# Service difficulty reports: N587NN

A list on [N587NN](https://openairdocs.org/aircraft/N587NN.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 · 61 reports

- [SDR VNAA2026073122003](https://openairdocs.org/sdr/VNAA2026073122003.md): Selector Valve · faulted · Jul 30, 2026 · N587NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > PROX SYS CAUTION MSG IN FLIGHT / REMOVED & REPLACED LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10-000/400-801-A01.
- [SDR VNAA2026073021702](https://openairdocs.org/sdr/VNAA2026073021702.md): Control Lever · unserviceable · Jul 28, 2026 · N587NN · Cndair CL6002D24 · Landing Gear Selector
  > GEAR DISAGREE CAUTION MSG 400FT IN FLIGHT, REMOVED AND REPLACED PSEU IAW AMM 32-61-01-000/400-801-A01. LANDING GEAR PSS PASSED. REMOVED AND REPLACED LANDING GEAR CONTROL PANEL LEVER IAW AMM 32-31-01-000/400-802-A01.CYCLE LANDING GEAR 10 TIMES. OPS TEST GOOD
- [SDR VNAA2026072721301](https://openairdocs.org/sdr/VNAA2026072721301.md): Structure · damaged · Jul 26, 2026 · N587NN · Cndair CL6002D24 · Fuselage Main, Structure
  > BIRDSTRIKE WITH LARGE BIRD AT 800FT AGL ON TAKE OFF. MAIN IMPACT BELOW FO'S WINDSHIELD. [AROUND 160KTS] / REPAIR COMPLETED IAW WITH REO 690-53-11-2228 AND SRM 51-40-11-001-001-A01
- [SDR VNAA2026050417002](https://openairdocs.org/sdr/VNAA2026050417002.md): Pin · loose · Apr 24, 2026 · N587NN · Cndair CL6002D24 · Engine Mount Section
  > RIGHT ENG VIBE BETWEEN 1.5-1.9 CONTINUOUSLY. RAN QRH PROCEEDURE 3 TIMES. WHEN WE DECREASED POWER VIBES INCREASED TO 1.9; IN CLIMB DETENT VIBES DECREASED. REMOVED AND REPLACED RH ENGINE FAN BLADE PINS IAW CRJ 900 AMM 12-20-72-640-803-A01. PERFORMED VIBRATION R
- [SDR VNAA20241103011](https://openairdocs.org/sdr/VNAA20241103011.md): Web · cracked · Oct 25, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193. ELECTRICAL BAY WEB FLOOR LH SIDE FS193 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR VNAA20241103007](https://openairdocs.org/sdr/VNAA20241103007.md): Intercostal · corroded · Oct 25, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. DUE FOR NOT ALLOWABLE DAMAGE ON INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WERE REPLACED PER CRJ900 SRM 53-21-23-
- [SDR VNAA20241102002](https://openairdocs.org/sdr/VNAA20241102002.md): Drag Angle · cracked · Oct 25, 2024 · N587NN · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.00) TO STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM (TRACE
- [SDR VNAA20241103005](https://openairdocs.org/sdr/VNAA20241103005.md): Support Plate · corroded · Oct 16, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17,) ON LH/RH MAIN WHEEL WELL. CORROSION ON CONNECTORS SUPPORT PLATES RH (PX33, PX17,) ON RH MAIN WHEEL WELL WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED IS OUT LIMITS PER CRJ900 SRM
- [SDR VNAA20241103003](https://openairdocs.org/sdr/VNAA20241103003.md): Floorbeam · corroded · Oct 16, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00. CORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00 WAS REMOVED PER CRJ/900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED IS OUT LIMITS
- [SDR VNAA20241102008](https://openairdocs.org/sdr/VNAA20241102008.md): Support · cracked · Oct 16, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Internal Mounting 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. AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPAIRED PER REO 690-28-25-026 REV
- [SDR VNAA20241102007](https://openairdocs.org/sdr/VNAA20241102007.md): Floorbeam · cracked · Oct 16, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1863 REV.--
- [SDR VNAA20241103024](https://openairdocs.org/sdr/VNAA20241103024.md): Drag Angle · cracked · Oct 2, 2024 · N587NN · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.00) TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.
- [SDR VNAA20241103023](https://openairdocs.org/sdr/VNAA20241103023.md): Fitting · corroded · Oct 2, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > PER ROBBERY PROCEDURE: REMOVE FLOOR FITTING SEAT TRACK P/N: A414251-1 OF FWD LAVATORY FROM A/C: N587NN TO BE INSTALLED ON A/C N588NN TO ATTEND NRC 0235 THEN INSTALL A SERVICEABLE UNIT ON A/C N587NN. FITTING PN: A414251-1 (1EA) AISLE CORNER AT FWD LAV WAS F
- [SDR VNAA20241103022](https://openairdocs.org/sdr/VNAA20241103022.md): Skin · dented · Oct 2, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT AND RIGHT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH/RH TO STGR 21LH/RH. DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT AND RIGHT VENTRAL FIN FAIRING BTW FS
- [SDR VNAA20241103021](https://openairdocs.org/sdr/VNAA20241103021.md): Hinge · corroded · Oct 2, 2024 · N587NN · Bombdr CL6002D15 · Ailerons
  > CORROSION AT AILERON LUG R5 OF CENTER HINGE FITTING. LUG R5 OF CENTER HINGE FITTING WAS REPAIRED PER REO 670-57-61-237 REV - -
- [SDR VNAA20241103020](https://openairdocs.org/sdr/VNAA20241103020.md): Canister · corroded · Sep 29, 2024 · N587NN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > CRACK AT SLAT TRACK CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, RH MAIN FUEL TANK. CRACK AT SLAT TRACK CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.- -
- [SDR VNAA20241103019](https://openairdocs.org/sdr/VNAA20241103019.md): Canister · corroded · Sep 28, 2024 · N587NN · Bombdr CL6002D15 · Wing Miscellaneous Structure
  > CRACK AT SLAT TRACK CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK. CRACK AT SLAT TRACK CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.- -
- [SDR VNAA20241103018](https://openairdocs.org/sdr/VNAA20241103018.md): Seat Track · corroded · Sep 28, 2024 · N587NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > INITAL INSPECTION SEVERAL CORROSION ON SEAT RAIL LBL9 LBL27 RBL9 TO FS688. CORROSION ON SEAT RAIL WERE REPLACED PER CRJ 900 AMM 53-00-49
- [SDR VNAA20241103017](https://openairdocs.org/sdr/VNAA20241103017.md): Seat Track · corroded · Sep 28, 2024 · N587NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON NUT SUPPORT OF ENTRANCE COMPARTMENT AT FWD /INB POSITION. NUT SUPPORT OF ENTRANCE COMPARTMENT AT FWD /INB POSITION WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
- [SDR VNAA20241103016](https://openairdocs.org/sdr/VNAA20241103016.md): Seat Track · corroded · Sep 28, 2024 · N587NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA). LH SIDE SEAT RAIL BTW FS744 TO FS761 WAS FOUND OUT OF LIMITS AND LH SIDE SEAT RAIL BTW FS762.85 TO FS 969.00 (5EA) WERE EVALUATED ARE WITHIN LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND LH S
- [SDR VNAA20241103015](https://openairdocs.org/sdr/VNAA20241103015.md): Seat Track · corroded · Sep 28, 2024 · N587NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS720.85. CORROSION ON SEAT RAILS BTW FS379.00 TO FS 662.00 (5EA) WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-49-101-001-A01; CRJ900 SRM 53-31-49-101-001
- [SDR VNAA20241103002](https://openairdocs.org/sdr/VNAA20241103002.md): Seat Track · corroded · Sep 28, 2024 · N587NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED ARE WITHIN LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01
- [SDR VNAA20241103001](https://openairdocs.org/sdr/VNAA20241103001.md): Seat Track · corroded · Sep 28, 2024 · N587NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA). RH SIDE SEAT RAIL BTW FS744.15 TO FS762.85 AND FS 786.15 TO FS830.40+45.60 (2EA) WERE EVALUATED OUT OF LIMITS AND RH SIDE SEAT RAIL BTW FS762.85 TO FS786.15 AND FS830.40+45.60 TO FS 969.0 (4EAS)
- [SDR VNAA20241102017](https://openairdocs.org/sdr/VNAA20241102017.md): Floor Support · corroded · Sep 28, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR BEAM LBL9 BTW FS1015.00 TO FS1051.00 AT AFT BAGGAGE BAY CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM LBL9 BTW FS1015.00 TO FS1051.00 AT AFT BAGGAGE BAY CARGO COMPARTMENT FLOOR STRUCTURE. WAS REPAIRED PER CRJ900 SRM 53-00-41-2
- [SDR VNAA20241102016](https://openairdocs.org/sdr/VNAA20241102016.md): Frame · corroded · Sep 28, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME FS1088.20 BTW STGR 24RH AND STGR 23LH AT AFT BAGGAGE BAY COMPARTMENT (BELOW FLOOR). FRAME FS1088.20 BTW STGR 24RH AND STGR 23LH AT AFT BAGGAGE BAY COMPARTMENT (BELOW FLOOR) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-06-101-003-A02 AN
- [SDR VNAA20241103014](https://openairdocs.org/sdr/VNAA20241103014.md): Floor Support · cracked · Sep 27, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLO
- [SDR VNAA20241103004](https://openairdocs.org/sdr/VNAA20241103004.md): Intercostal · worn · Sep 27, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > WEAR ON INTERCOSTAL LOCATED AT STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. INTERCOSTAL LOCATED AT STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE WAS REPLACED PER DWG PLSH670-3020
- [SDR VNAA20241102015](https://openairdocs.org/sdr/VNAA20241102015.md): Rib · damaged · Sep 27, 2024 · N587NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > DISCREPANCY: ELONGATED HOLE IN SETTLEMENT AREA OF ACCESS PANEL 572CT. TRAILING EDGE CLOSING RIB WAS REPLACED PER CRJ900 SRM 51-42-22-001-001-A01 AND PER CRJ900 SRM 51-42-21-001-001-A01.
- [SDR VNAA20241102014](https://openairdocs.org/sdr/VNAA20241102014.md): Frame · corroded · Sep 27, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME FS= 319.70 BTW STRG 26LH TO 26RH AT MAINAVIONICSCOMPARTMENT. (E/E) CORROSION ON FRAME FS= 319.70 BTW STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PERCRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED, THEREFORE IS WHITHIN OF L
- [SDR VNAA20241102013](https://openairdocs.org/sdr/VNAA20241102013.md): Frame · corroded · Sep 27, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME FS= 310.00 BTW STRG 26LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) CORROSION ON FRAME FS= 310.00 BTW STRG 26LH TO 25RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PERCRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ 90
- [SDR VNAA20241102012](https://openairdocs.org/sdr/VNAA20241102012.md): Frame · corroded · Sep 27, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME FS295.00 BTW STGR 26LH TO STGR 26RH. CORROSION ON FRAME FS295.00 BTW STGR 26LH TO STGR 26RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-06-101-002-A04
- [SDR VNAA20241102011](https://openairdocs.org/sdr/VNAA20241102011.md): Joint · corroded · Sep 27, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON FUSELAGE CIRCUMFRENTIAL JOINTINTERFACE, BTW FS280.00/ FS282.86 AND STGR 26LH TO 25RH. CORROSION ON FUSELAGE CIRCUMFRENTIAL JOINTINTERFACE, BTW FS280.00/ FS282.86 AND STGR 26LH TO 25RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALU
- [SDR VNAA20241103013](https://openairdocs.org/sdr/VNAA20241103013.md): Bracket · corroded · Sep 26, 2024 · N587NN · Bombdr CL6002D15 · Cargo/Baggage Doors
  > CORROSION ON BRACKETS, MACHINED (9EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (9EAS) 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 5
- [SDR VNAA20241103012](https://openairdocs.org/sdr/VNAA20241103012.md): Plate · corroded · Sep 26, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ONUPPER/LOWER FACE OF PLATES LBL 3.4 (PLATE 1) BTW FS533.00 AND FS 549.00 (PLATE 2) BTW FS 645.00 AND FS 661.00 AT FWD CARGO COMPARTMENT. PLATES LBL 3.4 (PLATE 1) BTW FS533.00 AND FS 549.00 (PLATE 2) BTW FS 645.00 AND FS 661.00 AT FWD CARGO COMPART
- [SDR VNAA20241103010](https://openairdocs.org/sdr/VNAA20241103010.md): Web · cracked · Sep 26, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193. CRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR VNAA20241103009](https://openairdocs.org/sdr/VNAA20241103009.md): Frame · corroded · Sep 26, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 349.00 BTW STGR 26RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS 349.00 BTW STGR 26RH AND STGR 26LH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATE WITHIN LIMITS PER CRJ90
- [SDR VNAA20241103008](https://openairdocs.org/sdr/VNAA20241103008.md): Frame · corroded · Sep 26, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON INTERCOSTAL BTW FS349.00 TO FS364.00 STGR 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL BTW FS349.00 TO FS364.00 STGR 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS
- [SDR VNAA20241103006](https://openairdocs.org/sdr/VNAA20241103006.md): Skin · corroded · Sep 26, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > IN REFERANCE TO RC TRFKE001DESZ CORROSION ON INTERNAL SKIN CUTOUT SEAL SETTLEMENT AREA DOOR STRUCTURE AT MAIN AVIONICS COMPARTMENT. INTERNAL SKIN CUTOUT DOOR SURROUND STRUCTURE AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER 690-53-21-032 REV --.
- [SDR VNAA20241102010](https://openairdocs.org/sdr/VNAA20241102010.md): Cargo Track · corroded · Sep 26, 2024 · N587NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND WEAR ON RAILS (05EAS) AT FWD BAGGAGE BAY COMPARTMENT. CORROSION AND WEAR ON RAILS (05EAS) AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ900 SRM 51-12-00-001-001-A01 AND SEAT RAILS (3EAS) WERE EVALUATED W
- [SDR VNAA20241102009](https://openairdocs.org/sdr/VNAA20241102009.md): Rib · cracked · Sep 26, 2024 · N587NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > CRACKED WING RIB SS 15.50 AT RH INB WING. CRACKED WING RIB SS 15.50 AT RH INB WING WAS REPAIRED PER REO 690-57-41-446 REV - -
- [SDR VNAA20241102006](https://openairdocs.org/sdr/VNAA20241102006.md): Angle · corroded · Sep 26, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP ANGLE AND LOWER ANGLE KICK PLATE ON STGR 18LH BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME. MID CAP ANGLE AND LOWER ANGLE KICK PLATE ON STGR 18LH BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME WERE EVALUATED
- [SDR VNAA20241102005](https://openairdocs.org/sdr/VNAA20241102005.md): Mount · corroded · Sep 25, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Structure (General)
  > CORROSION WAS DETECTED IN THE ANGLED MOUNT (IN THE AREA COVERED BY THE PROTECTOR PLATE) BTW FS 319.70 AND FS 349.00. ANGLE MOUNTING BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-002-A
- [SDR VNAA20241102004](https://openairdocs.org/sdr/VNAA20241102004.md): Housing · worn · Sep 24, 2024 · N587NN · Bombdr CL6002D15 · Cargo/Baggage Doors
  > WEAR (02 LOCATIONS) ON EXTERNAL HANDLE HOUSING OF THE AFT BAGGAGE BAY DOOR. (C2). EXTERNAL HANDLE HOUSING OF THE AFT BAGGAGE BAY DOOR WAS REPAIRED PER REO 670-52-31-031 REV. -B
- [SDR VNAA20241102003](https://openairdocs.org/sdr/VNAA20241102003.md): Drag Angle · cracked · Sep 24, 2024 · N587NN · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.00) TO STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.
- [SDR VNAA20241102001](https://openairdocs.org/sdr/VNAA20241102001.md): Receptacle · damaged · Sep 24, 2024 · N587NN · Bombdr CL6002D15 · Fuselage Main, Structure
  > SPEED TAPE APPLIED - AOA VANE COVER WITHIN 4915 FLIGHT HOURS (19,990.25 FH), REPAIR OR REPLACE OF THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. RECEPTACLES (2EAS) WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.
- [SDR VNAA2024052711101](https://openairdocs.org/sdr/VNAA2024052711101.md): Pseu · inoperative · May 24, 2024 · N587NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MESSAGE ON APPROACH TO LANDING. RE-CYCLED, SAME MSG, RAN QRC/QRH CHECKLIST. MANUAL GEAR EXTENSION SUCCESSFUL. UPON LANDING NOSEWHEEL STEERING INOP / REMOVED AND REPLACED PSEU. PERFORMED EXTENSION RETRACTION OPERATIONAL TEST AGAIN, NO FAUL
- [SDR VNAA2024041111101](https://openairdocs.org/sdr/VNAA2024041111101.md): Indicator · unserviceable · Apr 8, 2024 · N587NN · Cndair CL6002D24 · Aircraft Fuel Filter/Strainer
  > XFLOW PUMP CAUTION MSG IN FLIGHT / DEFERRED XFLOW PUMP PER MEL 28-13-10 CAT C, M/FC FUNCTION C/W BY PULLING AND COLLARING CBP1 S5 AND CBP2 R7 / INTERROGATED MDC. FOUND B1-006805. T/S SYSTEM IAW CRJ900 FIM 28-41-22-810-802-A01-PSA. REMOVED AND REPLACED FGQC IAW
- [SDR VNAA202306270001](https://openairdocs.org/sdr/VNAA202306270001.md): Skin Panel · damaged · Jun 27, 2023 · N587NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LEFT FUSELAGE HAS DAMAGE BELOW N AND E IN THE LOGO ( DENT ABOUT 3 INCHES)
- [SDR VNAA202201241112](https://openairdocs.org/sdr/VNAA202201241112.md): Harness · fault message · Jan 20, 2022 · N587NN · Cndair CL6002D24 · Landing Gear Position and Warning
  > ANTI-SKID CAUTION OUTBOARD MESSAGE APPEARED ON APPROACH WHEN GEAR LOWERED. CREW DID A GO AROUND, RAN THE QRH AND DECLARED AN EMERGENCY. LANDED WITH NO ISSUES. DEF A/SKID OB CHANNEL PER MEL 32-44-01-2 CAT B. M/FUNCTION C/W. C/W OPS CHECK OF THE BRAKE SYSTEM P
- [SDR VNAA202201211111](https://openairdocs.org/sdr/VNAA202201211111.md): Anti-Skid Sys · false indication · Jan 17, 2022 · N587NN · Cndair CL6002D24 · Brake Anti-Skid Section
  > ON APPROACH, AS GEAR WAS PUT DOWN, CREW RECEIVED ANTI-SKID OUTBOARD FAULT AND OUTBOARD GROUND SPOILER FAULT MESSAGE. CREW DID A GO AROUND, RAN QRH AND REQUESTED 23R FOR LONGER LANDING DISTANCE. FLIGHT DECLARED AN EMERGENCY, NO BRACE, TRUCKS DID ROLL. FLIGHT LA

Next page: https://openairdocs.org/aircraft/N587NN/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 = 'N587NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N587NN/reports

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