# Service difficulty reports: N602NN

A list on [N602NN](https://openairdocs.org/aircraft/N602NN.md).

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

- [SDR VNAA2026072521202](https://openairdocs.org/sdr/VNAA2026072521202.md): Skin · dented · Jul 23, 2026 · N602NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > EA 5321-2026-0570 (560FH PERM REPAIR - FUSELAGE SKIN DENTED. REPAIR FOR REWORKED DENT AND GOUGE DAMAGE TO FUSELAGE SKIN PANEL BETWEEN BS 295 & BS 310, STR 13 & STR 14R. REO 690-53-21-2176 INCORPORATED.
- [SDR VNAA2026061218801](https://openairdocs.org/sdr/VNAA2026061218801.md): Gcu · faulted · Jun 9, 2026 · N602NN · Cndair CL6002D24 · AC Generator-Alternator
  > AAN AC ESS BUS FAIL, WILL NOT TRANSFER / REMOVED AND REPLACED GCU 1 IAW AMM 24€“11€“07€“000/400€“801. OPS CHECK GOOD. PERFORMED SUCCESSFUL OPS CHECK OF ESS BUS TRANSFER SYSTEM IAW AMM 24€“51€“00€“710€“803.
- [SDR VNAA20260303015](https://openairdocs.org/sdr/VNAA20260303015.md): Fitting · corroded · Jan 20, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON THE LOWER FITTING OF FOLDING WORKSHELF AT FWD LAVATORY. LOWER FITTING WAS REPLACED IAW CMM 25-40-19.
- [SDR VNAA20260303014](https://openairdocs.org/sdr/VNAA20260303014.md): Fitting · corroded · Jan 20, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Equipment Attach Fittings
  > CORRODED FLOOR FITTING ON ACCESS 107. FLOOR FITTING WAS REPLACED IAW CMM 25-33-21.
- [SDR VNAA20260303012](https://openairdocs.org/sdr/VNAA20260303012.md): Floor Support · cracked · Jan 18, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, RBL 12, BS 221.73 - 229. THE FLOOR SUPPORT WAS REPAIRED IAW REO 690-53-11-2129, REV-.
- [SDR VNAA20260303016](https://openairdocs.org/sdr/VNAA20260303016.md): Rib · cracked · Jan 17, 2026 · N602NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > CRACKED MACHINED WING RIB, LEADING EDGE SS58.41, RT WING. THE RIB WAS REPAIRED IAW REO 690-57-41-240, REV -.
- [SDR VNAA20260303011](https://openairdocs.org/sdr/VNAA20260303011.md): Seat Track · corroded · Jan 17, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > TWO CORRODED SEAT TRACK SECTIONS, LBL 9, BS 581 - 677 IN THE PAX CABIN. THE SEAT TRACK SECTIONS WERE EVALUATED OUT OF LIMITS IAW SRM 53-31-49-101-001-A02, AND WERE REPLACED IAW SRM 53-00-49, CONFIG. A12.
- [SDR VNAA20260303010](https://openairdocs.org/sdr/VNAA20260303010.md): Seat Track · corroded · Jan 17, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED TWO SEAT TRACK SECTIONS, BS 364 - 485, & BS 581 - 677, RBL 9 IN THE PAX CABIN. THE SEAT TRACKS WERE EVALUATED AND FOUND OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, AND SRM 53-41-49-101-001-A02, REPLACED IAW AMM 53-00-49.
- [SDR VNAA20260303009](https://openairdocs.org/sdr/VNAA20260303009.md): Fitting · corroded · Jan 17, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON FOUR MACHINED FITTINGS IN THE FWD, CTR CARGO BAY. THE FOUR MACHINED FITTINGS WERE EVALUATED TO EXCESSIVE CORROSION IAW SRM 51-10-06-001-001-A01 AND REPLACED IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, AND SRM 51-42-10-001-001-A01.
- [SDR VNAA20260303005](https://openairdocs.org/sdr/VNAA20260303005.md): Hinge · corroded · Jan 17, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Door Hinge
  > CORROSION ON THE HINGE OF ACCESS PANEL 832ET OF PASSENGER DOOR. THE HINGE WAS REPLACED ON STEP PANEL 832ET IAW SRM 51-41-02-001-001-A01.
- [SDR VNAA20260303004](https://openairdocs.org/sdr/VNAA20260303004.md): Seat Track · corroded · Jan 16, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE RT SIDE SEAT TRACK, BS 669.40 - 720.85, & BS 744.15 - 761.85 IN THE PAX CABIN. THE SEAT TRACK EVALUATED OUT OF LIMITS IAW 53-41-51-101-001-A02, AND WERE REPLACED IAW AMM 53-00-49, CONFIG. A12.
- [SDR VNAA20260303003](https://openairdocs.org/sdr/VNAA20260303003.md): Seat Track · corroded · Jan 16, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED LT SIDE SEAT TRACK, BS 744.15 - 761.85, AND BS 785.15 - 847+16 IN THE PAX CABIN. THE SEAT TRACK WAS EVALUATED OUT OF LIMITS IAW SRM 53-41-51-101-001-A02, AND WAS REPLACED IAW AMM 53-00-49, CONFIG. A12.
- [SDR VNAA20260303001](https://openairdocs.org/sdr/VNAA20260303001.md): Web · cracked · Jan 15, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACKED WEB, RT SIDE BS 193, FWD E & E BAY. THE WEB WAS REPAIRED IAW SRM 53-11-43-201-001-A01.
- [SDR VNAA20260303002](https://openairdocs.org/sdr/VNAA20260303002.md): Floorbeam · cracked · Jan 15, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACK ON FLOOR BEAM RBL12 ON FS280 BELLOW FLIGHT COMPARTMENT. FLOOR BEAM RBL12 ON FS280 BELLOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2127 REV. - -
- [SDR VNAA20260205015](https://openairdocs.org/sdr/VNAA20260205015.md): Web · cracked · Jan 15, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON WEB RH SIDE FS 193.0 AT FWD EQUIPMENT COMPARTMENT. WEB RH SIDE FS 193.0 AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER SRM 53-11-43-201-001-A01
- [SDR VNAA20260303008](https://openairdocs.org/sdr/VNAA20260303008.md): Tube · corroded · Jan 14, 2026 · N602NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON DOOR SILL, BS 310 - 349 AND TUBE ASSY OF ELECTRICAL HARNESS ON BS 322.15 AT LOWER SUROUND STRUCTURE PASSENGER DOOR CUT-OUT. CORROSION REMOVED IAW SRM 51-21-06-001-001-A01 AND THE DOOR SILL WAS EVALUATED WITHIN LIMITS & THE TUBE ASSY WAS EVALUATED
- [SDR VNAA20260303007](https://openairdocs.org/sdr/VNAA20260303007.md): Rib · cracked · Jan 14, 2026 · N602NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > CRACKED LT WING L/E RIB SS 15.50. THE RIB WAS REPAIRED IAW REO 690-57-41-580, REV-.
- [SDR VNAA20260303006](https://openairdocs.org/sdr/VNAA20260303006.md): Drag Angle · cracked · Jan 11, 2026 · N602NN · Bombdr CL6002D15 · Fuselage, Stabilizer Attach Fittings
  > CRACKED LT AFT DRAG ANGLE BETWEEN UNION OF FUSELAGE AND VERTICAL STABILIZER. 67.5% REAR SPAR DATUM. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.
- [SDR VNAA20260303013](https://openairdocs.org/sdr/VNAA20260303013.md): Seat Track · corroded · Dec 4, 2025 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK, RBL 9, BS 881 - 897. THE SEAT TRACK WAS EVALUATED, AND FOUND TO EXCESS DAMAGE IAW SRM 53-51-51-101-001-A02, AND REPLACED IAW AMM 53-00-49-400-801.
- [SDR VNAA2025021011104](https://openairdocs.org/sdr/VNAA2025021011104.md): Fadec · unserviceable · Feb 8, 2025 · N602NN · Cndair CL6002D24 · Fuel Controlling System
  > R FADEC CAUTION MSG. NO ABNORMAL ENGINE INDICATIONS / REMOVED AND REPLACED RH ENG FADEC IAW AMM 73-21-01-000/400-801-A01, OPS TEST GOOD.
- [SDR VNAA202307121112](https://openairdocs.org/sdr/VNAA202307121112.md): Wheel · unserviceable · Jul 9, 2023 · N602NN · Cndair CL6002D24 · Wheel/Ski/Float
  > RH IB MLG TIRE MISSING THROUGH BOLT / REMOVED AND REPLACED RH IB MLG WTA IAW CRJ 900 AMM 32-41-01-000/400-801-A01-PSA.NO DEFECTS NOTED AT THIS TIME.
- [SDR VNAA202301280003](https://openairdocs.org/sdr/VNAA202301280003.md): Seat Track · corroded · Jan 28, 2023 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL RBL9.00 BETWEEN FS360-485. ORROSION AT SEAT RAIL RBL9.00 BETWEEN FS360.00-FS485.00 WAS EVALUATED OUT OF LIMITSDUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-21-49-101-001-A01 AND CRJ-900SRM 53-31-49-101-001-A02 THEREFORE SECTION OF SEAT RA
- [SDR VNAA202301280002](https://openairdocs.org/sdr/VNAA202301280002.md): Slat Track · corroded · Jan 28, 2023 · N602NN · Bombdr CL6002D15 · Leading Edge Devices
  > CORROSION ON SLAT TRACKS UPPER/LOWER,1-2 AND 2-2 AT LH WING. TRACK 2 OF SLAT 2 WAS MEASUREMENT AND WAS FOUND WITHIN LIMITS PER REO 690-57-42-950 REV-. TRACK 2 OF SLAT 1 WAS REPLACED PER CRJ-900 AMM27-81-41-000-802-A01 AND AMM 27-81-41-400-802-A01
- [SDR VNAA202301280001](https://openairdocs.org/sdr/VNAA202301280001.md): Skin · damaged · Jan 28, 2023 · N602NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > SEVERAL NICKS AT LOWER SKIN OF AFT FUSELAGE BETWEEN FS 1015.0 AND FS 1047.0 AND BETWEEN STRG 27L AND STRG 25R. REPAIRED PER EA 23-C9-53-0053 REV. IR, SECTION III - PERMANENT REPAIR
- [SDR VNAA202301270005](https://openairdocs.org/sdr/VNAA202301270005.md): Seat Track · corroded · Jan 27, 2023 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL RBL9.00 BETWEEN FS581.- 00-FS661+32.00. CORROSION AT SEAT RAIL RBL9.00 BETWEEN FS581.00-FS661+32.00 WAS EVALUATED OUT OF LIMITS DUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-31-49-101-001-A02 THEREFORE SECTION OF SEAT RAIL RBL9.00 BETWEEN F
- [SDR VNAA202301270004](https://openairdocs.org/sdr/VNAA202301270004.md): Seat Track · corroded · Jan 27, 2023 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL RBL9.00 BETWEEN FS349.- 00-FS360.00. SEAT RAIL RBL9.00 BETWEEN FS349.00-FS360.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101- 001-A01 AND WAS REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A12)
- [SDR VNAA202301270003](https://openairdocs.org/sdr/VNAA202301270003.md): Seat Track · corroded · Jan 27, 2023 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > : CORROSION ON SEAT RAIL AT LBL 27.00 BETWEEN FS 364.00-FS485.00. SEAT RAIL AT LBL 27.00 BETWEEN FS 364.00-FS485.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A12)
- [SDR VNAA202301270002](https://openairdocs.org/sdr/VNAA202301270002.md): Seat Track · corroded · Jan 27, 2023 · N602NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION AT SEAT RAIL LBL9.00 BETWEEN FS581-FS661+32. CORROSION AT SEAT RAIL LBL9.00 BETWEEN FS581-FS661+32 WAS EVALUATED OUT OF LIMITS DUE TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-31-49-101- 001-A02 THEREFORE SECTION OF SEAT RAIL LBL9.00 BE
- [SDR VNAA202301270001](https://openairdocs.org/sdr/VNAA202301270001.md): Panel · cracked · Jan 27, 2023 · N602NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > CRACK ON FWD/AFT PANEL SIDE AT CORNER FOR STEP (ACCESS 832CT), PAX DOOR. FWD/AFT PANEL SIDE AT CORNER FOR STEP (ACCESS 832CT), PAX DOOR WERE REPAIRED PER CRJ-900 SRM-52-11-04-201-004- A01.
- [SDR VNAA202107271111](https://openairdocs.org/sdr/VNAA202107271111.md): Filter · unserviceable · Jul 25, 2021 · N602NN · Cndair CL6002D24 · Air Distribution System
  > ON APPROACH HIGH POWER SETTING REQUIRED TO MAINTAIN SPEED AND BURNING SMELL IN COCKPIT DURING LANDING AND GROUND ROLL. PERFORMED POWER ASSURANCE CHECK W/ CREW IAW AMM 71-00-00-720-804-A02. PERFORMED OPERATIONAL TEST OF AC DISTRIBUTION SYSTEM IAW CRJ 900 AMM 21
- [SDR VNAA202104271113](https://openairdocs.org/sdr/VNAA202104271113.md): Detector · unserviceable · Apr 25, 2021 · N602NN · Cndair CL6002D24 · Trailing Flap Position Indicating System
  > FLAPS FAIL CAUTION MESSAGE APPEARED IN FLIGHT. CREW RAN THE QRH AND DECLARED AN EMERGENCY INTO CLT. CONDUCTED A FLAPLESS LANDING ON RWY 36C. PASSENGERS DID NOT BRACE. TRUCKS WERE ROLLED AS A PRECAUTION. FLIGHT LANDED SAFELY AND AIRCRAFT HAS BEEN CLEARED FOR TH

## 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 = 'N602NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N602NN/reports

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