N577NN
Service difficulty reports · 60
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 = 'N577NN' 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 = 'N577NN' 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 VNAA2026062519704Frame · corrodedCORROSION FOUND ON THE FORWARD SIDE OF FRAME SECTION 310 BETWEEN THE BOTTOM CENTER STRINGER 27 AND LEFT HAND 26 / BLENDED DAMAGE AREAS. PERFORMED NDT (LPI & EDDY CURRENT) WITH NO DEFECTS AND RESTORED FINISH IAW REO 690-53-21-2151.SDR VNAA2026062519603Frame · corrodedCORROSION FOUND ON THE FORWARD BOTTOM SIDE OF FRAME SECTION 310 BETWEEN THE BOTTOM CENTER STRINGER 27 AND RIGHT HAND 26. BLENDED DAMAGE AREAS. PERFORMED NDT (LPI & EDDY CURRENT) WITH NO DEFECTS AND RESTORED FINISH IAW REO 690-53-21-2151.SDR VNAA2026062519502Frame · corrodedCORROSION FOUND ON THE AFT BOTTOM SIDE OF FRAME SECTION 295 BETWEEN THE BOTTOM CENTER STRINGER 27 AND RIGHT HAND 26 / BLENDED DAMAGE AREAS. PERFORMED NDT (LPI & EDDY CURRENT) WITH NO DEFECTS AND RESTORED FINISH IAW REO 690-53-21-2151.SDR VNAA2025120311102Tire · blownRH MLG TIRES BLOWN ON TAXI. / RH IB TIRE + WHEEL ASSY REMOVED AND REPLACED IAW CRJ 900 AMM 32-41-01-000/400-801-A01-PSASDR VNAA2025101011101Windshield · arcedFOS WINDSHIELD ARCING IN FLIGHT QRH COMPLETED. REMOVED AND REPLACED FO SIDE WINDSHIELD IAW AMM 56-11-01-000/400-801-A01-PSA. OPS TEST OF FO SIDE WINDSHIELD TEMPERATURE CONTROL PASSED IAW AMM 30-41-06-710-801-A01. PRESSURIZED THE AIRCRAFT FOR LEAK TEST OF THESDR VNAA2024061811101Acm · unserviceableR PACK AUTO FAIL CAUTION MSG. FA'S REPORTED SMOKE IN CABIN. PACK TEMP HIT 99C / TROUBLESHOT AND FOUND RH ACM TO BE SEIZED UP. REMOVED AND REPLACED RH ACM IAW CRJ 900 AMM 21-51-08-000/400-801-A01. RH PACKS SYSTEM OPS AND LEAKS CHECKS GOOD IAW CRJ 900 AMM 21-51-SDR VNAA202404090014Striker · corrodedCORROSION ON SILL STRIKER AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW STA FS 319.70 TO FS 349.00 WAS FOUND. SILL STRIKER AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW STA FS 319.70 TO FS 349.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-2SDR VNAA202404080008Plate · corrodedCORROSION ON KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. KICKPLATE AND MID CAP BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-001-A02 AND WERESDR VNAA202404090011Rib · corrodedCORROSION ON WINGLET LOWER CLOSING RIB AT RH WINGLET CORROSION ON WINGLET LOWER CLOSING RIB AT RH WINGLET WAS REPAIRED PER REO 690-57-31-229 REV. --SDR VNAA202404090004Seat Track · corrodedCORROSION ON SEAT RAIL (SEVERAL LOCATIONS) BTW FS477.40 TO FS693.00 LBL/RBL 9.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL (SEVERAL LOCATIONS) BTW FS477.40 TO FS693.00 LBL/RBL 9.00 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-0SDR VNAA202404080015Door Sill · corrodedCORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00. AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-23-201-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ9SDR VNAA202404080010Plate · corrodedCORROSION ON LOWER FACE OF PLATES LBL 3.4 (PLATE 1) BTW FS533.00 AND FS 549.00 (PLATE 2) BTW FS 645.00 AND FS 661.00 AT FWD CARGO COMPARTMENT. DUE TO NO DAMAGE IS ALLOWED ON THE FORWARD BAGGAGE BAY STRUCTURE, PLATES LBL 3.4 (PLATE 1) BTW FS533.00 AND FS 549.00SDR VNAA202404090016Door Sill · corrodedAFT DOOR SILL REMOVAL IN REFERENCE TO NRC 0095, CORROSION ON FWD CHORD AT C2 BTW STA FS 1000.00TO FS 1015.00 WAS FOUND. FWD CHORD AT C2 BTW STA FS 1000.00TO FS 1015.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-23-101-001-A01 AND WAS VERIFIED PER CRJ900SDR VNAA202404090015Angle · corrodedAFT SILL REMOVAL IN REFERENCE TO NRC 0109, CORROSION ON MOUNTING ANGLE AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW STA FS 319.70 TO FS 349.00 WAS FOUND MOUNTING ANGLE AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW STA FS 319.70 TO FS 349.00 WAS SDR VNAA202404090013Fitting · corrodedCORROSION ON FITTING (4E/A) OF ATTACHMENT POINT AT GALLEY 1 AND CORROSION ON FITTING (2EA) OF ATTACHMENT POINT AT ENTRANCE COMPARTMENT. (FLOOR STRUCTURE AREA). FITTING (4E/A) OF ATTACHMENT POINT AT GALLEY 1 AND CORROSION ON FITTING (2EA) OF ATTACHMENT POINT ASDR VNAA202404090012Seat Track · corrodedCORROSION ON SEAT RAIL (SEVERAL LOCATIONS) BTW FS693.00 TO FS847+16.00 RBL 9.00 AND CORROSION ON SEAT RAIL BTW FS693.00 TO FS720.85 LBL 9.00 AT PASSENGER CABIN CORROSION ON SEAT RAIL (SEVERAL LOCATIONS) BTW FS693.00 TO FS847+16.00 RBL 9.00 AND CORROSION ON SEASDR VNAA202404090010Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 RH/LH (SEVERAL LOCATIONS) BTW FS379.00 TO FS669.40 AT PASSENGER CABIN. SIDE SEAT RAIL STGR 15 RH/LH BTW FS379.00 TO FS669.40 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02; CRJ900 SRM 53SDR VNAA202404090009Hinge Fitting · wornFREE 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 VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103 REV. BSDR VNAA202404090008Canister · crackedDURING INSPECTION OF THE TASK CARD 600-08E2-JIC IT WAS DETECTED CRACK IN CANISTER WELDED NO.3 INTO, STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3 INTO, STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.--SDR VNAA202404090007Canister · crackedDURING INSPECTION OF THE TASK CARD 500-08E2-JIC IT WAS DETECTED 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 VNAA202404090006Rib · crackedAFTER ACCESS PANEL 521BL REMOVAL , CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. LH INBOARD FIXED L/E RIB AT STA 57.16 WAS REPAIRED PER REO 690-57-41-420 REV. --SDR VNAA202404090005Seat Track · corrodedCORROSION ON SEAT RAIL (SEVERAL LOCATIONS) BTW FS847.00+16.00 TO FS977.00 LBL/RBL 9.00 AT PASSENGER CABIN. SEAT RAIL BTW FS847.00+16.00 TO FS977.00 LBL/RBL 9.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WERE REPLSDR VNAA202404090003Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 RH/LH (SEVERAL LOCATIONS) BTW FS669.40 TO FS977.00 AT PASSENGER CABIN. SIDE SEAT RAILS STGR 15 RH/LH BTW FS669.40 TO FS977.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRSDR VNAA202404090002Strap · corrodedCORROSION ON STRAP INNER AT FS349.00 / STGR#17RH ON SURROUND STRUCTURE OF THE GALLEY SERVICE DOOR. STRAP INNER AT FS349.00 / STGR#17RH ON SURROUND STRUCTURE OF THE GALLEY SERVICE DOOR WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS RESDR VNAA202404090001Door Sill · corrodedCORROSION ON SILL AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW FS319.70 / FS349.00. SILL AT FWD SURROUND STRUCTURE OF GALLEY SERVICE DOOR BTW FS319.70 / FS349.00 WAS EVALUATED OUT OF LIMITS AND WAS REPLACED PER CRJ-900 SRM 53-21-23-101-002-A02 AND CRSDR VNAA202404080018Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1702 REV. - -SDR VNAA202404080017Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1701 REV. - -SDR VNAA202404080016Rib · elongatedELONGATED HOLES ON LH INBOARD FIXED L/E MACHINED RIB AT SLAT STA. 57.16, PERFORM PERM REPAIR IAW ENGINEERING DISPOSITION.L LH INBOARD FIXED L/E RIB AT STA 57.16 WAS REPAIRED PER REO 690-57-41-420 REV. --SDR VNAA202404080014Skin · damagedSPEED TAPE APPLIED - LH #2 SLAT AFT SKIN AT SS329.00 THE SUBJECT REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE FOR 650 FH FROM THE EXPIRY OF THE E.A. 23-C9-57-1049 REVISION IR TIME VALIDITY (800 FH, REF) LH #2 SLAT AFT SKIN AT SS329.00 WAS REPAIRED PER REO 69SDR VNAA202404080013Intercostal · corrodedCORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH BTW STA. FS=310 TO FS=349 AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH BTW STA. FS=310 TO FS=349 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A0SDR VNAA202404080012Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01SDR VNAA202404080011Bracket · corrodedCORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER CRJ-900 SRM SDR VNAA202404080009Strap · crackedCRACK ON STRAP AT FAIRING PANEL 196DR. STRAP AT FAIRING PANEL 196DR WAS REPAIRED PER REO 690-53-82-052 REV. --SDR VNAA202404080004Skin · nickedSEVERAL NICKS ON FUSELAGE SKIN, ON STA 1000.00 TO STA 1047 BTW STGR 22RH TO STGR 27. NICKS ON FUSELAGE SKIN, ON STA 1000.00 TO STA 1047 BTW STGR 22RH TO STGR 27 WERE REPAIRED PER REO 690-53-61-1357 REV. - -SDR VNAA202404080003Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN. SETTLEMENT AREA OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-452 REV - -.SDR VNAA202404080002Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN. SETTLEMENT AREA OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-453 REV - -.SDR VNAA202404080001Skin · corrodedCORROSION AT RH WINGLET LOWER AREA BTW WGLTS0.00./WS398.93 AND FS695.00 /FS794.50. RH WINGLET LOWER AREA BTW WGLTS0.00./WS398.93 AND FS695.00 /FS794.50 WAS REPAIRED PER REO 690-57-31-228 REV. --SDR VNAA202404080007Access Panel · damagedPERM REPAIR - LH PYLON ACCESS PANELS 412EB AND 412GB REF REO 690-54-51-050 WHITHIN 800 FH, REPAIR THE AFFECTED PARTS ACCORDING TO APPROVED PROCEDURES. LH PYLON ACCESS PANELS 412EB AND 412GB WERE REPAIRED PER REO 690-54-51-052 REV. - -SDR VNAA202404080006Counterbalance · wornWEAR AND NICKS ON FWD COUNTERBALANCE ARM OF FWD DOOR AT FWD CARGO COMPARTMENT. WEAR AND NICKS ON FWD COUNTERBALANCE ARM OF FWD DOOR AT FWD CARGO COMPARTMENT. WAS REPAIRED PER REO 690-52-35-389 REV. --SDR VNAA202404080005Counterbalance · wornWEAR AND NICKS ON FWD/AFT COUNTERBALANCE ARM OF CENTER DOOR AT FWD CARGO COMPARTMENT. FWD/AFT COUNTERBALANCE ARM OF CENTER DOOR AT FWD CARGO COMPARTMENT WERE REPAIRED PER REO 690-52-35-388 REV. - - AND PER REO 690-52-35-390 REV. - -SDR VNAA20231126011Canister · crackedCRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.--SDR VNAA202304191111Acm · unknownCABIN SMOKE ON TAKEOFF. RIGHT PACK AUTOFAIL ON LANDING / C/W OPS CHECK OF AIR-CONDITIONING SYSTEM IAW CRJ900 AMM 21-51-00-710-801 R/H PACK R/H PACK OVER TEMPED B-1 211943 C/W L/H AND R/H ENGINE START AND RUN AT IDLE IAW CRJ 900 AMM 71-00-00-866-806 NO INDICATISDR VNAA202303311111Unknown · unknownRUD LIMITER FAULT CAUTION MSG IN FLIGHT. / REMOVED AND REPLACED L/H FADEC IAW CRJ 900 AMM 73-21-01-000/400-801-A01. OPS CHECKS GOOD. PERFORMED RUDDER TRAVEL LIMITER OPS CHECK IAW CRJ 900 AMM 27-25-00-710-801-A01. OPS CHECK GOOD AT THIS TIMESDR VNAA202303291111Bleed Valve · unserviceableL ENG SURGE CLOSED CAUTION MSG & L FADEC FAULT STATUS MSG IN FLIGHT / INSTALLED NEW LH ENG OBV IAW CRJ900 AMM 75-31-01-400-801. OPS CHECK/LEAK CHECK GOOD. IDLE SPEED CHECK GOOD IAW CRJ900 AMM 71-00-00-720-801. NO SURGING.SDR VNAA202202141111Sensor · overheatedAFTER TAKE OFF THE CREW GOT BRAKE TEMP OVER HEAT INDICATOR MESSAGE. THEY RAN THE QRH AND MADE THE DECISION TO RETURN TO BGR. THEY WERE NOT OVERWEIGHT AND NO BRACE WAS CALLED. THE CREW DID DECLARED A EMERGENCY AND TRUCKS DID ROLL BUT THEY WERE NOT NEEDED. NO FUSDR VNAA202110221115Control Unit · faultedFLAPS FAILED ON APPROACH INTO VPS. THEY LANDED WITHOUT INCIDENT AND THE FIRE TRUCKS MET THE AIRCRAFT AND EXAMINED THE BRAKES FOR DAMAGE. INTERROGATED MDC TO FIND B1 CODES 007795/007794/006796/007812. T/S FAULTS IAW CRJ 900 FIM 27-51-01-810-803/802-A01, 27-52-SDR VNAA202110221112Control Unit · faultedAFTER BLOCKING OUT IN HSV, FLIGHT GOT FLAPS FAIL CAUTION. FLIGHT RTG AND MX WAS ABLE TO GET MESSAGE TO CLEAR. ONCE IN FLIGHT, FLAPS FAIL MESSAGE APPEARED AGAIN. FLIGHT CONTINUED TO CLT. ONCE ON APPROACH, AN EMERGENCY WAS DECLARED DUE TO FLAPS FAIL MESSAGE. FLISDR VNAA2020100811101Manifold · failedSTEERING INOPERABLE CAUTION MESSAGE IN FLIGHT. REMOVED AND REPLACED NWS WIRE HARNESS. REMOVED AND REPLACED NWS MANIFOLD. OPERATIONS AND LEAK CHECK GOOD.SDR VNAA2020100211103Lamp · inoperativeRT AFT EMERGENCY AND FWD PASSENGER DOOR EXIT SIGNS WILL NOT ILLUMINATE. RELAMPED RT AFT EMERGENCY LIGHT. OPERATIONS CHECK GOOD. PERFORMED OPERATIONS CHECK OF FWD EXIT SIGN. OPERATIONS CHECK GOOD.SDR VNAA2020093011101Steering Unit · malfunctionedCREW CALLED IN TO REPORT INCIDENT AT 1946L AFTER COMPLETING RDU-CLT CONTINUATION TO GIVE DISPATCH COORDINATOR NECESSARY INFORMATION TO COMPLETE THIS REPORT. WHILE ENROUTE FROM IAD-CLT CREW DECLARED EMERGENCY FOR NOSE WHEEL STEERING INOPERABLE. UPON GETTING C
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