# Service difficulty reports: N566NN

A list on [N566NN](https://openairdocs.org/aircraft/N566NN.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 · 56 reports

- [SDR VNAA2024121911101](https://openairdocs.org/sdr/VNAA2024121911101.md): Manifold · faulted · Dec 16, 2024 · N566NN · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP CAUTION MSG AT ABOUT 12000 FT. / PERFORMED UN-ATE SCAN OF NWS STYSTEM IAW UN-ATE USER GUIDE. SENT RESULTS TO TECH ANALYSTS. TROUBSHOT LANDING GEAR SELECTOR VALVE IAW FIM 32-51-35-810-801(A01) PASSED WITH A READING OF 59.6OHMS. REMOVED AND REPLACE
- [SDR VNAA2024102511101](https://openairdocs.org/sdr/VNAA2024102511101.md): Selector Valve · unserviceable · Oct 22, 2024 · N566NN · Cndair CL6002D24 · Landing Gear Steering System
  > SHORTLY AFTER TAKEOFF, A STEERING INOP MESSAGE WAS RECEIVED. THE FLIGHT PROCEEDED TO CLT AND THE CREW DECLARED AN EMERGENCY ONCE THEY GOT CLOSER TO CLT. / REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ 900 AMM 32-32-10-000/400-801. STEERING FAULT DID
- [SDR VNAA2024092311102](https://openairdocs.org/sdr/VNAA2024092311102.md): Tire · damaged · Sep 20, 2024 · N566NN · Cndair CL6002D24 · Tire
  > A/C IS RTF FOR POSSIBLE TIRE DAMAGE ON TAKEOFF. / REMOVED AND REPLACED LHIB WHEEL AND TIRE ASSEMBLY IAW CRJ 900 AMM 32-41-01-000/400-801-A01-PSA. PERFORMED VISUAL CHECK OF LH MLG FOR TIRE BURST DAMAGE IAW CRJ 900 AMM 05-51-29-210-802.
- [SDR VNAA2024031711102](https://openairdocs.org/sdr/VNAA2024031711102.md): Windshield · cracked · Mar 14, 2024 · N566NN · Cndair CL6002D24 · Flight Compartment Windows
  > WINDSHIELD HEAT CAUSING ARCING AND CRACKING / REMOVED AND INSTALLED THE CA WINDSHIELD IAW CRJ 900 AMM 56-11-01-400-801-A01-PSA. OPS CHECK OF THE WINDSHIELD TEMP CONTROLLER GOOD. OPS CHECK OF THE WINDSHIELD-WIPER DRIVE ARM GOOD. LEAK CHECK GOOD. NO FURTHER DEF
- [SDR VNAA202402290030](https://openairdocs.org/sdr/VNAA202402290030.md): Bushing · corroded · Feb 23, 2024 · N566NN · Bombdr CL6002D15 · Ailerons
  > AFTER REMOVAL OF LH AILERON BUSHINGS, CORROSION ON LUG BORE OF L1, L2, L5 AND L6 OF CENTER HINGE FITTINGS OF LEFT AILERON. BORE OF L1, L2, L5 AND L6 OF CENTER HINGE FITTINGS OF LEFT AILERON WERE REPAIRED PER REO 670-57-61-237, REV. -- NOTE F AND G
- [SDR VNAA202402290025](https://openairdocs.org/sdr/VNAA202402290025.md): Skin · damaged · Feb 22, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES 3(EAS) ON FUSELAGE SKIN ON STGR 17 LH AND BTW FS 379 TO FS 421. FUSELAGE SKIN ON STGR 17 LH AND BTW FS 379 TO FS 421 WAS BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-01-101-005-A05.
- [SDR VNAA202402290008](https://openairdocs.org/sdr/VNAA202402290008.md): Canister · cracked · Feb 12, 2024 · N566NN · Bombdr CL6002D15 · Wing Main, Frame Structure
  > CRACK IN CANISTER NO.3, STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER NO.3, STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577.REV.--
- [SDR VNAA202402290031](https://openairdocs.org/sdr/VNAA202402290031.md): Bushing · corroded · Feb 11, 2024 · N566NN · Bombdr CL6002D15 · Ailerons
  > AFTER REMOVAL OF RH AILERON BUSHINGS, CORROSION ON LUG BORES OF R1, R2 AND R6 OF CENTER HINGE FITTING OF RIGHT AILERON. BORES OF R1, R2 AND R6 OF CENTER HINGE FITTING OF RIGHT AILERON WERE REPAIRED PER REO 670-57-61-237, REV. -- NOTE F AND G
- [SDR VNAA202402290020](https://openairdocs.org/sdr/VNAA202402290020.md): Rib · cracked · Feb 6, 2024 · N566NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > AFTER ACCESS PANEL 521BL REMOVAL TO SLAT LUBRICATION, CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV - -
- [SDR VNAA202402290014](https://openairdocs.org/sdr/VNAA202402290014.md): Floorbeam · cracked · Feb 6, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1677 REV --
- [SDR VNAA202402290013](https://openairdocs.org/sdr/VNAA202402290013.md): Floorbeam · cracked · Feb 6, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1677 REV--
- [SDR VNAA202402290012](https://openairdocs.org/sdr/VNAA202402290012.md): Intercostal · worn · Feb 6, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > WORN INTERCOSTAL LOCATED AT STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. CRJ900 SRM 53-21-03-101-004-A04, WAS FABRICATED PER DWG SH670-30202 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR VNAA202402290007](https://openairdocs.org/sdr/VNAA202402290007.md): Hinge Fitting · excess play · Jan 28, 2024 · N566NN · Bombdr CL6002D15 · Rudder Structure
  > AFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. (AYP). HINGE FITTINGS # 2 AND # 3 WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 PAR.6.C. AND PER RIL #2
- [SDR VNAA202402290017](https://openairdocs.org/sdr/VNAA202402290017.md): Seat Track · corroded · Jan 26, 2024 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SIDE SEAT RAIL OF STRG 15RH BETWEEN FS 744.15 TO FS 761.85. SIDE SEAT RAIL OF STRG 15RH BETWEEN FS 744.15 TO FS 761.85 WAS EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202402290003](https://openairdocs.org/sdr/VNAA202402290003.md): Seat Track · corroded · Jan 26, 2024 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN SEVERAL LOCATIONS AT SEAT RAIL LBL 9 BTW F.S.379.00 TO F.S. 453. SEAT RAIL LBL 9 BTW F.S.379.00 TO F.S. 453.00 WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202402290002](https://openairdocs.org/sdr/VNAA202402290002.md): Skin · nicked · Jan 26, 2024 · N566NN · Bombdr CL6002D15 · Trailing Edge Flaps
  > NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5. NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 WERE BLENDED PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE EVALUATED WITHIN LIMITS PER CRJ900 SRM 57-52-01-101-001-A01
- [SDR VNAA202402290001](https://openairdocs.org/sdr/VNAA202402290001.md): Skin · dented · Jan 26, 2024 · N566NN · Bombdr CL6002D15 · Trailing Edge Flaps
  > DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5. DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 WERE MEASURED AND WERE EVALUATED WITHIN LIMITS PER CRJ-900 SRM 57-52-01-101-001-A01
- [SDR VNAA202402290018](https://openairdocs.org/sdr/VNAA202402290018.md): Seat Track · corroded · Jan 25, 2024 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS RBL 9 STA 421 TO 501 (2E/A) AND LBL 9 STA 581 TO 661+32. SIDE SEAT RAIL OF STRG 15RH BTW FS 661.00 + 90 TO FS 720.85 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202402290016](https://openairdocs.org/sdr/VNAA202402290016.md): Seat Track · corroded · Jan 25, 2024 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 669.40 TO FS 720.85. SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 669.40 TO FS 720.85 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202402290011](https://openairdocs.org/sdr/VNAA202402290011.md): Bracket · corroded · Jan 25, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET MACHINED (4 EA´S) ON FLOOR STRUCTURE AT FWD CARGO COMPARTMENT BTW FS 517 TO FS 661.00+16.00 AND BTW STGR 23 RH TO 22LH. BRACKET MACHINED (4 EA´S) ON FLOOR STRUCTURE AT FWD CARGO COMPARTMENT BTW FS 517 TO FS 661.00+16.00 AND BTW STGR 23 R
- [SDR VNAA202402290010](https://openairdocs.org/sdr/VNAA202402290010.md): Seat Track · corroded · Jan 25, 2024 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS RBL 9 STA 421 TO 501 (2E/A) AND LBL 9 STA 581 TO 661+32. SEAT RAILS RBL 9 STA 421 TO 501 (2E/A) AND LBL 9 STA 581 TO 661+32 WERE EVALUATED OUT OF LIMITS PER CRJ 900 SRM 53-21-49-101-001-A01; CRJ900 SRM 53-31-49-101-001-A02 AND WERE R
- [SDR VNAA202402290027](https://openairdocs.org/sdr/VNAA202402290027.md): Duct · cracked · Jan 24, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Attach Fittings
  > CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH WAS REPAIRED PER REO 690-28-25-016. REV. --
- [SDR VNAA202402290028](https://openairdocs.org/sdr/VNAA202402290028.md): Skin · cracked · Jan 23, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 18 RH TO 19 RH AND AT FS629. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 18 RH TO 19 RH AND AT FS629 WAS REPAIRED PER REO 690-53-31-816 REV - -
- [SDR VNAA202402290023](https://openairdocs.org/sdr/VNAA202402290023.md): Web · cracked · Jan 23, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR VNAA202402290022](https://openairdocs.org/sdr/VNAA202402290022.md): Rib · cracked · Jan 23, 2024 · N566NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-322 REV.--
- [SDR VNAA202402290021](https://openairdocs.org/sdr/VNAA202402290021.md): Rib · cracked · Jan 23, 2024 · N566NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-323 REV.--
- [SDR VNAA202402290019](https://openairdocs.org/sdr/VNAA202402290019.md): Rib · cracked · Jan 23, 2024 · N566NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > AFTER ACCESS PANEL 621BR REMOVAL TO SLAT LUBRICATION, CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING. CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240 REV - -
- [SDR VNAA202402290026](https://openairdocs.org/sdr/VNAA202402290026.md): Skin · damaged · Jan 22, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 16 LH TO 17 LH AND BTW FS 501 TO FS 517. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 16 LH TO 17 LH AND BTW FS 501 TO FS 517 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03
- [SDR VNAA202402290024](https://openairdocs.org/sdr/VNAA202402290024.md): Skin · damaged · Jan 22, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 14 RH AT FS 379. LIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 14 RH AT FS 379 WAS REPAIRED PER REO 690-53-21-1726 REV. - -
- [SDR VNAA202402280008](https://openairdocs.org/sdr/VNAA202402280008.md): Skin · damaged · Jan 21, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE (1EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR15 BTW FS280 - FS264. LIGHTNING STRIKE (1EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR15 BTW FS280 - FS264 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03
- [SDR VNAA202402280007](https://openairdocs.org/sdr/VNAA202402280007.md): Skin · damaged · Jan 21, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE (2EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR14 BTW FS248.5 - FS233.5. LIGHTNING STRIKE (2EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR14 BTW FS248.5 - FS233.5 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03
- [SDR VNAA202402280006](https://openairdocs.org/sdr/VNAA202402280006.md): Skin · damaged · Jan 21, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ( 1EA) ON FUSELAGE SKIN BTW STGR 14 RH TO STGR 15RH AND BTW FS 1051 TO FS 1069. LIGHTNING STRIKE ( 1EA) ON FUSELAGE SKIN BTW STGR 14 RH TO STGR 15RH AND BTW FS 1051 TO FS 1069. WAS BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WAS EVALU
- [SDR VNAA202402280003](https://openairdocs.org/sdr/VNAA202402280003.md): Skin · damaged · Jan 21, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 19 RH TO STGR 20 RH AT FS 549. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 19 RH TO STGR 20 RH AT FS 549 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03
- [SDR VNAA202402280002](https://openairdocs.org/sdr/VNAA202402280002.md): Skin · damaged · Jan 21, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 23 RH AT FS 596. LIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 23 RH AT FS 596 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03
- [SDR VNAA202402280005](https://openairdocs.org/sdr/VNAA202402280005.md): Drag Angle · cracked · Jan 20, 2024 · N566NN · Bombdr CL6002D15 · 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). AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-2
- [SDR VNAA202402280004](https://openairdocs.org/sdr/VNAA202402280004.md): Drag Angle · cracked · Jan 20, 2024 · N566NN · Bombdr CL6002D15 · 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). AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-
- [SDR VNAA202402280001](https://openairdocs.org/sdr/VNAA202402280001.md): Skin · scratched · Jan 4, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > SEVERAL SCRATCH ON EXTERNAL REAR FUSELAGE SKIN AREA BTW FS985.00 - FS1000.00 AND STGR 14 - STGR 16. FUSELAGE SKIN AREA BTW FS985.00 - FS1000.00 AND STGR 14 - STGR 16 WAS REPAIRED PER REO 690-53-61-1346 REV - -
- [SDR VNAA202402290015](https://openairdocs.org/sdr/VNAA202402290015.md): Floor Support · cracked · Jan 3, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > 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). FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE
- [SDR VNAA202402290009](https://openairdocs.org/sdr/VNAA202402290009.md): Intercostal · corroded · Jan 3, 2024 · N566NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT FS316 BTW LBL 9 TO RBL 9. INTERCOSTAL AT FS316 BTW LBL 9 TO RBL 9 WAS REPAIRED PER REO 690-53-21-1717 REV -.
- [SDR VNAA202402290005](https://openairdocs.org/sdr/VNAA202402290005.md): Seat Track · corroded · Jan 3, 2024 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 785.15 TO FS 797. SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 785.15 TO FS 797.00 WAS EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202402290004](https://openairdocs.org/sdr/VNAA202402290004.md): Seat Track · corroded · Jan 3, 2024 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 847.00 + 61 TO FS 865. CORROSION ON STRG 15LH BETWEEN FS 847.00 + 61 TO FS 865.00 WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONF A12)
- [SDR VNAA202402290006](https://openairdocs.org/sdr/VNAA202402290006.md): Seat Track · corroded · Dec 13, 2023 · N566NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 744.15 TO FS 761.85. SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 744.15 TO FS 761.85 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12).
- [SDR VNAA202306110001](https://openairdocs.org/sdr/VNAA202306110001.md): Fitting · unknown · Jun 11, 2023 · N566NN · Cndair CL6002D24 · Fuselage Structure (General)
  > NEW HSTA FITTING AV670-23105-006S MISDRILLED AND REQUIRES NEW FITTING. PERFORMED A MAJOR REPAIR TO R/H HSTA UPPER FITTING ASSY.
- [SDR VNAA202304211111](https://openairdocs.org/sdr/VNAA202304211111.md): Unknown · unknown · Apr 20, 2023 · N566NN · Cndair CL6002D24 · Landing Gear Steering System
  > DURING TAKEOFF, MESSAGE FOR NOSE WHEEL STEERING CAME UP DURING FLIGHT. TROUBLESHOT PER FIM 32-51-50-810-801. B1-007464. C/W OPS CHECK OF NWS IAW CRJ 900 AMM 32-51-00-710-801. OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA2020102611101](https://openairdocs.org/sdr/VNAA2020102611101.md): Sensor · failed · Oct 23, 2020 · N566NN · Cndair CL6002D24 · Landing Gear Brake System
  > AFTER TAKE OFF FROM CAK THE CREW RECEIVED A BTMS INDICATION. THEY HAD THE PASSENGERS BRACE, DECLARED AN EMERGENCY AND RETURNED TO CAK. THEY LANDED SAFELY AND WITHOUT INCIDENT. TRUCKS ROLLED. THE PASSENGERS ARE OK AND THE CREW WILL CONTINUE ON WITH THEIR FL
- [SDR VNAA2020051901101](https://openairdocs.org/sdr/VNAA2020051901101.md): Door Seal · damaged · May 17, 2020 · N566NN · Cndair CL6002D24 · Passenger/Crew Doors
  > DURING CLIMB OUT OF PNS, AT FL200 CREW BEGAN HEARING POPPING NOISE AND BEGAN TO FEEL PRESSURE DROPPING. CREW NOTICED CABIN ALT RISING. CREW DONNED O2 MASKS, BEGAN EMERGENCY DESCENT AND DECLARED AN EMERGENCY WITH ATC. CREW RECEIVED NO WARNINGS AND CABIN ALT N
- [SDR VNAA202004229991](https://openairdocs.org/sdr/VNAA202004229991.md): Megaphone · inoperative · Apr 22, 2020 · N566NN · Cndair CL6002D24 · Emergency Equipment
  > MEGA PHONE INOP. CHANGE BATTERIES, STILL WILL NOT WORK. INSTALLED SERVICEABLE MEGAPHONE.
- [SDR VNAA202004219996](https://openairdocs.org/sdr/VNAA202004219996.md): Frame · corroded · Apr 21, 2020 · N566NN · Cndair CL6002D24 · Fuselage Main, Frame
  > FUSELAGE LOWER FRAME AT FS295, STGR27 IS CORRODED ON FWD SIDE. REPAIRED IAW CRJ 900 SRM 53-00-06-101-002-A04
- [SDR VNAA202004219995](https://openairdocs.org/sdr/VNAA202004219995.md): Door Sill · corroded · Apr 21, 2020 · N566NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL IS CORRODED AT 2 LOCATIONS BETWEEN FS 280.00 AND FS 319.75. LOCATED, DRILLED AND INSTALLED NEW FLOOR SILL. IAW CRJ900 SRM'S 51-42-06-001-001-A01, 51-42-13-001-001-A01, 57-42-21-001-001-A01, 51-40-11-001-001-A01.
- [SDR VNAA202004219994](https://openairdocs.org/sdr/VNAA202004219994.md): Intercostal · corroded · Apr 21, 2020 · N566NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH INTERCOSTALS BETWEEN FS349.00 AND FS364.00, STR26L TO STR 26R ARE CORRODED. LOCATED AND DRILLED LH AND RH INTERCOSTALS AT FS349.00 TO FS 364.00 IAW CRJ 900 SRM 51-40-11-001-001-A01.

Next page: https://openairdocs.org/aircraft/N566NN/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 = 'N566NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N566NN/reports

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