N556NN

Service difficulty reports · 79

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 = 'N556NN' 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 VNAA202311280007Skin · nickedSEVERAL NICKS BTW FS1000.00 TO FS1047.00 BTW STGR#27 TO STGR#25 RH SIDE EXTERNAL FUSELAGE. NICKS ON FUSELAGE SKIN BTW FS1000 TO FS1047, BTW STGR 26RH TO STGR 25RH AND BTW FS1000 TO FS1031, BTW STGR 27 TO STGR 26RH WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-Oct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202311280006Skin · damagedLIGHTING STRIKE BTW FS517.00 TO FS533.00 AND BTW STGR#25 TO STGR#26 RH SIDE (1EA) LIGHTING STRIKE BTW FS549.00 TO FS565.00 AND BTW STGR#25 TO STGR#26 RH SIDE(1EA) , LIGHTING STRIKE BTW FS629.00 TO FS613.00 AND BTW STGR#25 TO STGR#24 RH SIDE (1EA). LIGHTING STOct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202311280004Skin · nickedSEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 WERE REMOVED PER CRJ900 SRM 51-12-00-001-001-A01; WERE EVALUATED WITHIN LIMITS BTW FLS 45 TO FLS 65.5 AND WEROct 6, 2023 · N556NN · Cndair CL6002D24 · Trailing Edge FlapsSDR VNAA202311280003Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE LH , BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) CRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE LH , BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (Oct 6, 2023 · N556NN · Cndair CL6002D24 · Vertical StabilizerSDR VNAA202311280002Door Sill · corrodedCORROSION ON LOWER SILL OF AFT BAGGAGE-BAY DOOR CUT OUT. (C2). CORROSION ON LOWER SILL OF AFT BAGGAGE-BAY WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-23-201-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01, CRJ900 SRM 51-42-06-001-001-A01 ANOct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202311280001Seat Track · corrodedCORROSION ON SIDE TRACKS AT FWD CARGO COMPARTMENT. CORROSION REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED, (2EAS) WITHIN LIMITS AND (2EAS) OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01, AND WERE VERIFIED PER CRJ900 AIPC 25-51-02-01 ITEMOct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202307121111Pcu · unserviceableINTERMITTENT ABNORMAL VIBRATION AT HIGHER AIRSPEED AND POWER, UN-COMMANDED SLIGHT RUDDER MOVEMENT, VIBRATION NOT HARMONIC WITH ENGINES, SLIGHT RIGHT PULL AT AUTO PILOT DISCONNECT. REMOVED AND REPLACED SPHERICAL BALL, BOLT AND BUSHING ON RUDDER PCU SYSTEM 3 IAWJul 9, 2023 · N556NN · Cndair CL6002D24 · Rudder Control SystemSDR VNAA202305291111Unknown · unknownGEAR DISAGREE UPON RETRACTION. RED X ON NOSE GEAR INDICATION / ADJUSTED PROX SENSOR P22 IAW CRJ 900 FIM 32-61-05-810-853 (B1 007437) & PERFORMED OPS CHECK OF THE LANDING GEAR EXT/ RET SYSTEM IAW CRJ 900 AMM 32ˆ’30ˆ’00ˆ’710ˆ’801. OPS CHECK GOOD, FAULT DID NMay 26, 2023 · N556NN · Cndair CL6002D24 · Landing Gear SystemSDR VNAA202305161111Windshield · crackedL WINDSHIELD STARTED ARCING IN FLIGHT, CRACKED \ REMOVED AND REPLACED WINDSHIELD IAW CRJ900 AMM 56-11-01-400-A01-PSA. OPS CHECK AND LEAK CHECK GOOD.May 14, 2023 · N556NN · Cndair CL6002D24 · Flight Compartment WindowsSDR VNAA2022112711110Skin · handler errorLAV CART HIT RIGHT AFT SECTION OF AIRCRAFT BY LAV SERVICE DOOR / REPAIR OF R/H AFT FUSELAGE WAS PERFORMED BY MHIRJ TECHNICIANS IAW MHIRJ WORK ORDER #MIS-5501 AND REO 690-53-51-356 INSTRUCTIONS. REPAIR IS FOUND TO BE ACCEPTABLE AND AIRCRAFT IS APPROVED FOR RETUNov 24, 2022 · N556NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202210221116Transducer · malfunctionedON APPROACH INTO SBN, RECEIVED ANTI-SKID CAUTION AT 1500' CREW DECLARED AN EMERGENCY. TRUCKS ROLLED. NO BRACE. FLIGHT LANDED WITHOUT ANY ISSUES AND WAS ABLE TO TAXI TO THE GATE. CREW CONTACTING MX AT THIS TIME. FOUND BROKEN WIRE ON LH INBD WHEELS TRANSDUCER. ROct 21, 2021 · N556NN · Cndair CL6002D24 · Brake Anti-Skid SectionSDR VNAA202110011111Controller · faultedDURING CLIMB OUT OF PNS, AT FL040, THERE WAS A FLASH ON THE FO SIDE WINDSHIELD. CREW AT FIRST BELIEVED THEY WERE BEING LASERED, AND CONTINUED CLIMB. AT FL140, FO WINDSHIELD BEGAN SPARKING. TURNED OFF FO WINDSHIELD HEAT AND PROBLEM STOPPED. FLIGHT DIVERETED TO Sep 29, 2021 · N556NN · Cndair CL6002D24 · Windshield/Door Rain/Ice RemovalSDR VNAA202102031112Stringer · damagedDURING UNSCHEDULED MAINTENANCE AT CINCINNATI, OH (CVG), BLENDING WAS DISCOVERED ON STRINGER 16R BETWEEN APPROXIMATELY FS 435 AND FS 448 DURING REPAIR OF THE FUSELAGE SKIN PER EA 21-C9-53-064-A. UPON INVESTIGATION, THE STRINGER IS IN A NO DAMAGE ALLOWED AREA AJan 30, 2021 · N556NN · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA2021020311011Skin · damagedDURING ROUTINE MAINTENANCE AT THE DAYTON, OH FACILITIES OF THE DAYTON INTERNATIONAL AIRPORT (DAY), THE MAINTENANCE TEAM IDENTIFIED FOUR CREASES AND /DENTS ON THE RT SIDE OF THE FUSELAGE, FS 437.00 BETWEEN STRINGERS 16R & 17R. THE DAMAGE IS 6.25 L X 3.75 W X .Jan 30, 2021 · N556NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA2020071011101Warning System · false activationAIR RETURN DUE TO MAINTENANCE ENROUTE FOR PRESSURIZATION ISSUE FORWARD SERVICE DOOR CAUTION MESSAGE ILLUMINATED. CREW WAS ABLE TO LAND AND TAXI TO GATE UNDER OWN POWER WITHOUT ANY ISSUES. FURTHERMORE, AN EMERGENCY WAS NOT DECLARED IN CLT. FWD SVC DR CAUTIONJul 9, 2020 · N556NN · Cndair CL6002D24 · Door Warning SystemSDR VNAA2020012299907Angle · corrodedFS 280 J ANGLE CORRODED BETWEEN LBL9 AND RBL9. ON FURTHER INVESTIGATION, FOUND THE J ANGLE TO BE CORRODED BEYOND LIMITS. MAX BLEND LIMIT IS .006. CORROSION DEPTH WAS .011. REF 53-00-00-101-001-A01. REMOVED CORRODED J ANGLE IAW SRM 51-42-06-001-001-A01, 51-42Jan 22, 2020 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA2020012299906Frame · corrodedFS 349 FRAME CORRODED AT STR 27 AFT SIDE. REMOVED CORRODED FRAME SEGMENT AT FS 349.00 FROM STRINGER L23 TO R24 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE FRAME SEGMENT IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-AJan 22, 2020 · N556NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA2020012299905Intercostal · corrodedFS 349 - 364 LT STR 27 INTERCOSTAL CORRODED. INTERCOSTAL OUT OF LIMITS DUE TO NO DAMAGE ALLOWED IN AREA. REMOVED INTERCOSTAL IAW SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01. LOCATED AND DRILLED INTERCOSTAL IAW SRM 51-40-11-001-A01. INSTALLED A NEJan 22, 2020 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA2020012299904Intercostal · corrodedFS 349 - 364 RH SIDE OF STR 27 INTERCOSTAL CORRODED. INTERCOSTAL OUT OF LIMITS DUE TO NO DAMAGE ALLOWED IN AREA. REMOVED INTERCOSTAL IAW SRM 51-42-21-001-000-A01 AND SRM 51-42-06-001-001-A01. LOCATED AND DRILLED INTERCOSTAL IAW SRM 51-40-11-001-001-A01. Jan 22, 2020 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA2020012299903Frame · corrodedFS 310 STR 26L - 26R CORRODED ON FWD AND AFT SIDES OF FRAME. RMEOVED DAMAGED SECTION OF FS 310 IAW SRM 53-00-06-201-006-A01. INSTALLED NEW SERVICEABLE FRAME SECTION IAW SRM 53-00-06-201-006-A01. PERFORMED EDDY CURRENT OF FS 310 FRAME CUTLINE EDGES IAW Jan 22, 2020 · N556NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA2020012299902Drag Angle · crackedRH AFT FUSELAGE TO VERTICAL STAB DRAG ANGLE CRACKED. REMOVED RT AFT FUSELAGE TO VERTICAL STAB CRACKED DRAG ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01. LOCATED AND DRILLED NEW SERVICABLE RT AFT FUSELAGE TO VERTICAL STAB Jan 22, 2020 · N556NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR VNAA2020012299901Drag Angle · crackedLEFT AF FUSELAGE VERTICAL DRAG ANGLE CRACKED. REMOVED LEFT AFT FUSELAGE TO VERTICAL CRACKED DRAG ANGLE IAW SRM 51-12-13, 51-42-21 AND 51-42-22. LOCATED AND DRILLED NEW LEFT AFT FUSELAGE TO VERTICAL DRAG ANGLE IAW SRM 51-40-11, 51-42-13, 51-42-21 AND 51-42-2Jan 22, 2020 · N556NN · Cndair CL6002D24 · Horizontal Stabilizer StructureSDR VNAA2019100231101Light · inoperativeLH AFT EXTERIOR EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED LH AFT EXTERIOR EMERGENCY LIGHT IAW CRJ 900 AMM 33-51-15-000/400-801-A05 OPS CHECK GOODAug 31, 2019 · N556NN · Cndair CL6002D24 · Emergency LightingSDR VNAA2018080431101Relay · failedTHE CREW REPORTED A LOSS OF AC ESS BUSS DURING APPROACH. AN EMERGENCY WAS DECLARED.MX REPLACED THE RELAY K124.Aug 3, 2018 · N556NN · Cndair CL6002D24 · Electrical Power SystemSDR VNAA2017092111101Pcu · faultyOB SPOILERON/OB FLIGHT SPOILER CAUTION MSG, CREW DECLARED EMERGENCY. MX R&R RH OB MULTI-FUNCTION SPOILER PCU OPS AND LEAK CHECK GOOD.Sep 21, 2017 · N556NN · Cndair CL6002D24 · Drag Control SystemSDR VNAA2017020600010Warning Message · false activationOUTBOARD SPOILERONS & OUTBOARD FLIGHT SPOILERS CAUTION MESSAGE DURING DECENT. COMPLIED WITH SYSTEM RESET. MESSAGE CLEARED AND DID NOT REAPPEAR.Feb 6, 2017 · N556NN · Cndair CL6002D24 · Drag Control SystemSDR VNAA2016031800025Light · shortedCREW REPORTED F/O'S MAPLIGHT CIRCUIT BREAKER CBP2-G7 POPPED ON APPROACH. MAINTENANCE TROUBLESHOT AND DEFERRED F/O'S SIDE POST MAPLIGHT. THE ACFT WAS RELEASED FOR SERVICE.Mar 18, 2016 · N556NN · Cndair CL6002D24 · Flight Compartment LightingSDR VNAA2016020500010Sign · detachedCREW REPORTED EMERGENCY EXIT SIGN BY GALLEY SERVICE DOOR MISSING. MAINTENANCE INSPECTED, TEMPORARILY SECURED EMERGENCY EXIT SIGN AND PLACED ON DEFERRED APPEARANCE ITEM LIST. ACFT RELEASED FOR SERVICE.Feb 5, 2016 · N556NN · Cndair CL6002D24 · Emergency LightingSDR VNAA2015081200023Acm · seizedCREW REPORTED SMOKE IN CABIN ON FINAL APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R RT AIR CYCLE MACHINE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Aug 12, 2015 · N556NN · Cndair CL6002D24 · Cabin Cooling System
Back to N556NN