N35836, cancelled Jun 29, 2005

Service difficulty reports · 46

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 = 'N35836' AND deregistration_id = 'N35836-2005-06-29'
  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 CALA0500042Seat Track · corrodedINSPECTION FOUND F/O'S AFT O/B SEAT TRACK CORRODED. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-40-01.Feb 6, 2005 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0500041Panel · crackedINSPECTION FOUND A 2 INCH CRACK IN UPPER TRAILING EDGE PANEL LOCATED FORWARD OF O/B SIDE OF GROUND SPOILER, LEFT UPPER WING, XRS 91.0 TO 111.5. A NEW PANEL WAS INSTALLED IAW SRM 51-30-2.Feb 3, 2005 · N35836 · Doug DC982 · Wing, Plate/SkinSDR CALA0500040Door Frame · crackedINSPECTION FOUND A 1.75 INCH CRACK IN NWW LT DOOR JAMB AT UPPER LOCK FASTENER FOR SPRAY DEFLECTOR GUARD, STA 45. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 110.Feb 3, 2005 · N35836 · Doug DC982 · Fuselage Main, StructureSDR CALA0500036Skin · crackedINSPECTION FOUND A 1 INCH CRACK BELOW LOWER FORWARD LATCH OF MID CARGO DOOR SKIN. THE DOOR SKIN WAS REPAIRED IAW SRM 52-05, FIGURE 26A.Feb 1, 2005 · N35836 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0500035Pan · crackedINSPECTION FOUND A .75 INCH CRACK AT CORNER OF LOWER FORWARD INNER PAN OF FORWARD CARGO DOOR. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A.Jan 31, 2005 · N35836 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0500031Floor Panel · delaminatedINSPECTION FOUND LT CENTER FLOOR PANEL DELAMINATED AND HOLES PUNCHED IN PANEL AT STA 465-541, LBL 20 TO LBL 40. A NEW PANEL WAS INSTALLED IAW SRM 53-05, PAGE 122B.Jan 29, 2005 · N35836 · Doug DC982 · Fuselage Floor PanelSDR CALA0500028Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1322 UNDER RT LAV, RBL 20. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 79A.Jan 28, 2005 · N35836 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0500025Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK AT FORWARD O/B END OF FORWARD ENTRY FLOOR SUPPORT TEE AT STA 180, RBL 43. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2.Jan 27, 2005 · N35836 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0500024Seat Track · corrodedINSPECTION FOUND LT MIDDLE SEAT TRACK CORRODED FROM STA 1022-1250, S18L. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 4F.Jan 26, 2005 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0500022Structure · corrodedINSPECTION FOUND SUBFLOOR CORRODED UNDER LEFT O/B SEAT TRACK AT STA 1174, LBL 60. THE CORRODED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-70-4.Jan 26, 2005 · N35836 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0500021Seat Track · corrodedINSPECTION FOUND LEFT I/B CABIN SEAT TRACK CORRODED FROM STA 1022-1250, LBL 25. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4.Jan 24, 2005 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0500020Seat Track · corrodedINSPECTION FOUND CAPTAIN'S AFT I/B SEAT TRACK CORRODED AT STA 83.55 - 101.55, LBL 10. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01.Jan 22, 2005 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0500017Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 180, LBL 12 TO LBL 37. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-2.Jan 21, 2005 · N35836 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0500016Rib · crackedINSPECTION FOUND A .75 INCH CRACK IN RIB AND DOUBLER AT LT WING LEADING EDGE INTERNALLY BETWEEN NR 9 AND NR 10 SLAT TRACK CUTOUTS, STA XRS 324. THE CRACKED RIB AND CLIP ANGLE WERE REMOVED AND A NEW RIB AND CLIP ANGLE WERE INSTALLED IAW SRM 51-10-03, 51-30-02,Jan 21, 2005 · N35836 · Doug DC982 · Wing, Rib/BulkheadSDR CALA0500057Cusp Web · corrodedINSPECTION FOUND RT CUSP CORRODED AT STA 200. A SMALL SECTION OF THE UPPER CUSP CHORD WAS TRIMMED OUT TO REMOVE LOCAL CORROSION AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5311-01216.Jan 20, 2005 · N35836 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0500012Longeron · crackedINSPECTION FOUND A .75 INCH CRACK IN LONGERON 4L AT STA 160. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02 FIGURE 18.Jan 17, 2005 · N35836 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0500009Floor Support · corrodedINSPECTION FOUND CENTER FLOOR SUPPORT BETWEEN I/B AND MIDDLE SEAT TRACKS CORRODED AROUND SCREW HOLES AT LT SIDE STA 1155, BL 0 TO LBL 30. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-01.Jan 16, 2005 · N35836 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100894Clip · out of adjTHE TAILCONE EXTERIOR RELEASE HANDLE PULL FROM CLIPS WAS LOW. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.Sep 23, 2001 · N35836 · Doug DC982 · Aerodynamic FairingsSDR CALA0100893Frame · crackedINSPECTION FOUND A CRACK IN TAIL COMPARTMENT CANTED FRAME AT STA 1446, L3R AN L26L. THE CRACKED FRAME CAP WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.Sep 21, 2001 · N35836 · Doug DC982 · Fuselage Main, FrameSDR CALA0100891Fitting · crackedINSPECTION FOUND A 2.5" CRACK IN R/H WING GROUND SPOILER ACTUATOR FITTING. A DOUBLER WAS INSTALLED IAW ECRA 5740-01317 AND DRAWING SRO9570010.Sep 20, 2001 · N35836 · Doug DC982 · SpoilersSDR CALA0100890Fitting · crackedINSPECTION FOUND A 2.25" CRACK IN L/H WING LEFT I/B GROUND SPOILER ACTUATOR SUPPORT FITTING. REPAIRED IAW ECRA 5740-01317 AND DRAWING SR09570010.Sep 20, 2001 · N35836 · Doug DC982 · SpoilersSDR CALA0100887Door Frame · corrodedINSPECTION FOUND MID BAGGAGE BIN LOWER DOOR JAMB CORRODED AROUND H-SHEAR AT STA 636-693. A REPAIR DOUBLER AND SPACER WERE INSTALLED IAW SRM 53-05, FIGURE 63.Sep 19, 2001 · N35836 · Doug DC982 · Fuselage Main, StructureSDR CALA0100886Door Frame · corrodedINSPECTION FOUND AFT BAGGAGE BIN LOWER DOOR JAMB CORRODED BETWEEN STA 1155-1211. A Z-ANGLE BEAM REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63.Sep 19, 2001 · N35836 · Doug DC982 · Fuselage Main, StructureSDR CALA0000502Acm · leakingWHEN THROTTLES WERE BROUGHT UP FOR TAKEOFF (DURING TAKEOFF ROLL) A NOXIOUS FOUL ODOR ENTERED THE AIRCRAFT THROUGH THE AIR CONDITIONING PACKS. THE CREW AND PASSENGERS BECAME NAUSEOUS. THE FLIGHT CREW DONNED THEIR O2 MASKS AND THE AIRCRAFT WAS RETURNED TO IAH.Apr 18, 2000 · N35836 · Doug DC982 · Cabin Cooling SystemSDR CALA0000141Power Supply · inoperativeINSPECTION FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. A NEW POWER SUPPLY AND BATTERY PACK WERE INSTALLED IAW MM 33-53-00, PAGE 407.Feb 8, 2000 · N35836 · Doug DC982 · Emergency LightingSDR CALA9900538Fairing · gougedLEFT WING NR 4 SLAT TRACK CAN GOUGED. WELDED CAN PER DRWG 5935801 AND INSTALLED PER MM 27-80-01.May 13, 1999 · N35836 · Doug DC982 · Leading Edge DevicesSDR CALA9900527Tail Cone · out of adjustTAIL COMPARTMENT INTERIOR TAIL CONE RELEASE HANDLE PULL TOO HIGH (45 LBS). RIGGED TAIL CONE RELEASE MECHANISM PER MM 53-53-00.May 11, 1999 · N35836 · Doug DC982 · Aerodynamic FairingsSDR CALA9900525Bracket · crackedLEFT FORWARD EMERGENCY EXIT DOOR SEAL RETAINER SUPPORT BRACKET CRACKED AT RIVET (.5). REPLACED FORWARD LOWER RETAINER BRACKET PER SRM 51-30-2.May 11, 1999 · N35836 · Doug DC982 · Emergency ExitsSDR CALA9900523Skin · gougedFUSELAGE SKIN IS GOUGED UNDER AFT END OF ADF ANTENNA. BLENDED GOUGE AND INSTALLED REPAIR PER SRM 53-04 FIG 38 VIEW G.May 11, 1999 · N35836 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900492Retainer · corrodedLEFT FORWARD EMERGENCY EXIT DOOR CORROSION FOUND AT LOWER AFT CORNER SEAL RETAINER. REMOVED AND REPLACED SEAL RETAINER PER SRM 51-30-2.May 8, 1999 · N35836 · Doug DC982 · Emergency ExitsSDR CALA990497Jamb · corrodedFORWARD CORGO DOOR JAMB PAN LOWER SECTION IS CORRODED. INSTALLED SPLICE REPAIR ON DOOR JAMB PER SRM 53-05 FIG 44.May 7, 1999 · N35836 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9900500Doubler · crackedAFT SERVICE DOOR DOUBLER AROUND HOLD OPEN HOOK CRACKED (1) OUTER SKIN. INSTALLED DOUBLER REPAIR PER EC/RA 5205-01008.May 7, 1999 · N35836 · Doug DC982 · Service DoorsSDR CALA9900496Seat Track · corrodedSEAT TRACK NR 2 CORROSION AT NUT PLATE HOLES FROM STA 1136 - 1174. REPLACED SEAT TRACK LEFT CENTER STA 1079 - 1305 PER SRM 51-30-01.May 7, 1999 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900487Seat Track · corrodedLEFT MOST INBOARD SET TRACK HAS CORROSION AT CENTER CHANNEL STA 1105. REMOVED AND REPLACED SEAT TRACK PER SRM 53-05 FROM STA 1041 - 1309.May 5, 1999 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900484Seat Track · corrodedRIGHT CENTER SEAT TRACK CORRODED STA 200 AND 237. REMOVED AND REPLACED SEAT TRACK STA 200 - 247 PER SRM 51-30-1.May 4, 1999 · N35836 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9900470Bulkhead Doubler · corrodedCORROSION AT AFT PRESSURE BULKHEAD AND VERTICAL BULKHEAD INTERSECTION AT STA 1338 FROM L-29LT TO L-29RT. REMOVED CORROSION AND INSTALLED SERVICEABLE JACK PAD DOUBLER PER SRM 51-10-3 AND DRAWING NR PL J936439 AND J936667.May 3, 1999 · N35836 · Doug DC982 · Fuselage Main, BulkheadSDR CALA9900469Skin · holeTEMPORARY REPAIR APPROXIMATELY STA 383 L-29LT WHERE PREVIOUS PHONE ANTENNA INSTALLED. INSTALLED DOUBLERS PER SRM 53-04 FIG 38.May 3, 1999 · N35836 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900467Beam · crackedHOU - FORWARD SERVICE DOOR NR 4 BEAM IS CRACKED AT FORWARD END 1.5 INCH. INSTALLED NEW BEAM PER SRM 51-30-2 AND 51-30-1. (M)Apr 30, 1999 · N35836 · Doug DC982 · Service DoorsSDR CALA9900466Beam · crackedHOU - MAIN CABIN DOOR NR 1 BEAM IS CRACKED AT BOTH ENDS .625 INCH FORWARD AND 1 INCH AFT. REMOVED AND REPLACED BEAM PER SRM 51-30-0. (M)Apr 30, 1999 · N35836 · Doug DC982 · Passenger/Crew DoorsSDR CALA9900465Angle · crackedHOU - RIGHT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-30-2. (M)Apr 30, 1999 · N35836 · Doug DC982 · Vertical StabilizerSDR CALA9900464Angle · crackedHOU - LEFT INNER ATTACH ANGLE CRACKED 1 INCH, DORSAL FIN. REMOVED AND REPLACED ANGLE PER SRM 51-30-2. (M)Apr 30, 1999 · N35836 · Doug DC982 · Vertical StabilizerSDR CALA9900453Escape Line · frayedRIGHT OVERWING EXIT ESCAPE LINE IS FRAYED AT ATTACH HOOK. REPLACED ESCAPE LINE PER MM 25-61-00.Apr 29, 1999 · N35836 · Doug DC982 · Emergency EquipmentSDR CALA9900452Escape Line · frayedLEFT OVERWING EMERGENCY EXIT ESCAPE LINE IS FRAYED AT ATTACH HOOK. REPLACED ESCAPE LINE PER MM 25-61-00.Apr 29, 1999 · N35836 · Doug DC982 · Emergency EquipmentSDR CALA9900223Fuse · blownINSPECTION FOUND MIDDLE SECTION OF SEAT MOUNTED EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND MOST OUTBOARD FUSE OF MIDDLE POWER SUPPLY PACK BLOWN. THE FUSE WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHTING WAS RESTORED.Mar 4, 1999 · N35836 · Doug DC982 · Emergency LightingSDR CALA9601479Slide · fell offFORWARD ENTRY DOOR SLIDE FELL OFF DOOR. REINSTALLED SLIDE PACK PER MAINTENANCE MANUAL.Oct 17, 1996 · N35836 · Doug DC982 · Emergency EquipmentSDR CAL950187T/R Cntl Valve · rupturedSFO - FLT 0165 - THE MAIN CABIN BEGAN TO FILL WITH SMOKE DURING TAXI TO TERMINAL AFTER LANDING AT SFO. THE AIRCRAFT WAS STOPPED ON THE TAXIWAY, THE L-1 DOOR AND TAIL CONE EMERGENCY SLIDES WERE DEPLOYED, AND THE PASSENGERS EVACUATED AS A PRECAUTIONARY MEASURE.Mar 9, 1995 · N35836 · Doug DC982 · Engine Thrust Reverser
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