N554CA

Service difficulty reports · 210

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 = 'N554CA' 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 SWIA202161815None · crackedNOSE HYDRAULICS COMPARTMENT - INTERCOSTAL JUST OTBD OF BLOWOUT PANEL HAS CRACK IN AFT RADIUS (C-CHECK RO 10/22/2021) REMOVED AND REPLACED INTERCOSTAL AT NOSE HYD COMPARTMENT OTBD OF BLOW OUT PANEL. IAW CRJ900 SRM 51-42-06-001-001-A01 AND DWG CC670-33045Aug 12, 2021 · N554CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA202161911None · wornR/H WING SLAT TRACK 3-2 I/B FWD SIDE ROLLER TURNS ROUGHLY, O/B FWD SIDE ROLLER TURNS ROUGHLY AND O/B AFT SIDE ROLLER HAS A FLAT SPOT. (C-CHECK RO 10/22/2021) REMOVED AND REPLACED ROLLERS WITH NEW ROLLERS AND SHIMS ON RH WING SLAT TRACK 3-2 I/B FWD, O/Aug 11, 2021 · N554CA · Cndair CL6002D24 · Wing, Nacelle/Pylon Attach FittingsSDR SWIA202161910None · wornR/H WING SLAT TRACK 2-2 O/B FWD SIDE ROLLER TURNS ROUGHLY. (C-CHECK RO 10/22/2021) REMOVED AND REPLACED RH WING SLAT TRACK 2-2 SIDE ROLLER AT O/B FWD LOCATION WITH NEW UNIT REF CRJ-900 AMM 27-81-44-400-802-A01. SEE ATTACHED CONTINUATION CARD FOR DETAIAug 11, 2021 · N554CA · Cndair CL6002D24 · Wing, Nacelle/Pylon Attach FittingsSDR SWIA202161909None · wornR/H WING SLAT TRACK 1-2 O/B AFT SIDE ROLLER HAS A FLAT SPOT. (C-CHECK RO 10/22/2021) REMOVED AND REPLACED ROLLER WITH NEW ROLLER AND SHIM RH WING SLT TRACK 1-2 O/B AFT SIDE ROLLER. REF: CRJ900 AMM 27-81-44-000-801-A01 AND 27-81-44-400-801-A01. OPS TESAug 11, 2021 · N554CA · Cndair CL6002D24 · Wing, Nacelle/Pylon Attach FittingsSDR SWIA202161908None · wornL/H WING SLAT TRACK 3-2 I/B AFT SIDE ROLLER TURNS ROUGHLY. (C-CHECK RO 10/22/2021) REMOVED AND REPLACED L/H WING SLAT TRACK 3-2 I/B AFT SIDE ROLLER WITH NEW UNIT REF CRJ-900 AMM 27-81-44-400-803-A01. SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PEAug 11, 2021 · N554CA · Cndair CL6002D24 · Wing, Fuselage Attach FittingsSDR SWIA202161907None · wornL/H WING SLAT TRACK 2-2 I/B FWD SIDE ROLLER HAS A FLAT SPOT. (C-CHECK RO 10/22/2021) REMOVED AND REPLACED L/H WING SLAT TRCAK 2-2 SIDE FWD SIDE ROLLER WITH NEW P/N CC670-12048-3 REF CRJ900 AMM 27-81-44-000-802-A01, AMM 27-81-44-400-802-A01,SW 1632. SEEAug 11, 2021 · N554CA · Cndair CL6002D24 · Wing, Fuselage Attach FittingsSDR SWIA202161906None · wornL/H WING SLAT TRACK 1-2 I/B AFT SIDE ROLLER TURNS ROUGHLY AND O/B AFT SIDE ROLLER HAS A FLAT SPOT. (C-CHECK RO 10/22/2021) REMOVED AND REPLACED L/H WING SLAT TRACK 1-2 I/B AFT SIDE ROLLER WITH NEW UNIT REF CRJ-900 AMM 27-81-44-400-801-A01. SEE ATTACHEAug 11, 2021 · N554CA · Cndair CL6002D24 · Wing, Fuselage Attach FittingsSDR SWIA202161814None · corrodedFWD BAGGAGE BAY DOOR LOWER JOINT PLATE HAS EVIDENCE OF CORROSION @FS519.64 BETWEEN STRINGERS 25L & 27 (C-CHECK RO 10/22/2021) REMOVED CORROSION ON FWD BAGGAGE BAY DOOR LOWER JOINT PLATE @FS519.64 BETWEEN STRINGERS 25L & 27, REF. CRJ900 SRM 51-21-06-001-Aug 11, 2021 · N554CA · Cndair CL6002D24 · DoorsSDR SWIA202161813None · corrodedAFT BAGGAGE BAY DOOR SILL HAS EVIDENCE OF CORROSION (C-CHECK RO 10/22/2021) AFT BAGGAGE BAY DOOR SILL FOUND TO BE OUT LIMITS REF CRJ900 SRM 53-61-23-001-001-A01. REMOVED BAD AFT BAGGAGE BAY DOOR SILL REF CRJ900 SRM 51-42-06-001-001-A01, REF CRJ900 SRM 5Aug 11, 2021 · N554CA · Cndair CL6002D24 · DoorsSDR SWIA202161812None · cracked*SUSPECTED CRACK ON THE V-STAB RH AFT DRAG ANGLE (C-CHECK RO 10/22/2021) REPAIRED V-STAB RH AFT DRAG ANGLE REF CRJ900 SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY.Aug 10, 2021 · N554CA · Cndair CL6002D24 · Empennage StructureSDR SWIA202161811None · corroded* GALLEY SERVICE DOORSILL ANGLE IS CORRODED. FLAGGED (C-CHECK RO 10/22/2021) REMOVED AND REPLACED GALLEY SERVICE DOOR LOWER SILL ANGLE BETWEEN FS319.00 TO FS349.00 IAW CRJ 900 SRM 51-42-06-001-001-A01 / DRAWING #SH670-31950 REV NC. COMPLIED WITH 51-900-Aug 9, 2021 · N554CA · Cndair CL6002D24 · DoorsSDR SWIA202161810None · corroded* LH WHEEL WELL PANELS 542AZ AND 542AB LANDINGS ARE CORRODED. FLAGGED (C-CHECK RO 10/22/2021) REMOVED AND REPLACED LH WHEEL WELL LANDING (ATTACH ANGLES) 542AZ REF CRJ900 AMM 51-42-21-001-001-A01 AND DWG CC670-10320 REV F LEAK CHECKS GOOD. COMPLIED WITHAug 8, 2021 · N554CA · Cndair CL6002D24 · DoorsSDR SWIA202161809None · corroded* RH WHEEL WELL PANELS 642AZ AND 642AB LANDINGS ARE CORRODED. FLAGGED (C-CHECK RO 10/22/2021) REPAIRED CORRODED LANDINGS FOR RH WHEEL WELL PANELS 642AZ AND 642AB REF REO 690-57-22-060 REV--, DATED 2021-08-31. SEE CONTINUATION FOR DETAILS. NO LEAKS NOTEAug 8, 2021 · N554CA · Cndair CL6002D24 · DoorsSDR SWIA202161808None · gougedNUMEROUS GOUGES NOTED IN FUSELAGE UNDER RH VENTRAL FIN FAIRING STRUCTURAL ATTACHMENT. (C-CHECK RO 10/22/2021) REPAIRED NUMEROUS GOUGES IN FUSELAGE UNDER RH VENTRAL FIN FAIRING STRUCTURAL ATTACHMENT PER REO 690-53-00-465 REV. -- DATE 2021-09-03 . COMPLIEAug 7, 2021 · N554CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202161807None · gougedNUMEROUS GOUGES NOTED IN FUSELAGE UNDER LH VENTRAL FIN FAIRING STRUCTURAL ATTACHMENT. (C-CHECK RO 10/22/2021) GOUGES IN FUSELAGE UNDER L/H VENTRAL FIN REPAIRED REF REO 690-53-00-465 REV--, DATED 2021-09-03. COMPLIED WITH 51-900-1002-SKY. SEE CONTINUATIOAug 7, 2021 · N554CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202161806None · corrodedGALLEY #1 HAS 4EA CORRADED MOUNTING FEET FWD INBD FOOT, AFT INBD FOOT, MID INBD FOOT AND AFT OTBD FOOT REQUIRES REPLACMENT. (C-CHECK RO 10/22/2021) REPLACED 3 EA CORRODED GALLEY 1 FEET (MOUNT FITTINGS) PER SAFRAN CMM 35-33-67 AND REPAIRED 1 EA CORRODED Aug 7, 2021 · N554CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202161805None · dentedD: REFER TO EAML 696703. / REFER TO EAML 696583. 2 DENTS FOUND AT FORWARD LEFT FUELSAGE. / DENT #1. FS 297.25. STRG 15LH. DENT # 1 IS CIRCULAR, MEASURING 1.25?L, X 1.25?W, X 0.007?D. / DENT #2. FS 296. STRG 16LH. DENT # 2 IS CIRCULAR, MEASURING 1.25?L, X 1.25?Jul 31, 2021 · N554CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202161948None · damagedREMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR PER AMM (C-CHECK RO 10-22-21) REPLACED LH AILERON WING AFT SPAR BUSHINGS AND HARDWARE REF CRJ900 AMM 20-31-00-400-802-A01.Jul 15, 2021 · N554CA · Cndair CL6002D24 · Wing StructureSDR SWIA202161941None · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA46514-670-52-11-287, REV. E N554CA-PR - TWO CRACKS IN THE MAIN CABIN DOOR STAIR, COMPLIED WITH REO 670-52-11-287, REV. E, .PERMANENT REPAIR IS DUE WITHIN 5200 FLIGHT HOURS WITH ESCALATION PROVIDED BY REO 690-52-1Jul 12, 2021 · N554CA · Cndair CL6002D24 · Fuselage, Door HingeSDR SWIA202161804None · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA66905-690-53-11-1303 554CA MXCODEID54940-PR - DAMAGE FOUND ON FUSELAGE SKIN LOCATED BETWEEN FS193.00- FS202.75 AND STR 14R-STR16R (RVSM ZONE). COMPLIED WITH TEMPORARY REPAIR PER REO 690-53-11-1303 REV-- DATED 2021-02-Jul 12, 2021 · N554CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202161803None · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA52673-690-57-41-248 554CA MXCODEID48706-PR - TEMPORARY DISPOSITION FOR BLENDED WEAR DAMAGE TO LH WING FIXED LEADING EDGE SKIN AT SS144.94. COMPLIED WITH TEMPORARY REPAIR PER REO 690-57-41-248. PERMANENT REPAIR DUE WITHJul 12, 2021 · N554CA · Cndair CL6002D24 · Wing, Fuselage Attach FittingsSDR SWIA202156962Strut · dischargedONCE SELECTING GEAR TO UP POSITION ON TAKEOFF, PROX SYS 1 FAULT STATUS CAME UP FOLLOWED BY A GEAR DISAGREE MASTER WARNING, RAN QRH GEAR WAS SELECTED DOWN AND MESSAGE EXTINGUISHED, RETURNED TO FIELD. SERVICED NLG SHOCK STRUT WITH NITROGEN AND OIL REF AMM 12Mar 12, 2021 · N554CA · Cndair CL6002D24 · Nose/Tail Landing Gear Strut/AxleSDR SWIA202008252080Engine · contaminatedDURING TAKEOFF ROLL, BLUEISH ELECTRICAL SMELLING SMOKE BEGAN TO ENTER THE FLIGHT DECK ALONG EACH SIDE OF THE FLIGHT DECK A SMOKE LAV (DID NOT CATCH FWD OR AFT) MASTER WARNING APPEARED. FLIGHT ATTENDANTS REPORTED THE SMELL AND HAZE IN THE CABIN. FLIGHT 3614Aug 25, 2020 · N554CA · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR SWIA2019021245509Target · out of adjustAFTER TAKEOFF NONE OF THE GEAR CAME UP. DIVERTED. (FLT#4986) CLOSED ADJUSTED TARGET FOR PX37,IAW AMM. RIG CHECKS GOOD.Feb 12, 2019 · N554CA · Cndair CL6002D24 · Landing Gear Position and WarningSDR SWIA2017111043971Stiffener · corrodedSTIFFENER UNDER TOP PLATE ON PAX DOOR IS CORRODED. REMOVED AND REPLACED THE STIFFENER IAW SRM.Oct 26, 2017 · N554CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA2017111043969Plate · corrodedPAX DOOR TOP PLATE HAS CORROSION. REMOVED AND REPLACED THE TOP PLATE IAW SRM.Oct 26, 2017 · N554CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA201743424Frame · gougedGOUGE DAMAGE FOUND ON FRAME BS 1126 BETWEEN STRINGERS 7 - 8R. REMOVED AND REPLACED THE FRAME IAW REO.Jun 17, 2017 · N554CA · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA201743425Stringer · chafedCHAFE DAMAGE TO STRINGER 7R BETWEEN BS 1144 AND 1150. REPAIRED THE STRINGER IAW REO.Jun 14, 2017 · N554CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA201743423Stringer · chafedCHAFE DAMAGE TO STRINGER 6R BETWEEN BS 1144 AND 1150, OUT OF LIMITS IAW SRM. REPAIRED THE STRINGER IAW REO.Jun 14, 2017 · N554CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA201541692Stringer · corrodedSTRINGER 25R AT BS 324 CORRODED. R & R THE STRINGER IAW SRM.Nov 30, 2015 · N554CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA201541686Frame · corrodedBS 319 FRAME IS CORRODED BETWEEN STRINGERS 25L-25R. REPAIRED THE FRAME IAW REO.Nov 29, 2015 · N554CA · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA201541687Seat Track · corrodedRIGHT SIDE SEAT TRACK BS 847+32 - 865 CORRODED. R & R THE SEAT TRACK IAW AMM.Nov 28, 2015 · N554CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201541681Intercostal · corrodedINTERCOSTAL CORRODED STRINGER 27L BETWEEN BS 349 - 364. R & R THE INTERCOSTAL.Nov 28, 2015 · N554CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA201541680Intercostal · corrodedINTERCOSTAL CORRODED AT STRINGER 27R BETWEEN BS 349 - 364. REPLACED THE INTERCOSTAL IAW SRM.Nov 28, 2015 · N554CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA201541684Seat Track · corrodedRIGHT SIDE, SEAT TRACK BS 785 - 847 + 16 CORRODED IN SEVERAL AREAS. R & R THE SEAT TRACK IAW AMM.Nov 25, 2015 · N554CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201541678Seat Track · corrodedRIGHT SIDE, SEAT TRACK BS 477 - 581 CORRODED. R & R THE SEAT TRACK IAW AMM.Nov 25, 2015 · N554CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201541677Frame · corrodedCORROSION OUT OF LIMITS AT BS 349 STRINGERS 26 - 27L. REPLACED THE FRAME IAW SRM.Nov 24, 2015 · N554CA · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA201541676Frame · corrodedBS 310 FRAME AT STRINGER 26R - 26L CORRODED OUT OF LIMITS. REPAIRED THE FRAME IAW REO.Nov 24, 2015 · N554CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA201541690Bulkhead Web · corrodedBS 280 BULKHEAD WEB LOWER CORRODED AND CRACKED AT LBL 12. REPAIRED THE BULKHEAD WEB IAW REO.Nov 23, 2015 · N554CA · Cndair CL6002D24 · Fuselage Main, BulkheadSDR SWIA201541685Seat Track · corrodedRIGHT SIDE, SEAT TRACK BS 865 - 969 CORRODED AND GOUGED IN SEVERAL AREAS. R & R THE SEAT TRACK IAW AMM.Nov 23, 2015 · N554CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201541683Seat Track · corrodedLEFT SIDE, SEAT TRACK BS 785 - 847 + 16 CORRODED AND GOUGED IN SEVERAL AREAS. R & R THE SEAT TRACK IAW AMM.Nov 23, 2015 · N554CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201541682Seat Track · corrodedLEFT SIDE, SEAT TRACK BS 847 + 16 - 913 CORRODED AND GOUGED IN SEVERAL AREAS. R & R THE SEAT TRACK IAW AMM.Nov 23, 2015 · N554CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201541679Seat Track · corrodedLEFT SIDE, SIDE SEAT TRACK BS 913 - 969 CORRODED AND GOUGED IN SEVERAL AREAS. R & R THE SEAT TRACK IAW AMM.Nov 23, 2015 · N554CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201541691Floorbeam · corrodedCORROSION FOUND ON THE FLOORBEAM AT BS 280. R & R THE FLOORBEAM IAW SRM AND REO.Nov 22, 2015 · N554CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWIA201541689Floor Panel · crackedRIGHT TRU BAY FLOOR PANEL CRACKED AT BS 193. REPAIRED THE FLOOR PANEL IAW REO.Nov 21, 2015 · N554CA · Cndair CL6002D24 · Fuselage Floor PanelSDR SWIA201541688Floor Panel · crackedLEFT TRU BAY FLOOR CRACKED AT BS 193. REPAIRED FLOOR PANEL IAW REO.Nov 21, 2015 · N554CA · Cndair CL6002D24 · Fuselage Floor PanelSDR SWIA2014061238147Bulb · inoperativeTWO BULBS INOPERATIVE ON LOWER AFT EMERGENCY EXIT LIGHT INTERIOR OF SERVICE DOOR. REPLACED BULBS IAW AMM.Jun 11, 2014 · N554CA · Cndair CL6002D24 · Emergency LightingSDR SWIA201436054Sill · corrodedSERVICE DOOR AFT FLOOR SILL IS CORRODED. C-CHECK REPAIRED SERVICE DOOR AFT FLOOR SILL IAW STS EA.Jan 6, 2014 · N554CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA201436058Skin · chafedAFT BELLY CHAFED UNDER AFT BELLY PANELS AT BL 0. C-CHECK BLENDED OUT DAMAGE UNDER AFT BELLY PANELS AT BL 0 & RESTORED FINISH IAW REO.Jan 5, 2014 · N554CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA201436057Wire Harness · chafedRT ENG IDG CABLES ARE CHAFING IN TWO AREAS. C-CHECK REPAIRED RT ENG IDG CABLES IN TWO AREAS IAW REO.Jan 5, 2014 · N554CA · Cndair CL6002D24 · Electrical Power System Wiring
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