OF LEFT FWD STORE CLOSET HAD EXFOLIATION CORROSION. REMOVED AND REPLACED FLOOR PANEL FWD OF LEFT STORE CLOSET IAW DC-10 MM 53-22-01.Sep 5, 2004 · N14075 · Doug DC1030 · Fuselage Floor PanelSDR WLDA200492Floor Support · corrodedDURING "B4" CHECK IN BYH, FOUND LBL30 FS 1907 TO 2007 FLOOR SUPPORT CORRODED. REMOVED SURFACE CORROSION OF APPROXIMATELY .002 OF MATERIAL LBL30 FS 1907 TO 2007 FLOOR SUPPORT. TREATED BARE AREAS WITH ALODINE, CLEANED THEN PRIMED AREA IAW DC-10 SRM 51-21-01.Sep 5, 2004 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WLDA200491Floor Support · corrodedDURING "B4" CHECK IN BYH, FOUND RBL30 F/S 1907 TO 2007 FLOOR SUPPORT CORRODED. REMOVED SURFACE CORROSION OF APPROXIMATELY .002 OF MATERIAL RBL30 FS 1907 TO 2007 FLOOR SUPPORT. TREATED BARE AREAS WITH ALODINE, CLEANED THEN PRIMED AREA IAW DC-10 SRM 51-21-01.Sep 5, 2004 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR WLDA200459Cadc · inoperativeITEM: RCH725/13 NGU/NAP REJECTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON CAPT'S INDICATOR, F/O'S INDICATED OK. RTO AT 105KTS. REMOVED AND REPLACED CADC, PERFORMED PITOT STATIC CHECK, FOUND ALL NORMAL. REMOVED AND REPLACED PITOT STATIC TUBE PRECAUTIONARY. PREAug 13, 2004 · N14075 · Doug DC1030 · Airspeed/Mach IndicatorSDR WRLA200423Slide · failedDURING MAINTENANCE CHECK, GYR R-1 DOOR SLIDE SCHEDULE FOR TEST DEPLOYMENT, THE TEST ACCOMPLSHED PER DC-10 MM, DURING THE TEST CHECK THE SLIDE INFLATED WHEN THE DOOR WAS APPROXIMATELY 3/4 OPEN AND DEPLOYED INSIDE THE AIRCRAFT (THE SLIDE NEVER LEFT THE DOOR WAYMay 26, 2004 · N14075 · Doug DC1030 · Escape SlideSDR WRLA200422Control Unit · failedAIRCRAFT N14075 FLIGHT 8012 FROM LIRN TO KNGU, DURING THE LANDING AT THE KNGU THE RIGHT OUTBOARD ANTI-SKID FAIL LIGHT ILLUMINATED IN FLIGHT. DUE TO THE SHORT RUNWAY AT KNGU THE CREW DECIDED TO LAND AT KNTU. AT THE KNTU MAINTENANCE REMOVED & REPLACED THE ANTIMay 11, 2004 · N14075 · Doug DC1030 · Brake Anti-Skid SectionSDR WRLA200421Indicator · failedTHE AIRCRAFT NR 1 VERTICAL GYRO WAS INOPERATIVE, ON CLIMBOUT OF BAHRAIN N2 (FIRST OFFICER) FAILED, THE CREW UNABLE TO RESET OR RESTORE IT AND DECIDED TO RETURN BACK TO BAHRAIN. AT BAHRAIN MAINTENANCE REPLACED THE F/O ATTITUDE DIRECTOR INDICATOR PER MM 34-23-0May 7, 2004 · N14075 · Doug DC1030 · Attitude and Direction Data SystemSDR WRLA200414Cowl Door · missingAIRCRAFT N14075 DEPT. FROM LIRN TO KNGU AT 2100Z WHILE AIRCRAFT CRUISING AFTER 5 HOURS AND 40 MIN.APPROX. 0240Z (ACCORDING TO THE CAPTAIN REPORT) THE ACFT. SHUDDERED AND BOUNCED FOR APPROX. 1/2 SECOND, THEN RETURNED TO STABLE FLIGHT, ACFT. CONTINUE TO KNGU ANApr 11, 2004 · N14075 · Doug DC1030 · Engine Cowling SystemSDR WRLA200328Light · inoperativeEMERGENCY ISLE LIGHT INOPERATIVE AT 21J. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED GOODNov 18, 2003 · N14075 · Doug DC1030 · Emergency LightingSDR WRLA200314Heat Exchanger · leakingNR 2 PNEUMATIC MANIFOLD FAILURE LIGHT ILLUMINATED WITH TWO PACKS OFF AND TWO PNEUMATIC SYSTEMS OFF. AGAIN EXECUTE VOL II 01-10-09 EMERGENCY PROCEDURE. FOUND EXCESSIVE HOT AIR LEAKAGE FROM NR 1 AND NR 2 HEAT EXCHANGERS TO BOTH ACM'S CONNECT SLEEVES AND FROM BJun 21, 2003 · N14075 · Doug DC1030 · Pneumatic Distribution SystemSDR WRLA200225Control Cable · brokenLEFT RUDDER CABLE BROKE AT APPROXIMATE STATION 1920. REPLACED RUDDER LEFT CONTROL CABLE SEGMENT 1D AND PERFORMED RIGHT CHECK IAW DC-10 MM 27-20-00. RIG CHECKED ACCOMPLISHED. FOUND CHAFED WIRE HARNESS FOR L4 FLIGHT ATTENDANT CONTROL PANEL BELOW FLOOR AT APPROct 11, 2002 · N14075 · Doug DC1030 · Rudder Control SystemSDR WRLA200221Terminal · burnedDURING PREFLIGHT SERVICING, AC BUS NR 1 CIRCUIT BREAKERS POPPED. FURTHER NOTED TERMINAL STRIP BURNED IN CENTER ACCESSORY COMPARTMENT. ACCOMPLISHED ALL NECESSARY REPAIRS. REPLACED THE FOLLOWING COMPONENTS REPAIRED TERMINAL STRIP S3521, LUGS ON FEEDER TO THE Aug 29, 2002 · N14075 · Doug DC1030 · Electrical Power System WiringSDR WRLA200210Control Valve · failedAFTER TAKEOFF OB FLAP FAILED TO RETRACT-CONFIRMED BY FLAP INDICATIONS TAPES AND PHYSICAL INSP. COMMENCING FUEL DUMP TO RETURN, FLAPS RETRACTED ON THERE OWN AND OPERATED NORMALLY FOR LANDING. DETERMINED LT OB FLAP AND RT OB FLAP ONE DID REMAIN EXTENDED AFTER Apr 19, 2002 · N14075 · Doug DC1030 · Trailing Edge Flap ActuatorSDR WRLA200207Gps · failedAIRCRAFT RETURNED TO FRANKFORT DUE TO GPS NAVIGATIONAL ERROR. RESET GPS (ALL THREE UNITS) BY SWAPPING NAVIGATIONAL DATA, TO EXPIRED DATA BASE AND BACK TO ACTUAL NAVIGATIONAL DATA BASE. ALL FUNCTIONS BACK TO NORMAL. DATA BASE RELOADED. (M)Mar 18, 2002 · N14075 · Doug DC1030 · Global Positioning SystemSDR WRLA200106Slide · deployedDEPLOYED L1 SLIDE PER WORLD AIRWAYS WORK CARD NON ROUTINE TASK CARD AND DC-10 AIRCRAFT MAINTENANCE MANUAL. SLIDE FAILED TO FULLY DEPLOY DUE TO 2 EACH RETENTION CABLES BEING HUNG UP IN THEIR RETAINERS, ALSO DUE TO THE FAILURE TO FULLY DEPLOY, THE PRESSURE RELIMar 19, 2001 · N14075 · Doug DC1030 · Escape SlideSDR CALA0001580Rib · crackedINSPECTION FOUND A 6 INCH CRACK IN NR 2 PYLON SAILBOAT FAIRING LOWER RIB. REPAIR WAS COMPLETED IAW ECRA 5412-01011, SRM 51-31-01, AND DOUGLAS DRAWING AVB7306.Oct 14, 2000 · N14075 · Doug DC1030 · Nacelle/Pylon, Longeron/StringerSDR CALA0001579Access Panel · damagedINSPECTION FOUND LT WING FUEL TANK ACCESS PANELS 534BT, 534AT, AND 539CB DAMAGED. THE PANELS WERE REPLACED IAW MM 57-31-00.Oct 14, 2000 · N14075 · Doug DC1030 · Wing, Plate/SkinSDR CALA0001578Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WING O/B FLAP AFT HINGE UPPER BRACKET. A NEW BRACKET WAS INSTALLED IAW SRM 51-31-01.Oct 14, 2000 · N14075 · Doug DC1030 · Trailing Edge FlapsSDR CALA9901462Bulkhead Tee · corrodedINSPECTION FOUND ANGLE TEE ATTACHED TO PRESSURE BULKHEAD AT STA 2007, LBL 5 CORRODED. THE ANGLE TEE WAS REPAIRED IAW SRM 53-40-00, FIGURE 16.Nov 1, 1999 · N14075 · Doug DC1030 · Fuselage Main, BulkheadSDR CALA9901451Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON PRE-COOLER CUTOUT AT RT SIDE. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH A REPAIR ANGLE IAW ECRA 5450-01283.Nov 1, 1999 · N14075 · Doug DC1030 · Nacelle/Pylon, Plate/SkinSDR CALA9901450Tip · bentINSPECTION FOUND THE LEFT AND RIGHT I/B ELEVATOR T/E TIPS BENT. THE BENT AREAS WERE TRIMMED OUT AND NEW EDGE PORTIONS WERE INSTALLED IAW SRM 55-30-00, FIGURE 2 51-35-02, AND 51-31-01.Nov 1, 1999 · N14075 · Doug DC1030 · Elevator StructureSDR CALA9900197Controller · inopTHE AIRFLOW FROM PACKS WERE NOT EFFICIENT DURING FLIGHT. THE NR 1 PACK WAS PLACED IN MANUAL AND FLOW WAS ZERO. UPON INCREASING FLOW ON NR 1 PACK, THE CABIN RATE INCREASED TO 1,000 FEET IN STANDBY AND SMOKE ENTERED THE COCKPIT. THE NR 1 PACK WAS PUT TO FULL Feb 27, 1999 · N14075 · Doug DC1030 · Cabin Temperature ControllerSDR CALA9802085Battery Pack · dischargedTHE EMERGENCY LIGHTS WOULD NOT TEST DURING PREDEPARTURE CHECK. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY PACK AND CHARGER AND OPERATION CHECKED GOOD.Nov 20, 1998 · N14075 · Doug DC1030 · Emergency LightingSDR CALA9801986Charger · inoperativeTHE EMERGENCY LIGHTS WOULD NOT TEST ON PREDEPARTURE CHECK. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY PACK AND CHARGER AND OPERATIONAL CHECKS WERE GOOD.Oct 27, 1998 · N14075 · Doug DC1030 · Emergency LightingSDR CALA9801805Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING FIXED LEADING EDGE RIB BETWEEN XFS 1042 AND XFS 1192. THE RIB WAS REMOVED. A NEW PART WAS INSTALLED IAW SRM 57-21-00 FIGURE 8, 51-21-01 AND 51-31-01.Sep 17, 1998 · N14075 · Doug DC1030 · Wing, Rib/BulkheadSDR CALA9801804Angle · crackedINSPECTION FOUND A 1.6 INCH CRACK ON RT AND LT WING INBOARD ISLAND LOWER AFT INBOARD SPLICE ANGLE OF RIB. THE SPLICE ANGLE WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 57-22-01, FIGURE 2, 51-21-01, AND 51-33-01.Sep 17, 1998 · N14075 · Doug DC1030 · Wing Miscellaneous StructureSDR CALA9801803Frame · corrodedINSPECTION FOUND CORROSION ON LOWER FLANGE OF FRAMES IN CENTER CARGO COMPARTMENT AT STA 1721 BETWEEN STRINGER 50L AND 50R AND AT STA 1780 BETWEEN STRINGER 50L AND 50R. THE CORRODED OUTER CAPS OF FRAMES WERE TRIMMED OUT. THE AREAS WERE REINFORCED WITH OUTER CSep 16, 1998 · N14075 · Doug DC1030 · Fuselage Main, FrameSDR CALA9801764Skin · corrodedINSPECTION FOUND CENTER CARGO COMPARTMENT INTERIOR SKIN SWELLING AT STA 1520 TO 1560 BETWEEN STRINGER 45R AND 46R. THE SKIN WAS REPAIRED IAW ENGINEERING ORDER MF-MAN-D10-53-86829.Sep 15, 1998 · N14075 · Doug DC1030 · Fuselage Main, Plate/SkinSDR CALA9801763Cap · crackedINSPECTION FOUND A 6 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE INBOARD SIDE CAP AT L3. THE CAP WAS REMOVED AND A NEW CAP WAS INSTALLED IAW SRM 51-33-01 AND 55-12-01.Sep 15, 1998 · N14075 · Doug DC1030 · Horizontal Stabilizer StructureSDR CALA9801762Cap · crackedINSPECTION FOUND AN 11 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE LOWER OUTBOARD CAP AT L4. THE CAP WAS REMOVED AND A NEW CAP WAS INSTALLED IAW SRM 51-21-01, 51-31-01, AND 55-12-01, FIGURE 3.Sep 15, 1998 · N14075 · Doug DC1030 · Horizontal Stabilizer StructureSDR CALA9801638Support · corrodedINSPECTION FOUND GALLEY FLOOR SUPPORT CORRODED AT STA 1910, LBL 25. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-31-01.Sep 8, 1998 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9801637Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 1920 AND 2007, RBL 55. THE FLOOR SUPPORT WAS REMOVED. A NEW PART WAS INSTALLED IAW SRM 51-31-01.Sep 8, 1998 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9801635Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1887 BETWEEN LBL 35 & 45 AND BETWEEN LBL 45 & 90. THE FLOOR SUPPORTS WERE REMOVED AND NEW PARTS WERE INSTALLED IAW SRM 51-31-01.Sep 5, 1998 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9801634Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1887 BETWEEN RBL 0 - RBL 25, RBL 25 - 35, RBL 35 - 60, AND RBL 60 - 90. THE FLOOR SUPPORTS WERE REMOVED AND NEW PARTS WERE INSTALLED IAW SRM 51-31-01.Sep 5, 1998 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9801633Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 460, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-31-01.Sep 5, 1998 · N14075 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9801632Support · corrodedINSPECTION FOUND CORROSION ON FLOOR SUPPORTS AT STA 1900, LBL 6 AND RBL 6. THE FLOOR SUPPORTS WERE REMOVED AND NEW PARTS WERE INSTALLED IAW SRM 51-31-01.Sep 5, 1998 · N14075 · Doug DC1030 · Fuselage Miscellaneous Structure
Back to N14075, cancelled May 21, 2013