N553NN

Service difficulty reports · 59

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 = 'N553NN' 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 VNAA2026033115301Position Sensor · false indicationPITCH FEEL CAUTION IN FLIGHT. / REMOVED AND REPLACED THE POSITION SENSOR ASSY IAW AMM 27-42-05-000/400-801. OPS CHECK OF THE POSITION ASSY WAS GOOD, NO FAULTS ARE NOTED AT THIS TIME.Mar 30, 2026 · N553NN · Cndair CL6002D24 · Elevator Tab Control SystemSDR VNAA2026040115401Pitch Control · faultedPITCH FEEL CAUTION AND STAB CH 1 INOPERATIVE. STATUS MESSAGE IN FLIGHT. PERFORMED SPOST IAW AMM 27-61-05-740-801-A03-PSA. FAULTS EXTINGUISHED.Mar 27, 2026 · N553NN · Cndair CL6002D24 · Stabilizer Control SystemSDR VNAA2026022012901Control Unit · faultedEMERGENCY RETURN TO FIELD AND STAB TRIM RUNAWAY. REMOVED AND REPLACED HORIZONTAL STAB MCU IAW AMM 27-42-07-000/400-801-A01. REMOVED AND REPLACED SSCU 1 IAW AMM 27-61-05-000/400-801-A01. OPS CHECKED IAW AMM 27-61-05-740-801. OPS CHECK GOOD NO DEFECTS NOTES.Feb 19, 2026 · N553NN · Cndair CL6002D24 · Stabilizer Control SystemSDR VNAA2025111911101Warning Message · false activationRTF-AFT CARGO DOOR CAUTION MSG AFTER TAKE OFF. PERFORMED OPS TEST OF AFT BAGGAGE DOOR IAW AMM 52-31-00-710-801.Nov 18, 2025 · N553NN · Cndair CL6002D24 · Door Warning SystemSDR VNAA20250529034Bushing · corrodedAFTER REMOVAL OF RH AILERON BUSHINGS, CORROSION WAS FOUND ON LUG BORE OF R1, R2, R5 AND R6 OF CENTER HINGE FITTINGS AND HINGE LUG INBOARD OF RIGHT AILERON. LUGS R1 & R6 WERE CLEANED PER CRJ 900 SRM TASK 51-26-00-001-001-A01 CLEANING AND NOT DAMAGE FOUND. LUGApr 29, 2025 · N553NN · Bombdr CL6002D15 · AileronsSDR VNAA20250529033Lug · corrodedAFTER REMOVAL OF RH AILERON BUSHINGS, CORROSION WAS FOUND ON LUG BORE OF R1, R2, R5 AND R6 OF CENTER HINGE FITTINGS AND HINGE LUG INBOARD OF RIGHT AILERON. AFTER REMOVAL OF RH AILERON BUSHINGS, CORROSION WAS FOUND ON LUG BORE OF R1, R2, R5 AND R6 OF CENTERApr 26, 2025 · N553NN · Bombdr CL6002D15 · AileronsSDR VNAA20250529032Access Panel · elongatedAFTER REMOTION OF FLOOR PANEL 281JLF: CRACK ON HINGE AFT/FWD, ALSO MISSING DECAL AND DEGRADED PAINT ON STEP PLATE AT AFT CARGO COMPARTMENT. FWD/AFT HINGE AT STEP PLATE AT AFT CARGO COMPARTMENT WERE REPL•A CED PER CRJ-900 SRM 51-42-06-001-001-A01, DECAL WAS Apr 25, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, StructureSDR VNAA20250529031Access Panel · elongatedELONGATED HOLE ON SETTLEMENT AREA OF ACCESS PANEL 684CB AT RH INB FLAP. ELONGATED HOLE ON SETTLEMENT AREA OF ACCESS PANEL 684CB AT RH INB FLAP WAS REPAIRED PER REO 690-57-52-527 REV.--. (THE AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTS FROM THE ISSUE DATE OFApr 24, 2025 · N553NN · Bombdr CL6002D15 · Wing, Plate/SkinSDR VNAA20250529030Canister · crackedCRACK ON CANISTER WELDED NO. 3 IN WS 148.01 AT INTERNAL LH MAIN FUEL TANK. CRACK ON CANISTER WELDED NO. 3 IN WS 148.01 AT INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. - -Apr 24, 2025 · N553NN · Bombdr CL6002D15 · Wing Miscellaneous StructureSDR VNAA20250529029Canister · crackedCRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. - -Apr 24, 2025 · N553NN · Bombdr CL6002D15 · Wing Miscellaneous StructureSDR VNAA20250529028Floorbeam · corrodedCORROSION ON FLOOR BEAM LBL 27.00 BTW FS1000-FS1069 AT AFT CARGO COMPARMENT. PAINT ON UPPER FACE OF FLOOR BEAM LBL ON FLOOR BEAM LBL 27.00 BTW FS1000 TO FS1010 AND FS 1069 TO FS1057 AT AFT CARGO COMPARMENT WAS REMOVED PER CRJ900 SRM 51-26-01-001-001-A01, WAApr 23, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20250529023Frame · corrodedCORROSION ON FRAME AND ATTACH FLANGE FS1047.00 BTW STGR 24L-26L AT AFT CARGO COMPARTMENT . EVALUATED DAMAGE ON FRAME AND ATTACH FLANGE FS1047.00 BTW STGR 24L-26L AT AFT CARGO COMPARTMENT ITS NOT ALLOWED PER CRJ900 SRM 53-61-06-101-003-A02 AND REPAIRED PER REApr 23, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA20250529022Shear Panel · crackedCORROSION ALONG SHEAR PANEL BTW FS1088.20-FS1098.20 AT AFT CARGO COMPARTMENT. CORROSION ALONG SHEAR PANEL BTW FS1088.20-FS1098.20 AT AFT CARGO COMPARTMENT WAS REMOVED AND FOUND WITHIN LIMITS PER REO 670-53-61-1080 REV. - -.Apr 23, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250529021Floorbeam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RBL 12 TO CROSSBEAM FS280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM RBL 12 TO CROSSBEAM FS280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1987 REV - -Apr 23, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20250529020Floorbeam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LBL 12 TO CROSSBEAM FS280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT . COCKPIT FLOOR LONGITUDINAL BEAM LBL 12 TO CROSSBEAM FS280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1988 REV - -Apr 23, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20250529024Rib · crackedCRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING. CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING WAS REPAIRED PER REO 690-57-51-362 REV - -Apr 22, 2025 · N553NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA20250529019Intercostal · corrodedCORROSION ON INTERCOSTAL BTW FS310 TO FS319 AND STGR 20RH SIDE ON INTERNAL FUSELAGE STRTUCTURE. DUE TO EXCESIVE DAMAGE INTERCOSTAL BTW FS310 TO FS319 AND STGR 20RH IS OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 THEREFORE WAS REPLACED PER CRJ900 SRM 51Apr 22, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250529018Door Frame · corrodedCORROSION ON LOWER SURROUND STRUCTURE BTW FS519.64 TO FS562.63 AND STGR26 TO STGR25 LH SIDE AT FWD BAGGAGE BAY DOOR. LOWER SURROUND STRUCTURE BTW FS519.64 TO FS562.63 AND STGR26 TO STGR25 LH SIDE AT FWD BAGGAGE BAY DOOR WAS REPAIRED PER REO 690-53-31-983 REV.Apr 22, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, StructureSDR VNAA20250529017Seat Track · corrodedCORROSION ON SIDE SEAT RAIL (4 EAS) BTW FS 379.00 TO FS 669.40 AND STGR 15RH AT CABIN PAX. EVALUATED,SIDE SEAT RAIL (4 EAS) BTW FS 379.00 TO FS 669.40 AND STGR 15RH ARE OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 AND REPLAApr 22, 2025 · N553NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250529016Seat Track · corrodedCORROSION ON SIDE SEAT RAIL (5 EAS) BTW FS 379.00 TO FS 669.40 AND STGR 15LH AT CABIN PAX. EVALUATED, SIDE SEAT RAIL (5 EAS) BTW FS 379.00 TO FS 669.40 AND STGR 15LH ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND REPApr 22, 2025 · N553NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250529015Seat Track · corrodedCORROSION ON SEAT TRACKS LBL 27 (1E/A), RBL 9 (1E/A) AND LBL 9 (1E/A) BTW FS349.00 TO FS477.40 AT CABIN PAX. EVALUATED, SEAT TRACKS LBL 27 (1E/A), RBL 9 (1E/A) AND LBL 9 (1E/A) BTW FS349.00 TO FS477.40 AT CABIN PAX DUE TO EXCESIVE DAMAGE PER CRJ 900 SRM 53Apr 22, 2025 · N553NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250529014Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL (7 EAS) AT STGR 15 LH, BTW FS669.40 TO FS977.00 AT CABIN PAX. EVALUATED, LH SIDE SEAT RAIL (7 EAS) AT STGR 15 LH, BTW FS669.40 TO FS977.00 ARE OUT OFF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 ANApr 22, 2025 · N553NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250529013Seat Track · corrodedCORROSION ON SEAT RAIL ON LBL 27 (2 EAS),LBL9 (4 EAS) AND RBL9 (5 EAS) BTW FS 477.40 TO FS693.00 AT CABIN PAX. EVALUATED, SEAT RAIL ON LBL 27 (2 EAS),LBL9 (4 EAS) AND RBL9 (5 EAS) BTW FS 477.40 TO FS693.00 AT CABIN PAX DUE TO EXCESIVE DAMAGE PER CRJ-900 SRM Apr 22, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250529027Floorbeam · corrodedCORROSION ON FLOOR BEAM LBL 9.00 BTW FS1000-FS1069 AT AFT CARGO COMPARMENT. PAINT ON UPPER FACE OF FLOOR BEAM LBL 9.00 BTW FS 1000 TO FS 1010 AND FS 1069 TO FS 1056 AT AFT CARGO COMPARMENT WAS REMOVED PER CRJ900 SRM 51-26-01-001-001-A01, WAS EVALUATED, AFTERApr 21, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20250529026Floorbeam · corrodedCORROSION ON CROSSBEAM SECTION (FS280) BTW LBL 9.00 / RBL 9.00. CROSS BEAM FS.280 R/H WAS CLEANED AND NOT DAMAGED WAS FOUND PER CRJ-900 SRM 51-26-00-001-001-A01, EVALUATED WAS DUE EXCESSIVE CORROSIÓN ON LH CROSS BEAM FS.280 AT COCKPIT CABIN FLOOR WAS FOUND OFApr 21, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20250529025Bracket · corrodedCORROSION ON MACHINED BRACKETS (8 E/A'S) AND FWD/AFT PLATE AT FWD CARGO COMPARTMENT. PAINT ON MACHINED BRACKETS (4 E/A'S) ON FS.517 TO FS.661+16 AND STGR.22LH AND STGR.21LH AND FWD/AFT PLATE AT FWD CARGO COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-26-01-001-0Apr 21, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250529006Floorbeam · corrodedCORROSION ON FLOORBEAM FS280 BTW LBL9.00 / RBL9.00 AT PILOTS CABIN STRUCTURE. EXCESSIVE CORROSION ON FLOORBEAM FS280 BTW LBL9.00 / RBL9.00 WAS EVALUATED PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 5Apr 21, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20250529005Stringer · corrodedCORROSION OVER STGR27 BTW FS280 / FS310 AT MAIN AVIONICS COMPARTMENT. REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, EVALUATED,THEREFORE OUT OF LIMITS PER CRJ900 SRM 53-21-03-101-002-A04 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-4Apr 21, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250529004Web · crackedDISCREPANCY: CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE FS193.00. CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01Apr 21, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250529003Valve · wornWEAR ON FLOATATION VALVE AT AFT ACCESSORIES COMPARTMENT BULKHEAD FS 1098. FLOATATION VALVE AT AFT ACCESSORIES COMPARTMENT BULKHEAD FS 1098 WAS REPLACED PER CRJ900 AMM 21-32-02 CONFIG. A02Apr 20, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250529002Hinge · corrodedCORROSION AND CRACK ON HINGE OF ACCESS PANEL 832AT. EXCESSIVE DAMAGE ON HINGE OF ACCESS PANEL 832AT PER CRJ900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ900 SRM 51-41-02-001-001Apr 20, 2025 · N553NN · Bombdr CL6002D15 · Fuselage, Door HingeSDR VNAA20250529001Support · wornWEAR ON FLAP FITTING AND PLATE SUPPORT OF "FLAP STUB FAIRING" 171DL AND 172DR AT RH/LH WING TRAILING EDGE ROOT WING. DUE EXCESSIVE DAMAGE ON FLAP FITTING AND PLATE SUPPORT OF "FLAP STUB FAIRING" 171DL AND 172DR AT RH/LH WING TRAILING EDGE (ROOT WING) WERE FOApr 20, 2025 · N553NN · Bombdr CL6002D15 · Trailing Edge FlapsSDR VNAA20250528006Skin · corrodedWEAR ON SKIN PANEL LOWER SECTION OF FUSELAGE BTW FS 910.00/919.00 STGR 27/26RH. BLENDED OUT ON SKIN PANEL LOWER SECTION OF FUSELAGE BTW FS 910.00/919.00 STGR 27/26RH WAS PERFORMED PER CRJ-900 SRM 51-12-00-001-001-A01 AND EVALUATED, THEREFORE IS WITHIN LIMITS IApr 20, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA20250528005Angle · corrodedCORROSION ON MID CAP AND KICKPLATE BTW FS 310.00 TO FS 349.00 AT LOWER SORROUND STRUCTURE PASSENGER DOOR. EVALUATED WERE DUE TO EXCESSIVE CORROSION, KICKPLATE AND MID CAP ON LOWER SORROUND STRUCTURE PASSENGER DOOR PER CRJ900 SRM 53-21-23-101-001-A02 AND REPApr 20, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250529011Hinge Fitting · gougedLH WING SPS21.80 OUTBOARD HINGE FITTING GOUGE. LH WING SPS21.80 OUTBOARD HINGE FITTING GOUGE WAS REPAIRED PER REO 690-57-51-425 REV. --Apr 18, 2025 · N553NN · Bombdr CL6002D15 · Wing Main, Frame StructureSDR VNAA20250529010Hinge Fitting · gougedRH WING WS24.50 OUTBOARD HINGE FITTING GOUGED. RH WING WS24.50 OUTBOARD HINGE FITTING GOUGE WAS REPAIRED PER REO 690-57-51-420. REV --Apr 18, 2025 · N553NN · Bombdr CL6002D15 · Wing Main, Frame StructureSDR VNAA20250529009Skin · corrodedCORROSION DAMAGE TO FUSELAGE SKIN BETWEEN FS280.00-FS295.00 AND STR24R-STR25R. CORROSION DAMAGE TO FUSELAGE SKIN BETWEEN FS280.00-FS295.00 AND STR24R-STR25R WAS REPAIRED PER REO 690-53-21-1933 REV. - - .Apr 18, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA20250529008Bracket · cracked2900 FH PERM REPAIR - TEMPORARY DISPOSITION FOR DENT DAMAGE TO INBD LOWER WING T/E SKIN BETWEEN WSTA14.500 AND WSTA50.000, RHS SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 2900 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO. WITHIN 2900 FLIGHT HOApr 18, 2025 · N553NN · Bombdr CL6002D15 · Wing Miscellaneous StructureSDR VNAA20250529007Bracket · crackedCRACK ON BRACKET OF AFT RAIL AT AFT CARGO COMPARTMENT DOOR FS 1047.00, BTW STGR 16LH AND STGR 17LH. BRACKET OF AFT RAIL AT AFT CARGO COMPARTMENT DOOR FS 1047.00, BTW STGR 16LH AND STGR 17LH WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01. AND SRM 51-42-06-Apr 18, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20250528004Skin · dentedDENT ON EXTERNAL SKIN BTW FS295.00 TO FS 310.00 AND STGR 19RH TO STGR 20RH AT FWD FUSELAGE. DENT ON EXTERNAL SKIN BTW FS295.00 TO FS 310.00 AND STGR 19RH TO STGR 20RH AT FWD FUSELAGE WAS REPAIRED PER REO 670-51-00-085 REV.-A AND PER REO 690-53-21-1941 REVApr 18, 2025 · N553NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA20250528003Skin · wornWEAR ON FIXED LEADING EDGE (622AR, 622BR, 631AR) AT RH WING. WEAR ON FIXED LEADING EDGE (622AR, 622BR, 631AR) WERE REPAIRED PER REO 690-57-41-501 REV. - -, REO 690-57-41-503 REV. - - AND REO 690-57-41-504 REV-.Apr 18, 2025 · N553NN · Bombdr CL6002D15 · Wing, Plate/SkinSDR VNAA20250528002Skin · dentedSEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING WERE BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01, WAS EVALUATED, AREA ON LOWER SKIApr 18, 2025 · N553NN · Bombdr CL6002D15 · Trailing Edge FlapsSDR VNAA20250528001Hinge Fitting · gougedRH WING SPS21.80 OUTBOARD HINGE FITTING GOUGE. RH WING SPS21.80 OUTBOARD HINGE FITTING GOUGE WAS REPAIRED PER REO 690-57-51-421 REV --.Apr 18, 2025 · N553NN · Bombdr CL6002D15 · Wing StructureSDR VNAA20250529012Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL (7 EAS) AT STGR 15 RH, BTW FS669.40 TO FS977.00 AT CABIN PAX. EVALUATED, RH SIDE SEAT RAIL (7 EAS) AT STGR 15 RH, BTW FS669.40 TO FS977.00 ARE OUT OFF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AApr 4, 2025 · N553NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202307051114Acm · unserviceableR PACK AUTO FAIL CAUTION MESSAGE AND R PACK TEMP CAUTION MESSAGE WHEN WE LANDED RAN QRH SMOKE SEEN AND SMELLED IN THE CABIN / REMOVED AND REPLACED TEMP CONTROL VALVE AND ACM IAW CRJ AMM 21-51-20-000/400-801 AND 21-51-08-000/400-801. OPS CHECK AND LEAK CHECK GOJul 3, 2023 · N553NN · Cndair CL6002D24 · Cabin Cooling SystemSDR VNAA202301111111Transducer · leakingHYD SYS 2 LO PRESS IN FLT, INBD FLT SPOILER/SPLRONS / AFTER INSPECTION FOUND HYD SYS 2 PRESSURE MANIFOLD TRANSDUCER TO BE LEAKING. REMOVED AND REPLACED TRANSDUCER IAW CRJ900 AMM 29-31-01-000/400-801."Jan 9, 2023 · N553NN · Cndair CL6002D24 · Hydraulic Power Accumulator, MainSDR VNAA202111261111Unknown · odorFUEL SMELL IN AFT OF CABIN / PERFORMED WALK THROUGH-AROUND. NO SIGNS OF FUEL LEAKS OR SMELLS."Nov 22, 2021 · N553NN · Cndair CL6002D24 · Air Distribution SystemSDR VNAA202111129995Rib · crackedCRACK ON RH WING LE RIBAT SS 57.16Nov 12, 2021 · N553NN · Cndair CL6002D24 · Fuselage Main, BulkheadSDR VNAA202104011111Flap System · malfunctionedRETURN TO FIELD FLAPS OVERSPEED AUDIO CLICKING CAME ON DURING CLIMBOUT. THEY RETURNED TO FIELD AND LANDED WITH NO OTHER ISSUES. CLEARED INHIBITS IAW CRJ 900 AMM 45-45-00-970-821 (A01). SWAPPED SFECUS IAW CRJ 900 AMM 27-50-00-710-801. PERFORMED OPERATIONAL CHECMar 30, 2021 · N553NN · Cndair CL6002D24 · Trailing Edge Flap Control SystemSDR VNAA2020082311101Acm · failedFLIGHT 5316 CLT-LYH DECLARED EMERGENCY ON FINAL APPROACH FOR SMOKE IN THE CABIN, AIRCRAFT WAS BALE TO LAND SAFELY AND TAXI OFF RUNWAY NO ISSUES. AIRCRAFT MET BY FIRE AND RESCUE ON TAXI WAY NO INDICATION OF FIRE. AIRCRAFT PROCEEDED TO TAXI TO GATE AND DEPLANE NAug 19, 2020 · N553NN · Cndair CL6002D24 · Cabin Cooling System
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