# Service difficulty reports: N573NN

A list on [N573NN](https://openairdocs.org/aircraft/N573NN.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 · 65 reports

- [SDR VNAA2025090311101](https://openairdocs.org/sdr/VNAA2025090311101.md): Motor · failed · Sep 1, 2025 · N573NN · Cndair CL6002D24 · Hydraulic Pump (Electric/Engine), Main
  > HYD 3 LO PRESS, HYD PUMP 3A CAUTION. IB GNS SPLRS. ON LANDING R REV INOP CAUTION. / REMOVED AND REPLACED HYD SYS 3A ACMP IAW CRJ 900 AMM 29-12-03-000/400-801. OPS CHECK AND LEAK CHECK GOOD.
- [SDR VNAA2024120811102](https://openairdocs.org/sdr/VNAA2024120811102.md): Window · unserviceable · Dec 5, 2024 · N573NN · Cndair CL6002D24 · Flight Compartment Windows
  > RIGHT WINDOW ARCING IN FLIGHT MULTIPLE TIMES. RIGHT WINDOW CAUTION ILLUMINATED. / REMOVED AND REPLACED RH SIDE WINDOW IAW CRJ 900 AMM 56-12-01-000/400-801-A01-PSA. LEAK CHECK GOOD. WINDOW TEMP CONTROLLER OPS CHECK GOOD IAW CRJ 900 AMM 30-41-06-710-801.
- [SDR VNAA2024040911103](https://openairdocs.org/sdr/VNAA2024040911103.md): Coffeemaker · smoke · Apr 8, 2024 · N573NN · Cndair CL6002D24 · Buffet/Galleys
  > LH COFFEE MAKER SMOKING / TROUBLESHOT IAW CRJ 900 FIM 21-22-00-810-806-A01. UPON OBSERVATION NO SMOKE OR SMELL WAS FOUND. LH COFFEE MAKER NEEDS REPLACED. REMOVED AND REPLACED LH COFFEE MAKER IAW CRJ 900 AMM 25-32-06-000/400-801-A08-PSA. OPS TEST GOOD.
- [SDR VNAA202403230020](https://openairdocs.org/sdr/VNAA202403230020.md): Bushing · corroded · Feb 17, 2024 · N573NN · Bombdr CL6002D15 · Ailerons
  > CORROSION ON BORES OF CENTER FITTING LUGS R1,R2,R5, R6 AND UPPER BORE ON OUTBD FITTING AT RH AILERON. BORES OF CENTER FITTING LUGS R1,R2,R5, R6 AND UPPER BORE ON OUTBD FITTING AT RH AILERON WERE REPAIRED PER PER REO 670-57-61-237 REV - -
- [SDR VNAA202403230019](https://openairdocs.org/sdr/VNAA202403230019.md): Bushing · corroded · Feb 17, 2024 · N573NN · Bombdr CL6002D15 · Ailerons
  > CORROSION ON BORES OF CENTER FITTING LUGS L1, L3, L5 AND L6 WAS FOUND AT LH AILERON. CORROSION ON BORES OF CENTER FITTING LUGS L1, L3, L5 AND L6 AT LH AILERON WERE REPAIRED PER PER REO 670-57-61-237 REV - -
- [SDR VNAA202403230011](https://openairdocs.org/sdr/VNAA202403230011.md): Bushing · corroded · Feb 17, 2024 · N573NN · Bombdr CL6002D15 · Ailerons
  > INBD BORE OF FITTING #1 WAS FOUND ON LH WING TRAILING EDGE. INBD BORE OF FITTING #1 WAS FOUND ON LH WING TRAILING EDGE WAS REPAIRED PER ETI-900-23-010 REV. ORIG. & REO 690-57-51-334 REV. --
- [SDR VNAA202403230018](https://openairdocs.org/sdr/VNAA202403230018.md): Canister · cracked · Feb 16, 2024 · N573NN · Bombdr CL6002D15 · Fuel Storage
  > DURING INSPECTION OF THE TASK CARD 600-08E2-JIC, IT WAS DETECTED 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:REPAIR PER REO 670-57-42-577. REV. - -
- [SDR VNAA202403230017](https://openairdocs.org/sdr/VNAA202403230017.md): Hinge Fitting · nicked · Feb 16, 2024 · N573NN · Bombdr CL6002D15 · Ailerons
  > NICK ON AILERON HINGE FITTING 3 (INBD LUG) AT RH WING REAR SPAR. NICK ON AILERON HINGE FITTING 3 (INBD LUG) AT RH WING REAR SPAR WAS REPAIRED PER REO 690-57-51-331 REV. - -
- [SDR VNAA202403230029](https://openairdocs.org/sdr/VNAA202403230029.md): Seat Track · corroded · Feb 15, 2024 · N573NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS BTW FS=581 TO FS=661+32 AND LBL 9'' / RBL 9''. FLOOR SEAT RAILS BTW FS=581 TO FS=661+32 AND LBL 9'' / RBL 9'' ARE OUT OFF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 NOTE 1 AND FLOOR SEAT RAILS BTW FS=581 TO FS=661+32 AND LBL
- [SDR VNAA202403230028](https://openairdocs.org/sdr/VNAA202403230028.md): Seat Track · corroded · Feb 15, 2024 · N573NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS BTW FS=485 TO FS=581 LBL 9'' / RBL 9''. FLOOR SEAT RAILS BTW FS=485 TO FS=581 LBL 9'' / RBL 9''. WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202403230027](https://openairdocs.org/sdr/VNAA202403230027.md): Seat Track · corroded · Feb 15, 2024 · N573NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: CORROSION ON FLOOR SEAT RAILS BTW FS=349 TO FS=485 LBL 9'' / RBL 9''. FLOOR SEAT RAILS BTW FS=349 TO FS=485 LBL 9'' / RBL 9''. WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12
- [SDR VNAA202403230025](https://openairdocs.org/sdr/VNAA202403230025.md): Plate · corroded · Feb 15, 2024 · N573NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > DISCREPANCY: CORROSION ON KICK PLATE AND MID CAP AT PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON KICK PLATE AND MID CAP AT PASSENGER DOOR SURROUND STRUCTURE WERE REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01,FOR EXCESSIVE DAMAGE MID CAP OUT OFF LIMITS PER
- [SDR VNAA202403230021](https://openairdocs.org/sdr/VNAA202403230021.md): Seat Track · corroded · Feb 15, 2024 · N573NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS BTW FS=661+32 TO FS=677 AND LBL 9'' / RBL 9' CORROSION ON FLOOR SEAT RAILS BTW FS=661+32 TO FS=677 AND LBL 9'' / RBL 9'' WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-
- [SDR VNAA202403230015](https://openairdocs.org/sdr/VNAA202403230015.md): Skin · dented · Feb 15, 2024 · N573NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING. DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING WERE REPAIRED PER REO 690-53-61-1348REV --
- [SDR VNAA202403230014](https://openairdocs.org/sdr/VNAA202403230014.md): Seat Track · corroded · Feb 15, 2024 · N573NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS BTW FS=785 TO FS=977, STGR 15 LH AND RH. SIDE SEAT RAIL STGR 15L BTW FS785.15 TO FS969; STGR 15R BTW FS785.15 TO FS927 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRM 53-51-49-101-001-A02 AND WER
- [SDR VNAA202403230013](https://openairdocs.org/sdr/VNAA202403230013.md): Seat Track · corroded · Feb 15, 2024 · N573NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS, FS=677 TO FS=761, STGR15, LH AND RH SIDE SEAT RAILS, FS=677 TO FS=761, STGR15, LH AND RH WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12).
- [SDR VNAA202403230012](https://openairdocs.org/sdr/VNAA202403230012.md): Seat Track · corroded · Feb 15, 2024 · N573NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS BTW FS=847+16 TO FS=977 AND LBL 9''. FLOOR SEAT RAILS BTW FS=847+16 TO FS=977 AND LBL 9''. WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNA2024F00004](https://openairdocs.org/sdr/VNA2024F00004.md): Drag Angle · cracked · Feb 15, 2024 · N573NN · Bombdr CL6002D15 · Vertical Stabilizer
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE
- [SDR VNA2024F00003](https://openairdocs.org/sdr/VNA2024F00003.md): Drag Angle · cracked · Feb 15, 2024 · N573NN · 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). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT
- [SDR VNA2024F00001](https://openairdocs.org/sdr/VNA2024F00001.md): Floor Support · cracked · Feb 15, 2024 · N573NN · Bombdr CL6002D15 · Fuselage Structure (General)
  > CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-
- [SDR VNAA202403230026](https://openairdocs.org/sdr/VNAA202403230026.md): Striker · corroded · Feb 14, 2024 · N573NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > SEVERAL CORROSIONS ON SEAL STRIKER (R1) LOCATED BTW FS=310.00 TO FS=349.00 AND RBL 43" AT FUSELAGE FLOOR STRUCTURE SERVICE DOOR. SEAL STRIKER (ANGLE-MOUNTING)(R1) LOCATED BTW FS=310.00 TO FS=349.00 AND RBL 43" AT FUSELAGE FLOOR STRUCTURE SERVICE DOOR WAS REPL
- [SDR VNAA202403230024](https://openairdocs.org/sdr/VNAA202403230024.md): Skin · damaged · Feb 14, 2024 · N573NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > PERM REPAIR BEFORE 20,337.49 FH - LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN FS501.00 - FS661+16 & STR26L - STR23R THIS TEMPORARY DISPOSITION IS VALID FOR 600 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO AT REV - -. PERM REPAIR BEFORE 20,33
- [SDR VNAA202403230023](https://openairdocs.org/sdr/VNAA202403230023.md): Striker · damaged · Feb 14, 2024 · N573NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > REPAIR TO PAX DOOR SEAL STRIKER PERMANENT REPAIR REQD TO PASSENGER DOOR SEAL STRIKER. SEE W.O. AND REO 670-53 -22-001 FOR DETAILS. PAX DOOR SEAL STRIKER WAS REPAIRED PER REO 670-53-22-001. REV. J. REPAIR (TYPE IV)
- [SDR VNAA202403230022](https://openairdocs.org/sdr/VNAA202403230022.md): Bracket · corroded · Feb 14, 2024 · N573NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (05 EAS) OF INTERNAL STRUCTURE AT FWD & CTR CARGO COMPARTMENT. BRACKETS, MACHINED (05 EAS) OF INTERNAL STRUCTURE AT FWD & CTR CARGO COMPARTMENT WERE REPLACED PERCRJ900 SRM 51-42-22-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001
- [SDR VNAA202403230010](https://openairdocs.org/sdr/VNAA202403230010.md): Rib · cracked · Feb 14, 2024 · N573NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > AFTER ACCESS PANEL 521BL REMOVAL, CRACK ON MACHINED RIB LEADING EDGE SS 57.16 AT LEFT WING. (SM). MACHINED RIB LEADING EDGE SS 57.16 AT LEFT WING. (SM) WAS REPAIRED PER REO 690-57-41-240. REV. --
- [SDR VNAA202403230009](https://openairdocs.org/sdr/VNAA202403230009.md): Intercostal · corroded · Feb 13, 2024 · N573NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW STGR 27LH TO STGR 26LH, BTW FS 349.00 TO FS 364.00. INTERCOSTAL BTW STGR 27LH TO STGR 26LH, BTW FS 349.00 TO FS 364.00 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.
- [SDR VNAA202403230008](https://openairdocs.org/sdr/VNAA202403230008.md): Support Fitting · corroded · Feb 13, 2024 · N573NN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > CORROSION ON JACK FITTING SUPPORTS LH/RH AT FWD JACK FITTING. CORROSION ON JACK FITTING SUPPORTS LH AND RH AT FWD JACK FITTING WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 WERE MEASURED AND FOUND SUPPORT LH WITHIN LIMITS AND SUPPORT RH OUT OFF LIMITS PER
- [SDR VNAA202403230007](https://openairdocs.org/sdr/VNAA202403230007.md): Web · cracked · Feb 13, 2024 · N573NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > DISCREPANCY: INITIAL INSPECTION': CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. (SM) ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. (SM) WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.
- [SDR VNAA202403230006](https://openairdocs.org/sdr/VNAA202403230006.md): Arm · worn · Feb 12, 2024 · N573NN · Bombdr CL6002D15 · Cargo/Baggage Doors
  > WEAR ON FWD AND AFT COUNTERBALANCE ARM AT FWD CARGO COMPARTMENT DOOR AND WEAR ON FWD COUNTERBALANCE ARM OF CTR CARGO COMPARTMENT DOOR. WEAR ON FWD AND AFT COUNTERBALANCE ARM AT FWD CARGO COMPARTMENT DOOR AND WEAR ON FWD COUNTERBALANCE ARM OF CTR CARGO COMPAR
- [SDR VNAA202403230005](https://openairdocs.org/sdr/VNAA202403230005.md): Pad · damaged · Feb 11, 2024 · N573NN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > DURING REPAIR D JACKING PAD HELICOIL INSERT LHS IN REF. REO 670-57-22-004 REV.F, TOOL MARK WERE NOTED. DURING REPAIR D JACKING PAD HELICOIL INSERT LHS WAS DETECTED DAMAGE,TOOL MARK WERE NOTED. REPAIR PREVIOUS. THEREFORE JACKING FITTING ASSY WAS REPLACED
- [SDR VNA2024F00002](https://openairdocs.org/sdr/VNA2024F00002.md): Rib · cracked · Feb 11, 2024 · N573NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > AFTER ACCESS PANEL 621BR REMOVAL, CRACK ON MACHINED RIB LEADING EDGE SS 57.16 AT RIGHT WING. CRACK ON MACHINED RIB LEADING EDGE SS 57.16 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240. REV. - -
- [SDR VNAA202403230016](https://openairdocs.org/sdr/VNAA202403230016.md): Skin · dented · Feb 5, 2024 · N573NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING. DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING WERE REPAIRED PER REO 690-53-61-1349 REV --
- [SDR VNAA2023111411102](https://openairdocs.org/sdr/VNAA2023111411102.md): Unknown · unknown · Nov 12, 2023 · N573NN · Cndair CL6002D24 · Door Warning System
  > SERVICE DOOR CAUTION MSG IN FLIGHT / INTERROGATED MDC AND FOUND B1 CODE 007792. TROUBLESHOT IAW CRJ 900 FIM 52-70-06-810-811-A02. SUSPECTED PROXIMITY SENSOR PX38 OUT OF RIG. ADJUSTED GALLEY SERVICE DOOR SENSOR PX38 IAW CRJ 900 52-70-06-820-802-A01. OPS CHECK G
- [SDR V0XD20230926001](https://openairdocs.org/sdr/V0XD20230926001.md): Skin · scratched · Sep 26, 2023 · N573NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT RS 333.00 TO FS 477.0 BETWEEN STGR 24R AND STGR 25R IS SCRATCHED. CORRECTIVE ACTION: CLEANED AREA, VERIFIED BLENDED AREA MEASUREMENTS PERFORMED NDT IAW OLIVER WYMAN/CAVOK EA 23-C9-53-0689 REV. C DATED 9/25/2023. DTE TO BE ACCOMPLISHED WITHIN 1
- [SDR VNAA202207051111](https://openairdocs.org/sdr/VNAA202207051111.md): Smoke Detector · unserviceable · Jul 3, 2022 · N573NN · Cndair CL6002D24 · Smoke Detection
  > SMOKE AFT LAV. REMOVED AND REPLACED SMOKE DETECTOR IAW CRJ 900 AMM 26-16-01-000/400-801-A01-PSA OPS CHECK GOOD. PERFORMED OPS TEST OF THE AIR CONDITIONING DISTRIBUTION SYSTEM IAW CRJ 900 AMM 21-51-00-710-801. OPS CHECK GOOD. NO SMOKE OR ODORS DETECTED.
- [SDR VNAA202111231111](https://openairdocs.org/sdr/VNAA202111231111.md): Control Unit · unserviceable · Nov 20, 2021 · N573NN · Cndair CL6002D24 · Stabilizer Actuator
  > ENROUTE TO CLT THE CREW RECEIVED A STAB TRIM/MACH TRIM FAIL MESSAGES. THE CREW RAN THE QRH AND THE RESET WAS UNSUCCESSFUL. THEY DECLARED EMERGENCY AND WERE CLEARED DIRECT TO CLT. THEY LANDED AND TAXIED TO THE GATE WITHOUT FURTHER ISSUE. NO FURTHER INFORMATION.
- [SDR VNAA202111071111](https://openairdocs.org/sdr/VNAA202111071111.md): Reservoir · malfunctioned · Nov 4, 2021 · N573NN · Cndair CL6002D24 · Hydraulic Reservoir, Main
  > ON DEPARTURE, #3 HYD SYSTEM CAUTION DURING GEAR RETRACTION. THEY DECLARED AN EMERGENCY, RETURNED TO CLT AND LANDED WITHOUT ISSUES IN CLT. THEY WERE NOT OVERWEIGHT ON LANDING. RTF-UPON SELECTED GEAR UP AFTER ROTATION HYD PUMP 3A AMBER CAS. FOLLOWED BY INBD GRND
- [SDR VNAA202109101111](https://openairdocs.org/sdr/VNAA202109101111.md): Power Unit · defective · Sep 9, 2021 · N573NN · Cndair CL6002D24 · Electrical Power System
  > BURNING ELECTRICAL SMELL IN FLIGHT DECK WHILE CONNECTED TO GROUND POWER AND BATTERY MASTER ON. FOUND GOUND POWER UNIT TO BE DEFECTIVE. POWERED UP APU IAW 49-10-00-866-801-A02. NO SMELL OF BURNING ELECTRICAL AC OK FOR SERVICE
- [SDR VNAA202105181111](https://openairdocs.org/sdr/VNAA202105181111.md): Acm · smoke · May 14, 2021 · N573NN · Cndair CL6002D24 · Cabin Cooling System
  > WHILE ON TAXI OUT TO RUNWAY, THE AC PACKS OVERHEATED AND THEY STARTED TO PUSH SMOKE INTO THE CABIN. CREW TURNED THE PACKS OFF AND THE CABIN STARTED TO CLEAR OUT. THEY RETURNED TO GATE AND MAINTENANCE HAS BEEN CALLED. PERFORMED OPS CHECK OF THE AIR CONDITIONING
- [SDR VNAA202011081112](https://openairdocs.org/sdr/VNAA202011081112.md): Transducer · unknown · Nov 5, 2020 · N573NN · Cndair CL6002D24 · Landing Gear Brake System
  > REJECTED TAKE OFF FOR AN ANTI SKID AMBER CAUTION MESSAGE RUNWAY 10 AT 70 KNOTS. NO EMERGENCY. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. R & R WHEEL SPEED TRANSDUCER.
- [SDR VNAA2020080911102](https://openairdocs.org/sdr/VNAA2020080911102.md): Nut · loose · Aug 6, 2020 · N573NN · Cndair CL6002D24 · Wheel/Ski/Float
  > FLIGHT 5633, ON TAKEOFF ABNOMAL WHEEL VIBRATIONS AND UNUSUAL STEERING NEAR ROTATION. DECLARED EMERGENCY AS A PRECAUTION AND WAS ABLE TO LAND SAFELY. TORQUED NLG WHEEL NUTS IAW AMM 32-42-01-400-801.
- [SDR VNAA2020060299911](https://openairdocs.org/sdr/VNAA2020060299911.md): Web · corroded · Jun 2, 2020 · N573NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RIGHT WEB BEHIND FS 280 BULKHEAD, FOUND TO BE CORRODED DURING ACCOMPLISHMENT OF ACCESS FOR 280 STRUCTURAL REPAIR. WEB REPAIRED.
- [SDR VNAA2020060299910](https://openairdocs.org/sdr/VNAA2020060299910.md): Crossbeam · corroded · Jun 2, 2020 · N573NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 RT CROSSBEAM FOUND TO BE CORRODED BETWEEN RBL12 AND BL0. CROSSBEAM REPLACED.
- [SDR VNAA202006029999](https://openairdocs.org/sdr/VNAA202006029999.md): Crossbeam · corroded · Jun 2, 2020 · N573NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 LT CROSSBEAM FOUND TO BE CORRODED BETWEEN LBL 12 AND BL 0. CROSSBEAM REPLACED.
- [SDR VNAA202006029998](https://openairdocs.org/sdr/VNAA202006029998.md): Support Angle · corroded · Jun 2, 2020 · N573NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 FWD FLOOR SUPPORT ANGLE BETWEEN LBL 12 AND RBL 12 IS CORRODED. REPLACED ANGLE.
- [SDR VNAA202006029997](https://openairdocs.org/sdr/VNAA202006029997.md): Stringer · corroded · Jun 2, 2020 · N573NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 26R IS CORRODED BETWEEN FS 319 AND FS 333. REPLACED STRINGER.
- [SDR VNAA202006029996](https://openairdocs.org/sdr/VNAA202006029996.md): Frame · corroded · Jun 2, 2020 · N573NN · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 310 IS CORRODED BETWEEN STR 26L AND STR 26R.
- [SDR VNAA202006029995](https://openairdocs.org/sdr/VNAA202006029995.md): Joint · corroded · Jun 2, 2020 · N573NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 CIRCUMVENTION JOINT IS CORRODED BETWEEN STGR 25L AND 25R.
- [SDR VNAA202006029994](https://openairdocs.org/sdr/VNAA202006029994.md): Intercostal · corroded · Jun 2, 2020 · N573NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ATTACHMENT ANGLE FWD OF FS 364, RBL 26 IS CORRODED. REMOVED CORRODED INTERCOSTAL AT STR 26R. REPLACED INTERCOSTAL.
- [SDR VNAA202006029993](https://openairdocs.org/sdr/VNAA202006029993.md): Stringer · corroded · Jun 2, 2020 · N573NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R IS CORRODED FWD OF FS 364. REPLACED STRINGER.

Next page: https://openairdocs.org/aircraft/N573NN/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 = 'N573NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N573NN/reports

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