# Service difficulty reports: N598NN

A list on [N598NN](https://openairdocs.org/aircraft/N598NN.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 · 66 reports

- [SDR VNAA2026092926101](https://openairdocs.org/sdr/VNAA2026092926101.md): Door Frame · damaged · Sep 27, 2026 · N598NN · Cndair CL6002D24 · Fuselage Main, Structure
  > AVIONICS DOOR FRAME, LIGHTNING STRIKE. PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN MHIRJ REO 690-53-21-2189.
- [SDR VNAA2026092525804](https://openairdocs.org/sdr/VNAA2026092525804.md): Skin · damaged · Sep 25, 2026 · N598NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > REPAIR TO FUSELAGE STRUCTURE BETWEEN FS661.00-FS661.00+16.00 AND STR25R-27 / PERFORMED ALL WORKS USING STEPS AND DRAWINGS LISTED IN MHIRJ REO 690-53-31-1166
- [SDR VNAA2026092525703](https://openairdocs.org/sdr/VNAA2026092525703.md): Skin · damaged · Sep 25, 2026 · N598NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > REPAIR TO FUSELAGE STRUCTURE BTA FS235.00-FS280.00 & STR25R-STR27 / PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN MHIRJ REO 690-53-11-2252
- [SDR VNAA2026092525602](https://openairdocs.org/sdr/VNAA2026092525602.md): Skin · damaged · Sep 25, 2026 · N598NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > REPAIR TO FUSELAGE STRUCTURE BETWEEN BS 295 - 319.70, STR 24 -27R. PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN REO 690-53-21-2197
- [SDR VNAA2026092525501](https://openairdocs.org/sdr/VNAA2026092525501.md): Skin Panel · damaged · Sep 25, 2026 · N598NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > REPAIR TO FUSELAGE LOWER SKIN PANEL BTW BS 295 AND 349 BETWEEN STR 25 & 27L. PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN REO 690-53-21-2195.
- [SDR VNAA2026041316103](https://openairdocs.org/sdr/VNAA2026041316103.md): Fan · odor · Apr 9, 2026 · N598NN · Cndair CL6002D24 · Central Display
  > DISPLAY FAN LOUD WITH ELECTRICAL ODOR, CW FIM 21-24-12-810-802-A01 AND FOUND DISPLAY FAN #2 TO BE BAD. DEFERRED DISPLAY FAN #2 PER MEL 21-24-02-2 CAT C. C/W M/FC BY PULLING AND COLLARING CBP1 B2. PLACARDS PLACED. VERIFIED DISPLAY COOL MSG DID NOT APPEAR. REM
- [SDR VNAA2025071111101](https://openairdocs.org/sdr/VNAA2025071111101.md): Tire · blown · Jul 9, 2025 · N598NN · Cndair CL6002D24 · Tire
  > ON TAKE OFF TIRE BLEW, ON GROUND CONFIRMED TREAD MISSING LEFT OB MAIN TIRE / REMOVED AND REPLACED THE #1 MLG TIRE WHEEL ASSEMBLY IAW CRJ900 AMM 32-41-01-000/400-801-A01.
- [SDR VNAA20250602012](https://openairdocs.org/sdr/VNAA20250602012.md): Coaming · worn · May 26, 2025 · N598NN · Cndair CL6002D24 · Engine Thrust Reverser
  > WEAR ON LATCH COAMING AND PADS ON RH AND LH UPPER/LOWER TRANSCOWLS. LATCH COAMING AND PADS ON RH AND LH UPPER/LOWER TRANSCOWLS. WERE REPLACED PER REO 670-54-21-1207 REV. A, PER CRJ-900 SRM 51-42-10-001-001-A01, CRJ-900 SRM 51-42-06-001-001-A01,PER CRJ-900 AMM
- [SDR VNAA20250602004](https://openairdocs.org/sdr/VNAA20250602004.md): Hinge · damaged · May 21, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > REPLACE ENTRY WAY PIANO HINGE. PIANO HINGE WAS REPLACED PER CRJ-900 SRM 53-21-23-201-007-A01 AND SRM 51-42-21-001--001-A01.
- [SDR VNAA20250602016](https://openairdocs.org/sdr/VNAA20250602016.md): Skin · corroded · May 4, 2025 · N598NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > EROSION AND CORROSION WAS FOUND ON ANTENNA AND SETTLEMENT AREA EXTERNAL FUSELAGE SKIN. CORROSION ON SETTLEMENT AREA EXTERNAL FUSELAGE SKIN WAS REMOVED PER CRJ-900 SRM 53-00-01-201-017-A01. AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-01-201-017-A01 AND A
- [SDR VNAA20250602015](https://openairdocs.org/sdr/VNAA20250602015.md): Rib · cracked · Apr 30, 2025 · N598NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON RIB LEADING EDGE SS57.16 WAS FOUND CRACK ON RIB LEADING EDGE SS57.16 WAS REPAIRED PER REO 690-57-41-240 REV
- [SDR VNAA20250602014](https://openairdocs.org/sdr/VNAA20250602014.md): Fitting · corroded · Apr 29, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION ON FLOOR FITTING ACCESS 107 COUNTER AT GALLEY 1. FLOOR FITTING ACCESS 107 COUNTER AT GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-96
- [SDR VNAA20250602013](https://openairdocs.org/sdr/VNAA20250602013.md): Floor Support · cracked · Apr 23, 2025 · N598NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > 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).FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE
- [SDR VNAA20250602011](https://openairdocs.org/sdr/VNAA20250602011.md): Diaphragm · cracked · Apr 23, 2025 · N598NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON DIAPHRAGM RBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE. CRACK ON DIAPHRAGM RBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE WAS REPAIRED PER REO 670-53-82-478 REV - A.
- [SDR VNAA20250602009](https://openairdocs.org/sdr/VNAA20250602009.md): Canister · cracked · Apr 23, 2025 · N598NN · Cndair CL6002D24 · Aircraft Fuel Distribution System
  > CRACK 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 REPIARED PER REO670-57-42-577. REV.
- [SDR VNAA20250602008](https://openairdocs.org/sdr/VNAA20250602008.md): Canister · cracked · Apr 23, 2025 · N598NN · Cndair CL6002D24 · Aircraft Fuel Distribution System
  > CRACK 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 REPIARED PER REO670-57-42-577. REV.
- [SDR VNAA20250602005](https://openairdocs.org/sdr/VNAA20250602005.md): Hinge · worn · Apr 23, 2025 · N598NN · Cndair CL6002D24 · Rudder Structure
  > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON RUDDER HINGE ASSY NO. 4 AT VERTICAL STABILIZER. RUDDER HINGE ASSY NO. 4 AT VERTICAL STABILIZER WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01.
- [SDR VNAA20250602010](https://openairdocs.org/sdr/VNAA20250602010.md): Lug · corroded · Apr 22, 2025 · N598NN · Cndair CL6002D24 · Ailerons
  > CORROSION ON HOUSING (6EAS) OF HINGE FITTINGS 2,3,4 (OUTBD AND INBD) AT RH WING REAR SPAR. HOUSNGS OF HINGE FITTINGS 2 & 3 (OUTBD AND INBD) AT RH WING REAR SPAR WERE CLEANED PER CRJ 700/900 SRM 51-12-00-001-001-A01 AND HOLE OF HINGE 4 WERE REPAIRED PER REO RE
- [SDR VNAA20250602007](https://openairdocs.org/sdr/VNAA20250602007.md): Rib · cracked · Apr 22, 2025 · N598NN · Cndair CL6002D24 · Leading Edge Devices
  > CRACK ON RIB LEADING EDGE SS57.16 WAS FOUND. CRACK ON RIB RH LEADING EDGE SS57.16 WAS REPAIRED PER REO 690-57-41-240 REV
- [SDR VNAA20250602006](https://openairdocs.org/sdr/VNAA20250602006.md): Frame · corroded · Apr 22, 2025 · N598NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME 847.00 + 32.00 BTW STGR 26L TO STGR 26R AT FUSELAGE INTERNAL STRUCTURE. CORROSION ON FRAME 847.00 + 32.00 BTW STGR 26L TO STGR 26R AT FUSELAGE INTERNAL STRUCTURE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS P
- [SDR VNAA20250601010](https://openairdocs.org/sdr/VNAA20250601010.md): Frame · corroded · Apr 22, 2025 · N598NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME 645.00 BTW STGR 18L AND STGR 19L AT AT CABIN FLOOR STRUCTURE. ON FRAME 645.00 BTW STGR 18L AND STGR 19L AT AT CABIN FLOOR STRUCTURE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-31-06-101-0
- [SDR VNAA20250601009](https://openairdocs.org/sdr/VNAA20250601009.md): Stringer Splice · corroded · Apr 22, 2025 · N598NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER AND STRINGER SPLICE 25R BTW FS319.70 TO FS333.00 AT MAIN AVIONICS COMPARTMENT. STRINGER AND STRINGER SPLICE 25R BTW FS319.70 TO FS333.00 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-03-101-002-A04 AND
- [SDR VNAA20250601008](https://openairdocs.org/sdr/VNAA20250601008.md): Doubler · corroded · Apr 22, 2025 · N598NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL PRODUCTION DOUBLER BTW FS295.00/FS310.00 AND STGR26L/STGR26R AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL PRODUCTION DOUBLER BTW FS295.00/FS310.00 AND STGR26L/STGR26R AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-
- [SDR VNAA20250602029](https://openairdocs.org/sdr/VNAA20250602029.md): Seat Track · corroded · Apr 21, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF LBL9 BTW FS693.00 TO FS1000.00 (3EA). SEAT RAILS OF LBL9 BTW FS693.00 TO FS1000.00 (3EA) WERE EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02, AND WERE REPLACED PER CRJ-900 A
- [SDR VNAA20250602017](https://openairdocs.org/sdr/VNAA20250602017.md): Seat Track · corroded · Apr 21, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS693.00 (6EA). EVALUATED, DUE EXCESSIVE DAMAGE ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS693.00 (6EAS) PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49.
- [SDR VNAA20250601007](https://openairdocs.org/sdr/VNAA20250601007.md): Seat Track · corroded · Apr 21, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL BTW FS744.15 TO FS969.00. LH SIDE SEAT RAIL BTW FS744.15 TO FS969.00 WERE EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49 CONF(A12).
- [SDR VNAA20250601006](https://openairdocs.org/sdr/VNAA20250601006.md): Seat Track · corroded · Apr 21, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL BTW FS744.15 TO FS969.00 (6EA). RH SIDE SEAT RAIL BTW FS744.15 TO FS969.00 (6EA) WERE EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49 CON
- [SDR VNAA20250601005](https://openairdocs.org/sdr/VNAA20250601005.md): Seat Track · corroded · Apr 21, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF LBL27 BTW FS379.00 TO FS581.00 (3EA). CORROSION ON SEAT RAILS OF LBL27 BTW FS379.00 TO FS581.00 (3EA) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12.
- [SDR VNAA20250601004](https://openairdocs.org/sdr/VNAA20250601004.md): Seat Track · corroded · Apr 21, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF LBL9 BTW FS379.00 TO FS693.00 (5EA). CORROSION ON SEAT RAILS OF LBL9 BTW FS379.00 TO FS693.00 (5EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACE
- [SDR VNAA20250601003](https://openairdocs.org/sdr/VNAA20250601003.md): Seat Track · corroded · Apr 21, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A02, SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED
- [SDR VNAA20250601002](https://openairdocs.org/sdr/VNAA20250601002.md): Seat Track · corroded · Apr 21, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). CORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A01 AND SRM 53-41-49-101-001-A02 AND WERE R
- [SDR VNAA20250602028](https://openairdocs.org/sdr/VNAA20250602028.md): Seat Track · corroded · Apr 20, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF RBL9 BTW FS693.00 TO FS1000.00 (3EA). SEAT RAILS OF RBL9 BTW FS693.00 TO FS1000.00 (3EA) WERE EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02, AND WERE REPLACED PER CRJ-900
- [SDR VNAA20250602027](https://openairdocs.org/sdr/VNAA20250602027.md): Door Frame · worn · Apr 20, 2025 · N598NN · Cndair CL6002D24 · Fuselage Main, Structure
  > WEAR ON FRAME OF EMERGENCY EXIT DOOR SURROUND STRUCTURE LH ON FS785.15. FRAME OF EMERGENCY EXIT DOOR SURROUND STRUCTURE LH ON FS785.15 WAS REPAIRED, THE AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTHS FROM THE ISSUE DATE OF THIS REPAIR PER REO 690-53-41-532 1
- [SDR VNAA20250602026](https://openairdocs.org/sdr/VNAA20250602026.md): Intercostal · corroded · Apr 20, 2025 · N598NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS (3 EAS) BTW FS349.00/FS364.00 AND STGR26L/STGR26R AT MAIN AVIONICS COMPARMENT DOOR SURROUND STRUCTURE. CORROSION ON INTERCOSTALS (3 EAS) BTW FS349.00/FS364.00 AND STGR26L/STGR26R AT MAIN AVIONICS COMPARMENT DOOR SURROUND STRUCTURE W
- [SDR VNAA20250602025](https://openairdocs.org/sdr/VNAA20250602025.md): Stringer · corroded · Apr 20, 2025 · N598NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 26R BTW FS333.00 TO FS364.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR 26R BTW FS333.00 TO FS364.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED EXCESIVE DAMAGE PER CRJ/900 SRM 53-21-03-101-006-A04 AND REPLACED PER CRJ-900 SRM-51-42-06-
- [SDR VNAA20250602022](https://openairdocs.org/sdr/VNAA20250602022.md): Angle · corroded · Apr 20, 2025 · N598NN · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION ON ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE BTW FS310.00 AND FS349.00. DUE TO EXCESSIVE DAMAGE ON ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE BTW FS310.00 AND FS349.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01
- [SDR VNAA20250601001](https://openairdocs.org/sdr/VNAA20250601001.md): Floor Support · corroded · Apr 20, 2025 · N598NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SILL, LOCATED BTW FS=349.00 AND RBL 43" AT FUSELAGE FLOOR STRUCTURE. FLOOR SILL, LOCATED BTW FS=349.00 AND RBL 43" AT FUSELAGE FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-21-1938 REV. -.
- [SDR VNAA20250602024](https://openairdocs.org/sdr/VNAA20250602024.md): Bracket · corroded · Apr 19, 2025 · N598NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. PAINT ON BRACKETS(3E/AS) BTW FS 533.00/FS 549.00 STRG 24/25RH, FS 565.00 STRG 23/22LH AND FS 661.00 STRG 27/26LH WAS REMOVED PER CRJ-900 SRM 51-26-01-001-001-A01, GVI WAS
- [SDR VNAA20250602023](https://openairdocs.org/sdr/VNAA20250602023.md): Hinge · worn · Apr 19, 2025 · N598NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > WEAR IN PASSENGER-DOOR PIANO HINGE ON THE FUSELAGE SIDE, BETWEEN FS333.00 AND FS349. PASSENGER-DOOR PIANO HINGE ON THE FUSELAGE SIDE, BETWEEN FS333.00 AND FS349.00 WAS REPAIRED PER REO 670-53-21-582 REV. -G.
- [SDR VNAA20250602020](https://openairdocs.org/sdr/VNAA20250602020.md): Skin · damaged · Apr 18, 2025 · N598NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > PERMANENT REPAIR OF THE PAX DOOR CUTOUT LOWER FWD CORNER ACCOMPLISH PERMANENT REPAIR PER REO 690-53-21-1441. PAX DOOR CUT OUT LOWER FWD CORNER WAS REPAIRED PER CRJ-900 SRM 53-21-01-201-010-A01.
- [SDR VNAA20250602021](https://openairdocs.org/sdr/VNAA20250602021.md): Skin · damaged · Apr 17, 2025 · N598NN · Cndair CL6002D24 · Vertical Stabilizer
  > DAMAGE ON RH VERTICAL STAB REAR SPAR DATUM. RH VERTICAL STAB REAR SPAR DATUM WAS REPAIRED PER REO 690-53-71-087 REV. -
- [SDR VNAA20250602019](https://openairdocs.org/sdr/VNAA20250602019.md): Drag Angle · cracked · Apr 17, 2025 · N598NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) CORRECTIVE ACTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DATU
- [SDR VNAA20250602018](https://openairdocs.org/sdr/VNAA20250602018.md): Drag Angle · cracked · Apr 17, 2025 · N598NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) CORRECTIVE ACTION: CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DA
- [SDR VNAA20250602001](https://openairdocs.org/sdr/VNAA20250602001.md): Skin · dented · Apr 17, 2025 · N598NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW FS 1181.00 TO FS1211.00 OF THE AREA COVERED BY LH/RH VENTRAL FIN FAIRING DENTS ON EX•TER NAL FUSELAGE SKIN BTW FS 1181.00 TO FS1211.00 OF THE AREA COVERED BY LH/RH VENTRAL FIN FAIRING WERE REPAIRED PER REO 690-53-7
- [SDR VNAA20250602003](https://openairdocs.org/sdr/VNAA20250602003.md): Fitting · corroded · Apr 2, 2025 · N598NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AND MISSING NUT ON GALLEY FLOOR SUPPORTS (2EAS) LOCATED BTW FS 280.00 - FS 295.00 AT FUSELAGE FLOOR STRUCTURE RH. CORROSION LOCATED BTW FS 280.00 - FS 295.00 AT FUSELAGE FLOOR STRUCTURE RH WAS EVALUATED DUE TO EXCESIVE DAMAGE ON SUPPORT (1EA) PER CR
- [SDR VNAA20250602002](https://openairdocs.org/sdr/VNAA20250602002.md): Fitting · corroded · Apr 2, 2025 · N598NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SETTLEMENT FITTING (1EA) BTW FS 379 AND FS 394, RBL12 OF FWD LAVATORY AT FUSELAGE FLOOR STRUCTURE. CORROSION ON SETTLEMENT FITTING (1EA) BTW FS 379 AND FS 394, RBL12 OF FWD LAVATORY AT FUSELAGE FLOOR STRUCTURE WAS EVALUATED DUE TO EXCESIVE DAMAG
- [SDR VNAA2024072211101](https://openairdocs.org/sdr/VNAA2024072211101.md): Wire Harness · faulted · Jul 18, 2024 · N598NN · Cndair CL6002D24 · Landing Gear System Wiring
  > BRAKE OVERHEAT WARNING MSG IN FLIGHT / REMOVED AND REPLACED LH OB PROXIMITY SENSOR HARNESS ASSEMBLY IAW CRJ 900 AMM 32-61-05-000/400-803-A01. ALL OPS CHECKS GOOD AT THIS TIME. THIS CLEARS MEL.
- [SDR VNAA2024050711102](https://openairdocs.org/sdr/VNAA2024050711102.md): Unknown · odor · May 4, 2024 · N598NN · Cndair CL6002D24 · Air Distribution System
  > UPON BATTERY MASTER SWITCH ON BURNING SMELL IN FLIGHT DECK / INTERROGATED MDC FOUND NO B1 CODES. TROUBLESHOT SMELL IN THE COCKPIT BY RESETTING THE AIRCRAFT 2 TIMES. TURNED BOTH THE PACKS ON. SET WINDOW HEAT ON HIGH. TURNED RECIRCULATING FAN ON. SET DISPLAY FAN
- [SDR VNAA2024050711101](https://openairdocs.org/sdr/VNAA2024050711101.md): Unknown · odor · May 4, 2024 · N598NN · Cndair CL6002D24 · Air Distribution System
  > BURNING SMELL AFTER APU START, ENGINES SHUT DOWN ON APU BLEED SUPPLY / STARTED APU IAW CRJ900 AMM 49-10-00-866-801-A01 RAN PACKS AT FULL BLAST STILL NO SMELL. RAN BOTH ENGINES WITH PACKS AND RECIRCULATION FAN IAW CRJ900 AMM 71-00-00-866-806-A02. NO SMELL. TAXI
- [SDR VNAA2023101611101](https://openairdocs.org/sdr/VNAA2023101611101.md): Acm · odor · Oct 14, 2023 · N598NN · Cndair CL6002D24 · Cabin Cooling System
  > FA AND PASSENGERS REPORT VISUAL SMOKE IN THE CABIN WITH RUBBER BURNING SMELL DURING THE TAKE OFF ROLL, BLEED CONFIGURED AUTO/ISO-CLOSED, APU OFF/BOTH ENGINES/BOTH PACKS WHERE ON / REMOVED AND REPLACED RH ACM IAW CRJ900 AMM 21-51-08-000/400-801 A01. OPS AND LEA

Next page: https://openairdocs.org/aircraft/N598NN/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 = 'N598NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N598NN/reports

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