# Service difficulty reports: N608NN

A list on [N608NN](https://openairdocs.org/aircraft/N608NN.md).

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

- [SDR VNAA202608200025](https://openairdocs.org/sdr/VNAA202608200025.md): Lug · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Ailerons
  > AFTER RT AILERON BUSHINGS REMOVAL WAS FOUND CORROSION ON LUG BORE R2 AT CENTER FITTING RT AILERON. LUG BORE R2 AT CENTER FITTING, RH AILERON WAS REPAIRED PER REO 670-57-61-237 REV.-- "
- [SDR VNAA202608200024](https://openairdocs.org/sdr/VNAA202608200024.md): Fitting · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Ailerons
  > CORROSION ON CENTER FITTING OF LH AILERON L5 LUG BORE. REPAIRED PER REO 670-57-61-237
- [SDR VNAA202608200023](https://openairdocs.org/sdr/VNAA202608200023.md): Fitting · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORRODED FLOOR FITTING IN AFT ACCESS 107 OUTSIDE (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 107 OUTSIDE (1EA) ON GALLEY WAS FABRICATED AND INSTALLED PER EA NO:2531-2026-0889 REV: - - SECTION III PERMANENT REPAIR.
- [SDR VNAA202608200022](https://openairdocs.org/sdr/VNAA202608200022.md): Fitting · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-21."
- [SDR VNAA202608200021](https://openairdocs.org/sdr/VNAA202608200021.md): Bearing · worn · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Rudder/Tab, Attach Fittings
  > FREE PLAY ON BEARINGS OF RUDDER HINGES NR 2 AND 3 AT REAR SPAR OF VERTICAL STABILIZER. BEARINGS OF RUDDER HINGES NR 2 AND 3 AT REAR SPAR OF VERTICAL STABILIZER WERE REPLACED PER RIL #1213 REV. NC.
- [SDR VNAA202608200020](https://openairdocs.org/sdr/VNAA202608200020.md): Floor Support · cracked · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT RBL 12, BTW BS 221.73 - 229, (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50) AT FWD FUSELAGE INTERNAL STRUCTURE. FLOOR SUPORT RBL 12.0 BTW BS 221.73 - 229 (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50) AT FWD FUSELAGE INTERNAL
- [SDR VNAA202608200019](https://openairdocs.org/sdr/VNAA202608200019.md): Canister · cracked · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CRACK ON CANISTER WELDED NO.3 IN STA WS=148 AT INTERNAL LH MAIN FUEL TANK. CRACK ON CANISTER WELDED NO.3 IN STA WS=148 AT INTERNAL LT MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV -.
- [SDR VNAA202608200018](https://openairdocs.org/sdr/VNAA202608200018.md): Seat Track · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > WEAR RH SEAT RAIL FS 847.00 +16.00 TO 977.00 AT PAX CABIN. RT SEAT RAIL FS 847.00 +16.00 TO 977.00 AT PAX CABIN. WAS EVALUATED OUT OF LIMITS PER SRM 53-51-49-101-001-A02 AND REPLACED PER AMM 53-00-49.
- [SDR VNAA202608200017](https://openairdocs.org/sdr/VNAA202608200017.md): Seat Track · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SIDE RAIL BTW FS=700 TO FS=379 AT CPAX. CORROSION ON LH SIDE RAIL BTW FS=700 TO FS=379 AT CPAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.
- [SDR VNAA202608200016](https://openairdocs.org/sdr/VNAA202608200016.md): Seat Track · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SIDE RAIL BTW FS=881 TO FS=785 AT CPAX. CORROSION ON LH SIDE RAIL BTW FS=881 TO FS=785 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.
- [SDR VNAA202608200015](https://openairdocs.org/sdr/VNAA202608200015.md): Seat Track · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE RAIL BTW FS=744 TO FS=761 AT CPAX. CORROSION ON RH SIDE RAIL BTW FS=744 TO FS=761 AT CPAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.
- [SDR VNAA202608200014](https://openairdocs.org/sdr/VNAA202608200014.md): Seat Track · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE RAIL BTW FS=421 TO 485, FS=501 TO FS=570, FS=610 TO FS=720 AT CPAX. RIGHT SIDE RAIL BTW FS=421 TO 485, FS=501 TO FS=570, FS=610 TO FS=720 AT CPAX WERE REPLACED PER CRJ900 AMM 53-00-49"
- [SDR VNAA202608200013](https://openairdocs.org/sdr/VNAA202608200013.md): Seat Track · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL=26 BTW FS=486 TO FS=597 AT CPAX. CORROSION ON SEAT RAIL LBL=26 BTW FS=486 TO FS=597 AT CPAX. WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49.
- [SDR VNAA202608200012](https://openairdocs.org/sdr/VNAA202608200012.md): Seat Track · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL=10 BTW FS=598 TO FS=669.40 AT CPAX. CORROSION ON SEAT RAIL LBL=10 BTW FS=598 TO FS=669.40 AT CPAX. WAS EVALUATED OUT OF LIMITS PER SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.
- [SDR VNAA202608200011](https://openairdocs.org/sdr/VNAA202608200011.md): Seat Track · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL RBL9.00 BTW FS=486 TO FS=597, FS=598 TO FS=669.40 AT CPAX. CORROSION ON SEAT RAIL RBL9.00 BTW FS=486 TO FS=597, FS=598 TO FS=669.40 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.
- [SDR VNAA202608200010](https://openairdocs.org/sdr/VNAA202608200010.md): Seat Track · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL=26 BTW FS=364 TO FS=485 AT PAX CABIN. CORROSION ON SEAT RAIL LBL=26 BTW FS=364 TO FS=485 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A02. AND SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.
- [SDR VNAA202608200009](https://openairdocs.org/sdr/VNAA202608200009.md): Seat Track · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 9 BTW BS 379 - 485 AT CPAX. CORROSION ON SEAT TRACK LBL 9 BTW BS 379 - 485 AT CPAX. WAS EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A02 AND SRM 53-31-49-101-001-A02 REPLACED IAW AMM 53-00-49.
- [SDR VNAA202608200008](https://openairdocs.org/sdr/VNAA202608200008.md): Seat Track · corroded · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK RBL9, BTW BS 349 - 485 AT CPAX. CORROSION ON SEAT TRACK RBL9.00 BTW FS=349 TO FS=485 AT CPAX. WAS EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A02 AND SRM 53-31-49-101-001-A02 REPLACED IAW AMM 53-00-49.
- [SDR VNAA202608200007](https://openairdocs.org/sdr/VNAA202608200007.md): Floor Support · cracked · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2234
- [SDR VNAA202608200006](https://openairdocs.org/sdr/VNAA202608200006.md): Rib · cracked · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON RIB LEADING EDGE SS 57.16 AT RH WING. CRACK ON RIB LEADING EDGE SS 57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV. -.
- [SDR VNAA202608200005](https://openairdocs.org/sdr/VNAA202608200005.md): Rib · cracked · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON RIB LEADING EDGE SS 57.16 AT LH WING. RIB LEADING EDGE SS 57.16 AT LH WING WAS REPAIRED PER REO 690-57-41-240 REV -.
- [SDR VNAA202608200004](https://openairdocs.org/sdr/VNAA202608200004.md): Web · cracked · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193. ELECTRICAL BAY FLOOR WEB RIGHT SIDE WAS REPAIRED PER SRM 53-11-43-201-001-A01
- [SDR VNAA202608200003](https://openairdocs.org/sdr/VNAA202608200003.md): Skin · damaged · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Trailing Edge Flaps
  > SEVERAL NICKS, EROSION AND WEAR ON LOWER SKIN OF LH INBOARD FLAP FLS 15.5 TO FLS 75.5 WAS REPAIRED PER CRJ900 SRM 57-52-01-201-005-A01
- [SDR VNAA202608200002](https://openairdocs.org/sdr/VNAA202608200002.md): Tail Cone · dented · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Aerodynamic Fairings
  > DENT IN TAILCONE WAS REPAIRED IAW REO 690-53-84-062 REV -.
- [SDR VNAA202608200001](https://openairdocs.org/sdr/VNAA202608200001.md): Door · cracked · Aug 14, 2026 · N608NN · Cndair CL6002D24 · Fluid Service Doors
  > DOOR WASTE ASSEMBLY WAS REPAIRED PER EA NO: 2542-2026-0913 REV. -
- [SDR VNAA202305220012](https://openairdocs.org/sdr/VNAA202305220012.md): Hinge · elongated · May 22, 2023 · N608NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > AFTER HINGE REMOVAL IN REF. NRC 00005, ELONGATED HOLES (3EAS) WAS FOUND. ELONGATED HOLES (3EAS) WERE REPAIRED PER REO 690-53-21-1626 REV.-A
- [SDR VNAA202305220011](https://openairdocs.org/sdr/VNAA202305220011.md): Stringer · damaged · May 22, 2023 · N608NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > DENTS 2 (EA´S) ON INBOARD FLAP, LOWER SKIN. AT WS 29.00 TO WS 68.00. 3.5 IN FROM T.E. DENTS (2 EAS) ON INBOARD FLAP, LOWER SKIN AT WS 29.00 TO WS 68.00 WERE EVALUATED AS FOLLOWS: DENT 1 (BTW FLS25.50 AND FLS30.00) WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 57
- [SDR VNAA202305220010](https://openairdocs.org/sdr/VNAA202305220010.md): Skin · cracked · May 22, 2023 · N608NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL NICKS ON LOWER SKIN OF AFT FUSELAGE BTW FS 977.00 TO 1051.3 AND STG 21 RH TO STR 27. NICKS ON LOWER SKIN OF AFT FUSELAGE BTW FS 977.00 TO 1051.3 AND STG 21 RH TO STR 27 WERE REPAIRED PER EA EA 23-C9-53-0562-IR; EA 23-C9-53-0565-IR;EA 23-C9-53-0566-I
- [SDR VNAA202305220009](https://openairdocs.org/sdr/VNAA202305220009.md): Skin · cracked · May 22, 2023 · N608NN · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > WEAR MARK ON EXTERNAL FUSELAGE SKING BTW FS897-FS913 AND BTW STGR 26L-27. WEAR ON EXTERNAL FUSELAGE SKIN BTW FS897 TO FS913 AND STGR 26L TO STGR 27 WAS REPAIRED PER EA 23-C9-53-0554 REV. IR
- [SDR VNAA2023052202](https://openairdocs.org/sdr/VNAA2023052202.md): Seat Track · worn · May 22, 2023 · N608NN · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION WAS FOUND BETWEEN THE FOLLOWING STATIONS: FROM FS 785.15 TO FS 797.00 OF THE R/H SIDE SEAT RAIL. CORRECTIVE ACTION: R/H SIDE SEAT RAIL FROM FS 785.15 TO FS 797.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER C
- [SDR VNAA2023052201](https://openairdocs.org/sdr/VNAA2023052201.md): Seat Track · worn · May 22, 2023 · N608NN · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > "DISC.- CORROSION ON SEAT RAIL RBL 9 BTW F.S.349.00 TO F.S. 359.00. CA- SEAT RAIL RBL 9 BTW F.S.349.00 TO F.S. 359.00 WAS EVALUATED OUT OF LIMITS PER CRJ/900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ/900 AMM 53-00-49-000-801 ( CONFIG A12) AND CRJ-900
- [SDR VNAA202109301111](https://openairdocs.org/sdr/VNAA202109301111.md): Sensor · faulted · Sep 27, 2021 · N608NN · Cndair CL6002D24 · Landing Gear Brake System
  > CREW GOT A BRAKE TEMP OVER HEAT MESSAGE ON TAKE OFF IN CLT. THEY WERE BETWEEN 30-40KTS WHEN THEY REJECTED THEY TAKE OFF AND NOTIFIED ATC OF THE ISSUE. THEY EXITED THE RUNWAY AND PARKED AT A HARD STAND WHERE EMERGENCY VEHICLES WERE ON STANDBY MONITORING THE BRA
- [SDR VNAA202104271112](https://openairdocs.org/sdr/VNAA202104271112.md): Skin · gouged · Apr 24, 2021 · N608NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DURING OVERNIGHT MAINTENANCE, MX REPORTED A GOUGE ON THE AC SKIN GOUGE LOCATED AT FS581-FS597 STGR20L Ï¿½ STGR21L THE GOUGE DIMENSIONS ARE AS FOLLOWS.781"L X.375"W X.0085"D. THE AC SKIN (P/N SH690-33202-19) IS FABRICATED FROM 2024-T3.150Ï¿½, CHEM MILLED D
- [SDR VNAA202103121111](https://openairdocs.org/sdr/VNAA202103121111.md): Tire · failed · Mar 11, 2021 · N608NN · Cndair CL6002D24 · Tire
  > CREW REPORTED RH OUTBOARD MLG TIRE BLOWN ON LANDING. REMOVED AND REPLACE RH OB WHEEL ASSEMBLY
- [SDR VNAA2020040241102](https://openairdocs.org/sdr/VNAA2020040241102.md): Gcu · malfunctioned · Mar 31, 2020 · N608NN · Cndair CL6002D24 · AC Regulator
  > DURING CRUISE TO MKE THE CAPT REPORTED A IDG 1, GEN 1, AC BUS 1 MAGENTA FAULT. HE DIVERTED TO DAY PER OUR REQUEST. MX HAD TO TROUBLESHOOT, RE-RACKED IDG 1 AND IDG 2 GENERATOR CONTROL UNIT IAW CRJ 900 AMM. OPS TEST GOOD AT THIS TIME.

## 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 = 'N608NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N608NN/reports

---
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