N58545, cancelled Jun 7, 2013

Service difficulty reports · 22

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 = 'N58545' AND deregistration_id = 'N58545-2013-06-07'
  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 CALA9802118Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED UNDER KEEL BEAM AREA AT BS 676, LONGERON 30. A PERMANENT REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ENGINEERING ORDER 07512 AND SRM 53-04, FIGURE 38, SHEET 3.Nov 29, 1998 · N58545 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9802117Panel · crackedINSPECTION FOUND A 4 INCH CRACK IN RT LOWER VERTICAL STABILIZER SLIDING PANEL. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01 FIGURE 2, 51-10-2A, 51-10-4, 51-10-3 AND 51-30-2.Nov 29, 1998 · N58545 · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR CALA9802106Skin · dentedA DENT WAS FOUND IN RT FUSELAGE SKIN AFT OF R-1 SERVICE DOOR. THE DENTED AREA WAS CUT OUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12A AND 12B AND SRM 51-10-3.Nov 24, 1998 · N58545 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9802105Skin · dentedA DENT WAS FOUND IN RT FUSELAGE SKIN FOURTEEN INCHES FORWARD OF AFT BAG BIN DOOR. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 12B.Nov 24, 1998 · N58545 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9800079Skin · crackedINSPECTION FOUND THREE EACH .5 INCH CRACKS AT RIVETS OF AFT PRESSURE BULKHEAD T-CAP SKIN, STA 996, LONGERON 8-9R. A SKIN REPAIR WAS INSTALLED IAW DACO DRAWING J060138.Jan 17, 1998 · N58545 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9700981Apu · failedTHE APU FIRE DETECTION LOOP LIGHT ILLUMINATED AFTER TAKEOFF. THE FIRE BOTTLE WAS DISCHARGED AND THE LIGHT EXTINGUISHED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE APU COMPARTMENT WAS INSPECTED AND THERE WAS NO EVIDENCE OF FIRE FOJul 1, 1997 · N58545 · Doug DC932 · APU Core EngineSDR CALA9700587Actuator · out of adjustRIGHT MAIN LANDING GEAR FAILED TO RETRACT ON TAKEOFF. FOUND MAIN LANDING GEAR ACTUATOR OUT OF ADJUSTMENT. ADJUSTED MAIN LANDING GEAR ACTUATOR IN ACCORDANCE WITH MAINTENANCE MANUAL.Apr 22, 1997 · N58545 · Doug DC932 · Landing Gear ActuatorSDR CALA9700197Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN BELTFRAME WITH CORROSION AT STA 897, LONGERON 23L. THE CORRODED AREA WAS REMOVED, A REPAIR WAS SPLICED IN IAW SRM 53-03, FIGURE 2A.Jan 20, 1997 · N58545 · Doug DC932 · Fuselage Main, FrameSDR CALA9700208Longeron · crackedINSPECTION FOUND A .25 INCH CRACK IN LONGERON 17L AT STA 237. A NEW LONGERON SECTION AND SPLICE SECTION WERE INSTALLED IAW SRM 53-02, FIGURE 2.Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9700207Splice · crackedINSPECTION FOUND A .5 INCH CRACK IN LONGERON 29L SPLICE BETWEEN STA 416 AND 418. A NEW SPLICE WAS INSTALLED IAW SRM 51-30-5.Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9700206Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT CARGO L-ANGLE AT STA 756 LONGERON 28L AND A .5 INCH CRACK IN L-ANGLE AT STA 756 LONGERON 26L. THE ANGLES WERE REPLACED IAW SRM 51-30-0.Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9700205Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT CARGO LONGERON 30 AT FORWARD BULKHEAD STA 756. REPAIRED IAW SRM 53-02, FIGURE 12.Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9700196Longeron · corrodedINSPECTION FOUND LONGERON 28L CORRODED BETWEEN STA 230 TO 235. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9700195Support · crackedINSPECTION FOUND A .25 INCH CRACK IN FLOOR SUPPORT FOR LEFT INBOARD FLOOR AT STA 680. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-11-3.Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9700194Angle · crackedINSPECTION FOUND A 2.5 INCH CRACK IN FLOOR ATTACH ANGLE AT STA 680. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5.Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9700193Stiffener · crackedINSPECTION FOUND A .25 INCH CRACK IN STIFFENER BETWEEN LONGERON 2L AND 3L AT STA 996. THE CRACK WAS STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2.Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9700192Angle · crackedINSPECTION FOUND A .25 AND 1.5 INCH CRACK IN FLOOR SUPPORT ANGLE UNDER SEAT TRACK AT STA 658. THE FLOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-30-5.Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9700191Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN LONGERON 17R AT STA 960. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9700190Longeron · crackedINSPECTION FOUND A .5 INCH CRACK IN LONGERON 17R AT STA 256. REPAIR SPLICES WERE INSTALLED IAW SRM 53-02, FIGURE 2.Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9601705Skin · damagedTHE AIRCRAFT STRUCK A FLOCK OF BIRDS DURING CLIMBOUT BETWEEN 2,500 TO 3,000 FEET. THE AIRCRAFT WAS RETURNED TO CLE. MAINTENANCE DISCOVERED IMPACT DAMAGE TO FUSELAGE SKIN, APPROXIMATELY 2 FEET BY 2 INCHES IN AREA, TWO FEET AFT OF RADOME ON LT FORWARD LOWER SKNov 20, 1996 · N58545 · Doug DC932 · Fuselage Main, Plate/SkinSDR CAL960464Uplock Spring · brokenIAH - FLT 1453 - THE GEAR DOOR OPEN LIGHT ILLUMINATED IN-FLIGHT WITH HYDRAULIC SYSTEM ON LOW. A GEAR UPLATCH CHECK WAS PERFORMED AND THE LIGHT EXTINGUISHED AND REMAINED OUT. MAINTENANCE FOUND RT MLG DOOR UPLATCH MECHANISM SPRING BROKEN. THE MECHANISM WAS REMApr 12, 1996 · N58545 · Doug DC932 · Landing Gear Door Retract SectionSDR CAL950856Skin · crackedIAH - INSPECTION FOUND A .1250 INCH CRACK IN SKIN AT STATION 996 BETWEEN LONGERONS 9 AND 10R. A REPAIR WAS FABRICATED AND INSTALLED IN REFERENCE TO DAC DRAWING J060138 AND EA 5361-01001. (M)Sep 19, 1995 · N58545 · Doug DC932 · Fuselage Main, Plate/Skin
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