# Service difficulty reports: N72829, cancelled Jun 15, 2005 A list on [N72829, cancelled Jun 15, 2005](https://openairdocs.org/deregistered/N72829-2005-06-15.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA9900628](https://openairdocs.org/sdr/CALA9900628.md): Retainer · cracked · Jun 2, 1999 · N72829 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND A 2 INCH CRACK ON FORWARD CARGO DOOR LOWER LEFT PAN SEAL RETAINER UNDER DOOR LATCH MECHANISM. A REPAIR WAS INSTALLED IAW ECRA 5210-01343. - [SDR CALA9900609](https://openairdocs.org/sdr/CALA9900609.md): Skin · dented · Jun 1, 1999 · N72829 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 218 AT LONGERON 18L. THE DENTED AREA WAS REPAIRED IAW ECRA 5330-02817. - [SDR CALA9900581](https://openairdocs.org/sdr/CALA9900581.md): Skin · dented · May 28, 1999 · N72829 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 120 ABOVE LONGERON 18L. AN INTERNAL DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA9900579](https://openairdocs.org/sdr/CALA9900579.md): Beam · cracked · May 27, 1999 · N72829 · Doug DC982 · Passenger/Crew Doors > INSPECTION FOUND A.375 INCH CRACK IN MAIN CABIN DOOR NR 7 BEAM. THE DOOR BEAM WAS REPAIRED IAW SRM 52-05, FIGURE 31. - [SDR CALA9900578](https://openairdocs.org/sdr/CALA9900578.md): Skin · cracked · May 26, 1999 · N72829 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 389, LONGERON 30. A DOUBLER WAS INSTALLED IAW SRM 53-04 AND ECRA 5330-02812. - [SDR CALA9900577](https://openairdocs.org/sdr/CALA9900577.md): Seat Track · corroded · May 26, 1999 · N72829 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 200. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-05, FIGURE 4F. - [SDR CALA9900576](https://openairdocs.org/sdr/CALA9900576.md): Skin · cracked · May 26, 1999 · N72829 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND A.25 INCH CRACK WITH BEND AT LOCKING HANDLE IN FORWARD CARGO DOOR EXTERIOR SKIN. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 30. - [SDR CALA9900575](https://openairdocs.org/sdr/CALA9900575.md): Angle · cracked · May 25, 1999 · N72829 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.5 INCH CRACK IN LT INNER ATTACH ANGLE AT FORWARD LOWER ATTACH POINT FOR VERTICAL STABILIZER, FUSELAGE STA 1418. A 1.5 INCH CRACK WAS FOUND IN RT INNER ATTACH ANGLE AT FORWARD LOWER ATTACH POINT FOR VERTICAL STABILIZER, FUSELAGE STA 1418. - [SDR CALA9900574](https://openairdocs.org/sdr/CALA9900574.md): Longeron · cracked · May 25, 1999 · N72829 · Doug DC982 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A 1 CRACK IN LONGERON 2R AND FOUND A 1 INCH CRACK IN LONGERON 2L AT STA 1418. THE CRACKED SECTIONS OF LONGERON WERE REMOVED, NEW SECTIONS AND SPLICES WERE INSTALLED IAW SRM 53-02, FIGURE 18. - [SDR CALA9900573](https://openairdocs.org/sdr/CALA9900573.md): Beam · cracked · May 24, 1999 · N72829 · Doug DC982 · Passenger/Crew Doors > INSPECTION FOUND A 1 INCH CRACK AT BOTH ENDS OF MAIN CABIN DOOR NR 1 BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-1. - [SDR CALA9900572](https://openairdocs.org/sdr/CALA9900572.md): Beam · cracked · May 24, 1999 · N72829 · Doug DC982 · Service Doors > INSPECTION FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR NR 4 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-02 AND 51-30-05. - [SDR CALA9900571](https://openairdocs.org/sdr/CALA9900571.md): Seat Track · corroded · May 24, 1999 · N72829 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LEFT CENTER SEAT TRACK CORRODED FROM STA 1079 TO 1231. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. - [SDR CALA9900570](https://openairdocs.org/sdr/CALA9900570.md): Skin · dented · May 23, 1999 · N72829 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND LT FUSELAGE SKIN DENTED BELOW CUSP LINE AT STA 218. THE DENTED AREA WAS ROUTED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 25. - [SDR CALA9900569](https://openairdocs.org/sdr/CALA9900569.md): Seat Track · corroded · May 22, 1999 · N72829 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 218 TO 256. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30. - [SDR CALA9900567](https://openairdocs.org/sdr/CALA9900567.md): Seat Track · corroded · May 20, 1999 · N72829 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 218-237. A NEW SECTION OF SEAT TRACK WAS SPLICED IN IAW SRM 53-05, FIGURE 4F. - [SDR CALA9900563](https://openairdocs.org/sdr/CALA9900563.md): Seat Track · corroded · May 20, 1999 · N72829 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LEFT OUTBOARD SEAT TRACK CORRODED AT STA 1136-1128. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-2. - [SDR CALA9900562](https://openairdocs.org/sdr/CALA9900562.md): Jamb · corroded · May 20, 1999 · N72829 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CORROSION ON FORWARD BAG BIN DOOR JAMB PAN AT STA 370-427. A NEW PAN AND DOUBLERS WERE INSTALLED IAW SRM 53-05. - [SDR CALA9900561](https://openairdocs.org/sdr/CALA9900561.md): Seat Track · corroded · May 20, 1999 · N72829 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LEFT INBOARD SEAT TRACK CORRODED AT STA 1212-1222. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01. - [SDR CALA9900560](https://openairdocs.org/sdr/CALA9900560.md): Escape Line · frayed · May 19, 1999 · N72829 · Doug DC982 · Emergency Equipment > INSPECTION FOUND THE LEFT OVERWING EXIT ESCAPE LINE FRAYED AT ATTACH HOOK. THE ESCAPE LINE WAS REMOVED AND REPLACED IAW MM 25-61-00, PAGE 204-205. - [SDR CALA9900002](https://openairdocs.org/sdr/CALA9900002.md): Duct · ruptured · Jan 2, 1998 · N72829 · Doug DC982 · Air Intake Anti/De-Ice System > THE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED AFTER TAKEOFF. THRUST WAS REDUCED TO IDLE WITH THE FIRE HANDLE AND LOOP LIGHT EXTINGUISHING SHORTLY AFTERWARDS. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT - [SDR CALA970788](https://openairdocs.org/sdr/CALA970788.md): Intercostal · cracked · May 19, 1997 · N72829 · Doug DC982 · Passenger/Crew Doors > INSPECTION FOUND A 1.5 INCH CRACK IN MAIN CABIN DOOR INTERCOSTAL AT AFT HANDLE TORQUE TUBE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-10-3. - [SDR CALA9700789](https://openairdocs.org/sdr/CALA9700789.md): Intercostal · cracked · May 17, 1997 · N72829 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.5 AND.75 INCH CRACK IN AFT BAGGAGE BIN INTERCOSTAL BETWEEN FLOORBEAMS AT STA 1271 TO 1294. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2. ## 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 = 'N72829' AND deregistration_id = 'N72829-2005-06-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N72829-2005-06-15/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.