N582NN
Service difficulty reports · 54
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 = 'N582NN' 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.
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 = 'N582NN' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VNAA2026082523501Selector Valve · unserviceableGEAR DISAGREE MASTER WARNING / INTERROGATED MDC AND FOUND B1 CODE 005968. PERFORMED OPERATIONAL TEST OF THE LANDING GEAR EXTENSION/RETRACTION SYSTEM IAW AMM 32-30-00-710-801-A01. LANDING GEAR RETRACTION ON ALL GEARS FAILED ON MULTIPLE ATTEMPTS. TROUBLESHOT ALLSDR VNAA2026062620003Control Unit · unserviceableAFTER FLAPS 20 TAKEOFF, FLAPS FAIL CAUTION MSG AND FLAPS FAILED AT FLAPS 17 AND SLATS 20. REMOVE AND REPLACED THE SLATS/FLAPS ELECTRONIC CONTROL UNIT IAW AMM 27-51-05-000/400-801. TESTED THE (SFECU2) BY CLEARING OF INHIBIT IAW AMM 45-45-00-970-821. PERFORM THSDR VNAA2025032411102Windshield · fireFRONT RIGHT WINDSHIELD SEALANT CAUGHT FIRE AT THE GATE, WINDSHIELD SHATTERED AS A RESULT. [WINDSHIELD HEAT HAD BEEN LEFT IN LOW POSITION FOR THE REPO FROM HANGAR]. NO MEDICAL ATTENTION WAS REPORTED. / PERFORMED INSTALLATION OF THE R/H WINDSHIELD AS REQUIRED SDR VNAA2025011311101Sensor · abnormalWING OVHT WARNING MSG INTERMITTENT IN FLIGHT. / INSP RH INBD TEMP SENSOR AND FOUND 1 PIN NOT SECURE. INSTALLED PIN IAW AMM 30ˆ’12ˆ’06ˆ’400ˆ’801 OPS CHECK GOOD.SDR VNAA2024122311102Pressure System · unserviceableCABIN ALTITUDE WARNING MESSAGE AT 24000FT / REMOVED AND REPLACED BOTH CABIN PRESSURE CONTROLLERS IAW CRJ 900 AMM 21-31-04-000/400-801. REMOVED AND REPLACED CABIN PRESSURE CONTROL PANEL IAW CRJ 900 AMM 21-33-01-000/401-801. OPS TEST GOOD. PERFORMED OPS TEST OFSDR VNAA20240619002Fitting · corrodedMANUFACTURING PART. IN REFERENCE NRC 00169: FABRICATE PN: A661091-1 (FLOOR FITTING ) 1EA IN ACCORDANCE WITH EA NO: A1-690-25-00209. FITTING (1 EA) WAS MANUFATURED PN: A661091-1 PER EA Nº: A1-690-25-00209 REV. ORIGINALSDR VNAA20240618009Frame · corrodedCORROSION ON FRAME FS= 349 BETWEEN STRG 26LH TO 25RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS= 349 BETWEEN STRG 26LH TO 25RH AT MAIN AVIONICS COMPARTMENT.SDR VNAA20240619012Strap · corrodedCORROSION ON STRAP, INNER FS 349.00 AND STGR 17LH AT PASSENGER DOOR SURROUND STRUCTURE. FITTING WAS FOUND OUT OFF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01SDR VNAA20240619031Strap · corrodedCORROSION ON STRAP, INNER FS 319.70 AND STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE. STRAP, INNER FS 319.70 AND STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE WAS REPAIRED PER REO 690-53-21-1774 REV - -SDR VNAA20240619030Seat Track · corrodedCORROSION AT SIDE SEAT RAIL OF STRG 15LH/RH BETWEEN FS785.15 FS - 847+8.40. CORROSION AT SIDE SEAT RAIL OF STRG 15LH/RH BETWEEN FS785.15 FS - 847+8.40. WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49SDR VNAA20240619029Seat Track · corrodedCORROSION AT SIDE SEAT RAIL OF STRG 15LH/RH BETWEEN FS744.15 - FS 761.85. 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 VNAA20240619028Seat Track · corrodedCORROSION AT SIDE SEAT RAIL OF STRG 15LH BETWEEN FS699.40 - FS 720.85. SIDE SEAT RAIL OF STRG 15LH BETWEEN FS699.40 - FS 720.85 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 VNAA20240619027Seat Track · corrodedCORROSION ON SEAT RAILS (SEVERAL LOCATIONS) LBL 9 AND RBL 9 BTW FS 874.00 TO FS 977.00 AT PASSENGER CABIN. PER CRJ900 SRM 53-51-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNAA20240619026Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 477.40 TO FS 581 LBL 9.00 AT CABIN PAX. SEAT RAIL BTW FS 477.40 TO FS 581 LBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNAA20240619025Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 477.40 TO FS 669.00 RBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 669.00 RBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNAA20240619024Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 364 TO FS 477.40 LBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 364 TO FS 477.40 LBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNAA20240619023Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 349.00 TO FS 477.40 RBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 349.00 TO FS 477.40 RBL 9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNAA20240619022Plate · corrodedCORROSION ON JOINT PLATE FS 519.64 OF FWD BAGGAGE BAY DOOR SURROUND STRUCTURE AT FWD CARGO COMPARTMENT. JOINT PLATE FS 519.64 OF FWD BAGGAGE BAY WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-23-001-001-A02, AND WAS REPLACED PER CRJ900 SRM 51-42-22-001-001-SDR VNAA20240619021Strap · corrodedCORROSION ON STRAP OF FLOOR STRUCTURE FS 581.00 BTW STGR 24RH TO STGR 27 AT FWD CARGO COMPARTMENT. STRAP OF FLOOR STRUCTURE FS 581.00 BTW STGR 24RH TO STGR 27 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01, WAS FABRICATED PER DWG: SH670-33320SDR VNAA20240619020Access Panel · crackedCRACK IN ACCESS PANEL 171CL. ACCESS PANEL 171CL WAS REPAIRED PER REO 670-53-82-430. REV--SDR VNAA20240619017Skin · erodedEROSION ON LEADING EDGE AT SLAT 3 OF THE RH WING. LEADING EDGE AT SLAT 3 OF THE RH WING WAS REPAIRED PER REO 690-57-42-1066 REV. --SDR VNAA20240619013Intercostal · corrodedCORROSION ON INTERCOSTALS (2 EAS) BTW STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTALS (2 EAS) BTW STA. FS= 349 TO FS= 364 NEAR STGR 27 WERE EVALUATED OUT OF
LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND WERE REPLACED PER CRJSDR VNAA20240619011Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01SDR VNAA20240619010Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01SDR VNAA20240619009Web · crackedCRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB. UPPER WEB OF ADG COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01.SDR VNAA20240619005Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR BEAM RBL 12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPAIRED PER REO 690-53-11-1758 REV. --SDR VNAA20240619004Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPAIRED PER REO 690-53-11-1758 REV. --SDR VNAA20240619003Rib · crackedCRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. WING RIB AT FLS 168.07 AT WING TRAILING EDGE OF LH WING WAS REPAIRED PER REO 690-57-51-354 REV. --SDR VNAA20240618010Hinge Fitting · excess playFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #2103 REV. B.SDR VNAA20240618007Skin · corrodedCORROSION ON DOOR CUT-OUT INNER SKIN AT E/E MAIN COMPARTMENT. CORROSION ON DOOR CUT-OUT INNER SKIN AT E/E MAIN COMPARTMENT WAS REMOVED AND WAS EVALUATED WITHIN LIMITS PER REO 690-53-21-032 REV. --SDR VNAA20240618006Arm · gougedCTR BAGGAGE BAY DOOR FWD INNER ARM WITHIN 1384.3 FHS FROM IR (BEFORE 19,227.08 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. CTR BAGGAGE BAY DOOR FWD INNER ARM WAS REPAIRED PER REO 690-52-35-411 REV. - - IN REFRENCE TO ESDR VNAA20240619016Bracket · corrodedCORROSION ON BRACKETS, MACHINED (7EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. CORROSION ON BRACKETS, MACHINED (7EAS) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM
53-32-58-101-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-01; CRJ900 SRM 5SDR VNAA20240619015Plate · corrodedCORROSION ON PLATES (BL0) (2EAS) PLATE 1 BTW FS 517.00 STGR 27. PLATE 2 BTW FS565.00 STGR 27. AT FWD CARGO COMPARTMENT. STRINGER 27 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE FABRICATED PER (EO) SH670-3337, AND WERE REPLACED PESDR VNAA20240619014Mount · crackedAFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM) AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM) WAS REPAIRED PER REO 690-28SDR VNAA20240619008Skin · wornWEAR ON LOWER SKIN OF SETTLEMENT AREA OF ACCESS PANELS 583AB, 586AB, 592AB AND 597AB AT LH WING. LOWER SKIN OF SETTLEMENT AREA OF ACCESS PANELS 583AB, 586AB, 592AB AND 597AB AT LH WING WAS REPAIRED PER REO 690-57-21-471. REV. - -SDR VNAA20240619006Lug · corrodedSCRATCH ON HOUSING OF LUG 1, LUG 2 AND LUG 6 AT RH AILERON WAS FOUND. SCRATCH ON HOUSING OF LUG 1, LUG 2 AND LUG 6 AT RH AILERON WAS FOUND WERE REPAIRED PER REO 670-57-61-237 REV - - NOTES FSDR VNAA20240619007Lug · corrodedSCRATCH ON HOUSING OF LUG 2 AND LUG 5 AT LH AILERON WAS FOUND. SCRATCH ON HOUSING OF LUG 2 AND LUG 5 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV - - NOTES FSDR VNAA20240619001Hinge · corrodedCORROSION ON HOUSING OF HINGE FITTING 2 (OUTBD AND INBD) FITTING 3 (INBD) AT LH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 2 (OUTBD AND INBD) FITTING 3 (INBD) AT LH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-357 REV. - - AND ETI-900-24-004 REV. SDR VNAA20240618012Lug · scratchedHOUSING OF HINGE FITTING 1 (OUTBD), FITTING 3 (OUTBD AND INBD) & FITTING 4 (OUTBD AND INBD) AT RH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 1 (OUTBD), FITTING 3 (OUTBD AND INBD) & FITTING 4 (OUTBD AND INBD) AT RH WING REAR SPAR WERE REPAIRED PERSDR VNAA20240618011Lug · scratchedHOUSING OF HINGE FITTING 1 (OUTBD) FITTING 4 (OUTBD AND INBD) AT LH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 1 (OUTBD) FITTING 4 (OUTBD AND INBD) AT LH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-357 REV. - -SDR VNAA20240618005Arm · gougedCTR BAGGAGE BAY DOOR AFT INNER ARM WITHIN 1384.3 FHS FROM IR (BEFORE 19,227.08 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. CTR BAGGAGE BAY DOOR AFT INNER ARM WAS REPAIRED PER REO 690-52-35-412 REV. - - IN REFRENCE TOSDR VNAA20240618004Skin · damagedLIGHTNING STRIKES (14 EAS) ON FUSELAGE SKIN AT FS 295 TO FS 693 BTW STGR 23RH TO STGR 14RH. LIGHTNING STRIKES (14 EAS) ON FUSELAGE SKIN AT FS 295 TO FS 693 BTW STGR 23RH TO STGR 14RH WERE REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03 AND REO 690-53-21-1769SDR VNAA20240618003Hinge · corrodedCENTER FITTING BORE LUG R1, R2, R5 AND R6 AT RH AILERON. CENTER FITTING BORE LUG R1, R2, R5 AND R6 AT RH AILERON WERE REPAIRED PER REO 670-57-61-237 REV--SDR VNAA202406190007Hinge · corrodedCENTER FITTING BORE LUG L1, L2, L5 AND L6 AT LH AILERON. CENTER FITTING BORE LUG L1, L2, L5 AND L6 AT LH AILERON.SDR VNAA2024061908001Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (4EAS) LOCATED BTW FS=280 TO FS=295 AND RBL17'' AND RBL 38'', FS=295 AND LBL20'', FS=310 AND LBL37'' AT FUSELAGE FLOOR STRUCTURE. CORROSION ON FLOOR SUPPORTS (4EAS) AT FUSELAGE FLOOR STRUCTURE WERE EVALUATED OUT OF LIMITS PER CRJ-SDR VNAA202307181112Sensor · malfunctionedLHIB BRAKE OVHT WARNING MSG AFTER T/O., BTMS INDICATION WOULD RADOMLY DASHOUT START AFTER GEAR RETRACTION AND CONTINUED WITH GEAR EXTENDED. REMOVED AND REPLACED LHIB MLG BRAKE TEMP SENSOR IAW CRJ 900 AMM 32-46-01-000/400-801-A01-PSA. NO FURTHER DEFECTS NOTED ASDR VNAA202201091111Brake · overheatedDURING LANDING THE CREW GOT A BREAK TEMP OVER HEAT MESSAGE. A EMERGENCY WAS DECLARED BY THE CREW AND TRUCKS DID ROLL IN BUT NOT NEEDED. THE CREW DID NOT CALLED FOR A BRACE ON LANDING. THE AIRCRAFT WAS ABLE TO TAXI TO A GATE UNDER THEIR OWN POWER. NO FURTHER INSDR VNAA202110211113Idg · faultedCREW HAD AN IDG CAUTION MESSAGE INFLIGHT AND RAN THE QRH. CREW MADE THE DECISION TO DIVERT TO CAK AS IT WAS A MX BASE AND COULD LIKELY DEAL WITH THE ISSUE BETTER THAN AN OUTSTATION. IDG 2 CAUTION MESSAGE IN FLIGHT. QRH RUN IDG 2 DISCONNECT PUSHED. / DEF IDG 2 SDR VNAA2021102001111Idg · faultedCREW HAD AN IDG CAUTION MESSAGE INFLIGHT AND RAN THE QRH. CREW MADE THE DECISION TO DIVERT TO CAK AS IT WAS A MX BASE AND COULD LIKELY DEAL WITH THE ISSUE BETTER THAN AN OUTSTATION. IDG 2 CAUTION MESSAGE IN FLIGHT. QRH RUN IDG 2 DISCONNECT PUSHED. / DEF IDG 2 SDR VNAA202009149991Angle · corrodedFS 280.00 FORWARD "J" ANGLE IS CORRODED. INSTALLED NEW SERVICEABLE FS 280 J ANGLE, IAW CRJ 200 900 SRM 51-42-06-001-001-A01 AND 42-21-001-010-A01.
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