N14524, cancelled May 31, 2000

Service difficulty reports · 50

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 = 'N14524' AND deregistration_id = 'N14524-2000-05-31'
  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 CALA9900209Wire · brokenINSPECTION FOUND THE OVERHEAD EMERGENCY LIGHT AT ROW 10 INOPERATIVE. MAINTENANCE FOUND LIGHT WIRE PULLED FROM SPLICE. THE WIRE WAS RESPLICED AND OPERATION CHECKED GOOD.Mar 2, 1999 · N14524 · Doug DC932 · Light System WiringSDR CALA9900208Batteries · dischargedINSPECTION FOUND BOTH NACELLE EMERGENCY LIGHTS INOPERATIVE. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD.Mar 2, 1999 · N14524 · Doug DC932 · Emergency LightingSDR CALA9900207Batteries · dischargedINSPECTION FOUND THE TAIL CONE EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. THE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD.Mar 1, 1999 · N14524 · Doug DC932 · Emergency LightingSDR CALA9900105Wire · looseTHE AFT FLIGHT ATTENDANT STATION EMERGENCY LIGHT SWITCH WAS FOUND INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE ON SWITCH. THE LOOSE WIRE WAS TIGHTENED AND SYSTEM OPERATION CHECKED GOOD IAW MM 33-50-00, PAGES 203-204.Feb 2, 1999 · N14524 · Doug DC932 · Light System WiringSDR CALA9900104Wire · brokenTHE AFT CEILING EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM ROW 23 TO TAIL SECTION. MAINTENANCE FOUND WIRING TO BATTERY POWER PACKS BROKEN. THE WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0.Feb 2, 1999 · N14524 · Doug DC932 · Light System WiringSDR CALA9900103Wire · brokenTHE CABIN EMERGENCY LIGHTS FROM COCKPIT TO ROW 13 WERE FOUND INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0, PAGE 501.Feb 2, 1999 · N14524 · Doug DC932 · Light System WiringSDR CALA9900102Wire · brokenTHE LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0, PAGE 501.Feb 2, 1999 · N14524 · Doug DC932 · Light System WiringSDR CALA9900096Connector · dirtyINSPECTION FOUND THE L-1 PORTABLE EMERGENCY LIGHT INOPERATIVE. THE CONNECTOR WAS CLEANED AND SECURED AND OPERATION OF THE LIGHT CHECKED GOOD.Jan 30, 1999 · N14524 · Doug DC932 · Emergency LightingSDR CALA9900093Wire · brokenINSPECTION FOUND THE ESCAPE PATH LIGHT INBOARD OF FORWARD FIRST CLASS COAT CLOSET INOPERATIVE. MAINTENANCE FOUND BROKEN WIRING. THE ESCAPE PATH LIGHT WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-0, PAGE 501.Jan 29, 1999 · N14524 · Doug DC932 · Light System WiringSDR CALA9900092Fitting · crackedINSPECTION FOUND AFT CARGO DOOR THIRD BEAM END FITTING CRACKED AT AFT SIDE OF DOOR. THE CRACK WAS .1875 INCH LONG. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2.Jan 28, 1999 · N14524 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9900084Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR BEAM END FITTING AT AFT SIDE OF DOOR. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5, PAGE 4.Jan 27, 1999 · N14524 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9900037Rib · crackedRIB CRACKED THROUGH FASTENER HOLE INSIDE LEFT WING L/E XRS545 (.5) 12 INCES OUTSIDE OF NR 5 SLAT CENTER TRACK. REMOVED AND INSTALLED NEW RIB PER SRM 51-30-2.Jan 20, 1999 · N14524 · Doug DC932 · Wing, Rib/BulkheadSDR CALA9900062Tab · debondRIGHT AILERON INBOARD TAB HAS APPROXIMATELY 1 BY 10 DEBONDED LOWER SKIN. REMOVED AND REPLACED RIGHT AILERON PER MM 27-10-2.Jan 16, 1999 · N14524 · Doug DC932 · Aileron TabsSDR CALA9900011Angle · crackedRIB TO LOWER LE ANGLE CRACKED INSIDE RIGHT WING APPROX 8 O/B OF VORTILON. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-5, 51-10-0, 51-10-3, AND 51-10-2.Jan 13, 1999 · N14524 · Doug DC932 · Wing Miscellaneous StructureSDR CALA9900010Terminal · failedAFT DOOR EMERGENGY EXIT LIGHT INOP. REPAIRED TERMINAL AT LIGHT AND OPS CHECK OK PER MM 33-53-01.Jan 11, 1999 · N14524 · Doug DC932 · Emergency LightingSDR CALA9900101Spar · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING AFT SPAR AT I/B ACTUATOR HINGE FORWARD FORGING FROM I/B LOWER BOLT AREA, APPROXIMATELY XRS 164. THE FASTENERS WERE REMOVED AND THE CRACKED SECTION OF SPAR WAS CUT OUT. A NEW SPAR SECTION WAS INSTALLED USING SPLICEJan 2, 1999 · N14524 · Doug DC932 · Wing SparSDR CALA9900004Control · inopTHE LT MLG UNSAFE LIGHT ILLUMINATED ON UPLATCH CHECK AFTER TAKEOFF. WHEN THE SLATS AND FLAPS WERE EXTENDED TO FIVE DEGREES AND THE AIRCRAFT WAS SLOWED TO 210 KNOTS FOR A RETURN TO IAH, THE UNSAFE LIGHT EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THEJan 3, 1998 · N14524 · Doug DC932 · Landing Gear Position and WarningSDR CALA9701678Spar Cap · crackedINSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF RT HORIZONTAL STABILIZER LOWER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE CRACKED SECTION OF SPAR WAS CUT OUT IAW SRM 55-02, FIGURE 8. A REPLACEMENT SPAR SECTION AND REPAINov 24, 1997 · N14524 · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR CALA9701660Spar Cap · crackedINSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF LT HORIZONTAL STABILIZER LOWER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE CRACKED SECTION OF SPAR CAP WAS CUT OUT IAW SRM 55-02, FIGURE 8. A REPLACEMENT SECTION OF SPAR CANov 20, 1997 · N14524 · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR CALA9701659Spar Cap · crackedINSPECTION FOUND A 2 INCH CRACK AT OUTBOARD END OF RT HORIZONTAL STABILIZER UPPER SPAR CAP. THE OUTBOARD FITTING AND BULKHEAD WERE REMOVED IAW SRM 51-30-1. THE CRACKED SPAR SECTION WAS CUT OUT IAW SRM 55-02, FIGURE 8. A REPLACEMENT SPAR SECTION AND REPAIR ANov 20, 1997 · N14524 · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR CALA9701658Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED AT FS 323, LONGERON 24. THE DENTED AREA WAS CUT OUT IAW SRM 53-04. A DOUBLER, FINGER DOUBLER, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-04, 51-10-3, 51-30-2, AND 51-30-5.Nov 20, 1997 · N14524 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9701657Floorbeam · corrodedINSPECTION FOUND CORROSION ON FLOORBEAM NUT PLATE AT STA 965. A DOUBLER, FILLER, AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-30-5, AND ECRA 5320-01488.Nov 20, 1997 · N14524 · Doug DC932 · Fuselage Main, Floor BeamSDR CALA9701656Floor Panel · corrodedINSPECTION FOUND FLOOR PANEL AND HAT CHANNEL CORRODED UNDER PILOT'S SEAT. A NEW PANEL AND HAT CHANNEL WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-20-0.Nov 20, 1997 · N14524 · Doug DC932 · Fuselage Floor PanelSDR CALA9701655Jamb · corrodedINSPECTION FOUND DOOR JAMB AND SUB FLOOR CORRODED AT FS 200 BY R-1 DOOR. THE CORRODED DOOR JAMB PAN AND SUB FLOOR SECTIONS WERE REMOVED IAW SRM 53-05, FIGURE 55. FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-05, 51-10-3, AND 51-30-5.Nov 20, 1997 · N14524 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9701654Support · corrodedINSPECTION FOUND FLOORBOARD SUPPORT AT FORWARD PASSENGER ENTRYWAY CORRODED BETWEEN NR 1 SEAT TRACK AND CENTERLINE FLOORBEAM. THE FLOOR SUPPORT WAS REMOVED, A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-4, 51-10-3, AND 51-30-5.Nov 20, 1997 · N14524 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9701653Skin · dentedINSPECTION FOUND DENTS IN E AND E COMPARTMENT DOOR EXTERIOR SKIN. THE SKIN WAS REMOVED, NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-3.Nov 20, 1997 · N14524 · Doug DC932 · Electrical/Electronic Compartment DoorsSDR CALA9701581Longeron · corrodedINSPECTION FOUND LONGERON 25R CORRODED IN FORWARD CARGO COMPARTMENT AT STA 218. THE LONGERON WAS REMOVED IAW SRM 53-10-03. A NEW LONGERON AND SPLICE SECTION WERE FABRICATED AND INSTALLED IAW SRM 53-02, 51-10-3 AND 51-30-2.Nov 3, 1997 · N14524 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9701580Doubler · gougedINSPECTION FOUND GOUGED DOUBLER AT FORWARD PASSENGER DOOR CUTOUT FOR DOOR LATCH HOOK ASSEMBLY. THE OLD DOUBLER WAS REMOVED IAW SRM 51-30-2. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-05, 51-10-3, 51-30-1, AND 51-30-2.Nov 3, 1997 · N14524 · Doug DC932 · Passenger/Crew DoorsSDR CALA9701579Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN LONGERON 2L AT STA 1079. THE CRACKED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-02. A REPAIR SECTION, SPLICE AND ATTACH BRACKET WERE FABRICATED AND INSTALLED IAW SRM 53-02, 51-30-5 AND ECRA 5310-03589.Nov 3, 1997 · N14524 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9701578Cover · crackedINSPECTION FOUND A 1 INCH CRACK IN RT ELEVATOR FLIGHT TAB MECHANISM CONTROL COVER AT STA XHS 95. THE CRACKED AREA WAS REMOVED, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 55-03, 51-10-3, 51-30-2, AND 51-30-8.Nov 3, 1997 · N14524 · Doug DC932 · Elevator StructureSDR CALA9701577Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED AT FS 360 BETWEEN LONGERON 21R AND 22R. THE DENTED AREA WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND 51-30-2.Nov 3, 1997 · N14524 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9701519Intercostal · dentedINSPECTION FOUND INTERCOSTAL DENTED BETWEEN STA 560 AND 579 AT LONGERON 28R. THE INTERCOSTAL WAS REMOVED. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, 51-10-3, AND 51-30-1.Oct 30, 1997 · N14524 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9701518Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 680-699, LONGERON 16L. THE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-11-3, 51-11-2, 51-10-3, AND 51-30-2.Oct 30, 1997 · N14524 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9701517Intercostal · crackedINSPECTION FOUND INTERCOSTAL CRACKED INSIDE R-1 DOOR AT CENTER OF DOOR BELOW LATCH MECHANISM. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.Oct 30, 1997 · N14524 · Doug DC932 · Service DoorsSDR CALA9701516Skin · dentedINSPECTION FOUND RT WING NR 1 LEADING EDGE SLAT SKIN DENTED. THE DENTED AREA WAS CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 57-06 AND 51-10-3.Oct 29, 1997 · N14524 · Doug DC932 · Leading Edge DevicesSDR CALA9701515Stiffener · crackedINSPECTION FOUND A 2 CRACK IN HORIZONTAL STIFFENER ON FORWARD FACE OF AFT PRESSURE BULKHEAD AT L13R. THE STIFFENER WAS REMOVED. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-5.Oct 29, 1997 · N14524 · Doug DC932 · Fuselage Main, BulkheadSDR CALA9701514Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 284, LONGERON 24. THE DENTED AREA WAS CUT OUT. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-04 AND 53-04, FIGURE 12.Oct 29, 1997 · N14524 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9700111Hyd Line · leakingTHE RT HYDRAULIC SYSTEM LOST ALL QUANTITY DURING FLIGHT. ABNORMAL PROCEDURES WERE ACCOMPLISHED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE ON RIGHT THRUST REVERSER VALVE LEAKING. THE LINE WAS REMOVED AND REPLACED. Jan 29, 1997 · N14524 · Doug DC932 · Hydraulic System, MainSDR CALA9601541Duct · crackedTHE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED SHORTLY AFTER TAKEOFF. THE FIRE WARNING CEASED AFTER THE ENGINE THROTTLE WAS RETARDED LESS THAN TEN PERCENT. BOTH FIRE LOOPS TESTED NORMAL AND ALL ENGINE INDICATIONS WERE NORMAL. THE FLIGHT CONTINUED AT Oct 31, 1996 · N14524 · Doug DC932 · Pneumatic Distribution SystemSDR CALA9600769Pushrod · bentTHE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE FLIGHT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND PUSHROD AT GROUND SENSE SECTOR BENT. THE PUSHROD WAS REMOVED AND REPLACED. THE NLG GROUND SENSE WAS TESTED IAW MM 32-23-1, PAGE 204A. THE LANDINJun 7, 1996 · N14524 · Doug DC932 · Landing Gear Retraction/Extension SystemSDR CAL951140Floor Web · crackedIAH - INSPECTION FOUND A 1 INCH CRACK IN COCKPIT FLOOR WEB AT BS 89.050 AND A 2 INCH CRACK FOUND AT BS 83.550. THE FLOOR WEB WAS REPAIRED IAW ECRA 5310-03193 AND ECRA 531003031. (X)Dec 7, 1995 · N14524 · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL950804Longeron · corrodedHOU - INSPECTION FOUND CORROSION ON LONGERON 26L BETWEEN STATION 945-960. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3 AND RIVETS WERE INSTALLED IAW SRM 51-30-2. (M)Aug 27, 1995 · N14524 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CAL950803Longeron · corrodedHOU - INSPECTION FOUND CORROSION ON LONGERONS 26L TO 28L IN AFT BAGGAGE BIN BETWEEN STATION 937-945. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3 AND RIVETS WERE REPLACED IAW SRM 51-30-2. (M)Aug 27, 1995 · N14524 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CAL950805Rib · crackedHOU - INSPECTION FOUND THREE .25 INCH CRACKS IN WING LEADING EDGE RIB AT STATION XRS 501. A DOUBLER, FILLER, AND CLIP WERE FABRICATED AND INSTALLED IAW ECRA 5720-01260. (M)Aug 24, 1995 · N14524 · Doug DC932 · Wing, Rib/BulkheadSDR CAL950762Skin · crackedHOU - INSPECTION FOUND A .5 INCH CRACK IN SKIN ON TOP SIDE OF NR 2 ENGINE PYLON. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-02. (M)Aug 23, 1995 · N14524 · Doug DC932 · Nacelle/Pylon StructureSDR CAL950497Prox Control Box · inoperativeIAH - FLT 1536 - THE LEFT GEAR UNSAFE LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK AFTER DEPARTING IAH. CYCLING THE GEAR AND REPEATING THE UPLATCH CHECK GAVE NO CHANGE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE LANDING GEAR PJun 17, 1995 · N14524 · Doug DC932 · Landing Gear Position and WarningSDR CAL950472Seal · failedFLT NR 1781 - GSO - THE CABIN BEGAN TO FILL WITH SMOKE DURING TAXI OUT FOR DEPARTURE. THE AIRCRAFT BEGAN A RETURN TO THE GATE AND WAS ACCOMPANIED BY EMERGENCY VEHICLES AS A PRECAUTIONARY MEASURE. NO EVIDENCE OF FIRE WAS OBSERVED. THE PASSENGERS WERE DEPLANEJun 9, 1995 · N14524 · Doug DC932 · Cabin Cooling SystemSDR CAL950338S/O Valve · leakFLT NR 1581 - IAH - UPON LANDING FOUND HYDRAULIC FLUID LEAKING AT RUDDER. FOUND RUDDER POWER SHUTOFF VALVE LEAKING. REPLACED SHUTOFF VALVE NO FURTHER ACTION. (W)Apr 27, 1995 · N14524 · Doug DC932 · Rudder Control SystemSDR CAL950153Bungee Cyl · inoperativeFLT NR 1647 - CLE - THE LEFT MLG RED UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND BOTH RED LIGHTS EXTINGUISHED WITH THREE GREEN GEAR LIGHTS INDICATED. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDEFeb 26, 1995 · N14524 · Doug DC932 · Landing Gear Retraction/Extension SystemSDR CAL950148Eel Batt · dischargedJAX - FLT 1521 - THE FWD OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING A PREFLIGHT CHECK. THE BATTERIES FOR THE FWD OVERWING EMERGENCY EXIT LIGHT WERE REMOVED AND REPLACED. OPERATION OF THE EMERGENCY EXIT LIGHT WAS RESTORED. (W)Feb 23, 1995 · N14524 · Doug DC932 · Emergency Lighting
Back to N14524, cancelled May 31, 2000