N602NN

Service difficulty reports · 31

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 = 'N602NN' 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 VNAA2026072521202Skin · dentedEA 5321-2026-0570 (560FH PERM REPAIR - FUSELAGE SKIN DENTED. REPAIR FOR REWORKED DENT AND GOUGE DAMAGE TO FUSELAGE SKIN PANEL BETWEEN BS 295 & BS 310, STR 13 & STR 14R. REO 690-53-21-2176 INCORPORATED.Jul 23, 2026 · N602NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA2026061218801Gcu · faultedAAN AC ESS BUS FAIL, WILL NOT TRANSFER / REMOVED AND REPLACED GCU 1 IAW AMM 24€“11€“07€“000/400€“801. OPS CHECK GOOD. PERFORMED SUCCESSFUL OPS CHECK OF ESS BUS TRANSFER SYSTEM IAW AMM 24€“51€“00€“710€“803.Jun 9, 2026 · N602NN · Cndair CL6002D24 · AC Generator-AlternatorSDR VNAA20260303015Fitting · corrodedCORROSION ON THE LOWER FITTING OF FOLDING WORKSHELF AT FWD LAVATORY. LOWER FITTING WAS REPLACED IAW CMM 25-40-19.Jan 20, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20260303014Fitting · corrodedCORRODED FLOOR FITTING ON ACCESS 107. FLOOR FITTING WAS REPLACED IAW CMM 25-33-21.Jan 20, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Equipment Attach FittingsSDR VNAA20260303012Floor Support · crackedCRACKED FLOOR SUPPORT, RBL 12, BS 221.73 - 229. THE FLOOR SUPPORT WAS REPAIRED IAW REO 690-53-11-2129, REV-.Jan 18, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20260303016Rib · crackedCRACKED MACHINED WING RIB, LEADING EDGE SS58.41, RT WING. THE RIB WAS REPAIRED IAW REO 690-57-41-240, REV -.Jan 17, 2026 · N602NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA20260303011Seat Track · corrodedTWO CORRODED SEAT TRACK SECTIONS, LBL 9, BS 581 - 677 IN THE PAX CABIN. THE SEAT TRACK SECTIONS WERE EVALUATED OUT OF LIMITS IAW SRM 53-31-49-101-001-A02, AND WERE REPLACED IAW SRM 53-00-49, CONFIG. A12.Jan 17, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260303010Seat Track · corrodedCORRODED TWO SEAT TRACK SECTIONS , BS 364 - 485, & BS 581 - 677, RBL 9 IN THE PAX CABIN. THE SEAT TRACKS WERE EVALUATED AND FOUND OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, AND SRM 53-41-49-101-001-A02, REPLACED IAW AMM 53-00-49.Jan 17, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260303009Fitting · corrodedCORROSION ON FOUR MACHINED FITTINGS IN THE FWD, CTR CARGO BAY. THE FOUR MACHINED FITTINGS WERE EVALUATED TO EXCESSIVE CORROSION IAW SRM 51-10-06-001-001-A01 AND REPLACED IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, AND SRM 51-42-10-001-001-A01.Jan 17, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20260303005Hinge · corrodedCORROSION ON THE HINGE OF ACCESS PANEL 832ET OF PASSENGER DOOR. THE HINGE WAS REPLACED ON STEP PANEL 832ET IAW SRM 51-41-02-001-001-A01.Jan 17, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Door HingeSDR VNAA20260303004Seat Track · corrodedCORROSION ON THE RT SIDE SEAT TRACK, BS 669.40 - 720.85, & BS 744.15 - 761.85 IN THE PAX CABIN. THE SEAT TRACK EVALUATED OUT OF LIMITS IAW 53-41-51-101-001-A02, AND WERE REPLACED IAW AMM 53-00-49, CONFIG. A12.Jan 16, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260303003Seat Track · corrodedCORRODED LT SIDE SEAT TRACK, BS 744.15 - 761.85, AND BS 785.15 - 847+16 IN THE PAX CABIN. THE SEAT TRACK WAS EVALUATED OUT OF LIMITS IAW SRM 53-41-51-101-001-A02, AND WAS REPLACED IAW AMM 53-00-49, CONFIG. A12.Jan 16, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260303001Web · crackedCRACKED WEB, RT SIDE BS 193, FWD E & E BAY. THE WEB WAS REPAIRED IAW SRM 53-11-43-201-001-A01.Jan 15, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20260303002Floorbeam · crackedCRACK ON FLOOR BEAM RBL12 ON FS280 BELLOW FLIGHT COMPARTMENT. FLOOR BEAM RBL12 ON FS280 BELLOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2127 REV. - -Jan 15, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Main, Floor BeamSDR VNAA20260205015Web · crackedCRACK ON WEB RH SIDE FS 193.0 AT FWD EQUIPMENT COMPARTMENT. WEB RH SIDE FS 193.0 AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER SRM 53-11-43-201-001-A01Jan 15, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA20260303008Tube · corrodedCORROSION ON DOOR SILL, BS 310 - 349 AND TUBE ASSY OF ELECTRICAL HARNESS ON BS 322.15 AT LOWER SUROUND STRUCTURE PASSENGER DOOR CUT-OUT. CORROSION REMOVED IAW SRM 51-21-06-001-001-A01 AND THE DOOR SILL WAS EVALUATED WITHIN LIMITS & THE TUBE ASSY WAS EVALUATEDJan 14, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Main, StructureSDR VNAA20260303007Rib · crackedCRACKED LT WING L/E RIB SS 15.50. THE RIB WAS REPAIRED IAW REO 690-57-41-580, REV-.Jan 14, 2026 · N602NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA20260303006Drag Angle · crackedCRACKED LT AFT DRAG ANGLE BETWEEN UNION OF FUSELAGE AND VERTICAL STABILIZER. 67.5% REAR SPAR DATUM. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.Jan 11, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Stabilizer Attach FittingsSDR VNAA20260303013Seat Track · corrodedCORRODED SEAT TRACK, RBL 9, BS 881 - 897. THE SEAT TRACK WAS EVALUATED, AND FOUND TO EXCESS DAMAGE IAW SRM 53-51-51-101-001-A02, AND REPLACED IAW AMM 53-00-49-400-801.Dec 4, 2025 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2025021011104Fadec · unserviceableR FADEC CAUTION MSG. NO ABNORMAL ENGINE INDICATIONS / REMOVED AND REPLACED RH ENG FADEC IAW AMM 73-21-01-000/400-801-A01, OPS TEST GOOD.Feb 8, 2025 · N602NN · Cndair CL6002D24 · Fuel Controlling SystemSDR VNAA202307121112Wheel · unserviceableRH IB MLG TIRE MISSING THROUGH BOLT / REMOVED AND REPLACED RH IB MLG WTA IAW CRJ 900 AMM 32-41-01-000/400-801-A01-PSA.NO DEFECTS NOTED AT THIS TIME.Jul 9, 2023 · N602NN · Cndair CL6002D24 · Wheel/Ski/FloatSDR VNAA202301280003Seat Track · corrodedCORROSION AT SEAT RAIL RBL9.00 BETWEEN FS360-485. ORROSION AT SEAT RAIL RBL9.00 BETWEEN FS360.00-FS485.00 WAS EVALUATED OUT OF LIMITSDUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-21-49-101-001-A01 AND CRJ-900SRM 53-31-49-101-001-A02 THEREFORE SECTION OF SEAT RAJan 28, 2023 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202301280002Slat Track · corrodedCORROSION ON SLAT TRACKS UPPER/LOWER,1-2 AND 2-2 AT LH WING. TRACK 2 OF SLAT 2 WAS MEASUREMENT AND WAS FOUND WITHIN LIMITS PER REO 690-57-42-950 REV-. TRACK 2 OF SLAT 1 WAS REPLACED PER CRJ-900 AMM27-81-41-000-802-A01 AND AMM 27-81-41-400-802-A01Jan 28, 2023 · N602NN · Bombdr CL6002D15 · Leading Edge DevicesSDR VNAA202301280001Skin · damagedSEVERAL NICKS AT LOWER SKIN OF AFT FUSELAGE BETWEEN FS 1015.0 AND FS 1047.0 AND BETWEEN STRG 27L AND STRG 25R. REPAIRED PER EA 23-C9-53-0053 REV. IR, SECTION III - PERMANENT REPAIRJan 28, 2023 · N602NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202301270005Seat Track · corrodedCORROSION AT SEAT RAIL RBL9.00 BETWEEN FS581.- 00-FS661+32.00. CORROSION AT SEAT RAIL RBL9.00 BETWEEN FS581.00-FS661+32.00 WAS EVALUATED OUT OF LIMITS DUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-31-49-101-001-A02 THEREFORE SECTION OF SEAT RAIL RBL9.00 BETWEEN FJan 27, 2023 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202301270004Seat Track · corrodedCORROSION AT SEAT RAIL RBL9.00 BETWEEN FS349.- 00-FS360.00. SEAT RAIL RBL9.00 BETWEEN FS349.00-FS360.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101- 001-A01 AND WAS REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A12)Jan 27, 2023 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202301270003Seat Track · corroded: CORROSION ON SEAT RAIL AT LBL 27.00 BETWEEN FS 364.00-FS485.00. SEAT RAIL AT LBL 27.00 BETWEEN FS 364.00-FS485.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A12)Jan 27, 2023 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202301270002Seat Track · corrodedINITIAL INSPECTION: CORROSION AT SEAT RAIL LBL9.00 BETWEEN FS581-FS661+32. CORROSION AT SEAT RAIL LBL9.00 BETWEEN FS581-FS661+32 WAS EVALUATED OUT OF LIMITS DUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-31-49-101- 001-A02 THEREFORE SECTION OF SEAT RAIL LBL9.00 BEJan 27, 2023 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202301270001Panel · crackedCRACK ON FWD/AFT PANEL SIDE AT CORNER FOR STEP (ACCESS 832CT), PAX DOOR. FWD/AFT PANEL SIDE AT CORNER FOR STEP (ACCESS 832CT), PAX DOOR WERE REPAIRED PER CRJ-900 SRM-52-11-04-201-004- A01.Jan 27, 2023 · N602NN · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA202107271111Filter · unserviceableON APPROACH HIGH POWER SETTING REQUIRED TO MAINTAIN SPEED AND BURNING SMELL IN COCKPIT DURING LANDING AND GROUND ROLL. PERFORMED POWER ASSURANCE CHECK W/ CREW IAW AMM 71-00-00-720-804-A02. PERFORMED OPERATIONAL TEST OF AC DISTRIBUTION SYSTEM IAW CRJ 900 AMM 21Jul 25, 2021 · N602NN · Cndair CL6002D24 · Air Distribution SystemSDR VNAA202104271113Detector · unserviceableFLAPS FAIL CAUTION MESSAGE APPEARED IN FLIGHT. CREW RAN THE QRH AND DECLARED AN EMERGENCY INTO CLT. CONDUCTED A FLAPLESS LANDING ON RWY 36C. PASSENGERS DID NOT BRACE. TRUCKS WERE ROLLED AS A PRECAUTION. FLIGHT LANDED SAFELY AND AIRCRAFT HAS BEEN CLEARED FOR THApr 25, 2021 · N602NN · Cndair CL6002D24 · Trailing Flap Position Indicating System
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