# Service difficulty reports: N600NN

A list on [N600NN](https://openairdocs.org/aircraft/N600NN.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 68 reports

- [SDR VNAA2026090224201](https://openairdocs.org/sdr/VNAA2026090224201.md): Access Panel · missing · Aug 31, 2026 · N600NN · Cndair CL6002D24 · Wing, Plate/Skin
  > ACCESS PANEL ON TOP OF LT WING MISSING (591AT). PREFORMED GVI IAW AMM 05-20-00-210-801-PSA STEP B, NO DEFECTS NOTED. INSTALLED TRAILING EDGE WEDGE IAW AMM 57-52-32-400-807-A01.
- [SDR VNAA2026050817702](https://openairdocs.org/sdr/VNAA2026050817702.md): Ecu · faulted · May 6, 2026 · N600NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP CAUTION IN FLIGHT SYSTEM DID NOT COME BACK AFTER RESETING WITH QRH PROCEDURES. / INTERROGATED MDC FOUND MULTIPLE B1 CODES FOR NWS ECU REMOVED AND REPLACED NWS ECU IAW CRJ900 AMM 32€“51€“10€“000/400-801. OPS CHECK GOOD.
- [SDR VNAA2026050417406](https://openairdocs.org/sdr/VNAA2026050417406.md): Control Wheel · unserviceable · May 2, 2026 · N600NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP CAUTION ON APPROACH PRIOR TO GEAR DOWN SELECTION. REMOVED AND REPLACED THE PILOT HAND WHEEL CONTROL IAW AMM 32-51-01-000/400-801-A01. PERFORMED OPERATIONAL TEST OF THE NOSE WHEEL STEERING IAW AMM 32-51-00-710-801-A01. THE OPERATIONAL CHECK GOOD
- [SDR VNAA2026050417204](https://openairdocs.org/sdr/VNAA2026050417204.md): Warning Message · false activation · May 1, 2026 · N600NN · Cndair CL6002D24 · Central Warning
  > STEERING INOP CAUTION IN FLIGHT. PERFORMED SYSTEM RESET PER MIPM MSG EXTINGUISHED AND DID NOT REOCCUR.
- [SDR VNAA2026042916801](https://openairdocs.org/sdr/VNAA2026042916801.md): Control Handle · inoperative · Apr 28, 2026 · N600NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP IN FLIGHT. / REMOVED AND REPLACED PILOT HAND CONTROL IAW CRJ 900 AMM 32€“51€“01€“000/400€“801. OPS CHECK GOOD.
- [SDR VNAA2026012011201](https://openairdocs.org/sdr/VNAA2026012011201.md): Windshield · cracked · Jan 16, 2026 · N600NN · Cndair CL6002D24 · Flight Compartment Windows
  > ENROUTE TO CVG THE CREW SAW A CRACK IN THE WINDSHIELD AND GOT A WINDSHIELD HEAT CAUTION MESSAGE. REMOVED AND REPLACED RH WINDSHIELD IAW CRJ-900 AMM 56-11-01-000/400-801-A01-PSA. COMPLETED FINIAL TORQUE CHECK, SEALED AND COMPLETED OPS CHECK (OPS CHECK GOOD)
- [SDR VNAA20250715034](https://openairdocs.org/sdr/VNAA20250715034.md): Skin · gouged · Jul 12, 2025 · N600NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > GOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94. GOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94 WAS REPAIRED PER REO 690-57-41-522 REV. - -.
- [SDR VNAA20250715027](https://openairdocs.org/sdr/VNAA20250715027.md): Panel · gouged · Jul 12, 2025 · N600NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > GOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94. GOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94 WAS REPAIRED PER REO 690-57-41-522 REV. - -.
- [SDR VNAA20250715023](https://openairdocs.org/sdr/VNAA20250715023.md): Seat Track · corroded · Jun 12, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FITING (PN: A414251-1) 1EA FRONT CORNER AT FWD LAV. FITTING (PN: A414251-1) 1EA FRONT CORNER AT FWD LAV WAS REPLACE PER SAFRAN CMM 25-40-40.
- [SDR VNAA20250715022](https://openairdocs.org/sdr/VNAA20250715022.md): Fitting · corroded · Jun 12, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Equipment Attach Fittings
  > CORROSION ON FLOOR FITTING (PN: CDSP2019-7C-620) 1EA ACCESS 107 COUNTER AT GALLEY 1. BRACKET FLOOR FITTING ACCESS 107 COUNTER AT GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-96
- [SDR VNAA20250715026](https://openairdocs.org/sdr/VNAA20250715026.md): Seat Track · corroded · Jun 9, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF RBL9 BTW FS581.00 TO FS693.00 (3EA). SEAT RAILS OF LBL9 BTW FS581.00 TO FS693.00 (3EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 AND SRM 51-41
- [SDR VNAA20250715025](https://openairdocs.org/sdr/VNAA20250715025.md): Seat Track · corroded · Jun 9, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF RBL9 BTW FS581.00 TO FS693.00 (3EA). SEAT RAILS OF LBL9 BTW FS581.00 TO FS693.00 (3EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 AND SRM 51-41
- [SDR VNAA20250715024](https://openairdocs.org/sdr/VNAA20250715024.md): Seat Track · corroded · Jun 9, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF RBL9 BTW FS581.00 TO FS693.00 (3EA). SEAT RAILS OF RBL9 BTW FS581.00 TO FS693.00 (3EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 AND CRJ-900
- [SDR VNAA20250715014](https://openairdocs.org/sdr/VNAA20250715014.md): Mount · corroded · Jun 9, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON ANGLE MOUNTING OF SERVICE DOOR SURROUND. ANGLE MOUNTING OF SERVICE DOOR SURROUND WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-21-23-101-002-A02 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR VNAA20250714007](https://openairdocs.org/sdr/VNAA20250714007.md): Canister · cracked · Jun 9, 2025 · N600NN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK. CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV -
- [SDR VNAA20250714009](https://openairdocs.org/sdr/VNAA20250714009.md): Seat Track · corroded · Jun 9, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (3EA). LH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (3EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49.
- [SDR VNAA20250714008](https://openairdocs.org/sdr/VNAA20250714008.md): Seat Track · corroded · Jun 9, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (4EA). RH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (4EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49.
- [SDR VNAA20250715008](https://openairdocs.org/sdr/VNAA20250715008.md): Drag Angle · cracked · Jun 8, 2025 · N600NN · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW LH DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW LH DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (T
- [SDR VNAA20250715007](https://openairdocs.org/sdr/VNAA20250715007.md): Drag Angle · cracked · Jun 8, 2025 · N600NN · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT RH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT RH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL
- [SDR VNAA20250714006](https://openairdocs.org/sdr/VNAA20250714006.md): Rib · cracked · Jun 8, 2025 · N600NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING WAS REPAIRED REO 690-57-41-240 REV --
- [SDR VNAA20250714010](https://openairdocs.org/sdr/VNAA20250714010.md): Bracket · corroded · Jun 8, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKET MACHINED FS 517.00, FS565.00 BTW STRG 26/27, FS 533.00 BTW FS549.00 STRG24/25RH AND FS629 BTW STGR 26 TO 27 LH (4 EAS) ON FWD / CTR BAGGAGE-BAY WERE EVALUATED OUT O
- [SDR VNAA20250714005](https://openairdocs.org/sdr/VNAA20250714005.md): Seat Track · corroded · Jun 8, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS AT RBL9/LBL9 FROM FS693 TO FS 1000.00 AND RBL27/LBL27 BTW FS927 TO FS1000 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. CORROSION ON SEAT RAILS AT RBL9/LBL9 FROM FS693 TO FS 1000.00 AND RBL27/LBL27 BTW FS927 TO FS1000 WAS EVALUATED OUT
- [SDR VNAA20250714004](https://openairdocs.org/sdr/VNAA20250714004.md): Seat Track · corroded · Jun 8, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 744.15 TO FS 977.00 AND STGR 15LH AT CABIN PAX. SEAT RAIL BTW FS 744.15 TO FS 977.00 AND STGR 15LH AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02 AND WERE REPLAC
- [SDR VNAA20250714003](https://openairdocs.org/sdr/VNAA20250714003.md): Seat Track · corroded · Jun 8, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 744.15 TO FS 977.00 AND STGR 15RH AT CABIN PAX. SEAT RAIL BTW FS 744.15 TO FS 977.00 AND STGR 15RH AT CABIN PAX. WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ
- [SDR VNAA20250714002](https://openairdocs.org/sdr/VNAA20250714002.md): Skin · corroded · Jun 8, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND AFTER ATG ANTENNA ON CONNECTORS SKIN SETTLEMENT AREA BTW STA: 1007. 50 STG 25R TO 26R. CORROSION WAS FOUND AFTER ATG ANTENNA ON CONNECTORS SKIN SETTLEMENT AREA BTW STA: 1007. 50 STG 25R TO 26R WAS REPAIRED PER EA 53-20-25-0854 REV. A.
- [SDR VNAA20250714001](https://openairdocs.org/sdr/VNAA20250714001.md): Doubler · corroded · Jun 8, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > CORROSION ON PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW FS1000-FS1015 AND STRINGERS 25RH-26RH AT AFT CARGO COMPARTMENT. PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW FS1000-FS1015 AND STRINGERS 25RH-26RH AT AFT CARGO COMPARTMENT WERE REPLACED P
- [SDR VNAA20250714014](https://openairdocs.org/sdr/VNAA20250714014.md): Web · cracked · Jun 7, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMP. AREA AROUND ADG PUMP WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01
- [SDR VNAA20250714015](https://openairdocs.org/sdr/VNAA20250714015.md): Retainer · worn · Jun 7, 2025 · N600NN · Bombdr CL6002D15 · Nacelle/Pylon, Main Frame
  > WEAR IN SEAL RETAINER NEAR 7-8 HRS AT LH AFT CORE COWL. SEAL RETAINER NEAR 7-8 HRS AT LH AFT CORE COWL WAS REPAIRED PER REO 690-54-13-239 REV. - A
- [SDR VNAA20250714013](https://openairdocs.org/sdr/VNAA20250714013.md): Drip Tray · corroded · Jun 7, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR PANEL SUPPORT ANGLE BTW LBL 9.00 / RBL 9.00 AT FS 280. CORROSION ON FLOOR PANEL SUPPORT ANGLE BTW LBL 9.00 / RBL 9.00 AT FS 280.00 WAS REMOVED PER CRJ/900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-21-43-101-001
- [SDR VNAA20250714011](https://openairdocs.org/sdr/VNAA20250714011.md): Plate · corroded · Jun 6, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS 645.00 AND FS 661.00 AT FWD CARGO COMPARTMENT. CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS 645.00 AND FS 661.00 AT FWD CARGO COMPARTMENT WAS EVALUATED OUT LIMITS PER CRJ 900 SRM 53-32-58-101-001-
- [SDR VNAA20250714020](https://openairdocs.org/sdr/VNAA20250714020.md): Plate · cracked · Jun 5, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON PROTECTOR PLATE ON LOWER SILL AT GALLEY SERVICE DOOR SURROUND STRUCTURE. PROTECTOR PLATE ON LOWER SILL AT GALLET SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ-900 - SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ900 SRM 51-42
- [SDR VNAA20250715003](https://openairdocs.org/sdr/VNAA20250715003.md): Skin · dented · Jun 5, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL SKIN RH SIDE BTW FS409.00 TO FS421.00 AND STGR 8RH TO 9RH AT FORWARD FUSELAGE. DENT ON EXTERNAL SKIN RH SIDE BTW FS409.00 TO FS421.00 AND STGR 8RH TO 9RH AT FORWARD FUSELAGE WAS REPAIRED PER REO 690-53-21-1980 REV.- -.
- [SDR VNAA20250715002](https://openairdocs.org/sdr/VNAA20250715002.md): Skin · worn · Jun 5, 2025 · N600NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WAS BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND SETTLE
- [SDR VNAA20250715001](https://openairdocs.org/sdr/VNAA20250715001.md): Skin · worn · Jun 5, 2025 · N600NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN WAS BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND AREA OF
- [SDR VNAA20250714018](https://openairdocs.org/sdr/VNAA20250714018.md): Skin · damaged · Jun 4, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN LIGHTNING STRIKE DAMAGE AT FASTENER LOCATION. REPAIRED PER REO 670-53-00-045 REV-K, SECTION 2
- [SDR VNAA20250714019](https://openairdocs.org/sdr/VNAA20250714019.md): Skin · damaged · Jun 4, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN LIGHTNING STRIKE DAMAGE REPAIR AROUND FASTENER COUNTERSINK. FUSELAGE SKIN LIGHTNING STRIKE DAMAGE REPAIR AROUND FASTENER COUNTERSINK WERE REPAIRED PER REO 670-53-00-045 REV-K, SECTION 3
- [SDR VNAA20250715012](https://openairdocs.org/sdr/VNAA20250715012.md): Hinge Fitting · excess play · Jun 4, 2025 · N600NN · Bombdr CL6002D15 · Rudder Structure
  > 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. REV. B
- [SDR VNAA20250715011](https://openairdocs.org/sdr/VNAA20250715011.md): Seat Track · damaged · Jun 4, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS PILOT/CO-PILOT SEAT TRACK WEAR STRIP. PILOT SEAT TRACK OB WAS REPAIRED PER REO 670-53-11-210 REV.- D AND SEAT TRACKS CO-PILOT IB AND OB AND PILOT SEAT TRACK IB MUST BE ATTENDED UNDER NRCS 00
- [SDR VNAA20250715010](https://openairdocs.org/sdr/VNAA20250715010.md): Skin · damaged · Jun 4, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > 3895FH PERM REPAIR - REQUEST FOR EXTENSION TO NEXT C CHECK OF EA 23-C9-53-1114 REV A WITHIN 3895 FLIGHT HOURS AFTER SECTION I OF REV.A, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART.// ENGINEERING COMME
- [SDR VNAA20250715009](https://openairdocs.org/sdr/VNAA20250715009.md): Seat Track · damaged · Jun 4, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS PILOT/CO-PILOT SEAT TRACK WEAR STRIP. CO-PILOT SEAT TRACK IB WAS REPAIRED PER REO 670-53-11-210 REV.- D AND SEAT TRACKS CO-PILOT OB, CAPTAIN IB AND OB MUST BE ATTENDED UNDER NRCS 00013/NRC 0
- [SDR VNAA20250714012](https://openairdocs.org/sdr/VNAA20250714012.md): Floorbeam · corroded · Jun 4, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR PANEL SUPPORT ANGLE BTW LBL 9.00 / RBL 9.00 AT FS 280. CORROSION ON FLOOR PANEL SUPPORT ANGLE BTW LBL 9.00 / RBL 9.00 AT FS 280.00 WAS REMOVED PER CRJ/900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-21-43-101-001
- [SDR VNAA20250714017](https://openairdocs.org/sdr/VNAA20250714017.md): Skin · damaged · Jun 4, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > TEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGE TO FUSELAGE SKINS WITHIN 1942 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. PERM REPAIR - FUSELAGE SKIN LIGHTNING STRIKE DAM
- [SDR VNAA20250714016](https://openairdocs.org/sdr/VNAA20250714016.md): Seat Track · damaged · Jun 4, 2025 · N600NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS PILOT/CO-PILOT SEAT TRACK WEAR STRIP. SAME PILOT SEAT TRACK IB WAS REPAIRED PER REO 670-53-11-210 REV.- D AND SEAT TRACKS CO-PILOT IB AND OB AND PILOT SEAT TRACK OB MUST BE ATTENDED UNDER NR
- [SDR VNAA20250715033](https://openairdocs.org/sdr/VNAA20250715033.md): Skin · nicked · Jun 2, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > NICK ON FUSELAGE SKIN BTW FS645.00-FS661.00 AND STGR 17LH-STGR 18LH AT FWD FUSELAGE. NICK ON FUSELAGE SKIN BTW FS645.00-FS661.00 AND STGR 17LH-STGR 18LH AT FWD FUSELAGE WAS REPAIRED PER REO 690-53-31-1024 REV.--.
- [SDR VNAA20250715032](https://openairdocs.org/sdr/VNAA20250715032.md): Skin · dented · May 31, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > PROTUBERANCE DENT ON FUSELAGE SKIN BTW FS295.00 / FS310.00 AND STGR 26RH / STGR 27 AT FWD FUSELAGE. E ACTION: PROTUBERANCE DENT ON FUSELAGE SKIN BTW FS295.00 / FS310.00 AND STGR 26RH / STGR 27 AT FWD FUSELAGE WAS REPAIRED PER REO 690-53-21-1976 REV.- -
- [SDR VNAA20250715031](https://openairdocs.org/sdr/VNAA20250715031.md): Skin · worn · May 31, 2025 · N600NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > DURING INSPECTION OF THE RC TRFKE001VY3R WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (583AB,586AB,592AB,595AB,597AB) AT LH WING LOWER SKIN. RRECTIVE ACTION: WEAR ON SETTLEMENT AREA OF FAIRINGS (583AB,586AB,592AB,595AB,597AB) AT LH WING LOWER SKIN WERE BLE
- [SDR VNAA20250715030](https://openairdocs.org/sdr/VNAA20250715030.md): Skin · nicked · May 31, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > SEVERAL NICKS ON EXTERNAL SKIN BTW FS 1015.00/FS 1051.30 AND STGR 27/STGR 24R AT REAR FUSELAGE. NICKS ON EXTERNAL SKIN BTW FS 1015.00/FS 1051.30 AND STGR 27/STGR 24R AT REAR FUSELAGE WAS BLEND OUT CRJ900 SRM 51-12-00-001-001-A01 AND FOUND SKIN BTW FS 1015/FS
- [SDR VNAA20250715029](https://openairdocs.org/sdr/VNAA20250715029.md): Skin · worn · May 31, 2025 · N600NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > DURING INSPECTION OF THE RC TRFKE001P4A1 WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (683AB,686AB,692AB,695AB,697AB) AT RH WING LOWER SKIN RECTIVE ACTION: WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (683AB,686AB,692AB,695AB,697AB) AT RH WING LOWER SK
- [SDR VNAA20250715028](https://openairdocs.org/sdr/VNAA20250715028.md): Stiffener · damaged · May 31, 2025 · N600NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > 3200FH PERM REPAIR - TEMPORARY DISPOSITION FOR MULTIPLE DAMAGE IN RH NLG WHEEL WELL & AVIONICS BAY HARNESS WITHIN 3200FH, PERFORM A PERMANENT REPAIR OR REPLACE PART(S) IAW APPROVED PROCEDURES.// ENGINEERING COMMENTS: SUBMIT A NEW RFTS & DAMAGE REPORT. ECTIVE
- [SDR VNAA20250715021](https://openairdocs.org/sdr/VNAA20250715021.md): Fitting · corroded · May 28, 2025 · N600NN · Bombdr CL6002D15 · Ailerons
  > CORROSION ON HOUSING LUGS R5, R6 AT AILERON RH. HOUSING LUGS R5, R6 AT AILERON RH WERE REPAIRED PER REO 670-57-61-237 REV - -

Next page: https://openairdocs.org/aircraft/N600NN/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N600NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N600NN/reports

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