# Service difficulty reports: N582NN

A list on [N582NN](https://openairdocs.org/aircraft/N582NN.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 · 54 reports

- [SDR VNAA2026082523501](https://openairdocs.org/sdr/VNAA2026082523501.md): Selector Valve · unserviceable · Aug 24, 2026 · N582NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE MASTER WARNING / INTERROGATED MDC AND FOUND B1 CODE 005968. PERFORMED OPERATIONAL TEST OF THE LANDING GEAR EXTENSION/RETRACTION SYSTEM IAW AMM 32-30-00-710-801-A01. LANDING GEAR RETRACTION ON ALL GEARS FAILED ON MULTIPLE ATTEMPTS. TROUBLESHOT ALL
- [SDR VNAA2026062620003](https://openairdocs.org/sdr/VNAA2026062620003.md): Control Unit · unserviceable · Jun 25, 2026 · N582NN · Cndair CL6002D24 · Trailing Edge Flap Control System
  > AFTER FLAPS 20 TAKEOFF, FLAPS FAIL CAUTION MSG AND FLAPS FAILED AT FLAPS 17 AND SLATS 20. REMOVE AND REPLACED THE SLATS/FLAPS ELECTRONIC CONTROL UNIT IAW AMM 27-51-05-000/400-801. TESTED THE (SFECU2) BY CLEARING OF INHIBIT IAW AMM 45-45-00-970-821. PERFORM TH
- [SDR VNAA2025032411102](https://openairdocs.org/sdr/VNAA2025032411102.md): Windshield · fire · Mar 23, 2025 · N582NN · Cndair CL6002D24 · Flight Compartment Windows
  > FRONT RIGHT WINDSHIELD SEALANT CAUGHT FIRE AT THE GATE, WINDSHIELD SHATTERED AS A RESULT. [WINDSHIELD HEAT HAD BEEN LEFT IN LOW POSITION FOR THE REPO FROM HANGAR]. NO MEDICAL ATTENTION WAS REPORTED. / PERFORMED INSTALLATION OF THE R/H WINDSHIELD AS REQUIRED
- [SDR VNAA2025011311101](https://openairdocs.org/sdr/VNAA2025011311101.md): Sensor · abnormal · Jan 10, 2025 · N582NN · Cndair CL6002D24 · Airfoil Anti/De-ice System
  > WING OVHT WARNING MSG INTERMITTENT IN FLIGHT. / INSP RH INBD TEMP SENSOR AND FOUND 1 PIN NOT SECURE. INSTALLED PIN IAW AMM 30ˆ’12ˆ’06ˆ’400ˆ’801 OPS CHECK GOOD.
- [SDR VNAA2024122311102](https://openairdocs.org/sdr/VNAA2024122311102.md): Pressure System · unserviceable · Dec 21, 2024 · N582NN · Cndair CL6002D24 · Cabin Pressure Control System
  > CABIN ALTITUDE WARNING MESSAGE AT 24000FT / REMOVED AND REPLACED BOTH CABIN PRESSURE CONTROLLERS IAW CRJ 900 AMM 21-31-04-000/400-801. REMOVED AND REPLACED CABIN PRESSURE CONTROL PANEL IAW CRJ 900 AMM 21-33-01-000/401-801. OPS TEST GOOD. PERFORMED OPS TEST OF
- [SDR VNAA20240619002](https://openairdocs.org/sdr/VNAA20240619002.md): Fitting · corroded · May 22, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > MANUFACTURING PART. IN REFERENCE NRC 00169: FABRICATE PN: A661091-1 (FLOOR FITTING) 1EA IN ACCORDANCE WITH EA NO: A1-690-25-00209. FITTING (1 EA) WAS MANUFATURED PN: A661091-1 PER EA Nº: A1-690-25-00209 REV. ORIGINAL
- [SDR VNAA20240618009](https://openairdocs.org/sdr/VNAA20240618009.md): Frame · corroded · May 22, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME FS= 349 BETWEEN STRG 26LH TO 25RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS= 349 BETWEEN STRG 26LH TO 25RH AT MAIN AVIONICS COMPARTMENT.
- [SDR VNAA20240619012](https://openairdocs.org/sdr/VNAA20240619012.md): Strap · corroded · May 15, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON STRAP, INNER FS 349.00 AND STGR 17LH AT PASSENGER DOOR SURROUND STRUCTURE. FITTING WAS FOUND OUT OFF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
- [SDR VNAA20240619031](https://openairdocs.org/sdr/VNAA20240619031.md): Strap · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON STRAP, INNER FS 319.70 AND STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE. STRAP, INNER FS 319.70 AND STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE WAS REPAIRED PER REO 690-53-21-1774 REV - -
- [SDR VNAA20240619030](https://openairdocs.org/sdr/VNAA20240619030.md): Seat Track · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SIDE SEAT RAIL OF STRG 15LH/RH BETWEEN FS785.15 FS - 847+8.40. CORROSION AT SIDE SEAT RAIL OF STRG 15LH/RH BETWEEN FS785.15 FS - 847+8.40. WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49
- [SDR VNAA20240619029](https://openairdocs.org/sdr/VNAA20240619029.md): Seat Track · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SIDE SEAT RAIL OF STRG 15LH/RH BETWEEN FS744.15 - FS 761.85. EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA20240619028](https://openairdocs.org/sdr/VNAA20240619028.md): Seat Track · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS699.40 - FS 720.85. SIDE SEAT RAIL OF STRG 15LH BETWEEN FS699.40 - FS 720.85 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA20240619027](https://openairdocs.org/sdr/VNAA20240619027.md): Seat Track · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS (SEVERAL LOCATIONS) LBL 9 AND RBL 9 BTW FS 874.00 TO FS 977.00 AT PASSENGER CABIN. PER CRJ900 SRM 53-51-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA20240619026](https://openairdocs.org/sdr/VNAA20240619026.md): Seat Track · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 581 LBL 9.00 AT CABIN PAX. SEAT RAIL BTW FS 477.40 TO FS 581 LBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA20240619025](https://openairdocs.org/sdr/VNAA20240619025.md): Seat Track · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 669.00 RBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 669.00 RBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA20240619024](https://openairdocs.org/sdr/VNAA20240619024.md): Seat Track · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 364 TO FS 477.40 LBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 364 TO FS 477.40 LBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA20240619023](https://openairdocs.org/sdr/VNAA20240619023.md): Seat Track · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON SEAT RAIL BTW FS 349.00 TO FS 477.40 RBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 349.00 TO FS 477.40 RBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA20240619022](https://openairdocs.org/sdr/VNAA20240619022.md): Plate · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON JOINT PLATE FS 519.64 OF FWD BAGGAGE BAY DOOR SURROUND STRUCTURE AT FWD CARGO COMPARTMENT. JOINT PLATE FS 519.64 OF FWD BAGGAGE BAY WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-23-001-001-A02, AND WAS REPLACED PER CRJ900 SRM 51-42-22-001-001-
- [SDR VNAA20240619021](https://openairdocs.org/sdr/VNAA20240619021.md): Strap · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP OF FLOOR STRUCTURE FS 581.00 BTW STGR 24RH TO STGR 27 AT FWD CARGO COMPARTMENT. STRAP OF FLOOR STRUCTURE FS 581.00 BTW STGR 24RH TO STGR 27 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01, WAS FABRICATED PER DWG: SH670-33320
- [SDR VNAA20240619020](https://openairdocs.org/sdr/VNAA20240619020.md): Access Panel · cracked · May 14, 2024 · N582NN · Bombdr CL6002D15 · Aerodynamic Fairings
  > CRACK IN ACCESS PANEL 171CL. ACCESS PANEL 171CL WAS REPAIRED PER REO 670-53-82-430. REV--
- [SDR VNAA20240619017](https://openairdocs.org/sdr/VNAA20240619017.md): Skin · eroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Leading Edge Devices
  > EROSION ON LEADING EDGE AT SLAT 3 OF THE RH WING. LEADING EDGE AT SLAT 3 OF THE RH WING WAS REPAIRED PER REO 690-57-42-1066 REV. --
- [SDR VNAA20240619013](https://openairdocs.org/sdr/VNAA20240619013.md): Intercostal · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS (2 EAS) BTW STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTALS (2 EAS) BTW STA. FS= 349 TO FS= 364 NEAR STGR 27 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND WERE REPLACED PER CRJ
- [SDR VNAA20240619011](https://openairdocs.org/sdr/VNAA20240619011.md): Drag Angle · cracked · May 14, 2024 · N582NN · Bombdr CL6002D15 · Vertical Stabilizer
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01
- [SDR VNAA20240619010](https://openairdocs.org/sdr/VNAA20240619010.md): Drag Angle · cracked · May 14, 2024 · N582NN · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01
- [SDR VNAA20240619009](https://openairdocs.org/sdr/VNAA20240619009.md): Web · cracked · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB. UPPER WEB OF ADG COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01.
- [SDR VNAA20240619005](https://openairdocs.org/sdr/VNAA20240619005.md): Floorbeam · cracked · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR BEAM RBL 12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPAIRED PER REO 690-53-11-1758 REV. --
- [SDR VNAA20240619004](https://openairdocs.org/sdr/VNAA20240619004.md): Floorbeam · cracked · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPAIRED PER REO 690-53-11-1758 REV. --
- [SDR VNAA20240619003](https://openairdocs.org/sdr/VNAA20240619003.md): Rib · cracked · May 14, 2024 · N582NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE OF LH WING WAS REPAIRED PER REO 690-57-51-354 REV. --
- [SDR VNAA20240618010](https://openairdocs.org/sdr/VNAA20240618010.md): Hinge Fitting · excess play · May 14, 2024 · N582NN · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous Structure
  > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #2103 REV. B.
- [SDR VNAA20240618007](https://openairdocs.org/sdr/VNAA20240618007.md): Skin · corroded · May 14, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > CORROSION ON DOOR CUT-OUT INNER SKIN AT E/E MAIN COMPARTMENT. CORROSION ON DOOR CUT-OUT INNER SKIN AT E/E MAIN COMPARTMENT WAS REMOVED AND WAS EVALUATED WITHIN LIMITS PER REO 690-53-21-032 REV. --
- [SDR VNAA20240618006](https://openairdocs.org/sdr/VNAA20240618006.md): Arm · gouged · May 14, 2024 · N582NN · Bombdr CL6002D15 · Cargo/Baggage Doors
  > CTR BAGGAGE BAY DOOR FWD INNER ARM WITHIN 1384.3 FHS FROM IR (BEFORE 19,227.08 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. CTR BAGGAGE BAY DOOR FWD INNER ARM WAS REPAIRED PER REO 690-52-35-411 REV. - - IN REFRENCE TO E
- [SDR VNAA20240619016](https://openairdocs.org/sdr/VNAA20240619016.md): Bracket · corroded · May 13, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. CORROSION ON BRACKETS, MACHINED (7EAS) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-01; CRJ900 SRM 5
- [SDR VNAA20240619015](https://openairdocs.org/sdr/VNAA20240619015.md): Plate · corroded · May 13, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON PLATES (BL0) (2EAS) PLATE 1 BTW FS 517.00 STGR 27. PLATE 2 BTW FS565.00 STGR 27. AT FWD CARGO COMPARTMENT. STRINGER 27 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE FABRICATED PER (EO) SH670-3337, AND WERE REPLACED PE
- [SDR VNAA20240619014](https://openairdocs.org/sdr/VNAA20240619014.md): Mount · cracked · May 13, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > 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. (SM) AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM) WAS REPAIRED PER REO 690-28
- [SDR VNAA20240619008](https://openairdocs.org/sdr/VNAA20240619008.md): Skin · worn · Apr 22, 2024 · N582NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > WEAR ON LOWER SKIN OF SETTLEMENT AREA OF ACCESS PANELS 583AB, 586AB, 592AB AND 597AB AT LH WING. LOWER SKIN OF SETTLEMENT AREA OF ACCESS PANELS 583AB, 586AB, 592AB AND 597AB AT LH WING WAS REPAIRED PER REO 690-57-21-471. REV. - -
- [SDR VNAA20240619006](https://openairdocs.org/sdr/VNAA20240619006.md): Lug · corroded · Apr 22, 2024 · N582NN · Bombdr CL6002D15 · Wing, Control Surface Attach Fittings
  > SCRATCH ON HOUSING OF LUG 1, LUG 2 AND LUG 6 AT RH AILERON WAS FOUND. SCRATCH ON HOUSING OF LUG 1, LUG 2 AND LUG 6 AT RH AILERON WAS FOUND WERE REPAIRED PER REO 670-57-61-237 REV - - NOTES F
- [SDR VNAA20240619007](https://openairdocs.org/sdr/VNAA20240619007.md): Lug · corroded · Apr 22, 2024 · N582NN · Bombdr CL6002D15 · Wing, Control Surface Attach Fittings
  > SCRATCH ON HOUSING OF LUG 2 AND LUG 5 AT LH AILERON WAS FOUND. SCRATCH ON HOUSING OF LUG 2 AND LUG 5 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV - - NOTES F
- [SDR VNAA20240619001](https://openairdocs.org/sdr/VNAA20240619001.md): Hinge · corroded · Apr 22, 2024 · N582NN · Bombdr CL6002D15 · Wing, Control Surface Attach Fittings
  > CORROSION ON HOUSING OF HINGE FITTING 2 (OUTBD AND INBD) FITTING 3 (INBD) AT LH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 2 (OUTBD AND INBD) FITTING 3 (INBD) AT LH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-357 REV. - - AND ETI-900-24-004 REV.
- [SDR VNAA20240618012](https://openairdocs.org/sdr/VNAA20240618012.md): Lug · scratched · Apr 22, 2024 · N582NN · Bombdr CL6002D15 · Wing, Control Surface Attach Fittings
  > HOUSING OF HINGE FITTING 1 (OUTBD), FITTING 3 (OUTBD AND INBD) & FITTING 4 (OUTBD AND INBD) AT RH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 1 (OUTBD), FITTING 3 (OUTBD AND INBD) & FITTING 4 (OUTBD AND INBD) AT RH WING REAR SPAR WERE REPAIRED PER
- [SDR VNAA20240618011](https://openairdocs.org/sdr/VNAA20240618011.md): Lug · scratched · Apr 22, 2024 · N582NN · Bombdr CL6002D15 · Wing, Control Surface Attach Fittings
  > HOUSING OF HINGE FITTING 1 (OUTBD) FITTING 4 (OUTBD AND INBD) AT LH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 1 (OUTBD) FITTING 4 (OUTBD AND INBD) AT LH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-357 REV. - -
- [SDR VNAA20240618005](https://openairdocs.org/sdr/VNAA20240618005.md): Arm · gouged · Apr 22, 2024 · N582NN · Bombdr CL6002D15 · Cargo/Baggage Doors
  > CTR BAGGAGE BAY DOOR AFT INNER ARM WITHIN 1384.3 FHS FROM IR (BEFORE 19,227.08 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. CTR BAGGAGE BAY DOOR AFT INNER ARM WAS REPAIRED PER REO 690-52-35-412 REV. - - IN REFRENCE TO
- [SDR VNAA20240618004](https://openairdocs.org/sdr/VNAA20240618004.md): Skin · damaged · Apr 22, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES (14 EAS) ON FUSELAGE SKIN AT FS 295 TO FS 693 BTW STGR 23RH TO STGR 14RH. LIGHTNING STRIKES (14 EAS) ON FUSELAGE SKIN AT FS 295 TO FS 693 BTW STGR 23RH TO STGR 14RH WERE REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03 AND REO 690-53-21-1769
- [SDR VNAA20240618003](https://openairdocs.org/sdr/VNAA20240618003.md): Hinge · corroded · Apr 22, 2024 · N582NN · Bombdr CL6002D15 · Wing, Control Surface Attach Fittings
  > CENTER FITTING BORE LUG R1, R2, R5 AND R6 AT RH AILERON. CENTER FITTING BORE LUG R1, R2, R5 AND R6 AT RH AILERON WERE REPAIRED PER REO 670-57-61-237 REV--
- [SDR VNAA202406190007](https://openairdocs.org/sdr/VNAA202406190007.md): Hinge · corroded · Apr 22, 2024 · N582NN · Bombdr CL6002D15 · Wing, Control Surface Attach Fittings
  > CENTER FITTING BORE LUG L1, L2, L5 AND L6 AT LH AILERON. CENTER FITTING BORE LUG L1, L2, L5 AND L6 AT LH AILERON.
- [SDR VNAA2024061908001](https://openairdocs.org/sdr/VNAA2024061908001.md): Floor Support · corroded · Apr 22, 2024 · N582NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS (4EAS) LOCATED BTW FS=280 TO FS=295 AND RBL17'' AND RBL 38'', FS=295 AND LBL20'', FS=310 AND LBL37'' AT FUSELAGE FLOOR STRUCTURE. CORROSION ON FLOOR SUPPORTS (4EAS) AT FUSELAGE FLOOR STRUCTURE WERE EVALUATED OUT OF LIMITS PER CRJ-
- [SDR VNAA202307181112](https://openairdocs.org/sdr/VNAA202307181112.md): Sensor · malfunctioned · Jul 14, 2023 · N582NN · Cndair CL6002D24 · Landing Gear Brake System
  > LHIB BRAKE OVHT WARNING MSG AFTER T/O., BTMS INDICATION WOULD RADOMLY DASHOUT START AFTER GEAR RETRACTION AND CONTINUED WITH GEAR EXTENDED. REMOVED AND REPLACED LHIB MLG BRAKE TEMP SENSOR IAW CRJ 900 AMM 32-46-01-000/400-801-A01-PSA. NO FURTHER DEFECTS NOTED A
- [SDR VNAA202201091111](https://openairdocs.org/sdr/VNAA202201091111.md): Brake · overheated · Jan 5, 2022 · N582NN · Cndair CL6002D24 · Landing Gear Brake System
  > DURING LANDING THE CREW GOT A BREAK TEMP OVER HEAT MESSAGE. A EMERGENCY WAS DECLARED BY THE CREW AND TRUCKS DID ROLL IN BUT NOT NEEDED. THE CREW DID NOT CALLED FOR A BRACE ON LANDING. THE AIRCRAFT WAS ABLE TO TAXI TO A GATE UNDER THEIR OWN POWER. NO FURTHER IN
- [SDR VNAA202110211113](https://openairdocs.org/sdr/VNAA202110211113.md): Idg · faulted · Oct 18, 2021 · N582NN · Cndair CL6002D24 · AC Generator-Alternator
  > CREW HAD AN IDG CAUTION MESSAGE INFLIGHT AND RAN THE QRH. CREW MADE THE DECISION TO DIVERT TO CAK AS IT WAS A MX BASE AND COULD LIKELY DEAL WITH THE ISSUE BETTER THAN AN OUTSTATION. IDG 2 CAUTION MESSAGE IN FLIGHT. QRH RUN IDG 2 DISCONNECT PUSHED. / DEF IDG 2
- [SDR VNAA2021102001111](https://openairdocs.org/sdr/VNAA2021102001111.md): Idg · faulted · Oct 18, 2021 · N582NN · Cndair CL6002D24 · AC Generator-Alternator
  > CREW HAD AN IDG CAUTION MESSAGE INFLIGHT AND RAN THE QRH. CREW MADE THE DECISION TO DIVERT TO CAK AS IT WAS A MX BASE AND COULD LIKELY DEAL WITH THE ISSUE BETTER THAN AN OUTSTATION. IDG 2 CAUTION MESSAGE IN FLIGHT. QRH RUN IDG 2 DISCONNECT PUSHED. / DEF IDG 2
- [SDR VNAA202009149991](https://openairdocs.org/sdr/VNAA202009149991.md): Angle · corroded · Sep 14, 2020 · N582NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > FS 280.00 FORWARD "J" ANGLE IS CORRODED. INSTALLED NEW SERVICEABLE FS 280 J ANGLE, IAW CRJ 200 900 SRM 51-42-06-001-001-A01 AND 42-21-001-010-A01.

Next page: https://openairdocs.org/aircraft/N582NN/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 = 'N582NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N582NN/reports

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