# Service difficulty reports: N569NN

A list on [N569NN](https://openairdocs.org/aircraft/N569NN.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR VNAA2026030313402](https://openairdocs.org/sdr/VNAA2026030313402.md): Acm · smoke · Mar 1, 2026 · N569NN · Cndair CL6002D24 · Cabin Cooling System
  > SMOKE IN CABIN, MAINLY IN BACK OF CABIN. DENSE SMOKE IN THE TOP. REMOVED AND REPLACED RH PACK ACM IAW AMM 21-51-08-000/400-801-A01. INSTALLATION COMPLETED UP TO CLOSE OUT. PERFORMED OPS TEST AND LEAK TEST OF THE R PACK IAW AMM 21-51-00-710-801-A01 AND AMM 21-
- [SDR VNAA2025082211102](https://openairdocs.org/sdr/VNAA2025082211102.md): Smoke Detector · false activation · Aug 21, 2025 · N569NN · Cndair CL6002D24 · Smoke Detection
  > UPON REACHING CRUISE ALTITUDE SMOKE ALARM WENT OFF AND CREW RAN QRH. PERFORMED OPERATIONAL TEST OF FWD LAVATORY SMOKE DETECTOR IAW AMM 26-16-00-710-802-A01-PSA. OPS TEST GOOD.
- [SDR VNAA2025060911101](https://openairdocs.org/sdr/VNAA2025060911101.md): Start Valve · inoperative · Jun 6, 2025 · N569NN · Cndair CL6002D24 · Engine Start Valves/Controls
  > LEFT ENG START VALVE OPENED IN FLT. EMERGENCY DECLARED. / REMOVE AND REPLACED RELAYS K23,K25,AND K31 OF JB11-PCB4 IAW CRJ 900 AMM 20-42-00-960-801-A03. REMOVED AND REINSTALLED JB1A IAW CRJ 900 AMM 24-06-09-000/400-801. PERFORMED OPERATIONAL CHECKS OF JB11 IAW
- [SDR VNAA2024080511101](https://openairdocs.org/sdr/VNAA2024080511101.md): Sensor · erratic · Aug 1, 2024 · N569NN · Cndair CL6002D24 · Landing Gear Brake System
  > BTMS RHIB INDICATION 20 AND SPARADIC IN FLIGHT / REMOVED AND REPLACED RHIB BRAKE TEMP SENSOR IAW CRJ 900 AMM 32-46-01-000/400-801-A01-PSA. OPS TEST GOOD.
- [SDR VNAA2024071911101](https://openairdocs.org/sdr/VNAA2024071911101.md): Windshield · arced · Jul 18, 2024 · N569NN · Cndair CL6002D24 · Flight Compartment Windows
  > L WINDSHIELD ARCING IN FLIGHT / REMOVED AND REPLACED THE LH WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA.OPERATIONAL TEST PERFORMED IAW CRJ 900 AMM 30-41-06-710-801 AND AMM 21-31-00-910-801.OPS.TEST GOOD AT THIS TIME.
- [SDR VNAA2024053111101](https://openairdocs.org/sdr/VNAA2024053111101.md): Blade · unserviceable · May 30, 2024 · N569NN · Cndair CL6002D24 · Turbine Engine Air Inlet Section
  > LEFT ENGINE HIGH VIBES ON TAKEOFF. 2.0 MAX. COULDNT ADVANCE THRUST ABOVE IDLE WITHOUIT HIGH VIBES RETURN TO FIELD / REMOVED AND REPLACED FAN BLADE PINS FOR LH ENG IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA. OPS CHECK GOOD
- [SDR VNAA202403070006](https://openairdocs.org/sdr/VNAA202403070006.md): Doubler · corroded · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage Main, Structure
  > F.S. 280.00 L/H WEB DOUBLER IS CORRODED ON THE END AT COCKPIT ENTRANCE. REMOVED SPLICE PLATE AND CUT WEB IAW CRJ-900-SRM-53-11-10-201-004-A01 STEPS 1 AND 2, FABRICATED AND INSTALLED REPAIR PARTS FOR LH WEB REPAIR IAW CRJ-900-SRM-53-11-10-201-004-A01 CC6
- [SDR VNAA202403070016](https://openairdocs.org/sdr/VNAA202403070016.md): Seat Track · corroded · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > 132686 DISCREPANCY: SEAT TRACK AT LBL 27 IS CORRODED BETWEEN FS 927 AND FS 985. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK BETWEEN FS 927 AND FS 985 AT LBL27 IAW CRJ 900 AMM 53-00-49-400-801-A12. 20275-288-0-0A
- [SDR VNAA202403070015](https://openairdocs.org/sdr/VNAA202403070015.md): Angle · corroded · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL ANGLE IS CORRODED. REMOVED AND REPLACED MID CAP ANGLE I.A.W. CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR VNAA202403070014](https://openairdocs.org/sdr/VNAA202403070014.md): Frame · corroded · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 319.70 FRAME IS CORRODED BETWEEN STGR 25L AND STGR 27. REPAIRED FS 319.70 FRAME IAW CRJ-900 SRM 53-00-06-201-001-A03 SH670-31355-1S
- [SDR VNAA202403070013](https://openairdocs.org/sdr/VNAA202403070013.md): Drag Angle · cracked · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE IS CRACKED AT DOOR MOTOR ASSIST PULLEY LOCATION. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE AFT DRAG ANGLE P# 601R31772-5S IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA202403070012](https://openairdocs.org/sdr/VNAA202403070012.md): Floor Skin · corroded · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage Floor Panel
  > THE FWD-MOST MOUNTING AREA ON THE FLOOR IS SEVERELY CORRODED/DAMAGE AND REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE FITTING P/N: CDSP2019-7C-760 AT GALLEY FWD-MOST MOUNTING AREA IAW CRJ900 SRM 51-41-02-001-001-A01. CDSP2019-7C-760
- [SDR VNAA202403070011](https://openairdocs.org/sdr/VNAA202403070011.md): Seat Track · corroded · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT AT RBL9 BETWEEN F.S.847+16 TO F.S.985 IS GOUGED AND CORRODED.. REMOVED SEAT TRACK SEGMENT AT RBL9 BETWEEN F.S.847+16 TO F.S.985 IAW CRJ900 AMM53-00-49-000-801 (CONFIG A12) INSTALLED NEW SERVICEABLE SEAT TRACK SEGMENT AT RBL9 BETWEEN F.S.84
- [SDR VNAA202403070009](https://openairdocs.org/sdr/VNAA202403070009.md): Angle · corroded · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > HN00134783 DISCREPANCY: AFTER REMOVAL OF F.S 280 J ANGLE. LH FLOOR BEAM FOUND TO BE CORRODED CORRECTIVE ACTION: REMOVED AND INSTALLED NEW BEAM P/N CC670-34094-1 IAW CRJ-900-SRM-51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01 CC670-34
- [SDR VNAA202403070010](https://openairdocs.org/sdr/VNAA202403070010.md): Rib · cracked · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Leading Edge Devices
  > FIXED L/E CLOSING RIB AT SS 446.86 IS CRACKED. REMOVED AND REPLACED FIXED L/E CLOSING RIB AT SS 446.86 IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND MHIRJ REO 690-57-41-409 REV-- DATED 2024-01-16. CC670-12529-4
- [SDR VNAA202403070008](https://openairdocs.org/sdr/VNAA202403070008.md): Floorbeam · cracked · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > F.S. 280.00 FLOORBEAM AT RBL 9.00 OUTBOARD SIDE IS CRACKED. REPLACED R/H F.S.280 FLOOR BEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01 CC670-34094-2
- [SDR VNAA202403070007](https://openairdocs.org/sdr/VNAA202403070007.md): Doubler · corroded · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > F.S. 280.00 L/H WEB DOUBLER IS CORRODED ON THE END AT COCKPIT ENTRANCE. REMOVED SPLICE PLATE AND CUT WEB IAW CRJ-900-SRM-53-11-10-201-004-A01 STEPS 1 AND 2, FABRICATED AND INSTALLED REPAIR PARTS FOR LH WEB REPAIR IAW CRJ-900-SRM-53-11-10-201-004-A01 CC6
- [SDR VNAA202403070005](https://openairdocs.org/sdr/VNAA202403070005.md): Angle · corroded · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > F.S. 280.00, FORWARD "J" ANGLE IS HEAVILY CORRODED. UPON REMOVAL OF CHANNEL, FORWARD FACE OF F.S. 280.00 CROSSBEAM COVERED BY CHANNEL WILL NEED EVALUATED FOR CORROSION. REMOVED F.S 280 'J' ANGLE CC670-34095-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21
- [SDR VNAA202403070004](https://openairdocs.org/sdr/VNAA202403070004.md): Angle · cracked · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage Main, Structure
  > HN00134375 DISCREPANCY: R/H COCKPIT SIDEPOST, LOWER AFT CLIP IS CRACKED IN RADIUS. INSTALLED NEW SERVICEABLE RH COCKPIT LOWER AFT FITTING PN/ GC212-0045-4S IAW CRJ900 SRM 51-42-21-001-001-A01 GC212-0045-4
- [SDR VNAA202403070003](https://openairdocs.org/sdr/VNAA202403070003.md): Skin · corroded · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INNER SKIN FOUND CORRODED IN MULTIPLE AREAS. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR INNER SKIN P/N:601R318024-15 IAW CRJ900 SRM 51-40-11-001-001-A01. REFERENCE JOB CARD HN00133323 FOR INSTALL.
- [SDR VNAA202403070002](https://openairdocs.org/sdr/VNAA202403070002.md): Slat Track · cracked · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-3 IS CHAFED. CHAFE IS APPROX 0.250 LONG, 0.250 WIDE AND 0.010 DEEP. REPAIRED SLAT TRACK 3-3 IAW MHIRJ REO 690-57-42-1020 REV-- DATED 1-2-24 CC670-12092-9
- [SDR VNAA202403070001](https://openairdocs.org/sdr/VNAA202403070001.md): Seat Track · corroded · Mar 7, 2024 · N569NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT AT LBL9 BETWEEN F.S.847+16 TO F.S.985 IS CORRODED.. REMOVED AND REPLACED SEAT TRACK SEGMENT AT LBL9 BETWEEN F.S.847+16 TO F.S.985 IAW CRJ 900 AMM 53-00-49-400-801-A12
- [SDR VNAA202308311111](https://openairdocs.org/sdr/VNAA202308311111.md): Unknown · unknown · Aug 29, 2023 · N569NN · Cndair CL6002D24 · Air Distribution System
  > DEPARTING OFF 18L, APPLIED FULL POWER AND THEY IMMEDIATELY SMELLED AND SAW SMOKE COMING OUT OF GASPER / RE-PERFORMED POST COMP WASH EVACUATION RUN AS REQUIRED FOR L ENGINE BLEED IAW CRJ-900 AMM 72ˆ’00ˆ’00ˆ’100ˆ’803ˆ’A01ˆ’PSA. NO FUMES OR SMOKE NOTED AFTE
- [SDR VNAA202307261111](https://openairdocs.org/sdr/VNAA202307261111.md): Sensor · faulted · Jul 22, 2023 · N569NN · Cndair CL6002D24 · Landing Gear Brake System
  > BRAKE OVHT WARNIMG MESSAGE IN FLIGHT. REMOVED AND REPLACED LOB BRAKE TEMPERATURE SENSOR IAW CRJ900 AMM 32-46-01-000/400-801. SELF TEST OF THE THERMOCOUPLE SENSOR GOOD PER AMM 32-46-01-740-801. THIS CLEARS MEL.
- [SDR VNAA202306221111](https://openairdocs.org/sdr/VNAA202306221111.md): Unknown · unknown · Jun 22, 2023 · N569NN · Cndair CL6002D24 · Passenger/Crew Doors
  > LOUD HISSING NOISE AT FLT LV 230 FELT PRESS CHANGE DECLARED EMERGENCY. INSPECTS PAX SEAL FOUND SEAL IN LWR RH CORNER TO BE LOOSE AND OUT OF TRACK. REINSTALLED SEAL INTO TRACK CLEAN SEAL AND PREFOMED PRESS CK NO LEAKS NOTED. SYS LEAK CHECK GOOD AT THIS TIME IAW
- [SDR VNAA202303091111](https://openairdocs.org/sdr/VNAA202303091111.md): None · none · Mar 7, 2023 · N569NN · Cndair CL6002D24 · Air Distribution System
  > STRONG SMELL IN CABIN RECORDED BY BOTH FA'S AND SEVERAL PAX RIGHT AFTER PUSHBACK COCKPIT INDICATIONS NORMAL. C/W RIGHT HAND ENGINE WASH IAW CRJ 900 AMM 72-00-00-100-803-A01-PSA.
- [SDR VNAA202109131111](https://openairdocs.org/sdr/VNAA202109131111.md): Gcu · malfunctioned · Sep 10, 2021 · N569NN · Cndair CL6002D24 · AC Generator-Alternator
  > WHILE ENROUTE TO ECP, CAPTAIN STATED THAT THE COCKPIT WENT DARK AND WHEN THE LIGHTS CAME BACK ON THEY HAD AN AC ESS BUS FAIL MESSAGE. CREW FOLLOWED THE QRH WITH NO VALID RESULTS. DECIDED TO RETURN TO CLT. CAPTAIN DID DECLARE GOING BACK AND THEN CANCELED THE EM
- [SDR VNAA2020073111101](https://openairdocs.org/sdr/VNAA2020073111101.md): Warning Message · false activation · Jul 26, 2020 · N569NN · Cndair CL6002D24 · Drag Control System
  > OB FLT SPOILER OB SPOILERONS CAUTION MSGS IN FLIGHT. CW SELF TEST OF THE SSCU IAW AMM OPS CHECK GOOD.
- [SDR VNAA2020032421101](https://openairdocs.org/sdr/VNAA2020032421101.md): Warning System · false activation · Mar 21, 2020 · N569NN · Cndair CL6002D24 · Landing Gear Steering System
  > CREW HAD A STEERING INOP CAUTION MESSAGE EN ROUTE TO OAJ. THE CREW FOLLOWED THEIR QRH AND AIR RETURNED BACK TO CLT. THEY DECLARED AN EMERGENCY AS A PRECAUTION BUT ONCE THE CREW LANDED SAFELY AND WAS TAXIING ON THEIR OWN THE EMERGENCY CREWS WERE CALLED OFF. THE
- [SDR VNAA202003229994](https://openairdocs.org/sdr/VNAA202003229994.md): Web · cracked · Feb 25, 2020 · N569NN · Cndair CL6002C10 · Passenger/Crew Doors
  > MULTIPLE CRACKS LOCATED ON PAX DOOR AFT WEB BENEATH STRUT.INSTALLED REPAIR PARTS IAW CRJ 900 SRM 52-11-04-201-004-A01.
- [SDR VNAA202003229993](https://openairdocs.org/sdr/VNAA202003229993.md): Web · cracked · Feb 24, 2020 · N569NN · Cndair CL6002C10 · Passenger/Crew Doors
  > CRACKS FOUND DOING REPAIR OF PAX DOOR AFT WEB, CRACKS LOCATED IN STEP REDIUS OF 2ND & 3RD STEP OF AFT WEB. FABRICATED REPAIR PARTS IAW CRJ900 SRM 52-11-04-201-004-A01. INSTALLED REPAIR PARTS IAW CRJ900 SRM 52-11-04-201-004-A01
- [SDR VNAA202003229992](https://openairdocs.org/sdr/VNAA202003229992.md): Web · cracked · Feb 23, 2020 · N569NN · Cndair CL6002C10 · Passenger/Crew Doors
  > MULTIPLE CRACKS LOCATED ON PAX DOOR AFT WEB BENEATH STRUT.CUTOUT DAMAGE IAW CRJ900 SRM 52-11-04-201-004-A01. REPAIR ZONE 4 TYPE 2
- [SDR VNAA202003229991](https://openairdocs.org/sdr/VNAA202003229991.md): Frame · corroded · Feb 19, 2020 · N569NN · Cndair CL6002C10 · Fuselage Main, Frame
  > LOWER FRAME SECTOR AT F.S. 310.00 CORRODED BETWEEN STR 26L & 26R, FWD & ACT FACE. COMPLIED WITH STEPS 1-3 OF CRJ 900 SRM 53-00-06-201-006-A01 FOR 201 SPLICE REPAIR.
- [SDR VNAA2020010211101](https://openairdocs.org/sdr/VNAA2020010211101.md): Cabin Pressure · malfunctioned · Jan 1, 2020 · N569NN · Cndair CL6002D24 · Cabin Pressure Control System
  > CREW HAD A CABIN ALTITUDE ISSUE AFTER TAKEOFF SO THEY DECLARED AN EMERGENCY AND RETURNED TO CLT WHERE THEY LANDED WITHOUT FURTHER INCIDENT. PERFORMED OPERATION TEST OF PRESS CONTROL SYSTEM IN MAN MODE, OPS CHECK GOOD.
- [SDR VNAA2019072311101](https://openairdocs.org/sdr/VNAA2019072311101.md): Wire Harness · chafed · Jul 23, 2019 · N569NN · Cndair CL6002D24 · Landing Gear System Wiring
  > DURING APPROACH. THE CREW RECEIVED A MAIN LANDING GEAR OVERHEAT WARNING MESSAGE. THE CREW RAN THE QRH AND WAS UNABLE TO GET THE MESSAGE TO EXTINGUISH. TEMPERATURES WERE NORMAL DURING THE APPROACH. FOLLOWING THE QRH THE CREW DECLARED AN EMERGENCY AND THE TRUCKS
- [SDR VNAA2019053111101](https://openairdocs.org/sdr/VNAA2019053111101.md): Panel · cracked · May 31, 2019 · N569NN · Cndair CL6002D24 · Passenger/Crew Doors
  > 690-52-11-565 (CRACKS IN PAX DOOR ZONE 2) C/W PERM REPAIR IAW GREO 670-52-11-287 REV E. "CONTINUATION OF SDR REPORT VNAA2019053111101 (ADDITIONAL CRACK FOUND WHILE INSPECTION EXISTING CRACK IN PAX DOOR ZONE 2)"
- [SDR VNAA2017072311101](https://openairdocs.org/sdr/VNAA2017072311101.md): Unknown · odor · Jul 23, 2017 · N569NN · Cndair CL6002D24 · Air Distribution System
  > AIRCRAFT PUSHED BACK FROM THE GATE AND AFTER THE CREW STARTED THE RIGHT ENGINE THEY REPORTED THAT A SMOKE ODOR WAS PRESENT IN THE COCKPIT AND CABIN AND THAT THE GROUND CREW COULD ALSO DETECT THE ODOR IN THE AFT CARGO BAY. THE WAS AIRCRAFT PUSHED BACK TO THE GA
- [SDR VNAA2016121500029](https://openairdocs.org/sdr/VNAA2016121500029.md): Mcu · faulty · Dec 15, 2016 · N569NN · Cndair CL6002D24 · Flight Control System
  > STABILIZER AND MACH TRIM FAIL MESSAGE. REMOVED AND REPLACED MCU.
- [SDR VNAA2016102900037](https://openairdocs.org/sdr/VNAA2016102900037.md): Outflow Valve · inoperative · Oct 29, 2016 · N569NN · Cndair CL6002D24 · Pressure Regulator/Outflow Valve
  > CABIN ALTITUDE CAUTION MESSAGE DURING CRUISE. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO THE NEAREST SUITABLE MAINTENANCE FACILITY. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE OUT
- [SDR VNAA2016101200013](https://openairdocs.org/sdr/VNAA2016101200013.md): Acm · failed · Oct 12, 2016 · N569NN · Cndair CL6002D24 · Cabin Cooling System
  > RIGHT A/C PACK AUTO FAIL MESSAGE AND RIGHT TEMP 99C DURING TAXI, CREW ALSO REPORTED SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT ACM DIFFICULT TO ROTATE. MAINTENANCE REMOVED AND REPLACED RIGHT ACM AND PERFORMED
- [SDR VNAA2016030800013](https://openairdocs.org/sdr/VNAA2016030800013.md): Pressure Sensor · dirty · Mar 8, 2016 · N569NN · Cndair CL6002D24 · Fuel Boost Pump
  > CREW REPORTED RECEIVING A LT MAIN EJECTOR CAUTION MESSAGE, ALONG WITH THE FUEL BOOST PUMPS CYCLING DURING CRUISE AT FL220. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, CLEANED THE LT PRIMARY EJECTOR’S PRESSURE SENSOR CONNE
- [SDR VNAA2015062500037](https://openairdocs.org/sdr/VNAA2015062500037.md): Tire · failed · Jun 25, 2015 · N569NN · Cndair CL6002D24 · Tire
  > RT INBD TIRE BLEW WHILE LANDING. R & R BOTH RT MLG WHEEL, TIRE ASSEMBLIES,

## 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 = 'N569NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N569NN/reports

---
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