N842EX

Service difficulty reports not matched to an aircraft · 34

They name N842EX, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N842EX' AND registry_match IS NULL
  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 V0XR201208230001Attach Angle · crackedRT WING ROOT FAIRING ATTACHMENT ANGLE CRACKED. R & R RT WING ROOT FAIRING ATTACHMENT ANGLE.Aug 23, 2012 · N842EX · Dhav DHC8106 · Fuselage Main, Attach FittingsSDR 2012FA0000548Angle · crackedRIGHT WING ROOT FAIRING ATTACHMENT ANGLE CRACKED. R & R RIGHT WING ROOT FAIRING ATTACHMENT ANGLE.Aug 6, 2012 · N842EX · Dhav DHC8102 · Wing, Attach FittingsSDR V0XR2012042700012Skin · dentedTWO DENTS ARE OUT OF LIMITS ON FLIGHT DECK ESCAPE HATCH. DENT NR 2 MEASURES 2.6 X 2.6 X 0.050" DEEP. DENT NR 1 MEASURES 2.7 X 2.8 X 0.050" DEEP. BOTH DENTS ARE WITHIN LIMITS OF REPAIR DWG 8-52-1218. NDT SHOWS NO CRACKS INDICATED IAW DASH 8-100 NDTM PART 6.Apr 27, 2012 · N842EX · Dhav DHC8106 · Emergency ExitsSDR V0XR2012042700011Plate · corrodedLADDER PLATE FOR PANEL 624BT HAS PITTING. REPAIRED LADDER PLATE BETWEEN STATIONS YW=261-333 RT WING IAW REPAIR DWG 8-57-633.Apr 27, 2012 · N842EX · Dhav DHC8106 · Wing Miscellaneous StructureSDR V0XR2012042700010Access Panel · corrodedFUEL PANEL 624CT IS PITTED. REMOVED PITTED CORROSION ON FUEL PANEL 624CT IAW REPAIR DWG 8-57-320.Apr 27, 2012 · N842EX · Dhav DHC8106 · Wing, Plate/SkinSDR V0XR2012042700009Plate · corrodedLADDER PLATE FOR PANEL 624AT HAS PITTING. REPAIRED LADDER PLATE BETWEEN STATIONS YW=171.2-261.0 IAW REPAIR DWG 8-57-611.Apr 27, 2012 · N842EX · Dhav DHC8106 · Wing Miscellaneous StructureSDR V0XR2012042700008Access Panel · corrodedFUEL PANEL 624BT IS PITTED, REMOVED PITTED CORROSION ON PANEL 624BT IAW REPAIR DWG 8-57-320.Apr 27, 2012 · N842EX · Dhav DHC8106 · Wing, Plate/SkinSDR V0XR2012042700007Plate · corrodedLADDER PLATE FOR PANEL 624CT HAS PITTING. REPAIRED LADDER PLATE BETWEEN STATIONS YW=333-423 IAW REPAIR DWG 8-57-984.Apr 27, 2012 · N842EX · Dhav DHC8106 · Wing Miscellaneous StructureSDR V0XR2012042700006Skin · dentedDENT ON LT SIDE OF OF RT NACELLE AT XN=72.0 AND ZN=1.0. DENT ON COWL ASSY IS LOCATED 6.25" FROM TOP EDGE OF DOOR AND 8.25" FROM FORWARD EDGE. DENT IS MEASURED AT 0.015 DEEP AND 0.700 DIAMETER AND FOUND TO BE IN LIMITS WITH SRM 54-00-16 AND REPAIR DWG 8-71-885Apr 27, 2012 · N842EX · Dhav DHC8106 · Nacelle/Pylon, Plate/SkinSDR V0XR2012042700005Skin · misrepairedRT ELEVATOR AT YH=129.7 MISREPAIRED. REPAIRED IAW REPAIR DWG 8-55-2360.Apr 27, 2012 · N842EX · Dhav DHC8106 · Elevator, Plate/SkinSDR V0XR2012042700004Bearing Race · damagedHORIZONTAL CENTER HINGE POINT BUSHING RACE DAMAGED. REPAIRED HORIZONTAL CENTER HINGE POINT BUSHING RACE IAW REPAIR DWG 8-55-2361, REV 2.Apr 27, 2012 · N842EX · Dhav DHC8106 · Horizontal Stabilizer StructureSDR V0XR2012042700003Skin · misrepairedRT UPPER ELEVATOR SKIN AT YH=54.0, XH=20.0 MISREPAIRED. REPAIRED IAW REPAIR DWG 8-55-2359.Apr 27, 2012 · N842EX · Dhav DHC8106 · Elevator, Plate/SkinSDR V0XR2012042700002Bearing Race · damagedDAMAGE ON LT ELEVATOR INBOARD BEARING RACE. REMOVED DAMAGE ON LT INBD BEARING RACE, ALODINED, PRIMED AND PAINTED IAW REPAIR DWG 8-55-2357, SRM 51-40-11, 51-20-26, AND 51-20-16.Apr 27, 2012 · N842EX · Dhav DHC8106 · Elevator StructureSDR V0XR2012042700001Strap · corrodedRIGHT WING ROOT FAIRING ATTACH STRAP HAS CORROSION EXCEEDING ALLOWABLE LIMITS. INSTALLED 85350774-002 STRAP IAW SRM 51-40-07 AND 51-42-05.Apr 27, 2012 · N842EX · Dhav DHC8106 · Fuselage Miscellaneous StructureSDR V0XR2012042600007Skin · dentedDENT AT X=291 BETWEEN STRINGER 11 AND 12. REPAIRED DENT IAW REPAIR DWG 8-53-12089 ISSUE 2. EDDY CURRENT GOOD, NO DEFECT. ULTRASONIC BOND CHECK GOOD, NO DEFECT.Apr 26, 2012 · N842EX · Dhav DHC8106 · Fuselage Main, Plate/SkinSDR V0XR2012042600006Stringer · corrodedSTRINGER 30P AT STATION 182 FORWARD CORRODED. CUT OUT CORRODED SECTION OF STRINGER 30P AND SPLICED IN NEW SECTION FROM FRAME 187-151 IAW SRM 53-10-21 AND 51-10-00.Apr 26, 2012 · N842EX · Dhav DHC8106 · Fuselage Main, Longeron/StringerSDR V0XR2012042600005Skin · dentedDENT IN SKIN AT X=161 BETWEEN STRINGER 31 AND 32R. REPAIRED DENT WITH REPAIR DOUBLER IAW REPAIR DWG 8-53-12086.Apr 26, 2012 · N842EX · Dhav DHC8106 · Fuselage Main, Plate/SkinSDR V0XR2012042600004Skin · dentedDENT IN SKIN AT BS 319, S26 - 27R. DENT FOUND TO BE 0.040 DEEP AND 4.0" LONG, ASPECT RATIO 100. FABRICATED REPAIR DOUBLER AND INSTALLED IAW REPAIR DWG 8-53-12081.Apr 26, 2012 · N842EX · Dhav DHC8106 · Fuselage Main, Plate/SkinSDR V0XR2012042600003Skin · dentedDENT IN SKIN AT BS 304, S25R UNDER WING ICE SHIELD. DENT MEASURES 0.600 DIAMETER, 0.004 DEEP ABOVE STRINGER 25S AND IS WITHIN LIMITS IAW RD 8-53-1210. NDT SHOWS NO CRACKS INDICATED IAW NDTM PART 6.Apr 26, 2012 · N842EX · Dhav DHC8106 · Fuselage Main, Plate/SkinSDR V0XR2012042600002Skin · dentedDENT IN SKIN AT BS 298, S24R UNDER ICE SHIELD AREA. DENT MEASURES 0.600 DIA, 0.009 DEEP, .5" BELOW STRINGER 24S. DENT IS WITHIN LIMITS OF RD 8-53-1210. NDT INDICATES NO CRACKS IAW NDTM PT 6.Apr 26, 2012 · N842EX · Dhav DHC8106 · Fuselage Main, Plate/SkinSDR V0XR201203220001Rib · crackedCRACKED RIB AT YH 6.00 ON LT ELEVATOR. R & R CRACKED RIB AT YH 6.00 ON LT ELEVATOR IAW DWG 85520268.Mar 22, 2012 · N842EX · Dhav DHC8102 · Elevator, Spar/RibSDR V0XR2011102000002Angle · corrodedCORROSION FOUND ON CLIP ANGLES THAT TIE FRAME X = 488.5 TO STRINGER 23L, FWD AND AFT SIDE. AFTER FURTHER INVESTIGATION FOUND CLIP ANGLES THAT TIE FRAME X = 488.5 TO STRINGER 23L FWD AND AFT SIDE TO BE OUT OF LIMITS. FABRICATED NEW ANGLES OF 0.032 IN 2024-T3,Oct 20, 2011 · N842EX · Dhav DHC8102 · Fuselage Miscellaneous StructureSDR V0XR201110200001Doubler · corrodedAIRSTAIR DOUBLER AT THE FWD SIDE OF TOP STEP IS CORRODED. R & R DOUBLER IAW AMM 52-10-00-02 AND SRM 51-10-00.Oct 20, 2011 · N842EX · Dhav DHC8102 · Passenger/Crew DoorsSDR PCAA0309111Wire · brokenWHILE PERFORMING MAINTENANCE POSTFLIGHT INSPECTION, ONE FLOOR LEVEL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. A BROKEN WIRE WAS FOUND AND REPAIRED. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE.Sep 17, 2003 · N842EX · Dhav DHC8102 · Light System WiringSDR PCAA0309106Wire · looseDURING ROUTINE MAINTENANCE VISIT THE EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. AFTER INSPECTION A BROKEN WIRE WAS DISCOVERED. WIRE WAS RESECURED, AND THE OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.Sep 4, 2003 · N842EX · Dhav DHC8102 · Light System WiringSDR PCAA0302044Spring · weakROC-LGA - FLIGHT 3905 CREW REPORTED THAT AFTER LANDING GEAR WAS SELECTED DOWN, GEAR HORN SOUNDED, AND NOSE GEAR INDICATED UNSAFE. ALTERNATE EXTENSION INDICATOR SHOWED UNSAFE NOSE GEAR. ALTERNATE EXTENSION PROCEDURE USED, AND NOSE GEAR INDICATED DOWN AND LOCKFeb 19, 2003 · N842EX · Dhav DHC8102 · Landing Gear Retraction/Extension SystemSDR PCAA0302039Bulb · looseDURING ROUTINE MAINTENANCE VISIT 3RD RED FLOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. CONNECTOR PIN WAS RESOLDERED, AND BULB REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Feb 7, 2003 · N842EX · Dhav DHC8102 · Emergency LightingSDR PCAA0302037Wire · loosePIT-FLIGHT 3716 CREW REPORTED EMERGENCY LIGHTS FLICKERED ON AND OFF IN FLIGHT. MAINTENANCE FOUND A WIRE STICKING UP FROM LIGHT STRIP. WIRE WAS RESECURED. AIRCRAFT RETURNED TO SERVICE.Feb 7, 2003 · N842EX · Dhav DHC8102 · Light System WiringSDR PCAA0208093Engine · leakingSCE-PIT FLIGHT#3825. CREW REPORTED LOSS OF OIL PRESSURE ON #2 ENGINE. ENGINE SHUT DOWN AND EMERGENCY DECLARED. MAINTENANCE FOUND A CUT O RING ON TRANSFER TUBE BETWEEN OIL PRESSURE REGULATOR AND MAIN OIL FILTER. O RING REPLACED. MAIN AND SCAVANGE OIL FILTERS REAug 13, 2002 · N842EX · Dhav DHC8102 · Engine Oil PressureSDR PCAA0206066Socket · inoperativeDURING ROUTINE MAINTENANCE VISIT FORWARD RED EMERGENCY AISLE TRACK LIGHT FOUND INOPERATIVE. SOCKET PN 10-1307-5 REPLACED AND RELAMPED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Jun 15, 2002 · N842EX · Dhav DHC8102 · Emergency LightingSDR PCAA0111141Wire · damagedDURING ROUTINE MAINTENANCE VISIT ONE SECTION OF EMERGENCY PATHWAY LIGHTS FOUND INOPERATIVE. LOOSE CONNECTION FOUND AND WIRING REPAIRED. OPERATIONAL CHECK GOOD . AIRCRAFT RETURNED TO SERVICE.Nov 24, 2001 · N842EX · Dhav DHC8102 · Light System WiringSDR PCAA0110125Window · crackedLGA- FLIGHT# 3969. CREW REPORTED CAPTAINS SIDE WINDOW CRACKED. MAINTENANCE REPLACED CAPTAINS SIDE WINDOW IN ACCORDANCE WITH MAINTENANCE MANUAL CHAPTER 56-10-16. AIRCRAFT RETURNED TO SERVICE.Oct 21, 2001 · N842EX · Dhav DHC8102 · Flight Compartment WindowsSDR PCAA0105037Actuator · brokenMDT- FLIGHT 3716. CREW REPORTED RIGHT GEAR INTRANSIT LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION, OK DURING EXTENSION. MAINTENANCE FOUND SPRING ON UPLOCK ACTUATOR BROKEN. THE RIGHT GEAR UPLOCK ACTUATOR WAS REMOVED AND REPLACED IN ACCORDANCE WITH DASH 8May 4, 2001 · N842EX · Dhav DHC8102 · Landing Gear Retraction/Extension SystemSDR PCAA0008047Structure · crackedMDT - DURING A SPOT INSPECTION, THE REAR FUSELAGE STRUCTURAL MEMBERS AT FRAME 4 STRINGER 4 BOTH LEFT AND RIGHT WERE BOTH FOUND CRACKED. REPAIRS WERE MADE IAW RD8-55-199 AND RD8-55-961. THE AIRCRAFT WAS RETURNED TO SERVICE.Jul 30, 2000 · N842EX · Dhav DHC8102 · Fuselage Main, Structure
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