# Service difficulty reports: N607NN

A list on [N607NN](https://openairdocs.org/aircraft/N607NN.md).

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

- [SDR VNAA2026071320009](https://openairdocs.org/sdr/VNAA2026071320009.md): Retainer · corroded · Jun 14, 2026 · N607NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > SECONDARY NRC AFTER PRESSURE SEAL REMOVAL ON AFT CARGO DOOR, CORROSION FOUND SEVERAL PLACES ON BOTTOM FACE AFT CARGO COMPARTMENT. CORROSION ON RETAINERS SEAL (3 EAS) AT AFT DOOR C2. WERE REMOVED PER CRJ 900 SRM SRM 51-21-06-001-001-A01. AND FOUND OUT OF LIMIT
- [SDR VNAA2026071320008](https://openairdocs.org/sdr/VNAA2026071320008.md): Hinge Fitting · corroded · Jun 10, 2026 · N607NN · Cndair CL6002D24 · Ailerons
  > CORROSION ON CENTER HINGUE FITTING L5 WAS FOUND. CENTER HINGE FITTING LUG BORE L5 AILERON LH WAS REPAIRED PER REO 670-57-61-237 REV --
- [SDR VNAA2026071320007](https://openairdocs.org/sdr/VNAA2026071320007.md): Hinge Fitting · corroded · Jun 10, 2026 · N607NN · Cndair CL6002D24 · Ailerons
  > CORROSION ON CENTER HINGUE FITTING R2 WAS FOUND. CENTER HINGE FITTING LUG BORE R2 AILERON RH WAS REPAIRED PER REO 670-57-61-237 REV --
- [SDR VNAA2026071320006](https://openairdocs.org/sdr/VNAA2026071320006.md): Fitting · corroded · Jun 10, 2026 · N607NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN FWD ON ENTRANCE (1EA). CORROSION FLOOR FITTING IN FWD ON ENTRANCE (1EA) WAS REPLACED PER CMM 25-33-06
- [SDR VNAA2026071320004](https://openairdocs.org/sdr/VNAA2026071320004.md): Fitting · corroded · Jun 10, 2026 · N607NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1 WAS REPLACED PER CMM 25-33-21.
- [SDR VNAA2026071320003](https://openairdocs.org/sdr/VNAA2026071320003.md): Fitting · corroded · Jun 10, 2026 · N607NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1 WAS REPLACED PER CMM 25-33-21.
- [SDR VNAA2026071320002](https://openairdocs.org/sdr/VNAA2026071320002.md): Fitting · corroded · Jun 10, 2026 · N607NN · 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 PER CMM 25-33-21
- [SDR VNAA202607120020](https://openairdocs.org/sdr/VNAA202607120020.md): Hinge · worn · Jun 9, 2026 · N607NN · Cndair CL6002D24 · Rudder Structure
  > EXCCESSIVE FREE PLAY (LATERAL AND LONGITUDINAL) OF BEARINGS FOUND ON BOTH 2 CENTRAL RUDDER HINGES OF VERTICAL STABILAZER REAR SPAR. HINGE 3 WAS REPAIRED PER RIL #1213 REV. A. AND HINGE 2 WAS REPLACED PER RIL #2103 REV. B.
- [SDR VNAA202607120019](https://openairdocs.org/sdr/VNAA202607120019.md): Rib · cracked · Jun 9, 2026 · N607NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON OUTB MACHINED RIB OF FLS 168.07 TRAILING EDGE AREA AT WING RH. RIB OF FLS 168.07 TRAILING EDGE AREA AT RH WING WAS REPAIRED PER REO 690-57-51-542 REV. - -
- [SDR VNAA202607120018](https://openairdocs.org/sdr/VNAA202607120018.md): Floorbeam · cracked · Jun 9, 2026 · N607NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK ON CENTER FLOOR BEAM RBL12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CENTER FLOOR BEAM RBL12.0 BTW 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR S
- [SDR VNAA202607120017](https://openairdocs.org/sdr/VNAA202607120017.md): Frame · damaged · Jun 7, 2026 · N607NN · Cndair CL6002D24 · Fuselage Main, Frame
  > FOLDED FRAME (FS1015.00) BTW STGR 17L TO 19L ON LOWER SURROUND STRUCTURE AT AFT BAGGAGE BAY DOOR. FOLDED FRAME (FS1015.00) BTW STGR 17L TO 19L ON LOWER SURROUND STRUCTURE AT AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND SRM 51-42-
- [SDR VNAA202607120016](https://openairdocs.org/sdr/VNAA202607120016.md): Seat Track · corroded · Jun 6, 2026 · N607NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAILS BTW FS=349 TO FS=477 AND RBL 9'' ALSO IN FS 379 AND LBL 9 AT CPAX. FLOOR SEAT RAILS BTW FS=349 TO FS=477 AND RBL 9'' ALSO IN FS 379 AND LBL 9 AT CPAX WERE REPLACED PER CRJ900 AMM 53-00-49-400-801 (CONFIG A12)
- [SDR VNAA202607120015](https://openairdocs.org/sdr/VNAA202607120015.md): Seat Track · corroded · Jun 6, 2026 · N607NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 16L, BS 501 TO BS 549 AND BS 645 TO BS 693 AT CPAX. SIDE SEAT TRACAK STR 16L, BS 501 TO BS 549 AND BS 645 TO BS 693 AT CPAX WERE REPLACE IAW AMM 53-00-49-400-801 (CONFIG A12).
- [SDR VNAA202607120014](https://openairdocs.org/sdr/VNAA202607120014.md): Seat Track · corroded · Jun 6, 2026 · N607NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL STGR 15 RH, FS 453 TO FS 501 AND FS 661+74 TO FS 693 AT CPAX. SIDE SEAT RAIL STGR 15 RH, BS 453 TO BS 501 AND BS 661+74 TO BS 693 AT CPAX WERE REPLACED IAW AMM 53-00-49-400-801 (CONFIG A12).
- [SDR VNAA2026071320005](https://openairdocs.org/sdr/VNAA2026071320005.md): Fitting · corroded · Jun 5, 2026 · N607NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN FRONT PAPER CONTAINER AND UNDER WASTE CONTAINER ON FWD LAV (1EA). FLOOR FITTING IN FRONT PAPER CONTAINER AND UNDER WASTE CONTAINER ON FWD LAV (1EA) WAS REPLACED PER SAFRAN CMM 25-40-19.
- [SDR VNAA202607120013](https://openairdocs.org/sdr/VNAA202607120013.md): Seat Track · corroded · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BTW FS 693 TO FS 927 AND STGR 15LH AT CABIN PAX. SEAT TRACK REPLACED IAW AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202607120012](https://openairdocs.org/sdr/VNAA202607120012.md): Seat Track · corroded · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BTW FS 693 TO FS 927 AND STGR 15RH AT CABIN PAX. THE SEAT TRACK REPLACED IAW AMM 53-00-49-400-801(CONFIG A12).
- [SDR VNAA202607120011](https://openairdocs.org/sdr/VNAA202607120011.md): Bulkhead · corroded · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > DURING INSPECTION OF THE JOB CARD TRFKE00CCHN1: CORROSION ON DOOR POST BULKHEAD AT RBL 12 & LBL 12 AT FS 280.00 AT RH/LH SIDE LOWER SECTION. CORROSION ON DOOR POST BULKHEAD AT RBL 12 & LBL 12 AT FS 280.00 AT RH/LH SIDE LOWER SECTION WAS REMOVED PER CRJ 900 S
- [SDR VNAA202607120010](https://openairdocs.org/sdr/VNAA202607120010.md): Rib · cracked · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACKED MACHINED RIB SS 15.50 ON INBD FIXED LEADING EDGE AT RH WING. RIB SS 15.50 ON INBD FIXED LEADING EDGE AT RT WING REPAIR PER REO 690-57-41-613 REV - -
- [SDR VNAA202607120009](https://openairdocs.org/sdr/VNAA202607120009.md): Web · cracked · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB LH SIDE FS193.00 ( BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT. CRACK ON ELECTRICAL BAY FLOOR WEB LH SIDE FS193.00 ( BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER SRM 53-
- [SDR VNAA202607120008](https://openairdocs.org/sdr/VNAA202607120008.md): Stand Off · cracked · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Doors
  > CRACK PAD SUPPORT (1EA) AT RH AFT CORE. PAD SUPPORT (1EA) AT RH AFT CORE WAS REPLACED PER SRM 51-42-06-001-001-A01.
- [SDR VNAA202607120007](https://openairdocs.org/sdr/VNAA202607120007.md): Skin · damaged · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON EXTERNAL SKIN AT FS 910 AND FS 919, STRINGER 27 ON CENTER FUSELAGE. WEAR ON EXTERNAL SKIN AT FS 919 STRINGER 27 ON CENTER FUSELAGE WAS BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND FOUND WITHIN LIMITS PER CRJ900 SRM 53-51-01-101-003-A05 AND WEAR
- [SDR VNAA202607120006](https://openairdocs.org/sdr/VNAA202607120006.md): Box Beam · damaged · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Fuselage Main, Structure
  > 800FH PERM REPAIR - TEMPORARY REPAIR FOR DAMAGED HOLE TO LH NLG BOX SIDE BEAM BETWEEN FS228.42-FS235.00 THIS TEMPORARY REPAIR IS ACCEPTABLE FOR 800 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO. // ENGINEERING COMMENTS: FWD FITTING STR 26A LH (PN CC6
- [SDR VNAA202607120005](https://openairdocs.org/sdr/VNAA202607120005.md): Fairing · dented · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Trailing Edge Flaps
  > 3801.90FH PERM REPAIR - LH FLAP STUB FAIRING (171DL) WITHIN 3801.90 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. LH FLAP STUB FAIRING (171DL) WAS REPAIRED PER EA NO: 53
- [SDR VNAA202607120004](https://openairdocs.org/sdr/VNAA202607120004.md): Drag Angle · cracked · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FW/AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. (ET) HFEC INSPECTION WAS PERFORMED 01 CRACK WAS FOUND ON AFT DRAG ANGLE AND FWD DRAG ANGLE NO CRACKS WERE FOUND. IAW NDT
- [SDR VNAA202607120003](https://openairdocs.org/sdr/VNAA202607120003.md): Drag Angle · cracked · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. REPAIRED PER SRM 55-31-00-201-001-A01
- [SDR VNAA202607120002](https://openairdocs.org/sdr/VNAA202607120002.md): Angle · cracked · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Passenger/Crew Doors
  > RACK AFT ANGLE ON PASSENGER DOOR. CRACK AFT ANGLE ON PASSENGER DOOR WAS REPAIR PER SRM 52-11-04-201-002-A01.
- [SDR VNAA202607120001](https://openairdocs.org/sdr/VNAA202607120001.md): Handle · worn · Jun 1, 2026 · N607NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > WEAR ON HANDLE FRAME AT AFT BAGGAGE BAY DOOR. DOOR WAS REPAIRED PER REO 670-52-31-031 REV. - BV. - B
- [SDR VNAA2026071320001](https://openairdocs.org/sdr/VNAA2026071320001.md): Access Panel · cracked · Apr 18, 2026 · N607NN · Cndair CL6002D24 · Aerodynamic Fairings
  > CRACK ON ACCESS PANEL 172CR AT OVER WING FAIRING. ACCESS PANEL 172CR AT OVER WING FAIRING WAS REPAIRED PER REO 679-53-82-430 REV - -, AND STIFFENER WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.
- [SDR VNAA2024120311102](https://openairdocs.org/sdr/VNAA2024120311102.md): Steering Sys · abnormal · Nov 24, 2024 · N607NN · Cndair CL6002D24 · Steering Unit
  > STEERING INOP CAUTION ON TAKEOFF CLIMB / PERFORMED MIPM RESET. MSG EXTINGUISHED. PROBLEM DID NOT REOCCUR.
- [SDR VNAA2024120311101](https://openairdocs.org/sdr/VNAA2024120311101.md): Steering Sys · abnormal · Nov 24, 2024 · N607NN · Cndair CL6002D24 · Steering Unit
  > STEERING INOP CAUTION MSG AFTER TAKEOFF / C/W MIPM RESET FOR STEERING INOP, FAULT DID NOT REOCCUR.
- [SDR VNAA202308221112](https://openairdocs.org/sdr/VNAA202308221112.md): Manifold · unserviceable · Aug 20, 2023 · N607NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP MESSAGE AFTER TAKEOFF. QRH PROCEDURE DID NOT CLEAR MESSAGE. / TROUBLESHOT STEERING INOP THROUGH B1-007464 FOUND IN MDC IAW CRJ 900 FIM 32-51-50-810-801. REMOVED AND REPLACED STEERING MANIFOLD IAW CRJ 900 AMM 32-51-50-000/400-801. BITE TEST AND OP
- [SDR VNAA202308221111](https://openairdocs.org/sdr/VNAA202308221111.md): Selector Valve · unserviceable · Aug 19, 2023 · N607NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP IN FLIGHT, AFTER GEAR UP / R/R LANDING GEAR SELECTOR VALVE IAW CRJ 900 AMM 32-32-15-000/400-801. T/S IAW CRJ 900 FIM 32-51-50-810-801. B1-007464. OPS/LEAK CHECK GOOD.
- [SDR VNAA202303110003](https://openairdocs.org/sdr/VNAA202303110003.md): Plate · cracked · Mar 11, 2023 · N607NN · Bombdr CL6002D15 · Doors
  > PERM REPAIR NEEDS PERFORMED FOR CRACKS IN ZONE 5 ON AFT SIDE OF PAX DOOR: PERFORMED PERMANENT REPAIR TO PAX DOOR ZONE 5 IAW CRJ-900 SRM 52-11-04-201-006-A01
- [SDR VNAA202303110002](https://openairdocs.org/sdr/VNAA202303110002.md): Drag Angle · cracked · Mar 11, 2023 · N607NN · Bombdr CL6002D15 · Doors
  > PERM REPAIR NEEDS PERFORMED FOR CRACKS IN ZONE 3 ON AFTSIDE OF PAX DOOR: REPAIRED DAMAGED PAX DOOR AFT DRAG ANGLE IAW CRJ 900 SRM 52-11-04-201-002-A01 REPAIR TYPE 1 STEPS 5.B THROUGH CLOSE-OUT. REFERENCE THE TASK SECTION OF THIS CARD FOR WORK PERFORMED
- [SDR VNAA202303110001](https://openairdocs.org/sdr/VNAA202303110001.md): Web · cracked · Mar 11, 2023 · N607NN · Bombdr CL6002D15 · Doors
  > PERM REPAIR OF CRACK DAMAGE TO PAX DOOR NEEDS PERFORMED: REPAIRED PAX DOOR FWD WEB IAW CRJ-900 SRM 52-11-04-201-004-A01.
- [SDR VNAA202012181111](https://openairdocs.org/sdr/VNAA202012181111.md): Trim System · abnormal · Dec 16, 2020 · N607NN · Cndair CL6002D24 · Rudder Tab Control System
  > RTO-THE CREW REJECTED THE TAKE OFF FROM RUNWAY 36R AT IDLE PWER AND SPEED NOT ABOVE TAXI SPEED FOR AN AILERON TRIM UNCOMMANDED FULL LEFT WING DOWN AND RUDDER TRIM UNCOMMANDED FULL LEFT RUDDER. CBP 2 F3 POPPED. THE CREW IS CURRENTLY RETURNING TO THE GATE FOR
- [SDR VNAA2019090911102](https://openairdocs.org/sdr/VNAA2019090911102.md): Transmitter · out of rig · Sep 9, 2019 · N607NN · Cndair CL6002D24 · Elevator Control System
  > IN LEVEL FLIGHT CREW RECEIVED ELEVATOR SPLIT CAUTION MESSAGE. CREW RAN THRU THE QRH, DECLARED AN EMERGENCY AND LANDED GSP WITHOUT INCIDENT. RE-RIGGED/INDEXED LEFT ELEVATOR POSITION TRANSMITTER. SYSTEM OPS CHECKED 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 = 'N607NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N607NN/reports

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