N616NN

Service difficulty reports · 37

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 = 'N616NN' 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 VNAA2026060918702Pump · unserviceableEDP 1A FAIL DURING CRUISE / REMOVED AND REPLACED HYD SYSTEM #1 EDP IAW CRJ900 AMM TASK(S) 29-11-01-000/400-801-A01-PSA. OPS CHECKS GOOD, NO FURTHER DISCREPANCIES NOTED AT THIS TIME.Jun 8, 2026 · N616NN · Cndair CL6002D24 · Hydraulic Pump (Electric/Engine), MainSDR VNAA2026051918101Acm · failedEVACUATION DUE TO CABIN SMOKE AND BURNING SMELL / TROUBLESHOOT IAW CRJ FIM 21-22-00-810-806. PERFORMED OPS TEST OF THE AIR CONDITIONING DISTRIBUTION SYSTEM IAW CRJ AMM 21€“50€“00€“862€“801 AND FOUND R PACK AUTO FAIL. PERFORMED INSPECTION OF RH AND LH WIMay 15, 2026 · N616NN · Cndair CL6002D24 · Cabin Cooling SystemSDR VNAA2025110411102Relief Valve · inoperativeGEAR DISAGREE WARNING IN FLIGHT. / REMOVED AND REPLACED MLG SELECTOR VALVE IAW CRJ 900 AMM 32-32-10-000/400-801. REMOVED AND REPLACED #3 BALANCE RELIEF VALVE IAW CRJ 900 AMM 29-12-05-000/400-802. LEAK CHECK AND OPS CHECK GOOD. THIS CLEARS MELOct 30, 2025 · N616NN · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR VNAA2025081111101Smoke Detector · false activationCAPTAIN SAW A SMOKE IN THE AFT LAV MESSAGE POPPED UP. PERFORMED OPS CHECK OF AFT LAV SMOKE DETECTOR IAW AMM 26-16-00-710-801-A01-PSA. OPS CHECK GOOD.Aug 8, 2025 · N616NN · Cndair CL6002D24 · Smoke DetectionSDR VNAA202302040025Skin · scratchedSCRATCHES ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5% BTW STGR 22LH TO STGR 21LHMar 27, 2023 · N616NN · Cndair CL6002D24 · Standard Practices/StructuresSDR VNAA202302040009Support Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL. (SM) SUMMARY: CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL WERE EVALUATED PER CRJ-900 SRM 53-00-00-101-001-A01 AND WERE REMar 27, 2023 · N616NN · Cndair CL6002D24 · Fuselage Structure (General)SDR VNAA202302040032Angle · crackedCRACK AT FWD SUPPORT ANGLE 2EA OF UPPER ACCUMULATOR AT NOSE HYDRAULICS COMPARTMENTMar 27, 2023 · N616NN · Cndair CL6002D24 · Standard Practices/StructuresSDR VNAA202302040005Skin · corrodedCORROSION ON LEADING EDGE (LIP SKIN) OF RH ENGINE INLET COWL LEADING EDGE (LIP SKIN) OF RH ENGINE INLET COWL WAS REPAIRED PER EA 23-C9-55-0324 REV. IR.SECTION III-PERMANENT REPAIRMar 26, 2023 · N616NN · Cndair CL6002D24 · Nacelle/Pylon, Plate/SkinSDR VNAA202302040004Skin · nickedSEVERAL NICKS ON EXTERNAL FUSELAGE SKIN BTW FS 1000.00 TO FS 1047.00, BTW STGR 27 TO STGR 22 RH NICKS ON EXTERNAL FUSELAGE SKIN BTW FS 1000.00 TO FS 1047.00, BTW STGR 27 TO STGR 22 RH WERE REPAIRED PER EA 23-C9-53-0319 REV. IR SECTION III - PERMANENT REPAIRMar 26, 2023 · N616NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202302040026Skin · dentedDENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH TO STGR 21LHMar 25, 2023 · N616NN · Cndair CL6002D24 · Standard Practices/StructuresSDR VNAA202302040001Skin Panel · nickedSEVERAL NICKS ON LOWER/FWD FACE OF LH/RH INBOARD FLAP FROM FLS 15.00 TO FLS 65.50Mar 25, 2023 · N616NN · Cndair CL6002D24 · Trailing Edge FlapsSDR VNAA202302040015Slat Track · corrodedCORROSION ON SLAT TRACK LOWER SURFACE 3-2, RH WING SLAT #3. CORROSION ON SLAT TRACK LOWER SURFACE 3-2, RH WING SLAT #3. WAS REPAIRED PER REO 690-57-42-966 REV --Mar 24, 2023 · N616NN · Cndair CL6002D24 · Leading Edge Slat Control SystemSDR VNAA202302040014Slat Track · corrodedCORROSION ON SLAT TRACK LOWER SURFACE 3-2, LH WING SLAT #3 CORROSION ON SLAT TRACK LOWER SURFACE 3-2, LH WING SLAT #3 WAS REPAIRED PER REO 690-57-42-965 REV --Mar 24, 2023 · N616NN · Cndair CL6002D24 · Leading Edge Slat Control SystemSDR VNAA202302040003Frame · corrodedCORROSION ON FWD INNER HANDLE FRAME OF FORWARD BAGGAGE-BAY DOOR INTERAL STRUCTURE FWD INNER HANDLE FRAME OF FORWARD BAGGAGE-BAY DOOR INTERAL STRUCTURE WAS REPAIRED PER REO 690-52-35-329 REV --Mar 24, 2023 · N616NN · Cndair CL6002D24 · Cargo/Baggage DoorsSDR VNAA202302040033Fireshield · damagedDURING FORWARD CORE COWL FIRESHIELD DAMAGE REPAIR WITH NRC 00089, HONEYCOMB CORE FORWARD EDGE WAS DRILLED (4 BY 4 INCH SQUARE)Mar 24, 2023 · N616NN · Cndair CL6002D24 · Nacelle/Pylon StructureSDR VNAA202302040011Channel · corrodedCORROSION ON SEAL RETAINER STRIP (NUTS STRIP) ON LH/RH WING-TO-FUSELAGE SEAL (VIEW FROM WHEEL WELL AREA) ON WING TRAILING EDGE SEALS. (AYP) SEAL RETAINER STRIP (NUTS STRIP) ON LH/RH WING-TO-FUSELAGE SEAL WERE REPLACED PER PER EA 23-C9-57-0305 REV A. SECTIMar 23, 2023 · N616NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202302040029Hinge Fitting · corrodedAFTER BUSHING REMOVAL CORROSION WAS FOUND ON LUGS (4EAS) AT LH AILERON HINGE #2 AND HINGE #3Mar 22, 2023 · N616NN · Cndair CL6002D24 · Wing StructureSDR VNAA202302040030Hinge Fitting · corrodedAFTER BUSHING REMOVAL CORROSION WAS FOUND ON LUGS 4EA AT RH AILERON HINGE #2 AND HINGE #3Mar 22, 2023 · N616NN · Cndair CL6002D24 · Wing StructureSDR VNAA202302040007Skin · wornWEAR ON EXTERNAL FUSELAGE SKIN BTW FS 897.00 TO FS 913.00, BTW STGR 27 TO STGR 26LH EXTERNAL FUSELAGE SKIN BTW FS 897.00 TO FS 913.00, BTW STGR 27 TO STGR 26LH WAS REPAIRED PER EA 23-C9-53-0266 REV. IR AND REO 670-53-00-290 REV. -FMar 21, 2023 · N616NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202302040031Door · damagedDURING HEAT EXCHANGER REPLACEMENT TEST, HOSE BURSTED AT THE CONNECTION OF THE GROUND PNEUMATIC PLANT, AND ACCESS DOOR 311AL WAS BENDEDMar 18, 2023 · N616NN · Cndair CL6002D24 · DoorsSDR VNAA202302040002Skin Panel · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN BTW FS 333.00 TO FS 349.00, BTW STGR 25RH TO STGR 23RH EXTERNAL FUSELAJE SKIN BTW FS 333.00 TO FS 349.00, BTW STGR 25RH TO STGR 23RH WAS REPAIRED PER EA 23-C9-53-0270 REV.IR SECTION III-PERMANENT REPAIR.Mar 15, 2023 · N616NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202302040010Support Angle · corrodedCORROSION ON MLG ELECTRICAL/HYDRAULIC PROTECTIVE COVER SUPPORT ANGLE (SETTLEMENT AREA OF ACCESS PANEL 642AZ/542AZ) ON LH/RH MLG WHEEL WELL MLG ELECTRICAL/HYDRAULIC PROTECTIVE COVER SUPPORT ANGLES SETTLEMENT AREA OF ACCESS PANELS 642AZ/542AZ ON LH/RH MLG WHEMar 12, 2023 · N616NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202302040028Vane · damagedELONGATED HOLE ON ACCESS PANEL 684ETMar 6, 2023 · N616NN · Cndair CL6002D24 · Standard Practices/StructuresSDR VNAA202302040019Seat Track · corrodedCORROSION AT SEAT RAIL LBL9 BETWEEN FS485-FS581Mar 5, 2023 · N616NN · Cndair CL6002D24 · Fuselage Structure (General)SDR VNAA202302040018Seat Track · corrodedCORROSION AT SEAT RAIL RBL9 BETWEEN FS661+32 - FS683.5 DUE TO CORROSION NOT ALLOWABLE DAMAGE (SECTION CROSS) ON SEAT RAIL RBL9 BETWEEN FS661+32 - FS683.5 WAS REPLACED PER CRJ-900 SRM 53-31-49-101-001-A02 AND CRJ-900 AMM 53-00-49Mar 5, 2023 · N616NN · Cndair CL6002D24 · Fuselage Internal Mounting StructureSDR VNAA202302040020Seat Track · corrodedCORROSION AT SEAT RAIL LBL9 BETWEEN FS581-FS661+32Mar 5, 2023 · N616NN · Cndair CL6002D24 · Fuselage Structure (General)SDR VNAA202302040017Seat Track · corrodedCORROSION AT SEAT RAIL RBL9 BETWEEN FS581- FS661+32. DUE TO CORROSION NOT ALLOWABLE DAMAGE (SECTION CROSS) ON SEAT RAIL RBL9 BETWEEN FS581- FS661+32.WAS REPLACED PER CRJ-900 SRM 53-31-49-101-001-A02 AND CRJ-900 AMM 53-00-49Mar 5, 2023 · N616NN · Cndair CL6002D24 · Fuselage Internal Mounting StructureSDR VNAA202302040016Seat Track · corrodedORROSION AT SEAT RAIL RBL9 BETWEEN FS485 - FS581.. DUE TO CORROSION NOT ALLOWABLE DAMAGE (SECTION CROSS) ON SEAT RAIL RBL9 BETWEEN FS485 - FS581. WAS REPLACED PER CRJ-900 SRM 53-31-49-101-001-A02 AND CRJ-900 AMM 53-00-49Mar 5, 2023 · N616NN · Cndair CL6002D24 · Fuselage Internal Mounting StructureSDR VNAA202302040021Seat Track · corrodedCORROSION AT SEAT RAIL LBL9 BETWEEN FS661+32-FS683.5Mar 5, 2023 · N616NN · Cndair CL6002D24 · Fuselage Structure (General)SDR VNAA202302040022Seat Track · corrodedCORROSION AT SEAT RAIL LBL9 BETWEEN FS349 TO FS485Mar 5, 2023 · N616NN · Cndair CL6002D24 · Fuselage Structure (General)SDR VNAA202302040023Seat Track · corrodedCORRSION AT SEAT RAIL LBL9 BTW FS379 TO FS485Mar 5, 2023 · N616NN · Cndair CL6002D24 · Fuselage Structure (General)SDR VNAA202302040024Access Panel · corrodedCORROSION ON ACCESS PANEL 622DZ, 542AZ, 642AZ, 542BZ AND 642BZFeb 27, 2023 · N616NN · Cndair CL6002D24 · Wing StructureSDR VNAA202302040027Access Panel · corrodedCORROSION ON ACCESS PANEL 542BZFeb 27, 2023 · N616NN · Cndair CL6002D24 · Standard Practices/StructuresSDR VNAA202302040013Web · corrodedCORROSION ON MACHINED SUPPORT ANGLE OF MAIN LANDING GEAR WHEEL BIN MOUNTING STRUCTURE AT RBL/LBL 16 ON RH/LH WHEEL WELL AREA. CORRECTIVE ACTION: MACHINED SUPPORT ANGLES WERE REPAIRED PER REO 690-53-83-068 REV.-AFeb 24, 2023 · N616NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202302040012Intercostal · corrodedCORROSION ON TIRE BURST COVER INTERCOSTAL (2 EAS, INB/OUTB FACE OF INTERCOSTAL) ON SUPPORT STRUCTURE OF ACCESS PANNEL 642AZ/542AZ ON WHEEL WELL AREA RH/LH. TIRE BURST COVER INTERCOSTAL LH WAS EVALUATED WITHIN OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 ANDFeb 23, 2023 · N616NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202302040008Support · corrodedCORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA, RBL 45/LBL 45 CORRECTIVE ACTION: SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA, RBL 45/LBL 45 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101Feb 23, 2023 · N616NN · Cndair CL6002D24 · Fuselage Structure (General)SDR VNAA202302040006Connector · corrodedCORROSION ON CONNECTORS & BACKSHELSL, AT LH/RH WING REAR SPAR CORRECTIVE ACTION: BACKSHELLS AND CONNECTORS OF LWP1 AND RWP1 POSITIONS AT LH/RH WING REAR SPAR WERE CLEANED AND REPLACED PER CRJ-900 ESPM 20-26-00 AND PER CRJ-900 ESPM 20-14-00. ALL TEST OK.Feb 23, 2023 · N616NN · Cndair CL6002D24 · Miscellaneous Wiring
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