# Service difficulty reports: N619NN

A list on [N619NN](https://openairdocs.org/aircraft/N619NN.md).

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

- [SDR VNAA202304270005](https://openairdocs.org/sdr/VNAA202304270005.md): Stringer · corroded · Apr 24, 2023 · N619NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 26R BTW FS=364.00/349.0 AT MAIN AVIONICS COMPARTMENT. (E/E)
- [SDR VNAA202304270004](https://openairdocs.org/sdr/VNAA202304270004.md): Frame · corroded · Apr 24, 2023 · N619NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME FS= 364.00 BETWEEN STRG 26RH TO 26RH AT MAIN AVIONICS COMPARTMENT
- [SDR VNAA202304270023](https://openairdocs.org/sdr/VNAA202304270023.md): Skin · dented · Apr 19, 2023 · N619NN · Cndair CL6002D24 · Trailing Edge Flaps
  > SEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FROM FLS 15.00 TO FLS 65.50
- [SDR VNAA202304270003](https://openairdocs.org/sdr/VNAA202304270003.md): Support · corroded · Apr 19, 2023 · N619NN · Cndair CL6002D24 · Wing, Landing Gear Attach Fittings
  > CORROSION ON LH/RH MLG SIDE STAY SUPPORT.
- [SDR VNAA202304270033](https://openairdocs.org/sdr/VNAA202304270033.md): Support · corroded · Apr 18, 2023 · N619NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION ON SUPPORTS (2EA) AT LH WHEEL WELL AREA BTW FS=797 TO FS=830 AND LBL / RBL 45".
- [SDR VNAA202304270008](https://openairdocs.org/sdr/VNAA202304270008.md): Channel · corroded · Apr 14, 2023 · N619NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON INTERNAL PRODUCTION DOUBLER AND ANCHORE NUT IN STA. FS=310 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT
- [SDR VNAA202304270020](https://openairdocs.org/sdr/VNAA202304270020.md): Skin · corroded · Apr 13, 2023 · N619NN · Cndair CL6002D24 · Nacelle/Pylon, Plate/Skin
  > CORROSION ON LEADING EDGE (LIP SKIN) OF RH ENGINE INLET COWL.
- [SDR VNAA202304270010](https://openairdocs.org/sdr/VNAA202304270010.md): Acoustic Liner · dented · Apr 12, 2023 · N619NN · Cndair CL6002D24 · Nacelle/Pylon Structure
  > DENT AT 7:00 O'CLOCK POSITION CLOSE TO THE LEADING EDGE ON METAL PERFORATE ACOUSTIC LINER OF RIGHT FORWARD CORE COWL
- [SDR VNAA202304270019](https://openairdocs.org/sdr/VNAA202304270019.md): Lug · corroded · Apr 4, 2023 · N619NN · Cndair CL6002D24 · Wing, Control Surfaces
  > CORROSION ON BORE LUGS AT HINGE FITTING #2 (I/B AND O/B) & HINGE FITTING#3 (O/B), RH AILERON
- [SDR VNAA202304270018](https://openairdocs.org/sdr/VNAA202304270018.md): Hinge Fitting · worn · Mar 19, 2023 · N619NN · Cndair CL6002D24 · Vertical Stabilizer
  > AFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO.2 AND NO. 3 AT VERYTICAL STABILIZER REAR SPAR MIDDLE SECTION.
- [SDR VNAA202304270017](https://openairdocs.org/sdr/VNAA202304270017.md): Coupling · corroded · Mar 17, 2023 · N619NN · Cndair CL6002D24 · Aircraft Fuel Distribution System
  > CORROSION ON COUPLINGS OF FUEL OVERWING VENT TUBING, LOCATED IN WHEEL WELL AREA BTW FS=797.00 TO FS= 813 AND RBL 39".
- [SDR VNAA202304270015](https://openairdocs.org/sdr/VNAA202304270015.md): Hinge Fitting · corroded · Mar 16, 2023 · N619NN · Cndair CL6002D24 · Empennage Flight Control Surfaces, Attach Fittings
  > CORROSION ON LOWER RUDDER HINGE AT REAR SPAR OF VERTICAL STABILIZER
- [SDR VNAA202304270014](https://openairdocs.org/sdr/VNAA202304270014.md): Angle · corroded · Mar 15, 2023 · N619NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON KICK PLATE ANGLE AT LOWER SILL, FUSELAGE PASSENGER DOOR FRAME
- [SDR VNAA202304270013](https://openairdocs.org/sdr/VNAA202304270013.md): Cap · corroded · Mar 15, 2023 · N619NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP AT LOWER SILL, FUSELAGE PASSENGER DOOR FRAME
- [SDR VNAA202304270012](https://openairdocs.org/sdr/VNAA202304270012.md): Skin · dented · Mar 15, 2023 · N619NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENTS ON EXTERNAL FUSELAGE SKIN, REAR FUSELAGE SKIN COVERED BY RH VENTRAL FIN FAIRING
- [SDR VNAA202304270011](https://openairdocs.org/sdr/VNAA202304270011.md): Skin · dented · Mar 15, 2023 · N619NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENTS ON EXTERNAL FUSELAGE SKIN, REAR FUSELAGE SKIN COVERED BY LH VENTRAL FIN FAIRING.
- [SDR VNAA202304270009](https://openairdocs.org/sdr/VNAA202304270009.md): Seat Track · corroded · Mar 15, 2023 · N619NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL LBL 9.0 BETWEEN FS364.00-FS485.00
- [SDR VNAA202304270035](https://openairdocs.org/sdr/VNAA202304270035.md): Support · corroded · Mar 14, 2023 · N619NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON HYD LINE SUPPORTS (4 EAS) AT LH / RH WHEEL WELL AREA BTW FS=797 TO FS= 830 AND LBL 40" AND 35" / RBL 40" AND 35"
- [SDR VNAA202304270034](https://openairdocs.org/sdr/VNAA202304270034.md): Support · corroded · Mar 14, 2023 · N619NN · Cndair CL6002D24 · Standard Practices/Structures
  > CORROSION ON LH/RH CONNECTORS SUPPORT PX10J1, PX01J1 AND PX09J1.
- [SDR VNAA202304270032](https://openairdocs.org/sdr/VNAA202304270032.md): Retainer · corroded · Mar 14, 2023 · N619NN · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION ON SEAL RETAINER OF LH/RH WING TO FUSELAGE FAIRING AT WHEEL WELL AREA.
- [SDR VNAA202304270031](https://openairdocs.org/sdr/VNAA202304270031.md): Rib · corroded · Mar 14, 2023 · N619NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CORROSION ON RIB #1 AT RH WING.
- [SDR VNAA202304270030](https://openairdocs.org/sdr/VNAA202304270030.md): Access Panel · corroded · Mar 14, 2023 · N619NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON SETTLEMENT AREA OF ACCESS PANELS 542AZ, 542BZ, 642BZ AND 642AZ
- [SDR VNAA202304270029](https://openairdocs.org/sdr/VNAA202304270029.md): Door · corroded · Mar 14, 2023 · N619NN · Cndair CL6002D24 · Landing Gear Doors
  > CORROSION ON RH MLG DOOR ON INTERNAL AND EXTERNAL SKIN
- [SDR VNAA202304270028](https://openairdocs.org/sdr/VNAA202304270028.md): Skin · corroded · Mar 14, 2023 · N619NN · Cndair CL6002D24 · Landing Gear Doors
  > CORROSION ON LH MLG DOOR ON INTERNAL AND EXTERNAL SKIN
- [SDR VNAA202304270007](https://openairdocs.org/sdr/VNAA202304270007.md): Frame · corroded · Mar 14, 2023 · N619NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME FS= 310 BETWEEN STRG 24LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E)
- [SDR VNAA202304270006](https://openairdocs.org/sdr/VNAA202304270006.md): Frame · corroded · Mar 14, 2023 · N619NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME FS=333 BETWEEN STRG 25LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E)
- [SDR VNAA202304270002](https://openairdocs.org/sdr/VNAA202304270002.md): Pressure Deck · corroded · Mar 14, 2023 · N619NN · Cndair CL6002D24 · Wing, Plate/Skin
  > CORROSION ON DOUBLER OF WING STUD LOWER SKIN AT LH WHEELWELL AREA BTW FS 797 TO FS=830 AND LBL 38".
- [SDR VNAA202304270001](https://openairdocs.org/sdr/VNAA202304270001.md): Block · corroded · Mar 14, 2023 · N619NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION ON LH/RH MLG HYDRAULICS LINES BLOCKS AND THEIR SUPPORTS
- [SDR VNAA202304270027](https://openairdocs.org/sdr/VNAA202304270027.md): Valve · corroded · Mar 13, 2023 · N619NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON FLOATATION VALVE OF AFT ACCESSORIES COMPARTMENT BULKHEAD FS 1098
- [SDR VNAA202304270026](https://openairdocs.org/sdr/VNAA202304270026.md): Cylinder · corroded · Mar 12, 2023 · N619NN · Cndair CL6002D24 · Nose/Tail Landing Gear Strut/Axle
  > CORROSION IN LOWER SURFACE OF NLG OUTER CYLINDER
- [SDR VNAA202304270025](https://openairdocs.org/sdr/VNAA202304270025.md): Retainer · corroded · Mar 12, 2023 · N619NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CORROSION ON RETAINER SEALS AT ACCESS PANEL 583AB, 583BB, 683AB, 683BB
- [SDR VNAA202304270024](https://openairdocs.org/sdr/VNAA202304270024.md): Frame · corroded · Mar 12, 2023 · N619NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > CORROSION ON FWD HANDLE FRAME AT FWD / CENTER BAGGAGE BAY DOOR INTERNAL STRUCTURE.
- [SDR VNAA202304270022](https://openairdocs.org/sdr/VNAA202304270022.md): Skin · corroded · Mar 11, 2023 · N619NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND IN DRAIN OF THE LOWER TAILCONE FS1181.00.
- [SDR VNAA202304270021](https://openairdocs.org/sdr/VNAA202304270021.md): Channel · corroded · Mar 11, 2023 · N619NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > IN TAILCONE AND THE DRAG ANGLE ADJACENT TO BELOW RUDDER WAS FOUND CORROSION
- [SDR VNAA202304270016](https://openairdocs.org/sdr/VNAA202304270016.md): Doubler · corroded · Feb 1, 2023 · N619NN · Cndair CL6002D24 · Empennage Structure
  > CORROSION ON LIGHTNING PROTECTION STRIP ON RH/LH HORIZONTAL STABILIZER TIP EXTERNAL STRUCTURE (ACCESS PANEL 343BR AND 333BL)

## 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 = 'N619NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N619NN/reports

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