N331CA

Service difficulty reports · 284

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 = 'N331CA' AND registry_match = 'registration'
  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 V0XD20180521001Seat Track · corrodedNR 1 SEAT TRACK, BS 350 - 485 WAS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.May 17, 2018 · N331CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR V0XD20150516002Gusset · corrodedGUSSET AT BS 319.7, STRINGER 21R HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE GUSSET IAW SRM 53-21-23, 51-42-06, 51-40-11, 51-42-21, 51-25-16, AND 51-21-11.May 12, 2018 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20180517004Intercostal · corrodedINTERCOSTAL BETWEEN FS 310.00 AND 319.00 IS CORRODED. REMOVED AND REPLACED INTERCOSTAL(PN:SH670-32047-1) IAW SRM 51-21-23, 51-42-21, 51-42-06, 51-40-11, 51-21-11, 51-25-16, ESPM 20-23-01, AND 20-12-00May 11, 2018 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20180517003Frame · corrodedFRAME 319.70 AT STGR 20R IS CORRODED. REMOVE AND REPLACED FRAME 319.70(PN: SH670-32029-3) IAW SRM 51-42-21, 51-40-11, 51-21-11, 51-42-06, 51-42-13, AND 51-25-16.May 11, 2018 · N331CA · Cndair CL6002C10 · Fuselage Main, StructureSDR V0XD20180517008Angle · corrodedKICK ANGLE SHOWING SIGNS OF CORROSION ON THE SERVICE DOOR. REMOVED AND REPLACED THE KICK ANGLE IAW SRM 51-42-06, AND 51-42-21.May 8, 2018 · N331CA · Cndair CL6002C10 · Service DoorsSDR V0XD20180514009Baffle · crackedLEFT LOWER TRANSCOWL BAFFLE IS CRACKED. REMOVED AND REPLACED THE BAFFLE IAW SRM 51-42-06.May 5, 2018 · N331CA · Cndair CL6002C10 · Engine Exhaust SystemSDR V0XD2018052100002Fitting · corrodedFOUR EACH FITTINGS AT SERVICE DOOR THRESHOLD HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE FITTINGS ON THE SERVICE DOOR THRESHOLD IAW SRM 53-21-23, 51-42-21, 51-40-11, 51-25-16, 51-42-06, AND AMM 53-21-27.May 3, 2018 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20180519001Strap · corrodedRT WING TO BODY EYEBROW PANEL ATTACHMENT STRAP HAS SIGNS OF CORROSION. REPLACED RT WING TO BODY EYEBROW PANEL ATTACHMENT STRAP IAW SRM 51-42-13, 51-42-06.May 2, 2018 · N331CA · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR V0XD20180517009Cap · corrodedSERVICE DOOR SURROUND STRUCTURE MID CAP HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE CAP IAW SRM 51-42-06, AND 51-42-21.May 2, 2018 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20180514004Structure · gougedRIGHT AILERON UPPER LEADING EDGE FOUND GOUGED. REPAIRED AILERON, PERFORMED NDT, AND RESTORED THE FINISH IAW REO 670-57-61-279 REV --.May 1, 2018 · N331CA · Cndair CL6002C10 · AileronsSDR V0XD20180517011Door Sill · corrodedGALLEY SERVICE DOOR SILL AND SILL LIP HAVE SIGNS OF CORROSION. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-06, AND 51-42-21.Apr 30, 2018 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20180516001Fitting · corrodedFRAME BS 319.7 FITTING AT STRINGER 18R HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-21, 51-40-11, 51-25-16, 51-21-11, AND 53-21-23.Apr 30, 2018 · N331CA · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR V0XD20180514008Door Sill · corrodedAFT CARGO DOOR SILL HAS SIGNS OF CORROSION AT SEVERAL AREAS. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-06, 51-42-21, 51-40-11, 51-42-13, 51-25-16, 51-21-11, AND 53-61-23.Apr 30, 2018 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20180514007Strap · crackedAFT WING TO BODY FAIRING STRAP CRACKED. REMOVED AND REPLACED THE STRAP IAW SRM 51-26-00, AND 51-42-10.Apr 30, 2018 · N331CA · Cndair CL6002C10 · Aerodynamic FairingsSDR V0XD20180517010Tripler · gougedAFTER FUSELAGE, BS 977, STRINGER 27, TRIPLER GOUGED. REMOVED AND REPLACED THE TRIPLER IAW REO 670-53-61-56,2 REV A.Apr 29, 2018 · N331CA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR V0XD20180514006Floorbeam · corrodedBS 280 FLOORBEAM HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06, 51-42-13, 51-42-21, AND 53-11-41.Apr 29, 2018 · N331CA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR V0XD20180514003Seat Track · corrodedRIGHT NR 2 SEAT TRACK HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.Apr 29, 2018 · N331CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR V0XD20180514002Support Bracket · corrodedAFT LOWER FUSELAGE WING TO BODY FAIRING SUPPORT L BRACKET AT BS 939.00 AND STGR 27 HAS SIGNS OF CORROSION. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-42-06.Apr 29, 2018 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20180514001Seat Track · corrodedLEFT AND RIGHT INBD NR 3 SEAT TRACKS HAVE SIGNS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-013, AND AMM 53-00-49. Apr 29, 2018 · N331CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR V0XD20180514005Floorbeam · crackedFLOORBEAM ANGLE AT RBL 26, BS 280 CRACKED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06, 51-42-13, AND 51-25-16.Apr 27, 2018 · N331CA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR 2016F00207Bracket · out of positionTWO MISLOCATED BRACKETS ON STRINGER 14R BETWEEN BS 1015 AND 1031. REPAIRED IAW REO 670-53-61-1277.Oct 12, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR 2016F00204Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM AT LBL 9.00 BS 1031. NO DAMAGE ALLOWED IN THIS AREA.Oct 9, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR N6WA2016062502Handle · defectivePASSENGER OUTER DOOR HANDLE CAUTION MSG INTERMITTENT DURING FLT. DEFERRED PASSENGER OUTER DOOR HANDLE IAW MEL 52-70-01, CAT A.Jun 25, 2016 · N331CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR V0XD20160428088Stringer · corrodedSTRINGER 26L IS CORRODED, BETWEEN FS 333 & 349. R & R STRINGER IAW SRM 51-42-06 & 51-42-21.Apr 26, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR V0XD20160428087Intercostal · corrodedMAIN AVIONICS DOOR SURROUND STRUCTURE FWD LT INBD INTERCOSTAL HAS CORROSION. R & R INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.Apr 26, 2016 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20160427083Frame · corrodedFS 364 FRAME IN AVIONICS BAY IS CORRODED. CUT OUT DAMAGED SECTION OF FRAME. CUT & INSTALLED NEW SECTION OF FRAME WITH REPAIR SPLICES & DOUBLERS IAW REO 670-53-21-687 DATED 03 AUG 2012 & REO 670-53-21-1291 DATED 26 APR 2016.Apr 26, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, FrameSDR V0XD20160427082Stringer · corrodedSTRINGER 26R IN AVIONICS BAY IS CORRODED, BETWEEN FS 333 & 349.00. R & R STRINGER 26R IAW SRM 51-42-06 & 51-42-21.Apr 26, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR V0XD20160428089Intercostal · corrodedMAIN AVIONICS DOOR SURROUND STRUCTURE AT FS 364, FWD RT INBD INTERCOSTAL HAS CORROSION. R & R INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.Apr 25, 2016 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20160427085Frame · corrodedFS FRAME 319 IS CORRODED, BETWEEN STRINGER 25L & 26R. CUT OUT DAMAGED SECTION OF FRAME 319, FROM STRINGER 25L - 26R. CUT & INSTALLED NEW FRAME SECTION, PN SH670-31355-1S, WITH REPAIR PARTS IAW REO 670-53-21-799 DATED 30 JAN 2012.Apr 25, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, FrameSDR V0XD20160427084Frame · corrodedFS 295 FRAME IS CORRODED, BETWEEN STRINGER 25L & 26L, BETWEEN 25R & 24R, & BETWEEN 27R & 26R. CUT OUT DAMAGED SECTION OF FRAME 295, FROM 25L TO 25R. CUT & INSTALLED NEW SECTION OF FRAME WITH REPAIR PARTS IAW REO 670-53-21-799 DATED 30 JAN 2012.Apr 25, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, FrameSDR V0XD201604026080Skin · corrodedCORROSION ON INNER FUSELAGE SKIN AT FRAME 364 & STRINGER 26R. REMOVED CORROSION, REMAINING MATERIAL OUT OF LIMITS, FABRICATED AND INSTALLED SHIM IAW REO 670-53-1290 DATED 4 21 16 & SRM 53-21-01 & 53-00-00. NDT PERFORMED.Apr 25, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR V0XD201604025078Door Sill · corrodedFORWARD RT FLOOR SILL HAS SIGNS OF CORROSION. REMOVED RT FLOOR SILL & INSTALLED SERVICEABLE SILL IAW SRM 51-42-06, 51-42-13 & 51-42-21.Apr 25, 2016 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD201604025076Handle · corrodedPASSENGER DOOR, EXTERNAL HANDLE FLAPPER DOOR IS CRACKED. REMOVED PAX DOOR EXTERNAL FLAPPER DOOR HANDLE & INSTALLED SERVICEABLE PAX DOOR EXTERNAL FLAPPER DOOR HANDLE IAW AMM 51-42-06, 51-40-11 & 20-60-06.Apr 25, 2016 · N331CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR V0XD201604025075Fitting · corrodedGALLEY 2 HAS ONE CORRODED FOOT. REMOVED CORRODED GALLEY 2 FOOT. INSTALLED SERVICEABLE FOOT IAW AMM 20-21-00.Apr 25, 2016 · N331CA · Cndair CL6002C10 · Buffet/GalleysSDR V0XD201604025074Fitting · corrodedGALLEY 1 HAS TWO CORRODED FEET. REMOVED GALLEY 1 CORRODED FEET & DOUBLERS. INSTALLED SERVICEABLE FEET & DOUBLERS IAW CMM 25-33-42.Apr 25, 2016 · N331CA · Cndair CL6002C10 · Buffet/GalleysSDR V0XD201604026081Panel · gougedLEFT LOWER COWL GANG DRAIN PANEL GOUGED. BLENDED DAMAGE, FOUND TO BE OUT OF LIMITS. FABRICATED & INSTALLED DOUBLER IAW SRM 54-23-00, 51-42-06, 51-25-06 & AMM 51-21-10. NDT PERFORMED.Apr 24, 2016 · N331CA · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous StructureSDR V0XD201604025077Stringer · damagedSTRINGER 7L IN AFT EQUIPMENT BAY HAS BROKEN BRACKET & CHAFE DAMAGE. ACCOMPLISHED MAJOR REPAIR TO STRINGER 7L AT FRAME STATION 1144.00 CHAFE DAMAGE BY REMOVING DAMAGED STRINGER, PERFORMING NDT, FABRICATING REPAIR PARTS & INSTALLING A NEW STRINGER & REPAIR PARTApr 24, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR V0XD201604025073Floorbeam · corrodedRIGHT & LEFT 280 BEAM IS CORRODED. ACCOMPLISHED PERMANENT REPAIR TO THE BEAM TO CORRECT CORROSION, BY R & R THE LT & RT 280 BEAMS IAW SRM 51-42-21, 53-11-41, 51-42-13, 53-11-41, 51-40-11, 51-42-22 & AMM 20-70-00 & SB 670-BA-53-026 REV B DATED 05 2006. NDT PEApr 23, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR V0XD201604025071Angle · corrodedAFT COCKPIT 1/4 TURN ANGLE IS CORRODED. REMOVED AFT COCKPIT 1/4 TURN ANGLE, PN CC670-33292-13S, & INSTALLED SERVICEABLE AFT COCKPIT 1/4 TURN ANGLE IAW SRM 51-42-06, 51-42-13 & 51-40-11.Apr 23, 2016 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20160425069Bulkhead · corrodedFS 280 BULKHEAD WEBS, LT & RT ARE CORRODED. REMOVED DAMAGED AREA, FABRICATED & INSTALLED REPAIR PARTS IAW REO 670-53-11-594 & SRM 51-42-06.Apr 23, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, BulkheadSDR V0XD201604025079Floorbeam · corrodedFLOORBEAM AT LBL 27, BETWEEN FS 1015 & 1031 IS CORRODED. ACCOMPLISHED MAJOR REPAIR TO THE FLOORBEAM BY CUTTING OUT CORRODED SECTION, PERFORMING NDT, FABRICATING REPAIR PARTS & INSTALLING THEM IAW REO 670-53-00-029 REV A DATED 2010 08 31 & AMM 51-21-01, 20-70-Apr 22, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR V0XD201604025072Angle · corrodedPASSENGER DOOR FWD & AFT CLOSE OUT ANGLES HAVE SIGNS OF CORROSION. REMOVED FWD CLOSE OUT ANGLE & INSTALLED SERVICEABLE CLOSE OUT ANGLE. AFT CLOSE OUT ANGLE DAMAGE FOUND TO BE IN PAINT, PRIMED & TOP COATED IAW SRM 51-42-21, 51-42-06, 51-25-06, 51-25-16 & 53-2Apr 20, 2016 · N331CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20160420068Angle · corrodedPASSENGER DOOR FWD & MID-CAPS HAVE SIGNS OF CORROSION. R & R PAX DOOR FWD & MID-CAPS, PN SH670-31821-5 & PN SH670-31825-9S, IAW SRM 51-42-06, 51-41-02, 51-41-00 & 51-40-11. WO 80394, WC 8067.Apr 20, 2016 · N331CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR V0XD20160419067Stringer · corrodedSTRINGER 25R IN MAIN AVIONICS COMPARTMENT, BETWEEN FS 295 & 333 HAS SIGNS OF CORROSION. R & R STRINGER 25R IAW SRM 51-42-06 & 51-42-21. WO 80394 & WC 1126.Apr 18, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR V0XD20160419066Doubler · gougedTHE DOUBLER & TRIPLER FROM PREVIOUS REPAIR AT FS 977, LOWER FUSELAGE SKIN IS GOUGED. REMOVED EXISTING REPAIR PARTS. FABRICATED DOUBLER & TRIPLER & INSTALLED IAW REO 670-53-61-562 REV-A DATED 01 MAR 2010. ADDITIONALLY ACCOMPLISHED MODSUM IS670538200021, REV Apr 16, 2016 · N331CA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR N6WA2015112202Wire Harness · disconnectedCEILING EMER LIGHT AT ROW 15 INOPERATIVE. CONNECTED HARNESS TO PLUG. OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM 33-51-00.Nov 22, 2015 · N331CA · Cndair CL6002C10 · Light System WiringSDR N6WA2015102901Warning System · false activationPASSENGER DOOR CAUTION MSG ON LANDING. PERFORMED INSPECTION OF THE PAX DOOR PROXIMITY SENSORS & PROXIMITY SWITCH IAW AMM 52-70-04. PERFORMED OPERATIONS CHECK IAW AMM 52-70-00. OPERATIONS CHECKED GOOD.Oct 29, 2015 · N331CA · Cndair CL6002C10 · Door Warning SystemSDR N6WA2015070802Light · inoperativeOVERHEAD EMER LIGHT OUT AT ROW 9. DEFERRED CEILING LIGHT AT ROW 9 IAW MEL 33-51-01B.Jul 8, 2015 · N331CA · Cndair CL6002C10 · Emergency LightingSDR N6WA2015062201Door · openGPU DOOR OPEN IN FLIGHT. PERFORMED INSPECTION OF GPU DOOR & SURROUNDING AREA IAW AMM 05-21-00. ZONAL INSPECTION, NO DEFECTS OR DAMAGE NOTED AT THIS TIME.Jun 22, 2015 · N331CA · Cndair CL6002C10 · Service DoorsSDR N6WA2015060801Connector · dirtyGLD UNSAFE CAUTION ON TAKEOFF. CLEANED ANTENNA COAX CONNECTORS. PERFORMED BIT TEST. OPERATIONS CHECKED GOOD IAW AMM 34-44-01.Jun 8, 2015 · N331CA · Cndair CL6002C10 · Navigation System Wiring
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