N10834, cancelled Jun 1, 2007

Service difficulty reports · 66

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 = 'N10834' AND deregistration_id = 'N10834-2007-06-01'
  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 CALA0200495Longeron · crackedINSPECTION FOUND A 1" CRACK IN TAIL COMPARTMENT LONGERON 2R AT STA 1418. REPAIRED LONGERON IAW SRM 53-02, FIGURE 18.Oct 12, 2002 · N10834 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0200494Frame · crackedINSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, L2R. REPAIRED FRAME IAW SRM 53-03, FIGURE 31A.Oct 12, 2002 · N10834 · Doug DC982 · Fuselage Main, FrameSDR CALA0200490Skin · dentedINSPECTION FOUND A DENT IN L/H FUSELAGE SKIN AFT OF FORWARD ENTRY DOOR. THE DENTED SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 53-04.Oct 9, 2002 · N10834 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000957Pan · gougedINSPECTION FOUND FORWARD CARGO DOOR TOP PAN FLANGE GOUGED AT STOP. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW 51-10-02, 51-30-02, 51-10-03, AND ECRA 5330-02819.Jun 21, 2000 · N10834 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000953Retainer · crackedINSPECTION FOUND NR 1 ENGINE APRON FORWARD UPPER SUPPORT (RETAINER) BENT WITH A SIX INCH CRACK. THE RETAINER WAS REMOVED AND REPLACED IAW SRM 51-30-2.Jun 21, 2000 · N10834 · Doug DC982 · Engine Mount SectionSDR CALA0000952Stringer · crackedINSPECTION FOUND A 2 INCH CRACK IN HORIZONTAL STABILIZER DOG HOUSE STRINGER. THE CRACKED AREA WAS REMOVED AND A NEW STRINGER WAS INSTALLED IAW SRM 51-30-2, 53-01, AND 55-01, FIGURE 2.Jun 21, 2000 · N10834 · Doug DC982 · Horizontal Stabilizer, Spar/RibSDR CALA0000949Seat Track · corrodedINSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174 - 1207, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4, AND 51-10-4.Jun 20, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000948Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 180, LBL 16 - 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5.Jun 20, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000947Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180 - 208, LONGERON 18L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-30-2.Jun 20, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000946Attach Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR UPPER AFT INNER ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.Jun 20, 2000 · N10834 · Doug DC982 · Passenger/Crew DoorsSDR CALA0000945Panel · corrodedINSPECTION FOUND LT LOWER FUEL PANEL NR 1363 CORRODED ON MOUNT FACE AND IN COUNTERSINK. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW MM 51-30-2.Jun 20, 2000 · N10834 · Doug DC982 · Wing, Plate/SkinSDR CALA0000944Skin · crackedINSPECTION FOUND TWO 3 INCH CRACKS IN MID CARGO DOOR I/B SKIN. THE CRACKED AREA WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-10-4.Jun 20, 2000 · N10834 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000942Nut Plate · corrodedINSPECTION FOUND CORROSION AROUND AND UNDER NUT PLATES INSIDE AFT CARGO LOWER TORQUE BOX AT FS 1183, LONGERON 27R AND 28R. THE TORQUE BOX WAS REPAIRED IAW ECRA 5310-04023.Jun 20, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000929Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT STA 1287, LONGERON 30 TO 29R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-30-2.Jun 20, 2000 · N10834 · Doug DC982 · Fuselage Main, StructureSDR CALA0000928Frame · corrodedINSPECTION FOUND AFT SIDE OF FRAME CORRODED AT STA 1309, LONGERON 30. THE CORRODED SECTION OF FRAME WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 2A, SHEET 1, PAGE 4A.Jun 20, 2000 · N10834 · Doug DC982 · Fuselage Main, FrameSDR CALA0000927Structure · crackedINSPECTION FOUND A .5 INCH CRACK IN RT MLG I/B DOOR AFT LOWER CORNER AT REPAIR DOUBLER. REMOVED AND REPLACED DOUBLER IAW SRM 51-30-1.Jun 20, 2000 · N10834 · Doug DC982 · Landing Gear DoorsSDR CALA0000920Structure · bentINSPECTION FOUND THE AFT LOWER CORNER OF AFT CARGO DOOR BENT. REPAIRED AREA IAW ECRA 5230-01557.Jun 19, 2000 · N10834 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000919Stop · gougedINSPECTION FOUND FORWARD CARGO DOOR FORWARD SEAL FLANGE DOOR STOPS A-E GOUGED. REPAIRED AREAS IAW ECRA 5330-02819.Jun 19, 2000 · N10834 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000918Cargo Track · corrodedINSPECTION FOUND LT CARGO TIE DOWN TRACK IN AFT PIT CORRODED AROUND CLIP NUT HOLES AT FS 1155 - 1320, LONGERON 27L. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-4.Jun 19, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000917Pan · gougedINSPECTION FOUND AFT CARGO DOOR PAN GOUGED AT STOP NR 5 ON FORWARD EDGE AND AT STOP NR 4 ON AFT EDGE. BOTH AREAS WERE REPAIRED IAW ECRA 5330-02819.Jun 19, 2000 · N10834 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000916Support Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN SUPPORT AT TAIL COMPARTMENT RT SIDE IN CEILING JUST AFT OF FRAME STA 1380. THE CRACK WAS STOP DRILLED AND A STACKED ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 53-01.Jun 19, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000911Skin · dentedINSPECTION FOUND AFT CARGO DOOR OUTER SKIN DENTED JUST ABOVE AFT ACCESS PANEL. THE DENTED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 1 AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 1 AND 51-30-2.Jun 16, 2000 · N10834 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000906Channel · crackedINSPECTION FOUND SUPPORT CHANNELS CRACKED AT CENTER FLOOR PANEL BETWEEN FS 886 AND 946. THE CRACKS WERE 2 INCHES LONG. THE FLOOR PANEL WAS REMOVED IAW SRM 51-30-1. THE SUPPORT CHANNELS WERE REMOVED AND NEW CHANNELS WERE INSTALLED IAW 51-10-4 AND 51-30-0. TJun 15, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000905Cargo Track · corrodedINSPECTION FOUND MID CARGO RT TRACK AFT OF DOOR CORRODED UNDER NUT CLIPS AT FS 683 - 786, LONGERON 27R. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 51-30-1, AND 51-30-2.Jun 15, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000904Rib · crackedINSPECTION FOUND A 6 INCH CRACK IN RT WING L/E RIB AT TRACK NR 8, XRS 248. THE CRACK WAS STOP DRILLED IAW SRM 57-01, FIGURE 3. A REPAIR ANGLE WAS INSTALLED IAW SRM 57-10, FIGURE 3 AND 51-30-2.Jun 15, 2000 · N10834 · Doug DC982 · Wing, Rib/BulkheadSDR CALA0000902Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT STA 389, LONGERON 24L. THE SKIN WAS REPAIRED IAW SRM 53-04, SHEETS 12 & 20.Jun 15, 2000 · N10834 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000901Skin · canningINSPECTION FOUND RIGHT FUSELAGE SKIN OIL CANNING AT STA 484, LONGERON 23R-24R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.Jun 14, 2000 · N10834 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000900Support Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN EXTERNAL FUSELAGE LOWER SURFACE WING TO BODY FAIRING SUPPORT TEE AT FS 916. THE SUPPORT WAS REMOVED AND A REPLACEMENT SUPPORT ANGLE WAS INSTALLED IAW SRM 51-30-5.Jun 14, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000897Vane · crackedINSPECTION FOUND A .25 INCH CRACK IN NR 2 RT FIXED VANE I/B LOWER SURFACE. REPAIRED AND BONDED DOUBLER WITH RIVETS IAW SRM 57-04 AND 51-71-00.Jun 13, 2000 · N10834 · Doug DC982 · Wing, Plate/SkinSDR CALA0000896Pan · gougedINSPECTION FOUND FORWARD CARGO DOOR FORWARD PAN FLANGE STOPS H-L GOUGED. THE GOUGED AREAS WERE TRIMMED OUT AND REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5330-02819, SRM 51-10-3, 51-10-4, AND 51-30-2.Jun 13, 2000 · N10834 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000873Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED WITH A .5 INCH CRACK AT FS 315 BETWEEN LONGERON 22L AND 23L. THE DENT WAS BLENDED OUT IAW SRM 53-04, FIGURE 38. THE CRACK WAS CUT OUT AND A FINGER DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-3, AND 51-Jun 13, 2000 · N10834 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000865Skin · corrodedINSPECTION FOUND LT AFT UPPER FUSELAGE SKIN CORRODED AROUND FASTENERS JUST BELOW DORSAL FIN AT STA 1429 - 1435. A REPAIR STRAP WAS INSTALLED IAW SRM 53-05, 51-10-3, AND 51-30-5.Jun 10, 2000 · N10834 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000864Cargo Track · corrodedINSPECTION FOUND MID CARGO TIE DOWN TRACK CORRODED AT FS 595 - 785, LONGERON 27L. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.Jun 10, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000863Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT FS 1032 - 1309, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 53-05, AND 51-10-3.Jun 10, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000850Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT FS 670, RBL 22.5. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 53-05, FIGURE 4F, AND 51-10-3.Jun 8, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000849Pan · crackedINSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR PAN AT FORWARD DOOR CAM AREA. THE OLD DOUBLER WAS REMOVED AND A NEW DOOR PAN DOUBLER WAS INSTALLED IAW SRM 51-30-2, 52-05, FIGURE 26A, 51-10-4, 51-10-3.Jun 8, 2000 · N10834 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000848Seat Track · corrodedINSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT FS 218 - 238. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4, 51-10-3, 51-10-4, 51-30-1, 51-30-5, AND 51-30-6.Jun 8, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000847Seat Track · corrodedINSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT FS 1088 - 1231. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 53-05, FIGURE 4.Jun 8, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000842Web · puncturedINSPECTION FOUND HOLE PUNCTURED IN RT CUSP WEB UNDER FLOOR SUPPORT AT FS 200, RBL 44. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2. THE FLOOR SUPPORT WAS REINSTALLED IAW SRM 51-30-1.Jun 7, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000841Seat Track · corrodedINSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174 - 1207, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4, AND 51-10-4.Jun 7, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000840Seat Track · corrodedINSPECTION FOUND SEAT TRACK LUGS CORRODED AT FS 378, RBL 22.5. THE SEAT TRACK WAS REMOVED AND NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, AND 53-05-4.Jun 7, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000839Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 160 - 200, LBL 44.5 AND STA 180, LBL 16 - 36. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-5.Jun 7, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000838Mount · corrodedINSPECTION FOUND G-2 GALLEY I/B FORWARD MOUNT FITTING CORRODED. THE FITTING WAS REMOVED AND AND NEW FITTING WAS INSTALLED IAW SRM 51-30-5.Jun 7, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000817Attach Angle · crackedINSPECTION FOUND R-1 DOOR THRESHOLD AFT ATTACH ANGLE CRACKED AND CORRODED. THE ANGLE AND DOUBLER WERE REMOVED AND A NEW ANGLE AND DOUBLER WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-2, 51-10-4, AND 51-10-3.Jun 2, 2000 · N10834 · Doug DC982 · Fuselage Main, Attach FittingsSDR CALA0000816Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 200 AND 250, LBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5.Jun 2, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000815Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT AT L-2 DOOR, STA 1155. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.Jun 2, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000788Rib · crackedINSPECTION FOUND A 3 INCH CRACK IN I/B RIB OF RIGHT FLAP WEDGE ASSEMBLY NR 6. THE CRACK WAS DRILLED OUT AND A NEW RIB WAS INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-5.Jun 1, 2000 · N10834 · Doug DC982 · Trailing Edge FlapsSDR CALA9801347Tail Cone · warpedTHE FORCE REQUIRED TO RELEASE TAIL CONE DURING FUNCTIONAL CHECK WAS EXCESSIVE. THE TAIL CONE HUNG UP ON RIGHT SIDE LATCH PINS. A SERVICEABLE TAIL CONE WAS INSTALLED AND ADJUSTED IAW MM 53-53-00.Jul 24, 1998 · N10834 · Doug DC982 · Aerodynamic FairingsSDR CALA9801323Skin · dentedINSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 229-237 ABOVE CUSP LINE. A REPAIR WAS INSTALLED IAW ECRA 5330-02687.Jul 23, 1998 · N10834 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9801322Beam · corrodedINSPECTION FOUND CORROSION ON MID BAG BIN Z BEAM AT THRESHOLD, STA 636-693. CORROSION WAS ALSO FOUND ON AFT BAG BIN Z BEAM AT THRESHOLD STA 1155-1212. REPAIRS WERE INSTALLED IAW SRM 53-05, FIGURE 63.Jul 22, 1998 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure
Back to N10834, cancelled Jun 1, 2007