N595NN
Service difficulty reports · 50
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 = 'N595NN' 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 = 'N595NN' 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 VNAA2025111211101Smoke Detector · false activationSMOKE FWD LAV WARNING DISP IN FLIGHT. COMPLETED QRC DIVERTED MEM / PERFORMED OPS CHECK OF FWD LAV SMOKE DETECTOR IAW AMM 26-16-00-710-804-A01-PSA. NO DEFECTS NOTED AT THIS TIME. NO BURN MARKS NOTED.SDR VNAA2025041411103Sink · cloggedAFT LAV SINK OVER FLOWED, CAUSED SMOKE AFT LAV TO DISPLAY ON ED1 VISIBLE SMOKE IN LAV, SINK FAUCET CAME OFF COMPLETELY. VISIBLE SMOKE WAS NOTED IN THE AFT LAV, AND NO MEDICAL ATTENTION WAS REQUIRED / OPENED UP ALL COMPARTMENTS FOR DETAILED INTERNAL GVI INSPECTSDR VNAA202501210030Seat Track · crackedMANUFACTURING PART. IN REFERENCE NRC 00218: FABRICATE FITTING SEAT TRACK P/N: 9401251-1 (2 EAS) IN REFERENCE TO EA NO: A1-690-25-00357 MMARY OF NRC 00218: FITTING SEAT TRACK P/N: 9401251-1 (2 EAS) WERE FABRICATED PER EA NO: A1-690-25-00357.SDR VNAA202501210025Seat Track · corrodedCORROSION ON SEAT RAILS (4 EAS) AT RBL9/LBL9 FROM FS693 TO FS 969.00 CORROSION ON SEAT RAILS (4 EAS) AT RBL9/LBL9 FROM FS693 TO FS 969.00 AT PASSENGER CABIN WAS REMOVED PER CRJ900 SRM
51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-41-SDR VNAA202501210024Seat Track · corrodedCORROSION ON SIDE SEAT RAILS (6 EAS) AT STGR 15LH FROM FS744.15 TO FS 969.00 CORROSION ON SIDE SEAT RAILS (6 EAS) AT STGR 15LH FROM FS744.15 TO FS 969.00 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-41-49-10SDR VNAA202501210023Seat Track · corrodedCORROSION ON SIDE SEAT RAILS (6 EAS) AT STGR 15RH FROM FS744.15 TO FS 969.00. CORROSION ON SIDE SEAT RAILS (6 EAS) AT STGR 15RH FROM FS744.15 TO FS 969.00 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-41-49-101-SDR VNAA202501210022Seat Track · corrodedCORROSION ON SEAT RAILS LBL9 (3 EAS), LBL27 (2 EAS) AND RBL9 (5 EAS) BETWEEN FS447.40 TO FS693.00 AT PASSENGER CABIN. CORROSION ON SEAT RAILS LBL9 (3 EAS), LBL27 (2 EAS) AND RBL9 (5 EAS) BETWEEN FS447.40 TO FS693.00 AT PASSENGER CABIN WAS REMOVED PER CRJ900 SDR VNAA202501210021Seat Track · corrodedCORROSION ON SEAT RAILS LBL9 (1 EA), LBL27 (1 EA) AND RBL9 (1 EA) BETWEEN FS 349.00 TO FS 477.40 AT PASSENGER CABIN, CORROSION ON SEAT RAIL LBL27 (1 EA) AND RBL9 (1 EA) BETWEEN FS 349.00 TO FS 477.40 AT PASSENGER CABIN WAS REMOVED PER CRJ900 SRM 51-21-06-001-SDR VNAA202501210019Stringer · corrodedCORROSION ON STGR 20LH BTW FS310.00 AND FS333.00 CORROSION ON STGR 20LH BTW FS310.00 AND FS333.00 WAS ATTENDED PER REO 690-53-21-1863 REV.--.SDR VNAA202501210018Floor Support · corrodedCORROSION ON MID CAP BTW FS 310.00 AND 333.00 LBL 43. MID CAP BTW FS 310.00 AND 333.00 LBL 43 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01SDR VNAA202501210017Floor Support · corrodedCORROSION ON GALLEY FLOOR SUPPORTS (5EAS) LOCATED BTW FS 280.00 - FS 295.00 AND AT FWD FUSELAGE FLOOR STRUCTURE. PER CRJ-900 SRM 51-42-21-001-001-A01 AND GALLEY FLOOR SUPPORT (1EAS) LOCATED BTW FS 280.00 - FS 295.00 WAS CLEANED PER CRJ900 SRM 51-26-00-001-SDR VNAA202501210014Intercostal · corrodedCORROSION ON INTERCOSTAL BTW FS= 349.00 TO FS= 364.00 AND STGR 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL BTW FS= 349.00 TO FS= 364.00 AND STGR 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ/900 SRM 51-21-06-001-001-A01 AND EVALUATED WSDR VNAA202501210016Access Panel · corrodedCORROSION ON SETTLEMENT AREA AT ACCESS PANEL 572AB OF LH WING CORROSION ON SETTLEMENT AREA AT ACCESS PANEL 572AB OF LH WING WAS REPAIRED PER REO 690-57-31-251 REV- -SDR VNAA20250121007Track · crackedCRACK ON STRUCTURE OF THE AFT DOOR TRACK AT AFT BAGGAGE BAY DOOR CRACK ON STRUCTURE OF THE AFT DOOR TRACK (DIAPHRAGM) AT AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 , SRM 51-42-21-001-001-A01 AND SRM 51-42-13-001-001-A01.SDR VNAA2025012100 13Intercostal · corrodedCORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS= 349.00 TO FS= 364.00 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS= 349.00 TO FS.364 STG 20RH AT MAIN AVIONICS COMPARTMENT WERE REPLACED PER CRJ900 SRM 51-42-21-0SDR VNAA202501210012Floorbeam · corrodedCK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BSDR VNAA202501210026Hinge Fitting · excess playFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. CORRECTIVE ACTION: SUMMARY: HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103 REV.SDR VNAA202501210028Canister · crackedCRACK IN CANISTER NO.3 , STA. WS148 OF INTERNAL LH MAIN FUEL TANK CRACK IN CANISTER NO.3 , STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV.SDR VNAA20250121009Plate · corrodedCORROSION ON KICK PLATE AT PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON KICK PLATE AT PASSENGER DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01SDR VNAA202501210027Canister · crackedCRACK IN CANISTER NO.3 , STA. WS148 OF INTERNAL RH MAIN FUEL TANK CANISTER WELDED NO. 3 IN STA WS 148.00 RH FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --SDR VNAA202501210015Intercostal · corrodedCORROSION ON INTERCOSTAL BTW FS= 349.00 TO FS= 364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL BTW FS= 349.00 TO FS= 364.00 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM-51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01SDR VNAA20250121008Skin · dentedDURING INSPECTION OF THE TASK CARD 200-01-JIC. IT WAS DETECTED DENT ON SKIN RH BTW FS 169.00 TO FS 177.00 AT FWD FUSELAGE DENT ON SKIN RH BTW FS 169.00 TO FS 177.00 AT FWD FUSELAGE WAS REPAIRED PER REO 690-53-11-1925 REV - -SDR VNAA20250121006Drag Angle · crackedCRACKS ON RH / LH VERTICAL STABILIZER INTERSECTS WITH THE FUSELAGE ATTACHMENT FWD DRAG ANGLES, (BOTH SIDES). RH / LH VERTICAL STABILIZER INTERSECTS WITH THE FUSELAGE ATTACHMENT FWD DRAG ANGLES, (BOTH SIDES) WERE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01SDR VNAA20250121005Fairing · elongatedBULLET FAIRING FWD FRAME ELONGATED FASTENER HOLE BULLET FAIRING FWD FRAME ELONGATED FASTENER HOLE WAS REPAIRED PER REO 690-55-32-188 REV.--SDR VNAA20250121004Arm · excess playFWD BAGGAGE BAY DOOR FWD INNER ARM WITHIN 2099.65 FLIGHT HOURS AFTER SECTION I (3963.35FH FROM EA 23-C9-52- 0913 RELEASE) (BEFORE 19,894.41 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES.CORRECTIVE ACTION: SUMMARY: FWD BAGGSDR VNAA20250121003Fan Cowl · dentedTRFKE00AP6E2:EA23-C9-54-0795-PERM REPAIR BEFORE 19,894.41 FH - DOOR ASSY, FAN COWL, LWR (LH)ORRECTIVE ACTION: SUMMARY: DOOR ASSY, FAN COWL, LWR (LH) WAS REPAIRED PER REO 670-54-14-1012. REV. B. AND REO 690-54-14-761 REV -- (P1).SDR VNAA20250121001Floorbeam · corrodedCRACKED 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 690-53-11-1914 REV --SDR VNAA202501210029Floorbeam · corrodedCORROSION AT MOUNTING ANGLE AND 3 LOWER SILL ANGLES (WEB FLOOR PROTECTOR ANGLES) OF SERVICE DOOR SURROUND STRUCTURE. CORROSION ON 3 LOWER SILL ANGLES (WEB FLOOR PROTECTOR ANGLES) OF SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED WITHIN LIMITS PERSDR VNAA20250121002Seat Track · damagedTEMP/PERM REPAIR FOR MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS PERM REPAIR FOR MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS WAS PERFORMED PER REO 670-53-11-210 REV-DSDR VNAA202501210020Seat Track · corrodedCORROSION AT SIDE SEAT RAIL (2 EAS) OF STRG 15RH/STRG 15LH BETWEEN FS669.40 TO FS720.85 CORROSION AT SIDE SEAT RAIL (2EAS) OF STRG 15RH/STRG 15LH BETWEEN FS669.40 TO FS720.85 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CSDR VNAA202501210011Skin · wornWEAR ON INTERNAL FUSELAGE SKIN, SETTLEMENT AREA OF AVIONICS COMPARTMENT DOOR. (E/E). WEAR ON INTERNAL FUSELAGE SKIN, SETTLEMENT AREA OF AVIONICS COMPARTMENT DOOR. (E/E). WAS REPAIRED PER REO 690-53-21-032 REV. ••SDR VNAA2024090211101Acm · odorSTRONG SMELL IN CABIN WITH HAZY AIR. R PACK TEMP CLIMBED TO 73C. / REMOVED AND REPLACED RH ACM IAW CRJ900 AMM 21-51-08-000/400-801. OPERATIONAL CHECK GOOD NO FAULTS, LEAK CHECK GOOD.SDR VNAA2024011711101Cover · missingUPON FURTHER INSPECTION NOTED COVER MISSING FOR LOW PRESSURE GROUND AIR CONNECTION AND LANYARD END FRAYED. REF. CRJ900 AMM 21-20-02-400-801-A01 / INSTALLED NEW LOW PRESSURE GROUND AIR CONNECTION COVER IAW CRJ 900 AMM 21-20-02-400-801-A01. REMOVED AND REPLACED SDR VNAA202306061111Acm · smokeSMOKE IN THE CABIN / REMOVED AND REPLACED RH ACM IAW CRJ900 AMM 21-51-08-000/400-801. REMOVED AND REPLACED MT20 IAW CRJ-900 AMM 21-51-10-000/400-801. RH PACK FAULT CLEARED. ALL OPS CHECKS AND LEAK CHECKS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.SDR VNAA202208021111Spoiler · warning messageCA OF 5646 ON TAIL 595 DECLARED EMERGENCY AT 2230Z FOR FLT SPLRS CAUTION MESSAGE IN FLIGHT, LANDED SAFELY WITH NO INJURIES, NO O2 MASKS, AND NO CALL FOR BRACE. TRUCKS ROLLED AND CA HAD THEM STANDBY TO BE SAFE UNTIL HE LANDED AND THEY WERE CLEARED OUT. IB FLT SSDR VNAA202110181111Acm · smokeAT 1000FT ABOUT 3-4NM OUT OF KGSP THE CREW HAD REALIZED THERE WAS SMOKE IN THE CABIN/COCKPIT. PILOTS WERE THEN NOTIFIED OF A LH PACJK FAILURE. CREW LANDED SAFELY ON THE GROUND AT 1758. DISPATCH WAS NOT NOTIFIED OF THE OCCURANCE UNTIL 1805Z, THEY BLOCKED IN AT SDR VNAA202107201111Selector Valve · malfunctionedGEAR DISAGREE RED MESSAGE WITH GEAR SELECT DOWN GOING INTO BHM. THE GEAR EMERGENCY HANDLE WAS USED, BUT NO EMERGNCY WAS DECLARED. AIRCRAFT LANDED SAFELY IN BHM. THEY HAD TO BE TOWED INTO THE GATE. R+R MLG SELECTOR VALVE IAW CRJ 900 AMM 32-32-10-000/400-801-A01SDR VNAA202104121111Skin · scratchedDURING SCHEDULED MAINTENANCE AT CVG THE MAIN CABIN (PAX) OUTER DOOR SKIN WAS REPORTED TO BE SCRATCHED / GOUGED ON THE UPPER FORWARD CORNER OF THE DOOR. DAMAGE WAS REPORTED AT SIX (6) LOCATIONS. SEE FIGURE 1 SHEET 1-3 FOR SIZE AND LOCATION OF DAMAGE. / PER ENGISDR VNAA202102041111Shutoff Valve · unserviceableAFTER BEING CLEARED FOR TAKEOFF IN TYS, CREW REPORTED A REJECTED TAKE OFF WHILE ON RWY 23L, AT 2KTS. CREW REPORTED A LT ENG BLEED (C) MSG. AIRCRAFT RETURN TO GATE. R & R LT COWL ANTI-ICE SOV IAW CRJ900 AMM 30-22-01-000/400-801-A01. OPS CHECK GOOD.SDR VNAA2020111211211Warning Message · illuminatedMAINTENANCE EMERGENCY FOR INBOARD SPOILERONS CAUTION MESSAGE IN FLIGHT. CREW DID NOT HAVE PASSENGERS BRACE OR THE FIRE TRUCKS ROLL. WAS ABLE TO LAND SAFELY AND TAXI TO GATE UNDER OWN POWER.SDR VNAA2020022751101Windshield · arcedIN FLIGHT THE CAPTAINS SIDE WINDSHIELD HEAT TERMINAL BLOCK BEGAN TO SMOKE AND STRONG ELECTRICAL BURNING. REMOVED AND REPLACED WINDSHIELD (LH) IAW CRJ 900 AMM. LEAK AND OPS CHECK GOOD.SDR VNAA2020021501101Motor · failedCREW LOST HYDRAULIC SYSTEM 3 DURING APPROACH INTO ATL. THEY DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MX REPLENISHED HYDRAULIC SYSTEM 3 TO CORRECT LEVEL . REMOVED AND REPLACED #3B HYDRAULIC PUMP DUE TO HYDRAULIC FLUID STARVATION IAW CRJ 900 AMSDR VNAA202001031102Warning Message · false activationOB SPLRNS AND OB FLT SPLRS AMBER MESSAGE. PERFORMED SYSTEM RESET, PROBLEM DID NOT REOCCURSDR VNAA20191212101Warning Message · false activationAT FL100 FLIGHT 5345 RECEIVED INBOARD FLIGHT SPOILERONS AND SPOILER CAUTION MESSAGE. CAPT FOLLOWED QRH WHILE FO FLEW THE AC. PAX WERE NOTIFIED OF THE EMERGENCY LANDING BY THE FLIGHT ATTENDANTS. THE AC LANDED SAFELY AND TAXI TO THE GATE UNDER OWN POWER. EMERGENSDR VNAA201908121101Windshield · crackedCLIMBING TO 17000, CAPTAIN SIDE WINDSHIELD CRACKED. CREW DECLARED EMERGENCY BACK TO DEPARTURE, WHERE CABIN WAS PREPPED FOR EMERGENCY LANDING. EMERGENCY EQUIPMENT RESPONDED AND AIRCRAFT WAS ABLE TO TAXI BACK TO GATE. MAINTENANCE REMOVED AND REPLACED LEFT WINDOSDR VNAA2019100121001Battery Pack · inoperativeMULTIPLE FWD EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED 3 EMERGENCY LIGHT BATTERIES. P/N 2013-1A S/N 6114, 87108, 121690. OPS CHECKED GOOD.SDR VNAA2019011511101Shutoff Valve · malfunctionedRECIVED A LT AND RT WING ANITICE CAUTION MSG ON DESCENT INTO MSN. CREW DECLARED AND LANDED WITHOUT INCIDENT. OUTSTATION MAINTENANCE REMOVED AND REPLACED THE LH WING A/I MODULATING SOV. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.SDR VNAA2018092711101Acm · failedSUPPLEMENTAL INFORMATION: MX REMOVED AND REPLACED RH ACM. OPS AND LEAK CHECK GOOD. THIS CLEARS MELSDR VNAA2017100811101A/C Pack · failedDURING TAXI, RECEIVED A RT PACK AUTO FAIL MESSAGE AND THE FLIGHT ATTENDANT SMELLED SMOKE.SDR VNAA2016121200021Sign · brokenEMERGENCY LIGHT AT PASSENDOR DOOR BROKEN. SECURED HARDWARE ON ENTRANCE COMPARTMENT EMERGENCY EXIT SIGN.
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