N8390A

Service difficulty reports · 87

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 = 'N8390A' 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.

SDR REXA201100371Structure · damagedDOUBLER AT FS 589-613 S-19L-22L TEMP REPAIRED IAW BSC EO 601R-53-15724 AND BOMBARDIER REO 601R-53-61-3361. PERMANENTLY REPAIRED IAW BOMBARDIER REO 601R-53-61-4071.Jun 8, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100368Skin · damagedSECOND FASTENER BELOW STRINGER 13R AT FS 409+16 HAS LIGHTNING STRIKE DAMAGE TO COUNTERSINK MEASURING 0.500"L X 0.400"W X 0.003" DEEP. REPAIRED IAW REO 601R-53-00-419, REPAIR 13.Jun 8, 2011 · N8390A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201100370Floor Support · corrodedSERVICE DOOR THRESHOLD VERTICAL FLOOR SUPPORT FROM FS 319.00 TO FS 349 IS CORRODED. REPAIRED IAW SRM 51-42-21, 51-42-06, 51-42-13.Jun 7, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100364Structure · damagedFASTENER HOLE AT FS 409+32 IN S-13R LIGHTNING DAMAGE. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 12.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100363Window Frame · damagedCABIN WINDOW FRAME SCREW COUNTERSINK JUST AFT OF FS 409+48 LIGHTNING DAMAGE. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 11.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Main, StructureSDR REXA201100362Structure · damagedFASTENER AFT OF FS 424 AT S-10R HAS LIGHTNING STRIKE DAMAGE. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 7.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100361Structure · damagedFASTENER AFT OF FS 513 BETWEEN S-10R AND S-11R HAS LIGHTNING DAMAGE. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 6.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100360Structure · damagedFASTENER AFT OF FS 409+81 BETWEEN S-26L AND S-27 HAS LIGHTNING DAMAGE. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 1.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100359Structure · damagedONE FASTENER LOCATED AT FS 409+32 BETWEEN S-7L AND S-8L HAS LIGHTNING STRIKE DAMAGE ON OUTER PERIMETER OF COUNTERSINK 0.075"L X 0.050"W X 0.007" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 19.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100358Structure · damagedTHE SECOND FASTENER AFT OF FS 409+80 IN S-6L HAS LIGHTNING STRIKE DAMAGE ON COUNTERSINK 0.180"L X 0.070"W X 0.021" DEEP. REPAIRED IAW BOMBARDIER REO REO 601R-53-00-419 REPAIR 18.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100357Structure · damagedTHE THIRD FASTENER FWD OF FS 364.00 AT S-8L HAS LIGHTNING STRIKE DAMAGE AND AREA HAS BEEN PREVIOUSLY BLENDED 0.400" DIAMETER 0.005" DEPTH. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 16.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100356Structure · damagedFIRST FASTENER AFT OF FS 235 ON S-16R HAS LIGHTNING STRIKE DAMAGE ON FASTENER HEAD. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 14.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100355Structure · damagedTHE FIRST BELOW S-13R AT FS394 HAS LIGHTNING STRIKE DAMAGE AROUND THE OUTSIDE PERIMETER OF COUNTERSINK 0.325"L X 0.525"W X 0.004" MAX DEPTH. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 OP91.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100354Structure · damagedFOURTH FASTENER FWD OF FS 409+112 AT S-11R HAS LIGHTNING STRIKE DAMAGE TO COUNERSINK 0.125"L X 0.050"W X 0.013" MAX DEPTH. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 8.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100353Structure · damagedONE FASTENER LOCATED AT FS 439 BETWEEN S-5L AND S-6L HAS LIGHTNING STRIKE DAMAGE TO COUNTERSINK 0.050" DIAMETER X 0.013" MAX DEPTH. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 5.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100352Structure · damagedFOURTH FASTENER AFT OF FS 473 IN S-5L HAS LIGHTNING STRIKE DAMAGE TO COUNTERSINK .1"L X 0.05" X 0.010" MAX DEPTH. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 4.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100351Structure · damagedTHE FIRST FASTENER FWD OF FS 409+48 IN S-27 HAS LIGHTNING STRIKE DAMAGE AROUND ENTIRE PERIMETER OF COUNTERSINK AND DAMAGE TO FASTENER HOLE MAX DEPTH 0.009". REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 2.Jun 6, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100367Structure · damagedTHIRD FASTENER FWD OF FS 379 AT S-8L HAS LIGHTNING STRIKE DAMAGE TO COUNTERSINK. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 15.Jun 5, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100365Structure · damagedFASTENER BETWEEN FS 409+64 AND 409+80 IN S-12R HAS LIGHTNING STRIKE DAMAGE IN COUNTERSINK 0.400"L X 0.0450"W X 0.005" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-00-419 REPAIR 10.Jun 5, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100330Bulkhead · crackedPRESSURE BULKHEAD AT FS 202.75 LBL 23.75 CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-563 REV A TYPE 1 AND BSC SR 601R-53-0101A.May 30, 2011 · N8390A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100329Floor Support · crackedFS 280 BULKHEAD AFT FLOOR SUPPORT ANGLE CRACKED ON AFT SIDE UPPER RADIUS IN TWO PLACES (RBL 9 AND LBL 9). REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORPORATION EO 601R-53-0110.May 28, 2011 · N8390A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100328Bulkhead · corrodedFS 280 BULKHEAD LOWER WEB IS CORRODED FROM LBL 9 TO RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORPORATION EO 601R-53-0110.May 28, 2011 · N8390A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201000301Bracket · out of adjustGEAR DISAGREE. DEFERRED GEAR IAW MEL. FOUND PROXIMITY TARGET MOUNTING BRACKET OUT OF ADJUSTMENT, REPOSITIONED, OPS CHECK GOOD IAW AMM 32-61-05-400-804. THIS CLEARS DM 34876.Dec 15, 2010 · N8390A · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA201000255Seal · missingDURING ARRIVAL IN MILWAUKEE, WI (MKE), THE FLIGHT CREW REPORTED AN AIR NOISE IN THE FLIGHT DECK AREA. A CABIN PRESSURE FLUCUATION WAS ALSO REPORTED BUT NOT ABLE TO BE QUANTIFIED. UPON FURTHER INSPECTION, A 1.5 INCH PORTION OF THE SEAL BETWEEN THE MAIN WINDSHNov 10, 2010 · N8390A · Cndair CL6002B19 · Flight Compartment WindowsSDR REXA201000195Skin · dentedLEFT OUTBOARD FLAP VANE HAD A DENT IN THE VANE LEADING EDGE SKIN APPROXIMATELY 9 INCHES FROM THE INBOARD EDGE AT WS 181.5. THE DAMAGE MEASURES 1.6 INCHES LONG BY 0.9 INCH WIDE WITH A MAXIMUM DEPTH OF 0.095 INCH. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010Oct 11, 2010 · N8390A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA201000104Ecu · failedFLAPS FAIL CAUTION AT FL210 FLAPS AT 0 DEGREES, LANDING WITH 0 DEGREE FLAPS. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH(H)(6)(I), AMOC DATED MARCH 27, 2009, TR# 27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-052G. REAug 17, 2010 · N8390A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201000065Sensing Element · malfunctionedMLG OVERHEAT FAIL FOLLOWED BY MLG OVERHEAT WARNING. T/S WIRING PER FIM 26-10-00. REMOVED AND REPLACED RT WHEEL BIN HEAT SENSING ELEMENT IAW AMM 26-14-04. OPS CHECK GOOD. OK FOR SERVICE.May 4, 2010 · N8390A · Cndair CL6002B19 · Overheat DetectionSDR REXA200700063Carbon Seal · leakingCREW REPORTED A LAV SMOKE WARNING WHICH WAS CONFIRMED BY FLIGHT ATTENDANT. ENGINE WAS SHUT DOWN AT THE GATE AND MAINTENANCE WAS CALLED. MAINTENANCE TROUBLESHOT LAV SMOKE DETECTOR AND FOUND NO DISCREPANCIES. FURTHER INVESTIGATION LED TO A BOROSCOPE OF THE LTNov 11, 2007 · N8390A · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR REXA200600100Apu · leakingTHE AIRCRAFT WAS BOARDING PASSENGERS AT KXNA WHEN THE CABIN BEGAN TO FILL WITH OIL SMOKE. BOARDING WAS SUSPENDED AND ALL PASSENGERS WERE REMOVED FROM THE AIRCRAFT. CFR RESPONDED AS A PRECAUTION. NO EVIDENCE OF FIRE WAS NOTED, BUT THERE WAS A PUDDLE OF OIL UNov 2, 2006 · N8390A · Cndair CL6002B19 · APU Oil SystemSDR REX2005F00039Engine · failed(REF NR: 05-064) ON CLIMB OUT, AT ABOUT FL303, THERE WAS A LOUD BANG AND THE NR 2 ENGINE ITT SPIKED. THIS WAS FOLLOWED BY A LOSS OF N1 AND OIL PRESSURE. FLIGHT CREW FOLLOWED THE QRH PROCEDURES AND DECLARED AN EMERGENCY. THE PIC REQUESTED AND RECEIVED PERMMay 13, 2005 · N8390A · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR REXA02026Acm · malfunctionedLAVATORY EICAS SMOKE INDICATION IN FLIGHT. TROUBLESHOT PROBLEM TO THE RT AIR CYCLE MACHINE. DEFERRED RIGHT ACM IAW MEL.Dec 8, 2002 · N8390A · Cndair CL6002B19 · Cabin Cooling SystemSDR REXA02025Odor · detectedCREW RECEIVED EICAS TOILET SMOKE INDICATION, THERE WAS A SLIGHT SMOKY HAZE IN THE VICINITY OF THE LAVATORY AS WELL AS A STRONG SMELL OF BURNED PLASTIC. QRH FOLLOWED UNEVENTFUL UNSCHEDULED RETURN TO AIRPORT. RAN CABIN PACK, INSPECTED AND OPERATIONALLY CHECKEDDec 5, 2002 · N8390A · Cndair CL6002B19 · Air Distribution SystemSDR REXA02024Smoke Detector · false indicationCREW RECEIVED EICAS TOILET SMOKE INDICATION ALONG WITH VISIBLE SMOKE IN AFT CABIN AND LAVATORY QRH FOLLOWED UNEVENTFUL UNSCHEDULED RETURN TO AIRPORT. PERFORMED ENGINE RUNS AND OPERATIONAL CHECKS OF BLEED AIR SYSTEM WITH NO DEFECTS NOTED.Dec 4, 2002 · N8390A · Cndair CL6002B19 · Smoke DetectionSDR REXA01006Pin · out of positionEN ROUTE TO MONTEREY, MEXICO THE FLIGHT CREW DISCOVERED THAT THE THRUST LEVER OF THE LEFT ENGIEN COULD NOT BE REDUCED BELOW 97 PERCENT N1. THE FLIGHT CREW CONTACTED MAINTENANCE CONTROL FOR POSSIBLE RESOLUTION. AFTER CONFERRING WITH MAINTENANCE ENGINEERING, IApr 16, 2001 · N8390A · Cndair CL6002B19 · Engine Cowling SystemSDR 20001026SH016Handle · brokenAFTER TAKEOFF UPON A GEAR RETRACTION, THE LANDING GEAR HANDLE SHAFT BROKE. AIRCRAFT RETURNED TO BASE AND LANDED SUCCESSFULLY. REDESIGN OF LANDING GEAR HANDLE WAS DONE AND AWAITING APPROVAL FROM CANADAIR. (X)Aug 11, 2000 · N8390A · Cndair CL6002B19 · Landing Gear SelectorSDR REXA00009Handle · defectiveUPON TAKEOFF OUT OF MEMPHIS, GEAR WAS SELECTED UP AND THE GEAR DID NOT RETRACT. AIRCRAFT RETURNED TO MEMPHIS WITHOUT INCIDENT. FOUND LANDING GEAR CONTROL HANDLE THAT WAS INSTALLED ON 8/11/2000 WAS DEFECTIVE. REPLACED LANDING GEAR CONTROL HANEL PERFORMED GEAAug 11, 2000 · N8390A · Cndair CL6002B19 · Landing Gear SelectorSDR REXA00008Handle · brokenLANDING GEAR CONTROL HANDLE BROKE OFF IN PILOT''S HAND WHILE ATTEMPTING TO RETRACT GEAR. GEAR DID NOT RETRACT. REMOVED AND REPLACED GEAR HANDLE ASSEMBLY. (M)Aug 11, 2000 · N8390A · Cndair CL6002B19 · Landing Gear Selector
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