# Service difficulty reports: N574NN

A list on [N574NN](https://openairdocs.org/aircraft/N574NN.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 VNAA2026102026701](https://openairdocs.org/sdr/VNAA2026102026701.md): Fan · failed · Oct 17, 2026 · N574NN · Cndair CL6002D24 · Air Distribution Fan
  > EVACUATION FOR FUMES IN AIRCRAFT. C/W FIM 21-22-00-810-806-A01 AND 21-21-00-810-806-A01. CABIN FUMES APPEAR TO BE FROM ACTIVATION OF O2 GENERATORS. FLIGHT DECK FUMES APPEAR RELATED TO NR 2 DISPLAY FAN FAIL. REMOVED AND REPLACED DISPLAY COOLING FAN NR 2 IAW A
- [SDR VNAA2026062920101](https://openairdocs.org/sdr/VNAA2026062920101.md): Actuator · unserviceable · Jun 25, 2026 · N574NN · Cndair CL6002D24 · Elevator Tab Control System
  > PITCH FEEL CAUTION IN FLIGHT / REMOVED LINEAR ACTUATOR #1 A141 AND INSTALLED LINEAR ACTUATOR #2 A140 IN ITS POSITION. OPS CHECK GOOD. INSTALLED NEW LINEAR ACTUATOR IAW AMM 27-31-23-400-801-A01-PSA. OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA2026062319201](https://openairdocs.org/sdr/VNAA2026062319201.md): Door · faulted · Apr 22, 2026 · N574NN · Cndair CL6002D24 · Doors
  > OVERHEAD BIN AT 15AC NOT ALLOWING FWD AND AFT EMERGENCY EXITS TO OPEN FOR EGRESS / PERFORMED ADJUSTMENT OF THE RODS OF THE OVERHEAD STORAGE COMPARTMENT INSTALLED ABOVE THE OVERWING EMERGENCY EXIT ON OVERHEAD BIN AT SEATS 15,16AC IAW AMM 25-23-00-820-803. INSTA
- [SDR VNAA2024110811101](https://openairdocs.org/sdr/VNAA2024110811101.md): Brake · faded · Nov 7, 2024 · N574NN · Cndair CL6002D24 · Landing Gear Brake System
  > I BELIEVE WE HAD A FLAT TIRE ON T/O. SLOWER ACCELLERATION. / PERFORMED GVI OF #1 BRAKE AS REQUIRED. BLED #1 BRAKE IAW CRJ900 AMM 32-43-00-870-801-A01-PSA. BRAKE #1 OPS CHECK SAT. A/C OK TO CONTINUE SERVICE. TAXI CHECK PERFORMED WITH CREW. NO DEFECTS NOTED.
- [SDR VNAA202405130029](https://openairdocs.org/sdr/VNAA202405130029.md): Fitting · corroded · Apr 26, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > IN REFERENCE NRC 00204: FABRICATE FITTING PN: A414252-3 (1EA) FWD LAV IN REFERENCE EA NO: A1-690-25-00182. FITTING PN: A414252-3 (1EA) FWD LAV WAS FABRICATED PER EA NO: A1-690-25-00182 SECTION III-PERMANENT REPAIR REV-- DATE 2024-04-26
- [SDR VNAA202405130028](https://openairdocs.org/sdr/VNAA202405130028.md): Fitting · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > WORK SHOP INTERIOR SHEET METAL: CORROSION ON FITING (1EA) BELOW THE SERVICE TABLE AT FWD LAV. FITTING P/N: A414252-3 (1EA) BELOW THE SERVICE TABLE AT FWD LAV. WAS REPLACED PER SAFRAN CMM 25-40-40
- [SDR VNAA202405130027](https://openairdocs.org/sdr/VNAA202405130027.md): Skin · damaged · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON EXTERNAL FUSELAGE ON FS 661 + 8 AND FS 661 + 16 BTW STGR 26/27 LH LIGTHING STRIKE ON EXTERNAL FUSELAGE ON FS 661 + 8 AND FS 661 + 16 BTW STGR 26/27 LH WAS REPAIRED PER REO 690-53-31-833 REV.- -
- [SDR VNAA202405130026](https://openairdocs.org/sdr/VNAA202405130026.md): Skin · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > CORROSION ON STGR 22RH BTW FS 1015.00 AND FS 1031.00 AT AFT CARGO COMPARTMENT, SKING WAS DRILLING IN REF NRC 00116. STRINGER 22RH BTW FS1015 TO FS1031 AT AFT CARGO COMPARTMENT AND FUSELAGE SKIN WERE REPAIRED PER REO 690-53-61-1377 REV --
- [SDR VNAA202405130025](https://openairdocs.org/sdr/VNAA202405130025.md): Hinge Fitting · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Ailerons
  > CORROSION ON BORE LUGS L4, L5 & L6 AT HINGE FITTINGS OF THE LH AILERON ASSY. BORE LUGS L4, L5 & L6 AT HINGE FITTINGS OF THE LH AILERON ASSY WERE REPAIRED PER REO 670-57-61-237 REV. --
- [SDR VNAA202405130024](https://openairdocs.org/sdr/VNAA202405130024.md): Floorbeam · cracked · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACK ON FLOOR BEAM RBL12, FS 280.00 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM RBL12, FS 280.00 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1725 REV. - -
- [SDR VNAA202405130023](https://openairdocs.org/sdr/VNAA202405130023.md): Floorbeam · cracked · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACK ON FLOOR BEAM LBL12, FS 280.00 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL12, FS 280.00 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1724 REV. - -
- [SDR VNAA202405130022](https://openairdocs.org/sdr/VNAA202405130022.md): Canister · cracked · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuel Storage
  > DURING INSPECTION OF THE TASK CARD TRFKE000WLRC: 600-08E2-JIC IT WAS DETECTED 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 REPAIRED PER REO PER REO 670-57-42-
- [SDR VNAA202405130021](https://openairdocs.org/sdr/VNAA202405130021.md): Floor Support · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON LBL27 FLOOR BEAM UPPER FACE BETWEEN FS1000.00- FS1047.00 AT AFT CARGO COMPRTMENT. LBL27 FLOOR BEAM UPPER FACE BETWEEN FS1000.00- FS1047.00 AT AFT CARGO COMPRTMENT WAS REPAIRED PER REO 690-53-61-1379. REV. --
- [SDR VNAA202405130020](https://openairdocs.org/sdr/VNAA202405130020.md): Floorbeam · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORROSION ON LBL9 FLOOR BEAM UPPER FACE BETWEEN FS1000.00- FS1047.00 AT AFT CARGO COMPRTMENT. LBL9 FLOOR BEAM UPPER FACE BETWEEN FS1000.00- FS1047.00 AT AFT CARGO COMPRTMENT WAS REPAIRED PER REO 690-53-61-1374. REV. --
- [SDR VNAA202405130019](https://openairdocs.org/sdr/VNAA202405130019.md): Doubler · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND ON AFTER ATG ANTENNA DOUBLERS INTERNAL STRUCTURE AND STIFFENERS BTW STA: 1007. STG 25R TO 26R. TG ANTENNA DOUBLERS INTERNAL STRUCTURE AND STIFFENERS WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WERE REPLACED PE
- [SDR VNAA202405130018](https://openairdocs.org/sdr/VNAA202405130018.md): Seat Track · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL RBL 9, LBL9 AND LBL27 BTW FS485.00 TO FS693.00 ON PASSENGER COMPARTMENT FLOOR STRUCTURE. SEAT RAIL RBL 9, LBL9 AND LBL27 BTW FS485.00 TO FS693.00 ON PASSENGER COMPARTMENT FLOOR STRUCTURE WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 5
- [SDR VNAA202405130017](https://openairdocs.org/sdr/VNAA202405130017.md): Seat Track · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > SENGER COMPARTMENT FLOOR STRUCTURE. DUE TO CORROSION ON SEAT RAILS RBL 9, LBL9 AND LBL27 BTW FS 349.00 TO FS 485.00 WAS NOT ALLOWED, WERE FOUND OUT OF LIMITS AND MUST BE REPLACED PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ-900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202405130016](https://openairdocs.org/sdr/VNAA202405130016.md): Seat Track · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL AT STGR 15RH, BTW FS 744.15 TO FS 761.85. E TO NOT PERMISIBLE DAMAGE ON RH SIDE SEAT RAIL AT STGR 15RH, BTW FS 744.15 TO FS 761.85 WAS REPLACED PER CRJ/900 SRM 53-41-49-101-001-A02 AND CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202405130015](https://openairdocs.org/sdr/VNAA202405130015.md): Seat Track · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL AT STGR 15RH, BTW FS 708.00 TO FS 720.85. DUE TO NOT ALLOWED DAMAGED ON SIDE SEAT RAIL OF STRG 15RH, BTW FS 677.00 TO FS 720.85 WAS REPLACED PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202405130014](https://openairdocs.org/sdr/VNAA202405130014.md): Rib · cracked · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > AFTER INTERNAL ZONAL INSPECTION, CRACK ON WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-346 REV.--
- [SDR VNAA202405130013](https://openairdocs.org/sdr/VNAA202405130013.md): Rib · cracked · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > AFTER INTERNAL ZONAL INSPECTION, CRACK ON WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-347 REV.--
- [SDR VNAA202405130012](https://openairdocs.org/sdr/VNAA202405130012.md): Bracket · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER SRM CRJ900 SRM 53-32-58-101-001-A01 AND REPLACE PER CRJ900 SRM 51-
- [SDR VNAA202405130011](https://openairdocs.org/sdr/VNAA202405130011.md): Web · cracked · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR VNAA202405130010](https://openairdocs.org/sdr/VNAA202405130010.md): Support Fitting · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON RH JACK FITTING SUPPORT RH, BTW FS265.00 TO FS278.00, BL0.00. IN REF TO: CARD TRFKE000YVWZ, CORROSION ON FRAME FS265.00 BTW SRGR 27 TO STGR 26RH. CORROSION ON RH JACK FITTING SUPPORT RH, BTW FS265.00 TO FS278.00, BL0.00 AND ON FRAME FS265.00 BTW
- [SDR VNAA20240513008](https://openairdocs.org/sdr/VNAA20240513008.md): Flap · nicked · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Trailing Edge Flaps
  > SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50. SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50 WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE EVALUATED BTW FLS15 TO FLS42 OUT OF LIMITS
- [SDR VNAA20240513007](https://openairdocs.org/sdr/VNAA20240513007.md): Skin · dented · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Trailing Edge Flaps
  > DENTS (3 LOCATIONS) ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 75.60 TO FLS 92.80. DENTS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 75.60 TO FLS 92.80 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 57-52-01-101-001-A01 AND WERE REPAIRED PER CRJ900 SRM 57-52-01-201-
- [SDR VNAA20240513006](https://openairdocs.org/sdr/VNAA20240513006.md): Skin · nicked · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Trailing Edge Flaps
  > SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP BTW FLS 15.00 TO FLS 65.50 WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE EVALUATED BTW FLS15 TO FLS42 OUT OF LIMITS AND B
- [SDR VNAA20240513005](https://openairdocs.org/sdr/VNAA20240513005.md): Hinge Fitting · excess play · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Rudder 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 VNAA20240513004](https://openairdocs.org/sdr/VNAA20240513004.md): Rib · cracked · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > AFTER INTERNAL ZONAL INSPECTION, CRACK ON WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-347 REV.--
- [SDR VNAA20240513003](https://openairdocs.org/sdr/VNAA20240513003.md): Bracket · corroded · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT.: BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER SRM CRJ900 SRM 53-32-58-101-001-A01 AND REPLACE PER CRJ900 SRM
- [SDR VNAA20240513002](https://openairdocs.org/sdr/VNAA20240513002.md): Skin · worn · Apr 18, 2024 · N574NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-460 REV. - -
- [SDR VNAA20240513009](https://openairdocs.org/sdr/VNAA20240513009.md): Tie Bar · worn · Apr 8, 2024 · N574NN · Bombdr CL6002D15 · Engine Thrust Reverser
  > INITIAL INSPECTION: WEAR ON THRUST REVERSER FLOATING TIE BAR (2EA) UPPER AND LOWER AT RH ENGINE. R ON THRUST REVERSER FLOATING TIE BAR (2EA) UPPER AND LOWER AT RH ENGINE WERE REPAIRED PER REO 690-54-22-066 REV. --, REO 690-54-22-067 REV. --, REO 690-54-24-015
- [SDR VNAA20240513001](https://openairdocs.org/sdr/VNAA20240513001.md): Skin · worn · Mar 20, 2024 · N574NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-459 REV. - -
- [SDR VNAA202304061112](https://openairdocs.org/sdr/VNAA202304061112.md): Unknown · unknown · Apr 5, 2023 · N574NN · Cndair CL6002D24 · Wing, Control Surfaces
  > 12€? SCRATCH WITH A MAX DEPTH OF.002€? IN THE LEADING EDGE OF THE #2 RH SLAT LEADING EDGE SKIN. PERMANENT REPAIR WAS C/W PER REO 690-57-42-972 INSTRUCTIONS.
- [SDR VNAA202210061113](https://openairdocs.org/sdr/VNAA202210061113.md): None · none · Oct 5, 2022 · N574NN · Cndair CL6002D24 · Air Distribution System
  > ELECTRICAL SMELL IN A/C CABIN AND CARGO COMP ON GROUND / CW CRJ 900 FIM 21-21-00-810-806(A01). NO DEFECTS NOTED.
- [SDR VNAA202103291111](https://openairdocs.org/sdr/VNAA202103291111.md): Acm · failed · Mar 29, 2021 · N574NN · Cndair CL6002D24 · Cabin Cooling System
  > ON TAXI OUT THE CAPTAIN/FO BEGAN TO SMELL A BURNING SMELL THEN GOT A CALL FROM THE FA IN THE BACK SAYING THERE IS SMOKE. THE PAX THEN EVACUATED THROUGH THE MAIN CABIN DOOR ON THE TAXIWAY. THE SMOKE WAS COMING FROM THE CENTER OF THE AIRCRAFT ACCORDING TO THE FA
- [SDR VNAA202102091112](https://openairdocs.org/sdr/VNAA202102091112.md): Skin · dented · Feb 5, 2021 · N574NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DURING OVERNIGHT MAINTENANCE AT DAYTON, OH (DAY), TECHNICIANS FOUND A DENT IN THE TOP FUSELAGE NOSE SKIN PANEL CENTERED ON THE PANEL AND LOCATED SLIGHTLY AFT OF THE FS 169 SPLICE. THE DENT MEASURES APPROXIMATELY 4.6Ï¿½ X 4.5Ï¿½ X.15Ï¿½ DEEP AND IS NOT WITHIN
- [SDR VNAA202102051111](https://openairdocs.org/sdr/VNAA202102051111.md): Stringer · damaged · Feb 3, 2021 · N574NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > REMOVED AND REPLACED ZONE 210 CENTER-LINE STRINGER ZONE 210 BELOW UPPER NOSE SKIN FORWARD EQUIPMENT COMPARTMENT, FROM FS169.00 TO FS202.75 PN CC670-33116-1 IAW CRJ900 SRM 51-42-06 AND SRM 51-40-11. THIS IS A MAJOR REPAIR. FORM 337 COMPLETED.
- [SDR VNAA2020080499911](https://openairdocs.org/sdr/VNAA2020080499911.md): Frame · corroded · Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > FWD AVI BAY FS 295 FRAME CORRODED BETWEEN STRG 26L TO 26R. INSTALLED NEW FRAME SEGMENT, 2 SPLICES, AND ATTACHING ANGLES AND PERFORMED FS295.00 FRAME REPAIR IAW CRJ900 SRM 53-00-06-201-006-A01.
- [SDR VNAA2020080499910](https://openairdocs.org/sdr/VNAA2020080499910.md): Floorbeam · corroded · Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > FS 280 FLOOR SUPPORT CROSSBEAM FLOOR SUPPORT J-ANGLE CORRODED BETWEEN LBL 9 AND RBL 9. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FS 280 J ANGLE BETWEEN LBL 9 & RBL 9 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR VNAA202008049999](https://openairdocs.org/sdr/VNAA202008049999.md): Web · cracked · Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR FWD HANDRAIL RETAINING BRACKET, FOUND FWD PAX DOOR STAIR WEB CRACKED. REPAIR DAMAGE IAW SRM 52-11-04-201-004-A01
- [SDR VNAA202008049998](https://openairdocs.org/sdr/VNAA202008049998.md): Intercostal · corroded · Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > UPON INSPECTION OF FS 349-364, INTERCOSTAL AT LBL 3 CORRODED AROUND LIGHTNING HOLES. FOUND INTERCOSTAL AND RBL3 FS 349-364 TO BE CORRODED AROUND LIGHTNING HOLES AS WELL. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL (P/N SH670-32075-4) IAW CRJ900
- [SDR VNAA202008049997](https://openairdocs.org/sdr/VNAA202008049997.md): Floor Support · corroded · Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL LOWER FLOOR SUPPORT ANGLE IS CORRODED. LOCATED, DRILLED AND INSTALLED PAX DOOR LOWER SILL FLOOR ANGLE SUPPORT IAW CRJ 900 SRM 51-40-11-001-001-A01.
- [SDR VNAA202008049996](https://openairdocs.org/sdr/VNAA202008049996.md): Bracket · corroded · Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY FLOOR STRUCTURE AT FS 581, LBL 2.6 MACHINED BRACKET CORRODED. LOCATED, DRILLED AND INSTALLED NEW MACHINED BRACKET IAW CRJ 900 SRM 51-40-11-001-001-A01.
- [SDR VNAA202008049995](https://openairdocs.org/sdr/VNAA202008049995.md): Bracket · corroded · Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY FLOOR STRUCTURE AT FS 533, LBL 2.6 MACHINED BRACKET CORRODED. COMPLETED REPAIR IAW STS EA 80-2020-001-001 REV IR
- [SDR VNAA202008049994](https://openairdocs.org/sdr/VNAA202008049994.md): Intercostal · corroded · Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > AVI BY, FS 349-364 INTERCOSTAL AT LBL 3 CORRODED AROUND LIGHTING HOLES STRG 27L. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL SH670-32075-3 IAW CRJ 900 SRMS 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR VNAA202008049993](https://openairdocs.org/sdr/VNAA202008049993.md): Seat Track · corroded · Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACKS LH AND RH SIDES FROM STA 379 TO 969 ARE CORRODED. FABRICATED AND REPLACED SEAT TRACKS IAW CRJ 900 SRM 53-00-49-201-002-A01 AND 51-40-11-001-001-A01. 22 TOTAL REPLACED.
- [SDR VNAA202008049992](https://openairdocs.org/sdr/VNAA202008049992.md): Drag Angle · cracked · Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE APPEARS TO BE CRACKED AT ASSIST PULLEY BRACKET. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 52-11-04-201-002-A01.
- [SDR VNAA202008049991](https://openairdocs.org/sdr/VNAA202008049991.md): Drag Angle · cracked · Aug 4, 2020 · N574NN · Bombdr CL6002D15 · Vertical Stabilizer
  > LEFT VERTICAL STAB AFT DRAG ANGLE CRACKED.2" LONG AT FWD END. LOCATED, DRILLED AND INSTALLED NEW LEFT VERTICAL STAB AFT DRY ANGLE IAW SRM 51-40-11-001-001-A01.
- [SDR VNAA2019103111101](https://openairdocs.org/sdr/VNAA2019103111101.md): Probe · failed · Oct 31, 2019 · N574NN · Cndair CL6002D24 · Landing Gear Brake System
  > DURING CLIMB, RECEIVED BRAKE OVERHEAT MSG. CREW DECLARED AN EMERGENCY AND RETURNED TO CLT. TRUCKS DID ROLL. AIRCRAFT LANDED AND WAS INSPECTED BY FIRE DEPT. AIRCRAFT THEN TAXIED TO THE GATE. MX DEFERRED RH IB BRAKE TEMP INDICATION. REMOVED AND REPLACED RH

Next page: https://openairdocs.org/aircraft/N574NN/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 = 'N574NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N574NN/reports

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