# Service difficulty reports: N596NN

A list on [N596NN](https://openairdocs.org/aircraft/N596NN.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 · 57 reports

- [SDR VNAA2026092525905](https://openairdocs.org/sdr/VNAA2026092525905.md): Windshield · smoke · Sep 24, 2026 · N596NN · Cndair CL6002D24 · Flight Compartment Windows
  > SPARKS AND SMOKE EMITTING FROM LOWER LEFTHAND WINDSHIELD IN FLIGHT L WINDSHIELD HEAT CAUTION. REMOVED LH WINDSHIELD IAW CRJ9 AMM 56-11-01-000-801-A01.REMOVED AND REPLACED LH W/S CONTROLLER IAW CRJ 900 AMM 30-41-06-000/400-801
- [SDR VNAA2026080722301](https://openairdocs.org/sdr/VNAA2026080722301.md): Brake · locked · Aug 5, 2026 · N596NN · Cndair CL6002D24 · Landing Gear Brake System
  > SUSPECT RH OUTBOARD BRAKE LOCKED UP DURING PUSHBACK / INSP BRAKE ASSY IAW CRJ-900 AMM 32-43-26-210-801-PSA. FOUND SHEARED PUCK MATERIAL.REMOVED AND REPLACED RH OB BRAKE UNIT IAW CRJ 900 AMM32-43-26-000/400-A02-PSA, OPS CHECK AND LEAK CHECK GOOD.
- [SDR VNAA2025111711103](https://openairdocs.org/sdr/VNAA2025111711103.md): Computer · unserviceable · Nov 16, 2025 · N596NN · Cndair CL6002D24 · Attitude and Direction Data System
  > DURING CLIMB OUT, LEFT PFD ATTITUDE INDICATOR REMOVED, RED FD, ATT,AND HDG FLAGS DISPLAYED ON PFD, ACCOMPANIED WITH AUTOPILOT DISCONNECT AND YD 1 INOPERATIVE AND PITCH FEEL FAULT STATUS MESSAGES. INTERROGATED MDC FOUND B1 CODE 005923 AND MULTIPLE OTHER ONES W
- [SDR VNAA2025090711101](https://openairdocs.org/sdr/VNAA2025090711101.md): Manifold · unserviceable · Sep 5, 2025 · N596NN · Cndair CL6002D24 · Steering Unit
  > STEERING INOP UPON TAKE OFF. FAULT HAPPENED UPON GEAR UP. / REPLACED STEERING MANIFOLD IAW AMM 32-51-50-400-801-A01. NO LEAK NOTED. BITE AND OPS TEST GOOD AT THIS TIME.
- [SDR VNAA2025081811101](https://openairdocs.org/sdr/VNAA2025081811101.md): Steering Sys · inoperative · Aug 12, 2025 · N596NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP CAUTION MSG ON TAKEOFF. / CYCLED SYSTEM CB'S, PROBLEM DID NOT REOCCUR.
- [SDR VNAA2025022811102](https://openairdocs.org/sdr/VNAA2025022811102.md): Skin · gouged · Feb 28, 2025 · N596NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE LOWER SKIN PANEL, GOUGING BETWEEN FS1031 - FS1040 AND S-21R - S-26R / INCORPORATED PERMANENT REPAIR REO 690-53-61-1516 REV -- TO THE FUSELAGE FS 1000.00 - FS 1051.30 & STR 20R - STR 27. (MHI MRT STATEMENT OF WORK ORDER # MIS-6305)
- [SDR VNAA2025021811101](https://openairdocs.org/sdr/VNAA2025021811101.md): Door · damaged · Feb 14, 2025 · N596NN · Cndair CL6002D24 · Service Doors
  > LOW PRESSURE AIR DOOR OPENS IN-FLIGHT POSSIBLE DAMAGE AFT OF DOOR / INSPECTED DAMAGE IN LP GROUND CONNECTION AREA IAW CRJ 900 SRM 53-61-01-001-003-A02. DAMAGE IS FOUND TO BE OUTSIDE OF LIMITS. CONDUCTED DAMAGE MAPPING OF AREA AND SUBMITTED TO ENGINEER. C/W DIR
- [SDR VNAA20241213003](https://openairdocs.org/sdr/VNAA20241213003.md): Hinge Fitting · corroded · Nov 28, 2024 · N596NN · Bombdr CL6002D15 · Galley Doors
  > DISCREPANCY: CORROSION ON HINGES AND HINGE FITTINGS AT AFT LAVATORY SERVICE DOOR 196ER
- [SDR VNAA202412150020](https://openairdocs.org/sdr/VNAA202412150020.md): Hinge · damaged · Nov 12, 2024 · N596NN · Cndair CL6002D24 · Passenger/Crew Doors
  > DAMAGE ON PAX DOOR HINGE (FUSELAGE SIDE) LUG LAND PAX DOOR HINGE (FUSELAGE SIDE) LUG LAND WAS REPAIRED PER REO 670-53-21-582 REV -F
- [SDR VNAA202412150019](https://openairdocs.org/sdr/VNAA202412150019.md): Skin · dented · Nov 8, 2024 · N596NN · Cndair CL6002D24 · Fuselage Main, Structure
  > SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH AND RH VENTRAL FIN FAIRINGS. CORRECTIVE ACTION: SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH AND RH VENTRAL FIN FAIRINGS WERE REPAIRED PER REO 670-51-00-085 REV -A, REO 690-53
- [SDR VNAA202412150018](https://openairdocs.org/sdr/VNAA202412150018.md): Rail · corroded · Nov 7, 2024 · N596NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15LH BTW FS 379.00 TO FS 469.00 SIDE SEAT RAIL STGR 15LH BTW FS 379.00 TO FS 469.00 IS OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202412150017](https://openairdocs.org/sdr/VNAA202412150017.md): Hinge · worn · Nov 7, 2024 · N596NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous 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 VNAA202412150016](https://openairdocs.org/sdr/VNAA202412150016.md): Floorbeam · corroded · Nov 7, 2024 · N596NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > DURING REMOVAL AT FLOOR PANEL SUPPORT IN FS280.00, CORROSION WAS FOUND ON RH CROSSBEAM OF FS 280. RH CROSSBEAM OF FS 280 WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01, CRJ900 SRM 51-42-10-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01
- [SDR VNAA202412150015](https://openairdocs.org/sdr/VNAA202412150015.md): Beam · corroded · Nov 7, 2024 · N596NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > DURING REMOVAL AT FLOOR PANEL SUPPORT IN FS280.00, CORROSION WAS FOUND ON LH CROSSBEAM OF FS 280.00. LH CROSSBEAM OF FS 280.00 WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01, CRJ900 SRM 51-42-10-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01
- [SDR VNAA202412150014](https://openairdocs.org/sdr/VNAA202412150014.md): Hinge · cracked · Nov 7, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FWD/MID/AFT HINGES, DEGRADED PAINT AND MISSING DECAL ON STEP PLATE AT AFT CARGO COMPARTMENT. FWD/MID/AFT HINGES ON STEP PLATE WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01; STEP PLATE WAS PAINTED PER CRJ 900 SRM 51-25-01-001-001-A01 AND DECAL
- [SDR VNAA202412150011](https://openairdocs.org/sdr/VNAA202412150011.md): Angle · corroded · Nov 7, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-001-A02 AND WAS REPLACED PER CRJ900 SRM
- [SDR VNAA202412150013](https://openairdocs.org/sdr/VNAA202412150013.md): Rail · corroded · Nov 6, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SEAT RAIL ON LBL9 (1EA) AND RBL9 (3EAS) BTW FS693.00 TO FS1000.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. CORRECTIVE ACTION: SEAT RAIL ON LBL9 (1EA) AND RBL9 (3EAS) BTW FS693.00 TO FS1000.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE WER
- [SDR VNAA202412150012](https://openairdocs.org/sdr/VNAA202412150012.md): Rail · corroded · Nov 6, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SEAT RAIL ON RBL27 BTW FS927.00 TO FS1031.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. SEAT RAIL ON RBL27 BTW FS927.00 TO FS1031.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. ARE OUT OF LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 THEREFO
- [SDR VNAA202412150010](https://openairdocs.org/sdr/VNAA202412150010.md): Rail · corroded · Nov 6, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LH SIDE SEAT RAIL BTW FS758.15 TO FS 913.00 (3EA) LH SIDE SEAT RAIL BTW FS758.15 TO FS 913.00 (3EA) ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49 (CON
- [SDR VNAA202412150009](https://openairdocs.org/sdr/VNAA202412150009.md): Rail · corroded · Nov 6, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON RH SIDE SEAT RAIL BTW FS785.15 TO FS 897.70 (2EA) RH SIDE SEAT RAIL BTW FS785.15 TO FS 897.70 (2EA) ARE OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12
- [SDR VNAA202412150008](https://openairdocs.org/sdr/VNAA202412150008.md): Rail · corroded · Nov 6, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SEAT RAILS OF LBL27 BTW FS364.00 TO FS501.00 (2EA) SEAT RAILS OF LBL27 BTW FS364.00 TO FS501.00 (2EA) WER
- [SDR VNAA202412150007](https://openairdocs.org/sdr/VNAA202412150007.md): Rail · corroded · Nov 6, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SEAT RAILS OF LBL9 BTW FS364.00 TO FS693.00 (5EA) CORROSION ON SEAT RAILS OF LBL9 BTW FS364.00 TO FS693.00 (5EA) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-00
- [SDR VNAA202412150006](https://openairdocs.org/sdr/VNAA202412150006.md): Rail · corroded · Nov 6, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > DESCRIPTION: CORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS693.00 (5EA) CORRECTIVE ACTION: SEAT RAILS OF RBL9 BTW FS349.00 TO FS693.00 (5EA) WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG.A12)
- [SDR VNAA202412150005](https://openairdocs.org/sdr/VNAA202412150005.md): Fitting · corroded · Nov 6, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (1EA) (FLOOR STRUCTURE AREA) FITTING OF ENTRANCE COMPARTMENT (1EA) (FLOOR STRUCTURE AREA) WAS FOUND OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 THEREFORE WAS REPLACEDPER CRJ-900 SRM 51-42-2
- [SDR VNAA202412150004](https://openairdocs.org/sdr/VNAA202412150004.md): Frame · corroded · Nov 6, 2024 · N596NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME FS1088.20 BTW STGR 24RH AND STGR 24LH AT AFT BAGGAGE BAY COMPARTMENT (BELOW FLOOR). C2 CORRCTIVE ACTION: CORROSION WAS REMOVED ON FRAME FS=1088.20 BTW STGR 24RH AND STGR 24LH AT AFT BAGGAGE BAY COMPARTMENT (BELOW FLOOR). C2, PER CRJ-900
- [SDR VNAA202412150003](https://openairdocs.org/sdr/VNAA202412150003.md): Doubler · corroded · Nov 6, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON PRODUCTION DOUBLER OF ANTENNA BTW FS 1000-1015 AND STRINGERS 25RH-26RH AT AFT CARGO COMPARTMENT. CORROSION ON AFT ATG NUTPLATE BRACKET BTW FS 1000-1015 AND STRINGERS 25RH-26RH AT AFT CARGO COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900
- [SDR VNAA202412150001](https://openairdocs.org/sdr/VNAA202412150001.md): Beam · cracked · Nov 6, 2024 · N596NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK 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). CORRECTIVE ACTION: FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMP
- [SDR VNAA20241213001](https://openairdocs.org/sdr/VNAA20241213001.md): Stringer Splice · corroded · Nov 6, 2024 · N596NN · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer
  > DISCREPANCY: INITIAL INSPECTION: CORROSION ON STRINGER SPLICE 25RH BTW FS 319.00 TO FS 333.00 AT MAIN AVIONICS COMPARTMENT.
- [SDR VNAA202412150002](https://openairdocs.org/sdr/VNAA202412150002.md): Door Sill · corroded · Nov 5, 2024 · N596NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT DOOR LOWER SILL AT DOOR CUT OUT BTW FS 1000.00 TO FS 1047.00. AFT CARGO COMPARTMENT DOOR LOWER SILL AT DOOR CUT OUT BTW FS 1000.00 TO FS 1047.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-23-201-001-A01 AND REPLA
- [SDR VNAA20241213019](https://openairdocs.org/sdr/VNAA20241213019.md): Stringer · corroded · Nov 5, 2024 · N596NN · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 26RH BTW FS349.00 TO FS364.00 AT MAIN AVIONICS COMPARTMENT. EVALUATED,DUE TO DAMAGE EXCEED ALLOWABLE DAMAGE LIMITS ON STRINGER 26RH BTW FS349.00 TO FS364.00 AT MAIN AVIONICS COMPARTMENT PER CRJ-900 SRM 53-21-03-101-006-A04 AND REPLACE
- [SDR VNAA20241213018](https://openairdocs.org/sdr/VNAA20241213018.md): Intercostal · corroded · Nov 5, 2024 · N596NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND WE
- [SDR VNAA20241213017](https://openairdocs.org/sdr/VNAA20241213017.md): Skin · corroded · Nov 5, 2024 · N596NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > CORROSION AND WEAR ON INTERNAL SKIN CUT OUT (SEAL SEATLEMENT AREA) DOOR SURROUND STRUCTURE AT MAIN AVIONICS COMPARTMENT. CORROSION AND WEAR ON INTERNAL SKIN CUT OUT (SEAL SEATLEMENT AREA) DOOR SURROUND STRUCTURE AT MAIN AVIONICS COMPARTMENT WAS REMOVED AND E
- [SDR VNAA20241213016](https://openairdocs.org/sdr/VNAA20241213016.md): Web · cracked · Nov 5, 2024 · N596NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK AT UPPER WEB BELOW SETTLEMENT AREA. UPPER WEB OF ADG WAS REPAIRED PER CRJ 900 SRM 53-11-43-201-001-A01
- [SDR VNAA20241213015](https://openairdocs.org/sdr/VNAA20241213015.md): Door Frame · corroded · Nov 5, 2024 · N596NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280. BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00 WAS REPAIRED PER CRJ900 SRM 53-11-10-201-006-A01
- [SDR VNAA20241213014](https://openairdocs.org/sdr/VNAA20241213014.md): Floorbeam · corroded · Nov 5, 2024 · N596NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00. CORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPLACED PER C
- [SDR VNAA202412131012](https://openairdocs.org/sdr/VNAA202412131012.md): Bracket · corroded · Nov 5, 2024 · N596NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > CORROSION ON MACHINED BRACKETS (5 E/A'S) AND FWD PLATE AT FWD CARGO COMPARTMENT. MACHINED BRACKETS (5 E/A'S) AND FWD PLATE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-21-001
- [SDR VNAA20241213011](https://openairdocs.org/sdr/VNAA20241213011.md): Rib · cracked · Nov 4, 2024 · N596NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > DISCREPANCY: DESCRIPTION: CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING.
- [SDR VNAA20241213010](https://openairdocs.org/sdr/VNAA20241213010.md): Support Bracket · cracked · Nov 4, 2024 · N596NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > DISCREPANCY: AFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH
- [SDR VNAA20241213020](https://openairdocs.org/sdr/VNAA20241213020.md): Frame · corroded · Nov 3, 2024 · N596NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 265.00 BTW STGR 26RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS 265.00 BTW STGR 26RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER C
- [SDR VNAA20241213009](https://openairdocs.org/sdr/VNAA20241213009.md): Hinge · corroded · Nov 3, 2024 · N596NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > DISCREPANCY: CORROSION AT PASSENGER DOOR STEP HINGE ON ACCESS PANEL 832ET
- [SDR VNAA20241213007](https://openairdocs.org/sdr/VNAA20241213007.md): Skin · nicked · Nov 3, 2024 · N596NN · Bombdr CL6002D15 · Trailing Edge Flaps
  > DISCREPANCY: SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FROM FLS 24.00 TO FLS 42.00
- [SDR VNAA20241213006](https://openairdocs.org/sdr/VNAA20241213006.md): Counterbalance · damaged · Nov 3, 2024 · N596NN · Bombdr CL6002D15 · Cargo/Baggage Doors
  > DISCREPANCY: SEVERAL GOUGES ON FWD/AFT COUNTERBALANCE ARM AT FWD BAGGAGE BAY DOOR
- [SDR VNAA20241213005](https://openairdocs.org/sdr/VNAA20241213005.md): Angle · corroded · Nov 3, 2024 · N596NN · Bombdr CL6002D15 · Service Doors
  > DISCREPANCY: INITIAL INSPECTION: CORROSION ON LOWER SIL BTW FS349.00 AND FS319.00 AT SERVICE DOOR
- [SDR VNAA20241213004](https://openairdocs.org/sdr/VNAA20241213004.md): Spar · corroded · Nov 2, 2024 · N596NN · Bombdr CL6002D15 · Wing Spar
  > DISCREPANCY: REPAIR TO WING INBD AUX/SPAR BETWEEN WS 24.5 - WS 34, RHS, REPLACE OR REPAIR THE DISCREPANT ITEM
- [SDR VNAA20241213012](https://openairdocs.org/sdr/VNAA20241213012.md): Rub Strip · worn · Oct 22, 2024 · N596NN · Bombdr CL6002D15 · Nacelle/Pylon Miscellaneous Structure
  > WEAR ON UPPER/LOWER AFT EDGE RUB STRIP ON FWD CORE COWL OF LH / RH ENGINE. UPPER/LOWER AFT EDGE RUB STRIP ON FWD CORE COWL OF LH / RH ENGINE WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR VNAA202302271111](https://openairdocs.org/sdr/VNAA202302271111.md): Window · arced · Feb 23, 2023 · N596NN · Cndair CL6002D24 · Flight Compartment Windows
  > LH WINDOW HEAT CAUTION MESSAGE FLAGGED IN FLIGHT, WINDOW VISIBLY ARCING AT THE BOTTOM MULTIPLE TIMES. / REMOVED AND REPLACED LH WINDOW IAW CRJ 900 AMM 56-12-01-000/400-801-A01. OPS CHECKS AND LEAK CHECKS GOOD
- [SDR VNAA202302221112](https://openairdocs.org/sdr/VNAA202302221112.md): None · none · Feb 21, 2023 · N596NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > MILLED RIB/FITTING CRACKED NEAR LOWER ROW OF FASTENERS IN FITTING. AFT SIDE OF MLG REAR SPAR (APPROX RH WS 49.00, INBOARD SIDE OF RH INBOARD MOST SPOILER RIGHT WING) / CONSTANT AVIATION PERFORMED TEMP REPAIR CLASSIFIED AS A MAJOR REPAIR IAW MHIRJ REO 690-57-21
- [SDR VNAA202302051112](https://openairdocs.org/sdr/VNAA202302051112.md): Wheel · separated · Feb 2, 2023 · N596NN · Cndair CL6002D24 · Tire
  > RH IB TIRE LOST TREAD / REMOVED AND REPLACED #3 MLG WHEEL AND TIRE ASSEMBLY IAW CRJ 900 AMM 32-41-01-000/400-801-A01-PSA. COMPLETED THE BURST TIRE INSPECTION FOR DAMAGE ON THE RHIB MLG TIRE AND ALL AREAS IAW CRJ900 AMM 05-51-29-210-802. ALL DAMAGE FOUND IS NOT
- [SDR VNAA202107051111](https://openairdocs.org/sdr/VNAA202107051111.md): Shutoff Valve · unserviceable · Jul 1, 2021 · N596NN · Cndair CL6002D24 · Engine Bleed Air System
  > THE CREW RECEIVED A LEFT BLEED CAUTION MESSAGE WHILE EN ROUTE TO CLT. THEY RAN THEIR QRH AND DIVERTED TO PHL, THEY DID NOT RAPIDLY DESCEND AND THE MASK DID NOT DEPLOY. NO BRACE WAS CALLED BY THE CREW BUT THEY DID DECLARE A EMERGENCY AND TRUCKS DID ROLL BUT NOT
- [SDR VNAA202105201112](https://openairdocs.org/sdr/VNAA202105201112.md): Manifold · unserviceable · May 18, 2021 · N596NN · Cndair CL6002D24 · Landing Gear Steering System
  > AFTER TAKEOFF THE CREW HAD RECEIVED A STEERING INOP CAUTION MSG, ONCE CLIMBED TO FL080 THEY REFERRED TO TO THE QRH. AFTER PROCEDURES THE ISSUES DID NOT DISSOLVE. THEY THEN CONTACTED ATC SAYING THEY WILL NEED VECTORS BACK INTO KCLT FOR MX ISSUE. ATC DECLARED EM

Next page: https://openairdocs.org/aircraft/N596NN/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 = 'N596NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N596NN/reports

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