# Service difficulty reports: N572NN

A list on [N572NN](https://openairdocs.org/aircraft/N572NN.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 · 60 reports

- [SDR VNAA2026082423401](https://openairdocs.org/sdr/VNAA2026082423401.md): Skin · dented · Aug 21, 2026 · N572NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENT FOUND BELOW AFT CARGO. BETWEEN FS1000.00 AND FS1015.00, STRG 19LH AND STRG 20LH. PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN MHIRJ REO 690-53-61-1772
- [SDR VNAA2026060918601](https://openairdocs.org/sdr/VNAA2026060918601.md): Acm · unserviceable · Jun 5, 2026 · N572NN · Cndair CL6002D24 · Cabin Cooling System
  > L PACK SHOWING 99C OUTPUT. SMOKE ODOR IN COCKPIT DURING APPROACH. DEFERRED LH PACK PER MEL 21-51-01-3. REMOVED AND REPLACED LH AIR CYCLE MACHINE IAW AMM 21€“51€“08€“000/400€“801-A01. OPS CHECK AND LEAK CHECK GOOD.
- [SDR VNAA2026040615801](https://openairdocs.org/sdr/VNAA2026040615801.md): Pump · overtemp · Apr 4, 2026 · N572NN · Cndair CL6002D24 · Hydraulic Pump (Electric/Engine), Main
  > HYD 3 HIGH TEMP CAUTION. TEMP AND PRESSURE GOOD ON 3B FAILED WITH 3A PUMP ON. / REMOVED AN REPLACED 3A ACMP IAW AMM 29-12-03-000/400-801-A01. SERVICED AND BLED HYD SYS 3 NO LEAK NOTED. OPS TEST GOOD AT THIS TIME.
- [SDR VNAA2026032515103](https://openairdocs.org/sdr/VNAA2026032515103.md): Manifold · unserviceable · Mar 21, 2026 · N572NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP CAUTION MSG APPEARED ON TAKE OFF ROTATION AND REMAINED ON THROUGHOUT FLIGHT. / REMOVED AND REPLACED THE STEERING MANIFOLD FROM NGL IAW CRJ 900 AMM 32-51-50-000-801. PERFORMED OPS CHECK OF NOSE WHEEL STEERING IAWCRJ900 AMM 32-51-00-710-801. OPS C
- [SDR VNAA2026021812502](https://openairdocs.org/sdr/VNAA2026021812502.md): Selector Valve · faulted · Feb 16, 2026 · N572NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > STEERING INOP MSG AFTER ROTATION BEFORE 400FT AGL, AFTER GEAR SELECTED UP / REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ 900 AMM 32-32-10-000/400-801-A01.RAN OPS CHECK IAW CRJ 900 32€“30€“00€“710€“801 OPS CHECK GOOD NO FURTHER DEFECTS NOTED.
- [SDR VNAA2025112611102](https://openairdocs.org/sdr/VNAA2025112611102.md): Unknown · odor · Nov 24, 2025 · N572NN · Cndair CL6002D24 · Air Distribution System
  > FLIGHT ATTENDANTS ADVISED US OF A STRONG SMOKE ODOR IN THE CABIN AROUND ROWS 15 AND 16 PRIOR TO LANDING. C/W FIM 21-22-00-810-806-A01. COULD NOT DUPLICATE.
- [SDR VNAA2025112011101](https://openairdocs.org/sdr/VNAA2025112011101.md): Selector Valve · faulted · Nov 19, 2025 · N572NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP CAUTION AFTER ROTATION. / REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ-900 FIM 32-51-50-810-801 AND AMM 32-32-10-000/400-801. OPS TEST GOOD AND LEAK TEST GOOD
- [SDR VNAA2025111811101](https://openairdocs.org/sdr/VNAA2025111811101.md): Warning Message · illuminated · Nov 16, 2025 · N572NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOPERATIVE CAUTION MSG 200 FT AFTER T/O. PERFORMED MIPM RESET FAULT EXTINGUISHED.
- [SDR VNAA2025041511105](https://openairdocs.org/sdr/VNAA2025041511105.md): Windshield · failed · Apr 14, 2025 · N572NN · Cndair CL6002D24 · Flight Compartment Windows
  > FO WINDSHIELD SHATTERED AT 25000FT. / REMOVED AND REPLACED THE RH WINDSHIELD IAW CRJ900 AMM 56-11-01-000/400-801-A01-PSA. OPS TEST GOOD. PRESSURIZATION TEST GOOD.
- [SDR VNAA20240425020](https://openairdocs.org/sdr/VNAA20240425020.md): Bushing · corroded · Mar 27, 2024 · N572NN · Bombdr CL6002D15 · Trailing Edge Flaps
  > CORROSION ON BORES OF LUGS (2EAS) AT HINGE NO.4 WAS FOUND AT LH WING TRAILING EDGE. BORES OF LUGS (2EAS) AT HINGE NO.4 WAS FOUND AT LH WING TRAILING EDGE WERE REPAIRED PER PER REO 690-57-51-345 REV. - -
- [SDR VNAA20240426005](https://openairdocs.org/sdr/VNAA20240426005.md): Floor Support · corroded · Mar 26, 2024 · N572NN · 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 RBL 4'', FS=319 AND RBL 4'' AT FUSELAGE FLOOR STRUCTURE. FLOOR SUPPORTS (4EAS) LOCATED BTW FS=280 TO FS=295 AND RBL17'' AND RBL 38'', FS=295 AND RBL 4'', FS=
- [SDR VNAA20240425012](https://openairdocs.org/sdr/VNAA20240425012.md): Angle · dented · Mar 26, 2024 · N572NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE LOWER SILL OF GALLEY SERVICE DOOR (FWD) SURROUND STRUCTURE. ANGLE LOWER SILL OF GALLEY SERVICE DOOR (FWD) SURROUND STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR VNAA20240425010](https://openairdocs.org/sdr/VNAA20240425010.md): Floor Support · corroded · Mar 26, 2024 · N572NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS (2EAS) LOCATED BTW FS=280 TO FS=295 AND LBL19'' AND LBL 37'' AT FUSELAGE FLOOR STRUCTURE. FLOOR SUPPORTS (2EAS) LOCATED BTW FS=280 TO FS=295 AND LBL19'' AND LBL 37'' AT FUSELAGE FLOOR STRUCTURE ARE OUT OFF LIMITS PER CRJ-900 SRM 53
- [SDR VNAA20240425009](https://openairdocs.org/sdr/VNAA20240425009.md): Hinge Fitting · excess play · Mar 26, 2024 · N572NN · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous Structure
  > FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103 REV. B
- [SDR VNAA20240426007](https://openairdocs.org/sdr/VNAA20240426007.md): Skin · nicked · Mar 25, 2024 · N572NN · Bombdr CL6002D15 · Trailing Edge Flaps
  > INITIAL INSPECTION: SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING. SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT LH WING WERE BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01, EVALUATED, BTW INBOARD F
- [SDR VNAA20240426006](https://openairdocs.org/sdr/VNAA20240426006.md): Seat Track · corroded · Mar 25, 2024 · N572NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS, LOCATED BTW FS=661+32 TO FS=693 AND LBL 9'' AND RBL 9''. FLOOR SEAT RAILS, LOCATED BTW FS=661+32 TO FS=693 AND LBL 9'' AND RBL 9'' WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-001-A02 AND SRM 53-41-49-101-001-001
- [SDR VNAA20240425018](https://openairdocs.org/sdr/VNAA20240425018.md): Canister · cracked · Mar 25, 2024 · N572NN · Bombdr CL6002D15 · 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 VNAA20240425017](https://openairdocs.org/sdr/VNAA20240425017.md): Canister · cracked · Mar 25, 2024 · N572NN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > CRACK IN CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. - -
- [SDR VNAA20240425015](https://openairdocs.org/sdr/VNAA20240425015.md): Seat Track · corroded · Mar 25, 2024 · N572NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAILS BTW FS379.00 TO FS581.00 (2EA), FS661+16 TO FS720.85 (2EA), FS744.15 TO FS761.85 (1EA) AND FS785.15 TO FS897.70 (3EA). IDE SEAT RAILS BTW FS379.00 TO FS581.00 (2EA), FS661+16 TO FS720.85 (2EA), FS744.15 TO FS761.85 (1EA) AND FS
- [SDR VNA2024F00006](https://openairdocs.org/sdr/VNA2024F00006.md): Seat Track · corroded · Mar 25, 2024 · N572NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAILS BTW FS379.00 TO FS581.00 (2EA), FS661+16 TO FS720.85 (2EA), FS744.15 TO FS761.85 (1EA) AND FS 785.15 TO FS 879.70(3EAS). SIDE SEAT RAILS BTW FS379.00 TO FS581.00 (2EA), FS661+16 TO FS720.85 (2EA), FS744.15 TO FS761.85 (1EA) A
- [SDR VNAA20240426004](https://openairdocs.org/sdr/VNAA20240426004.md): Angle · corroded · Mar 23, 2024 · N572NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > CORROSION ON ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE. FOR EXCESSIVE DAMAGE, ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE IT IS OUT OF LIMITS PER CRJ/900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER PER CRJ 900 SRM 51-41-02-001-001-A0
- [SDR VNAA20240425008](https://openairdocs.org/sdr/VNAA20240425008.md): Bracket · corroded · Mar 23, 2024 · N572NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (4EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS-MACHINED (2EAS) FS 517 AND FS 661 BTW STGR 27 TO 26 LH OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND NOT CORR
- [SDR VNAA20240425007](https://openairdocs.org/sdr/VNAA20240425007.md): Floorbeam · cracked · Mar 23, 2024 · N572NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1712 REV---
- [SDR VNAA20240425006](https://openairdocs.org/sdr/VNAA20240425006.md): Floorbeam · cracked · Mar 23, 2024 · N572NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOORBEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOORBEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1711 REV
- [SDR VNAA20240425005](https://openairdocs.org/sdr/VNAA20240425005.md): Intercostal · corroded · Mar 23, 2024 · N572NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT STGR 20RH BTW FS333.00 TO FS 349.00. INTERCOSTAL AT STGR 20RH BTW FS333.00 TO FS 349.00 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01.
- [SDR VNAA20240425004](https://openairdocs.org/sdr/VNAA20240425004.md): Angle · corroded · Mar 21, 2024 · N572NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE KICKPLATE AT PASSENGER DOOR SURROUND. REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR VNAA20240426009](https://openairdocs.org/sdr/VNAA20240426009.md): Skin · damaged · Mar 20, 2024 · N572NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > SEVERAL NICKS ON REAR FUSELAGE, BTW FS1000.00 TO FS1051.30 BTW STGR 27 TO STGR 24RH. SEVERAL NICKS ON REAR FUSELAGE, BTW FS1000.00 TO FS1051.30 BTW STGR 27 TO STGR 24RH WAS BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND EVALUATED,BTW 1000.00 TO FS1051.00
- [SDR VNAA20240426008](https://openairdocs.org/sdr/VNAA20240426008.md): Drag Angle · cracked · Mar 20, 2024 · N572NN · 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 (TRACE AT BL0.00). (SM). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (T
- [SDR VNAA20240426003](https://openairdocs.org/sdr/VNAA20240426003.md): Skin · worn · Mar 20, 2024 · N572NN · 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 WAS REPAIRED PER REO 690-57-21-458 REV - -.
- [SDR VNAA20240426002](https://openairdocs.org/sdr/VNAA20240426002.md): Skin · worn · Mar 20, 2024 · N572NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN.
- [SDR VNAA20240426001](https://openairdocs.org/sdr/VNAA20240426001.md): Skin · dented · Mar 20, 2024 · N572NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > DENT ON CANOPY SKIN BTW FS 241.60/FS 247.30 AND BL 0.00/ LBL 5.50. REF ( BTW STGR 2RH /STGR 2LH). NT ON CANOPY SKIN BTW FS 241.60/FS 247.30 AND BL 0.00/ LBL 5.50. REF ( BTW STGR 2RH /STGR 2LH) WAS REPAIRED PER REO 690-53-11-1721 REV -- AND REO 670-51-00-085
- [SDR VNAA202404250005](https://openairdocs.org/sdr/VNAA202404250005.md): Skin · dented · Mar 20, 2024 · N572NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > DENT ON TOP PANEL SKIN BTW FS 169.00/ FS202.75 AND BL0.00/LBL5.50. REPAIRED PER REO 690-53-11-1720 REV -- AND REO 670-51-00-085 REV - -
- [SDR VNAA20240425019](https://openairdocs.org/sdr/VNAA20240425019.md): Bushing · corroded · Feb 17, 2024 · N572NN · Bombdr CL6002D15 · Ailerons
  > WEAR ON BORES OF CENTER FITTING LUGS R1 AND R2 WAS FOUND AT RH AILERON. BORES OF CENTER FITTING LUGS R1 AND R2 WAS FOUND AT RH AILERON WERE REPAIRED PER PER REO 670-57-61-237 REV - - NOTES F
- [SDR VNAA20240425016](https://openairdocs.org/sdr/VNAA20240425016.md): Seat Track · corroded · Feb 5, 2024 · N572NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS LBL9 AND RBL9 BTW FS 847.00 TO FS 977.00 AT PASSENGER CABIN. FLOOR SEAT RAILS LBL9 AND RBL9 BTW FS 847.00 TO FS 977.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-001-A02 AND WERE REPLACED PER
- [SDR VNAA20240425013](https://openairdocs.org/sdr/VNAA20240425013.md): Seat Track · corroded · Feb 5, 2024 · N572NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS349.00 TO FS477,40 ON RBL9 (1EA) AND SEAT RAIL BTW FS379.00 TO FS485.00 ON LBL9 (1EA).. SEAT RAIL BTW FS349.00 TO FS477,40 ON RBL9 (1EA) AND SEAT RAIL BTW FS379.00 TO FS485.00 ON LBL9 (1EA). WERE EVALUATED OUT OF LIMITS PER CRJ90
- [SDR VNAA20240425011](https://openairdocs.org/sdr/VNAA20240425011.md): Seat Track · corroded · Feb 5, 2024 · N572NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: CORROSION ON FLOOR SEAT RAILS, LOCATED BTW FS=581 TO FS=661+32 AND LBL 9'' AND RBL 9''.
- [SDR VNAA20240425001](https://openairdocs.org/sdr/VNAA20240425001.md): Seat Track · corroded · Feb 5, 2024 · N572NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT TRACK LOCATED BTW FS=485 TO FS=581 AND LBL 9'' AND RBL 9''. FLOOR SEAT RAILS, WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202309010002](https://openairdocs.org/sdr/VNAA202309010002.md): Stringer · damaged · Sep 1, 2023 · N572NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF PREVIOUS REPAIRS, FOUND STGR13R JUST FWD OF FS265 TO HAVE 1EA ELONGATED HOLE. REPAIRED IAW CRJ 900 SRM 53-00-03-201-001-A02
- [SDR VNAA202309010001](https://openairdocs.org/sdr/VNAA202309010001.md): Skin · punctured · Sep 1, 2023 · N572NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > TUG IMPACT DAMAGE TO R/H SIDE OF NOSE SKIN FS 250 TO FS 265. REPAIRED IAW MHIRJ REO 690-53-11-1587 REV. – DATED 2023-08-16 AND MHIRJ REO 690-53-11-1591 REV. -- DATED 2023-08-25.
- [SDR VNAA202306231111](https://openairdocs.org/sdr/VNAA202306231111.md): Unknown · unknown · Jun 22, 2023 · N572NN · Cndair CL6002D24 · Air Distribution System
  > SMOKE SMELL MID CABIN AND AFT. OPS CHECKS PRODUCED NO NOTICEABLE SMELLS IAW CRJ900 FIM M21-22-00-810-806-A01 CYCLED LEFT AND RIGHT PACK THROUGH VARIOUS TEMPS AND BLEED SOURCES ALL SYSTEMS NORMAL
- [SDR VNAA202304201111](https://openairdocs.org/sdr/VNAA202304201111.md): Unknown · unknown · Apr 18, 2023 · N572NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP MSG IN FLIGHT WHEN MLG IN TRANSIT. PERFORMED REPACK OF NLG STRUT IAW AMM 32-21-20-000/400-801 USING ALTERNATE TORQUE PROCEDURE AMM 05-51-30-420-801 AT 110 INCH POUNDS. OPS AND LEAK CHECK GOOD. PERFORMED SUCCESSFUL OPS CHECK OF NOSEWHEEL STEERING
- [SDR VNAA202303110006](https://openairdocs.org/sdr/VNAA202303110006.md): Drag Angle · cracked · Mar 11, 2023 · N572NN · Bombdr CL6002D15 · Doors
  > PAX DOOR AFT DRAG ANGLE IS CRACKED:: REACOMPLISHED DRAG ANGLE REPAIR IAW CRJ-900 SRM 52-11-04-201
- [SDR VNAA202303110005](https://openairdocs.org/sdr/VNAA202303110005.md): Step · cracked · Mar 11, 2023 · N572NN · Bombdr CL6002D15 · Doors
  > PAX DOOR TOP STEP PANEL HAS 1EA CRACK ON THE AFT SIDE: REPAIRED DAMAGE IAW CRJ-900 SRM 52-11-04-201-006-A01
- [SDR VNAA202303110004](https://openairdocs.org/sdr/VNAA202303110004.md): Skin · dented · Mar 11, 2023 · N572NN · Bombdr CL6002D15 · Fuselage Structure (General)
  > L/H EXTERNAL FUSELAGE SKIN HAS MULTIPLE DENTS BETWEEN FS 193.00 AND FS 202.75 AFT OF TRU BAY DOOR. REMOVED AND REPLACED THE LH EXTERNAL FUSELAGE SKIN BETWEEN FS 193.00 AND FS 202.75 AFT OF TRU BAY DOOR IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A
- [SDR VNAA202201121111](https://openairdocs.org/sdr/VNAA202201121111.md): Controller · malfunctioned · Jan 8, 2022 · N572NN · Cndair CL6002D24 · Cabin Pressure Controller
  > DURING THE FLIGHT THE CREW RECEIVED A CABIN PRESSURE WARNING MESSAGE AND SHORTLY AFTER THE FAS REPORTED THE SMELL OF SMOKE IN THE MAIN CABIN. THE FLIGHT DIVERTED TO IAD AND STILL HAD A STRONG SMOKE SMELL IN THE COCKPIT AND MAIN CABIN AFTER LANDING. THE PAX WER
- [SDR VNAA202112051111](https://openairdocs.org/sdr/VNAA202112051111.md): A/C Pack · smoke · Dec 1, 2021 · N572NN · Cndair CL6002D24 · Cabin Cooling System
  > L PACK AUTOFAIL CAUTION MSG ACCOMPANIED BY L PACK FAULT STATUS MSG AND SMOKE IN CABIN. FOUND LH PACK TO SMOKE DEFERRED COCKPIT TEMP CONTROL SYS. REMOVED AND REPLACED LH ACM IAW CRJ 900 AMM 21-51-08-000/400-801. OPS CHECK GOOD. LEAK CHECK GOOD
- [SDR VNAA202102131112](https://openairdocs.org/sdr/VNAA202102131112.md): Skin · dented · Feb 10, 2021 · N572NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DURING ROUTINE OVERNIGHT MAINTENANCE IN PENSACOLA, FL (PNS), MAINTENANCE NOTED THAT THERE IS A DENT COMMON TO THE FUSELAGE SKIN BETWEEN FS 245, AND BETWEEN STRINGERS 22L AND 23L. THE DENT MEASURES.780Ï¿½ LONG X.330Ï¿½ WIDE X.035Ï¿½ DEEP. ITÏ¿½S WIDTH TO DEP
- [SDR VNAA202007139994](https://openairdocs.org/sdr/VNAA202007139994.md): Angle · corroded · Jul 13, 2020 · N572NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > FS 280 J-ANGLE LOCATED AT FLIGHT DECK ENTRANCE IS CORRODED AT 2 PLACES ON UPPER SURFACE. REMOVED FS 280 J-ANGLE AND INSTALLED NEW SERVICEABLE FS 280 J-ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR VNAA202007139992](https://openairdocs.org/sdr/VNAA202007139992.md): Angle · cracked · Jul 13, 2020 · N572NN · Bombdr CL6002D15 · Empennage Structure
  > RIGHT VERTICAL STAB AFT DRAG ANGLE APPEARS CRACKED. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE R/H VERTICAL STAB AFT DRAG ANGLE IAW CRJ900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.
- [SDR VNAA202007139991](https://openairdocs.org/sdr/VNAA202007139991.md): Drag Angle · cracked · Jul 13, 2020 · N572NN · Bombdr CL6002D15 · Vertical Stabilizer
  > LEFT VERTICAL STAB AFT DRAG ANGLE APPEARS CRACKED. REMOVED, LOCATED AND DRILLED AND INSTALLED NEW SERVICEABLE L/H V-STAB AFT DRAG ANGLE IAW CRJ900 SRM 51-42-13-001-001-A01

Next page: https://openairdocs.org/aircraft/N572NN/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 = 'N572NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N572NN/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.