N15525, cancelled Oct 18, 2000

Service difficulty reports · 24

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 = 'N15525' AND deregistration_id = 'N15525-2000-10-18'
  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 CALA9900091Power Supply · inopTHE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE B5-25 POWER SUPPLY AT STA 635 WAS REMOVED AND REPLACED.Jan 28, 1999 · N15525 · Doug DC932 · Emergency LightingSDR CALA9801390Skin · crackedINSPECTION FOUND AFT CARGO BARRIER DOOR SKIN CRACKED AND DELAMINATED ON INBOARD SIDE WITH A PUNCTURE ON OUTBOARD SIDE. THE DOOR WAS DISASSEMBLED. THE OUTER SKIN WAS REMOVED AND THE PUNCTURED AREA WAS TRIMMED OUT. NEW SKIN AND DOUBLERS WERE FABRICATED AND INSAug 5, 1998 · N15525 · Doug DC932 · Cargo CompartmentsSDR CALA9801388Skin · crackedINSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL UPPER SKIN HOLES ELONGATED AND CRACKED. THE PYLON UPPER SKIN WAS REMOVED, NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, 51-10-3, 51-30-2.Aug 5, 1998 · N15525 · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR CALA9801389Skin · corrodedINSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL LOWER SKIN DELAMINATED AND CORRODED. SKIN AND FINGER DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-0, 51-30-8, AND 51-30-2.Aug 4, 1998 · N15525 · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR CALA9801382Strap · crackedINSPECTION FOUND A 3 INCH CRACK IN NR 1 PYLON TRAILING EDGE PANEL DOUBLER STRAP. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-0.Jul 31, 1998 · N15525 · Doug DC932 · Nacelle/Pylon StructureSDR CALA9801381Bracket · gougedINSPECTION FOUND NR 1 THRUST REVERSER PANEL BRACKET GOUGED. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2A, AND 51-30-2.Jul 31, 1998 · N15525 · Doug DC932 · Engine Thrust ReverserSDR CALA9801380Angle · crackedINSPECTION FOUND A CRACK IN NR 1 PYLON TRAILING EDGE PANEL INTERCOSTAL ATTACH ANGLE. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-3, AND 51-00.Jul 31, 1998 · N15525 · Doug DC932 · Nacelle/Pylon StructureSDR CALA9801370Panel · corrodedINSPECTION FOUND CORROSION ON TOP SIDE LEFT WING PANEL NR 1122A. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-01, PAGE 8, 57-31-1, 51-10-3, AND 51-30-2.Jul 30, 1998 · N15525 · Doug DC932 · Wing, Plate/SkinSDR CALA9801365Splice · corrodedINSPECTION FOUND FLOOR PANEL SPLICE PLATE IN AFT CARGO PIT AT STA 935 CORRODED. A NEW FLOOR PANEL SPLICE PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.Jul 29, 1998 · N15525 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801364Panel · gougedINSPECTION FOUND RT WING LEADING EDGE PANEL NR 1248 GOUGED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-01, FIGURE 3, 51-10-3, AND 51-30-2.Jul 29, 1998 · N15525 · Doug DC932 · Wing, Plate/SkinSDR CALA9801363Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN ANGLE TO RT WING INBOARD BUTE DOOR STIFFENER ATTACHMENT POINT. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, FIGURE 1.Jul 29, 1998 · N15525 · Doug DC932 · Wing Miscellaneous StructureSDR CALA9801362Floor · crackedINSPECTION FOUND AFT CARGO FLOOR PANEL AT STA 756-935 CRACKED AND WORN IN SEVERAL PLACES. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0.Jul 29, 1998 · N15525 · Doug DC932 · Fuselage Floor PanelSDR CALA9701227Longeron · crackedINSPECTION FOUND A 1 CRACK IN LONGERON 17R AT STA 965. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 18.Aug 14, 1997 · N15525 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CAL960042Drive Mechanism · brokenFLT NR 1787 - IAH - LEFT LEADING EDGE SLAT WOULD NOT RETRACT AFTER LANDING AT IAH. NO IN FLIGHT ABNORMALITIES WERE OBSERVED. MAINTENANCE FOUND THE LEFT OUTBOARD SLAT DRIVE MECHANISM BROKEN. THE SLAT DRIVE MECHANISM WAS REMOVED AND REPLACED IAW MM 27-80-4. Jan 14, 1996 · N15525 · Doug DC932 · Leading Edge Slat Control SystemSDR CAL950844Jamb Door · dentedHOU - INSPECTION FOUND A DENT IN THE FORWARD SERVICE DOOR AFT JAMB. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 42. (M)Sep 20, 1995 · N15525 · Doug DC932 · Fuselage Main, Attach FittingsSDR CAL950842Skin · crackedHOU - INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT STATION 1038 BETWEEN LONGERON 10R AND 11R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, PAGE 8. (M)Sep 17, 1995 · N15525 · Doug DC932 · Fuselage Main, Plate/SkinSDR CAL950845Longeron · corrodedHOU - INSPECTION FOUND CORROSION ON LONGERON 30 IN AFT BAGGAGE BIN FROM STATION 935 TO 990. THE CORRODED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 53-02, FIG 16. (M)Sep 16, 1995 · N15525 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CAL950852Blkhd Web · crackedHOU - INSPECTION FOUND A 3.5 INCH CRACK ON AFT PRESSURE BULKHEAD WEB AT RIGHT EDGE OF AFT ENTRY DOOR JAMB. THE BULKHEAD WEB WAS REPAIRED IAW ECRA 5310-03164. (M)Sep 15, 1995 · N15525 · Doug DC932 · Fuselage Main, BulkheadSDR CAL950833Angle · crackedHOU - INSPECTION FOUND A 3 INCH CRACK IN LEFT WHEEL WELL ATTACH ANGLE. A NEW ANGLE WAS INSTALLED IAW SRM 51-30. (M)Sep 8, 1995 · N15525 · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL950843Bracket · crackedHOU - INSPECTION FOUND A .75 INCH CRACK IN NR 4 LEFT FLAP HINGE OUTBOARD BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-5. (M)Sep 7, 1995 · N15525 · Doug DC932 · Trailing Edge FlapsSDR CAL950839Cusp · corrodedHOU - INSPECTION FOUND CORROSION ON RIGHT CUSP AT STATION 165 JUST FORWARD OF DOOR JAMB. THE CUSP WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER SRM 53-05, FIGURE 55. (M)Sep 7, 1995 · N15525 · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL950838Cusp · corrodedHOU - INSPECTION FOUND CORROSION ON RIGHT CUSP AT STATION 200 JUST AFT OF DOOR JAMB. THE CUSP WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER SRM 53-05, FIGURE 55. (M)Sep 7, 1995 · N15525 · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL950834Bracket · crackedHOU - INSPECTION FOUND A .5 INCH CRACK IN THE RIGHT FLAP NR 4 FLAP HINGE INBOARD AND OUTBOARD BRACKETS. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-30-5. (M)Sep 7, 1995 · N15525 · Doug DC932 · Trailing Edge FlapsSDR CAL950832Jamb · corrodedHOU - INSPECTION FOUND CORROSION ON FORWARD BAGGAGE BIN DOOR JAMB. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 44, PAGE 105. (M)Sep 6, 1995 · N15525 · Doug DC932 · Fuselage Miscellaneous Structure
Back to N15525, cancelled Oct 18, 2000