N984CA, cancelled May 3, 2017

Service difficulty reports · 174

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 = 'N984CA' AND deregistration_id = 'N984CA-2017-05-03'
  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 SWIA201641882Reservoir · failedRETURNED TO DEPARTURE, DUE TO A GEAR DISAGREE. R & R NR 3 HYDRAULIC RESERVOIR IAW AMM. OPS CHECKS GOOD, NO LEAKS NOTED.Feb 12, 2016 · N984CA · Cndair CL6002B19 · Hydraulic Reservoir, MainSDR SWIA201540793Water Separator · contaminatedRETURNED TO THE FIELD FOR SMOKE IN THE LAV. CREW REPORTED SMOKE COMING FROM GASPERS. FOUND GLYCOL IN WATER SEPARATOR. REPLACED NR 1AND NR 2 WATER SEPARATORS. OPS CHECKS GOOD.Feb 27, 2015 · N984CA · Cndair CL6002B19 · Humidity Control SystemSDR SWIA201440016Skin · gougedWHILE PERFORMING BLENDING FOR EXTERIOR SKIN GOUGES FOR ADF ANTENNA ON MX TRANS 11509318, DISCOVERED 4 EACH LIGHTNING STRIKES AT ADF ANTENNA MOUNT HOLES. C-CHECK, UPON FURTHER INVESTIGATION, FOUND TO BE OLD TOOLING MARKS INSTEAD OF LIGHTNING STRIKES. ALSO FOUNov 14, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201440046Vane · chafedLEFT INBD FLAP VANE CHAFED AT OTBD L/E. BLENDED THE CHAFE IAW REO.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440045Vane · chafedLEFT INBD FLAP VANE CHAFED AT INBD L/E. BLENDED THE CHAFE IAW REO.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440042Hinge · gougedPASSENGER DOOR HINGE 5TH LUG BACK IS GOUGED ON THE FUSELAGE SIDE. BLENDED AND FOUND WITHIN LIMITS. IAW REO.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA201440040Skin · debondedRT WING OTBD L/E 630KL IS DEBONDED. BONDED RT WING OTBD L/E, 630KL IAW REO.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201440038Skin · debondedRT WING INBD L/E 620JL IS DEBONDED. BONDED RT WING INBD L/E IAW REO.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201440037Seat Track · corrodedSEAT TRACK AT RBL 9.0 FROM BS 599 - 599+86 CORRODED. R & R THE SEAT TRACK IAW AMM & REO.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201440035Seat Track · corrodedSEAT TRACK AT RBL 9.0 BS 409+126 - 599 HAS CORROSION. R & R SEAT TRACK IAW AMM & REO.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201440034Seat Track · corrodedSEAT TRACK AT RBL 9.0 FROM BS 399 - 409+126 HAS CORROSION. R & R SEAT TRACK IAW AMM & REO.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201440033Seat Track · corrodedSEAT TRACK AT LBL 9.0 FROM BS 399 - 409+126 HAS CORROSION. R & R SEAT TRACK IAW AMM & REONov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201440032Pressure Deck · crackedPRESSURE FLOOR AT BS 458 - 462 CRACKED BETWEEN BL 0.0 AND RBL 9.0. REPAIRED IAW REO. PERFORMED PRESSURIZATION CHECK IAW AMM.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201440031Pressure Deck · crackedPRESSURE FLOOR AT BS 458 - 462 CRACKED BETWEEN BL 0.0 AND LBL 9.0. REPAIRED IAW REO. PERFORMED PRESSURIZATION CHECK IAW AMM.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201440030Bulkhead Web · crackedCRACK AT FWD PRESSURE BULKHEAD WEB COMMON TO PARKING BRAKE FITTING, 3 O'CLOCK POSITION WHEN LOOKING FORWARD, REPAIRED IAW REO. PRESSURE CHECKED GOOD.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201440019Bulkhead Web · crackedCRACK NOTED ON FS621 BULKHEAD WEB, FWD FACE, ALONG LBL36.2 AT APPROXIMATELY WL 75 NEAR FLOOR LEVEL. C-CHECK, REPAIRED CRACK IAW REO. PARTS REMOVED WEIGHT 0.01 LBS, REPLACEMENT PARTS WEIGH 0.40 LBS, NET WEIGHT GAINED 0.39 LBS. SCALE TUC 1755, DUE 30 JUN 2015Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201440018Bulkhead Web · crackedCRACK NOTED ON BS 621 BULKHEAD WEB, FWD FACE ALONG BL 0 AT WL 90. C-CHECK. REPAIRED CRACK ON FS 621 BULKHEAD IAW REO. PRESSURE CHECK GOOD. COMPLIED WITH ST 51-900-1003, WEIGHED CUT OUT DAMAGED WEB SECTION AT .002 LBS AND REPAIR PARTS WITH ADDED FASTENERS ATNov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201440044Panel · crackedPANEL 221CLC HAS CRACKS AROUND SCREW HOLE. REPAIRED CRACKS AROUND SCREW HOLE ON PANEL IAW EA.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Standard Practices/StructuresSDR SWIA201440043Vane · chafedRIGHT WING INBD FLAP VANE L/E CHAFED 91.5 INCHES FROM OTBD END. BLENDED CHAFE IAW REO.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440041Panel · crackedPANEL 222CLC, HAS CRACKS AROUND SCREW HOLE. REPAIRED PANEL IAW EA.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA201440039Vane · chafedRIGHT WING INBD FLAP VANE L/E CHAFED 43 INCHES FROM OTBD END. BLENDED CHAFE IAW REO AND SRM. FOUND WITHIN LIMITS IAW REO.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440036Vane · chafedRIGHT WING INBD FLAP VANE L/E CHAFED 7.5" FROM OTBD END. BLENDED IAW REO. FOUND WITHIN LIMITS IAW REO.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440028Skin · dentedLEFT INBD FLAP HAS DENT ON LOWER SKIN OUTBD OF PANEL 584AB. REPAIRED IAW EA.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440024Attach Fitting · chafedLEFT MLT DOOR ROD ATTACH LUG ON DOOR IS CHAFED. C-CHECK, R & R THE LT MLG DOOR ATTACHMENT LUG REF SRM & REO.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Landing Gear DoorsSDR SWIA201440023Rod End · chafedLEFT MLG DOOR ROD END IS CHAFED AT THE BELLCRANK END. R & R THE LT MLG DOOR STRUT IAW AMM, DWG AND REO.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Landing Gear Door Retract SectionSDR SWIA201440022Bellcrank · chafedLT MLG DOOR BELLCRANK END IS CHAFED AT THE DOOR ROD CONNECTION END. R & R THE LT MLG DOOR BELLCRANK ASSY REF AMM, COMPLIED WITH REO AND DWG.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Landing Gear Door Retract SectionSDR SWIA201440021Rod End · chafedRIGHT MLG DOOR ROD END IS CHAFED AT THE BELLCRANK END. R & R THE RT MLG DOOR STRUT.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Landing Gear Door Retract SectionSDR SWIA201440020Bellcrank · chafedRT MLG DOOR BELLCRANK END IS CHAFED AT THE DOOR ROD CONNECTION END. C-CHECK, OUT OF LIMITS IAW DWG. R & R RT MLG DOOR BELLCRANK ASSY, REF AMM, CW REO.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Landing Gear Door Retract SectionSDR SWIA201440017Vane · chafedLEFT INBD FLAP VANE CHAFED AT CENTER L/E. BLENDED IAW REO.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440015Vane · gougedRT WING INBD FLAP VANE L/E HAS SMALL GOUGE 27.5" FROM OTBD END. BLENDED IAW REO.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440014Vane · chafedRT WING INBD FLAP VANE L/E CHAFED 70.5" FROM OTBD END. BLENDED AND REPAIRED IAW REO.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440012Skin · chafedLEFT AILERON UPPER L/E CHAFED. LT AILERON UPPER L/E SHROUD FOUND TO BE OUT OF LIMITS IAW REO REPLACED.Nov 7, 2014 · N984CA · Cndair CL6002B19 · AileronsSDR SWIA201440048Skin · failedDENTED LT FUSELAGE SKIN PANEL ON NOSE, BELOW CAPTAIN'S WINDOW. REPAIRED IAW REO.Nov 6, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201440029Panel · damagedPANEL 326AR, ZONE 300 FAILED GAP CHECK. CONTOURED VISOR PANEL. FOUND WITHIN LIMITS IAW REO.Nov 6, 2014 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201440027Panel · failedPANEL 326BR, ZONE 300 FAILED GAP CHECK, CONTOURED VISOR PANEL. FOUND WITHIN LIMITS IAW REO.Nov 6, 2014 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201440026Panel · failedPANEL 326BL, ZONE 300, FAILED GAP CHECK, CONTOURED VISOR PANEL IAW REO AND AMM.Nov 6, 2014 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201440025Panel · damagedPANEL 326AL ZONE 300, FAILED GAP CHECK, CONTOURED VISOR PANEL 326AL. FOUND WITHIN LIMITS IAW REO.Nov 6, 2014 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2014061938226Torque Link · galledLT ENGINE FORWARD MOUNT TORQUE LINK ASSEMBLY HAS GALLING IN BUSHING. INSTALLED NEW LINK ON THE LT ENGINE FWD YOKE MOUNT IAW AMM.Jun 17, 2014 · N984CA · Cndair CL6002B19 · Engine Mount SectionSDR SWIA2014061938225Bushing · galledLT ENGINE FORWARD MOUNT YOKE BUSHING HAS GALLING. INSTALLED NEW LT ENGINE FWD YOKE MOUNT IAW AMM.Jun 17, 2014 · N984CA · Cndair CL6002B19 · Engine Mount SectionSDR SWIA201437643Lamp · burned outLEFT OVERWING EMERGENCY LIGHT IS BURNED OUT. R & R LT OVERWING EXTERIOR EMERGENCY LIGHT LAMP IAW AMM.May 19, 2014 · N984CA · Cndair CL6002B19 · Emergency LightingSDR SWIA201437668Autopilot Sys · disconnectedAUTOPILOT INITIATED UNCOMMANDED PITCH CHANGE A/P WAS MANUALLY DISCONNECTED, FLIGHT PATH CORRECTED AND REENGAGED WITHOUT FURTHER INCIDENT. PERFORMED SERVO SPIN TEST IAW AMM. NO DEFECTS NOTED AND NO RELEVENT MDC MESSAGES WERE FOUND.May 17, 2014 · N984CA · Cndair CL6002B19 · Auto Flight SystemSDR SWIA201437403Bushing · damagedLEFT ENGINE AFT MOUNT THRUST SHAFT SPHERICAL BUSHING AND SPHERICAL BUSHING HOUSING HAS CORRODED. REPLACED LT ENGINE AFT MOUNT THRUST SHAFT SPHERICAL BUSHING AND SPHERICAL BUSHING HOUSING IAW AMM.May 7, 2014 · N984CA · Cndair CL6002B19 · Engine Mount SectionSDR SWIA201437053Lamp · burned outFORWARD EMERGENCY LIGHT OVERHEAD LIGHT IS BURNED OUT, REPLACED LAMP.Apr 6, 2014 · N984CA · Cndair CL6002B19 · Emergency LightingSDR SWIA201436785Sign · burned outLOWER RIGHT OVERWING EXIT EMERGENCY SIGN IS BURNED OUT. REPLACED SIGN AND INVERTER.Mar 16, 2014 · N984CA · Cndair CL6002B19 · Emergency LightingSDR SWIA201334853Light · inoperativeCEILING EMERGENCY LIGHT IN AFT POSITION BURNED OUT. FLT#5374 RELAMPED, PN 1317.Oct 7, 2013 · N984CA · Cndair CL6002B19 · Emergency LightingSDR SWIA201334381Light · inoperativeCEILING POD LIGHT ABEAM BURNED OUT. FLT#6224 RELAMPED.Aug 22, 2013 · N984CA · Cndair CL6002B19 · Emergency LightingSDR SWIA201333497Pump · failedRECEIVED GEAR DISAGREE WARNING MSG. BY THE TIME WE RAN CHECKLIST, ISSUE SELF-CORRECTED. NO PROBLEMS WITH LANDING GEAR EXTENSION ON LANDING. REPLACED 3A ELECTRIC HYD PUMP IAW AMM, PN: 848847, SN ON: MX572122, SN OFF: MX520285.May 17, 2013 · N984CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR SWIA201333361Web · crackedTRU WEB IS CRACKED AT FS 193 RIGHT. (C-CHECK) REPAIRED TRU WEB AT FS 193.00 RIGHT IAW REO.Apr 14, 2013 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201333360Web · crackedTRU WEB IS CRACKED AT FS 193 LEFT. (C-CHECK) INSTALLED REPAIR ON TRU WEB FS 193 LEFT IAW REO.Apr 14, 2013 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201333359Cap · wornLEFT INBD FLAP, INBD FLAP VANE CAP IS WORN BEYOND LIMITS. (C-CHECK) REPLACED WORN LEFT INBD FLAP, INBD FLAP VANE CAP IAW SRM.Apr 13, 2013 · N984CA · Cndair CL6002B19 · Trailing Edge Flaps
Back to N984CA, cancelled May 3, 2017