# Service difficulty reports: N630NN

A list on [N630NN](https://openairdocs.org/aircraft/N630NN.md).

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

- [SDR VNAA202510300004](https://openairdocs.org/sdr/VNAA202510300004.md): Hinge · worn · Oct 18, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > IN REFERENCE TO CARD TRFKE00EQH21': 52-11-01-201-002-A01-PERM REPAIR - PASSENGER DOOR HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IAW SRM TASK 52-11-01-201-002-A01. HINGE AT PASSENGER DOOR WAS REPLACED PER CRJ-900 SRM 52-11-01-201-002-A01
- [SDR VNAA202510310011](https://openairdocs.org/sdr/VNAA202510310011.md): Retainer · corroded · Oct 7, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, Structure
  > AFT MAIN AVIONICS COMPARTMENT DOOR SEAL REMOVAL IN REFERENCE NRC00053 CORROSION ON SEAL RETAINER AT SURROUND WAS FOUND. WERE EVALUATED,DUE TO EXCESSIVE DAMAGE ON SEAL RETAINER(4EA) AT MAIN AVIONICS COMPARTMENT DOOR PER SRM 53-00-00-101-001-A01 AND REPLACED
- [SDR VNAA202510310009](https://openairdocs.org/sdr/VNAA202510310009.md): Floor Support · corroded · Oct 2, 2025 · N630NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR FITTING ON ACCESS 305 (2EA´S) ON GALLEY 3 CORECTIVE ACTION: SUMMARY OF NRC00208: FLOOR FITTING (2 EAS) AND MANUFACTURED DOUBLER (1 EA) ON ACCESS 305 AT GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-30 AND FABRICATED PER REO 690-25-31-04
- [SDR VNAA202510310008](https://openairdocs.org/sdr/VNAA202510310008.md): Floor Support · corroded · Oct 2, 2025 · N630NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERIOR SHEET METAL: CORROSION FLOOR FITTING IN FRONT OF ACCESS 107 (1EA) ON GALLEY 1 FLOOR FITTING PN: CDSP2019-7C-620 ON ACCESS 107(1 EA) ON GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-33-44
- [SDR VNAA202510310010](https://openairdocs.org/sdr/VNAA202510310010.md): Floor Support · cracked · Sep 28, 2025 · N630NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER ANGLE REMOVAL IN REFERENCE NRC00115 BTW FS 265 TO FS280 CRACK WAS FOUND ON ANGLE. FLOOR ANGLE BS 265 TO FS280 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01
- [SDR VNAA202510310007](https://openairdocs.org/sdr/VNAA202510310007.md): Seat Track · corroded · Sep 28, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STRUCTURE, (02 SEGMENTS) STGR 15RH. (01 SEGMENT) BTW FS671.40 TO FS722.85. (02 SEGMENT) BTW FS783.15 TO FS846.00. SEAT RAIL (02 SEGMENTS) STGR 15RH. (01 SEGMENT) BTW FS671.40 TO FS722.85. (02 SEGMENT) BTW FS783.15 TO FS846.00 WERE
- [SDR VNAA202510310006](https://openairdocs.org/sdr/VNAA202510310006.md): Seat Track · corroded · Sep 28, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STRUCTURE, (02 SEGMENTS) STGR 15LH. (01 SEGMENT) BTW FS671.40 TO FS722.85. (02 SEGMENT) BTW FS 783.15 TO FS846.00. SEAT RAIL STRUCTURE, (02 SEGMENTS) STGR 15LH. (01 SEGMENT) BTW FS671.40 TO FS722.85. (02 SEGMENT) BTW FS 783.15 TO F
- [SDR VNAA202510310004](https://openairdocs.org/sdr/VNAA202510310004.md): Seat Track · corroded · Sep 28, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL RBL 9 BTW FS 482 TO 581, FS 581 TO 661+32 AND 661+32 TO 677 AT CABIN. SECTIONS SEAT RAIL RBL 9 BTW FS 482 TO 581, FS 581 TO 661+32 AND 661+32 TO 677 WERE REPLACED PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 AMM 53-00-49 CONFIG A12
- [SDR VNAA202510310002](https://openairdocs.org/sdr/VNAA202510310002.md): Support · cracked · Sep 27, 2025 · N630NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > DURING INSPECTION OF THE TASK CARD 53-20-260_R/H-JIC IT WAS DETECTED CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW CORECTIVE ACTION: AFT REFUEL DUCT MOUNT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW WAS REPAIRED PER REO 690-28-
- [SDR VNAA202510310005](https://openairdocs.org/sdr/VNAA202510310005.md): Seat Track · corroded · Sep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL 9 BTW FS 581 TO 661+32 AND 661+32 TO 677 AT CABIN. SEAT RAILS LBL 9 BTW FS 581 TO 661+32 AND 661+32 TO 677 AT CABIN PAX WERE EVALUATED OUT OFF LIMITS AND SEAT RAILS WERE REPLACED PER CRJ-900 SRM 53-31-49-101-001-A02 AND CRJ-900 AMM
- [SDR VNAA202510310003](https://openairdocs.org/sdr/VNAA202510310003.md): Door Sill · corroded · Sep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSIÓN ON SILL DOOR BTW STA 319.70-344 AT PASSENGER CABIN (CPAX). CORECTIVE ACTION: SILL DOOR BTW STA 319.70-344 AT PASSENGER CABIN (CPAX) WAS EVALUATED,THEREFORE IT IS OUT LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 AND REPLACED PER CRJ-900 SRM 51-42-06-00
- [SDR VNAA202510310001](https://openairdocs.org/sdr/VNAA202510310001.md): Rib · cracked · Sep 26, 2025 · N630NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > DURING INSPECTION OF THE TASK CARD 57-20-201_L/H-JIC. IT WAS DETECTED CRACK ON RIB LEADING EDGE SS57.16 AT LH WING. RIB LEADING EDGE SS57.16 AT LH WING WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.
- [SDR VNAA202510300010](https://openairdocs.org/sdr/VNAA202510300010.md): Stringer · corroded · Sep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON SPLICE AND STGR 26RH BTW FS333 TO FS349 AT MAIN AVIONICS COMPARTMENT. CORECTIVE ACTION: CORROSION ON SPLICE AND STGR 26RH BTW FS333 TO FS349 AT MAIN AVIONICS COMPARTMENT WERE REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01, WERE EVALUATED,THEREFORE I
- [SDR VNAA202510300009](https://openairdocs.org/sdr/VNAA202510300009.md): Stringer · corroded · Sep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 25 LH BTW FS 295 TO FS 310 AT MAIN AVIONICS COMPARTMENT. STGR 25 LH BTW FS 295 TO FS 310 AT MAIN AVIONICS COMPARTMENT WAS EVALUTED PER CRJ-900 SRM 53-21-03-101-006-A04 AND REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PER CRJ-900 SRM 51-
- [SDR VNAA202510300008](https://openairdocs.org/sdr/VNAA202510300008.md): Floorbeam · cracked · Sep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > DURING INSPECTION OF THE TASK CARD 53-10-219B IT WAS DETECTED CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280 AT FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280 AT FLOOR STRUCTUR
- [SDR VNAA202510300006](https://openairdocs.org/sdr/VNAA202510300006.md): Skin · corroded · Sep 26, 2025 · N630NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL SURROUND SKIN OF MAIN AVIONICS COMPARTMENT DOOR. CORROSION ON INTERNAL SURROUND SKIN OF MAIN AVIONICS COMPARTMENT DOOR WAS REPAIRED PER REO 690-53-21-032 REV -
- [SDR VNAA202510300007](https://openairdocs.org/sdr/VNAA202510300007.md): Web · cracked · Sep 25, 2025 · N630NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR VNAA202510300005](https://openairdocs.org/sdr/VNAA202510300005.md): Drag Angle · cracked · Sep 23, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.0). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT
- [SDR VNAA202510300003](https://openairdocs.org/sdr/VNAA202510300003.md): Hinge · cracked · Sep 23, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > IN REFERENCE TO CARD TRFKE00EQGK4': 53-21-23-201-007-A01-PERM REPAIR - PASSENGER DOOR SURROUND STRUCTURE - HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IN ACCORDANCE WITH CRJ900 SRM TASK 53-21-23-201-007-A01.// ENGINEERING COMMENTS: GENERATE NEW RFTS REQ
- [SDR VNAA202510300002](https://openairdocs.org/sdr/VNAA202510300002.md): Fitting · damaged · Sep 23, 2025 · N630NN · Cndair CL6002D24 · Wing Main, Frame Structure
  > REPAIR DAMAGED JACKING PAD HELICOIL INSERT LEFT, JACK FITTING LT WING WAS REPLACED PER SRM 51-42-21-001-001-A01.
- [SDR VNAA202510300001](https://openairdocs.org/sdr/VNAA202510300001.md): Hinge · corroded · Sep 23, 2025 · N630NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGES AND HINGE FITTINGS AT AFT LAVATORY SERVICE DOOR 196ER (ATTACHMENT HARDWARE INCLUDED). EVALUATED, DUE TO ECXSSESIVE DAMAGE ON HINGES (2 EAS) AND HINGE FITTINGS (2 EAS) AT AFT LAVATORY SERVICE DOOR 196ER PER CRJ 900 SRM 53-00-00-101-001-A0
- [SDR VNAA2025072811101](https://openairdocs.org/sdr/VNAA2025072811101.md): Seal · detached · Jul 26, 2025 · N630NN · Cndair CL6002D24 · Passenger/Crew Doors
  > MAIN CABIN DOOR SEAL CAME LOOSE IN FLIGHT / INSTALLED PORTIONS OF PASSENGER DOOR SEAL THAT WERE LOOSE IAW CRJ 900 AMM 52-11-07-400-801-A02-PSA, PRESSURE CHECK GOOD NO LEAKS DETECTED. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR VNAA2025031411103](https://openairdocs.org/sdr/VNAA2025031411103.md): Pin · faulted · Mar 12, 2025 · N630NN · Cndair CL6002D24 · Turbine Engine Air Inlet Section
  > EXCESSIVE N1 VIBRATION ON RH ENG. RAN QRH PROCEDURE. DID NOT CORRECT ISSUE AT NORMAL POWER SETTINGS. HAD TO REDUCE RH THRUST TO 72-73% TO KEEP VIB BELOW 1.7. / REMOVED AND REPLACED RH ENGINE FAN BLADE PINS IAW CRJ900 AMM 72-21-02-400-801-A01-PSA. PERFORMED VIB
- [SDR VNAA2024122311101](https://openairdocs.org/sdr/VNAA2024122311101.md): Window · unserviceable · Dec 19, 2024 · N630NN · Cndair · Flight Compartment Windows
  > CA WINDOW STARTED ARCING AROUND 16K FT FOLLOWED BY WINDOW HEAT CAUTION MSG. THERE WAS NO SMOKE OR ODOR, ONLY ARCING AND LASTED NO MORE THAN 10 MINUTES AND NO MEDICAL ATTENTION WAS REQUIRED. / REMOVED AND REPLACED CA SIDE WINDOW IAW AMM 56-12-01-400-801-A01-PSA
- [SDR VNAA2024082711101](https://openairdocs.org/sdr/VNAA2024082711101.md): Steering Sys · malfunctioned · Aug 24, 2024 · N630NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP CAUTION MSG IN FLIGHT. / PERFORMED FUNCTIONAL CHECK OF NOSE WHEEL STEERING IAW CRJ900 AMM 32ˆ’51ˆ’00ˆ’720ˆ’801. OPS CHECK GOOD, NO DEFECTS FOUND AT THIS TIME. ALSO VISUALLY INSP. SURROUNDING NLG COMPONENTS. NO VISUAL DEFECTS NOTED.

## 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 = 'N630NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N630NN/reports

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