# Service difficulty reports: N606NN

A list on [N606NN](https://openairdocs.org/aircraft/N606NN.md).

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

- [SDR VNAA2026060518401](https://openairdocs.org/sdr/VNAA2026060518401.md): Shutoff Valve · unserviceable · Jun 1, 2026 · N606NN · Cndair CL6002D24 · Compressor Bleed Valve
  > L BLEED CAUTION MSG IN FLIGHT / FOUND B1 006926 T/S IAW FIM 36-12-01-810-805. REMOVED AND REPLACED LH HPSOV IAW CRJ900 AMM 36-12-05-000/400-801. OPS CHECK GOOD, LEAK CHECK GOOD.
- [SDR VNAA202606060017](https://openairdocs.org/sdr/VNAA202606060017.md): Lug · corroded · May 19, 2026 · N606NN · Cndair CL6002D24 · Ailerons
  > CORROSION WAS FOUND ON LUG BORE #5 OF LH AILERON. REPAIRED PER REO 670-57-61-237 REV.-.
- [SDR VNAA202606060015](https://openairdocs.org/sdr/VNAA202606060015.md): Fitting · corroded · May 7, 2026 · N606NN · 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 IAW CMM 25-33-21.
- [SDR VNAA202606060016](https://openairdocs.org/sdr/VNAA202606060016.md): Fitting · corroded · Apr 29, 2026 · N606NN · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > CORROSION ON FWD RT FITTING (1EA) UNDER WASTER CONTAINER AT FWD LAV. FWD RT FITTING (1EA) UNDER WASTER CONTAINER AT FWD LAV WAS REPLACED PER SAFRAN CMM 25-40-19
- [SDR VNAA202606060014](https://openairdocs.org/sdr/VNAA202606060014.md): Acoustic Liner · cracked · Apr 24, 2026 · N606NN · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > AFTER Z STIFFENER REMOVAL ON LOWER RH TRANSCOWL CRACK WAS FOUND ON ACOUSTIC PANEL. LOWER RH TRANSCOWL ON ACOUSTIC PANEL WAS REPAIRED PER REO NUMBER 690-54-21-635 REV - -
- [SDR VNAA202606060013](https://openairdocs.org/sdr/VNAA202606060013.md): Bracket · corroded · Apr 24, 2026 · N606NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET MACHINED (10 EAS) BTW FS=517.00 TO FS=661.00+16 AT FWD/CENTER BAGGAGE BAY. PAINT ON BRACKET MACHINED BTW FS=517.00 TO FS=661.00+16 AT FWD/CENTER BAGGAGE BAY WAS REMOVED PER SRM 51-26-01-001-001-A01, GVI WAS PERFORMED PER NDTM TASK 51-20
- [SDR VNAA202606060012](https://openairdocs.org/sdr/VNAA202606060012.md): Seat Track · corroded · Apr 24, 2026 · N606NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND WEAR ON SEAT RAIL BTW FS349 TO FS 669 3EA LBL 27, 2EA LBL9, 4EA RBL9 AT FLOOR PASSENGER CABIN. WERE EVALUATED,DUE EXCESIVE DAMAGE ON SEAT RAIL BTW FS349 TO FS 669 3EA LBL 27, 2EA LBL 9, 4EA RBL 9 AT FLOOR PASSENGER CABIN PER CRJ-900 SRM 53-21-49
- [SDR VNAA202606060009](https://openairdocs.org/sdr/VNAA202606060009.md): Channel · cracked · Apr 24, 2026 · N606NN · Cndair CL6002D24 · Aerodynamic Fairings
  > CRACK AT INNER STRAP,AFT C-CHANNEL ALONG AFT WING-TO-FUSELAGE FAIRING 195DL. CRACK AT INNER STRAP,AFT C-CHANNEL ALONG AFT WING-TO-FUSELAGE FAIRING 195DL WAS REPLACED PER CRJ-900 NIEO 34 REV. 2009-01.
- [SDR VNAA202606060011](https://openairdocs.org/sdr/VNAA202606060011.md): Seat Track · cracked · Apr 23, 2026 · N606NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON SEAT RAIL BTW FS379 TO FS394 RBL 9 AT FLOOR PASSENGER CABIN. EVALUATED, DUE EXCESIVE DAMAGE ON SEAT RAIL BTW FS360 TO FS485 RBL9 AT FLOOR PASSENGER CABIN PER CRJ-900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ900 AMM 53-00-49.
- [SDR VNAA202606060010](https://openairdocs.org/sdr/VNAA202606060010.md): Rib · cracked · Apr 22, 2026 · N606NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON RIB LEADING EDGE SS57.16 AT LH WING. REPAIRED PER REPAIR PER REO 690-57-41-240 REV. - -
- [SDR VNAA202606060008](https://openairdocs.org/sdr/VNAA202606060008.md): Web · cracked · Apr 21, 2026 · N606NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR WEB RIGHT SIDE(BELOW ADG PUMP SUPPORT) FS193.00 AT ELECTRICAL BAY. CRACK ON FLOOR WEB RIGHT SIDE(BELOW ADG PUMP SUPPORT) FS193.00 AT ELECTRICAL BAY WAS REPAIRED PER SRM 53-11-43-201-001-A01.
- [SDR VNAA202606060007](https://openairdocs.org/sdr/VNAA202606060007.md): Bracket · cracked · Apr 21, 2026 · N606NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK FWD BRACKET SUPPORT OF UPPER ACCUMULATOR. CRACK FWD BRACKET SUPPORT OF UPPER ACCUMULATOR AT FWD EQUIPMENT COMPARTMENT WAS REPLACED CRJ-900 SRM 51-42-21-001-001-A01 AND SRM 51-41-02-001-001-A01.
- [SDR VNAA202606060006](https://openairdocs.org/sdr/VNAA202606060006.md): Bracket · cracked · Apr 21, 2026 · N606NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FWD/AFT INBD/OTBD CORNER OF BOX JB6 SUPPORT STRUCTURE AT FWD EQUIPMENT COMPARTMENT. BRACKET ASSY OF BOX JB6 SUPPORT STRUCTURE AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.
- [SDR VNAA202606060005](https://openairdocs.org/sdr/VNAA202606060005.md): Bracket · cracked · Apr 20, 2026 · N606NN · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED UPPER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH PYLON ACCESS PANEL 443BT AT RH PYLON. REPLACED PER SRM 51-42-06-001-001-A01.
- [SDR VNAA202606060004](https://openairdocs.org/sdr/VNAA202606060004.md): Structure · cracked · Apr 19, 2026 · N606NN · Cndair CL6002D24 · Emergency Exits
  > CRACKED TOP EDGE MEMBER AT RH FWD EMERGENCY EXIT. TOP EDGE MEMBER AT RH AFT EMERGENCY EXIT WAS REPAIRED PER REO 670-52-21-103 REV --.
- [SDR VNAA202606060003](https://openairdocs.org/sdr/VNAA202606060003.md): Skin · damaged · Apr 18, 2026 · N606NN · Cndair CL6002D24 · Trailing Edge Flaps
  > NICKS & DENTS ON LOWER SKIN OF LT INBD FLAP BTW FLS 15.00 TO FLS 75.6. NICKS ON LOWER SKIN OF LT INBD FLAP BTW FLS 48.00 TO FLS 75.60 WAS BLEND OUT IAW SRM 51-12-00-001-001-A01 & EVALUATED WITHIN OF LIMITS PER SRM 57-52-01-201-005-A01 AND LOWER SKIN OF LT IN
- [SDR VNAA202606060002](https://openairdocs.org/sdr/VNAA202606060002.md): Striker · dented · Apr 18, 2026 · N606NN · Cndair CL6002D24 · Fuselage Main, Structure
  > 1605FH PERM REPAIR - REPAIR TO PAX DOOR SEAL STRIKER - EXTENSION TO SRM 53-21-23-201-004-A01. PAX DOOR SEAL STRIKER WAS REPAIRED PER SRM 53-21-23-201-006-A01.
- [SDR VNAA202606060001](https://openairdocs.org/sdr/VNAA202606060001.md): Skin · damaged · Apr 18, 2026 · N606NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE TO FUSELAGE SKINS BETWEEN FS234.00 - FS364.00 AND BETWEEN STR 20L - STR24L. REPAIRED PER REO 690-53-00-656 REV -A AND REO 690-53-21-2139 REV -.
- [SDR VNAA2024110111101](https://openairdocs.org/sdr/VNAA2024110111101.md): Probe · unserviceable · Oct 30, 2024 · N606NN · Cndair CL6002D24 · Landing Gear Brake System
  > BRAKE OVERHEAT WARNING MSG AFTER TAKEOFF LHOB SPIKED TO 20. TEMP CAME TO APPROX.3 / REMOVED AND REPLACED LHOB BTMS IAW CRJ900 AMM 32-46-01-000/400-801-A01-PSA. SELF TEST GOOD. NO DEFECTS NOTED AT THIS TIME.
- [SDR VNAA2023112111101](https://openairdocs.org/sdr/VNAA2023112111101.md): Sensor · unknown · Nov 19, 2023 · N606NN · Cndair CL6002D24 · Landing Gear Brake System
  > BRAKE OVERHEAT WARNING IN FLIGHT RAN QRC/QRH RHIB FLUCTUATING WITH GEAR UP AND DOWN / REMOVED AND REPLACED R/H I/B BRAKE TEMP SENSOR IAW CRJ 900 AMM 32-46-01-000/400-801-A01-PSA. OPS CHECK GOOD.
- [SDR VNAA202308311113](https://openairdocs.org/sdr/VNAA202308311113.md): Unknown · unknown · Aug 30, 2023 · N606NN · Cndair CL6002D24 · Wing, Plate/Skin
  > DURING ROUTINE OPERATIONS AT PENSACOLA FL (PNS), MX REPORTS TYPE 3 LIGHTNING STRIKE DAMAGE TO THE RH WINGLET LWR SKIN DAMAGE REPORTED AT APPROX. 0.140€? L X 0.110€? W X 0.005€? D. PERM REPAIR IAW EA23-C9-57-1157 REV A TO LIGHTNING STRIKE DAMAGE TO LOWER RH
- [SDR VNAA202304290001](https://openairdocs.org/sdr/VNAA202304290001.md): Drag Angle · cracked · Apr 21, 2023 · N606NN · Cndair CL6002D24 · Vertical Stabilizer
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00)
- [SDR VNAA202304290004](https://openairdocs.org/sdr/VNAA202304290004.md): Seat Track · corroded · Apr 16, 2023 · N606NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL LH BTW FS 744.15 TO FS 761.85 AND STGR 15LH
- [SDR VNAA202304290003](https://openairdocs.org/sdr/VNAA202304290003.md): Seat Track · corroded · Apr 10, 2023 · N606NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL RBL9.00 BETWEEN FS421.00-FS469.00
- [SDR VNAA202304290005](https://openairdocs.org/sdr/VNAA202304290005.md): Hinge · corroded · Apr 6, 2023 · N606NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGE AT UPPER STAIR PASSENGER DOOR
- [SDR VNAA202304290002](https://openairdocs.org/sdr/VNAA202304290002.md): Drag Angle · cracked · Apr 6, 2023 · N606NN · Cndair CL6002D24 · Vertical Stabilizer
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00)
- [SDR VNAA202208251111](https://openairdocs.org/sdr/VNAA202208251111.md): Skin · damaged · Aug 22, 2022 · N606NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSE SKIN BLENDS FS240 & FS280, STR25R €“ STR26R. TWO SEPARATE DAMAGES ON BELLY AT FS 240 AND FS280 REQUIRED TEMP REPAIR AFTER BLENDING. C/W EA 22-C9-53-1012, REV IR FOR PERMANENT REPAIR.
- [SDR VNAA202207281112](https://openairdocs.org/sdr/VNAA202207281112.md): Detector · unserviceable · Jul 26, 2022 · N606NN · Cndair CL6002D24 · Smoke Detection
  > SMOKE AFT LAV WARN MSG INDICATED INTERMITTENTLY. DETECTOR TEST OK. NO VISIBLE OR SMELL OF SMOKE NOTED. REMOVED AND REPLACED AFT LAV SMOKE DETECTOR IAW CRJ900 AMM 26-16-01-000/400-801-A03.PERFORMED OPS TEST IAW CRJ900 AMM 26-16-00-710-801-A01 AND TEST GOOD AT
- [SDR VNAA202206091111](https://openairdocs.org/sdr/VNAA202206091111.md): Door · damaged · Jun 7, 2022 · N606NN · Cndair CL6002D24 · Passenger/Crew Doors
  > DURING OVERNIGHT MAINTENANCE AT JACKSON MI (JAN), THE MAINTENANCE TEAM REPORTS DAMAGE TO THE PAX DOOR UPPER LH CORNER. THE DAMAGE CONSISTS OF A MINOR GOUGING / SCRATCHES. THE DOOR SKIN (P/N 601R319066-7) IS FABRICATED FROM.160Ï¿½ 2024-T3. THE DAMAGED LOCATI
- [SDR VNAA202109021114](https://openairdocs.org/sdr/VNAA202109021114.md): Structure · cracked · Sep 2, 2021 · N606NN · Cndair CL6002D24 · Passenger/Crew Doors
  > ZONE 1 CRACKS REPORTED ON BOTH FWD AND AFT SIDES OF PAX DOOR / 670-52-11-287(ZONE1)_REV-E (PERM REPAIR - DISPOSITIONS FOR CRACKS IN PASSENGER DOOR (PHASE IV) / UPON FURTHER INSPECTION, FOUND DAMAGE TO BE IN ZONE 2 ON BOTH FWD AND AFT SIDES AND NOT ZONE 1 AS PR
- [SDR VNAA2020060711102](https://openairdocs.org/sdr/VNAA2020060711102.md): Relay · failed · Jun 3, 2020 · N606NN · Cndair CL6002D24 · Emergency Lighting
  > GALLEY SERVICE DOOR EMERGENCY LIGHT AND 1D EMERGENCY LIGHTS AND 8D EMERGENCY LIGHTS ILLUMINATED IN THE OFF POSITION (DS173, DS158, DS341) - REPLACED RELAY K198 AND INSPECTED ALL ESPU'S AND ASSOCIATED WIRING AND FOUND NO DEFECTS. TAXIED AC TO SIMULATE TURBULENC
- [SDR VNAA2019082511101](https://openairdocs.org/sdr/VNAA2019082511101.md): Light · inoperative · Aug 25, 2019 · N606NN · Cndair CL6002D24 · Emergency Lighting
  > MX FOUND 3 EMERGENCY LIGHT BY FWD SERVICE DOOR WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT. OPS CHECK GOOD.

## 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 = 'N606NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N606NN/reports

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