N561NN
Service difficulty reports · 66
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 = 'N561NN' 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 = 'N561NN' 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 VNAA2026032514901Window · burnedFO SIDE WINDOW HEATING ELEMENT INTERMITTENT GLOWING/ARCHING AT BASE / REMOVED AND REPLACED THE RH COCKPIT WINDOW IAW CRJ 900 AMM 56-12-01-000/400-801-A01-PSA. OPS AND LEAK CHECK PASSED.SDR VNAA2024060411101Acm · failedUPON DEPARTURE FROM CAK PASSING THROUGH 4,000' WE GOT AN ODOR OF AN ELECTRICAL BURNING SMELL IN THE COCKPIT. UPON CLIMBING THROUGH 10,000' OUTSIDE OF STERILE / REMOVED AND REPLACED THE L/H AND R/H AIR CYCLE MACHINE (ACM) AS REQUIRED IN ACCORDANCE WITH 900 CRJ SDR VNAA202401040031Bracket · corrodedCORROSION ON BRACKETS, MACHINED (5EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. CORROSION ON BRACKETS, MACHINED (5EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER SDR VNAA202401040030Intercostal · corrodedCORROSION ON INTERCOSTAL BTW STGR 27 /STGR 26LH AND FS 661.00+8.40 / FS661.00 +16.00 AT FWD CARGO COMPARTMENT. CORROSION ON INTERCOSTAL BTW STGR 27 /STGR 26LH AND FS 661.00+8.40 / FS661.00 +16.00 AT FWD CARGO COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-00SDR VNAA202401040028Rib · crackedCRACK WAS FOUND ON RIB LEADING EDGE SS57.16 AT RH WING. STEP 1 TO STEP 4 WAS PERFORMED PER REO 690-57-41-240 REV. -- AND DUE ADYACENT CRACK WAS FOUND RIB LEADING EDGE SS57.16 AT RH WING WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 , CRJ900 SRM 51-42-21-00SDR VNAA202401040027Rib · crackedCRACK WAS FOUND ON RIB LEADING EDGE SS57.16 AT LH WING. STEP 1 TO STEP 4 WAS PERFORMED PER REO 690-57-41-240 REV. -- AND DUE ADYACENT CRACK WAS FOUND RIB LEADING EDGE SS57.16 AT LH WING WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 , CRJ900 SRM 51-42-21-00SDR VNAA202401040025Floor Support · corrodedCORROSION AT LBL27 FLOOR BEAM BETWEEN FS=985.00 TO FS=1069.75. CORROSION ON FLOOR BEAM LBL27 BETWEEN FS=985.00 TO FS=1069.75 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-43-101-001-A02 AND WAS REPAIRED PER REO 690-53-61-1308 REV-- AND CRJ900 SRM 53-00-41-SDR VNAA202401040024Floor Support · corrodedCORROSION AT LBL9 FLOOR BEAM BETWEEN FS=1000.00 TO FS=1069.75. LBL9 FLOOR BEAM BETWEEN FS=1000.00 TO FS=1069.75 WAS REPAIRED PER REO 690-53-61-1305 REV. --SDR VNAA202401040023Floor Support · corrodedCORROSION AT RBL9 FLOOR BEAM BETWEEN FS= 1000.00 TO FS=1069.75. (SM). CORROSION AT RBL9 FLOOR BEAM BETWEEN FS= 1000.00 TO FS=1069.75 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS REPAIRED PER REO REO 690-53-61-1307 REV. --SDR VNAA202401040021Floor Support · corrodedCORROSION AT RBL27 FLOOR BEAM BETWEEN FS=1015.00 TO FS=1031.00. RBL27 FLOOR BEAM BETWEEN FS=1015.00 TO FS=1031.00 WAS REPAIRED PER REO 690-53-61-1306 REV. --SDR VNAA202401040019Support · corrodedCORROSION ON GALLEY SUPPORT BTW FS=310.00 LBL=20”, FWD FUSELAGE FLOOR STRUCTURE. CORROSION ON GALLEY SUPPORT BTW FS=310.00 LBL=20”, FWD FUSELAGE FLOOR STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WAS REPLACED PER CRJ900 SRM 51SDR VNAA202401040017Canister · 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. --SDR VNAA202401040016Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15RH AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15RH AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRM 53-51-49-101-001-A02 AND SDR VNAA202401040014Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15LH AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15LH AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02, CRJ900 SRM 53-51-49-101-001-A02 AND WASSDR VNAA202401040013Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 379.00 TO FS 669.40 AND STGR 15LH AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 379.00 TO FS 669.40 AND STGR 15LH AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02 AND WASSDR VNAA202401040012Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 379.00 TO FS 669.40 AND STGR 15RH AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 379.00 TO FS 669.40 AND STGR 15RH AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER AMM 53-00-49 (CONFISDR VNAA202401040007Door Sill · corrodedCORROSION ON LOWER SIL BTW FS=1000.00 TO FS=1047.00 AT AFT BAGGAGE BAY DOOR SURROUND STRUCTURE. CORROSION ON LOWER SIL BTW FS=1000.00 TO FS=1047.00 AT AFT BAGGAGE BAY DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-23-101-001-A01 AND SDR VNAA202401040006Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 477.40 TO FS 693.00 LBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 693.00 LBL 9.00 AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER AMM 53-00-49 (CONFIG A12)SDR VNAA202401040005Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 477.40 TO FS 693.00 RBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 477.40 TO FS 693.00 RBL 9.00 AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER AMM 53-00-49 (CONFIG A12).SDR VNAA202401040004Angle · corrodedCORROSION ON ANGLE KICKPLATE (STGR 17L) AT PASSENGER DOOR SURROUND STRUCTURE FS 310.00- 333.00. CORROSION ON ANGLE KICKPLATE (STGR 17L) AT PASSENGER DOOR SURROUND STRUCTURE FS
310.00- 333.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-001-A02 ANSDR VNAA202401040002Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 374.00 TO FS 477.40 LBL 9.00 AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 374.00 TO FS 477.40 LBL 9.00 AT CABIN PAX WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER AMM 53-00-49 (CONFIG A12)SDR VNAA202401040001Seat Track · corrodedCORROSION ON SEAT RAIL BTW FS 349.00 TO FS 477.40 RBL 9.00 AT CABIN PAX. SEAT RAIL (2 EAS) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ900 AMM 53-00-49SDR VNAA202401040015Intercostal · corrodedCORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 NEAR TO STGR 27 AT MAIN AVIONICS COMPARTMENT. (E/E). INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 NEAR TO STGR 27 AT MAIN AVIONICS COMPARTMENT. (E/E) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM SDR VNAA202401040034Canister · 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. --SDR VNAA202401040033Floor Support · nickedNICKS ON LONGITUDINAL BEAM LBL 27 BTW FS= 409.00 AND FS=421.00, FUSELAGE FLOOR STRUCTURE. LONGITUDINAL BEAM LBL 27 BTW FS= 409.00 AND FS=421.00, FUSELAGE FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-21-1684 REV --SDR VNAA202401040032Frame · corrodedCORROSION ON FR 847+16.00 BTW STGR 26 LH/RH WAS FOUND. CORROSION ON FR 847+16.00 BTW STGR 26 LH/RH WAS EVALUATED OUT OF LIIMTS PER CRJ900 SRM 53-51-06-101-003-A05 AND WAS REPAIRED PER CRJ900 SRM 53-00-06-201-001-A03.SDR VNAA202401040029Unknown · unknownFWD PAX ACCESS PANEL MOUNT HOLE ELONGATED. FWD PAX DOOR ACCESS PANEL MOUNT HOLE ELONGATED WAS REPAIRED PER ENGINEERING ORDER (REO) NUMBER 690-52-11-878 REV - - AND EA 21-C9-52-044 REV IR SECTION II - PERMANENT REPAIRSDR VNAA202401040026Skin · dentedDENT ON EXTERNAL LOWER FUSELAGE SKIN BTW STGR 23R/24R AND FS 280-25" AT FWD FUSELAGE. DENT ON EXTERNAL LOWER FUSELAGE SKIN BTW STGR 23R/24R AND FS 280-25" AT FWD FUSELAGE WAS REPAIRED PER PER REO 670-51-00-085 REV. -A AND REO 690-53-11-1644 REV. --SDR VNAA202401040022Retainer · nickedNICKS ON CUTOUT STRCTURE OF CENTER BAGGAGE BAY DOORS, FS=519.64 BTW STRG 20L-21L AND FS=661.00 BTW STGR23L-STGR24L CUTOUT STRCTURE OF CENTER BAGGAGE BAY DOORS, FS=519.64 BTW STRG 20L-21L AND FS=661.00 BTW STGR23L-STGR24L WAS REPAIRED PER REO 690-53-31-797 RESDR VNAA202401040018Intercostal · corrodedCORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS= 319.70 TO FS= 349.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS= 319.70 TO FS= 349.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER SDR VNAA202001040011Floorbeam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (RBL12) TO CROSSBEAM FS 280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM (RBL12) TO CROSSBEAM FS 280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1640 RESDR VNAA202401040010Web · crackedCRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG HYD PUMB. UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG HYD PUMB WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01SDR VNAA202401040009Hinge · damagedDURING MEASURE WITH GO-NO-GO GAUGE IN JOB CARD TRFKE006TPGE STEP 13.2 AT FUSELAGE PIANO HINGE AT PASSENGER DOOR WAS FOUND OUT OF LIMITS. REPLACEMENT IT´S NECESSARY. PIANO HINGE AT PASSENGER DOOR WAS REPLACED PER CRJ900 SRM 53-21-23-201-007-A01SDR VNAA20240104000Skin · corrodedCORROSION ON CUT OUT AT MAIN AVIONICS COMPARTMENT DOOR BTW FS 364.00 TO FS394.00 AND STGR 25LH TO 25RH. CORROSION ON CUT OUT AT MAIN AVIONICS COMPARTMENT DOOR BTW FS 364.00 TO FS394.00 AND STGR 25LH TO 25RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND SDR VNAA202401040003Arm · wornWEAR ON ROTATING ARM AT FWD CARGO BAGGAGE BAY DOOR. ROTATING ARM AT FWD CARGO BAGGAGE BAY DOOR WAS REPAIRED PER REO 690-52-35-362 REV. --SDR VNAA202202071112Epsu · faultyEMERGENCY LIGHTS INOP / REMOVED & REPLACED EPSU BATTERY PACK IAW CRJ900 AMM 33-51-17-000/400-801. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.SDR VNAA202110101111Window · arcedCA SIDE WINDOW ARCING NEAR BOTTOM SEAL, JUST ABOVE AND SLIGHTLY LEFT OF ASH TRAY / PERFORMED GVI OF CA SIDE WINDOW IAW CRJ900 AMM 56-11-01-210-801-A01-PSA REV C. FOUND BUBBLING AND DISCOLORATION ON BOTTOM SIDE OF WINDOW, FOUND DAMAGE TO BE OUT OF LIMITS. PERFOSDR VNAA202102231112Sensor · warning lightJUST AFTER TAKEOFF, THE CREW RECEIVED A WING ANTI-ICE CAUTION MESSAGE. TO AVOID FLYING INTO POTENTIAL ICING CONDITIONS, THE CREW LEVELED OFF AT FL030 TO RUN THEIR QRH. THEY DECIDED TO RETURN TO FIELD. NO EMERGENCY WAS DECLARED. REMOVED AND REPLACED LT WINGSDR VNAA202102161111Warning Light · illuminatedAT 80 KNOTS THE CREW RECIEVED AN AMBER ANTI ICE MESSAGE AND REJECTED THE TAKE OFF. THEY PULLED OVER AND CALLED MAINTENACE AT WHICH POINT THE MESSAGE WAS CLEARED. THE AIRCRAFT IS ON ITS WAY TO ITS DESTINATION. NO EMERGENCY.SDR VNAA202101251111Connector · unsecureON THE TAKEOFF ROLL, AS THE CREW APPROACHED V1 (AT ABOUT 130 KIAS) THEY RECEIVED A WING OVERHEAT CAUTION MESSAGE AND DECIDED TO REJECT THE TAKEOFF. ONCE THEY WERE OFF, THE CREW MADE AN ANNOUCEMENT TO THE PAX OF WHAT OCCURRED, AND ALSO CONTACTED MAINTENANCE. SDR VNAA202101041111Isolation Valve · failedTHE CREW REJECTED THE TAKE OFF FROM RUNWAY 25L. SPEED BELOW 40 KNOTS. RT REV UNSAFE AMBER MESSAGE. REMOVED AND REPLACED RT TR ISOLATION CONTROL VALVE, IAW CRJ900 AMM 78-32-09-000/400-801-A01.SDR VNAA2020090311102Rod · disconnectedOVERHEAD BIN INSTALLED INCORRECTLY CAUSING INTERFERENCE WITH EMERGENCY EXIT. CONDUCTED OPERATIONS CHECK ON EMERGENCY EXIT DOORS, FOUND RIGHT AFT HITTING BIN. FOUND ROD DISCONNECTED ON AFT END OF BIN 15. CONNECTED ROD IAW CRJ 900 AMM 25-23-01-000/400-801-A50. SDR VNAA2020072511101Controller · failedCREW INITIALLY REPORTED TO THE DISPATCHER PACK SMELL IN THE COCKPIT. INFORMATION WAS LATER REVEALED THAT THE CREW DECLARED AN EMERGENCY DUE TO THE WINDSHIELD HEATING ELEMENT CRACKLING AND SPARKING. THE CREW REPORTED THE PROBLEM TO MAINTENANCE IN CLT HOWEVER DISDR VNAA2020072311102Unknown · odorCREW REPORTED BAD ODOR FROM LT A/C PACK DURING FLIGHT. COMPLIED WITH HIGH POWER ENGINE RUNS WITH PACKS ON IAW AMM 21-51-00-710-801. NO ODOR PRESENT, OPS CHECKED GOOD.SDR VNAA2020071501102Unknown · odorSTRONG ODOR IN COCKPIT PRIOR TO ACTIVATING PACKS. PERFORMED OPS TEST OF THE RECIRCULATION FAN. PERFORMED OPS TEST OF THE DISPLAY COOLING SYSTEM. PERFORMED OPS TEST OF THE AIR CONDITIONING DISTRIBUTION SYSTEM, OPS CHECK GOOD NO UNUSUAL ODOR DETECTED.SDR VNAA202003249995Joint · corrodedCIRCUMFERENTIAL JOINT FROM F.S. 280.00 TO F.S. 282.86 BETWEEN STGR 27 AND STGR 25R CORRODED AROUND SEVERAL FASTENERS. COMPLETED EA 48-2020-055 REV IR.SDR VNAA202003249994Angle · corrodedFS 280.00 FWD J ANGLE IS CORRODED. REMOVED DAMAGED FWD "J" ANGLE AT FS280 IAW CRJ 900 SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE J-ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01.SDR VNAA202003249992Drag Angle · crackedSUSPECT CRACK AT LH AFT TAIL CONE DRAG ANGLE. REMOVED LH AFT TAIL CONE DRAG ANGLE (PART #AV670-21186-003) IAW CRJ 900 SRM 51-40-00-001-001-A01. INSTALLED NEW LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01,51-42-21-001-001-A01, AND 51-42-22-001-001-A01.SDR VNAA202003249991Drag Angle · crackedSUSPECT CRACK AT RH AFT TAIL CONE DRAG ANGLE. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE RH AFT DRY ANGLE PN:AV670-21186-004 IAW CRJ 900 SRM 51-40-11-001-001-A01.SDR VNAA202003249993Frame · corrodedFRAME AT FS 310.00 IS CORRODED BETWEEN STGR 26L AND 26R. REMOVED DAMAGED SECTION AND INSTALLED FRAME AND SPLICE AT FS 310, 26L TO 26R PER CRJ900 SRM 53-00-06-995-815.
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