# Service difficulty reports: N83071, cancelled Jun 11, 2003 A list on [N83071, cancelled Jun 11, 2003](https://openairdocs.org/deregistered/N83071-2003-06-11.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA9900638](https://openairdocs.org/sdr/CALA9900638.md): Support · corroded · Jun 4, 1999 · N83071 · Doug DC1030 · Wing Miscellaneous Structure > INSPECTION FOUND LT AND RT MLG A FRAME SUPPORT BEAM BOLT HOLES CORRODED. THE SUPPORT BEAM WAS REPAIRED IAW SRM 57-20-00, PAGE 104. - [SDR CALA9900630](https://openairdocs.org/sdr/CALA9900630.md): Mounting · corroded · Jun 3, 1999 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND MOUNTING PLATE ASSEMBLY CORRODED AT STA 1876-1886 FROM POSITION X = 0.02L TO X = 0.10L. THE MOUNTING PLATE WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 53-16-01. - [SDR CALA9900611](https://openairdocs.org/sdr/CALA9900611.md): Seat Track · corroded · Jun 2, 1999 · N83071 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LT SEAT TRACK CORRODED FROM STA 1866 TO 1856 AT POSITION X = 0.74L. THE SECTION OF SEAT TRACK WAS REPAIRED IAW SRM 53-70-00, FIGURE 6. - [SDR CALA9900610](https://openairdocs.org/sdr/CALA9900610.md): Floorbeam · corroded · Jun 2, 1999 · N83071 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1903 FROM POSITION X = 0.25L TO X = 0.25R. THE FLOOR SUPPORT BEAM WAS REPLACED IAW 53-16-00, FIGURE 10. - [SDR CALA9900607](https://openairdocs.org/sdr/CALA9900607.md): Seat Track · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RT SEAT TRACK CORRODED FROM STA 1876-1866 AT POSITION X = 0.60R AND X = 0.60L. THE SEAT TRACK SECTIONS WERE REPAIRED IAW SRM 53-70-00, FIGURE 6. - [SDR CALA9900606](https://openairdocs.org/sdr/CALA9900606.md): Seat Track · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RT SEAT TRACK CORRODED FROM STA 1866 TO 1856 AT POSITION X = 0.74R. THE CORRODED SECTION FOR SEAT TRACK WAS REPLACED IAW SRM 53-70-00, FIGURE 6. - [SDR CALA9900605](https://openairdocs.org/sdr/CALA9900605.md): Bulkhead Tee · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Main, Bulkhead > INSPECTION FOUND T-SECTION ON FORWARD FACE OF REAR PRESSURE BULKHEAD AT STA 2007 FROM POSITION X = 0.55L TO X = 0.65L CORRODED. THE CORRODED SECTION WAS REMOVED AND A SPLICE REPAIR WAS INSTALLED IAW SRM 53-40-00, FIGURE 16. - [SDR CALA9900604](https://openairdocs.org/sdr/CALA9900604.md): Floorbeam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.27R TO X = 0.33R AND POSITION X = 0.38R TO X = 0.56R. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9900603](https://openairdocs.org/sdr/CALA9900603.md): Floorbeam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X =0.04R TO X = 0.22R. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9900602](https://openairdocs.org/sdr/CALA9900602.md): Floorbeam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.60R TO X = 0.90R AND POSITION X = 0.60L TO X = 0.90L. THE FLOORBEAM CAPPING SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9900601](https://openairdocs.org/sdr/CALA9900601.md): Floorbeam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.04L TO X = 0.22L. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9900600](https://openairdocs.org/sdr/CALA9900600.md): Floorbeam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.27L TO X = 0.38L. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9900599](https://openairdocs.org/sdr/CALA9900599.md): Beam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 2007 TO 1893 AT POSITION X = 0.60L AND X = 0.60R. THE CORRODED BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9900598](https://openairdocs.org/sdr/CALA9900598.md): Beam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 2007 TO 1876 AT POSITION X = 0.25R AND X = 0.25L. THE CORRODED SECTIONS OF BEAM WERE REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9900597](https://openairdocs.org/sdr/CALA9900597.md): Beam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1996 TO 1903 AT POSITION X = 0.20R AND X = 0.20L. THE CORRODED BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9900596](https://openairdocs.org/sdr/CALA9900596.md): Beam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1986 FROM POSITION X = 0.60R TO 0.90R. THE CORRODED SECTION OF BEAM WAS REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9900595](https://openairdocs.org/sdr/CALA9900595.md): Beam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1986 FROM POSITION X = 0.27R TO X = 0.53R. THE BEAM SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9900594](https://openairdocs.org/sdr/CALA9900594.md): Beam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1866, POSITION X = 0.03L TO X = 0.28L AND POSITION X = 0.03R TO X = 0.28R. THE BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00 FIGURE 10. - [SDR CALA9900593](https://openairdocs.org/sdr/CALA9900593.md): Beam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1887 TO 1839 AT POSITION X = 0.03L AND X + 0.03R. THE BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9900592](https://openairdocs.org/sdr/CALA9900592.md): Beam · corroded · Jun 1, 1999 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1876 TO 1810 AT POSITION X = 0.36L AND X = 0.36R. THE BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10. - [SDR CALA9800882](https://openairdocs.org/sdr/CALA9800882.md): Light · inoperative · May 18, 1998 · N83071 · Doug DC1030 · Emergency Lighting > INSPECTION FOUND THE EMERGENCY FLOODLIGHT AT LAV B INOPERATIVE. THE FLOODLIGHT WAS REPLACED IAW MM 33-50-00. - [SDR CALA9800881](https://openairdocs.org/sdr/CALA9800881.md): Batteries · discharged · May 18, 1998 · N83071 · Doug DC1030 · Emergency Equipment > INSPECTION FOUND AFT MEGAPHONE INOPERATIVE. THE MEGAPHONE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 25-60-00. - [SDR CALA9800880](https://openairdocs.org/sdr/CALA9800880.md): Angle · cracked · May 17, 1998 · N83071 · Doug DC1030 · Wing Miscellaneous Structure > INSPECTION FOUND A 1 CRACK IN ANGLE AT LT WHEEL WELL REAR SPAR, WS 118. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-33-01, AND 51-31-01. - [SDR CALA9800234](https://openairdocs.org/sdr/CALA9800234.md): Trim Motor · cracked · Feb 14, 1998 · N83071 · Doug DC1030 · Stabilizer Control System > THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT ILLUMINATED WHILE EN ROUTE TO EWR. APPROPRIATE CHECKLISTS WERE FOLLOWED AND BOTH PUMPS WERE SHUTOFF. THE HYDRAULIC FLUID DEPLETED TO ZERO VERY SLOWLY AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUN - [SDR CALA9800175](https://openairdocs.org/sdr/CALA9800175.md): Skin · dented · Feb 2, 1998 · N83071 · Doug DC1030 · Leading Edge Devices > INSPECTION FOUND A 2 X 3 DENT IN LT INBOARD LEADING EDGE SLAT WITH SIX POPPED RIVETS AT STA XIS 240.844. REPAIRED IAW ECRA 5750-02897 AND PLACED ON DIP TO REPLACE RIB WITHIN 365 DAYS OR NEXT C-CHECK. - [SDR CALA9700809](https://openairdocs.org/sdr/CALA9700809.md): Fire Loop · chafed · Jun 2, 1997 · N83071 · Doug DC1030 · Fire Detection > THE NR 2 ENGINE FIRE WARNING LIGHT FOR B-LOOP (A LOOP WAS ON PLACARD) ILLUMINATED TEN MINUTES AFTER TAKEOFF. THE NR 2 ENGINE WAS SHUT DOWN, BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS RETURNED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE F - [SDR CALA9700669](https://openairdocs.org/sdr/CALA9700669.md): Support · corroded · Apr 8, 1997 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND CORROSION ON FLOOR SUPPORTS AT STA 1875, LBL 30 AND RBL 30. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 53-16-01 AND 51-35-01. - [SDR CALA9700668](https://openairdocs.org/sdr/CALA9700668.md): Support · corroded · Apr 8, 1997 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND CORROSION ON FLOOR SUPPORTS AT STA 1887, RBL 24-80, LBL 20-80, AND LBL 3- RBL 3. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 53-16-01 AND 51-35-01. - [SDR CALA9700667](https://openairdocs.org/sdr/CALA9700667.md): Support · corroded · Apr 8, 1997 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1880-2007, LBL 24 AND RBL 24. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 53-16-01 AND 51-33-01. - [SDR CALA9700670](https://openairdocs.org/sdr/CALA9700670.md): Intercostal · corroded · Apr 7, 1997 · N83071 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND CENTER CARGO INTERCOSTAL CORRODED BETWEEN STA 1720-1740, STRINGER 51-52R. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-00-01. - [SDR CAL951081](https://openairdocs.org/sdr/CAL951081.md): Bearing · failed · Dec 3, 1995 · N83071 · Doug DC1030 · Turbine Engine Accessory Drive > FLT NR 28 - LGW - THE NR 2 ENGINE WAS SHUT DOWN FOR LOSS OF OIL WHILE EN ROUTE TO LGW. THE ENGINE WAS SHUT DOWN WITH POSITIVE OIL PRESSURE AND THE AIRCRAFT LANDED AT LGW WITHOUT INCIDENT. PRELIMINARY FINDINGS REVEALED THE TRANSFER GEARBOX HAD SEPARATED FROM - [SDR CAL950879](https://openairdocs.org/sdr/CAL950879.md): Eel Batt Chrger · inoperative · Oct 3, 1995 · N83071 · Doug DC1030 · Emergency Lighting > EWR - FLT 0012 - WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED ON AFTER ARRIVING IN EWR, THE FORWARD FIRST CLASS AREA AND AFT COACH SECTION TRACK LIGHTING WOULD NOT COME ON. BOTH EMERGENCY LIGHT BATTERY CHARGERS WERE REMOVED AND REPLACED AND OPERATION OF THE TR - [SDR CAL950878](https://openairdocs.org/sdr/CAL950878.md): Eel Batt Charger · inoperative · Oct 3, 1995 · N83071 · Doug DC1030 · Emergency Lighting > EWR - FLT 0012 - WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED ON AFTER ARRIVING IN EWR, THE FORWARD FIRST CLASS AREA AND AFT COACH SECTION TRACK LIGHTING WOULD NOT COME ON. BOTH EMERGENCY LIGHT BATTERY CHARGERS WERE REMOVED AND REPLACED AND OPERATION OF THE TRA ## 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 = 'N83071' AND deregistration_id = 'N83071-2003-06-11' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N83071-2003-06-11/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.