N598NN
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 = 'N598NN' 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 = 'N598NN' 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 VNAA2026092926101Door Frame · damagedAVIONICS DOOR FRAME, LIGHTNING STRIKE. PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN MHIRJ REO 690-53-21-2189.SDR VNAA2026092525804Skin · damagedREPAIR TO FUSELAGE STRUCTURE BETWEEN FS661.00-FS661.00+16.00 AND STR25R-27 / PERFORMED ALL WORKS USING STEPS AND DRAWINGS LISTED IN MHIRJ REO 690-53-31-1166SDR VNAA2026092525703Skin · damagedREPAIR TO FUSELAGE STRUCTURE BTA FS235.00-FS280.00 & STR25R-STR27 / PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN MHIRJ REO 690-53-11-2252SDR VNAA2026092525602Skin · damagedREPAIR TO FUSELAGE STRUCTURE BETWEEN BS 295 - 319.70, STR 24 -27R. PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN REO 690-53-21-2197SDR VNAA2026092525501Skin Panel · damagedREPAIR TO FUSELAGE LOWER SKIN PANEL BTW BS 295 AND 349 BETWEEN STR 25 & 27L. PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN REO 690-53-21-2195.SDR VNAA2026041316103Fan · odorDISPLAY FAN LOUD WITH ELECTRICAL ODOR, CW FIM 21-24-12-810-802-A01 AND FOUND DISPLAY FAN #2 TO BE BAD. DEFERRED DISPLAY FAN #2 PER MEL 21-24-02-2 CAT C . C/W M/FC BY PULLING AND COLLARING CBP1 B2. PLACARDS PLACED. VERIFIED DISPLAY COOL MSG DID NOT APPEAR. REMSDR VNAA2025071111101Tire · blownON TAKE OFF TIRE BLEW, ON GROUND CONFIRMED TREAD MISSING LEFT OB MAIN TIRE / REMOVED AND REPLACED THE #1 MLG TIRE WHEEL ASSEMBLY IAW CRJ900 AMM 32-41-01-000/400-801-A01.SDR VNAA20250602012Coaming · wornWEAR ON LATCH COAMING AND PADS ON RH AND LH UPPER/LOWER TRANSCOWLS. LATCH COAMING AND PADS ON RH AND LH UPPER/LOWER TRANSCOWLS. WERE REPLACED PER REO 670-54-21-1207 REV. A, PER CRJ-900 SRM 51-42-10-001-001-A01, CRJ-900 SRM 51-42-06-001-001-A01,PER CRJ-900 AMMSDR VNAA20250602004Hinge · damagedREPLACE ENTRY WAY PIANO HINGE. PIANO HINGE WAS REPLACED PER CRJ-900 SRM 53-21-23-201-007-A01 AND SRM 51-42-21-001--001-A01.SDR VNAA20250602016Skin · corrodedEROSION AND CORROSION WAS FOUND ON ANTENNA AND SETTLEMENT AREA EXTERNAL FUSELAGE SKIN. CORROSION ON SETTLEMENT AREA EXTERNAL FUSELAGE SKIN WAS REMOVED PER CRJ-900 SRM 53-00-01-201-017-A01. AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-01-201-017-A01 AND ASDR VNAA20250602015Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 WAS FOUND CRACK ON RIB LEADING EDGE SS57.16 WAS REPAIRED PER REO 690-57-41-240 REVSDR VNAA20250602014Fitting · corrodedCORROSION ON FLOOR FITTING ACCESS 107 COUNTER AT GALLEY 1. FLOOR FITTING ACCESS 107 COUNTER AT GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-96SDR VNAA20250602013Floor Support · crackedCRACK 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 SDR VNAA20250602011Diaphragm · crackedCRACK ON DIAPHRAGM RBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE. CRACK ON DIAPHRAGM RBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE WAS REPAIRED PER REO 670-53-82-478 REV - A.SDR VNAA20250602009Canister · 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 REPIARED PER REO670-57-42-577. REV.SDR VNAA20250602008Canister · 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 REPIARED PER REO670-57-42-577. REV.SDR VNAA20250602005Hinge · wornFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON RUDDER HINGE ASSY NO. 4 AT VERTICAL STABILIZER. RUDDER HINGE ASSY NO. 4 AT VERTICAL STABILIZER WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01.SDR VNAA20250602010Lug · corrodedCORROSION ON HOUSING (6EAS) OF HINGE FITTINGS 2,3,4 (OUTBD AND INBD) AT RH WING REAR SPAR. HOUSNGS OF HINGE FITTINGS 2 & 3 (OUTBD AND INBD) AT RH WING REAR SPAR WERE CLEANED PER CRJ 700/900 SRM 51-12-00-001-001-A01 AND HOLE OF HINGE 4 WERE REPAIRED PER REO RESDR VNAA20250602007Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 WAS FOUND. CRACK ON RIB RH LEADING EDGE SS57.16 WAS REPAIRED PER REO 690-57-41-240 REVSDR VNAA20250602006Frame · corrodedCORROSION ON FRAME 847.00 + 32.00 BTW STGR 26L TO STGR 26R AT FUSELAGE INTERNAL STRUCTURE. CORROSION ON FRAME 847.00 + 32.00 BTW STGR 26L TO STGR 26R AT FUSELAGE INTERNAL STRUCTURE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PSDR VNAA20250601010Frame · corrodedCORROSION ON FRAME 645.00 BTW STGR 18L AND STGR 19L AT AT CABIN FLOOR STRUCTURE. ON FRAME 645.00 BTW STGR 18L AND STGR 19L AT AT CABIN FLOOR STRUCTURE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-31-06-101-0SDR VNAA20250601009Stringer Splice · corrodedCORROSION ON STRINGER AND STRINGER SPLICE 25R BTW FS319.70 TO FS333.00 AT MAIN AVIONICS COMPARTMENT. STRINGER AND STRINGER SPLICE 25R BTW FS319.70 TO FS333.00 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-03-101-002-A04 AND SDR VNAA20250601008Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER BTW FS295.00/FS310.00 AND STGR26L/STGR26R AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL PRODUCTION DOUBLER BTW FS295.00/FS310.00 AND STGR26L/STGR26R AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-SDR VNAA20250602029Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL9 BTW FS693.00 TO FS1000.00 (3EA). SEAT RAILS OF LBL9 BTW FS693.00 TO FS1000.00 (3EA) WERE EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02, AND WERE REPLACED PER CRJ-900 ASDR VNAA20250602017Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS693.00 (6EA). EVALUATED, DUE EXCESSIVE DAMAGE ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS693.00 (6EAS) PER CRJ-900 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49.SDR VNAA20250601007Seat Track · corrodedLH SIDE SEAT RAIL BTW FS744.15 TO FS969.00. LH SIDE SEAT RAIL BTW FS744.15 TO FS969.00 WERE EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49 CONF(A12).SDR VNAA20250601006Seat Track · corrodedRH SIDE SEAT RAIL BTW FS744.15 TO FS969.00 (6EA). RH SIDE SEAT RAIL BTW FS744.15 TO FS969.00 (6EA) WERE EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49 CONSDR VNAA20250601005Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL27 BTW FS379.00 TO FS581.00 (3EA). CORROSION ON SEAT RAILS OF LBL27 BTW FS379.00 TO FS581.00 (3EA) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12.SDR VNAA20250601004Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL9 BTW FS379.00 TO FS693.00 (5EA). CORROSION ON SEAT RAILS OF LBL9 BTW FS379.00 TO FS693.00 (5EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACESDR VNAA20250601003Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A02, SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACEDSDR VNAA20250601002Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). CORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A01 AND SRM 53-41-49-101-001-A02 AND WERE RSDR VNAA20250602028Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS693.00 TO FS1000.00 (3EA). SEAT RAILS OF RBL9 BTW FS693.00 TO FS1000.00 (3EA) WERE EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02, AND WERE REPLACED PER CRJ-900 SDR VNAA20250602027Door Frame · wornWEAR ON FRAME OF EMERGENCY EXIT DOOR SURROUND STRUCTURE LH ON FS785.15. FRAME OF EMERGENCY EXIT DOOR SURROUND STRUCTURE LH ON FS785.15 WAS REPAIRED, THE AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTHS FROM THE ISSUE DATE OF THIS REPAIR PER REO 690-53-41-532 1SDR VNAA20250602026Intercostal · corrodedCORROSION ON INTERCOSTALS (3 EAS) BTW FS349.00/FS364.00 AND STGR26L/STGR26R AT MAIN AVIONICS COMPARMENT DOOR SURROUND STRUCTURE. CORROSION ON INTERCOSTALS (3 EAS) BTW FS349.00/FS364.00 AND STGR26L/STGR26R AT MAIN AVIONICS COMPARMENT DOOR SURROUND STRUCTURE WSDR VNAA20250602025Stringer · corrodedCORROSION ON STGR 26R BTW FS333.00 TO FS364.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR 26R BTW FS333.00 TO FS364.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED EXCESIVE DAMAGE PER CRJ/900 SRM 53-21-03-101-006-A04 AND REPLACED PER CRJ-900 SRM-51-42-06-SDR VNAA20250602022Angle · corrodedCORROSION ON ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE BTW FS310.00 AND FS349.00. DUE TO EXCESSIVE DAMAGE ON ANGLE MID CAP AT PASSENGER DOOR SURROUND STRUCTURE BTW FS310.00 AND FS349.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01SDR VNAA20250601001Floor Support · corrodedCORROSION ON FLOOR SILL, LOCATED BTW FS=349.00 AND RBL 43" AT FUSELAGE FLOOR STRUCTURE. FLOOR SILL, LOCATED BTW FS=349.00 AND RBL 43" AT FUSELAGE FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-21-1938 REV. - .SDR VNAA20250602024Bracket · corrodedCORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. PAINT ON BRACKETS(3E/AS) BTW FS 533.00/FS 549.00 STRG 24/25RH, FS 565.00 STRG 23/22LH AND FS 661.00 STRG 27/26LH WAS REMOVED PER CRJ-900 SRM 51-26-01-001-001-A01, GVI WASSDR VNAA20250602023Hinge · wornWEAR IN PASSENGER-DOOR PIANO HINGE ON THE FUSELAGE SIDE, BETWEEN FS333.00 AND FS349. PASSENGER-DOOR PIANO HINGE ON THE FUSELAGE SIDE, BETWEEN FS333.00 AND FS349.00 WAS REPAIRED PER REO 670-53-21-582 REV. -G.SDR VNAA20250602020Skin · damagedPERMANENT REPAIR OF THE PAX DOOR CUTOUT LOWER FWD CORNER ACCOMPLISH PERMANENT REPAIR PER REO 690-53-21-1441. PAX DOOR CUT OUT LOWER FWD CORNER WAS REPAIRED PER CRJ-900 SRM 53-21-01-201-010-A01.SDR VNAA20250602021Skin · damagedDAMAGE ON RH VERTICAL STAB REAR SPAR DATUM. RH VERTICAL STAB REAR SPAR DATUM WAS REPAIRED PER REO 690-53-71-087 REV. -SDR VNAA20250602019Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) CORRECTIVE ACTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DATUSDR VNAA20250602018Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) CORRECTIVE ACTION: CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FWD DRAG ANGLES BTW 55.625% STGR DASDR VNAA20250602001Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW FS 1181.00 TO FS1211.00 OF THE AREA COVERED BY LH/RH VENTRAL FIN FAIRING DENTS ON EX•TER NAL FUSELAGE SKIN BTW FS 1181.00 TO FS1211.00 OF THE AREA COVERED BY LH/RH VENTRAL FIN FAIRING WERE REPAIRED PER REO 690-53-7SDR VNAA20250602003Fitting · corrodedCORROSION AND MISSING NUT ON GALLEY FLOOR SUPPORTS (2EAS) LOCATED BTW FS 280.00 - FS 295.00 AT FUSELAGE FLOOR STRUCTURE RH. CORROSION LOCATED BTW FS 280.00 - FS 295.00 AT FUSELAGE FLOOR STRUCTURE RH WAS EVALUATED DUE TO EXCESIVE DAMAGE ON SUPPORT (1EA) PER CRSDR VNAA20250602002Fitting · corrodedCORROSION ON SETTLEMENT FITTING (1EA) BTW FS 379 AND FS 394, RBL12 OF FWD LAVATORY AT FUSELAGE FLOOR STRUCTURE. CORROSION ON SETTLEMENT FITTING (1EA) BTW FS 379 AND FS 394, RBL12 OF FWD LAVATORY AT FUSELAGE FLOOR STRUCTURE WAS EVALUATED DUE TO EXCESIVE DAMAGSDR VNAA2024072211101Wire Harness · faultedBRAKE OVERHEAT WARNING MSG IN FLIGHT / REMOVED AND REPLACED LH OB PROXIMITY SENSOR HARNESS ASSEMBLY IAW CRJ 900 AMM 32-61-05-000/400-803-A01. ALL OPS CHECKS GOOD AT THIS TIME. THIS CLEARS MEL.SDR VNAA2024050711102Unknown · odorUPON BATTERY MASTER SWITCH ON BURNING SMELL IN FLIGHT DECK / INTERROGATED MDC FOUND NO B1 CODES. TROUBLESHOT SMELL IN THE COCKPIT BY RESETTING THE AIRCRAFT 2 TIMES. TURNED BOTH THE PACKS ON. SET WINDOW HEAT ON HIGH. TURNED RECIRCULATING FAN ON. SET DISPLAY FANSDR VNAA2024050711101Unknown · odorBURNING SMELL AFTER APU START, ENGINES SHUT DOWN ON APU BLEED SUPPLY / STARTED APU IAW CRJ900 AMM 49-10-00-866-801-A01 RAN PACKS AT FULL BLAST STILL NO SMELL. RAN BOTH ENGINES WITH PACKS AND RECIRCULATION FAN IAW CRJ900 AMM 71-00-00-866-806-A02. NO SMELL. TAXISDR VNAA2023101611101Acm · odorFA AND PASSENGERS REPORT VISUAL SMOKE IN THE CABIN WITH RUBBER BURNING SMELL DURING THE TAKE OFF ROLL, BLEED CONFIGURED AUTO/ISO-CLOSED, APU OFF/BOTH ENGINES/BOTH PACKS WHERE ON / REMOVED AND REPLACED RH ACM IAW CRJ900 AMM 21-51-08-000/400-801 A01. OPS AND LEA
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