# Service difficulty reports: N567NN A list on [N567NN](https://openairdocs.org/aircraft/N567NN.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 · 91 reports - [SDR VNAA2026091524801](https://openairdocs.org/sdr/VNAA2026091524801.md): Reservoir · unserviceable · Sep 13, 2026 · N567NN · Cndair CL6002D24 · Hydraulic Reservoir, Main > HYD 3 HIGH TEMP IN FLIGHT. FOLLOWED QRH PROBLEM DIDN'T GO AWAY. REMOVED AND REPLACED HYD SYSTEM NR 3 RESERVOIR IAW AMM 29-12-30-000/400-801. - [SDR VNAA2026052918301](https://openairdocs.org/sdr/VNAA2026052918301.md): Tire · blown · May 27, 2026 · N567NN · Cndair CL6002D24 · Tire > NUMBER 3 TIRE BLEW ON TAKE OFF ROLL / REMOVED AND REPLACED RH IB MLG WHEEL AND TIRE ASSEMBLY IAW AMM 32-41-01-000/400-801-A01-PSA. - [SDR VNAA2025111711101](https://openairdocs.org/sdr/VNAA2025111711101.md): Pcu · faulted · Nov 14, 2025 · N567NN · Cndair CL6002D24 · Drag Control System > OTBD FLT SPOILERS & OTBD SPOILERON INFLIGHT CAUTION MSG. REMOVED AND REPLACED LT OTBD MULTI FUNCTION SPOILER PCU IAW AMM 27-62-01-000-400-801-A02-PSA, AND PERFORMED AN OPS TEST OF MFS PCU IAW AMM 27-62-01-710-801-A01 OPS TESTED GOOD. - [SDR VNAA2025031411101](https://openairdocs.org/sdr/VNAA2025031411101.md): Window · cracked · Mar 11, 2025 · N567NN · Cndair CL6002D24 · Flight Compartment Windows > DURING CLIMB CAUTION MSG LEFT WINDOW HEAT THEN LEFT WINDSHIELD CRACKED IN MULTI PLACES. / REMOVED AND REPLACED THE LH WINDOW IAW CRJ 900 AMM 56-12-01-000/400-801-A01-PSA. OPS CHECK GOOD. LEAK CHECK GOOD. - [SDR VNAA2024071511102](https://openairdocs.org/sdr/VNAA2024071511102.md): Pseu · unserviceable · Jul 12, 2024 · N567NN · Cndair CL6002D24 · Landing Gear System > THROUGH ALL PHASES OF FLIGHT WITH GEAR UP WE HEARD A LOUD BANG AROUND THE NOSE AREA ACCOMPANIED WITH A PROX SYS FAULT STATUS AND GEAR POSITION INDICATIONS APPEARED ON EICAS. THESE EVENTS OCCURED AROUND 4 TIMES THROUGHOUT FLIGHT. UPON GEAR EXTENTION ALL INDICAT - [SDR VNAA20240531031](https://openairdocs.org/sdr/VNAA20240531031.md): Floor Support · cracked · May 1, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure > SECONDARY NRC IN REFERENCE NRC:156 AFTER FLOOR SUPPORT ANGLE RBL 12 REMOVAL, CRACK ON ANGLE WAS FOUND. ANGLE WAS REPLACED PER CRJ 900 SRM 51-42-20-001-001-A01 AND SRM 51-42-06-001-001-A01 - [SDR VNAA20240531030](https://openairdocs.org/sdr/VNAA20240531030.md): Bulkhead Web · corroded · May 1, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Bulkhead > AFTER RIVETS REMOVAL, FOUND CORROSION ON WEB, LOWER FS 280, RBL 12'' TO RBL 30''. WEB, LOWER FS 280, RBL 12'' TO RBL 30'' WAS REPAIRED PER CRJ900 SRM 53-11-10-201-004-A01 - [SDR VNAA20240531029](https://openairdocs.org/sdr/VNAA20240531029.md): Floorbeam · corroded · May 1, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Floor Beam > AFTER FLOOR PANEL SUPPORT ANGLE REMOVAL IN REF NRC 00075, CORROSION ON TRANSVERSE BEAM FS280 WAS FOUND BTW BL 0 - RBL 12. DUE EXCESSIVE CORROSION ON TRANSVERSE BEAM FS280 RH IT IS OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER C - [SDR VNAA20240531028](https://openairdocs.org/sdr/VNAA20240531028.md): Floor Support · cracked · May 1, 2024 · N567NN · Cndair CL6002D24 · 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). FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTU - [SDR VNAA20240531026](https://openairdocs.org/sdr/VNAA20240531026.md): Canister · cracked · Apr 30, 2024 · N567NN · Cndair CL6002D24 · Wing Main, Frame Structure > REF. TO: DURING INSPECTION OF THE TASK CARD TRFKE000WL78: 600-08E2-JIC IT WAS DETECTED CRACK IN CANISTER WELDED NO.3 STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO.3 STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. RE - [SDR VNAA20240531027](https://openairdocs.org/sdr/VNAA20240531027.md): Post · cracked · Apr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON RIVETS AREA BELOW FLOOR AT BULKHEAD DOOR POST, BTW RBL 12 AND FS 280.00. CRACK ON RIVETS AREA BELOW FLOOR AT BULKHEAD DOOR POST, BTW RBL 12 AND FS 280.00 WAS REPAIRED PER REO 690-53-11-1748 REV. - - [SDR VNAA20240531023](https://openairdocs.org/sdr/VNAA20240531023.md): Fitting · corroded · Apr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (3EA) (FLOOR STRUCTURE AREA) FITTING OF ENTRANCE COMPARTMENT (3EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 - [SDR VNAA20240531019](https://openairdocs.org/sdr/VNAA20240531019.md): Seat Track · corroded · Apr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > INITIAL INSPECTION: CORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 913.00 (5EA). RH SIDE SEAT RAIL BTW FS744.15 TO FS 913.00 (5EA) WERE EVALUATED, ARE OUT OFF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ90 - [SDR VNAA20240531018](https://openairdocs.org/sdr/VNAA20240531018.md): Seat Track · corroded · Apr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON SEAT RAILS LBL27 (1EA) BTW FS 485.00 TO FS 501.00 AT PASSENGER CABIN. SEAT RAILS LBL27 (1EA) BTW FS 485.00 TO FS 501.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00 - [SDR VNAA20240531017](https://openairdocs.org/sdr/VNAA20240531017.md): Seat Track · corroded · Apr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > INITIAL INSPECTION: CORROSION ON SEAT RAILS LBL9 BTW FS 364.00 TO FS 485.00 (1EA) AND FS 581.00 TO FS 693.00 (2EA) AT PASSENGER CABIN. SEAT RAILS LBL9 BTW FS 364.00 TO FS 485.00 (1EA) AND FS 581.00 TO FS 693.00 (2EA) WERE EVALUATED, ARE OUT OFF LIMITS PER CRJ - [SDR VNAA20240531016](https://openairdocs.org/sdr/VNAA20240531016.md): Seat Track · corroded · Apr 29, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON SEAT RAILS RBL9 (5EA) BTW FS 349.00 TO FS 693.00 AT PASSENGER CABIN. SEAT RAILS RBL9 (5EA) BTW FS 349.00 TO FS 693.00 AT PASSENGER CABIN. WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49 - [SDR VNAA20240531015](https://openairdocs.org/sdr/VNAA20240531015.md): Hinge Fitting · excess play · Apr 29, 2024 · N567NN · Cndair CL6002D24 · Vertical Stabilizer > AFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 3 AT VERTIC•A L STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103. REV.B. - [SDR VNAA20240531012](https://openairdocs.org/sdr/VNAA20240531012.md): Web · cracked · Apr 28, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193. ELECTRICAL BAY FLOOR WEB RH SIDE (BELOW ADG SUPPORT DOUBLER) FS193. WAS REPAIRED PER REO 690-53-11-1762 REV - - - [SDR VNAA20240531014](https://openairdocs.org/sdr/VNAA20240531014.md): Post · corroded · Apr 27, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Bulkhead > DURING INSPECTION OF THE TASK CARD 53-10-219, IT WAS DETECTED CORROSION ON BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00 BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00 WERE REPAIRED PER REO 690-53-11-1752 REV- - [SDR VNAA20240531013](https://openairdocs.org/sdr/VNAA20240531013.md): Floorbeam · corroded · Apr 27, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Floor Beam > INITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE FS280 (RBL9 TO LBL9) AT CABIN FLOOR STRUCTURE. FLOOR PANEL SUPPORT ANGLE FS280 (RBL9 TO LBL9) AT CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. - [SDR VNAA20240531011](https://openairdocs.org/sdr/VNAA20240531011.md): Bracket · corroded · Apr 25, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON MACHINED (8 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARMENT. MACHINED (8 EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE REPLACED PER CRJ900 SRM 51-42-20-001-001-A01 AND SRM 51-42-22-001-001-A01 - [SDR VNAA20240531010](https://openairdocs.org/sdr/VNAA20240531010.md): Plate · corroded · Apr 25, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Structure > CORROSION ON KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. RIS- WS 8070-1. CORROSION ON KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WERE REPLACED PER CRJ900 SRM 51-42-06-001- - [SDR VNAA20240531009](https://openairdocs.org/sdr/VNAA20240531009.md): Counterbalance · worn · Apr 25, 2024 · N567NN · Cndair CL6002D24 · Cargo/Baggage Doors > WEAR ON AFT COUTERBALANCE ARM AT FWD BAGGAGE BAY DOOR. WEAR ON AFT COUTERBALANCE ARM AT FWD BAGGAGE BAY DOOR BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01, ZONE 1,2 AND 3 WAS MEASURED AND FOUND WITHIN OF LIMITS PER CRJ900 SRM 52-35-09-201-001-A01 AND LOWER - [SDR VNAA20240531008](https://openairdocs.org/sdr/VNAA20240531008.md): Counterbalance · worn · Apr 25, 2024 · N567NN · Cndair CL6002D24 · Cargo/Baggage Doors > WEAR ON FWD / AFT COUTERBALANCE ARMS AT CENTER BAGGAGE BAY DOOR. RIS- WS 8070-1. WEAR ON FWD / AFT COUTERBALANCE ARMS AT CENTER BAGGAGE BAY DOOR BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01, ZONE 1,2 AND 3 WAS MEASURED AND FOUND WITHIN OF LIMITS PER CRJ9 - [SDR VNAA20240531007](https://openairdocs.org/sdr/VNAA20240531007.md): Skin · worn · Apr 25, 2024 · N567NN · Cndair CL6002D24 · Wing, Plate/Skin > WEAR ON SETTLEMENT AREA OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN. WERE REPAIRED PER REO 690-57-21-466 REV. -- - [SDR VNAA20240531006](https://openairdocs.org/sdr/VNAA20240531006.md): Skin · worn · Apr 25, 2024 · N567NN · Cndair CL6002D24 · Wing, Plate/Skin > IN REFERENCE TO RC TRFKE001HT5B: WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21 - [SDR VNAA20240531005](https://openairdocs.org/sdr/VNAA20240531005.md): Skin · damaged · Apr 25, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin > LIGHTNING STRIKE (1EAS) ON FUSELAGE SKIN AT FS 333 BTW STGR 22RH TO STGR 23RH. LIGHTNING STRIKE (1EAS) ON FUSELAGE SKIN AT FS 333 BTW STGR 22RH TO STGR 23RH WAS REPAIRED PER REO 690-53-21-1767 REV -A - [SDR VNA20240531003](https://openairdocs.org/sdr/VNA20240531003.md): Drag Angle · cracked · Apr 25, 2024 · N567NN · 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 BL0.00). (SM) CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR D - [SDR VNAA20240531025](https://openairdocs.org/sdr/VNAA20240531025.md): Seat Track · corroded · Apr 18, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS, LOCATED BTW FS=847 TO FS=977 AND LBL 9'' / RBL 9''. FLOOR SEAT RAILS, LOCATED BTW FS=847 TO FS=977 AND LBL 9'' / RBL 9''WERE EVALUATED, ARE OUT OFF LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 AND REPLACED PE - [SDR VNAA20240531024](https://openairdocs.org/sdr/VNAA20240531024.md): Fitting · corroded · Apr 18, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON SETTLEMENT FITTING OF GALLEY 1 (2EA) (FLOOR STRUCTURE AREA) FITTING OF GALLEY 1 (2EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03, AND WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 - [SDR VNAA20240531021](https://openairdocs.org/sdr/VNAA20240531021.md): Seat Track · corroded · Apr 18, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > INITIAL INSPECTION: CORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WERE EVALUATED,ARE OUT OFF LIMITS PER CRJ900 SRM 53- 21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND - [SDR VNAA20240531020](https://openairdocs.org/sdr/VNAA20240531020.md): Seat Track · corroded · Apr 18, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) INITIAL INSPECTION: CORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 942.00 (6EA) LH SIDE SEAT RAIL BTW FS744.15 TO FS 942.00 (6EA) WERE EVALUATED, ARE OUT OFF LIMITS PER CRJ-900 SRM 53-41-49-10 - [SDR VNAA20240531004](https://openairdocs.org/sdr/VNAA20240531004.md): Housing · worn · Apr 18, 2024 · N567NN · Cndair CL6002D24 · Cargo/Baggage Doors > WEAR ON HOUSING OF EXTERNAL HANDLE AT AFT BAGGAGE-BAY DOOR. WEAR ON HOUSING OF EXTERNAL HANDLE AT AFT BAGGAGE-BAY DOOR WAS REPAIRED PER REO 670-52-31-031 REV -B - [SDR VNAA202402050032](https://openairdocs.org/sdr/VNAA202402050032.md): Floorbeam · cracked · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Floor Beam > CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1661 RE - [SDR VNAA202402050031](https://openairdocs.org/sdr/VNAA202402050031.md): Buttstrap · corroded · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Structure > CORROSION ON FUSELAGE CIRCUMFRENTIAL JOINT BTW FS280.00/ FS282.86 AND STGR 24LH/23RH. CORROSION ON FUSELAGE CIRCUMFRENTIAL JOINT BTW FS280.00/ FS282.86 AND STGR 24LH/23RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, BTW STGR 27 TO STGR 23R WAS EVALUATED - [SDR VNAA202402050030](https://openairdocs.org/sdr/VNAA202402050030.md): Intercostal · corroded · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 394 TO FS= 409 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTALS (2 EAS) IN STA. FS= 394 TO FS= 409 NEAR STGR 27 AT MAIN AVIONICS BAY WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND REP - [SDR VNAA202402050029](https://openairdocs.org/sdr/VNAA202402050029.md): Intercostal · corroded · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL IN STA. FS= 349 TO FS= 364 NEAR STGR 27 RH SIDE AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL IN STA. FS= 349 TO FS= 364 NEAR STGR 27 RH SIDE AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND - [SDR VNAA202402050028](https://openairdocs.org/sdr/VNAA202402050028.md): Web · cracked · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB. UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01 - [SDR VNAA202402050027](https://openairdocs.org/sdr/VNAA202402050027.md): Skin · nicked · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin > SEVERAL NICKS ON SKIN (ZONE 1) BTW FS501.00 TO FS517.00 AND STGR 21 LH TO STGR 25 LH (ZONA 2) BTW FS 613.00 TO FS 629.00 AND STGR 21 LH TO STGR 25 LH AT FUSELAGE. SKIN (ZONE 1) BTW FS501.00 TO FS517.00 AND STGR 21 LH TO STGR 25 LH (ZONA 2) BTW FS 613.00 TO F - [SDR VNAA202402050026](https://openairdocs.org/sdr/VNAA202402050026.md): Skin · damaged · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin > LIGHTING STRIKE BTW FS280.00 TO FS295.00 AND BTW STGR 17 TO STGR 16 RH (1EA) LIGHTING STRIKE BTW FS379.00 TO FS394.00 AND BTW STGR 17 TO STGR 18 RH (1EA) AT SELAGE SKIN. LIGHTING STRIKE BTW FS280.00 TO FS295.00 AND BTW STGR 17 TO STGR 16 RH (1EA) LIGHTING ST - [SDR VNAA202402050025](https://openairdocs.org/sdr/VNAA202402050025.md): Skin · nicked · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin > SEVERAL NICKS ON FUSELAGE SKIN BTW STA 1000.00 TO STA 1069.75 AND BTW STGR 21RH TO STGR 27. SEVERAL NICKS ON FUSELAGE SKIN BTW STA 1000.00 TO STA 1069.75 AND BTW STGR 21RH TO STGR 27 WAS REPAIRED PER REO 690-53-61-1331 REV. -- - [SDR VNAA202402050024](https://openairdocs.org/sdr/VNAA202402050024.md): Skin · worn · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Wing, Plate/Skin > WEAR ON SETTLEMENT AREA OF FAIRING 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN. SETTLEMENT AREAS OF FAIRINGS 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01; SETTLEMENT AREAS OF - [SDR VNAA202402050023](https://openairdocs.org/sdr/VNAA202402050023.md): Skin · worn · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Wing, Plate/Skin > WEAR ON SETTLEMENT AREA OF FAIRINGS 583AB, 586AB, 592AB, 595AB AND 597AB AT LH WING LOWER SKIN. SETTLEMENT AREAS OF FAIRINGS 583AB, 586AB, 592AB, 595AB AND 597AB AT LH WING LOWER SKIN WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01; SETTLEMENT AREAS OF F - [SDR VNAA2024020650022](https://openairdocs.org/sdr/VNAA2024020650022.md): Seat Track · corroded · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 785.15 TO FS 830.40. CORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS 785.15 TO FS 830.40 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02, WAS FABRICATED PER CRJ900 SRM 53-00-49-201-002- - [SDR VNAA202402050021](https://openairdocs.org/sdr/VNAA202402050021.md): Seat Track · corroded · Feb 6, 2024 · N567NN · Cndair CL6002D24 · 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, WAS FABRICATED PER CRJ900 SRM 53-00-49-201-002-A01 AND WAS R - [SDR VNAA202402050020](https://openairdocs.org/sdr/VNAA202402050020.md): Skin · dented · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin > GOUGE AND DENT BELOW VENTRAL FIN FARING RH AREA BTW FS 1069.75 - FS 1088.00 AND STGR 21 - 22 RH AT REAR FUSELAGE. BELOW VENTRAL FIN FARING RH AREA BTW FS 1069.75 - FS 1088.00 AND STGR 21 - 22 RH AT REAR FUSELAGE WAS REPAIRED PER REO 690-53-00-548 REV. -- - [SDR VNAA202402050019](https://openairdocs.org/sdr/VNAA202402050019.md): Rib · cracked · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK WAS FOUND ON RIB LEADING EDGE SS57.16 AT RH WING. RIB LEADING EDGE SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV - - - [SDR VNAA202402050018](https://openairdocs.org/sdr/VNAA202402050018.md): Hinge Fitting · excess play · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Vertical Stabilizer > 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. HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL 2103 REV - [SDR VNAA202402050017](https://openairdocs.org/sdr/VNAA202402050017.md): Floor Support · corroded · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1031.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1031.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1333 REV. -- - [SDR VNAA202402050016](https://openairdocs.org/sdr/VNAA202402050016.md): Floor Support · corroded · Feb 6, 2024 · N567NN · Cndair CL6002D24 · Fuselage Main, Structure > CORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1334 REV. Next page: https://openairdocs.org/aircraft/N567NN/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 = 'N567NN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N567NN/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.