N567NN

Service difficulty reports · 91

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 = 'N567NN' 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 VNAA2026091524801Reservoir · unserviceableHYD 3 HIGH TEMP IN FLIGHT. FOLLOWED QRH PROBLEM DIDN'T GO AWAY. REMOVED AND REPLACED HYD SYSTEM NR 3 RESERVOIR IAW AMM 29-12-30-000/400-801.Sep 13, 2026 · N567NN · Cndair CL6002D24 · Hydraulic Reservoir, MainSDR VNAA2026052918301Tire · blownNUMBER 3 TIRE BLEW ON TAKE OFF ROLL / REMOVED AND REPLACED RH IB MLG WHEEL AND TIRE ASSEMBLY IAW AMM 32-41-01-000/400-801-A01-PSA.May 27, 2026 · N567NN · Cndair CL6002D24 · TireSDR VNAA2025111711101Pcu · faultedOTBD FLT SPOILERS & OTBD SPOILERON INFLIGHT CAUTION MSG. REMOVED AND REPLACED LT OTBD MULTI FUNCTION SPOILER PCU IAW AMM 27-62-01-000-400-801-A02-PSA, AND PERFORMED AN OPS TEST OF MFS PCU IAW AMM 27-62-01-710-801-A01 OPS TESTED GOOD.Nov 14, 2025 · N567NN · Cndair CL6002D24 · Drag Control SystemSDR VNAA2025031411101Window · crackedDURING CLIMB CAUTION MSG LEFT WINDOW HEAT THEN LEFT WINDSHIELD CRACKED IN MULTI PLACES. / REMOVED AND REPLACED THE LH WINDOW IAW CRJ 900 AMM 56-12-01-000/400-801-A01-PSA. OPS CHECK GOOD. LEAK CHECK GOOD.Mar 11, 2025 · N567NN · Cndair CL6002D24 · Flight Compartment WindowsSDR VNAA2024071511102Pseu · unserviceableTHROUGH ALL PHASES OF FLIGHT WITH GEAR UP WE HEARD A LOUD BANG AROUND THE NOSE AREA ACCOMPANIED WITH A PROX SYS FAULT STATUS AND GEAR POSITION INDICATIONS APPEARED ON EICAS. THESE EVENTS OCCURED AROUND 4 TIMES THROUGHOUT FLIGHT. UPON GEAR EXTENTION ALL INDICATJul 12, 2024 · N567NN · Cndair CL6002D24 · Landing Gear SystemSDR VNAA20240531031Floor Support · crackedSECONDARY NRC IN REFERENCE NRC:156 AFTER FLOOR SUPPORT ANGLE RBL 12 REMOVAL, CRACK ON ANGLE WAS FOUND. ANGLE WAS REPLACED PER CRJ 900 SRM 51-42-20-001-001-A01 AND SRM 51-42-06-001-001-A01May 1, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20240531030Bulkhead Web · corrodedAFTER RIVETS REMOVAL, FOUND CORROSION ON WEB, LOWER FS 280, RBL 12'' TO RBL 30''. WEB, LOWER FS 280, RBL 12'' TO RBL 30'' WAS REPAIRED PER CRJ900 SRM 53-11-10-201-004-A01May 1, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, BulkheadSDR VNAA20240531029Floorbeam · corrodedAFTER FLOOR PANEL SUPPORT ANGLE REMOVAL IN REF NRC 00075, CORROSION ON TRANSVERSE BEAM FS280 WAS FOUND BTW BL 0 - RBL 12. DUE EXCESSIVE CORROSION ON TRANSVERSE BEAM FS280 RH IT IS OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER CMay 1, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA20240531028Floor 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 STRUCTUMay 1, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20240531026Canister · crackedREF. TO: DURING INSPECTION OF THE TASK CARD TRFKE000WL78: 600-08E2-JIC IT WAS DETECTED CRACK IN CANISTER WELDED NO.3 STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO.3 STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REApr 30, 2024 · N567NN · Cndair CL6002D24 · Wing Main, Frame StructureSDR VNAA20240531027Post · crackedCRACK ON RIVETS AREA BELOW FLOOR AT BULKHEAD DOOR POST, BTW RBL 12 AND FS 280.00. CRACK ON RIVETS AREA BELOW FLOOR AT BULKHEAD DOOR POST, BTW RBL 12 AND FS 280.00 WAS REPAIRED PER REO 690-53-11-1748 REV. -Apr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA20240531023Fitting · corrodedCORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (3EA) (FLOOR STRUCTURE AREA) FITTING OF ENTRANCE COMPARTMENT (3EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01Apr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20240531019Seat Track · corrodedINITIAL INSPECTION: CORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 913.00 (5EA). RH SIDE SEAT RAIL BTW FS744.15 TO FS 913.00 (5EA) WERE EVALUATED, ARE OUT OFF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ90Apr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240531018Seat Track · corrodedCORROSION ON SEAT RAILS LBL27 (1EA) BTW FS 485.00 TO FS 501.00 AT PASSENGER CABIN. SEAT RAILS LBL27 (1EA) BTW FS 485.00 TO FS 501.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00Apr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240531017Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SEAT RAILS LBL9 BTW FS 364.00 TO FS 485.00 (1EA) AND FS 581.00 TO FS 693.00 (2EA) AT PASSENGER CABIN. SEAT RAILS LBL9 BTW FS 364.00 TO FS 485.00 (1EA) AND FS 581.00 TO FS 693.00 (2EA) WERE EVALUATED, ARE OUT OFF LIMITS PER CRJApr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240531016Seat Track · corrodedCORROSION ON SEAT RAILS RBL9 (5EA) BTW FS 349.00 TO FS 693.00 AT PASSENGER CABIN. SEAT RAILS RBL9 (5EA) BTW FS 349.00 TO FS 693.00 AT PASSENGER CABIN. WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49Apr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240531015Hinge Fitting · excess playAFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 3 AT VERTIC•A L STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103. REV.B.Apr 29, 2024 · N567NN · Cndair CL6002D24 · Vertical StabilizerSDR VNAA20240531012Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193. ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193. WAS REPAIRED PER REO 690-53-11-1762 REV - -Apr 28, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20240531014Post · corrodedDURING INSPECTION OF THE TASK CARD 53-10-219, IT WAS DETECTED CORROSION ON BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00 BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00 WERE REPAIRED PER REO 690-53-11-1752 REV-Apr 27, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, BulkheadSDR VNAA20240531013Floorbeam · corrodedINITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE FS280 (RBL9 TO LBL9) AT CABIN FLOOR STRUCTURE. FLOOR PANEL SUPPORT ANGLE FS280 (RBL9 TO LBL9) AT CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Apr 27, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA20240531011Bracket · corrodedCORROSION ON MACHINED (8 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARMENT. MACHINED (8 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE REPLACED PER CRJ900 SRM 51-42-20-001-001-A01 AND SRM 51-42-22-001-001-A01Apr 25, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20240531010Plate · corrodedCORROSION ON KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. RIS- WS 8070-1. CORROSION ON KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WERE REPLACED PER CRJ900 SRM 51-42-06-001-Apr 25, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA20240531009Counterbalance · wornWEAR ON AFT COUTERBALANCE ARM AT FWD BAGGAGE BAY DOOR. WEAR ON AFT COUTERBALANCE ARM AT FWD BAGGAGE BAY DOOR BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01, ZONE 1,2 AND 3 WAS MEASURED AND FOUND WITHIN OF LIMITS PER CRJ900 SRM 52-35-09-201-001-A01 AND LOWER Apr 25, 2024 · N567NN · Cndair CL6002D24 · Cargo/Baggage DoorsSDR VNAA20240531008Counterbalance · wornWEAR ON FWD / AFT COUTERBALANCE ARMS AT CENTER BAGGAGE BAY DOOR. RIS- WS 8070-1. WEAR ON FWD / AFT COUTERBALANCE ARMS AT CENTER BAGGAGE BAY DOOR BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01, ZONE 1,2 AND 3 WAS MEASURED AND FOUND WITHIN OF LIMITS PER CRJ9Apr 25, 2024 · N567NN · Cndair CL6002D24 · Cargo/Baggage DoorsSDR VNAA20240531007Skin · wornWEAR ON SETTLEMENT AREA OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN. WERE REPAIRED PER REO 690-57-21-466 REV. --Apr 25, 2024 · N567NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA20240531006Skin · wornIN REFERENCE TO RC TRFKE001HT5B: WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21Apr 25, 2024 · N567NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA20240531005Skin · damagedLIGHTNING STRIKE (1EAS) ON FUSELAGE SKIN AT FS 333 BTW STGR 22RH TO STGR 23RH. LIGHTNING STRIKE (1EAS) ON FUSELAGE SKIN AT FS 333 BTW STGR 22RH TO STGR 23RH WAS REPAIRED PER REO 690-53-21-1767 REV -AApr 25, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNA20240531003Drag 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). (SM) CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DApr 25, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR VNAA20240531025Seat Track · corrodedINITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS, LOCATED BTW FS=847 TO FS=977 AND LBL 9'' / RBL 9''. FLOOR SEAT RAILS, LOCATED BTW FS=847 TO FS=977 AND LBL 9'' / RBL 9''WERE EVALUATED, ARE OUT OFF LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 AND REPLACED PEApr 18, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240531024Fitting · corrodedCORROSION ON SETTLEMENT FITTING OF GALLEY 1 (2EA) (FLOOR STRUCTURE AREA) FITTING OF GALLEY 1 (2EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03, AND WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01Apr 18, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20240531021Seat Track · corrodedINITIAL INSPECTION: CORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WERE EVALUATED,ARE OUT OFF LIMITS PER CRJ900 SRM 53- 21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 ANDApr 18, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240531020Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) INITIAL INSPECTION: CORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 942.00 (6EA) LH SIDE SEAT RAIL BTW FS744.15 TO FS 942.00 (6EA) WERE EVALUATED, ARE OUT OFF LIMITS PER CRJ-900 SRM 53-41-49-10Apr 18, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20240531004Housing · wornWEAR ON HOUSING OF EXTERNAL HANDLE AT AFT BAGGAGE-BAY DOOR. WEAR ON HOUSING OF EXTERNAL HANDLE AT AFT BAGGAGE-BAY DOOR WAS REPAIRED PER REO 670-52-31-031 REV -BApr 18, 2024 · N567NN · Cndair CL6002D24 · Cargo/Baggage DoorsSDR VNAA202402050032Floorbeam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1661 REFeb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202402050031Buttstrap · corrodedCORROSION ON FUSELAGE CIRCUMFRENTIAL JOINT BTW FS280.00/ FS282.86 AND STGR 24LH/23RH. CORROSION ON FUSELAGE CIRCUMFRENTIAL JOINT BTW FS280.00/ FS282.86 AND STGR 24LH/23RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, BTW STGR 27 TO STGR 23R WAS EVALUATEDFeb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202402050030Intercostal · corrodedCORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 394 TO FS= 409 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTALS (2 EAS) IN STA. FS= 394 TO FS= 409 NEAR STGR 27 AT MAIN AVIONICS BAY WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND REPFeb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202402050029Intercostal · corrodedCORROSION ON INTERCOSTAL IN STA. FS= 349 TO FS= 364 NEAR STGR 27 RH SIDE AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL IN STA. FS= 349 TO FS= 364 NEAR STGR 27 RH SIDE AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 ANDFeb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202402050028Web · crackedCRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB. UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202402050027Skin · nickedSEVERAL NICKS ON SKIN (ZONE 1) BTW FS501.00 TO FS517.00 AND STGR 21 LH TO STGR 25 LH (ZONA 2) BTW FS 613.00 TO FS 629.00 AND STGR 21 LH TO STGR 25 LH AT FUSELAGE. SKIN (ZONE 1) BTW FS501.00 TO FS517.00 AND STGR 21 LH TO STGR 25 LH (ZONA 2) BTW FS 613.00 TO FFeb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202402050026Skin · damagedLIGHTING STRIKE BTW FS280.00 TO FS295.00 AND BTW STGR 17 TO STGR 16 RH (1EA) LIGHTING STRIKE BTW FS379.00 TO FS394.00 AND BTW STGR 17 TO STGR 18 RH (1EA) AT SELAGE SKIN. LIGHTING STRIKE BTW FS280.00 TO FS295.00 AND BTW STGR 17 TO STGR 16 RH (1EA) LIGHTING STFeb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202402050025Skin · nickedSEVERAL NICKS ON FUSELAGE SKIN BTW STA 1000.00 TO STA 1069.75 AND BTW STGR 21RH TO STGR 27. SEVERAL NICKS ON FUSELAGE SKIN BTW STA 1000.00 TO STA 1069.75 AND BTW STGR 21RH TO STGR 27 WAS REPAIRED PER REO 690-53-61-1331 REV. --Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202402050024Skin · wornWEAR ON SETTLEMENT AREA OF FAIRING 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN. SETTLEMENT AREAS OF FAIRINGS 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01; SETTLEMENT AREAS OF Feb 6, 2024 · N567NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA202402050023Skin · wornWEAR ON SETTLEMENT AREA OF FAIRINGS 583AB, 586AB, 592AB, 595AB AND 597AB AT LH WING LOWER SKIN. SETTLEMENT AREAS OF FAIRINGS 583AB, 586AB, 592AB, 595AB AND 597AB AT LH WING LOWER SKIN WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01; SETTLEMENT AREAS OF FFeb 6, 2024 · N567NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA2024020650022Seat Track · corrodedCORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 785.15 TO FS 830.40. CORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 785.15 TO FS 830.40 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02, WAS FABRICATED PER CRJ900 SRM 53-00-49-201-002-Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202402050021Seat 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, WAS FABRICATED PER CRJ900 SRM 53-00-49-201-002-A01 AND WAS RFeb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202402050020Skin · dentedGOUGE AND DENT BELOW VENTRAL FIN FARING RH AREA BTW FS 1069.75 - FS 1088.00 AND STGR 21 - 22 RH AT REAR FUSELAGE. BELOW VENTRAL FIN FARING RH AREA BTW FS 1069.75 - FS 1088.00 AND STGR 21 - 22 RH AT REAR FUSELAGE WAS REPAIRED PER REO 690-53-00-548 REV. --Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202402050019Rib · crackedCRACK WAS FOUND ON RIB LEADING EDGE SS57.16 AT RH WING. RIB LEADING EDGE SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV - -Feb 6, 2024 · N567NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA202402050018Hinge Fitting · excess playAFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL 2103 REVFeb 6, 2024 · N567NN · Cndair CL6002D24 · Vertical StabilizerSDR VNAA202402050017Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1031.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1031.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1333 REV. --Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202402050016Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1334 REV.Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Structure
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