N573NN
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 = 'N573NN' 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 = 'N573NN' 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 VNAA2025090311101Motor · failedHYD 3 LO PRESS, HYD PUMP 3A CAUTION. IB GNS SPLRS. ON LANDING R REV INOP CAUTION. / REMOVED AND REPLACED HYD SYS 3A ACMP IAW CRJ 900 AMM 29-12-03-000/400-801. OPS CHECK AND LEAK CHECK GOOD.SDR VNAA2024120811102Window · unserviceableRIGHT WINDOW ARCING IN FLIGHT MULTIPLE TIMES. RIGHT WINDOW CAUTION ILLUMINATED. / REMOVED AND REPLACED RH SIDE WINDOW IAW CRJ 900 AMM 56-12-01-000/400-801-A01-PSA. LEAK CHECK GOOD. WINDOW TEMP CONTROLLER OPS CHECK GOOD IAW CRJ 900 AMM 30-41-06-710-801.SDR VNAA2024040911103Coffeemaker · smokeLH COFFEE MAKER SMOKING / TROUBLESHOT IAW CRJ 900 FIM 21-22-00-810-806-A01. UPON OBSERVATION NO SMOKE OR SMELL WAS FOUND. LH COFFEE MAKER NEEDS REPLACED. REMOVED AND REPLACED LH COFFEE MAKER IAW CRJ 900 AMM 25-32-06-000/400-801-A08-PSA. OPS TEST GOOD.SDR VNAA202403230020Bushing · corrodedCORROSION ON BORES OF CENTER FITTING LUGS R1,R2,R5, R6 AND UPPER BORE ON OUTBD FITTING AT RH AILERON. BORES OF CENTER FITTING LUGS R1,R2,R5, R6 AND UPPER BORE ON OUTBD FITTING AT RH AILERON WERE REPAIRED PER PER REO 670-57-61-237 REV - -SDR VNAA202403230019Bushing · corrodedCORROSION ON BORES OF CENTER FITTING LUGS L1, L3, L5 AND L6 WAS FOUND AT LH AILERON. CORROSION ON BORES OF CENTER FITTING LUGS L1, L3, L5 AND L6 AT LH AILERON WERE REPAIRED PER PER REO 670-57-61-237 REV - -SDR VNAA202403230011Bushing · corrodedINBD BORE OF FITTING #1 WAS FOUND ON LH WING TRAILING EDGE. INBD BORE OF FITTING #1 WAS FOUND ON LH WING TRAILING EDGE WAS REPAIRED PER ETI-900-23-010 REV. ORIG. & REO 690-57-51-334 REV. --SDR VNAA202403230018Canister · crackedDURING INSPECTION OF THE TASK CARD 600-08E2-JIC, IT WAS DETECTED CRACK IN CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK WAS:REPAIR PER REO 670-57-42-577. REV. - -SDR VNAA202403230017Hinge Fitting · nickedNICK ON AILERON HINGE FITTING 3 (INBD LUG) AT RH WING REAR SPAR. NICK ON AILERON HINGE FITTING 3 (INBD LUG) AT RH WING REAR SPAR WAS REPAIRED PER REO 690-57-51-331 REV. - -SDR VNAA202403230029Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS=581 TO FS=661+32 AND LBL 9'' / RBL 9''. FLOOR SEAT RAILS BTW FS=581 TO FS=661+32 AND LBL 9'' / RBL 9'' ARE OUT OFF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 NOTE 1 AND FLOOR SEAT RAILS BTW FS=581 TO FS=661+32 AND LBL SDR VNAA202403230028Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS=485 TO FS=581 LBL 9'' / RBL 9''. FLOOR SEAT RAILS BTW FS=485 TO FS=581 LBL 9'' / RBL 9''. WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNAA202403230027Seat Track · corrodedDISCREPANCY: CORROSION ON FLOOR SEAT RAILS BTW FS=349 TO FS=485 LBL 9'' / RBL 9''. FLOOR SEAT RAILS BTW FS=349 TO FS=485 LBL 9'' / RBL 9''. WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12SDR VNAA202403230025Plate · corrodedDISCREPANCY: CORROSION ON KICK PLATE AND MID CAP AT PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON KICK PLATE AND MID CAP AT PASSENGER DOOR SURROUND STRUCTURE WERE REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01,FOR EXCESSIVE DAMAGE MID CAP OUT OFF LIMITS PER SDR VNAA202403230021Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS=661+32 TO FS=677 AND LBL 9'' / RBL 9' CORROSION ON FLOOR SEAT RAILS BTW FS=661+32 TO FS=677 AND LBL 9'' / RBL 9'' WERE EVALUATED OUT OF LIMITS PER
CRJ-900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-SDR VNAA202403230015Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING. DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING WERE REPAIRED PER REO 690-53-61-1348REV --SDR VNAA202403230014Seat Track · corrodedCORROSION ON SIDE SEAT RAILS BTW FS=785 TO FS=977, STGR 15 LH AND RH . SIDE SEAT RAIL STGR 15L BTW FS785.15 TO FS969; STGR 15R BTW FS785.15 TO FS927 WERE EVALUATED OUT OF LIMITS PER
CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRM 53-51-49-101-001-A02 AND WERSDR VNAA202403230013Seat Track · corrodedCORROSION ON SIDE SEAT RAILS, FS=677 TO FS=761, STGR15, LH AND RH SIDE SEAT RAILS, FS=677 TO FS=761, STGR15, LH AND RH WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12).SDR VNAA202403230012Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS=847+16 TO FS=977 AND LBL 9''. FLOOR SEAT RAILS BTW FS=847+16 TO FS=977 AND LBL 9''. WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)SDR VNA2024F00004Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE SDR VNA2024F00003Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE ATSDR VNA2024F00001Floor Support · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-SDR VNAA202403230026Striker · corrodedSEVERAL CORROSIONS ON SEAL STRIKER (R1) LOCATED BTW FS=310.00 TO FS=349.00 AND RBL 43" AT FUSELAGE FLOOR STRUCTURE SERVICE DOOR. SEAL STRIKER (ANGLE-MOUNTING)(R1) LOCATED BTW FS=310.00 TO FS=349.00 AND RBL 43" AT FUSELAGE FLOOR STRUCTURE SERVICE DOOR WAS REPLSDR VNAA202403230024Skin · damagedPERM REPAIR BEFORE 20,337.49 FH - LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN FS501.00 - FS661+16 & STR26L - STR23R THIS TEMPORARY DISPOSITION IS VALID FOR 600 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO AT REV - - . PERM REPAIR BEFORE 20,33SDR VNAA202403230023Striker · damagedREPAIR TO PAX DOOR SEAL STRIKER PERMANENT REPAIR REQD TO PASSENGER DOOR SEAL STRIKER. SEE W.O. AND REO 670-53 -22-001 FOR DETAILS. PAX DOOR SEAL STRIKER WAS REPAIRED PER REO 670-53-22-001. REV. J. REPAIR (TYPE IV)SDR VNAA202403230022Bracket · corrodedCORROSION ON BRACKETS, MACHINED (05 EAS) OF INTERNAL STRUCTURE AT FWD & CTR CARGO COMPARTMENT. BRACKETS, MACHINED (05 EAS) OF INTERNAL STRUCTURE AT FWD & CTR CARGO COMPARTMENT WERE REPLACED PERCRJ900 SRM 51-42-22-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001SDR VNAA202403230010Rib · crackedAFTER ACCESS PANEL 521BL REMOVAL, CRACK ON MACHINED RIB LEADING EDGE SS 57.16 AT LEFT WING. (SM). MACHINED RIB LEADING EDGE SS 57.16 AT LEFT WING. (SM) WAS REPAIRED PER REO 690-57-41-240. REV. --SDR VNAA202403230009Intercostal · corrodedCORROSION ON INTERCOSTAL BTW STGR 27LH TO STGR 26LH, BTW FS 349.00 TO FS 364.00. INTERCOSTAL BTW STGR 27LH TO STGR 26LH, BTW FS 349.00 TO FS 364.00 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.SDR VNAA202403230008Support Fitting · corrodedCORROSION ON JACK FITTING SUPPORTS LH/RH AT FWD JACK FITTING. CORROSION ON JACK FITTING SUPPORTS LH AND RH AT FWD JACK FITTING WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 WERE MEASURED AND FOUND SUPPORT LH WITHIN LIMITS AND SUPPORT RH OUT OFF LIMITS PERSDR VNAA202403230007Web · crackedDISCREPANCY: INITIAL INSPECTION': CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. (SM) ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. (SM) WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.SDR VNAA202403230006Arm · wornWEAR ON FWD AND AFT COUNTERBALANCE ARM AT FWD CARGO COMPARTMENT DOOR AND WEAR ON FWD COUNTERBALANCE ARM OF CTR CARGO COMPARTMENT DOOR. WEAR ON FWD AND AFT COUNTERBALANCE ARM AT FWD CARGO COMPARTMENT DOOR AND WEAR ON FWD COUNTERBALANCE ARM OF CTR CARGO COMPARSDR VNAA202403230005Pad · damagedDURING REPAIR D JACKING PAD HELICOIL INSERT LHS IN REF. REO 670-57-22-004 REV.F, TOOL MARK WERE NOTED. DURING REPAIR D JACKING PAD HELICOIL INSERT LHS WAS DETECTED DAMAGE ,TOOL MARK WERE NOTED. REPAIR PREVIOUS. THEREFORE JACKING FITTING ASSY WAS REPLACEDSDR VNA2024F00002Rib · crackedAFTER ACCESS PANEL 621BR REMOVAL, CRACK ON MACHINED RIB LEADING EDGE SS 57.16 AT RIGHT WING. CRACK ON MACHINED RIB LEADING EDGE SS 57.16 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240. REV. - -SDR VNAA202403230016Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING. DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING WERE REPAIRED PER REO 690-53-61-1349 REV --SDR VNAA2023111411102Unknown · unknownSERVICE DOOR CAUTION MSG IN FLIGHT / INTERROGATED MDC AND FOUND B1 CODE 007792. TROUBLESHOT IAW CRJ 900 FIM 52-70-06-810-811-A02. SUSPECTED PROXIMITY SENSOR PX38 OUT OF RIG. ADJUSTED GALLEY SERVICE DOOR SENSOR PX38 IAW CRJ 900 52-70-06-820-802-A01. OPS CHECK GSDR V0XD20230926001Skin · scratchedFUSELAGE SKIN AT RS 333.00 TO FS 477.0 BETWEEN STGR 24R AND STGR 25R IS SCRATCHED. CORRECTIVE ACTION: CLEANED AREA, VERIFIED BLENDED AREA MEASUREMENTS PERFORMED NDT IAW OLIVER WYMAN/CAVOK EA 23-C9-53-0689 REV. C DATED 9/25/2023. DTE TO BE ACCOMPLISHED WITHIN 1SDR VNAA202207051111Smoke Detector · unserviceableSMOKE AFT LAV. REMOVED AND REPLACED SMOKE DETECTOR IAW CRJ 900 AMM 26-16-01-000/400-801-A01-PSA OPS CHECK GOOD. PERFORMED OPS TEST OF THE AIR CONDITIONING DISTRIBUTION SYSTEM IAW CRJ 900 AMM 21-51-00-710-801. OPS CHECK GOOD. NO SMOKE OR ODORS DETECTED.SDR VNAA202111231111Control Unit · unserviceableENROUTE TO CLT THE CREW RECEIVED A STAB TRIM/MACH TRIM FAIL MESSAGES. THE CREW RAN THE QRH AND THE RESET WAS UNSUCCESSFUL. THEY DECLARED EMERGENCY AND WERE CLEARED DIRECT TO CLT. THEY LANDED AND TAXIED TO THE GATE WITHOUT FURTHER ISSUE. NO FURTHER INFORMATION.SDR VNAA202111071111Reservoir · malfunctionedON DEPARTURE, #3 HYD SYSTEM CAUTION DURING GEAR RETRACTION. THEY DECLARED AN EMERGENCY, RETURNED TO CLT AND LANDED WITHOUT ISSUES IN CLT. THEY WERE NOT OVERWEIGHT ON LANDING. RTF-UPON SELECTED GEAR UP AFTER ROTATION HYD PUMP 3A AMBER CAS. FOLLOWED BY INBD GRNDSDR VNAA202109101111Power Unit · defectiveBURNING ELECTRICAL SMELL IN FLIGHT DECK WHILE CONNECTED TO GROUND POWER AND BATTERY MASTER ON. FOUND GOUND POWER UNIT TO BE DEFECTIVE. POWERED UP APU IAW 49-10-00-866-801-A02. NO SMELL OF BURNING ELECTRICAL AC OK FOR SERVICESDR VNAA202105181111Acm · smokeWHILE ON TAXI OUT TO RUNWAY, THE AC PACKS OVERHEATED AND THEY STARTED TO PUSH SMOKE INTO THE CABIN. CREW TURNED THE PACKS OFF AND THE CABIN STARTED TO CLEAR OUT. THEY RETURNED TO GATE AND MAINTENANCE HAS BEEN CALLED. PERFORMED OPS CHECK OF THE AIR CONDITIONINGSDR VNAA202011081112Transducer · unknownREJECTED TAKE OFF FOR AN ANTI SKID AMBER CAUTION MESSAGE RUNWAY 10 AT 70 KNOTS. NO EMERGENCY. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. R & R WHEEL SPEED TRANSDUCER.SDR VNAA2020080911102Nut · looseFLIGHT 5633, ON TAKEOFF ABNOMAL WHEEL VIBRATIONS AND UNUSUAL STEERING NEAR ROTATION. DECLARED EMERGENCY AS A PRECAUTION AND WAS ABLE TO LAND SAFELY. TORQUED NLG WHEEL NUTS IAW AMM 32-42-01-400-801.SDR VNAA2020060299911Web · corrodedRIGHT WEB BEHIND FS 280 BULKHEAD, FOUND TO BE CORRODED DURING ACCOMPLISHMENT OF ACCESS FOR 280 STRUCTURAL REPAIR. WEB REPAIRED.SDR VNAA2020060299910Crossbeam · corrodedFS 280 RT CROSSBEAM FOUND TO BE CORRODED BETWEEN RBL12 AND BL0. CROSSBEAM REPLACED.SDR VNAA202006029999Crossbeam · corrodedFS 280 LT CROSSBEAM FOUND TO BE CORRODED BETWEEN LBL 12 AND BL 0. CROSSBEAM REPLACED.SDR VNAA202006029998Support Angle · corrodedFS 280 FWD FLOOR SUPPORT ANGLE BETWEEN LBL 12 AND RBL 12 IS CORRODED. REPLACED ANGLE.SDR VNAA202006029997Stringer · corrodedSTR 26R IS CORRODED BETWEEN FS 319 AND FS 333. REPLACED STRINGER.SDR VNAA202006029996Frame · corrodedFS 310 IS CORRODED BETWEEN STR 26L AND STR 26R.SDR VNAA202006029995Joint · corrodedFS 280 CIRCUMVENTION JOINT IS CORRODED BETWEEN STGR 25L AND 25R.SDR VNAA202006029994Intercostal · corrodedATTACHMENT ANGLE FWD OF FS 364, RBL 26 IS CORRODED. REMOVED CORRODED INTERCOSTAL AT STR 26R. REPLACED INTERCOSTAL.SDR VNAA202006029993Stringer · corrodedSTRINGER 26R IS CORRODED FWD OF FS 364. REPLACED STRINGER.
Back to N573NN