N562NN

Service difficulty reports · 65

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR VNAA2026090924601Start Valve · openR START VLV OPEN IN FLIGHT C/A REMOVED AND REPLACED STARTER AND STARTER CONTROL VALVE IAW AMM 80-11-01-000/400-801-AO1-PSASep 8, 2026 · N562NN · Cndair CL6002D24 · Engine Start Valves/ControlsSDR VNAA2026032615201Sensor · out of adjustON 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.Mar 22, 2026 · N562NN · Cndair CL6002D24 · Door Warning SystemSDR VNAA2025022811101Pcu · faultedOB 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.Feb 26, 2025 · N562NN · Cndair CL6002D24 · Drag Control SystemSDR VNAA2025012311101Unknown · odorSLIGHT 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-PJan 22, 2025 · N562NN · Cndair CL6002D24 · Air Distribution SystemSDR VNAA2024041211101Unknown · out of positionLEFT 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.Apr 10, 2024 · N562NN · Cndair CL6002D24 · Standard Practices/StructuresSDR VNAA202401050018Aileron · corrodedCORROSION 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. - -Nov 29, 2023 · N562NN · Bombdr CL6002D15 · AileronsSDR VNAA202401050023Rib · crackedCRACK 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.--Nov 24, 2023 · N562NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA202401050029Canister · crackedCRACK 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.- -Nov 18, 2023 · N562NN · Bombdr CL6002D15 · Wing StructureSDR VNAA202401050028Canister · crackedCRACK 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.- -Nov 18, 2023 · N562NN · Bombdr CL6002D15 · Wing StructureSDR VNAA202401050021Skin · scratchedSEVERAL 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 LINov 18, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202401050020Rib · crackedDURING 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.--Nov 18, 2023 · N562NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA202401050027Seat Track · corrodedCORROSION 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. A12Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202401050026Seat Track · corrodedCORROSION 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).Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202401050025Seat Track · corrodedCORROSION 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).Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202401050024Seat Track · corrodedCORROSION 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).Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202401050012Seat Track · corrodedCORROSION 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. A12Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Structure (General)SDR VNAA202401050011Seat Track · corrodedCORROSION 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 A12Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202401050010Seat Track · corrodedCORROSION 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).Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202401050009Seat Track · corrodedCORROSION 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)Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202401050008Angle · corrodedIN 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.Nov 17, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202401050015Skin · damagedIN 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 AROUNNov 15, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Structure (General)SDR VNAA202401050014Skin · damagedIN 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) Nov 15, 2023 · N562NN · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202401050007Door · corrodedCORROSION 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.Nov 15, 2023 · N562NN · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA202401050004Skin · damagedLIGHTNING 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 6Nov 15, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202401050003Striker · crackedIN 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 SRNov 15, 2023 · N562NN · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA202401050002Rib · wornIN 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 RENov 15, 2023 · N562NN · Bombdr CL6002D15 · Wing, Rib/BulkheadSDR VNAA202401050001Frame · corrodedCORROSION 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.Nov 15, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA202401040037Skin · wornWEAR 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.Nov 14, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA2024010400003Skin · nickedSEVERAL 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 FS28Nov 14, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA202401040035Skin · wornWEAR 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 WITHINov 14, 2023 · N562NN · Bombdr CL6002D15 · Wing, Nacelle/Pylon Attach FittingsSDR VNAA202401050006Drag Angle · crackedINITIAL 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 DANov 12, 2023 · N562NN · Bombdr CL6002D15 · Vertical Stabilizer, Spar/RibSDR VNAA202401050005Drag Angle · crackedCRACK 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.Nov 12, 2023 · N562NN · Bombdr CL6002D15 · Vertical Stabilizer, Spar/RibSDR VNAA202401050022Fitting · damagedDAMAGED 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.Nov 11, 2023 · N562NN · Bombdr CL6002D15 · Fuselage Structure (General)SDR VNAA202401050019Aileron · corrodedCORROSION 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. -BNov 10, 2023 · N562NN · Bombdr CL6002D15 · AileronsSDR VNAA202310011111Sensor · unserviceableBRAKE 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 Sep 27, 2023 · N562NN · Cndair CL6002D24 · Landing Gear Brake SystemSDR VNAA202204101111Control Valve · unserviceableDURING 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 AUApr 7, 2022 · N562NN · Cndair CL6002D24 · Air Distribution SystemSDR VNAA202112151111Skin Panel · scratchedDURING 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 FRODec 15, 2021 · N562NN · Cndair CL6002D24 · Emergency ExitsSDR VNAA202112131111Pump · failedAIRCRAFT 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,Dec 11, 2021 · N562NN · Cndair CL6002D24 · Hydraulic Pump (Electric/Engine), MainSDR VNAA202108171111Sensor · malfunctionedRH 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 INDICATIOAug 13, 2021 · N562NN · Cndair CL6002D24 · Landing Gear Brake SystemSDR VNAA202107291112Thermocouple · false indicationOCCURRED 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. INFRAJul 26, 2021 · N562NN · Cndair CL6002D24 · Landing Gear Brake SystemSDR VNAA202106221111Proximity Sensor · out of adjustNOSE 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 FOJun 19, 2021 · N562NN · Cndair CL6002D24 · Landing Gear Position and WarningSDR VNAA2020102911101Bleed Valve · inoperativeLT 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.Oct 28, 2020 · N562NN · Cndair CL6002D24 · Pneumatic Distribution SystemSDR VNAA2020022499903Floor Support · corrodedLH 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-Feb 24, 2020 · N562NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2020022499003Angle · corrodedFWD 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.Feb 24, 2020 · N562NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2020022499902Intercostal · corrodedTWO 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.Feb 24, 2020 · N562NN · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2020022499901Drag Angle · crackedSUSPECTED 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 TFeb 24, 2020 · N562NN · Bombdr CL6002D15 · Vertical StabilizerSDR VNAA2019052111102Window · crackedCAPTAINS SIDE WINDOW CRACKED IN FLIGHT AT 8000 FEET. MAINTENANCE REMOVED AND REPLACED CAPTAINS SIDE WINDOW, OPS CHECK GOOD.May 21, 2019 · N562NN · Cndair CL6002D24 · Flight Compartment WindowsSDR VNAA2019042111103Detector · failedCREW 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 SKEApr 21, 2019 · N562NN · Cndair CL6002D24 · Trailing Flap Position Indicating SystemSDR VNAA2019100243101Light · inoperativeFWD 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 / "Apr 3, 2019 · N562NN · Cndair CL6002D24 · Emergency LightingSDR VNAA2018042711101Unknown · odorDURING 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 APApr 27, 2018 · N562NN · Cndair CL6002D24 · Air Distribution System
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