N14890, cancelled Jul 14, 2003

Service difficulty reports · 45

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 = 'N14890' AND deregistration_id = 'N14890-2003-07-14'
  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 CALA0100468Megaphone · inoperativeTHE AFT CABIN MEGAPHONE WAS FOUND INOPERATIVE DURING TEST. THE AFT CABIN MEGAPHONE WAS REMOVED AND REPLACED IAW MM 25-60-00.May 17, 2001 · N14890 · Doug DC982 · Emergency EquipmentSDR CALA0000181Cable · out of rigTHE FORCE REQUIRED TO DROP TAILCONE USING EXTERIOR AND INTERIOR RELEASE HANDLES EXCEEDED 35 POUNDS. THE TAILCONE CABLES WERE RIGGED AND DROP CHECK WAS GOOD IAW MM 53-53-00.Feb 22, 2000 · N14890 · Doug DC982 · Aerodynamic FairingsSDR CALA0000177Beltframe · crackedINSPECTION FOUND A 2 INCH CRACK IN BELTFRAME AT STA 1380 BETWEEN LONGERONS 4L AND 5L. A DOUBLER WAS INSTALLED IAW SRM 51-30-02.Feb 17, 2000 · N14890 · Doug DC982 · Fuselage Main, FrameSDR CALA0000176Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 216 BETWEEN LONGERON 14R AND 15R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.Feb 17, 2000 · N14890 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000175Fitting · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN DOOR LOWER AFT STOP AREA INTERNAL FITTING. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-0.Feb 17, 2000 · N14890 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000173Door Jamb · crackedINSPECTION FOUND TWO 1.5 INCH CRACKS IN MAIN CABIN DOOR JAMB BOX GUSSET AT STA 207, LONGERONS 11L AND 15L. REPAIRS WERE INSTALLED AT EACH LOCATION IAW ECRA 5310-03985 AND ECRA 5310-03986.Feb 17, 2000 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000161Beltframe · corrodedINSPECTION FOUND FORWARD FACE OF BELTFRAME IN AFT BAG BIN CORRODED AT STA 1322, LONGERON 23L TO 29R. THE BELTFRAME WAS REPLACED AND A SPLICE REPAIR WAS INSTALLED IAW SRM 55-03, FIGURE 2A, 51-10-3, 51-30-2, 51-30-5.Feb 17, 2000 · N14890 · Doug DC982 · Fuselage Main, FrameSDR CALA0000159Floorbeam · wornINSPECTION FOUND CABIN FLOORBEAM LOWER FLANGE WORN AT STA 1193 IN AFT CARGO COMPARTMENT. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 86.Feb 16, 2000 · N14890 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0000157Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT STAIR DOOR ANGLE AT UPPER HINGE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.Feb 14, 2000 · N14890 · Doug DC982 · Entrance StairsSDR CALA0000156Cargo Track · crackedINSPECTION FOUND A 3 INCH CRACK IN TIE DOWN RAIL IN AFT BAG BIN AT STA 1271, LT SIDE. THE TIE DOWN RAIL WAS REMOVED AND A NEW TIE DOWN RAIL WAS INSTALLED IAW SRM 51-30-01.Feb 14, 2000 · N14890 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000155Cargo Track · corrodedINSPECTION FOUND RIGHT TIE DOWN RAIL TRACK CORRODED IN MID CARGO COMPARTMENT AT STA 693 TO AFT BULKHEAD. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 51-30-2.Feb 14, 2000 · N14890 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000154Cargo Track · corrodedINSPECTION FOUND LT TIE DOWN RAIL IN AFT CARGO COMPARTMENT CORRODED. THE TIE DOWN RAIL WAS REPLACED IAW SRM 51-10-3 AND 51-30-0.Feb 14, 2000 · N14890 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000150Intercostal · corrodedINSPECTION FOUND UPPER LEFT OF INTERCOSTAL CORRODED UNDER LEFT TIE DOWN RAIL AT STA 1309-1322, L28L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-20-02.Feb 12, 2000 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000149Intercostal · crackedINSPECTION FOUND MAIN CABIN DOOR INTERCOSTAL CRACKED BETWEEN NR 4 AND NR 5 BEAMS AFT OF INSIDE DOOR HANDLE. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2.Feb 11, 2000 · N14890 · Doug DC982 · Passenger/Crew DoorsSDR CALA0000144Seat Track · corrodedINSPECTION FOUND RT I/B SEAT TRACK CORRODED AT STA 200-280. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-3.Feb 10, 2000 · N14890 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900109Support · brokenTHE LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION BOUND FOR EWR. THE GEAR WAS CYCLED TWICE, BUT THE LIGHT WOULD NOT EXTINGUISH. THE FLIGHT WAS CONTINUED TO EWR WHERE IT LANDED WITHOUT PROBLEM. MAINTENANCE FOUND THE LT MAIN GEAR DOOR TARFeb 5, 1999 · N14890 · Doug DC982 · Landing Gear Position and WarningSDR CALA9800445Angle · crackedINSPECTION FOUND A .375 INCH CRACK IN VERTICAL STABILIZER FORWARD RIGHT SPAR SUPPORT ANGLE AT APPROXIMATELY 37.5 INCHES AFT OF STA 1089.5 IN TAIL COMPARTMENT ABOVE CATWALK. THE ANGLE WAS REPAIRED IAW SRM 55-02, FIGURE 26.Mar 14, 1998 · N14890 · Doug DC982 · Vertical StabilizerSDR CALA9800224Beltframe · crackedINSPECTION FOUND A 2 CRACK IN BELTFRAME AT LONGERON 2R AND A 2 CRACK IN BELTFRAME AT LONGERON 2L, STA 1418. A DOUBLER WAS INSTALLED TO ENCOMPASS BOTH CRACKS IAW SRM 53-05, FIGURE 32 AND ECRA 5311-01039.Feb 12, 1998 · N14890 · Doug DC982 · Fuselage Main, FrameSDR CALA9800215Cables · out of adjustTHE TAILCONE EXTERIOR RELEASE HANDLE PULLED AT 15 POUNDS. THE TAILCONE WAS RIGGED IAW WORK CARD 08-5350-1-0008.Feb 11, 1998 · N14890 · Doug DC982 · Aerodynamic FairingsSDR CALA9800213Angle · crackedINSPECTION FOUND VERTICAL FIN INNER ATTACH ANGLE ON RT AND LT SIDES CRACKED. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-5.Feb 10, 1998 · N14890 · Doug DC982 · Vertical StabilizerSDR CALA9800212Longeron · crackedINSPECTION FOUND LONGERON 2L CRACKED AT STA 1418. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 18.Feb 10, 1998 · N14890 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA9800205Splice · corrodedINSPECTION FOUND CORROSION ON TIEDOWN RAIL SPLICE AT STA 1220, LONGERON 28L, IN AFT CARGO COMPARTMENT. THE SPLICE WAS REMOVED AND A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-05-4.Feb 10, 1998 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9800204Angle · corrodedINSPECTION FOUND CORROSION IN LOWER FORWARD CORNER OF AFT CARGO DOOR CUTOUT AT STA 1155. A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.Feb 10, 1998 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9800203Fitting · crackedINSPECTION FOUND A 1.5 INCH CRACK IN AFT CABIN DOOR BEAM END FITTING AT LEFT CENTER STOP. A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.Feb 10, 1998 · N14890 · Doug DC982 · Passenger/Crew DoorsSDR CALA9800188Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1155, LONGERON 30 IN AFT CARGO COMPARTMENT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-2.Feb 5, 1998 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9800187Support · corrodedINSPECTION FOUND CORROSION ON THRESHOLD SUPPORT TEE BETWEEN STA 1155 AND 1174 AT AFT CARGO DOOR CUTOUT. THE THRESHOLD SUPPORT WAS REPLACED IAW SRM 51-10-2.Feb 5, 1998 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9800186Clips · brokenINSPECTION FOUND AFT FUSELAGE TAIL CONE EXTERIOR RELEASE HANDLE CLIPS BENT AND BROKEN. NEW CLIPS WERE INSTALLED AND TESTED IAW MM 53-53-00.Feb 5, 1998 · N14890 · Doug DC982 · Aerodynamic FairingsSDR CALA9800185Angle · crackedINSPECTION FOUND A 1.4 INCH CRACK IN AFT CABIN DOOR ANGLE INSIDE DOOR AT CENTER RIGHT DOOR STOP. THE ANGLE WAS REPLACED IAW SRM 51-30-2.Feb 4, 1998 · N14890 · Doug DC982 · Passenger/Crew DoorsSDR CALA9800003Skin · crackedINSPECTION FOUND A .5 INCH CRACK ABOVE BUMPER PAD IN LT MLG DOOR. THE CRACKED SKIN WAS REMOVED AND REPLACED IAW SRM 52-05.Jan 6, 1998 · N14890 · Doug DC982 · Landing Gear DoorsSDR CALA9601171Apu Compressor · damagedTHERE WAS A STRONG PUNGENT ODOR IN THE AIRCRAFT CABIN SHORTLY AFTER TAKEOFF. NO ODOR WAS NOTICED DURING CRUISE PORTION OF FLIGHT WITH BOTH PACKS OPERATING. MAINTENANCE FOUND THE APU COMPRESSOR DAMAGED AND SEAL LEAKING. THE APU WAS PLACARDED INOPERATIVE FOR Aug 15, 1996 · N14890 · Doug DC982 · APU Core EngineSDR CAL960620Downlock Sensor · inoperativeFLT 1105 - CLE - THE LEFT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION ON APPROACH TO CLE. CYCLING THE GEAR DID NOT HELP. THE GEAR WAS MANUALLY EXTENDED, BUT THE LIGHT REMAINED ON. THE GEAR WAS VISUALLY VERIFIED DOWN THROUGH THE VIEW PORT. THMay 17, 1996 · N14890 · Doug DC982 · Landing Gear Position and WarningSDR CAL960377Bracket · corrodedMIA - INSPECTION FOUND BRACKET PLATE CORRODED AT INTERSECTION OF FUSELAGE RIGHT CUSP FITTING AND FLOORBEAM, STATION 1338. THE CORRODED PLATE WAS REMOVED AND A NEW PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-01. (M)Feb 14, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL960376Support Brackets · crackedMIA - INSPECTION FOUND 3 SUPPORT BRACKETS CRACKED AT RT WING FIXED LEADING EDGE INNER RIB. TWENTY INCHES OUTBOARD OF SLAT TRACK NR 2. THE CRACKS WERE 2 INCHES, .50 INCH, AND .50 INCH LONG. THE BRACKETS WERE REMOVED. NEW BRACKETS WERE FABRICATED AND INSTALLFeb 13, 1996 · N14890 · Doug DC982 · Wing Miscellaneous StructureSDR CAL960378Fasteners · brokenMIA - INSPECTION FOUND TWO FASTENER HEADS POPPED ON RIGHT SIDE OF FUSELAGE AT FS 1000 AND 1005 BETWEEN L18R AND L19R, BELOW CUSP LINE. THE FASTENERS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. (M)Feb 12, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL960390Support · crackedMIA - INSPECTION FOUND A .75 INCH CRACK IN LT WING TRAILING EDGE X-SUPPORT MEMBER AT UPPER AFT LEG FORWARD OF ATTACH POINT, JUST INBOARD OF NR 1 SPOILER ACTUATOR. THE SUPPORT MEMBER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)Feb 11, 1996 · N14890 · Doug DC982 · Wing Miscellaneous StructureSDR CAL960389Support · crackedMIA - INSPECTION FOUND A 1 INCH CRACK IN LT WING TRAILING EDGE X-SUPPORT MEMBER AT UPPER AFT LEG FORWARD OF ATTACH POINT, JUST OUTBOARD OF NR 1 SPOILER ACTUATOR. THE SUPPORT MEMBER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)Feb 11, 1996 · N14890 · Doug DC982 · Wing Miscellaneous StructureSDR CAL960380Angle · corrodedMIA - INSPECTION FOUND THREE FLOOR SUPPORT 'Z' ANGLES CORRODED UNDER FLOORBOARD AT FORWARD ENTRY DOOR SILL AREA. THE FLOOR SUPPORT ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-4. (M)Feb 11, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL960379Web · corrodedMIA - INSPECTION FOUND HORIZONTAL WEB CORRODED AT THRESHOLD OF FORWARD ENTRY DOOR, 4 INCHES INBOARD OF AFT CORNER OF CUTOUT. THE CORROSION WAS REMOVED IAW SRM 53-01. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01. (M)Feb 11, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL960388Support · crackedMIA - INSPECTION FOUND A .6250 INCH CRACK IN FUSELAGE FAIRING SUPPORT ANGLE AT FS 807 BETWEEN LONGERON 25L AND LONGERON 26L. (X)Feb 9, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL960381Angle · crackedMIA - INSPECTION FOUND A .5625 INCH CRACK IN FUSELAGE FAIRING SUPPORT ANGLE AT FS 807, BETWEEN L26R AND L27R. THE CRACK WAS STOP DRILLED. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01. (M)Feb 9, 1996 · N14890 · Doug DC982 · Fuselage Miscellaneous StructureSDR CAL951033Gear Handle · bindingEWR - FLT 0609 - ALL THREE GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHTS EXTINGUISHED. MAINTENANCE CLEANED AND LUBRICATED THE LANDING GEAR HANDLE AND SWITCH. GEAR OPERATION AND INDICATIONS TESTED GOOD. (XNov 12, 1995 · N14890 · Doug DC982 · Landing Gear SelectorSDR CAL950723Fire Loop · inoperativeFLT NR 0114 - IAH - THE NR 1 ENGINE LOOP 'A' AND FIRE DETECT LOOP LIGHT ILLUMINATED WHILE ON DESCENT INTO IAH AT 15,000 FEET. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND BOTH FIRE BOTTLES WERE DISCHARGED. THE NR 1 ENGINE WAS SHUT DOWN. THE RED HANDLE LIGHT Aug 17, 1995 · N14890 · Doug DC982 · Fire DetectionSDR CAL950151Switch · failedFLT NR 0132 - EWR - ALL THREE GEAR INDICATORS REMAINED RED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND ONLY THE NOSE GEAR LIGHT AND DOOR LIGHT REMAINED ON. THE GEAR WAS CYCLED A SECOND TIME AND ALL INDICATIONS WERE NORMAL. THE THREE GEAR INDICATORS WENT Feb 24, 1995 · N14890 · Doug DC982 · Landing Gear Position and WarningSDR CAL950015Grd Shift Mech · frozenFLT NR 0262 - CLE - THE THREE GEAR RED UNSAFE LIGHTS AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED LEAVING CLE. THE GEAR WAS EXTENDED AND THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GJan 7, 1995 · N14890 · Doug DC982 · Landing Gear Retraction/Extension SystemSDR CAL950003Duct · blownSAT - FLT 0437 - A STRONG BURNING ODOR WAS OBSERVED IN THE COCKPIT AND CABIN ON FINAL APPROACH TO SAT WITH THE ICE PROTECTION ON. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LT AIR CONDITIONING SYSTEM DUCT BLOWN IN THE TAIL COMPARTMENT AFT OF WJan 3, 1995 · N14890 · Doug DC982 · Cabin Cooling System
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