# Service difficulty reports: N58545, cancelled Jun 7, 2013 A list on [N58545, cancelled Jun 7, 2013](https://openairdocs.org/deregistered/N58545-2013-06-07.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA9802118](https://openairdocs.org/sdr/CALA9802118.md): Skin · corroded · Nov 29, 1998 · N58545 · Doug DC932 · Fuselage Main, Plate/Skin > INSPECTION 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. - [SDR CALA9802117](https://openairdocs.org/sdr/CALA9802117.md): Panel · cracked · Nov 29, 1998 · N58545 · Doug DC932 · Vertical Stabilizer, Plate/Skin > INSPECTION 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. - [SDR CALA9802106](https://openairdocs.org/sdr/CALA9802106.md): Skin · dented · Nov 24, 1998 · N58545 · Doug DC932 · Fuselage Main, Plate/Skin > A 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. - [SDR CALA9802105](https://openairdocs.org/sdr/CALA9802105.md): Skin · dented · Nov 24, 1998 · N58545 · Doug DC932 · Fuselage Main, Plate/Skin > A 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. - [SDR CALA9800079](https://openairdocs.org/sdr/CALA9800079.md): Skin · cracked · Jan 17, 1998 · N58545 · Doug DC932 · Fuselage Main, Plate/Skin > INSPECTION 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. - [SDR CALA9700981](https://openairdocs.org/sdr/CALA9700981.md): Apu · failed · Jul 1, 1997 · N58545 · Doug DC932 · APU Core Engine > THE 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 FO - [SDR CALA9700587](https://openairdocs.org/sdr/CALA9700587.md): Actuator · out of adjust · Apr 22, 1997 · N58545 · Doug DC932 · Landing Gear Actuator > RIGHT 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. - [SDR CALA9700197](https://openairdocs.org/sdr/CALA9700197.md): Frame · cracked · Jan 20, 1997 · N58545 · Doug DC932 · Fuselage Main, Frame > INSPECTION 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. - [SDR CALA9700208](https://openairdocs.org/sdr/CALA9700208.md): Longeron · cracked · Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Main, Longeron/Stringer > INSPECTION 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. - [SDR CALA9700207](https://openairdocs.org/sdr/CALA9700207.md): Splice · cracked · Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.5 INCH CRACK IN LONGERON 29L SPLICE BETWEEN STA 416 AND 418. A NEW SPLICE WAS INSTALLED IAW SRM 51-30-5. - [SDR CALA9700206](https://openairdocs.org/sdr/CALA9700206.md): Angle · cracked · Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700205](https://openairdocs.org/sdr/CALA9700205.md): Longeron · cracked · Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO LONGERON 30 AT FORWARD BULKHEAD STA 756. REPAIRED IAW SRM 53-02, FIGURE 12. - [SDR CALA9700196](https://openairdocs.org/sdr/CALA9700196.md): Longeron · corroded · Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 28L CORRODED BETWEEN STA 230 TO 235. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2. - [SDR CALA9700195](https://openairdocs.org/sdr/CALA9700195.md): Support · cracked · Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700194](https://openairdocs.org/sdr/CALA9700194.md): Angle · cracked · Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 2.5 INCH CRACK IN FLOOR ATTACH ANGLE AT STA 680. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA9700193](https://openairdocs.org/sdr/CALA9700193.md): Stiffener · cracked · Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700192](https://openairdocs.org/sdr/CALA9700192.md): Angle · cracked · Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700191](https://openairdocs.org/sdr/CALA9700191.md): Longeron · cracked · Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A 1 INCH CRACK IN LONGERON 17R AT STA 960. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2. - [SDR CALA9700190](https://openairdocs.org/sdr/CALA9700190.md): Longeron · cracked · Jan 18, 1997 · N58545 · Doug DC932 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A.5 INCH CRACK IN LONGERON 17R AT STA 256. REPAIR SPLICES WERE INSTALLED IAW SRM 53-02, FIGURE 2. - [SDR CALA9601705](https://openairdocs.org/sdr/CALA9601705.md): Skin · damaged · Nov 20, 1996 · N58545 · Doug DC932 · Fuselage Main, Plate/Skin > THE 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 SK - [SDR CAL960464](https://openairdocs.org/sdr/CAL960464.md): Uplock Spring · broken · Apr 12, 1996 · N58545 · Doug DC932 · Landing Gear Door Retract Section > IAH - 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 REM - [SDR CAL950856](https://openairdocs.org/sdr/CAL950856.md): Skin · cracked · Sep 19, 1995 · N58545 · Doug DC932 · Fuselage Main, Plate/Skin > IAH - 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) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N58545-2013-06-07/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.