# Service difficulty reports: N597NN

A list on [N597NN](https://openairdocs.org/aircraft/N597NN.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 VNAA2026072821401](https://openairdocs.org/sdr/VNAA2026072821401.md): Windshield · cracked · Jul 24, 2026 · N597NN · Cndair CL6002D24 · Flight Compartment Windows
  > FO SIDE WINDSHIELD CRACKING, PERFORMED DAMAGE CHECK OF THE FO SIDE WINDSHIELD IAW AMM 56-11-01-210-801-PSA AND FOUND INTERLAYER BUBBLING IN THE TOP OUTBOARD CORNER. DAMAGE IS WITHIN LIMITS. PERFORMED OPS CHECK OF THE RH WINDSHIELD/SIDE WINDOW TEMP CONTROLLER
- [SDR VNAA2025081911102](https://openairdocs.org/sdr/VNAA2025081911102.md): Warning Message · illuminated · Aug 17, 2025 · N597NN · Cndair CL6002D24 · Central Warning
  > L ENG ITT WENT TO 966°C ON T/O WHILE IN TOGA FULL THRUST TO CLIMB TO LOWER ITT. / PERFORMED ENGINE WASH WITH CLEANING SOLUTION FOR PERFORMANCE IAW AMM 72-00-00-100-803-A01-PSA. ITT WITHIN LIMITS.
- [SDR VNAA202504140020](https://openairdocs.org/sdr/VNAA202504140020.md): Skin · worn · Mar 12, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SKIN, FUSELAGE BETWEEN FS 1031.00-FS1051.30 & STR21R-STR26R PERFORM INSPECTION EVERY 15800 FC FROM INITIAL REPAIR PER STS EA 48-2019-090 REV A. SKIN, FUSELAGE BETWEEN FS 1031.00-FS1051.30 & STR21R-STR26R WAS REPAIRED PER REO 690-53-61-1531 REV.--
- [SDR VNAA202504130008](https://openairdocs.org/sdr/VNAA202504130008.md): Drag Angle · cracked · Mar 11, 2025 · N597NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE AND FWD DRAG ANGLE (2 E/AS) BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE AND FWD DRAG ANGLE
- [SDR VNAA202504140019](https://openairdocs.org/sdr/VNAA202504140019.md): Frame · damaged · Mar 10, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Frame
  > ELONGATED HOLE ON FRAME BTW STA FS 661.00 + 62.00 STRG 23LH TO STRG 24LH AT FWD CARGO COMPARTMENT. ELONGATED HOLE ON FRAME BTW STA FS 661.00 + 62.00 STRG 23LH TO STRG 24LH AT FWD CARGO COMPARTMENT WAS REPAIRED PER EA NO: 53-2025-0353 REV.--
- [SDR VNAA202504140018](https://openairdocs.org/sdr/VNAA202504140018.md): Frame · worn · Mar 10, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Frame
  > WEAR ON FRAME BTW FS785.15 AT RH AFT EMERGENCY DOOR. WEAR ON FRAME BTW FS785.15 AT RH AFT EMERGENCY DOOR WAS BLENDED PER CRJ 900 SRM 51-12-00-001-001-A01 AND EVALUATED WITHIN LIMITS PER REO 690-53-41-524 REV. - -.
- [SDR VNAA202504140021](https://openairdocs.org/sdr/VNAA202504140021.md): Fitting · corroded · Mar 9, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION ON FITTING (2EA) BELOW THE SERVICE TABLE AND AISLE SIDE AT FWD LAV. FITTING PN:A414252-3 (1EA) BELOW THE SERVICE TABLE WAS REPLACED PER SAFRAN CMM 25-40-40 AND FITTING PN: A414251-1 (1EA) AISLE SIDE AT FWD LAV WAS FABRICATED AND INSTALLED PER EA
- [SDR VNAA202504140017](https://openairdocs.org/sdr/VNAA202504140017.md): Rib · cracked · Mar 9, 2025 · N597NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK IN FIXED LEADING EDGE RIB SS57.16 AT RH WING. RIB CRACKED SS57.16 AT RH WING WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01.
- [SDR VNAA202504140015](https://openairdocs.org/sdr/VNAA202504140015.md): Canister · cracked · Mar 9, 2025 · N597NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CRACKS IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO670-57-42-577. REV.--.
- [SDR VNAA202504140013](https://openairdocs.org/sdr/VNAA202504140013.md): Canister · cracked · Mar 9, 2025 · N597NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CRACKS IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REAPIARED PER REO670-57-42-577. REV.--
- [SDR VNAA202504140012](https://openairdocs.org/sdr/VNAA202504140012.md): Intercostal · corroded · Mar 9, 2025 · N597NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 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
- [SDR VNAA202504140010](https://openairdocs.org/sdr/VNAA202504140010.md): Doubler · corroded · Mar 9, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BTWN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BTWN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMEN WAS EVALUATED OUT OF LIMI
- [SDR VNAA202504140014](https://openairdocs.org/sdr/VNAA202504140014.md): Frame · corroded · Mar 8, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME 1088.20 BTW STGR 25LH/STGR 27 AT AFT BAGGAGE BAY COMPARTMENT. CORROSION ON FRAME 1088.20 BTW STGR 25LH/STGR 27 AT AFT BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 52-3
- [SDR VNAA202504140011](https://openairdocs.org/sdr/VNAA202504140011.md): Stringer · corroded · Mar 8, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 22RH BTWN FS. 333.00 TO FS 349.00 AT MAIN AVIONICS COMPARTMENT. (E/E). CORROSION ON STRINGER 22RH BTWN FS. 333.00 TO FS 349.00 AT MAIN AVIONICS COMPARTMENT. (E/E) WAS EVALUATED OUT LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPLACED
- [SDR VNAA202504140009](https://openairdocs.org/sdr/VNAA202504140009.md): Stringer · corroded · Mar 8, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 27 BTWN FS 280.00 AND FS 310. CORROSION ON STGR 27 BTWN FS 280.00 AND FS 310.00 WERE EVALUATED OUT LIMITS PER CRJ900 SRM 53-21-03-101-002-A04 AND REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR VNAA202504140008](https://openairdocs.org/sdr/VNAA202504140008.md): Stringer · cracked · Mar 8, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CRACK ON STGR 3LH (LINTEL AREA) STA. FS280.00 AT CIRCUNFERENTIAL SKIN JOINT. CRACK ON STGR 3LH (LINTEL AREA) STA. FS280.00 AT CIRCUNFERENTIAL SKIN JOINT WAS REPAIRED PER 690-53-21-1908 REV. --.THE AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTHS FROM THE ISSUE
- [SDR VNAA202504140007](https://openairdocs.org/sdr/VNAA202504140007.md): Seat Track · corroded · Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL 15RH (5EAS) BTW FS 379.00 TO FS 669.40. SIDE SEAT RAIL 15RH (5EAS) BTW FS 379.00 TO FS 669.40 WERE EVALUATED DUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53
- [SDR VNAA202504140006](https://openairdocs.org/sdr/VNAA202504140006.md): Seat Track · corroded · Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL 15LH (5 EAS) BTW FS 379.00 TO FS 669.40. SIDE SEAT RAIL 15LH (5 EAS) BTW FS 379.00 TO FS 669.40 WERE EVALUATED PER CRJ-900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12
- [SDR VNAA202504140005](https://openairdocs.org/sdr/VNAA202504140005.md): Seat Track · corroded · Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL 15LH (6EAS) BTW FS 669.40 TO FS 977. SIDE SEAT RAIL 15LH (6EAS) BTW FS 669.40 TO FS 977.00 WERE EVALUATED DUE TO EXCESSIVE DAMAGE PER CRJ/900 SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ/900 SRM 53-00-49-400-801 (CONFIG A12)
- [SDR VNAA202504140004](https://openairdocs.org/sdr/VNAA202504140004.md): Seat Track · corroded · Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL 15RH (6EAS) BTW FS 669.40 TO FS 977. SIDE SEAT RAIL 15RH (6EAS) BTW FS 669.40 TO FS 977.00 WERE EVALUATED DUE TO EXCESSIVE DAMAGE PER CRJ900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-
- [SDR VNAA202504140003](https://openairdocs.org/sdr/VNAA202504140003.md): Angle · corroded · Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. CORROSION ON 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 CR
- [SDR VNAA202504140002](https://openairdocs.org/sdr/VNAA202504140002.md): Seat Track · corroded · Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF LBL27 BTW FS477.40 TO FS581.00 (2EA). DUE TO EXCESIVE DAMAGE SEAT RAILS OF LBL27 BTW FS477.40 TO FS581.00 (2EA) WERE REPLACED PER CRJ-900 SRM 53-31-49-101-001-A02, CRJ-900 SRM 53-31-49-991-806 AND PER CRJ-900 AMM 53-00-49.
- [SDR VNAA202504140001](https://openairdocs.org/sdr/VNAA202504140001.md): Seat Track · corroded · Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF LBL9 BTW FS364.00 TO FS693.00 (5EA). DUE TO EXCESSIVE DAMAGE ON SEAT RAILS OF LBL9 BTW FS364.00 TO FS693.00 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, CRJ-900 SRM 53-31-49-101-001-A02 AND CRJ-900 SRM 5
- [SDR VNAA202504130015](https://openairdocs.org/sdr/VNAA202504130015.md): Seat Track · corroded · Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS693.00 (6EA) SUMMARY: SEAT RAILS OF RBL9 BTW FS349.00 TO FS693.00 (6EA) WERE EVALUATED OUT LIMITS PER CRJ 900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND WERE REPLACED
- [SDR VNAA202504130010](https://openairdocs.org/sdr/VNAA202504130010.md): Hinge · worn · Mar 7, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > WEAR ON PASSENGER DOOR HINGE (FUSELAGE SIDE) LUG LAND. PASSENGER DOOR HINGE (FUSELAGE SIDE) LUG LAND WAS REPAIRED PER REO 670-52-11-511 REV. -E
- [SDR VNAA202504130014](https://openairdocs.org/sdr/VNAA202504130014.md): Bracket · corroded · Mar 6, 2025 · N597NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MACHINED BRACKET (7EA) OF FLOOR STRUCTURE AT FWD CARGO COMPARTMENT. MACHINED BRACKET (3EA) OF FLOOR STRUCTURE AT FWD CARGO COMPARTMENT (FS533/FS549, BTW STGR 25/24, FS 565 BTW STGR 21/22, FS 645/ 661 BTW STGR 25/24 WERE CLEANED PER CRJ900 SRM 51-
- [SDR VNAA202504130013](https://openairdocs.org/sdr/VNAA202504130013.md): Web · cracked · Mar 6, 2025 · N597NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193. CRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER REO 690-53-11-1965 REV. -- AND PER REO 670-53-11-509 REV. -E
- [SDR VNAA202504130011](https://openairdocs.org/sdr/VNAA202504130011.md): Skin Panel · dented · Mar 6, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENT ON FWD FUSELAGE SKIN ON STGR 22 LH BTW FS 349.00 TO FS 364.00. DENT ON FWD FUSELAGE SKIN ON STGR 22 LH BTW FS 349.00 TO FS 364.00. WAS REPAIRED PER 690-53-21-1907 REV. --. UNTIL A TRANSPORT CANADA ACCEPTED NDTM TECHNIQUE HAS BEEN MADE AVALIABLE, THE AIR
- [SDR VNAA202504130009](https://openairdocs.org/sdr/VNAA202504130009.md): Plate · corroded · Mar 5, 2025 · N597NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION WAS FOUND ON KICKPLATE OF SURROUND STRUCTURE AT PASSENGER DOOR (L1). CORROSION ON KICKPLATE OF SURROUND STRUCTURE AT PASSENGER DOOR (L1) WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-23-101-001-
- [SDR VNAA202504130007](https://openairdocs.org/sdr/VNAA202504130007.md): Drag Angle · cracked · Mar 5, 2025 · N597NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM
- [SDR VNAA202504130004](https://openairdocs.org/sdr/VNAA202504130004.md): Skin · worn · Mar 5, 2025 · N597NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON SETTLEMENT AREA OF ACCESS PANELS 683AB, 686AB, 692AB 695AB AND 697AB. WEAR ON SETTLEMENT AREA OF ACCESS PANELS 683AB, 695AB AND 697AB WERE BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 EVALUATED WITHIN LIMITS PER CRJ-900 SRM 57-00-01-101-001-A03. WE
- [SDR VNAA202504130002](https://openairdocs.org/sdr/VNAA202504130002.md): Skin · scratched · Mar 4, 2025 · N597NN · Cndair CL6002D24 · Wing, Plate/Skin
  > SCRATCHES ON WINGS LOWER SURFACE RH WING REAR SIDE BTW WS294.50-WS343.50 AND LH WING REAR SIDE AT WS294.50. SCRATCHES ON WINGS LOWER SURFACE RH WING REAR SIDE BTW WS294.50-WS343.50 AND LH WING REAR SIDE AT WS294.50 WERE BLENDED PER CRJ-900 SRM 51-12-00-001-
- [SDR VNAA202504130001](https://openairdocs.org/sdr/VNAA202504130001.md): Fireshield · worn · Mar 4, 2025 · N597NN · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > RH LWR FWD CORE COWL WITHIN 6803.22 FH'S (BEFORE19,898.24 FH'S) REPAIR OR REPLACE THE DISCREPANT ITEM. RH LWR FWD CORE COWL, FIRE SHIELD WERE REPLACED PER. CRJ-900 S.R.M 54-23-00-201-005-A01 AND PER CRJ900 SRM 51-42-06-001-001-A01.
- [SDR VNAA202504140016](https://openairdocs.org/sdr/VNAA202504140016.md): Seat Track · corroded · Feb 17, 2025 · N597NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAIL BTW FS 847.00 TO FS977.00 LH/RH (4EAS) AT CABIN PAX. FLOOR SEAT RAIL BTW FS 847.00 TO FS977.00 LH/RH (4EAS) AT CABIN PAX WERE EVALUATED DUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AN
- [SDR VNAA202504130005](https://openairdocs.org/sdr/VNAA202504130005.md): Hinge · corroded · Feb 17, 2025 · N597NN · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION ON HINGE AT ACCESS PANEL 832ET. DUE TO EXCESSIVE DAMAGE ON HINGE AT ACCESS PANEL 832ET WAS EVALUATED PER CRJ-900 SRM 52-11-04-101-001-A01 AND REPLACE PER CRJ-900 SRM 51-41-02-001-001-A01
- [SDR VNAA2024070811101](https://openairdocs.org/sdr/VNAA2024070811101.md): Windshield · unserviceable · Jul 5, 2024 · N597NN · Cndair CL6002D24 · Flight Compartment Windows
  > RH WINDSHIELD HEAT TERMINAL CONNECTION BLOCK STARTED TO SPARK AND CREATE ELECTRICAL ODOR ON SHORT FINAL, SWITCHED RH WINDSHIELD HEAT TO THE OFF POSITION ORDOR AND SPARKS STOPPED / REMOVED AND REPLACED RH WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA.
- [SDR VNAA2024042611101](https://openairdocs.org/sdr/VNAA2024042611101.md): None · none · Apr 25, 2024 · N597NN · Cndair CL6002D24 · Standard Practices/Structures
  > RESET THE AIRCRAFT THEN PERFORMED THE OPERATION TEST OF THE ANTI-SKID CONTROL SYSTEM IAW CRJ 900 AMM 32-44-00-710-801-A01. OPS TEST GOOD AT THIS TIME AND NO FAULT FOUND.
- [SDR VNAA202302271114](https://openairdocs.org/sdr/VNAA202302271114.md): None · none · Feb 26, 2023 · N597NN · Cndair CL6002D24 · Emergency Exits
  > DURING OPERATIONS AT HEBRON KY (CVG), THE MAINTENANCE REPORTS A DENT WITH A MINOR GOUGE ON THE L/H FORWARD EMERGENCY EXIT DOOR FORWARD EDGE. DAMAGE 1: 0.5€? L X.25 W X.021€? D. / PERM REPAIR COMPLETED IAW EA-22-C9-52-1317-A.
- [SDR VNAA202110219999](https://openairdocs.org/sdr/VNAA202110219999.md): Web · cracked · Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > FOUND PASSENGER DOOR AFT STAIR WEB TO HAVE A CRACK AT ZONE-3. REPAIRED CRACK ON AFT STAIR WEB IAW CRJ900 SRM 52-11-04-201-004-A01.
- [SDR VNAA202110219998](https://openairdocs.org/sdr/VNAA202110219998.md): Seat Track · corroded · Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT TRACK FS785-FS847+8.4 SEGMENT IS CORRODED. INSTALLED RH SIDE SEAT TRACK FS 785-FS 847+8.4 IAW CRJ 900 AMM 53-00-49-400-801-A12
- [SDR VNAA202110219997](https://openairdocs.org/sdr/VNAA202110219997.md): Seat Track · corroded · Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT TRACK FS744.15-FS761.85 SEGMENT IS CORRODED. INSTALLED NEW RH SIDE SEAT TRACK FS744.15 TO FS761.85 IAW CRJ900 AMM 53-00-49-400-801-A12.
- [SDR VNAA202110219996](https://openairdocs.org/sdr/VNAA202110219996.md): Seat Track · corroded · Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK FS847+8.4-847+20 SEGMENT IS CORRODED. INSTALLED L/H SIDE SEAT RAIL TRACK FROM FS847+8.4-FS847+20 IAW CRJ900 AMM 53-00-49-400-801-A12.
- [SDR VNAA202110219995](https://openairdocs.org/sdr/VNAA202110219995.md): Seat Track · corroded · Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK FS785-FS847+8.4 SEGMENT IS CORRODED. INSTALLED NEW SERVICEABLE LH SIDE SEAT RAIL FS785-FS847+8.4 IAW CRJ900 AMM 53-00-49-400-801 CONFIG A12.
- [SDR VNAA202110219994](https://openairdocs.org/sdr/VNAA202110219994.md): Seat Track · corroded · Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK FS744.15-761.85 SEGMENT IS CORRODED. INSTALLED NEW SEAT TRACK AT LH FS744.15 TO FS761.85 PER CRJ900 AMM 53-00-49-400-801-A12.
- [SDR VNAA202110219993](https://openairdocs.org/sdr/VNAA202110219993.md): Seat Track · corroded · Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT TRACK AT RBL9 FROM FS 349.00 TO FS 485.00. INSTALLED FLOOR SEAT TRACK AT RBL 9 FROM FS 349.00 TO 485.00 IAW CRJ 900 AMM 53-00-44-400-801-A12.
- [SDR VNAA202110219992](https://openairdocs.org/sdr/VNAA202110219992.md): Seat Track · corroded · Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT TRACK AT LBL 9 FROM FS 364.00 TO FS 485.00. INSTALLED FLOOR SEAT TRACK AT LBL 9 FROM FS 364.00 TO FS 485.00 IAW CRJ 900 AMM 53-00-44-400-801-A12.
- [SDR VNAA202110219991](https://openairdocs.org/sdr/VNAA202110219991.md): Web · cracked · Oct 21, 2021 · N597NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > PAX DOOR AFT WEB CRACKED. PERFORM PERMANENT REPAIR OF PAX DOOR WEB AFT SIDE OF DOOR AT ZONE 2 E PER CRJ 900 SRM 52-11-04-201-004-A01 PAR 5-6
- [SDR VNAA202109021111](https://openairdocs.org/sdr/VNAA202109021111.md): Terminal Block · arced · Aug 30, 2021 · N597NN · Cndair CL6002D24 · Window System Wiring
  > ON DECENT THE RH TERMINAL BLOCK SPARKED. THE CREW RAN THE QRC AND QRH AND DID A RESET WINDOW HEAT MESSAGE AND THE MESSAGE CAME BACK IMMEDIATELY. THE CREW THEN TURNED OFF THE WINDOW HEAT AND THE MESSAGE DID NOT RETURN AND THEY DID NOT HAVE ANY FURTHER ISSUES. N
- [SDR VNAA202011201111](https://openairdocs.org/sdr/VNAA202011201111.md): Windshield · debonded · Nov 19, 2020 · N597NN · Cndair CL6002D24 · Flight Compartment Windows
  > WHILE ON DESCENT INTO SBN, THE F/O WINDSHIELD CRACKED TOWARDS THE MIDDLE OF THE WINDOW. ATC DECLARED AN EMERGENCY, THE FLIGHT LANDED WITHOUT INCIDENT. A RESCUE FLIGHT IS BEING SENT UP TO RECOVER THE TURN FLIGHT SBN TO CLT.
- [SDR VNAA2020090511102](https://openairdocs.org/sdr/VNAA2020090511102.md): Bracket · broken · Sep 4, 2020 · N597NN · Cndair CL6002D24 · Service Doors
  > SERVICE DOOR UPPER STABILIZER BAR DOOR BRACKET BROKEN. REMOVED AND REPLACED UPPER STABILIZER BAR DOOR BRACKET ON THE SERVICE DOOR. OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N597NN/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 = 'N597NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N597NN/reports

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