N15820, cancelled Mar 21, 2013

Service difficulty reports · 35

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 = 'N15820' AND deregistration_id = 'N15820-2013-03-21'
  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 CALA0300140Skin · crackedINSPECTION FOUND A 1/2" CRACK IN L-1 DOOR SKIN AT AFT LOWER CORNER. A REPAIR WAS INSTALLED IAW SRM 52-05, PAGE 223.Mar 23, 2003 · N15820 · Doug DC982 · Passenger/Crew DoorsSDR CALA0100862Skin Panel · dentedINSPECTION FOUND L/H I/B FLAP SKIN PANEL DENTED AFT OF MLG. A NEW SKIN PANEL WAS INSTALLED IAW SRM 51-30-1.Sep 12, 2001 · N15820 · Doug DC982 · Trailing Edge FlapsSDR CALA0100857Bracket · crackedINSPECTION FOUND ONE EACH 3/4" CRACK IN GUSSET ATTACH BRACKETS AT RIVET ATTACH ON L/H AND R/H SIDE OF NWW FWD WALL. A NEW STIFFENER WAS INSTALLED AT EACH LOCATION IAW SRM 53-14-1, FIGURE 4 AND 51-30-0.Sep 9, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100856Web · crackedINSPECTION FOUND A 3/4" CRACK IN UPPER WEB IN TAIL COMPARTMENT ON L/H SIDE BY RUDDER SECTOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, PAGE 9.Sep 9, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100855Web · crackedINSPECTION FOUND A 1.5 INCH CRACK IN VENT BOX WEB AT UPPER AFT CORNER AT STA 1485, RT SIDE. AN ANGLE BRACKET WAS INSTALLED IAW SRM 51-30-5.Sep 9, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100848Beltframe · crackedINSPECTION FOUND A 1" CRACK IN BELTFRAME AT STA 1418, LONGERON 2R. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW DRAWING SRO9530003.Sep 9, 2001 · N15820 · Doug DC982 · Fuselage Main, FrameSDR CALA0100847Cargo Track · corrodedINSPECTION FOUND LT TRACK TIE DOWN FLANGES IN AFT PIT CORRODED AT STA 1212. THE LT TRACK TIE DOWN FLANGES WERE REPAIRED IAW SRM 51-30-0.Sep 9, 2001 · N15820 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0100846Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN SUPPORT ANGLE ATTACHED TO AFT CROSSBEAM IN TAIL COMPARTMENT AT TORQUE TUBE, RT SIDE. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02.Sep 8, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100845Strap · crackedINSPECTION FOUND A 6 INCH CRACK IN TAIL COMPARTMENT STRAP CAP AT STA 1446, LONGERONS 2R/2L. THE STRAP CAP WAS REMOVED AND REPLACED IAW SRM 51-30-2.Sep 8, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100844Floor Support · corrodedINSPECTION FOUND UPPER SURFACE OF CENTER FLOOR SUPPORT CORRODED AT STA 1287-1307. THE CENTER FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01, FIGURE 2.Sep 7, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100842Splice · crackedINSPECTION FOUND A .75 INCH CRACK ON LONGERON SPLICE AT L28L BETWEEN STA 218 AND 229. THE LONGERON SPLICE WAS REMOVED AND A NEW SPLICE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.Sep 7, 2001 · N15820 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100835Seat Track · corrodedINSPECTION FOUND L/H O/B SEAT TRACK AT GALLEY MOUNT STA 1174 AND L/H CENTER SEAT TRACK AT GALLEY MOUNT STA 1193 CORRODED. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW SRM 51-30-01.Sep 6, 2001 · N15820 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900437Pipe · dentedTAIL CONE RELEASE CABLE GUIDE TUBE LOWER RIGHT HAS SEVERAL DAMAGED AREAS, DENTS, AND SHARP CREASES. REMOVED AND REPLACED PIPE ASSY PER MM 53-50-00.Apr 25, 1999 · N15820 · Doug DC982 · Aerodynamic FairingsSDR CALA9900436Cable · frayedUPPER LEFT TAILCONE RELEASE CABLE WORN AND FRAYED WHERE IT PASSES OVER UPPER PULLY. REMOVED AND REPLACED PULLY PER MM 53-53-00.Apr 25, 1999 · N15820 · Doug DC982 · Aerodynamic FairingsSDR CALA9900435Latch · wornUPPER LEFT TAIL CONE LATCH HAS DEEP INDENTATIONS ON BOTH SIDES. REMOVED AND REPLACED LATCH. PERFORMED FUNCTIONAL TEST PER CARD 08-5350-1-0008.Apr 25, 1999 · N15820 · Doug DC982 · Aerodynamic FairingsSDR CALA9900434Latch · wornUPPER RIGHT TAIL CONE LATCH HAS DEEP INDENTATIONS ON BOTH SIDES. REPLACED LATCH PIN, RIGGED CABLES PER MM 53-33-00 AND TESTED TAIL CONE PER CARD 08-5350-1-0008.Apr 25, 1999 · N15820 · Doug DC982 · Aerodynamic FairingsSDR CALA9900441Pan · crackedHI-SHEAR HOLE IS CRACKED (.25) IN FWD BAG BIN DOOR. FABRICATED AND INSTALLED STRAP PER EC/RA 5230-01462.Apr 23, 1999 · N15820 · Doug DC982 · Cargo/Baggage DoorsSDR CALA9900431Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD END OF FORWARD SERVICE DOOR NR 4 BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.Apr 22, 1999 · N15820 · Doug DC982 · Service DoorsSDR CALA9900430Gusset · crackedINSPECTION FOUND A .5 INCH CRACK IN GUSSET AT FORWARD END OF NR 1 BEAM ON FORWARD SERVICE DOOR. A NEW GUSSET WAS INSTALLED IAW SRM 51-30-5.Apr 22, 1999 · N15820 · Doug DC982 · Service DoorsSDR CALA9900427Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN HOLD OPEN HOOK CUTOUT OF FORWARD ENTRY DOOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 20A.Apr 20, 1999 · N15820 · Doug DC982 · Passenger/Crew DoorsSDR CALA9900426Beam · crackedINSPECTION FOUND A .5 INCH CRACK AT FORWARD AND AFT ENDS OF MAIN CABIN DOOR NR 1 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.Apr 19, 1999 · N15820 · Doug DC982 · Passenger/Crew DoorsSDR CALA9900425Jamb · corrodedINSPECTION FOUND THE FORWARD CARGO DOOR JAMB LOWER PAN SECTION CORRODED. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 44.Apr 19, 1999 · N15820 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9900422Seat Track · corrodedINSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 200-265. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-05.Apr 16, 1999 · N15820 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900421Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL OF FORWARD ENTRY DOOR JUST AFT OF INTERNAL DOOR HANDLE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-1 AND 51-30-2.Apr 16, 1999 · N15820 · Doug DC982 · Passenger/Crew DoorsSDR CALA9900420Skin · dentedINSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 237 BETWEEN LONGERON 17L AND 18L. THE SKIN AND LOWER SECTION OF FINGER DOUBLER WERE REPLACED IAW ECRA 5330-02445.Apr 16, 1999 · N15820 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900416Angle · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT Z-ANGLE CORRODED AROUND HI SHEARS. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63.Apr 15, 1999 · N15820 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9900411Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 383 BETWEEN L30 AND L29R. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 22.Apr 14, 1999 · N15820 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900389Spacer · corrodedINSPECTION FOUND MAIN BAGGAGE BIN Z-ANGLE CORRODED ON REPAIR SPACER AT STA 636 TO 693. THE SPACER WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 63.Apr 12, 1999 · N15820 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9700637Prox Sensor · damagedTHE GEAR DOOR OPEN LIGHT REMAINED ON WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH. A GO-AROUND WAS PERFORMED WHILE COMPLYING WITH ABNORMAL PROCEDURES. THE GEAR DOOR OPEN LIGHT REMAINED ON. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE D1-30May 4, 1997 · N15820 · Doug DC982 · Landing Gear Position and WarningSDR CALA9700548Skin · dentedINSPECTION FOUND A 2.75 INCH LONG BY .25 INCH DEEP DENT IN LT FUSELAGE SKIN AT STA 664 BETWEEN LONGERON 22L AND 23L. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38.Apr 9, 1997 · N15820 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9700549Jamb · corrodedINSPECTION FOUND MAIN BAGGAGE BIN DOORWAY JAMB BEAM CORRODED AROUND SEVERAL HI-SHEARS. THE CORROSION WAS REMOVED, DOUBLERS WERE INSTALLED IAW SRM 53-05, FIGURE 63.Apr 7, 1997 · N15820 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9700550Angle · crackedINSPECTION FOUND A .75 INCH CRACK IN LT WING LEADING EDGE RIB ANGLE JUST OUTBOARD OF 8L SLAT TRACK AT STA XRS 276. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.Apr 4, 1997 · N15820 · Doug DC982 · Wing Miscellaneous StructureSDR CALA9700444Actuator Link · brokenTHE LT MLG UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. THE GEAR WAS CYCLED, BUT THERE WAS NO CHANGE IN INDICATION. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG ACTUATOR LOWER LMar 31, 1997 · N15820 · Doug DC982 · Landing Gear ActuatorSDR CALA9601332Air Cyc Mach · inoperativeSMOKE ENTERED THE CABIN DURING TAXI OUT. THE AIRCRAFT WAS RETURNED TO THE GATE. THE AIR COND TURBINE NOZZLE C/B POPPED WHEN COLDER POSITION SELECTED. MAINTENANCE FOUND WIRING CHAFING/SHORTING TO RT TURBINE NOZZLE SHUTOFF VALVE. THE WIRING WAS SPLICED AND TSep 26, 1996 · N15820 · Doug DC982 · Cabin Cooling SystemSDR CALA9600659Control Valve · stuck openSTRONG FUMES WERE REPORTED IN THE CABIN AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A BURN-OUT PROCEDURE PER MM 21-20-02, PARAGRAPH 7C. THE RT CABIN TEMP CONTROL VALVE WAS FOUND STUCK IN TMay 29, 1996 · N15820 · Doug DC982 · Cabin Cooling System
Back to N15820, cancelled Mar 21, 2013