N12811, cancelled Jun 1, 2007

Service difficulty reports · 40

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 = 'N12811' AND deregistration_id = 'N12811-2007-06-01'
  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 CALA0400031Megaphone · inoperativeINSPECTION FOUND THE FORWARD CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED.Jan 15, 2004 · N12811 · Doug DC982 · Emergency EquipmentSDR CALA0300530Fan · seizedA/C HAD A CHRONIC INFLT PROBLEM WITH AN ELECTRICAL ODOR AFT. TROUBLESHOOTING PERFORMED. SOURCE OF ODOR APPEARED TO BE COMING FROM AFT GALLEY. COFFEEMAKERS, OVENS, & ACCESS PANELS INSPECTED, NO EVIDENCE OF BURNING. PACK BURNOUT PERFORMED & COALESCER BAGS R & R.Aug 17, 2003 · N12811 · Doug DC982 · Air Distribution FanSDR CALA0200341Beltframe · crackedINSPECTION FOUND A 1" CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, LONGERON 1. REPAIRED BELTFRAME IAW SRM 53-03, FIGURE 4.Jun 14, 2002 · N12811 · Doug DC982 · Fuselage Main, FrameSDR CALA0200338Web · crackedINSPECTION FOUND TAIL COMPARTMENT BELTFRAME WEB CRACKED AT STA 1463 L18R AND L18L. BOTH CRACKS WERE 2" LONG. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2.Jun 12, 2002 · N12811 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000459Pan · chafedINSPECTION FOUND AFT BAG BIN DOOR PAN CHAFED AT STOP PAD AREAS. REPAIRED IAW ECRA 5230-01540.Apr 11, 2000 · N12811 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000457Pan · chafedINSPECTION FOUND DOOR PAN CHAFED BY DOOR STOP IN TWO PLACES AT AFT SIDE AND THREE PLACES AT FORWARD SIDE, FORWARD BAGGAGE BIN. REPAIRED IAW ECRA 5230-01540.Apr 11, 2000 · N12811 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000455Longeron · crackedINSPECTION FOUND A HALF INCH CRACK IN LONGERON 4 LT AT STA 160. THE LONGERON WAS REPAIRED IAW ECRA 5310-04005.Apr 11, 2000 · N12811 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0000454Angle · crackedINSPECTION FOUND LT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1474 - 1485. THERE WERE FIVE CRACKS TOTALING 8 INCHES IN COMBINED LENGTH. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND 51-30-01.Apr 11, 2000 · N12811 · Doug DC982 · Vertical StabilizerSDR CALA0000413Cable · out of rigTHE FORCE REQUIRED TO DROP THE TAIL CONE USING INTERIOR AND EXTERIOR RELEASE HANDLES EXCEEDED 35 POUNDS. THE TAIL CONE RELEASE SYSTEM CABLES WERE ADJUSTED IAW MM 53-53-00.Apr 6, 2000 · N12811 · Doug DC982 · Aerodynamic FairingsSDR CALA0000408Frame · wornINSPECTION FOUND A HOLE WORN INTO FRAME WEB AT STA 1380 AT LT AIR CONDITIONING TEMP CONTROL VALVE. REPAIRED FRAME WEB IAW SRM 53-01.Apr 5, 2000 · N12811 · Doug DC982 · Fuselage Main, FrameSDR CALA0000407Beam · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR LOWER FORWARD BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2.Apr 5, 2000 · N12811 · Doug DC982 · Service DoorsSDR CALA0000406Cargo Track · corrodedINSPECTION FOUND AFT CARGO BIN LEFT AND RIGHT TIEDOWN TRACKS CORRODED AROUND NUT PLATE HOLES AT STA 1022. THE TIEDOWN TRACKS WERE REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-5.Apr 5, 2000 · N12811 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000405Pan · crackedINSPECTION FOUND MID CARGO BIN DOOR PAN CRACKED AT FORWARD AND AFT LATCH. REPAIRED IAW SRM 52-05, FIGURE 26A.Apr 5, 2000 · N12811 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000404Skin · gougedINSPECTION FOUND FORWARD CARGO DOOR SKIN GOUGED AT DOOR BOTTOM. REPAIRED IAW SRM 52-03, FIGURE 7.Apr 5, 2000 · N12811 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000402Pan · wornINSPECTION FOUND FORWARD CARGO DOOR OUTER PAN WORN AT DOOR STOP PADS. REPAIRED AFT STOPS IAW ECRA 5330-02819.Apr 5, 2000 · N12811 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000401Pan · wornINSPECTION FOUND FORWARD CARGO BIN LOWER DOOR PAN WORN IN TWO PLACES BY DOOR STOPS. TWO STRAPS WERE INSTALLED IAW ECRA 5330-02819.Apr 5, 2000 · N12811 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000394Floorbeam · gougedINSPECTION FOUND A HOLE GOUGED IN CABIN FLOORBEAM AT STA 396. A REPAIR WAS INSTALLED IAW SRM 53-05 SHEETS 1, 2 & 3.Apr 4, 2000 · N12811 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0000379Longeron · crackedINSPECTION FOUND A .5 INCH CRACK IN LONGERON 2R JUST OVER BELTFRAME AT STA 1429. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 18, SHEET 2.Mar 31, 2000 · N12811 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0000375Pan · crackedINSPECTION FOUND AFT BAG BIN DOOR EXTERIOR HANDLE PAN GOUGED WITH A 1 INCH CRACK. THE PAN WAS REMOVED AND REPLACED IAW MM 51-30-02.Mar 30, 2000 · N12811 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000374Beltframe · corrodedINSPECTION FOUND BELTFRAME CORRODED ON AFT SIDE AT STA 541 FROM LONGERON 29L TO 29R. THE CORROSION WAS REMOVED, TREATED AND PRIMED AREA IAW SRM 51-10-3 AND REINSTALLED FASTENERS IAW SRM 51-30-5.Mar 30, 2000 · N12811 · Doug DC982 · Fuselage Main, FrameSDR CALA0000373Beltframe · corrodedINSPECTION FOUND AFT BAG BIN BELTFRAME CORRODED AT STA 1238, LONGERON 24L. THE CORROSION WAS REMOVED, TREATED, AND PRIMED IAW SRM 53-01, FIGURE 1.Mar 30, 2000 · N12811 · Doug DC982 · Fuselage Main, FrameSDR CALA0000369Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 389, LONGERON 29R TO 30. A REPAIR WAS INSTALLED IAW ECRA 5330-02800.Mar 30, 2000 · N12811 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000421Seat Track · corrodedINSPECTION FOUND RT O/B SEAT TRACK CORRODED IN FORWARD GALLEY AREA AT STA 218-266. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F.Mar 30, 2000 · N12811 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000368Floor Support · crackedINSPECTION FOUND A .5 INCH CRACK IN MAIN CABIN FLOOR SUPPORT AT STA 826 UNDER RIGHT I/B SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.Mar 28, 2000 · N12811 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000367Seat Track · crackedINSPECTION FOUND A .75 INCH CRACK IN MAIN CABIN FLOOR SUPPORT AT STA 927 BELOW LT O/B SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-0.Mar 28, 2000 · N12811 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000366Floor Support · corrodedINSPECTION FOUND FORWARD R-1 ENTRY SLIDE ARMING BAR ATTACHED FORWARD AND AFT FLOOR SUPPORTS CORRODED. THE SUPPORTS WERE REMOVED AND NEW ONES WERE INSTALLED IAW SRM 51-30-1.Mar 28, 2000 · N12811 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000355Seat Track · corrodedINSPECTION FOUND LT CENTER SEAT TRACK CORRODED ON BOTH SIDES OF FLOOR SUPPORT FLANGES FROM FS 1041 - 1309. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-00.Mar 27, 2000 · N12811 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000332Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AND GOUGED AT STA 120-133, LONGERON 23R. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38.Mar 22, 2000 · N12811 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000330Line · frayedINSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY ESCAPE LINES FRAYED AT ATTACH HOOK. THE EMERGENCY ESCAPE LINES WERE REMOVED AND REPLACED IAW MM 25-60-00.Mar 22, 2000 · N12811 · Doug DC982 · Emergency EquipmentSDR CALA0000329Skin · dentedINSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 712, LONGERON 20L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.Mar 22, 2000 · N12811 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9801857Actuator · burntTHE CO-PILOT OBSERVED SMOKE COMING FROM THE THROTTLE QUADRANT AFTER TAKEOFF FROM COS. THE ELECTRICAL FIRE/SMOKE OF UNKNOWN ORIGIN EMERGENCY LIST WAS INITIATED AND THE AIRCRAFT WAS RETURNED TO COS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AUTO SSep 26, 1998 · N12811 · Doug DC982 · Drag Control ActuatorSDR CALA9800596Beam · crackedINSPECTION FOUND A 1 INCH CRACK AT FORWARD END AND AFT END OF NR 1 DOOR BEAM OF MAIN CABIN DOOR. A NEW NR 1 MAIN CABIN DOOR BEAM WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.Mar 26, 1998 · N12811 · Doug DC982 · Passenger/Crew DoorsSDR CALA9800589Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERCOSTAL AFT OF HANDLE TORQUE SHAFT. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-02 AND 51-30-05.Mar 25, 1998 · N12811 · Doug DC982 · Passenger/Crew DoorsSDR CALA9800588Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN DOOR EXTERIOR SKIN AROUND HOLD OPEN HOOK CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 20A, PAGE 43.Mar 25, 1998 · N12811 · Doug DC982 · Passenger/Crew DoorsSDR CALA9800587Pivot Plates · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER INBOARD AND OUTBOARD SET OF PIVOT PLATES CORRODED. THE PIVOT PLATES WERE REPLACED IAW SRM 51-30-5.Mar 25, 1998 · N12811 · Doug DC982 · Horizontal Stabilizer StructureSDR CALA9701510Retract Mech · malfunctionedTHE AIRCRAFT WAS STUCK IN GROUND MODE AND THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT MADE A NORMAL LANDING. MAINTENANCE CHECKED THE GROUND SENSING SWITCHES IAW MM 32-23-01 AND NO Oct 28, 1997 · N12811 · Doug DC982 · Landing Gear Retraction/Extension SystemSDR CALA9700188Bus Control · malfunctionedALL ELECTRICAL POWER FELL OFF LINE AND ARTS WAS INITIATED AFTER TAKEOFF. EMERGENCY POWER WAS TURNED ON, THE APU GENERATOR WAS PUT ON LINE, PARTIAL POWER WAS RESTORED. WHEN ATTEMPTING TO TURN EMERGENCY POWER OFF A LOUD HUM WAS HEARD FROM CIRCUIT BREAKER PANELFeb 17, 1997 · N12811 · Doug DC982 · AC Generation SystemSDR CALA9600967Airseal · wornTHE NR 1 ENGINE SPOOLED DOWN ACCOMPANIED BY A LOUD EXPLOSION WHILE CLIMBING THROUGH FL 310. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL Jul 6, 1996 · N12811 · Doug DC982 · Turbine SectionSDR CAL960033Skin · crackedIAH - FLT 1707 - INSPECTION FOUND A 5.25 INCH CRACK IN LEFT WING LEADING EDGE SKIN AT STA 242. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5730-01428. (X)Jan 16, 1996 · N12811 · Doug DC982 · Wing, Plate/SkinSDR CAL950515Eel Batteries · inoperativeFLT NR 0299 - EWR - INSPECTION FOUND THE INTERIOR EMERGENCY EXIT LIGHTS AT ROW 6-9 AND AT ENTRANCE TO COCKPIT DOOR INOPERATIVE. THE BATTERIES AT ROW 7 AND IN THE FORWARD OVERHEAD CEILING COMPARTMENT WERE REPLACED. OPERATION OF THE EMERGENCY EXIT LIGHTS WAS RJun 21, 1995 · N12811 · Doug DC982 · Emergency Lighting
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