# Service difficulty reports: N585NN

A list on [N585NN](https://openairdocs.org/aircraft/N585NN.md).

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

Page 1 of 2 · 58 reports

- [SDR VNAA2026090824501](https://openairdocs.org/sdr/VNAA2026090824501.md): Heater · inoperative · Sep 4, 2026 · N585NN · Cndair CL6002D24 · Pitot/Static Anti-Ice System
  > LEFT PITOT HEAT CAUTION MSG / REMOVED AND REPLACED ADSHC (A78) IAW CRJ 900 AMM 30-31-15-000/400-801-A01. OPS CHECK GOOD.
- [SDR VNAA2026073021601](https://openairdocs.org/sdr/VNAA2026073021601.md): Warning Message · false activation · Jul 27, 2026 · N585NN · Cndair CL6002D24 · Central Warning
  > INTERMITTENT RUDDER LIMIT AND XPDR FAIL CAUTION MSG IN FLIGHT WITH INTERMITTENT LOSS OF OIL TEMP, OIL PRESS, CABIN PRESS, AND APU DOOR IN POSITION INDICATION. CREW INFORMED ISSUE HAPPENED UPON TAKEOFF. RERACKED PSEU IAW AMM 32-61-01-000/400-801. OPS CHECK OF
- [SDR VNAA2026071221001](https://openairdocs.org/sdr/VNAA2026071221001.md): Steering Sys · faulted · Jul 8, 2026 · N585NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP ON TAKEOFF. PERFORMED MIPM RESET. PROBLEM DID NOT REOCCUR
- [SDR VNAA2024120811101](https://openairdocs.org/sdr/VNAA2024120811101.md): Windshield · cracked · Dec 4, 2024 · N585NN · Cndair CL6002D24 · Flight Compartment Windows
  > RH WINSHIELD STARTED ARCING CAUSING CRACK. REMOVED AND REPLACED THE RH WINDSHIELD IAW CRJ 900 AMM 56-10-05-000/400-801-A01.
- [SDR VNAA2024120411102](https://openairdocs.org/sdr/VNAA2024120411102.md): Life Vest · unserviceable · Dec 2, 2024 · N585NN · Cndair CL6002D24 · Central Display
  > PFD 1 FAILS WITH ELECTRICAL BURNING SMELL AND PFD 1 CB PANEL 2 V10 POPPED. PILOTS DESCRIBED HOW THEY SMELLED AN €ŒELECTRICAL BURNING SMELL€?. THE LOCATION OF THE SMELL WAS REPORTED IN THE COCKPIT. THE SOURCE OF THE SMELL WAS THE #1 PFD, WHILE THE DURATION OF
- [SDR VNAA20240726009](https://openairdocs.org/sdr/VNAA20240726009.md): Seat Track · corroded · Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) CORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) WERE EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 THEREFORE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) WERE REPLACED PER C
- [SDR VNAA20240726004](https://openairdocs.org/sdr/VNAA20240726004.md): Seat Track · corroded · Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS677.00 (6EA). CORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS677.00 (6EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 THEREFORE SEAT RAILS OF RBL9 BTW FS349.00 TO FS677.00 (6EA) WERE RE
- [SDR VNAA20240726003](https://openairdocs.org/sdr/VNAA20240726003.md): Seat Track · corroded · Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA). CORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA) WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 THEREFORE LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA) WERE RE
- [SDR VNAA20240726002](https://openairdocs.org/sdr/VNAA20240726002.md): Seat Track · corroded · Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (5EA). LH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49-A1
- [SDR VNAA20240726001](https://openairdocs.org/sdr/VNAA20240726001.md): Seat Track · corroded · Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ900SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49-A12
- [SDR VNAA20240723018](https://openairdocs.org/sdr/VNAA20240723018.md): Hinge Fitting · excess play · Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Vertical Stabilizer
  > INITIAL INSPECTION: FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO, 2 AND NO, 3 WERE REPLACED PER RIL #2103 REV. B.
- [SDR VNAA20240723017](https://openairdocs.org/sdr/VNAA20240723017.md): Seat Track · corroded · Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: CORROSION ON SEAT RAILS OF LBL9 BTW FS708.00 TO FS1000.00. CORROSION ON SEAT RAILS OF LBL9 BTW FS708.00 TO FS1000.00. EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02, SEAT RAILS OF LBL9 BTW FS708.00 TO FS1000.00. REPLACED PER AMM 53-
- [SDR VNAA20240723016](https://openairdocs.org/sdr/VNAA20240723016.md): Seat Track · corroded · Jun 21, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON SEAT RAILS OF RBL9 BTW FS693.00 TO FS847+16. CORROSION ON SEAT RAILS OF RBL9 BTW FS693.00 TO FS847+16. EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 THEREFORE SEAT RAILS OF RBL9 BTW FS693.00 TO FS847+16 WAS REPLACED PER PER CRJ900 AM
- [SDR VNAA20240726015](https://openairdocs.org/sdr/VNAA20240726015.md): Frame · corroded · Jun 20, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME FS= 310.00 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) CORROSION ON FRAME FS= 310.00 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED AND EVALUTED WITHIN LIMITS PER CRJ900 SRM 53-00-06-201-005-A01
- [SDR VNAA20240726006](https://openairdocs.org/sdr/VNAA20240726006.md): Mount · corroded · Jun 20, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Structure (General)
  > CORROSION ON ANGLE, MOUNTING BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE. CORROSION ON ANGLE, MOUNTING BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND REPLA
- [SDR VNAA20240723008](https://openairdocs.org/sdr/VNAA20240723008.md): Bracket · corroded · Jun 20, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER CRJ900 SRM
- [SDR VNAA20240726013](https://openairdocs.org/sdr/VNAA20240726013.md): Floorbeam · corroded · Jun 19, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORROSION INSIDE OF FLOOR PANEL SUPPORT ANGLE WITH THE CROSSBEAM UNION AT FS280.00 BTW RBL 12.00 AND LBL 12.00. FLOOR PANEL SUPPORT ANGLE WITH THE CROSSBEAM UNION AT FS280.00 BTW RBL 12.00 AND LBL 12.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101
- [SDR VNAA20240726011](https://openairdocs.org/sdr/VNAA20240726011.md): Frame · corroded · Jun 19, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 23LH TO STGR 22RH. CORROSION ON CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 23LH TO STGR 22RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, EVALUATED WITHIN LIMITS PER CRJ900 SRM
- [SDR VNAA20240726010](https://openairdocs.org/sdr/VNAA20240726010.md): Strap · corroded · Jun 19, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON JOINT STRAP FS= 333.00 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E). JOINT STRAP FS= 333.00 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E). WAS REPAIRED PER REO 690-53-21-1789 REV - -
- [SDR VNAA20240724004](https://openairdocs.org/sdr/VNAA20240724004.md): Lug · corroded · Jun 19, 2024 · N585NN · Bombdr CL6002D15 · Wing, Control Surface Attach Fittings
  > CORROSION ON HOUSING OF LUG 5 AT RH AILERON WAS FOUND. LUG 5 WAS REPAIRED PER REO 670-57-61-237 REV ORIGINAL
- [SDR VNAA20240726017](https://openairdocs.org/sdr/VNAA20240726017.md): Floorbeam · corroded · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > SECONDARY NRC FROM NRC 00122': AFTER REMOVAL, CORROSION ON RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-
- [SDR VNAA20240726016](https://openairdocs.org/sdr/VNAA20240726016.md): Floorbeam · corroded · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > SECONDARY NRC FROM NRC 00122': AFTER REMOVAL, CORROSION ON LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-0
- [SDR VNAA20240726014](https://openairdocs.org/sdr/VNAA20240726014.md): Post · corroded · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > IN REF TO: DURING INSPECTION OF THE TASK CARD 53-10-219B, IT WAS DETECTED CORROSION ON BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00. BULKHEAD DOOR POST RBL 12 AND LBL 12 WERE REPAIRED PER CRJ900 SRM 53-11-10-201-006-A01
- [SDR VNAA20240726012](https://openairdocs.org/sdr/VNAA20240726012.md): Intercostal · corroded · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN FS= 333.0 TO FS= 349.00 AT MAIN AVIONICS COMPARTMENT. (E/E). INTERCOSTAL ATTACHED TO STRINGER 20RH IN FS= 333.0 TO FS= 349.00 WAS EVALUATED PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS
- [SDR VNAA20240726005](https://openairdocs.org/sdr/VNAA20240726005.md): Bulkhead Web · corroded · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Bulkhead
  > CORROSION ON LH LOWER WEB AT BULKHEAD FS 280.00 LBL 12 ABOVE FLOOR. CORROSION ON LH LOWER WEB AT BULKHEAD FS 280.00 LBL 12 ABOVE FLOOR WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-11-10-201-003-A01 AND WAS REPAIRED PER CRJ-900 SRM 53-11-10-201-003-A01.
- [SDR VNAA20240724005](https://openairdocs.org/sdr/VNAA20240724005.md): Floor Support · cracked · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > SECONDARY NRC: IN REFERENCE TO JOB TRFKE000YVW3:53-10-303-JIC/001. AFTER REMOVAL FLOOR SUPPORT, CRACK ON FLOOR SUPPORT OF LBL12 BTW FS280 TO FS265 WAS FOUND. FLOOR SUPPORT OF LBL12 BTW FS280 TO FS265 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900
- [SDR VNAA20240723015](https://openairdocs.org/sdr/VNAA20240723015.md): Seat Track · corroded · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: CORROSION ON SEAT RAILS OF LBL9 BTW FS364.00 TO FS708.00. FLOOR SEAT RAILS OF LBL9 BTW FS364.00 TO FS708.00 (5EA) ARE OUT OFF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01,SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-
- [SDR VNAA20240723014](https://openairdocs.org/sdr/VNAA20240723014.md): Skin · gouged · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > 1211.83FH PERM REPAIR - TEMPORARY FOR LH SLAT NO.3 TE SKIN GOUGE WITHIN 1211.83 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. LH SLAT TE SKIN WAS REPAIRED PER REO 690-57
- [SDR VNAA20240723013](https://openairdocs.org/sdr/VNAA20240723013.md): Skin · worn · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-477 REV - -
- [SDR VNAA20240723012](https://openairdocs.org/sdr/VNAA20240723012.md): Fitting · damaged · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage, Landing Gear Attach Fittings
  > PERM REPAIR BEFORE 19,411.07 FH - TEMPORARY REPAIR FOR BURR DAMAGE TO NLG LOCK LINK FITTING BOLT HOLE THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 3650 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV - -. NLG LOCK LINK FITTING WAS REPAIRE
- [SDR VNAA20240723011](https://openairdocs.org/sdr/VNAA20240723011.md): Skin · worn · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB,686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (683AB,686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-478 REV - -.
- [SDR VNAA20240723010](https://openairdocs.org/sdr/VNAA20240723010.md): Seat Track · damaged · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > TEMP/PERM REPAIR FOR MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS PERMANENT REPAIR PILOT/CO-PILOT SEAT TRACK WEAR STRIP DUE TO MISSING OR LOOSE FASTENERS SEE INDIVIDUAL WO OR LB AND REO 670-53-11-210-C FOR DETAILS. PILOT/CO-PILOT
- [SDR VNAA20240723004](https://openairdocs.org/sdr/VNAA20240723004.md): Floorbeam · cracked · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPAIRED PER REO 690-53-11-1790 REV. --
- [SDR VNAA2024072300](https://openairdocs.org/sdr/VNAA2024072300.md): Drag Angle · cracked · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Vertical Stabilizer
  > INITIAL INSPECTION: CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 20.0% FRNT SPAR DATUM TO STGR DATUM TO 25.93% STGR DATUM. FWD DRAG ANGLE BTW 20.0% FRONT SPAR DATUM RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT WAS REPAIRED PER
- [SDR VNAA20240723001](https://openairdocs.org/sdr/VNAA20240723001.md): Intercostal · corroded · Jun 16, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL (2 EAS) BTW FS 349.00 TO FS 364.00, BTW STGR 26LH AND STGR 26RH OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE. (SM). INTERCOSTALS (2EAS) BTW FS349 TO FS364 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND WERE
- [SDR VNAA20240726008](https://openairdocs.org/sdr/VNAA20240726008.md): Angle · corroded · May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE, LOWER SILL (4EAS) BTW FS 319.70 TO FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE. ANGLE, LOWER SILL (4EAS) BTW FS 319.70 TO FS 349.00 WERE EVALUATED OUT OF LIMITS PER CRJ 900 SRM 53-00-00-101-001 -A01 AND WERE REPLACED PER CRJ900 SRM 51-42
- [SDR VNAA20240726007](https://openairdocs.org/sdr/VNAA20240726007.md): Strap · corroded · May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON STRAP, INNER (2EAS) FS 319.70 AND FS 349.00 OF STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE. STRAP, INNER (2EAS) FS 319.70 AND FS 349.00 OF STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE WERE EVALUATED OUT OF LIMITS PER CRJ900 S
- [SDR VNAA20240724003](https://openairdocs.org/sdr/VNAA20240724003.md): Floor Support · cracked · May 14, 2024 · N585NN · 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. FLOOR SUPPORT RBL 12.00 BTW FS 220.00 TO FS 229.00 WAS REPAIRED PER REO 690-53-11-1797 REV. - -
- [SDR VNAA20240724002](https://openairdocs.org/sdr/VNAA20240724002.md): Canister · cracked · May 14, 2024 · N585NN · Bombdr CL6002D15 · Wing Main, Frame Structure
  > SETTLEMENT FITTING AT FS310 LBL37 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01. CANISTER OF SLAT TRACK 1-3 AT RH FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV. - -
- [SDR VNAA20240724001](https://openairdocs.org/sdr/VNAA20240724001.md): Fitting · corroded · May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON SETTLEMENT FITTING (1EA) FS 310 ( LBL37) OF ENTRANCE COMPARTMENT AT FUSELAGE FLOOR STRUCTURE. SETTLEMENT FITTING AT FS310 LBL37 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
- [SDR VNAA20240723009](https://openairdocs.org/sdr/VNAA20240723009.md): Plate · corroded · May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CARGO COMPARTMENT. CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CARGO COMPARTMENT.
- [SDR VNAA20240723007](https://openairdocs.org/sdr/VNAA20240723007.md): Skin · corroded · May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > CORROSION ON JOINT PLATE UPPER LONGERON AND AFT HINGE BTW FS549.00 AND FS565.00 AT FWD BAGGAGE BAY DOOR SURROND STRUCTURE. JOINT PLATE UPPER LONGERON WAS REPAIRED PER REO 690-53-31-847 REV. -- AND AFT HINGE BTW FS549.00 AND FS565.00 AT FWD BAGGAGE BAY DOOR SU
- [SDR VNAA20240723006](https://openairdocs.org/sdr/VNAA20240723006.md): Web · cracked · May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RH FS193 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.
- [SDR VNAA20240723005](https://openairdocs.org/sdr/VNAA20240723005.md): Support · cracked · May 14, 2024 · N585NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM). REFUEL DUCT MOUNTING SUPPORT WAS REPAIRED PER REO 690-28-25-022 REV.--
- [SDR VNAA20240723002](https://openairdocs.org/sdr/VNAA20240723002.md): Fireshield · damaged · May 14, 2024 · N585NN · Bombdr CL6002D15 · Nacelle/Pylon, Bulkhead/Firewall
  > RH ENGINE LWR FWD CORE COWL FIRE SHIELD WITHIN 2,566.78 FLIGHT HOURS FROM IR (BEFORE 19,384.43FH) REPAIR OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. FIRESHIELD LWR FWD CORE COWL RH ENGINE WAS REPAIRED PER REO 690-54-23-384 REV - -
- [SDR VNAA2024021211101](https://openairdocs.org/sdr/VNAA2024021211101.md): Pin · unserviceable · Feb 8, 2024 · N585NN · Cndair CL6002D24 · Turbine Engine Air Inlet Section
  > INSPECTED LH FAN BLADES FOR STIFFNESS, NO DEFECTS FOUND, VIBE CHECK GOOD IAW CRJ 900 AMM 72-21-02-200-803-A01. HIGH TORQUE PIN T/S DUE WITHIN 15 CYCLES. / REMOVED AND REPLACED LH ENGINE FAN BLADE PINS IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA. PERFORMED VIB
- [SDR VNAA2024010311102](https://openairdocs.org/sdr/VNAA2024010311102.md): Unknown · unknown · Dec 31, 2023 · N585NN · Cndair CL6002D24 · Door Warning System
  > PAX DOOR WARNING MSG IN FLIGHT, PEFORMED QRH FOLLOWED BY CABIN ALT, ALSO FOLLOWED BY PROX SYSTEM FAULT ONE STATUS MSG+MANAULLY DEPLOYED MASKS FA NOTED WHISTLINGS SOUND COMING FROM PAX / C/W FULL RIG CHECK OF PAX DOOR IAW CRJ900 AMM 52-11-00-720-802-A01. NO OUT
- [SDR VNAA202304121111](https://openairdocs.org/sdr/VNAA202304121111.md): Fmu · unserviceable · Apr 8, 2023 · N585NN · Cndair CL6002D24 · Engine Fuel and Control
  > L ENGINE FLAMEOUT CAUTION MESSAGE IN FLIGHT, N1 AND N2 BOTH DECREASED MOMENTARILY THEN CAME BACK TO NORMAL INDICATIONS L ITT EXCEED C MESSAGE FOLLOWED / COMPLIED LH ENGINE BORESCOPE INSP. OF THE STAGE 1 AND 2 HPT, COMBUSTION LINER AND TURBINE NOZZLE IAW CRJ 90
- [SDR VNAA202207181113](https://openairdocs.org/sdr/VNAA202207181113.md): Sensor · unserviceable · Jul 16, 2022 · N585NN · Cndair CL6002D24 · Wheel/Ski/Float
  > RTF-LH OB BTMS WENT TO 2O IN FLIGHT / FOUND #1 MLG BTMS CONNECTER SLIGHTLY LOOSE. DEFERRED #1 MLG BTMS PER CRJ900 MEL 32-46-01 OPTION 4 CAT C. C/W M FUNCTION BY CAPPING CONNECTER WITH METAL DUST CAP AND SECURING TO HARNESS. REMOVED AND REPLACED #1 BRANK TEMP S
- [SDR VNAA202206131111](https://openairdocs.org/sdr/VNAA202206131111.md): None · none · Jun 10, 2022 · N585NN · Cndair CL6002D24 · Fuselage Main, Structure
  > PERMANENT REPAIR DUE TO FUSELAGE SKIN BETWEEN FS 364.00 AND FS 379.00 AND STR 22R- STR 23R / COMPLIED WITH EDDY CURRENT OF CUT OUT SECTIONS OF REPAIR AREA SURROUNDING FS 364.00, FS 379.00, AND STR 22R-23R USING REO 690-53-21-1520 REV. P2 AND CRJ900 NDTM 51-20

Next page: https://openairdocs.org/aircraft/N585NN/reports.md?page=2

## 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 = 'N585NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N585NN/reports

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