# Service difficulty reports: N562NN

A list on [N562NN](https://openairdocs.org/aircraft/N562NN.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 · 65 reports

- [SDR VNAA2026090924601](https://openairdocs.org/sdr/VNAA2026090924601.md): Start Valve · open · Sep 8, 2026 · N562NN · Cndair CL6002D24 · Engine Start Valves/Controls
  > R START VLV OPEN IN FLIGHT C/A REMOVED AND REPLACED STARTER AND STARTER CONTROL VALVE IAW AMM 80-11-01-000/400-801-AO1-PSA
- [SDR VNAA2026032615201](https://openairdocs.org/sdr/VNAA2026032615201.md): Sensor · out of adjust · Mar 22, 2026 · N562NN · Cndair CL6002D24 · Door Warning System
  > ON CLIMBOUT FWD SERVICE DOOR CAUTION ILLUMINATED. ADJUSTED SERVICE DOOR PROX SENSOR PX38 IAW AMM 52-70-06-820-802-A01. SENSOR READINGS WITHIN ACCEPTABLE LIMITS.
- [SDR VNAA2025022811101](https://openairdocs.org/sdr/VNAA2025022811101.md): Pcu · faulted · Feb 26, 2025 · N562NN · Cndair CL6002D24 · Drag Control System
  > OB SPOILERONS CAUTION AND OB FLTS SPOILERS CAUTION MSGS IN FLIGHT / REMOVED AND REPLACED LH OUTBOARD MULTI FUNCTION SPOILER PCU IAW CRJ 900 AMM 27-62-01-000/400-801-A02. OPERATIONAL CHECK GOOD.
- [SDR VNAA2025012311101](https://openairdocs.org/sdr/VNAA2025012311101.md): Unknown · odor · Jan 22, 2025 · N562NN · Cndair CL6002D24 · Air Distribution System
  > SLIGHT BURNING SMELL FROM AFT CABIN DURING TAKEOFF. THE SMELL WAS IN THE CABIN AND DISSIPATED QUICKLY, WITH NO MEDICAL ATTENTION REQUIRED. / TROUBLESHOT SMELL IAW CRJ900 FIM 21-22-00-810-806. PERFORMED LH AND RH ENGINE RUN IAW CRJ900 AMM 71-00-00-866-806-A02-P
- [SDR VNAA2024041211101](https://openairdocs.org/sdr/VNAA2024041211101.md): Unknown · out of position · Apr 10, 2024 · N562NN · Cndair CL6002D24 · Standard Practices/Structures
  > LEFT BLEED DUCT WARNING MSG IN FLIGHT / INSP AND FOUND MT138 TOUCHING THE LH WING SOV AND COWL SOV. ADJUSTED AND OPS CHECK MT138 IAW CRJ 900 FIM 36ˆ’21ˆ’01ˆ’810ˆ’818. OPS CHECK. NO MSG REAPPEAR.
- [SDR VNAA202401050018](https://openairdocs.org/sdr/VNAA202401050018.md): Aileron · corroded · Nov 29, 2023 · N562NN · Bombdr CL6002D15 · Ailerons
  > CORROSION ON BORE AT CENTER FITTING LUGS "L2" AND "L5" AT LH AILERON. BORE AT CENTER FITTING LUGS "L2" AND "L5" AT LH AILERON WERE REPAIRED PER REO 670-57-61-107 REV. -B AND REO 690-57-61-312 REV. - -
- [SDR VNAA202401050023](https://openairdocs.org/sdr/VNAA202401050023.md): Rib · cracked · Nov 24, 2023 · N562NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > CRACK WAS FOUND ON RIB LEADING EDGE SS57.16 AT LH WING. RIB LEADING EDGE SS57.16 AT LH WING WAS REPAIRED PER REO 690-57-41-240. REV.--
- [SDR VNAA202401050029](https://openairdocs.org/sdr/VNAA202401050029.md): Canister · cracked · Nov 18, 2023 · N562NN · Bombdr CL6002D15 · Wing Structure
  > CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV.- -
- [SDR VNAA202401050028](https://openairdocs.org/sdr/VNAA202401050028.md): Canister · cracked · Nov 18, 2023 · N562NN · Bombdr CL6002D15 · Wing Structure
  > CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV.- -
- [SDR VNAA202401050021](https://openairdocs.org/sdr/VNAA202401050021.md): Skin · scratched · Nov 18, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > SEVERAL SCRATCHES ON EXTERNAL FUSELAGE SKIN BELOW VENTRAL FIN FAIRINGS COVER LH AT REAR FUSELAGE. SCRATCHES ON EXTERNAL FUSELAGE SKIN BELOW VENTRAL FIN FAIRINGS COVER LH AT REAR FUSELAGE WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-A01 AND EVALUATED WITHIN LI
- [SDR VNAA202401050020](https://openairdocs.org/sdr/VNAA202401050020.md): Rib · cracked · Nov 18, 2023 · N562NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > DURING INSPECTION OF THE TASK CARD: 57-20-201_R/H-JIC. 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 VNAA202401050027](https://openairdocs.org/sdr/VNAA202401050027.md): Seat Track · corroded · Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS677.00 TO FS977.00 ON LBL9 AND RBL9 (4EA). SEAT RAIL BTW FS677.00 TO FS977.00 ON LBL9 AND RBL9 (4EA) WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG. A12
- [SDR VNAA202401050026](https://openairdocs.org/sdr/VNAA202401050026.md): Seat Track · corroded · Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS=785.15 AND FS=954.00. SIDE SEAT RAIL OF STRG 15LH BETWEEN FS=785.15 AND FS=954.00 WAS REPLACED PER AMM 53-00-49 (CONFIG. A12).
- [SDR VNAA202401050025](https://openairdocs.org/sdr/VNAA202401050025.md): Seat Track · corroded · Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SIDE SEAT RAIL OF STRG 15RH BETWEEN FS=785.15 AND FS=954.00. SIDE SEAT RAIL OF STRG 15RH BETWEEN FS=785.15 AND FS=954.00 WAS REPLACED PER AMM 53-00-49 (CONFIG. A12).
- [SDR VNAA202401050024](https://openairdocs.org/sdr/VNAA202401050024.md): Seat Track · corroded · Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH AND LH SIDE SEAT RAILS BTW FS=744 TO FS=761. RH AND LH SIDE SEAT RAILS BTW FS=744 TO FS=761 WAS REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG. A12).
- [SDR VNAA202401050012](https://openairdocs.org/sdr/VNAA202401050012.md): Seat Track · corroded · Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Structure (General)
  > CORROSION AT SEAT RAIL LBL9 BETWEEN FS]=597 TO FS=661. SEAT RAIL LBL9 BETWEEN FS]=597 TO FS=661 WAS REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG. A12
- [SDR VNAA202401050011](https://openairdocs.org/sdr/VNAA202401050011.md): Seat Track · corroded · Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL RBL 9 BTW FS480 TO FS 549 AND FROM FS 597 TO FS661. SEAT RAIL RBL 9 BTW FS480 TO FS 549 AND FROM FS 597 TO FS661 PER CRJ900 AMM 53-00-49 CONFIG A12
- [SDR VNAA202401050010](https://openairdocs.org/sdr/VNAA202401050010.md): Seat Track · corroded · Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS=669 AND FS=720. RH SIDE SEAT RAIL BTW FS=669 AND FS=720 WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG. A12).
- [SDR VNAA202401050009](https://openairdocs.org/sdr/VNAA202401050009.md): Seat Track · corroded · Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS=669 AND FS=720. LH SIDE SEAT RAIL BTW FS=669 AND FS=720 WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG. A12)
- [SDR VNAA202401050008](https://openairdocs.org/sdr/VNAA202401050008.md): Angle · corroded · Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > IN REF TO: DURING INSPECTION OF TASK 53-20-315-JIC,WAS FOUND CORROSION ON ANGLE BTW FS=319.70/FS=349.00 WL72.50. ANGLE BTW FS=319.70/FS=349.00 WL72.50 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.
- [SDR VNAA202401050015](https://openairdocs.org/sdr/VNAA202401050015.md): Skin · damaged · Nov 15, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Structure (General)
  > IN REF TO TRFKE00ABL9H SRM 53-00-00-201-003 PERM REPAIR BEFORE NEXT HMV FUSELAGE LIGHTNING STRIKE DAMAGE- TYPE 3 DAMAGE AROUND FASTENER CSK BTY THE NEXT HMV VISIT. PERFORM PERM REPAIR PER SRM 53-00-00-201-003-A03- PERM REPAIR DISPOSITION TO FUSELAGE SKIN AROUN
- [SDR VNAA202401050014](https://openairdocs.org/sdr/VNAA202401050014.md): Skin · damaged · Nov 15, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > IN REF TO TRFKE00ABL96:SRM-53-00-00-201-003_TYPE_1-2; PERM REPAIR BEFORE NEXT HMV - FUSELAGE LIGHTNING STRIKE DAMAGE - TYPE 1: DAMAGE ON SKIN ONLY BY THE NEXT HEAVY MAINTENANCE VISIT (HMV), PERFORM PERMANENT REPAIR PER SRM 53-00-00-201-003-A03 SECTION 5.A.(3)
- [SDR VNAA202401050007](https://openairdocs.org/sdr/VNAA202401050007.md): Door · corroded · Nov 15, 2023 · N562NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > CORROSION ON KICKPLATE AT PASSENGER DOOR. KICKPLATE AT PASSENGER DOOR WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.
- [SDR VNAA202401050004](https://openairdocs.org/sdr/VNAA202401050004.md): Skin · damaged · Nov 15, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE FS 171.00 WITHIN 1,628.27 FH (BEFORE 20,510.04 FH) AFTER ACCOMPLISHMENT OF SECTION I, REPAIR, OR REPLACE THE DISCREPANT AREAS IAW APPROVED PROCEDURES. LIGHTNING STRIKE WAS FOUND ON LH SKIN PANEL FS 171 & STGR23LH WAS REPAIRED PER REO 6
- [SDR VNAA202401050003](https://openairdocs.org/sdr/VNAA202401050003.md): Striker · cracked · Nov 15, 2023 · N562NN · Bombdr CL6002D15 · Passenger/Crew Doors
  > IN REF TO TRFKE009YXZ2:EA23-C9-53-0075; 2004.6FH PERM REPAIR - PAX DOOR SEAL STRIKER WITHIN 2004.6 FH (BEFORE 20,510.03 FH) REPLACE THE DISCREPANT ITEM IAW APPROVED PROCEDURES. DAMAGE TO THE PAX DOOR STRIKER, UPPER SEAL AT FS 349.00 WAS REPAIRED PER CRJ900 SR
- [SDR VNAA202401050002](https://openairdocs.org/sdr/VNAA202401050002.md): Rib · worn · Nov 15, 2023 · N562NN · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > IN REF TO TRFKE009BBKS:EA22-C9-57-1108; PERM REPAIR - RIB BAT WS14.50 WITHIN 2,856.35 FHS FROM IR (BEFORE 20,510.03 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. WEAR DAMAGE TO BATT RIB AT WS14.50, LHS WAS REPAIRED PER RE
- [SDR VNAA202401050001](https://openairdocs.org/sdr/VNAA202401050001.md): Frame · corroded · Nov 15, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME FS= 310 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS= 310 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-005-A01.
- [SDR VNAA202401040037](https://openairdocs.org/sdr/VNAA202401040037.md): Skin · worn · Nov 14, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > WEAR ON FUSELAGE EXTERNAL SKIN, LOCATED BTW FS= 897.70 / FS=927.00 AND STGR 27. WEAR ON FUSELAGE EXTERNAL SKIN, LOCATED BTW FS= 897.70 / FS=927.00 AND STGR 27 WAS REPAIRED PER REO 690-53-51-390 REV - - DISPOSITION.
- [SDR VNAA2024010400003](https://openairdocs.org/sdr/VNAA2024010400003.md): Skin · nicked · Nov 14, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > SEVERAL NICKS ON LOWER FUSELAGE, FS235.00 TO FS310.00 BTW STGR 25RH TO STGR 25LH. SEVERAL NICKS ON LOWER FUSELAGE, FS235.00 TO FS310.00 BTW STGR 25RH TO STGR 25LH WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND LOWER SKIN FWD FUSELAGE BTW FS235 TO FS28
- [SDR VNAA202401040035](https://openairdocs.org/sdr/VNAA202401040035.md): Skin · worn · Nov 14, 2023 · N562NN · Bombdr CL6002D15 · Wing, Nacelle/Pylon Attach Fittings
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB AND 683AB) AT RH/LH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB AND 683AB) AT RH/LH WING LOWER SKIN WERE BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND EVALUATED, THEREFORE IT IS WITHI
- [SDR VNAA202401050006](https://openairdocs.org/sdr/VNAA202401050006.md): Drag Angle · cracked · Nov 12, 2023 · N562NN · Bombdr CL6002D15 · Vertical Stabilizer, Spar/Rib
  > INITIAL INSPECTION': CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD 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 FWD DRAG ANGLE BTW 55.625% STGR DA
- [SDR VNAA202401050005](https://openairdocs.org/sdr/VNAA202401050005.md): Drag Angle · cracked · Nov 12, 2023 · N562NN · Bombdr CL6002D15 · Vertical Stabilizer, Spar/Rib
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STRG DATUM TO 67.5% REAR SPAR DATUM TRACE BL0.00 SM. CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01.
- [SDR VNAA202401050022](https://openairdocs.org/sdr/VNAA202401050022.md): Fitting · damaged · Nov 11, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Structure (General)
  > DAMAGED JACKING PAD HELICOIL INSERT ON WING RH. DURING INSPECTION AFTER REMOVE HELICOIL INSERT IT WAS DETECTED DAMAGE THREADS AT THE PERMANENT REPAIR PREVIOUS,THEREFORE JACKING FITTING ASSY WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.
- [SDR VNAA202401050019](https://openairdocs.org/sdr/VNAA202401050019.md): Aileron · corroded · Nov 10, 2023 · N562NN · Bombdr CL6002D15 · Ailerons
  > CORROSION ON BORE AT CENTER HINGE FITTING INBOARD LUGS AT AILERON RH. BORE AT CENTER HINGE FITTING INBOARD LUGS AT AILERON RH. WERE REPAIRED PER REO 670-57-61-107 REV. -B
- [SDR VNAA202310011111](https://openairdocs.org/sdr/VNAA202310011111.md): Sensor · unserviceable · Sep 27, 2023 · N562NN · Cndair CL6002D24 · Landing Gear Brake System
  > BRAKE OVERHEAT WARNING ON CLIMB OUT, RETURN TO FIELD, EMERGEMCY DECLARED / PLACED #3 BRAKE TEMP READOUT ON DEFERRAL PER MEL 32-46-01 CAT C. C/W M FUNC BY INSTALLING DUST CAPS AND SECURING HARNESS. OPTION 4. REMOVED AND REPLACED #3 BRAKE TEMPERATURE PROBE IAW
- [SDR VNAA202204101111](https://openairdocs.org/sdr/VNAA202204101111.md): Control Valve · unserviceable · Apr 7, 2022 · N562NN · Cndair CL6002D24 · Air Distribution System
  > DURING TAXI INTO THE GATE IN OAJ THE FA REPORTED TO THE FLIGHT DECK THAT SHE SAW SMOKE IN THE CABIN. THE CREW REPORTED THAT APPROXIMATELY 30 SECONDS LATER A RIGHT PACK AUTO-FAIL MESSAGE OCCURRED. THE A/C BLOCKED IN AND DEPLANED NORMALLY AT THE GATE. RH PACK AU
- [SDR VNAA202112151111](https://openairdocs.org/sdr/VNAA202112151111.md): Skin Panel · scratched · Dec 15, 2021 · N562NN · Cndair CL6002D24 · Emergency Exits
  > DURING ROUTINE MAINTENANCE AT BIRMINGHAM, AL (BHM). THE MAINTENANCE TEAM REPORTS A SCRATCH WAS FOUND RH AFT EMERGENCY EXIT SKIN (P/N SH670-36508-11). THE SCRATCH IS 0.006Ï¿½ DEEP AND 0.006Ï¿½ WIDE AND.5Ï¿½ LONG. THE SKIN PANEL, P/N SH670-36508-11, IS MADE FRO
- [SDR VNAA202112131111](https://openairdocs.org/sdr/VNAA202112131111.md): Pump · failed · Dec 11, 2021 · N562NN · Cndair CL6002D24 · Hydraulic Pump (Electric/Engine), Main
  > AIRCRAFT LOST NUMBER 3 HYD SYSTEM ON APPROACH INTO CLE. THEY FOLLOWED THE QRH AND LANDED WITH FLAPS 20. THEY DECLARED AN EMERGENCY. THEY DID NOT BRACE. THEY DID ROLE TRUCKS, AND NEEDED TO BE TOWED OFF THE RUNWAY. HYD 3 LOW / HYD PUMP 3A CAUTION MSGS IN CRUISE,
- [SDR VNAA202108171111](https://openairdocs.org/sdr/VNAA202108171111.md): Sensor · malfunctioned · Aug 13, 2021 · N562NN · Cndair CL6002D24 · Landing Gear Brake System
  > RH BRAKE OVER HEAT MSG AROUND FL 170. RAN THE QRH THEN THE MSG CLEARED. CREW THEN UNDECLARED AND EMERGNECY AND LANDED IN KCLT WITHOUT ANY ISSUES. RH IB BRAKE MADE BRAKE OVHT WARNING MESSAGE. COMPLIED WITH QRC AND QRH / DEFERRED #3 BRAKE TEMP SENSOR INDICATIO
- [SDR VNAA202107291112](https://openairdocs.org/sdr/VNAA202107291112.md): Thermocouple · false indication · Jul 26, 2021 · N562NN · Cndair CL6002D24 · Landing Gear Brake System
  > OCCURRED ON THE GROUND THE ENTIRE TIME. AS THE CREW WAS TAXIING OUT, THEY RECEIVED A BRAKE OVERHEAT CAUTION MESSAGE. THE CREW DECLARED WITH ATC ON THE GROUND, AND HAD FIRE & RESCUE TRUCKS FOLLOW THEM BACK TO THE GATE IN CASE ANY BRAKE COMPONENTS IGNITED. INFRA
- [SDR VNAA202106221111](https://openairdocs.org/sdr/VNAA202106221111.md): Proximity Sensor · out of adjust · Jun 19, 2021 · N562NN · Cndair CL6002D24 · Landing Gear Position and Warning
  > NOSE GEAR DID NOT RETRACT AND CREW RECEIVED A GEAR INDICATION WARNING. THEY RAN THE QRH, DECLARED AN EMERGENCY, AND RETURNED TO CVG. THEY LANDED SAFELY WITH NO ADDITIONAL INCIDENT. GEAR DISAGREE WARNING MESSAGE. NOSE GEAR DID NOT RETRACT. / INTERROGATED MDC FO
- [SDR VNAA2020102911101](https://openairdocs.org/sdr/VNAA2020102911101.md): Bleed Valve · inoperative · Oct 28, 2020 · N562NN · Cndair CL6002D24 · Pneumatic Distribution System
  > LT BLEED DUCT WARNING MESSAGE APPEARED IN FLIGHT. AFT F/A CALLED AND ADVISED OF A BURNING SMELL WITH NO SIGN OF SMOKE. CABIN PRESSURE WAS INCREASING ROUGHLY 600 FT, PER MIN. PERFORMED QRH AND LANDED IN TYS.
- [SDR VNAA2020022499903](https://openairdocs.org/sdr/VNAA2020022499903.md): Floor Support · corroded · Feb 24, 2020 · N562NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > LH FLOOR SUPPORT AT FS 1047.00 APPROX AT FLOORBAORD 281JLF HAS SMALL AREA OF CORROSION. MARKED WITH ORANGE TAPE. N.UPTON 02/04/20 (ROSEM) M/A: 1. N/A C/A: 1. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW CRJ900 SRM 53-61-43-101-
- [SDR VNAA2020022499003](https://openairdocs.org/sdr/VNAA2020022499003.md): Angle · corroded · Feb 24, 2020 · N562NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > FWD FUSELAGE F.S.280 FWD J-ANGLE CORODED AROUND CAMLOCK RECPICLS. (TK) M/A: 1. J CHANNEL FOUND TO BE OUT OF LIMITS IAW CRJ 900 SRM 53-00-00-19-001-A01. W.WILILAMS 02/05/20 C/A: 1. REMOVED J CHANNEL IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR VNAA2020022499902](https://openairdocs.org/sdr/VNAA2020022499902.md): Intercostal · corroded · Feb 24, 2020 · N562NN · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > TWO INTERCOSTALS CORRODED BETWEEN FS 349 ND FS364 AT STR 27. (TK) M/A: 1. UPON FURTHER INVESTIGATION FOUND INTERCOSTALS BETWEEN FS349 AND FS364 AT STGR 27 TO BE OUT OF LIMITS IAW CRJ 900 SRM 51-21-23-101-003-A02, REQUIRES REPLACEMENT. J.RAEDER 02/02/20 C/A: 1.
- [SDR VNAA2020022499901](https://openairdocs.org/sdr/VNAA2020022499901.md): Drag Angle · cracked · Feb 24, 2020 · N562NN · Bombdr CL6002D15 · Vertical Stabilizer
  > SUSPECTED CRACK ON LH AFT VERTICAL STAB DRAG ANGLE. F.HENRY 01/30/20 (ROSEM) M/A: 1. N/A. C/A: 1. PERFORMED EDDY CURRENT INSPECITON OF SUSPECTED CRACKED AREA IAW CRJ 900 NDTM PART 1 51-20-006-250-A01. FOUND ONE INDICATION 1" LONG BY 100% FSH IN THE RADIUS OF T
- [SDR VNAA2019052111102](https://openairdocs.org/sdr/VNAA2019052111102.md): Window · cracked · May 21, 2019 · N562NN · Cndair CL6002D24 · Flight Compartment Windows
  > CAPTAINS SIDE WINDOW CRACKED IN FLIGHT AT 8000 FEET. MAINTENANCE REMOVED AND REPLACED CAPTAINS SIDE WINDOW, OPS CHECK GOOD.
- [SDR VNAA2019042111103](https://openairdocs.org/sdr/VNAA2019042111103.md): Detector · failed · Apr 21, 2019 · N562NN · Cndair CL6002D24 · Trailing Flap Position Indicating System
  > CREW REPORTED FLAPS FAIL CAUTION ON ARRIVAL, BEFORE SETTING FLAPS. CREW FOLLOWED QRH, DECLARED AN EMERGENCY INTO CLT. CABIN WAS BRACED, AND TRUCKS ROLLED. FLIGHT LANDED WITHOUT INCIDENT AND WAS ABLE TO TAXI UNDER ITS OWN POWER TO GATE. R&R RH OB FLAP IB SKE
- [SDR VNAA2019100243101](https://openairdocs.org/sdr/VNAA2019100243101.md): Light · inoperative · Apr 3, 2019 · N562NN · Cndair CL6002D24 · Emergency Lighting
  > FWD LH EXTERIOR EMERGENCY LIGHT INOP. R AND R FWD LH EXTERIOR EMERGENCY LIGHT IAW CRJ 900 AMM 33-51-15-000/400-801-A05 OPS CHECK GOOD / "
- [SDR VNAA2018042711101](https://openairdocs.org/sdr/VNAA2018042711101.md): Unknown · odor · Apr 27, 2018 · N562NN · Cndair CL6002D24 · Air Distribution System
  > DURING CRUISE THE FA SMELLED SMOKE IN THE CABIN. THE CREW FOLLOWED THE CHECKLIST. ODOR DISSIPATED. DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. FIRE DEPT CHECKED OUT THE AIRCRAFT AND FOUND NO HOT SPOTS. MX RAN PACKS OFF EACH ENGINE AND THE AP

Next page: https://openairdocs.org/aircraft/N562NN/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 = 'N562NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N562NN/reports

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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.