N566NN

Service difficulty reports · 86

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 = 'N566NN' 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 VNAA202402290010Seat Track · corrodedCORROSION ON SEAT RAILS RBL 9 STA 421 TO 501 (2E/A) AND LBL 9 STA 581 TO 661+32. SEAT RAILS RBL 9 STA 421 TO 501 (2E/A) AND LBL 9 STA 581 TO 661+32 WERE EVALUATED OUT OF LIMITS PER CRJ 900 SRM 53-21-49-101-001-A01; CRJ900 SRM 53-31-49-101-001-A02 AND WERE RJan 25, 2024 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202402290027Duct · crackedCRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPAIRED PER REO 690-28-25-016. REV. --Jan 24, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Attach FittingsSDR VNAA202402290028Skin · crackedLIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 18 RH TO 19 RH AND AT FS629. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 18 RH TO 19 RH AND AT FS629 WAS REPAIRED PER REO 690-53-31-816 REV - -Jan 23, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202402290023Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01Jan 23, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202402290022Rib · crackedCRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-322 REV.--Jan 23, 2024 · N566NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA202402290021Rib · crackedCRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-323 REV.--Jan 23, 2024 · N566NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA202402290019Rib · crackedAFTER ACCESS PANEL 621BR REMOVAL TO SLAT LUBRICATION, CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING. CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240 REV - -Jan 23, 2024 · N566NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA202402290026Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 16 LH TO 17 LH AND BTW FS 501 TO FS 517. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 16 LH TO 17 LH AND BTW FS 501 TO FS 517 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03Jan 22, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202402290024Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 14 RH AT FS 379. LIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 14 RH AT FS 379 WAS REPAIRED PER REO 690-53-21-1726 REV. - -Jan 22, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202402280008Skin · damagedLIGHTNING STRIKE (1EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR15 BTW FS280 - FS264. LIGHTNING STRIKE (1EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR15 BTW FS280 - FS264 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03Jan 21, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202402280007Skin · damagedLIGHTNING STRIKE (2EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR14 BTW FS248.5 - FS233.5. LIGHTNING STRIKE (2EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR14 BTW FS248.5 - FS233.5 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03Jan 21, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202402280006Skin · damagedLIGHTNING STRIKE ( 1EA) ON FUSELAGE SKIN BTW STGR 14 RH TO STGR 15RH AND BTW FS 1051 TO FS 1069. LIGHTNING STRIKE ( 1EA) ON FUSELAGE SKIN BTW STGR 14 RH TO STGR 15RH AND BTW FS 1051 TO FS 1069. WAS BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WAS EVALUJan 21, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202402280003Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 19 RH TO STGR 20 RH AT FS 549. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 19 RH TO STGR 20 RH AT FS 549 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03Jan 21, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202402280002Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 23 RH AT FS 596. LIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 23 RH AT FS 596 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03Jan 21, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202402280005Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-2Jan 20, 2024 · N566NN · Bombdr CL6002D15 · Vertical StabilizerSDR VNAA202402280004Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-Jan 20, 2024 · N566NN · Bombdr CL6002D15 · Vertical StabilizerSDR VNAA202402280001Skin · scratchedSEVERAL SCRATCH ON EXTERNAL REAR FUSELAGE SKIN AREA BTW FS985.00 - FS1000.00 AND STGR 14 - STGR 16. FUSELAGE SKIN AREA BTW FS985.00 - FS1000.00 AND STGR 14 - STGR 16 WAS REPAIRED PER REO 690-53-61-1346 REV - -Jan 4, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202402290015Floor Support · crackedCRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTUREJan 3, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA202402290009Intercostal · corrodedCORROSION ON INTERCOSTAL AT FS316 BTW LBL 9 TO RBL 9. INTERCOSTAL AT FS316 BTW LBL 9 TO RBL 9 WAS REPAIRED PER REO 690-53-21-1717 REV -.Jan 3, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202402290005Seat Track · corrodedCORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 785.15 TO FS 797. SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 785.15 TO FS 797.00 WAS EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12)Jan 3, 2024 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202402290004Seat Track · corrodedCORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 847.00 + 61 TO FS 865. CORROSION ON STRG 15LH BETWEEN FS 847.00 + 61 TO FS 865.00 WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONF A12)Jan 3, 2024 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202402290006Seat Track · corrodedCORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 744.15 TO FS 761.85. SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 744.15 TO FS 761.85 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12).Dec 13, 2023 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202306110001Fitting · unknownNEW HSTA FITTING AV670-23105-006S MISDRILLED AND REQUIRES NEW FITTING. PERFORMED A MAJOR REPAIR TO R/H HSTA UPPER FITTING ASSY.Jun 11, 2023 · N566NN · Cndair CL6002D24 · Fuselage Structure (General)SDR VNAA202304211111Unknown · unknownDURING TAKEOFF, MESSAGE FOR NOSE WHEEL STEERING CAME UP DURING FLIGHT. TROUBLESHOT PER FIM 32-51-50-810-801. B1-007464. C/W OPS CHECK OF NWS IAW CRJ 900 AMM 32-51-00-710-801. OPS CHECK GOOD AT THIS TIME.Apr 20, 2023 · N566NN · Cndair CL6002D24 · Landing Gear Steering SystemSDR VNAA2020102611101Sensor · failedAFTER TAKE OFF FROM CAK THE CREW RECEIVED A BTMS INDICATION. THEY HAD THE PASSENGERS BRACE, DECLARED AN EMERGENCY AND RETURNED TO CAK. THEY LANDED SAFELY AND WITHOUT INCIDENT. TRUCKS ROLLED. THE PASSENGERS ARE OK AND THE CREW WILL CONTINUE ON WITH THEIR FLOct 23, 2020 · N566NN · Cndair CL6002D24 · Landing Gear Brake SystemSDR VNAA2020051901101Door Seal · damagedDURING CLIMB OUT OF PNS, AT FL200 CREW BEGAN HEARING POPPING NOISE AND BEGAN TO FEEL PRESSURE DROPPING. CREW NOTICED CABIN ALT RISING. CREW DONNED O2 MASKS, BEGAN EMERGENCY DESCENT AND DECLARED AN EMERGENCY WITH ATC. CREW RECEIVED NO WARNINGS AND CABIN ALT NMay 17, 2020 · N566NN · Cndair CL6002D24 · Passenger/Crew DoorsSDR VNAA202004229991Megaphone · inoperativeMEGA PHONE INOP. CHANGE BATTERIES, STILL WILL NOT WORK. INSTALLED SERVICEABLE MEGAPHONE.Apr 22, 2020 · N566NN · Cndair CL6002D24 · Emergency EquipmentSDR VNAA202004219996Frame · corrodedFUSELAGE LOWER FRAME AT FS295, STGR27 IS CORRODED ON FWD SIDE. REPAIRED IAW CRJ 900 SRM 53-00-06-101-002-A04Apr 21, 2020 · N566NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202004219995Door Sill · corrodedRH FLOOR SILL IS CORRODED AT 2 LOCATIONS BETWEEN FS 280.00 AND FS 319.75. LOCATED, DRILLED AND INSTALLED NEW FLOOR SILL. IAW CRJ900 SRM'S 51-42-06-001-001-A01, 51-42-13-001-001-A01, 57-42-21-001-001-A01, 51-40-11-001-001-A01.Apr 21, 2020 · N566NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202004219994Intercostal · corrodedRH INTERCOSTALS BETWEEN FS349.00 AND FS364.00, STR26L TO STR 26R ARE CORRODED. LOCATED AND DRILLED LH AND RH INTERCOSTALS AT FS349.00 TO FS 364.00 IAW CRJ 900 SRM 51-40-11-001-001-A01.Apr 21, 2020 · N566NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202004219993Intercostal · corrodedLH INTERCOSTAL BETWEEN FS349.00 AND FS364.00, STR26L TO STR 26R ARE CORRODED. LOCATED AND DRILLED LH AND RH INTERCOSTALS AT FS349.00 TO FS 364.00 IAW CRJ 900 SRM 51-40-11-001-001-A01.Apr 21, 2020 · N566NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202004219992Support Angle · corrodedPASSENGER DOOR CENTER FLOOR SILL SUPPORT ANGLE CORRODED AROUND NUT PLATES. REMOVED THE PAX DOOR CENTER FLOOR SILL SUPPORT ANGLE ASSY IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE ANGLE IAW CRJ900 Apr 21, 2020 · N566NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202004219991Doubler · crackedPAX DOOR,UPPER AFT CORNER DOUBLER IS CRACKED, LOCATED UNDER PANEL 832AR. REMOVED CRACKED DOUBLER. IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. LOCATED, DRILLED, AND INSTALLED NEW DOUBLER, PN: 601R-318094-2.Apr 21, 2020 · N566NN · Cndair CL6002D24 · Passenger/Crew DoorsSDR VNAA2019040981101Acm · seizedAIRCRAFT RETURNED TO THE FIELD DUE TO SMOKE SMELL IN THE CABIN AND COCKPIT. PERFORM POWER ASSURANCE CHECK. PERFORMED OPS CHECK HPSOV. PERFORMS CHECK OF A/C DISTRIBUTION SYSTEM. NO DEFECTS NOTED AT THIS TIME. CREW REPORTED A STRONG ELECTRICAL SMELL IN GALLEY.Apr 8, 2019 · N566NN · Cndair CL6002D24 · Cabin Cooling SystemSDR VNAA2018013111101Trim System · abnormalSTAB TRIM RUN AWAY IN FLIGHT, EMERGENCY WAS DECLARED. INSPECTED AND OPS CHECKED STAB TRIM SYSTEM, OPS CHECK GOOD WITH NO DEFECTS.Jan 31, 2018 · N566NN · Cndair CL6002D24 · Stabilizer Control SystemSDR VNAA2017030900004Selector Valve · faultySTEERING INOPERABLE CAUTION MESSAGE. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE.Mar 9, 2017 · N566NN · Cndair CL6002D24 · Landing Gear Steering System
Back to N566NN