N781CA, cancelled Jul 30, 2023

Service difficulty reports · 162

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 = 'N781CA' AND deregistration_id = 'N781CA-2023-07-30'
  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 ASOA201901145012Connector · contaminatedIN CRUISE AT FL350 RT PACK HI TEMP CAUTION MESSAGE DISPLAYED FOLLOWED BY LOSS OF CABIN PRESSURE. STARTED DESCENT TO 10000FT PASSENGER O2 MASKS DEPLOYED AS CABIN CLIMBED TO 15000 AUTO PRESS 1 AND 2 FAIL MESSAGES DISPLAYED. SUPPLEMENTAL INFORMATION UPON FURTHER Jan 14, 2019 · N781CA · Cndair CL6002B19 · Air Conditioning System WiringSDR ASOA201811025309Skin · corrodedLOWER WING PLANK SKIN CUTOUT RH BOOST PUMP HAS MULTIPLE INDICATIONS NOTED AROUND ENTIRE CIRCUMFERENCE ON HORIZ LANDING FOR PNL AND VERTICAL SURFACES 50% FSH FAILED NDT INSP. C/W CARD REO 601R-57-21-2884 BLENDED CORROSION.Nov 2, 2018 · N781CA · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2018110625308Bushing · failedREF:CO# 7312618 JOB#7731265A OP#9 L/H ELEVATOR FAILED BEARING BACKLASH SYSTEM NO.1 AT .230 AND SYSTEM NO.3 AT .232, MAX LIMIT IS .210. C/A REPAIRED L/H ELEVATOR IAW EXPRESSJET EC/TC RIL#0183 AND BOMBARDIER RIL# 0183 REV B, DATED 01/24/2014. REPLACED BUSHINGS ANov 2, 2018 · N781CA · Cndair CL6002B19 · Elevator StructureSDR ASOA201810315307Floorbeam · corrodedAFT CABIN FLOORBEAM HAS CORROSION ON UPPER SURFACE FS 559.00 RBL 9.0. COMPLIED WITH EC/TC REO 601R-53-41-2379 AND GENERIC REO 601R-53-41-2379 DATED: 10/29/2018.Oct 31, 2018 · N781CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201810305306Floorbeam · corrodedLBL 27 UPPER FLOORBEAM CAP FROM FS 574 TO FS 621 IS CORRODED. REPAIRED UPPER FLOORBEAM CAP IAW REO 601R-53-61-6743 REV -, ECTC REO 601R-53-61-6743 REV 0, REO 601R-53-61-3778, AND ECTC REO 601R-53-61-3778 REV C.Oct 30, 2018 · N781CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201810305305Skin · dentedDENT AT FS 582 STR 22L APPROX L 1.7" W 1.0" D .015". REPAIRED DENT AT FS 582 STR 22L IAW EA 32-2018-225 AND ECTC EA 32-2018-225 REV 0.Oct 30, 2018 · N781CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201810305304Skin · dentedDENT FOUND AT FS 409+16 ON STR 16L APPROX L=2", W=1.5, D=.012". REPAIRED DENT AT FS 409+16 AT STR 16L IAW EA 30-2018-231 AND ECTC EA 30-2018-231 REV 0.Oct 30, 2018 · N781CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2018110295301Sidewall Support · corrodedLEFT CARGO SIDEWALL SUPPORT HAD CORROSION BS 559+83, LBL 36. REPAIRED THE SIDEWALL SUPPORT IAW SNIEO 601R31133-S04, AND SNIEO CC601R31133 S04.Oct 29, 2018 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2018110295300Floor Support · corrodedCABIN LEFT SIDE FLOOR SUPPORT HAD SIGNS OF CORROSION, BS 409 - 409+16 AND 409+110. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-00-530, REV A, EC/TC 601R-53-00-530, REV A, REO 601R-53-00-708 REV --, AND EC/TC REO 601R-53-00-708 REV --.Oct 29, 2018 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201810295299Frame · corrodedAFT CARGO AREA HAS CORROSION BELOW FLOOR, FS 605.00, LBL 6.0 LOWER FRAME FLANGE. REMOVED AND REPLACED FRAME IAW SRM 51-40-11, 51-42-06, CC 601R36026 S01 AND EC/TC CC 601R36026 S01.Oct 29, 2018 · N781CA · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201810295298Not Reported · wornRT ELEVATOR FAILED BEARING BACKLASH SYSTEM NR 3 AT .285. MAX LIMIT IS .210. REPAIRED RT ELEVATOR IAW EC/TC RIL 0183 AND RIL 0183 REV B, DATED 01/24/2014.Oct 29, 2018 · N781CA · Cndair CL6002B19 · Elevator Miscellaneous StructureSDR ASOA201810295297Bulkhead · chafedFS 621 BULKHEAD FWD FACE HAS DAMAGE AROUND FASTENER HOLE AT LBL44, 18" ABOVE FLOOR LEVEL. REPAIRED FS 621 BULKHEAD FWD FACE IAW REO 601R-53-61-2155 REV -A, DATED 2013-08-13 AND EC/TC REO 601R-53-61-2155.Oct 29, 2018 · N781CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201810295296Bulkhead · gougedFS 621 BULKHEAD FWD FACE HAS 1 LIGHT GOUGE AT LBL 14, 3" ABOVE FLOOR LEVEL AND APPROX. .5" LONG. REPAIRED FS 621 BULKHEAD FWD FACE IAW REO 601R-53-61-2155 REV -A, DATED 2013-08-13 AND EC/TC REO 601R-53-61-2155.Oct 29, 2018 · N781CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2018110185293Skin · crackedREF: CO# 7312618 JOB# 7731265 OP# 25: LOWER WING PLANK ACCESS HOLE HAS MULTIPLE INDICATIONS NOTED IN THE LANDING FOR PANEL 650D B AT FWD AND AFT AREA, BOTH AREAS ARE 4" LONG BY 0.250" WIDE BY 50% SCREEN HEIGHT. FAILS NDT.C/A: REPAIRED IAW BOMBARDIER REO 601R-Oct 28, 2018 · N781CA · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2018110185292Skin · crackedREF: CO# 7312618 JOB# 7731265 OP# 26: LOWER WING PLANK ACCESS HOLE HAS MULTIPLE INDICATIONS NOTED IN THE LANDING FOR PANEL 640AB AT FWD AND AFT AREA, BOTH AREAS ARE 4" LONG BY 0.250" WIDE BY 50% SCREEN HEIGHT. FAILS NDT. C/A: REPAIRED IAW BOMBARDIER REO 601R-Oct 28, 2018 · N781CA · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA201810195279Hinge · wornRUDDER BACKLASH FAILED. SYSTEM NR 1 PCU AT 0.312" AND SYSTEM NO.3 PCU AT 0.340". BEARING FAILED AT 0.170". REPAIRED RUDDER SYSTEM BACKLASH IAW RIL'S 0602, 0392 AND EC/TC 0602 AND 0392. RUDDER BACKLASH PERFORMED IAW AMM 27-21-00-220-810. BACKLASH CHECK PASSED.Oct 19, 2018 · N781CA · Cndair CL6002B19 · Rudder StructureSDR ASOA2018101965267Door Sill · corrodedREF: CO 7312618 JOB 7731268 OP 30: LT AFT CARGO DOOR SILL CORRODED. C/A: REPAIRED LT AFT CARGO DOOR SILL IAW REO 601R-53-00-526 REV— DATED 22 MAY 2013 AND ECTC REO 601R-53-00-526.Oct 16, 2018 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2018101955266Skin · dentedREF: CO 7312618 JOB 7731265 OP 7022: FROM MX TRANS 17250131 DENT UNDER CARGO DOOR. COMPLIED WITH REO 601R-53-61-6255. COMPLY WITH LPI WITHIN 50FH, AND REINSPECT EVERY 300FH. PERMANENT REPAIR DUE IN 2800 FH BY TAT42138.8. ACCOMPLISH PERMANENT REPAIR PER REO 601Oct 15, 2018 · N781CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2018101995262Door Sill · corrodedREF: CO 7312618 JOB 7731268 OP 22: RT CARGO FLOOR SIDE SILL 559.00+80 TO FS 578.00, RBL 36.0 HAS CORROSION AROUND NUTPLATES. C/A: COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GENERIC REO 601R-53-00-526 REV. --, DATED: 05/22/2013 AS WRITTEN.Oct 9, 2018 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2018101995261Skin · chafedREF: CO 7312618 JOB 7731261 OP 79: CENTER WING LOWER PLANK IS CHAFED AT LBL45 & RBL45 FROM CONTACT WITH BELLY FAIRING 193AB. C/A: COMPLIED WITH EC/TC REO 601R-57-21-880 IN ACCORDANCE WITH REO 601R-57-21-880 REV. D, DATED: 03/06/2017 AS WRITTEN.Oct 9, 2018 · N781CA · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA201810075257Intercostal · corrodedMAIN AVIONICS DOOR SURROUND STRUCTURE HAS CORROSION AT TWO FWD INTERCOSTALS LBL 2.0, RBL 2.0 AND ONE AFT INTERCOSTAL RBL 2.0 FS 364 - 394. FRAME STATION 280.00 FWD J ANGLE IS CORRODED. REMOVED AND REPLACED ONE AFT INTERCOSTAL RBL 2.0 FS 364 - 394 IAW SRM 51-42Oct 7, 2018 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201810075256Cargo Track · corrodedCARGO FLOOR TRACKS AT FS 559.00+112 HAVE CORROSION, LBL 9.00 AND RBL 9.00. REMOVED AND REPLACED TRACKS IAW EC/TC REO 601R-53-00-485 AND GENERIC REO 601R-53-00-485 REV D, DATED 01/29/2018.Oct 7, 2018 · N781CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201810075255Cargo Track · corrodedCARGO TRACKS CORRODED FS 559.00+90, LBL 9.0, RBL 9.0 AND RBL 27.00. REMOVED AND REPLACED TRACKS IAW EC/TC REO 601R-53-00-485 AND GENERIC REO 601R-53-00-00485 REV D, DATED 01/29/2018.Oct 7, 2018 · N781CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201810045254Angle · corrodedFRAME STATION 280.00 FWD J ANGLE IS CORRODED. INSTALLED NEW SERVICEABLE FWD J ANGLE IAW SRM 51-42-21, 51-42-06, 51-44-06, 51-25-16.Oct 4, 2018 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2018100595242Bracket · corrodedREF: CO 7312618 JOB 7731268 OP 16: PAX DOOR BRACKET AND CLEAT CORRODED AT FS 343.00, LBL 33. C/A: REMOVED AND REPLACED BRACKET IAW SRM 51-42-06, 51-42-11 AND 51-42-10.Sep 29, 2018 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201809235310Fitting · crackedRT 484 FRAME O/B CLIP IS CRACKED. REPAIRED IAW REO 601R-53-41-2376 REV - DATE 2018-10-19.Sep 23, 2018 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2018100535241Strap · corrodedREF: CO 7312618 JOB 7731261 OP 158: CORROSION ON FLOOR PNL STRAP AT LT AFT EDGE OF PRESSURE BOX AT FS 559.0. C/A: FABBED AND REPLACED STRAP IAW SRM 53-41-43, 51-40-11, 51-25-01 AND 51-42-06.Sep 23, 2018 · N781CA · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2018100535240Seat Track · corrodedREF: CO 7312618 JOB 7731261 OP 205: WALL SEAT TRACK ON RT SIDE FROM FS 500 TO FS 545 CORRODED. C/A: REMOVE, FABBED AND REPLACED SEAT TRACK IAW REO 601R-53-00-485.Sep 23, 2018 · N781CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2018100535239Seat Track · corrodedREF: CO 7312618 JOB 7731261 OP 204: WALL SEAT TRACK ON RT SIDE FROM FS 449 TO FS 500 CORRODED. C/A: REMOVE, FABBED AND REPLACED SEAT TRACK IAW REO 601R-53-00-485.Sep 23, 2018 · N781CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201642343Floor Support · corrodedLEFT CABIN FLOOR SUPPORT AND ANGLE BETWEEN BS 518 AND 527. REPAIRED THE FLOOR SUPPORT AND ANGLE IAW REO.Jul 1, 2016 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642341Structure · bentFWD AND AFT LANDS FOR THE GROUND AIR CONDITIONING DOOR BENT. REPAIRED FWD AND AFT LANDS FOR THE GROUND AIR CONDITIONING DOOR IAW EA.Jul 1, 2016 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642338Floorbeam · corrodedFLOORBEAM AT BS 349 BETWEEN RBL 27 AND 38 HAS CORROSION BEYOND LIMITS. REPAIRED THE FLOORBEAM IAW EA.Jun 28, 2016 · N781CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201642339Angle · corrodedCARGO DOOR AFT LOWER ANGLE BEHIND COMBING IS CORRODED. THE ANGLE WAS REMOVED AND NEW ANGLE P/N: 600-35011-45 INSTALLED IAW SRM.Jun 21, 2016 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642337Bracket · corrodedCORROSION ON LOWER FRAME BRACKET AT BS 319 STRINGER 17R. REMOVED AND REPLACED LOWER FRAME BRACKET IAW SRM.Jun 20, 2016 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642336Vane · chafedRT INBOARD FLAP CENTER VANE CAP CHAFED. REMOVED AND REPLACED THE VANE CAP IAW SRM.Jun 19, 2016 · N781CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642333Vane · chafedL/H INBOARD FLAP CENTER VANE CAP CHAFED. REMOVED AND REPLACED THE VANE CAP IAW SRM.Jun 19, 2016 · N781CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642344Floor Support · corrodedRIGHT SIDE FUSELAGE INTERIOR FLOOR SUPPORT AT BS 349 HAS CORROSION. REPAIRED THE FLOOR SUPPORT IAW EA.Jun 17, 2016 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642335Vane · chafedRIGHT INBOARD FLAP OUTBOARD VANE CAP IS CHAFED. VANE CAP WAS REMOVED AND REPLACED IAW SRM.Jun 17, 2016 · N781CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642342Angle · corrodedGALLEY SERVICE DOOR THRESHOLD AT BS 319, ANGLE HAS CORROSION. REMOVED AND REPLACED THE ANGLE IAW SRM.Jun 16, 2016 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642340Threshold · corrodedPAX DOOR ENTRY THRESHOLD HAS CORROSION AT FWD AND AFT CUPS. INSTALLED FWD AND AFT PAX DOOR ENTRY THRESHOLD CUP IAW SRM.Jun 16, 2016 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642334Floor Support · corrodedLEFT SIDE INSIDE FUSELAGE AT BS 349, CORROSION ON FLOOR SUPPORT. REPAIRED THE FLOOR SUPPORT IAW EA.Jun 16, 2016 · N781CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642332Panel · failedHORIZONTAL STABILIZER VISOR PANEL 326AR FAILED GAP CHECK. REMOVED AND REPLACED IAW SRM.Jun 14, 2016 · N781CA · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR SWIA201642331Housing · gougedEXTERNAL CARGO DOOR HANDLE HOUSING IS GOUGED. A NEW EXTERNAL CARGO DOOR HANDLE INSTALLED IAW AMM AND SRM. OPERATIONAL TESTS GOOD.Jun 13, 2016 · N781CA · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA201642330Skin · dentedTWO DENTS ON THE RT LANDING GEAR DOOR. DRESSED THE DENTS IAW STS EA.Jun 12, 2016 · N781CA · Cndair CL6002B19 · Landing Gear DoorsSDR SWIA201641756Warning Light · illuminatedGEAR DISAGREE ON GEAR RETRACTION. OPENJan 12, 2016 · N781CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201540569Structure · crackedFOUND CRACKED AT BS 640, S9R CUT-OUT. REPAIRED IAW REO.Jan 5, 2015 · N781CA · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201439814Loop · failedRETURNED TO THE FIELD WITH AN ANTI-ICE DUCT WARNING MESSAGE. CHANGED THE RT WHEEL BIN LOOP. OPS CHECKED GOOD.Nov 5, 2014 · N781CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR SWIA201438819Connector · looseNOSE DOOR NOT OPERATING PROPERLY, DID NOT OPEN WITH HYDRAULIC 3A ON. DID OPEN WHEN HYDRAULIC 3A WAS OFF AND PRESSURE DECREASED IN SYSTEM 3. SECURED LOOSE CONNECTOR ON NLG DOOR SELECTOR VALVE. OPS CHECK OF NLG GEAR DOORS GOOD AT THIS TIME IAW AMM.Jul 18, 2014 · N781CA · Cndair CL6002B19 · Landing Gear System WiringSDR SWIA2014062338269Skin · damagedPAX DOOR LOWER INNER SKIN DAMAGED. REPAIRED PAX DOOR INNER SKIN IAW EA.Jun 13, 2014 · N781CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2014062338270Hinge · gougedPAX DOOR HINGE, ACFT SIDE, AFT LUG LAND IS GOUGED. REPAIRED PAX DOOR HINGE IAW EA.Jun 12, 2014 · N781CA · Cndair CL6002B19 · Fuselage, Door Hinge
Back to N781CA, cancelled Jul 30, 2023