# Service difficulty reports: N645NN

A list on [N645NN](https://openairdocs.org/aircraft/N645NN.md).

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

- [SDR VNAA2026062920505](https://openairdocs.org/sdr/VNAA2026062920505.md): Tiller · faulted · Jun 27, 2026 · N645NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP MSG IN FLIGHT. REMOVED AND REPLACED PILOT HAND TILLER IAW AMM 32-51-01-000/400-801-A01. OPS CHECKED GOOD.
- [SDR VNAA202601170008](https://openairdocs.org/sdr/VNAA202601170008.md): Access Panel · corroded · Jan 3, 2026 · N645NN · Cndair CL6002D24 · Wing, Plate/Skin
  > CORROSION ON ACCESS PANELS 542AZ 542BZ 642AZ AND 642BZ CORRODED ON ACCESS PANELS WERE REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED OUT OF LIMITS IAW SRM 53-00-00-101-001-A01 AND ACCESS PANELS 542AZ, 542BZ, 642AZ AND 642BZ WERE REPLACED AN
- [SDR VNAA202601180019](https://openairdocs.org/sdr/VNAA202601180019.md): Skin · damaged · Nov 27, 2025 · N645NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > IN REFERENCE TO: TASKCARD TRFKE00FCUS8, 8000FH PERM-REPAIR FUSELAGE SKIN LIGHTNING STRIKE DAMAGE ON SKIN ONLY (NO FASTENER AT DAMAGE LOCATION) WITHIN 8000FH, ACCOMPLISH PERMANENT REPAIR OF TEMP REPAIR PER 670-53-00-045 SECTION 1 PARAGRAPH B3. SEE ATTACHMENTS F
- [SDR VNAA202601180018](https://openairdocs.org/sdr/VNAA202601180018.md): Skin · corroded · Nov 27, 2025 · N645NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > IN REFERENCE TO: TASKCARD TRFKE00FCUS8, 8000FH PERM-REPAIR FUSELAGE SKIN LIGHTNING STRIKE DAMAGE ON SKIN ONLY (NO FASTENER AT DAMAGE LOCATION) WITHIN 8000FH, ACCOMPLISH PERMANENT REPAIR OF TEMP REPAIR PER 670-53-00-045 SECTION 1 PARAGRAPH B3. SEE ATTACHMENTS F
- [SDR VNAA202601180017](https://openairdocs.org/sdr/VNAA202601180017.md): Fitting · corroded · Nov 23, 2025 · N645NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR FITTING ON ACCESS 104 (1EA) AISLE SIDE AND BEHIND ACCESS 105B (1 EA) ON GALLEY 1. FLOOR FITTING ON ACCESS 104 AISLE SIDE AND BEHIND ACCESS 105B ON GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-32-02
- [SDR VNAA202601180016](https://openairdocs.org/sdr/VNAA202601180016.md): Plate · corroded · Nov 21, 2025 · N645NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > CORROSION AROUND FASTENER HOLE ON AFT CORNER OF THE LOWER PLATE OF CENTER BAGGAGE-BAY DOOR SEAL. LOWER PLATE OF CENTER BAGGAGE-BAY DOOR SEAL WAS EVALUATE FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACE PER CRJ-900 SRM 51-41-02-001-001-
- [SDR VNAA202601180015](https://openairdocs.org/sdr/VNAA202601180015.md): Hinge Fitting · corroded · Nov 20, 2025 · N645NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > CORROSION WAS FOUND AT CENTER HINGE FITTING ASSY LUGS #L1, #L2, #L3, #L4, #L5 AND #L6 (6 EA´S). ALSO ON AILERON HINGE FITTING #1 (1EA). FITTING #1 (1EA) AND L3, L4 OF CENTER HINGE FITTING (2EAS) AT LH AILERON WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A0.
- [SDR VNAA202601180013](https://openairdocs.org/sdr/VNAA202601180013.md): Hinge Fitting · corroded · Nov 18, 2025 · N645NN · Cndair CL6002D24 · Ailerons
  > AFTER BUSHINGS REMOVAL, CORROSION WAS NOTED ON RIGHT AILERON LUGS R1, R2, R5 AND R6. RIGHT AILERON LUGS R1, R2, R5 AND R6 WERE REPAIRED PER REO 670-57-61-237 REV. --
- [SDR VNAA202601180012](https://openairdocs.org/sdr/VNAA202601180012.md): Strap · cracked · Nov 15, 2025 · N645NN · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESSPANEL 193AB. SUPPORT STRUCTURE STRAP FAIRING ACCESS PANEL 193AL AND 193AR WERE REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01
- [SDR VNAA202601180010](https://openairdocs.org/sdr/VNAA202601180010.md): Bracket · corroded · Nov 15, 2025 · N645NN · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION ON INTERNAL ANGLES OF REFUEL/DEFUEL CONTROL PANEL SUPPORT STRUCTURE. CORROSION ON INTERNAL ANGLE P/N: CC670-39182-8 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-01-101- 001-A01 AND ANGLE 1EA (BR
- [SDR VNAA202601180020](https://openairdocs.org/sdr/VNAA202601180020.md): Bracket · corroded · Nov 14, 2025 · N645NN · Cndair CL6002D24 · Wing, Attach Fittings
  > CORROSION ON SUPPORT LINES WS 38 AT LH TRUNNION AREA WAS FOUND. SUPPORT LINES WS 38 AT LH TRUNNION WAS EVALUATED PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
- [SDR VNAA202601180014](https://openairdocs.org/sdr/VNAA202601180014.md): Support Fitting · corroded · Nov 14, 2025 · N645NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON NO. 2 AND 3 HYDRAULIC TUBES-FITTING SUPPORT, AFT OF RIGHT OUTER WING REAR SPAR AT WS24.50. FITTING SUPPORT, AFT OF RIGHT OUTER WING REAR SPAR AT WS24.50 WAS EVALUATE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ 900 SRM 51-42-06 001-
- [SDR VNAA202601180009](https://openairdocs.org/sdr/VNAA202601180009.md): Landing · cracked · Nov 14, 2025 · N645NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH HOUSING CUT OUT OF ACCESS DOOR 212AR). LATCH HOUSING ON AFT RH DOOR LANDING AT FS 188.00 (CUT OUT OF ACCESS DOOR 212AR) WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-10-001-001-A01
- [SDR VNAA202601180008](https://openairdocs.org/sdr/VNAA202601180008.md): Rib · cracked · Nov 14, 2025 · N645NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACKED WING RIB FLS168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. WING RIB FLS168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-492 REV - -
- [SDR VNAA202601180007](https://openairdocs.org/sdr/VNAA202601180007.md): Floorbeam · corroded · Nov 14, 2025 · N645NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK ON FLOOR BEAM RBL 12.0 BTW FS221.73-FS229.00 AT FWD FUSELAGE INTERNAL STRUCTURE. FLOORBEAM RBL 12.0 BTW FS221.73-FS229.00 AT FWD FUSELAGE INTERNAL STRUCTURE WAS REPAIRED PER REO 690-53-11-2086 REV. - -
- [SDR VNAA202601180006](https://openairdocs.org/sdr/VNAA202601180006.md): Fitting · corroded · Nov 14, 2025 · N645NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FITTINGS (2EA) BTW STA FS 280 TO STA FS 295 AND RBL 16 TO RBL 38.AND CORROSION ON FITTINGS (2EA) BTW STA 364 TO STA FS 379 AND LBL 13 TO LBL 40 APPROXIMATELY. FITTINGS (4EAS). BTW STA FS 280 TO STA FS 295 AND RBL 16 TO RBL 38 AND BTW STA 364 TO S
- [SDR VNAA202601180005](https://openairdocs.org/sdr/VNAA202601180005.md): Seat Track · corroded · Nov 14, 2025 · N645NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS RBL9; (4E/A) FROM FS581 TO FS977 AT PAX CABIN. CORRECTIVE ACTION: WERE EVALUATED, DUE TO EXCESSIVE DAMAGE ON SEAT RAILS RBL9; (3E/A) FROM FS581 TO FS 847+16 AT PAX CABIN PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-9
- [SDR VNAA202601180004](https://openairdocs.org/sdr/VNAA202601180004.md): Seat Track · corroded · Nov 14, 2025 · N645NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS LBL9; (1E/A) FROM FS377 TO FS485, (1E/A) FROM FS581 TO FS661+32 AND (3E/A) FROM FS677 TO FS1000 AT PAX CABIN. DUE TO EXCESSIVE DAMAGE ON SEAT RAILS LBL9; (1E/A) FROM FS377 TO FS485, (1E/A) FROM FS581 TO FS661+32 AND (3E/A) FROM F
- [SDR VNAA202601180003](https://openairdocs.org/sdr/VNAA202601180003.md): Seat Track · corroded · Nov 14, 2025 · N645NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAILS; (5E/A) FROM FS483 TO FS720, (1E/A) FROM FS744 TO FS761, (1E/A) FROM FS785 TO FS852 AND (2E/A) FROM FS847+19 TO FS969 AT PAX CABIN. LH SIDE SEAT RAILS (5E/A) FROM FA483 TO FS720, (1E/A) FROM FS744 TO FS761, (1E/A) FROM FS785 TO
- [SDR VNAA202601180002](https://openairdocs.org/sdr/VNAA202601180002.md): Seat Track · corroded · Nov 14, 2025 · N645NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAILS; (4E/A) FROM FS379 TO FS661+14, (1E/A) FROM FS744 TO FS761, (1E/A) FROM FS785 TO FS852 AND(2E/A) FROM FS847+19 TO FS969 ATPAX CABIN. CORROSION ON RH SIDE SEAT RAILS; (4E/A) FROM FS379 TO FS661+14, (1E/A) FROM FS744 TO FS761, (1
- [SDR VNAA202601170011](https://openairdocs.org/sdr/VNAA202601170011.md): Skin · corroded · Nov 14, 2025 · N645NN · Cndair CL6002D24 · Trailing Edge Flaps
  > CORROSION ON INNER SKIN TRAILING EDGE OF LH WING BTW STA BL45 TO STA WS 38, AND CORROSION ON INTERCOSTAL (2EA) OF LH WING T. EDGE BTW STA BL45 TO STA WS 38. CORROSION ON INNER SKIN TRAILING EDGE OF LH WING BTW STA BL45 TO STA WS 38 WAS REPAIRED PER REO 690-57
- [SDR VNAA202601180001](https://openairdocs.org/sdr/VNAA202601180001.md): Intercostal · corroded · Nov 13, 2025 · N645NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL (STRINGER 26L, STGR 27L, STGR 27R) BTW F.S. 349.00 AND F.S. 364.00 AT AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL (STRINGER 26L,) BTW F.S. 349.00 AND F.S. 364.00 AT AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-00
- [SDR VNAA202601170020](https://openairdocs.org/sdr/VNAA202601170020.md): Door Sill · corroded · Nov 13, 2025 · N645NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON LOWER SILL AT AFT DOOR CARGO COMPARTMENT. LOWER SILL AT AFT DOOR CARGO COMPARTMENT WAS EVALUATE FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-4
- [SDR VNAA202601170019](https://openairdocs.org/sdr/VNAA202601170019.md): Angle · corroded · Nov 13, 2025 · N645NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON KICKPLATE ANGLE AND ON MID CAP ANGLE FROM FS310 TO FS 349 AT PASSENGER DOOR SURROUND STRUCTURE. KICKPLATE ANGLE AND ON MID CAP ANGLE FROM FS310 TO FS 349 AT PASSENGER DOOR SURROUND STRUCTURE WERE EVALUATED FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 5
- [SDR VNAA202601170017](https://openairdocs.org/sdr/VNAA202601170017.md): Drip Tray · corroded · Nov 13, 2025 · N645NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON DRAIN CHANNELS (2 EAS) FS281.00 LBL14.00 AND RBL14.00 AT PAX CABIN. CORROSION WAS REMOVED ON DRAIN CHANNEL RH (1 EA) ON FS281.00 AT PAX CABIN PER CRJ 900 SRM 51-21-06-001-001-A01 AND EVALUATED THEREFORE IT IS WITHIN LIMITS PER CRJ-900 SRM 53-21
- [SDR VNAA202601170016](https://openairdocs.org/sdr/VNAA202601170016.md): Bracket · corroded · Nov 13, 2025 · N645NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS FS514.00, FS565.00, FS626.00, FS661.00 + 9.00 BTW STGR 26LH & 27 AND BTW STGR 22LH & STGR 23LH AND FS652.00 STGR 24RH & 25RH AT FWD/CENTER BAGGAGE BAY COMPARTMENT. BRACKETS FS514.00 BTW STGR 26LH & 27 AND FS514.00, FS565.00, FS626.00,
- [SDR VNAA202601170012](https://openairdocs.org/sdr/VNAA202601170012.md): Fitting · corroded · Nov 13, 2025 · N645NN · Cndair CL6002D24 · Wing, Attach Fittings
  > CORROSION ON RH/LH FITTINGS SUPPORTS OF CONECTORS PX10J1/PX02J1, PX09J1/PX01J1 AT MLG WHEEL WELL. RH/LH FITTINGS SUPPORTS OF CONECTORS PX10J1/PX02J1, PX09J1/PX01J1 AT MLG WHEEL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
- [SDR VNAA202601170010](https://openairdocs.org/sdr/VNAA202601170010.md): Nut Plate · corroded · Nov 13, 2025 · N645NN · Cndair CL6002D24 · Wing, Attach Fittings
  > CORROSION ON NUT STRIPS (2 E/A'S) AT UPPER AREA OF LH/RH WHEEL WELL AREA (APROX. RBL/LBL 49). NUT STRIPS (2 E/A'S) AT UPPER AREA OF LH/RH WHEEL WELL AREA (APROX. RBL/LBL 49) WERE EVALUATED FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLAC
- [SDR VNAA202601170009](https://openairdocs.org/sdr/VNAA202601170009.md): Angle · corroded · Nov 13, 2025 · N645NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CORROSION ON SETTLEMENT ANGLE OF ACCESS PANEL642AZ AT RH WING. SETTLEMENT ANGLE OF ACCESS PANEL 642AZ AT RH WING WAS EVALUATED FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER SRM 51-42-21-001-001-A01
- [SDR VNAA202601170006](https://openairdocs.org/sdr/VNAA202601170006.md): Angle · corroded · Nov 13, 2025 · N645NN · Cndair CL6002D24 · Wing, Landing Gear Attach Fittings
  > CORROSION ON ATTACHMENT POINT ANGLE OF SIDE STAY BONDING JUMPER AT LH MLG WHEEL WELL. ATTACHMENT POINT ANGLE OF SIDE STAY BONDING JUMPER AT LH MLG WHEEL WELL WAS EVALUATE FOUND TO EXCESSIVE DAMAGE PER CRJ900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900
- [SDR VNAA202601170004](https://openairdocs.org/sdr/VNAA202601170004.md): Shim · corroded · Nov 13, 2025 · N645NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON SHIMS OF DOOR HINGES OF LP GROUND CONNECTION ACCESS DOOR AT AFT FUSELAGE. SHIMS OF DOOR HINGES OF LP GROUND CONNECTION ACCESS DOOR AT AFT FUSELAGE WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR VNAA202601170003](https://openairdocs.org/sdr/VNAA202601170003.md): Hinge · corroded · Nov 13, 2025 · N645NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGE (1E/A) OF REFUEL ACCESS DOOR AT FWD LOWER FUSELAGE. HINGE (1E/A) OF REFUEL ACCESS DOOR AT FWD LOWER FUSELAGE WAS EVALUATED FOUND TO EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND
- [SDR VNAA202601170015](https://openairdocs.org/sdr/VNAA202601170015.md): Rib · cracked · Nov 11, 2025 · N645NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING. MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV - -
- [SDR VNAA202601170018](https://openairdocs.org/sdr/VNAA202601170018.md): Stringer · corroded · Nov 10, 2025 · N645NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR AND STAND-OF ON 26LH BTW FS295.00 TO FS310.00 AT E&E BAY.:STRINGER AND STAND-OFF WAS EVALUATED AND FOUND TO EXCESSIVE DAMAGE CRJ-900 SRM 53-21-03-101-002-A04 AND SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ900 SRM 51-42-13-001-001-A01 AND
- [SDR VNAA202601170014](https://openairdocs.org/sdr/VNAA202601170014.md): Angle · corroded · Nov 10, 2025 · N645NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CORROSION ON RH/LH MLG BIN SUPPORTS (6EA) BTW STA FS 693 TO STA FS847 AND CORROSION ON GUSSET (4EA) BTW STA FS 693 TO STA FS847,AND CORROSION ON FAIRING SUPPORT (4EAS) BTW STA FS 732 TO STA FS 752. CORROSION ON RH/LH MLG BIN SUPPORTS (3EA) BTW STA FS 693 TO S
- [SDR VNAA202601170013](https://openairdocs.org/sdr/VNAA202601170013.md): Angle · corroded · Nov 10, 2025 · N645NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CORROSION ON FAIRING SUPPORTS (SETTLEMENTS AREA, LOWER/UPPER) BTW STA FS847.00 TO STA FS881 BTW STR 18RH TO STR 18LH AND CORROSION ON FAIRING SUPPORT MEMBRANES BTW STA FS 847.00 TO STA FS881 AND BTW STR 25RH TO STR25LH. DUE TO EXCESSIVE DAMAGE ON ANGLE SUPPO
- [SDR VNAA202601180011](https://openairdocs.org/sdr/VNAA202601180011.md): Floorbeam · cracked · Nov 8, 2025 · N645NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2088 REV - -
- [SDR VNAA202601170007](https://openairdocs.org/sdr/VNAA202601170007.md): Diaphragm · corroded · Nov 8, 2025 · N645NN · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CORROSION ON DIAPHRAGM FAIRINGS IN STA FS 797.00 AND RBL/LBL 34 AT RH/LH MLG WHEEL WELL. DIAPHRAGM FAIRINGS IN STA FS 797.00 AND RBL/LBL 34 AT RH/LH MLG WHEEL WELL WERE EVALUATE FOUND TO EXCESSIVE DAMAGE PER CRJ900 SRM 51-10-06-001-001-A01 AND REPLACED PER C
- [SDR VNAA202601170005](https://openairdocs.org/sdr/VNAA202601170005.md): Support · corroded · Nov 8, 2025 · N645NN · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > CORROSION ON MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AND ON CONNECTORS SUPPORT PLATE (PX33, PX17, PX34, PX19) AT RH/LH WHEEL WELL AREA. MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AND ON CONNECTORS SUPPORT PLATE (PX33, PX17,
- [SDR VNAA202601170002](https://openairdocs.org/sdr/VNAA202601170002.md): Skin · dented · Nov 7, 2025 · N645NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL FUSELAGE SKIN BTW FS 477.40 TO FS 501.00 BTW STGR 17 LH TO STGR 18 LH. DENT ON EXTERNAL FUSELAGE SKIN BTW FS 477.40 TO FS 501.00 BTW STGR 17 LH TO STGR 18 LH WAS REPAIRED PER REO 670-51-00-085 REV - A AND REO 690-53-31-1091 REV - -
- [SDR VNAA202601170001](https://openairdocs.org/sdr/VNAA202601170001.md): Skin · dented · Oct 4, 2025 · N645NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW FS 1015.00 TO FS 1031.00 BTW STGR 20 LH TO STGR 23 LH. SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW FS 1015.00 TO FS 1031.00 BTW STGR 20 LH TO STGR 23 LH WERE REPAIRED PER REO 670-51-00-085 REV - A AND REO 690-53-61

## 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 = 'N645NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N645NN/reports

---
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