N17984

Service difficulty reports · 72

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 = 'N17984' 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 ASOA201909063045Light · inoperativeTHE CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHT STRIP @ ROW 10 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROW 10.Sep 6, 2019 · N17984 · Emb EMB145LR · Emergency LightingSDR ASOA201905077042Trunnion · crackedRT AFT MLG TRUNNION CRACKED. REMOVED AND REPLACED RT AFT MLG TRUNNION. AIRCRAFT STILL IN C CHECK.May 4, 2019 · N17984 · Emb EMB145LR · Wing, Landing Gear Attach FittingsSDR ASOA201905037041Structure · gougedTYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE APU FIREWALL MOUNTING STRUCTURE AT THE 06:00 POSITION WITH A GOUGE AND POSSIBLE CRACK. MAINTENANCE BLENDED OUT THE DAMAGE AND NO CRACK FOUND, THEN INSTALL A INTERNAL AND EXTERNAL DOUBLER WITH SHIMS FOR THE APU COMay 3, 2019 · N17984 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA201905167047Skin · crackedEXTERIOR SKIN CRACKED AT FRAME 75 STRINGER 2L. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLERS. AIRCRAFT WAS IN C CHECK AND IS NOW RELEASED AND RETURNED TO SERVICE.Apr 29, 2019 · N17984 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA201905017040Stringer · crackedSTRINGER 2L CRACKED AT FRAME 75. CUT OUT DAMAGED AREA AND INSTALLED J-SECTION PER ETD2019-145-055731. AIRCRAFT STILL IN C CHECK.Apr 29, 2019 · N17984 · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR ASOA201904237037Skin · crackedA/C IS IN C-CHECK WHEN INSPECTION FOUND THE EXTERIOR SKIN CRACKED AT FRAME 75,STRINGER 2R. MAINTENANCE REPAIRED THE SKIN AT FRAME 75 IAW EMB SRM 53-31-01 REF. FIGURE #219-FUR 53-00-016-72. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Apr 23, 2019 · N17984 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA201808231054Engine · odorTHE CREW REPORTED A STRONG OIL ODOR FROM THE PACKS AFTER TAKEOFF. MAINTNENACE INSPECTED AND REPLACED THE NR 1 ENGINE IAW TASK CARD 6271001. OPS CHECKED GOOD.Aug 21, 2018 · N17984 · Emb EMB145LR · Engine (Turbine/Turboprop)SDR ASOA201705043132Channel · corrodedSERVICE DOOR LOWER CHANNEL CORRODED AROUND ANCHOR NUTS. SERVICE DOOR LOWER CHANNEL REPLACED IAW SRM 51-40-02.May 4, 2017 · N17984 · Emb EMB145LR · Service DoorsSDR ASOA201705033130Beam · corrodedCARGO DOOR SURROUND STRUCTURE, LOWER BEAM FOUND CORRODED. OUT OF TOLERANCE. THE LOWER BEAM WAS REPLACED IAW SRM 51-40-02.May 3, 2017 · N17984 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA201705033129Door Frame · corrodedCORROSION ON PAX DOOR LOWER FRAME AROUND NUT PLATE HOLES. REPAIRED IAW ETD 2017-145-035391.May 3, 2017 · N17984 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA201705013126Channel · crackedRIGHT CHANNEL CRACKED ON FORWARD PRESSURE BULKHEAD IN NOSE WHEEL WELL. THE CHANNEL WAS REPLACED IAW SRM 51-40-02.May 1, 2017 · N17984 · Emb EMB145LR · Fuselage Main, BulkheadSDR ASOA201705013125Support · corrodedSURFACE CORROSION FOUND ON WASTE DRAIN VALVE SUPPORT. WASTE DRAIN VALVE SUPPORT REPLACED IAW SRM 51-40-02.May 1, 2017 · N17984 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA201705013124Floorbeam · corrodedFLOORBEAM CORRODED UNDER GUSSET AROUND ANCHOR NUT. THE FLOORBEAM WAS REPAIRED IAW SRM 53-24-10, PAR 3, FIG 202, SHEET 3.May 1, 2017 · N17984 · Emb EMB145LR · Fuselage Main, Floor BeamSDR ASOA201704283123Angle · crackedCOCKPIT LEFT FRAME 10, UPPER ANGLE CRACKED. ANGLE REPLACED IAW SRM 51-40-02.Apr 28, 2017 · N17984 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA201704283122Shear Tie · corrodedCARGO DOOR SURROUND STRUCTURE SHEAR TIE CORRODED AT FRAME 65. THE SHEAR TIE WAS REPAIRED IAW SRM 53-31-04, STEP 4F.Apr 28, 2017 · N17984 · Emb EMB145LR · Fuselage Internal Mounting StructureSDR ASOA201704203094Crossbeam · crackedNLG UPLOCK AFT CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.Apr 20, 2017 · N17984 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA201704203093Crossbeam · crackedNLG UPLOCK FORWARD CROSSBEAM CRACKED. FORWARD CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.Apr 20, 2017 · N17984 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA20151021083HFirewall · crackedDURING MAINTENANCE INSPECTION, A CRACK WAS FOUND IN THE APU FIREWALL AT APPROXIMATELY THE 2 O'CLOCK POSITION NEAR AN EXISTING DOUBLER. MAINTENANCE REMOVED THE EXISTING DOUBLER AND PERFORMED A COMBINATION REPAIR IAW SRM 53-32-13 AND THE ACFT WAS APPROVED FOR ROct 21, 2015 · N17984 · Emb EMB145LR · APU Cowling/ContainmentSDR ASOA20150421024CInverter · inoperativeTHE CREW REPORTED EMERGENCY LIGHTS ON FLOOR BETWEEN ROWS 2-8 AND EXIT SIGN BY MAIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.Apr 21, 2015 · N17984 · Emb EMB145LR · Emergency LightingSDR ASOA20130901102Computer · shortedELECTRICAL ODOR REPORTED IN COCKPIT WITH TERRAIN MESSAGE ON EICAS. MX R & R THE EGPWS COMPUTER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Sep 1, 2013 · N17984 · Emb EMB145LR · Independent Position Determining SystemSDR ASOA20130731086Bracket · unsecureMX REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN. MX SECURED THE MAIN DOOR HANDLE BRACKET. OPS CHECK OF THE MAIN DOOR SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 31, 2013 · N17984 · Emb EMB145LR · Passenger/Crew DoorsSDR ASOA20130730085Ground Stud · damagedMX REPORTED THE EMERGENCY LIGHTS CAME ON WITH THE CEILING AND SIDEWALL LIGHTS ACTIVATION AND LIGHTS IN ARM POSITION. MX FOUND GROUND STUD GS8008DC TO HAVE BAD GROUND CONNECTION. CLEANED THE SURFACE AND OPS CHECK OF THE EMERGENCY LIGHTS SUCCESSFUL. ACFT WAS Jul 30, 2013 · N17984 · Emb EMB145LR · Light System WiringSDR ASOA20130726082Battery Pack · dischargedPILOT REPORTED EMERGENCY LIGHTS INOPERATIVE. MX R & R THE NR 3 AND NR 4 EMERGENCY LIGHT SYS BATTERY PACKS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 26, 2013 · N17984 · Emb EMB145LR · Emergency LightingSDR ASOA20121230124Sensor · faultyFLIGHT DIVERTED, CREW REPORTED NR 1 ENGINE OIL PRESSURE IN FLIGHT FLUCTUATED BETWEEN 98-151 PSI. CREW SHUTDOWN ENGINE IN FLIGHT. MX R & R NR1 ENGINE OIL PRESSURE/TEMP SENSOR WITH OPS AND LEAK CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 30, 2012 · N17984 · Emb EMB145LR · Engine Oil PressureSDR ASOA20121015150Inverter · inoperativeEMERGENCY LIGHT FLOOR STRIPS NR 2 & 3 INOPERATIVE. R & R NR 3 INVERTER. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE.Oct 11, 2012 · N17984 · Emb EMB145LR · Emergency LightingSDR ASOA20120918077Inverter · inoperativeDURING ROUTINE INSPECTION, MX THE FORWARD 3 EMERGENCY AILSE PATH LIGHT STRIPS WERE INOPERATIVE. MX REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.Sep 18, 2012 · N17984 · Emb EMB145 · Emergency LightingSDR ASOA20120504043Fan · odorCREW REPORTED AN ELECTRICAL ODOR. INSPECTED AVIONICS BAY AND FOUND RECIRCULATION FANS INOPERATIVE. THE SYS WAS RESET AND OPS CHECKED GOOD. NO ELECTRICAL ODOR WAS FOUND.May 4, 2012 · N17984 · Emb EMB145LR · Air Distribution FanSDR C2XA11IA160Light · inoperativeIAH - DURING MAINTENANCE INSPECTION THE AFT AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATOINALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jul 25, 2011 · N17984 · Emb EMB145LR · Emergency LightingSDR C2XA11CL148Inverter · faultyDURING ROUTINE MAINTENANCE THE OVERHEAD EMERGENCY EXIT SIGN AT THE OVERWING ESCAPE HATCH WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.Jun 20, 2011 · N17984 · Emb EMB145LR · Emergency LightingSDR C2XA11SH073Fitting · looseSHV - DURING C-CHECK VERTICAL STAB SPAR 1 ATTACHMENT AT FRAME 75 SHOWS SIGNS OF MOVEMENT AT O/B AREAS (INSIDE AFT AVIONICS BAY). MAINTENANCE PERFORMED REPAIR OF FRAME 75 FITTING IAW EMB-145 EC5310-01317 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 26, 2011 · N17984 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA11SH072Structure · damagedSHV - DURING C-CHECK CARGO DOOR INNER STRUCTURE BELOW FWD PULLEY HAS MISS DRILL DAMAGE. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR INNER STRUCTURE AND RESTORED TO ORIGINAL FINISH IAW EMB-145 EC5230-01208 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVMar 26, 2011 · N17984 · Emb EMB145LR · Cargo/Baggage DoorsSDR C2XA11SH071Hinge · gougedSHV - DURING C-CHECK RUDDER II LOWER CENTER HINGE HAS A GOUGE. MAINTENANCE REMOVED AND REPLACED RUDDER II LOWER CENTER HINGE IAW EC5540-01028 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 26, 2011 · N17984 · Emb EMB145LR · Rudder StructureSDR C2XA11SH070Door Frame · corrodedSHV - DURING C-CHECK SERVICE DOOR AFT CUTOUT HAS CORROSION AT LOWER NUT PLATE HOLE. REPAIRED FRAME IAW EC5310-01548. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 23, 2011 · N17984 · Emb EMB145LR · Fuselage Main, StructureSDR C2XA11SH069Frame · corrodedSHV - DURING C-CHECK FRAME 65 HAS AREAS OF CORROSION. REPAIRED FRAME IAW EC5310-01505. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 23, 2011 · N17984 · Emb EMB145LR · Fuselage Main, FrameSDR C2XA10CL169Computer · faultyEWR FLT 2940 THE CREW REPORTED GLIDESLOPE ISSUES GOING INTO DTW. REPORTED A 1/2 DOT DIFFERENCE BETWEEN GLIDESLOPE INDICATIONS DURING CAT II GS COMPARATIVE. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR Nov 13, 2010 · N17984 · Emb EMB145LR · Integrated Flight SystemSDR C2XA09IA272Sealant · odorIAH - FLIGHT 2886, THE CREW REPORTED A BURNING SMELL WHILE TAXIING IN AND WAS STRONGER IN INTENSITY AS THE PARKING BRAKE WAS SET, AND WAS FOUND TO BE STRONGER IN THE MAIN CABIN DOOR / GALLEY AREA. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SMELL TO BE COct 27, 2009 · N17984 · Emb EMB145LR · Pitot/Static SystemSDR C2XA09SH070Door Frame · corrodedSHV - DURING C-CHECK CARGO DOOR CUTOUT LWR BEAM AREA CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Mar 1, 2009 · N17984 · Emb EMB145 · Fuselage Main, StructureSDR C2XA07CL093Uplock · faultyCLE FLIGHT 2251 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WARNING IN FLIGHT. THE AIRCRAFT DIVERTED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT LANDING GEAR UPLOCK BOX. OPERATIONAL CHECKS WERE GOOD.Nov 3, 2007 · N17984 · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR C2XA07RI069Light · inoperativeRIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND CEILING EMERGENCY LIGHTS AT ROW 3 AND ROW 14 INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULBS IAW EMB145 AMM 33-50-08 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.Aug 16, 2007 · N17984 · Emb EMB145LR · Emergency LightingSDR C2XA07IA131Proximity Switch · inoperativeIAH - FLIGHT 2598, THE CREW REPORTED A LOUD NOISE AND VIBRATION IN THE NOSE ARE DURING CRUISE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX PROXIMITY SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND Jun 5, 2007 · N17984 · Emb EMB145LR · Landing Gear Position and WarningSDR C2XA07IA120Brake Assy · malfunctionedIAH - FLIGHT 2528, THE CREW REPORTED A -BRK OUTBD- MESSAGE ON EICAS ON FINAL APPROACH, AND THAT THE OUTBOARD BRAKES DID NOT WORK ON ROLLOUT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE BRAKES WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROMay 18, 2007 · N17984 · Emb EMB145LR · Landing Gear Brake SystemSDR C2A07SH028Floor Support · corrodedSHV - DURING C-CHECK CORROSION ON CENTER OMEGA BEAM FROM FR 20 TO 23. MX REMOVED AND REPLACED CENTER OMEGA BEAM FROM FR 18-23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.May 13, 2007 · N17984 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA06CL063Proximity Switch · faultyCLE FLIGHT 3245 THE CREW REPORTED LOUD NOISE FROM NOSE GEAR AREA DURING CLIMBOUT ABOVE 1700 AND DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS WOULD NOT RETRACT. THE NLG DOOR SEQUENCE PROXIMITY SWITCH WAS REPLACED. OPERATIONAL CHECKS WEJun 27, 2006 · N17984 · Emb EMB145LR · Landing Gear Position and WarningSDR C2XA05RI017Wire Harness · burnedFLT 2969 - RIC - PRE-FLIGHT - DURING PRE-FLIGHT INSPECTION, SIDE WALL LIGHT AT SEAT 2A WAS SMOKING. RIC MAINTANACE REMOVED AND REPLACED LAMP HARNESS ASSY AND PERFORMED OPERATIONAL TESTS. OPS TEST GOOD. ACFT WAS APPROVED TO RETURNED TO SERVICE.Aug 8, 2005 · N17984 · Emb EMB145LR · Light System WiringSDR C2XA05SH041Floor Support · corrodedDURING C CHECK, PREVIOUS REPAIR TO LT OMEGA BEAM AT FS 20 WAS FOUND TO BE CORRODED. MX REMOVED DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-40-02, EC5320-01140 AND EC 5320-01137. ACFT APPROVED FOR RETURN TO SERVICE.May 23, 2005 · N17984 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA05SH042Floor Support · corrodedSHV - DURING C-CHECK THE RT OMEGA BEAM NUT PLATE IS CORRODED JUST AFT OF FRAME 23. MAINTENANCE INSTALLED HAT BEAM REPAIR ON RT OMEGA BEAM AT NUT PLATE HOLE AFT OF FR 23 IAW EMB SRM 53-21-10 FIG 206. INSTALLED NUT PLATE IAW EC 5320-01137. THE AIRCRAFT WAS APMay 23, 2005 · N17984 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA05RI001Light · burned outRIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT FLOOR STRIP, BY SEAT 6A, INOP. MAINTENANCE REMOVED AND REPLACED STRIP. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. THE ACFT WAS APPROVED TO RETURN TO SERVICE.Jan 13, 2005 · N17984 · Emb EMB145LR · Emergency LightingSDR C2XA04BT091Odor · detectedCREW REPORTED, (STRONG FUEL ODOR IN AIRCRAFT WHILE APU IS RUNNING.) MAINTENANCE TROUBLESHOT NO DEFECTS FOUND AND PLACED THE AIRCRAFT ON MEL FOR FURTHER FOLLOWUP. STL MAINTENANCE OPS. CHECKED THE APU WITH BOTH PACKS NR 1 AND NR 2 RUNNING FOR 30 MINUTES, NO Aug 15, 2004 · N17984 · Emb EMB145LR · Air Distribution SystemSDR C2XA03TY073Angle · corrodedDURING A SCHEDULED INSPECTION THE LOWER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE LOWER RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE AT COMPLEMay 20, 2003 · N17984 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA03TY072Angle · corrodedDURING A SCHEDULED INSPECTION THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE AT CMay 20, 2003 · N17984 · Emb EMB145LR · Fuselage Miscellaneous Structure
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