# Service difficulty reports: N592NN

A list on [N592NN](https://openairdocs.org/aircraft/N592NN.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 · 64 reports

- [SDR VNAA2026091124701](https://openairdocs.org/sdr/VNAA2026091124701.md): Selector Valve · unserviceable · Sep 9, 2026 · N592NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > PROXIMITY SYSTEM CAUTION AFTER TAKEOFF. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-32-10-000/400-801. PERFORMED NR 3 HYD SYS BLEED. OPS CHKD GOOD. GEAR SWING NEEDS CW.
- [SDR VNAA202504020041](https://openairdocs.org/sdr/VNAA202504020041.md): Lug · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > CORROSION ON BORE LUGS NO.2L, NO.3L, NO.-4L, NO.5L AND NO.6L AT LH AILERON CENTER FITTING BORE LUGS NO.2L, NO.3L, NO.4L, NO.5L AND NO.6L AT LH AILERON CENTER FITTING.WERE CLEANED PER CRJ 900 SRM TASK 51-26-00-001-001-A01 CLEANING & REPAIRED PER REO 670-57-61-
- [SDR VNAA202504020040](https://openairdocs.org/sdr/VNAA202504020040.md): Lug · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > CORROSION ON BORE LUGS NO.1R, NO.2R, NO.4R, NO.5R AND NO.6R AT RH AILERON CENTER FITTING. CENTER FITTINGS LUGS R 1, R 4 AND R 6 WERE CLEANED PER CRJ 900 SRM TASK 51-26-00-001-001-A01 CLEANING & AND NO DAMAGE FOUND & LUGS R 2 AND R 5 WERE REWORKED PER REO 670
- [SDR VNAA202504020039](https://openairdocs.org/sdr/VNAA202504020039.md): Skin · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DURING INSPECTION OF THE TASK CARD 53-21-301-JIC IT WAS DETECTED CORROSION ON INTERNAL SKIN BM FS 280.00 TO 295. CORROSION ON INTERNAL SKIN BTW FS 280.00 TO FS 295.00 AND STGR 25RH TO 24 RH WAS REPAIRED PER REO 690-53-21-1902 REV - -.
- [SDR VNAA202504020038](https://openairdocs.org/sdr/VNAA202504020038.md): Seat Track · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL ON LBL 9 (1EA) BTW FS 485.00 TO FS 581.00 AND RBL9 (1EA) BTW FS 661+32 TO FS669.40. SEAT RAIL ON LBL 9 (1EA) BTW FS 485.00 TO FS 581.00 AND RBL9 (1EA) BTW FS 661+32 TO FS669.40 WAS EVALUATED EXCESSIVE DAMAGE PER CRJ-900 SRM 53-31-49-10
- [SDR VNAA202504020037](https://openairdocs.org/sdr/VNAA202504020037.md): Door Frame · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. EVALUATED,DUE TO DAMAGE EXCEED ALLOWABLE DAMAGE PER CRJ900 SRM 53-21-23-101-001-A02, MID CAP AND REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01.
- [SDR VNAA202504020036](https://openairdocs.org/sdr/VNAA202504020036.md): Striker · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON STRIKER, SEAL BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE. EVALUATED, DUE TO EXCESIVE DAMAGE FOR CORROSIÓN ON STRIKER SEAL BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE IS OUT OFF LIMITSPER CRJ900 SRM53-00-00-1
- [SDR VNAA202504020035](https://openairdocs.org/sdr/VNAA202504020035.md): Seat Track · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL ON RBL 9 (2 EAS) BTWN FS 669.40 TO FS 988. CORROSION ON SEAT RAIL ON RBL 9 (1 EAS) BTWN FS 847 TO FS 988.00 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-51-49-101-001-A02. AND SEAT RAIL
- [SDR VNAA202504020034](https://openairdocs.org/sdr/VNAA202504020034.md): Seat Track · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL ON LBL 9 (2 EAS) BTWN 2FS 669.40 TO FS 985.00. CORROSION ON SEAT RAIL ON LBL 9 (2 EAS) BTWN 2FS 669.40 TO FS 985.00 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-51-49-101-001-A02.
- [SDR VNAA202504020033](https://openairdocs.org/sdr/VNAA202504020033.md): Floor Support · cracked · Apr 2, 2025 · N592NN · 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). CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR
- [SDR VNAA202504020032](https://openairdocs.org/sdr/VNAA202504020032.md): Canister · cracked · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV - -.
- [SDR VNAA202504020031](https://openairdocs.org/sdr/VNAA202504020031.md): Canister · cracked · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV - -.
- [SDR VNAA202504020030](https://openairdocs.org/sdr/VNAA202504020030.md): Panel · damaged · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PERM REPAIR - WITHIN 546.65FH ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. ENGINEERING COMMENTS: REPLACE ANCHOR NUT AS PER CRJ 900 SRM. SUMMARY: ELONGATE HOLE ON ACCESS PANEL DOOR (PN: CC670 10149
- [SDR VNAA202504020029](https://openairdocs.org/sdr/VNAA202504020029.md): Seat Track · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "CORROSION ON SEAT TRACKS LBL 27 (1E/A), LBL 9 (1E/A), RBL 9 (1E/A) BTW FS349.00 TO FS477.40. CORROSION ON SEAT TRACKS, LBL 9 (1E/A), RBL 9 (1E/A) BTW FS349.00 TO FS477.40 WERE EVALUATED EXCESSIVE DAMAGE PER CRJ-900 SRM 53-21-49-101-001-A01 PAR.3 B,FIG. 53-21
- [SDR VNAA202504020028](https://openairdocs.org/sdr/VNAA202504020028.md): Plate · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION ON KICKPLATE BTW FS349 TO FS310 AT PASSENGER DOOR SURROUND. KICKPLATE BTW FS349 TO FS310 AT PASSENGER DOOR SURROUND WAS EVALUATED EXCESSIVE CORROSION PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
- [SDR VNAA202504020027](https://openairdocs.org/sdr/VNAA202504020027.md): Floorbeam · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON RH CROSSBEAM FS 280 AT COCKPIT CABIN FLOOR. CROSSBEAM RH FS 280 AT COCKPIT CABIN FLOOR WAS EVALUATED DUE EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-01-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 5
- [SDR VNAA202504020026](https://openairdocs.org/sdr/VNAA202504020026.md): Floorbeam · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON LH CROSSBEAM FS 280 AT COCKPIT CABIN FLOOR. CROSSBEAM LH FS 280 AT COCKPIT CABIN FLOOR WAS EVALUATED DUE EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-01-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 5
- [SDR VNAA202504020025](https://openairdocs.org/sdr/VNAA202504020025.md): Seat Track · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL (7 EAS) AT STGR 15 RH, BTW FS669.40 TO FS977.00. CORROSION ON RH SIDE SEAT RAIL (7 EAS) AT STGR 15 RH, BTW FS669.40 TO FS977.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND R
- [SDR VNAA202504020024](https://openairdocs.org/sdr/VNAA202504020024.md): Seat Track · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL (6 EAS) AT STGR 15 LH, BTW FS669.40 TO FS977.00. CORROSION ON LH SIDE SEAT RAIL (6 EAS) AT STGR 15 LH, BTW FS669.40 TO FS977.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND RE
- [SDR VNAA202504020023](https://openairdocs.org/sdr/VNAA202504020023.md): Seat Track · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL (4 EAS) AT STGR 15 LH, BTW FS379.00 TO FS669.40. CORROSION ON LH SIDE SEAT RAIL (2EAS) AT STGR 15 LH, BTW FS565.00 TO FS669.40 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED, THEREFORE IS WITHIN LIMITS PER CRJ900
- [SDR VNAA202504020022](https://openairdocs.org/sdr/VNAA202504020022.md): Seat Track · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL (2 EAS) AT STGR 15 RH, BTW FS379.00 TO FS669.40. CORROSION ON RH SIDE SEAT RAIL (2 EAS) AT STGR 15 RH, BTW FS379.00 TO FS669.40. WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-31-4
- [SDR VNAA202504020021](https://openairdocs.org/sdr/VNAA202504020021.md): Intercostal · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL IN STA. FS= 349 TO FS= 364 BTW STGR 27 TO STGR 26RH AT MAIN AVIONICS COMPARTMENT. EVALUATED, DUE IT NOT ALLOW DAMAGE ON INTERCOSTAL IN STA. FS= 349 TO FS= 364 BTW STGR 27 TO STGR 26RH AT MAIN AVIONICS COMPARTMENT PER CRJ-900 SRM 53-2
- [SDR VNAA202504020019](https://openairdocs.org/sdr/VNAA202504020019.md): Floorbeam · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00. FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00 WAS EVALUATED EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-01-001-001-A01 AND REPLACED PER CRJ-900 SR
- [SDR VNAA202504020020](https://openairdocs.org/sdr/VNAA202504020020.md): Rub Strip · worn · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > "WEAR FOUND ON UPPER/LOWER AFT EDGE RUB STRIP OF FWD CORE COWL AT RH ENGINE. UPPER/LOWER AFT EDGE RUB STRIP OF FWD CORE COWL AT RH ENGINE WERE REPLACED PER CRJ900 SRM 54-23-00-201-006-A01"
- [SDR VNAA202504020018](https://openairdocs.org/sdr/VNAA202504020018.md): Channel · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED CHANNEL AND STRAP JOINT BTWN AFT FAIRING ACCESS PANEL 195DLJ196DR. EVALUATED,VISUAL INSPECTION AFTER CLEANED ON STRAP AND CHANEL WAS PERFORMED PER CRJ 900 SRM 51-11-00-001-001-A01, CRJ 900 NDT MANUAL 51-20-009-210 AND CRJ900 SRM 53-00-00-101-001-A01,
- [SDR VNAA202504020017](https://openairdocs.org/sdr/VNAA202504020017.md): Support · cracked · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. WAS REPAIRED PER. REO 690-28-25-034 REV.-
- [SDR VNAA202504020016](https://openairdocs.org/sdr/VNAA202504020016.md): Balance Arm · damaged · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Doors
  > WEAR ON FWD COUTER BALANCE ARMS AT FWD COMPARTMENT DOOR MECHANISM. WEAR ON FWD COUTER BALANCE ARMS AT FWD COMPARTMENT DOOR MECHANISM WERE REPAIRED PER CRJ900 SRM 52-35-09-201-001-A01 AND REO 690-52-35-489.
- [SDR VNAA202504020015](https://openairdocs.org/sdr/VNAA202504020015.md): Balance Arm · damaged · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > DAMAGED FWD/AFT COUNTER BALANCE ARMS AT CENTER CARGO COMPARTMENT DOOR MECHANISMS. FWD/AFT COUNTER BALANCE ARMS AT CENTER CARGO COMPARTMENT DOOR MECHANISMS WERE REPAIR PER REO 690-52-35-498 REV. - -.
- [SDR VNAA202504020014](https://openairdocs.org/sdr/VNAA202504020014.md): Skin · gouged · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL GOUGES ON SKIN BTW FS629.00 TO FS661.00 AND STGR 25 LH TO STGR 27 AT CENTER FUSELAGE. BLEN OUT ON GOUGES OVER SKIN BTW FS629.00 TO FS661.00 AND STGR 25 LH TO STGR 27 AT CENTER FUSELAGE WAS REPAIRED PER REO 690-53-31-937 REV- -.
- [SDR VNAA202504020013](https://openairdocs.org/sdr/VNAA202504020013.md): Arm · worn · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > WEAR ON AFT INNER ARM AT CTR BAGGAGE-BAY DOOR. WEAR ON AFT INNER ARM AT CTR BAGGAGE-BAY DOOR WAS REPAIRED PER REO 690-52-35-497 REV --. PERFORM DETAILED VISUAL INSPECTION PER NDTM 51-20-009 AT INTERVALS NOT TO EXCEED 800 FLIGHT HOU•R S TO ENSURE NO DAMAGE PRO
- [SDR VNAA202504020012](https://openairdocs.org/sdr/VNAA202504020012.md): Channel · cracked · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Aerodynamic Fairings
  > CRACKED CHANNEL AND STRAP JOINT BTWN AFT FAIRING ACCESS PANEL 195DL1196DR. EVALUATED,VISUAL INSPECTION AFTER CLEANED ON STRAP AND CHANEL WAS PERFORMED PER CRJ 900 SRM 51-11-00-001-001-A01 AND CRJ 900 NDT MANUAL 51-20-009-210 CORROSION ON STRAP WAS FOUND, NO C
- [SDR VNAA202504020011](https://openairdocs.org/sdr/VNAA202504020011.md): Fitting · corroded · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Service Doors
  > CORROSION ON HINGE AND HINGE FITTINGS AT SERVICE DOOR 196ER (ATTACHMENT HARDWARE INCLUDED). DUE TO EXCESSIVE DAMAGE, HINGES AND HINGE FITTINGS AT SERVICE DOOR 196ER WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SR
- [SDR VNAA202504020010](https://openairdocs.org/sdr/VNAA202504020010.md): Yoke · worn · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Control Column Section
  > INITIAL INSPECTION: WEAR ON YOKE ASSEMBLY OF THE SWIVEL PULLEY OF THE POWER-ASSIST CABLE ON THE INNER SIDE OF THE PASSENGER DOOR. WEAR ON YOKE ASSEMBLY OF THE SWIVEL PULLEY OF THE POWER-ASSIST CABLE ON THE INNER SIDE OF THE PASSENGER DOOR WAS REPAIRED PER REO
- [SDR VNAA202504020009](https://openairdocs.org/sdr/VNAA202504020009.md): Housing · worn · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > WEAR ON HOUSING OF EXTERNAL HANDLE AT AFT BAGGAGE BAY DOOR. HOUSING OF EXRENAL HANDLE AT AFT BAGGAGE BAY DOOR WAS REPAIRED PER REO 670-52-31-031 REV B.
- [SDR VNAA202504020008](https://openairdocs.org/sdr/VNAA202504020008.md): Angle · cracked · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DA
- [SDR VNAA202504020007](https://openairdocs.org/sdr/VNAA202504020007.md): Drag Angle · cracked · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPA
- [SDR VNAA202504020006](https://openairdocs.org/sdr/VNAA202504020006.md): Skin · dented · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > BIRD STRIKE DAMAGE WITHIN 795.42 FLIGHT HOURS OF INITIAL RELEASE AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. BIRD STRIKE DAMAGE, FRAME WAS REPAIRED PER REO 670-51-00-085.REV. -A AN
- [SDR VNAA202504020005](https://openairdocs.org/sdr/VNAA202504020005.md): Skin · chafed · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > PASSENGER DOOR SURROUND SKIN CHAFE DAMAGE WITHIN 652 FLIGHT HOURS FROM EXTENSION REQUEST (2,173 FH TOTAL), ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. PASSENGER DOOR SURROUND SKIN CHAFE DAMAGE PERM
- [SDR VNAA202504020004](https://openairdocs.org/sdr/VNAA202504020004.md): Guide Block · gouged · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > CENTER BAGGAGE BAY DOOR AFT UPPER AND LOWER GUIDE BLOCKS GOUGED. ALSO, CENTER GUIDE PIN GOUGED SAME LOCATION. AFT UPPER AND LOWER GUIDE BLOCKS GOUGED AND CENTER GUIDE PIN GOUGED ON CENTER BAGGAGE BAY DOOR WERE REPAIRED PER REO 690-53-31-942 REV - - AND PER EA
- [SDR VNAA202504020003](https://openairdocs.org/sdr/VNAA202504020003.md): Skin · gouged · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > PERM REPAIR - GOUGES TO FUSELAGE SKIN BETWEEN FS1031.00 - 1051.30 AND STR 21R-26R THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 6200 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO. WITHIN 2000 FLIGHT HOURS ACCOMPLISH A PERMANENT REPAIR IN ACCORDANC
- [SDR VNAA202504020002](https://openairdocs.org/sdr/VNAA202504020002.md): Floorbeam · cracked · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > INITIAL INSPECTION: CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690
- [SDR VNAA202504020001](https://openairdocs.org/sdr/VNAA202504020001.md): Floorbeam · cracked · Apr 2, 2025 · N592NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO690-53-11-1950 REV- -.
- [SDR VNAA2024080111101](https://openairdocs.org/sdr/VNAA2024080111101.md): A/C Pack · unserviceable · Jul 28, 2024 · N592NN · Cndair CL6002D24 · Cabin Cooling System
  > DURING TAXING INTO THE GATE, L PACK AUTO FAIL CAUTION MSG, FOLLOWED BY BURNING SMELL FWD CABIN SMOKE. L PACK FAULT STATUS MSG AFTER TURNING THE PACK OFF / FOUND LH ACM SEIZED, REPLACED LH PACK ACM IAW CRJ 900 AMM 21-51-08-400-801-A01. OPS CHECK AND LEAK CHECK
- [SDR VNAA202203151112](https://openairdocs.org/sdr/VNAA202203151112.md): Door Latch · worn · Mar 11, 2022 · N592NN · Cndair CL6002D24 · Service Doors
  > FLIGHT RETURNED TO FIELD DUE TO FORWARD SERVICE DOOR CAUTION MESSAGE. CREW REPORTS THAT THEY LANDED OVERWEIGHT AND DECLARED AN EMERGENCY. AIRCRAFT WAS ABLE TO MAKE IT BACK TO GATE UNDER THEIR OWN POWER. EMERGENCY VEHICLES WERE DISPATCHED. AIRCRAFT WILL NEED TO
- [SDR VNAA2021091399912](https://openairdocs.org/sdr/VNAA2021091399912.md): Web · cracked · Sep 14, 2021 · N592NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > CRACK FOUND AT FWD WEB OF PAX DOOR AT THE HANDRAIL BRACKET. C/W CRJ900 SRM REPAIR 52-11-04-201-004-A01.
- [SDR VNAA2021091399911](https://openairdocs.org/sdr/VNAA2021091399911.md): Seat Track · corroded · Sep 14, 2021 · N592NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK IS CORRODED BETWEEN FS 985 TO FS 1000. INSTALLED NEW SERVICEABLE SEAT TRACK RBL 9 BETWEEN FS 985 TO FS 1000 IAW CRJ900 AMM 53-00-49-4000-801-A12.
- [SDR VNAA2021091399910](https://openairdocs.org/sdr/VNAA2021091399910.md): Seat Track · corroded · Sep 14, 2021 · N592NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL9 BETWEEN FS 841+16 TO FS 989 REQUIRES FABRICATION DUE TO CORRODED BEYOND LIMITS. INSTALLED SEAT TRACK AT RBL 9 BETWEEN FS 847+16 TO FS 989 IAW CRJ900 AMM 53-00-49-400-801 (CONFIG A12).
- [SDR VNAA202109139999](https://openairdocs.org/sdr/VNAA202109139999.md): Floor Support · corroded · Sep 14, 2021 · N592NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > R/H/S FWD FUSELAGE FS 280-310 SIDE SILL CORRODED. INSTALLED NEW R/H FLOOR SILL FROM FS 280-310 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR VNAA202109139998](https://openairdocs.org/sdr/VNAA202109139998.md): Seat Track · corroded · Sep 14, 2021 · N592NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 FLOOR SEAT TRACK FS 349-493 SEGMENT IS CORRODED. INSTALLED SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A12.
- [SDR VNAA202109139997](https://openairdocs.org/sdr/VNAA202109139997.md): Seat Track · corroded · Sep 14, 2021 · N592NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 27 FLOOR SEAT TRACK FS 364-477 SEGMENT IS CORRODED. INSTALLED SEAT TRACK AT LBL 27 FS 364-485 IAW CRJ900 AMM 53-00-49-400-801-A12.

Next page: https://openairdocs.org/aircraft/N592NN/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 = 'N592NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N592NN/reports

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