# Service difficulty reports: N617NN

A list on [N617NN](https://openairdocs.org/aircraft/N617NN.md).

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

- [SDR VNAA2026080422201](https://openairdocs.org/sdr/VNAA2026080422201.md): Iru · unserviceable · Aug 2, 2026 · N617NN · Cndair CL6002D24 · Attitude and Direction Data System
  > PITCH FEEL FAULT STATUS MSG IN FLIGHT AND YD2 INOP, FMS 2 DISPLAYED IRS REVERTED LOST FO'S PFD INDICATION C/A REMOVED AND REPLACED IRU 2 IAW CRJ900 AMM 34-45-01-000/400-801-A01.
- [SDR VNAA20260501023](https://openairdocs.org/sdr/VNAA20260501023.md): Rib · cracked · Apr 24, 2026 · N617NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > CRACK ON RIB OF FIXED LEADING EDGE STA FS=58.41 (UPPER SIDE) AT RH WING. RIB OF FIXED LEADING EDGE STA FS=58.41 (UPPER SIDE) AT RH WING WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR VNAA20260501022](https://openairdocs.org/sdr/VNAA20260501022.md): Slider · corroded · Apr 24, 2026 · N617NN · Bombdr CL6002D15 · Engine Thrust Reverser
  > CORROSION ON INB SLIDER AT UPPER TRANSCOWL ENG RH. UPPER TRANSCOWL RH WAS REPLACED PER CRJ900 AMM 78-33-01
- [SDR VNAA20260501020](https://openairdocs.org/sdr/VNAA20260501020.md): Seat Track · corroded · Mar 23, 2026 · N617NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEVERAL POINTS SEAT RAIL BTW FS667 TO FS720.85 AND FS744.15 TO FS761.85 AT RBL15 CAB PAX. CORROSION ON SEVERAL POINTS SEAT RAIL BTW FS667 TO FS720.85 AND FS744.15 TO FS761.85 AT RBL15 CAB PAX WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ900 SRM 53-
- [SDR VNAA20260501019](https://openairdocs.org/sdr/VNAA20260501019.md): Fitting · corroded · Mar 23, 2026 · N617NN · Bombdr CL6002D15 · Fuselage, Equipment Attach Fittings
  > CORROSION ON FWD RH FITTING (1EA) UNDER WASTER CONTAINER AT FWD LAV. NEW FWD RH FITTING (1EA) UNDER WASTER CONTAINER AT FWD LAV WAS REPLACED SAFRAN CMM 25-40-40 REV. NO. 20
- [SDR VNAA20260501018](https://openairdocs.org/sdr/VNAA20260501018.md): Fitting · corroded · Mar 23, 2026 · N617NN · Bombdr CL6002D15 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-32-02
- [SDR VNAA20260501017](https://openairdocs.org/sdr/VNAA20260501017.md): Strip · corroded · Mar 22, 2026 · N617NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON METAL STRIP (LANDING DOOR), BTW STA FS 847 BTW STRINGER 20RH TO STRINGER 20LH, (UPPER/LWR AREA) WAS REWORKED AND FOUND OUT OF ALLOWABLE LIMITS. CORROSION ON METAL STRIP (LANDING DOOR), BTW STA FS 847 BTW STRINGER 20RH TO STRINGER 20LH, (UPPER/LW
- [SDR VNAA20260501016](https://openairdocs.org/sdr/VNAA20260501016.md): Lug · corroded · Mar 22, 2026 · N617NN · Bombdr CL6002D15 · Ailerons
  > AFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON INTERNAL FACE LUGS R1, R2, R3, R4, R5 AND R6 AT CENTER FITTING RH AILERONON. LUGS R3, R4 AND R6 AT CENTER FITTING RH AILERON WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND LUGS R1, R2 AND R5 WERE REPAIRED P
- [SDR VNAA20260501015](https://openairdocs.org/sdr/VNAA20260501015.md): Floor Support · cracked · Mar 20, 2026 · N617NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 220.00 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE. CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 220.00 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE WAS PER REO 690-53-11-2169 REV -.
- [SDR VNAA20260501001](https://openairdocs.org/sdr/VNAA20260501001.md): Bearing · excess play · Mar 19, 2026 · N617NN · Bombdr CL6002D15 · Vertical Stabilizer
  > FREE PLAY IN THE BEARINGS (2EA) OF THE CENTRAL HINGES OF THE RUDDER. FITTING #2 WAS REPLACED PER RIL #2103 REV.B AND BEARING ON FITTING #3 WAS REPLACED PER RIL #1213 REV. A.
- [SDR VNAA20260501021](https://openairdocs.org/sdr/VNAA20260501021.md): Fitting · worn · Mar 18, 2026 · N617NN · Bombdr CL6002D15 · Cargo/Baggage Doors
  > WEAR ON FITTING FROM STA FS 1051.30, STRINGER 12RH OF AFT BAGGAGE-BAY DOOR, WEAR ON FITTING FROM STA FS 1051.30, STRINGER 12RH WAS REPAIRED REO 690-53-61-1757 REV - -.
- [SDR VNAA20260501014](https://openairdocs.org/sdr/VNAA20260501014.md): Rib · cracked · Mar 18, 2026 · N617NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > CRACK ON MACHINED RIB OF LEADING EDGE SS 58.41 AT LH WING. CRACK ON MACHINED RIB OF LEADING EDGE SS 58.41 AT LT WING WAS REPAIRED PER REO 690-57-41-240 REV - -.
- [SDR VNAA20260501013](https://openairdocs.org/sdr/VNAA20260501013.md): Seat Track · corroded · Mar 18, 2026 · N617NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACKS OF AFT BAGGAGE -BAY,BETWEEN THE COORDINATES RBL9 TO RBL27,AND LBL7 TO LBL27,BTW STA FS 1000 TO STA 1069. CORROSION ON SEAT TRACKS OF AFT BAGGAGE -BAY,BETWEEN THE COORDINATES RBL9 TO RBL27,AND LBL7 TO LBL27,BTW STA FS 1000 TO STA
- [SDR VNAA20260501012](https://openairdocs.org/sdr/VNAA20260501012.md): Seat Track · corroded · Mar 17, 2026 · N617NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEVERAL POINTS SEAT RAIL BTW 364.00 TO FS409.00 AT LBL09 CAB PAX. CORROSION ON SEVERAL POINTS SEAT RAIL BTW 364.00 TO FS409.00 AT LBL09 CAB PAX WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ900 AMM
- [SDR VNAA20260501011](https://openairdocs.org/sdr/VNAA20260501011.md): Seat Track · corroded · Mar 17, 2026 · N617NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEVERAL POINTS SEAT RAIL BTW FS785.15 TO FS847.00+16.00 AND FS847+48.00 TO FS881.00 AT RBL15 CAB PAX. SEAT TRACK BTW FS785.15 TO FS847.00+16.00 AND FS847+48.00 TO FS881.00 AT RBL15 CAB PAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A
- [SDR VNAA20260501010](https://openairdocs.org/sdr/VNAA20260501010.md): Seat Track · corroded · Mar 17, 2026 · N617NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEVERAL POINTS SEAT RAIL BTW FS693 TO FS720.85 AND FS785.15 AT LBL15 CAB PAX. SEAT TRACK BTW FS693 TO FS720.85 AND FS785.15 AT LBL15 CAB PAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02 AND REPLACED IAW AMM 53-00-49 (CONFIG A12).
- [SDR VNAA20260501009](https://openairdocs.org/sdr/VNAA20260501009.md): Seat Track · corroded · Mar 17, 2026 · N617NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON RH SIDE SEAT RAIL (1EA) BTW STA FS 661+16 TO STA FS 669.40. CORROSION ON RH SIDE SEAT RAIL (1EA) BTW BS 661+16 TO BS 669.40 WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-31-49-101-001-A02 AND REPLACED PER AMM 53-00-49-400-801-A12.
- [SDR VNAA20260501008](https://openairdocs.org/sdr/VNAA20260501008.md): Seat Track · corroded · Mar 17, 2026 · N617NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > WEAR ON LH SIDE SEAT RAIL (1EA),BTW STA FS 379 TO STA FS 469.00,AND WEAR LH SIDE SEAT RAIL (1EA) BTW STA FS 469.00 TO STA FS 581,ALSO WEAR LH SIDE SEAT RAIL (1EA) BTW STA FS 581 TO STA FS 661+16. AND CORROSION ON WEAR LH SIDE SEAT RAIL (2EA) BTW STA FS 661+16
- [SDR VNAA20260501007](https://openairdocs.org/sdr/VNAA20260501007.md): Web · cracked · Mar 15, 2026 · N617NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF ATTACHMENT AREA OF ADG RESTOW PUMP. CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF ATTACHMENT AREA OF ADG RESTOW PUMP WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01
- [SDR VNAA20260501006](https://openairdocs.org/sdr/VNAA20260501006.md): Skin · dented · Mar 15, 2026 · N617NN · Bombdr CL6002D15 · Fuselage Structure (General)
  > FUSELAGE SKIN DENT WITHIN 6341.13 FH AFTER SECTION I, REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. DENT DAMAGE ON FUSELAGE SKIN BTW FS942.00 - FS954.00 AND STR21L - STR22L WAS REPAIRED PER CRJ-900 REO 690-53-51-539 REV.--
- [SDR VNAA20260501005](https://openairdocs.org/sdr/VNAA20260501005.md): Hinge · scratched · Mar 14, 2026 · N617NN · Bombdr CL6002D15 · Fuselage, Door Hinge
  > WEAR ON LUG LAND AT PIANO HINGE PASSENGER DOOR. LUG LAND AT PIANO HINGE PASSENGER DOOR WAS REPAIRED WITH INSPECTION REQUIREMENTS FOR TYPE REPAIR IV: THRESHOLD 5,700 FLIGHT CYCLES AND REPEAT WITH 5,700 FLIGHT CYCLES PER REO 670-53-21-582 REV.-G.
- [SDR VNAA20260501004](https://openairdocs.org/sdr/VNAA20260501004.md): Hinge · scratched · Mar 14, 2026 · N617NN · Bombdr CL6002D15 · Fuselage, Door Hinge
  > SCRATCHES ON SEVERAL POINTS AT PIANO HINGE LUGS PASSENGER DOOR. PIANO HINGE LUGS PASSENGER DOOR WAS REPAIRED WITH INSPECTION REQUIREMENTS FOR TYPE REPAIR I: THRESHOLD 5,700 FLIGHT CYCLES AND REPEAT WITH 5,700 FLIGHT CYCLES PER REO 670-53-21-582 REV.-G.
- [SDR VNAA20260501003](https://openairdocs.org/sdr/VNAA20260501003.md): Door · cracked · Mar 14, 2026 · N617NN · Bombdr CL6002D15 · Emergency Exits
  > CRACK ON TOP EDGE MEMBER AT LH AFT EMERGENCY EXIT DOOR. TOP EDGE MEMBER AT LH AFT EMERGENCY EXIT DOOR WAS REPAIRED PER REO 670-52-21-103 REV-.
- [SDR VNAA20260501002](https://openairdocs.org/sdr/VNAA20260501002.md): Drag Angle · cracked · Mar 12, 2026 · N617NN · Bombdr CL6002D15 · Vertical Stabilizer
  > CRACK ON AFT DRAG ANGLE OF LH VERTICAL STABILIZER. CRACK ON AFT DRAG ANGLE OF LH VERTICAL STABILIZER WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
- [SDR VNAA2026031013701](https://openairdocs.org/sdr/VNAA2026031013701.md): Frame · bent · Mar 6, 2026 · N617NN · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT FS280 BENT BETWEEN STR19R AND 20R / COMPLETED PERMANENT REPAIR OF FRAME 280.00 SPLICE REPAIR AT STR22 IAW REPAIR ENGINEERING ORDER (REO) 690-53-11-2071. NO ADDITIONAL DEFECTS NOTED AT THIS TIME.
- [SDR VNAA2026031013903](https://openairdocs.org/sdr/VNAA2026031013903.md): Not Reported · not reported · Mar 6, 2026 · N617NN · Cndair CL6002D24 · Fuselage Structure (General)
  > FUSELAGE STRUCTURE BETWEEN FS333.0 - FS265.0 AND STR 17R- 26R. / PERFORMED REPAIR IAW REPAIR ENGINEERING ORDER (REO) 690-53-00-638.
- [SDR VNAA2026031013802](https://openairdocs.org/sdr/VNAA2026031013802.md): Crossbeam · damaged · Mar 6, 2026 · N617NN · Cndair CL6002D24 · Fuselage Main, Structure
  > REO 690-53-21- 2052 REPAIR TO CROSSBEAM FS 295 BETWEEN RBL 37 AND RBL 45 REQUIRES FINAL DISPOSITION / COMPLETED PERMANENT REPAIR IAW REPAIR ENGINEERING ORDER (REO) 690-53-21-2052. NO ADDITIONAL DEFECTS NOTED AT THIS TIME.
- [SDR VNAA2024112611102](https://openairdocs.org/sdr/VNAA2024112611102.md): Service Door · ground damage · Nov 24, 2024 · N617NN · Cndair CL6002D24 · Fluid Service Doors
  > OUTER LAV DOOR IMPACTED BY LAV CART (AFT LAV) / PERFORMED PERMANENT REPAIR IAW REO 690-53-51-442.

## 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 = 'N617NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N617NN/reports

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