N430QX

Service difficulty reports · 213

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 = 'N430QX' 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 QXEA2014030400190Web · corrodedAFT CARGO BAY FLOOR WEB CORRODED. BLENDED IAW SRM 53-40-43-02-01. PERFORMED FPI OF BLENDED AREA IAW NDTM 51-00-01, NO DEFECTS NOTED. BLENDS FOUND TO BE WITHIN LIMITS IAW SRM 53-40-43-02-01. PERFORMED ECI ON BLENDED AREA, NO CRACKS FOUND AT THIS TIME IAW NDTFeb 28, 2014 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2014030400171Fitting · corrodedCORROSION FOUND UNDER FWD PAX DOOR LOWER AFT CORNER FITTING. BLENDED AFFECTED AREA IAW SRM 53-00-00-02-01. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00-02-01. EDDY CURRENT INSPECTION FOR SURFACE CRACKS PERFORMED IAW NTM PART 6 51-00-02. NO CRACKS NOTED.Feb 28, 2014 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2014030400191Threshold · corrodedTHRESHOLD MEMBER CORRODED BEYOND LIMITS. REMOVED THRESHOLD MEMBER IAW SRM 51-42-45-02-01 AND 51-42-05-02-01. INSTALLED NEW THRESHOLD IAW SRM 51-42-05-02-01.Feb 26, 2014 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2014030400172Bracket · corrodedBRACKET CORRODED INBD HINGE SHAFT FWD OF MACHINED WEB. REMOVED ANGLE IAW SRM 51-42-05-02-01. DRILLED NEW BRACKET IAW SRM 51-40-07-02-01. INSTALLED BRACKET IAW SRM 51-42-05-02-01.Feb 26, 2014 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2014030300168Support Bracket · corrodedCORROSION FOUND UNDER THE FWD PAX DOOR HINGE SHAFT ON A SUPPORT BRACKET BS 26.900 JUST FWD OF THE MACHINED WEB. REMOVED BRACKET IAW SRM 51-42-05-02-01. DRILLED NEW BRACKET IAW SRM 51-40-07-02-01. INSTALLED NEW BRACKET IAW SRM 51-42-05-02-01 AND 51-42-45-02-0Feb 26, 2014 · N430QX · Bombdr DHC8402 · Fuselage Main, Attach FittingsSDR QXEA2014030300167Support Angle · corrodedFWD PAX DOOR SUPPORT ANGLE AFT OF MACHINED WEB IS CORRODED. REMOVED ANGLE IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. DRILLED UP NEW ANGLE IAW SRM 51-40-07-02-01. INSTALLED NEW ANGLE IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. PRIMED RIVETS IAW SRM 51-42-05-0Feb 26, 2014 · N430QX · Bombdr DHC8402 · Passenger/Crew DoorsSDR QXEA2014030300166Support Bracket · corrodedCORROSION FOUND UNDER THE FWD PAX DOOR HINGE SHAFT ON A SUPPORT BRACKET STA 26.400 JUST AFT OF AFT MACHINED WEB. REMOVED LOWER ANGLE JUST AFT OF AFT MACHINED WEB BECAUSE OF EXCESSIVE CORROSION IAW SRM 51-42-05-02-01. DRILLED UP BRACKET IAW SRM 51-40-07-02-01.Feb 26, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Door HingeSDR QXEA2014030300162Skin · corrodedWING PANEL 524FT HAS SEVERAL AREAS OF SUSPECTED CORROSION. BLENDED OUT CORROSION IAW SRM 51-20-00-00-02. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-35-02-02.Feb 26, 2014 · N430QX · Bombdr DHC8402 · Wing, Plate/SkinSDR QXEA2014030400174Beam · corrodedFOUND LOWER SILL BEAM AT EMERGENCY EXIT CORRODED. REMOVED SILL BEAM IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. INSTALLED SILL BEAM IAW SRM 51-42-05-02-01 AND 51-42-45-02-01.Feb 24, 2014 · N430QX · Bombdr DHC8402 · Fuselage Main, StructureSDR QXEA2014030400173Angle · corrodedAFT CARGO FLOOR SHEAR WEB ANGLE HAS SUSPECTED CORROSION. BLENDED ANGLE IAW SRM 53-40-15-02-01. FOUND TO BE WITHIN LIMITS IAW SRM 53-40-15-02-01. BLENDED AREA ALODINED IAW SRM 51-21-10-02-01, PRIMED IAW SRM 51-25-10-02-01 AND PAINTED IAW SRM 51-25-15-02-01. Feb 21, 2014 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2014030300165Channel · corrodedFWD PAX DOOR THRESHOLD CHANNEL CORRODED BEYOND LIMITS. REMOVED THRESHOLD CHANNEL IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. DRILLED NEW CHANNEL IAW SRM 51-40-07-02-01. INSTALLED CHANNEL IAW SRM 51-42-05-02-01.Feb 21, 2014 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2014030300163Panel · corrodedWING SKIN MATING SURFACE UNDER PANEL 524CT HAS SEVERAL AREAS OF CORROSION. BLENDED CORROSION IAW SRM 57-20-35-02-02. PERFORMED ECI ON BLENDED AREAS. NO CRACKS FOUND IAW NDTM PART 6 51-00-01.Feb 21, 2014 · N430QX · Bombdr DHC8402 · Wing, Plate/SkinSDR QXEA2014030400187Floor Support · corrodedCORROSION ON FLOOR SUPPORT ANGLE. REPLACED FLOOR SUPPORT ANGLE IAW SRM 53-40-43-02-01.Feb 20, 2014 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2014022000143Seat Track · corrodedLT OTBD SEAT TRACK HAS CORROSION AT BS 241, 255, 272, 303, 318 AND 396. BLENDED CORROSION AT IAW SRM 51-21-00-00-02. BLENDS ARE WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED.Feb 18, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014022000142Seat Track · corrodedRT OTBD SEAT TRACK CORRODED AT BS 211. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREA IAW SRM Feb 18, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014030500196Seat Track · corrodedSEAT TRACK NR 16 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. INSTALLED NR 16 SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND AMM 20-10-01-430-801.Feb 17, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014030500195Seat Track · corrodedSEAT TRACK NR 11 FOUND TO BE CORRODED BEYOND LIMITS. REMOVED NR 11 SEAT TRACK IAW SRM 51-41-00-00-01, 51-42-05-02-01 AND 51-40-15-02-01. DRILLED NEW FASTENER HOLES IN NEW TRACK PN 85328210-115, DEBURRED AND COUNTERSUNK AS NECESSARY. ALL WORK DONE IAW SRM 51-Feb 17, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014022000144Seat Track · corrodedSEAT TRACK NR 16 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05-02-01, 51-40-15-02-01 AND AMM 20-10-01-430-801.Feb 17, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014022000141Seat Track · corrodedSEAT TRACK NR 11 FOUND TO BE CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-41-00-00-01, 51-42-05-02-01 AND 51-40-15-02-01.Feb 17, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014021900134Seat Track · corrodedLEFT INBD SEAT TRACK CORRODED AT BS 578-656. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLENDS ARE WITHIN LIMTIS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION OF ABOVE AREAS IAW NTM PART 6, 51-00-02. APPLIED ALODINE TREATMENT TO AFFECTED AREAS IAW SRM 51-Feb 17, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014021900138Tray · corrodedCORROSION ON AVIONICS TRAYS AND BOLTS AT BS 19.4 ABOVE STR 33. REMOVED AND REPLACED CORRODED SCREWS AND WASHERS IAW SRM 51-41-00-00-01. CLEANED AVIONICS TRAYS OF CORROSION IAW SRM 51-21-00-00-02. NO CORROSION DAMAGE NOTED.Feb 16, 2014 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2014022000140Seat Track · corrodedLT OTBD SEAT TRACK CORRODEDA T BS 148. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-40-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREAS IAW SRM Feb 14, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014021900133Seat Track · corrodedLEFT INBD SEAT TRACK CORRODED BS 272 - 549. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLENDS ARE WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREAS Feb 14, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014021900132Seat Track · corrodedRT INBD SEAT TRACK CORRODED AT BS 620. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREAS IAW SRMFeb 14, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014021900131Seat Track · corrodedRIGHT INBD SEAT TRACK CORRODED AT BS 589. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREAS IAW SRFeb 14, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014021900129Seat Track · corrodedRIGHT INBD SEAT TRACK CORRODED AT BS 216. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE FREEDOM OF MOVEMENT TO AFFECTED Feb 14, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014021900128Seat Track · corrodedLEFT INBD SEAT TRACK CORRODED AT BS 179. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLEND IS WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTED AREAS IAW Feb 14, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014022000139Seat Track · corrodedRIGHT OTBD SEAT TRACK CORRODED BS 247,279 & 372. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLENDS ARE WITHIN LIMITS IAW SRM 53-20-40-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECTEFeb 13, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014021900130Seat Track · corrodedRIGHT INBD SEAT TRACK CORRODED AT BS 371 AND 557. 1. BLENDED CORROSION IAW SRM 51-21-00-00-02. BLENDS ARE WITHIN LIMITS IAW SRM 53-20-49-02-02. EDDY CURRENT INSPECTION PERFORMED IAW NTM PART 6, 51-00-02. NO DEFECTS NOTED. APPLIED ALODINE TREATMENT TO AFFECFeb 13, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014021400112Seat Track · corrodedCORROSION FOUND ON LT SEAT TRACK AT Y9.25, BS 722.102. BLENDED CORROSION IAW SRM 53-40-49-02-02 AND 53-40-49-02-01. FOUND TO BE WITHIN LIMITS IAW SRM 53-40-49-02-01 AND 53-40-49-02-02. ALODINED BLENDED AREA IAW SRM 51-21-10-02-01.Feb 13, 2014 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2014030300164Panel · corrodedPANEL 624AT HAS CORROSION ON MATING SURFACE. BLENDED OUT DAMAGED AREA IAW SRM 57-20-35-01-01 BETWEEN STA YW237.399 AND YW201.069. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-35-01-01. PERFORMED ECI ON BLENDED AREA. NO CRACKS FOUND IAW NDTM PART 6 51-00-01.Feb 12, 2014 · N430QX · Bombdr DHC8402 · Wing, Plate/SkinSDR QXEA2014021400111Pivot Assy · corrodedFWD BAGGAGE DOOR PIVOT ASSY HAS SIGNS OF CORROSION. CLEANED AND INSPECTED FORWARD BAGGAGE PIVOT ASSY IAW SRM 51-26-00-02-01. FOUND CORRODED AND SEIZED BEARING. PIVOT ASSY HAD NO FURTHER EVIDENCE OF CORROSION. NEW BEARING ON ORDER. R & R SEIZED BEARING LOCATFeb 11, 2014 · N430QX · Bombdr DHC8402 · Cargo/Baggage DoorsSDR QXEA2013102801464Switch · brokenFORWARD EMERGENCY LIGHTING SWITCH DOES NOT ILLUMINATE. REPLACED THE SWITCH. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.Oct 28, 2013 · N430QX · Bombdr DHC8402 · Emergency LightingSDR QXEA2013091701394Display · inoperativePFT BLANKED OUT SHOWED "T" AND STAYED OFF FOR APPROX THREE MINUTES "PFD MON 1 FAIL" MESSAGE ON ED. DISPLAY RETURNED TO NORMAL AFTER ABOUT 3-4 MIN. RETURNED TO FIELD. LANDING UNEVENTFUL. REPLACED NR 1 PFD IAW MX 6316104 AS PRECAUTIONARY MEASURE. CLEANED PFD FSep 17, 2013 · N430QX · Bombdr DHC8402 · Central DisplaySDR QXEA2013081601272Unknown · unknownAUTOFEATHER SELECT BUTTON WILL NOT TEST WITH THE CAUTION ADVISORY TEST. PERFORMED GVI AND FOUND C/B F3 POPPED,"CAUTION ADV." NO HISTORY OF CIRCUIT BREAKER F3 WAS FOUND WITHIN THE LAST 14 DAYS. RESET CIRCUIT BREAKER IAW GPM 9.2.2 LAMP CHECKED GOOD. AUTOFEAAug 16, 2013 · N430QX · Bombdr DHC8402 · Propeller Feathering/ReversingSDR QXEA2013081501257Handle · out of adjustFOUND AFT SERVICE DOOR EXTERIOR HANDLE NOT RESTING IN THE DOOR CUT OUT WHEN THE DOOR IS CLOSED AND LOCKED FROM INSIDE THE ACFT. REMOVED THE LINER IAW AMM 25-26-26-000-801. ADJUSTED HANDLE OPEN STOP.Aug 15, 2013 · N430QX · Bombdr DHC8402 · Service DoorsSDR QXEA2013010600015Stop · wornDURING THE OPENING OF THE FORWARD EMERGENCY TYPE II EXIT, THE LOWER DOOR WAS UNABLE TO BE LOCKED TO THE WATER LANDING (DITCHING) POSITION. FOUND STOP TO BE WORN ON DOOR. REPLACED EXIT STOP IAW SRM 51-42-05.Jan 6, 2013 · N430QX · Bombdr DHC8402 · Emergency ExitsSDR QXEA2012100601184Switch · dirtyON LANDING THE GROUND SPOILERS FAILED TO DEPLOY. FLIGHT/TAXI SWITCH WILL NOT REMAIN IN THE TAXI POSITION. CLEANED NR 1 & NR 2 POWER LEVER 12 DEGREE SWITCHES IN POWER LEVER MODULE IAW CMM 76-10-01 PG 401 & 402. PERFORMED FUNCTIONAL TEST OF THE GROUND SPOILEROct 6, 2012 · N430QX · Bombdr DHC8402 · Power LeverSDR QXEA2012081300786Lamp · inoperativeEMERGENCY LIGHT SWITCH ON, FORWARD F/A CONTROL PANEL IS NOT ILLUMINATING. RELAMPED, OPS CHECK GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE.Aug 13, 2012 · N430QX · Bombdr DHC8402 · Emergency LightingSDR QXEA2012071900713Light · damagedTHE EMERGENCY FLOOR PATH LIGHTING DISCOLORED IN FRONT OF THE BAGGAGE DOOR (FWD) AND ALSO IN FRONT OF ROW 1. REPLACED AS REQUIRED IAW TC 6-33-70.Jul 19, 2012 · N430QX · Bombdr DHC8402 · Emergency LightingSDR QXEA2012070100593Seal · leakingENROUTE AT 25,000 FT, THERE WAS A LOUD SQUEAL FROM THE TYPE II/III EXIT DOOR ON THE FO'S SIDE. RETURNED TO FIELD, LANDING UNEVENTFUL. R & R RT FWD LOWER EMERGENCY EXIT DOOR SEAL IAW MM TASK 52-23-06-000-801 AND TASK 52-23-06-400-801. PRESSURIZATION LEAK CHJul 1, 2012 · N430QX · Bombdr DHC8402 · Emergency ExitsSDR QXEA2012050700372Stop · wornMAIN CABIN DOOR HANDLE IS HARD TO UNLOCK FROM INSIDE. COMPLIED WITH FUNCTION CHECK OF DOOR, FOUND FORCE TO UNLOCK EXCEEDS 60 LBS; REPLACED NR 5 STOP PIN FOR WEAR, ADJUSTED DOOR STOP BOLTS, STOP GUIDES, & DOWN LIMIT STOP IAW AMM PRESSURIZATION, RUN, LEAK CHECKMay 7, 2012 · N430QX · Bombdr DHC8402 · Passenger/Crew DoorsSDR QXEA2012041100286Seal · lack of lubeLEFT REAR PASSENGER DOOR SEEMS HARD TO OPEN. CLEANED AND LUBED AFT PAX DOOR SEAL, OPEN AND CLOSED DOOR MULTIPLE TIMES , DOOR OPEN AND CLOSES NORMAL. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.Apr 11, 2012 · N430QX · Bombdr DHC8402 · Passenger/Crew DoorsSDR QXEA2012031900231Handle · icedF/A REPORT MAIN CABIN DOOR RELEASE HANDLE IS VERY DIFFICULT TO LIFT UP WHEN OPENING DOOR. CLEANED ICE FROM LOWER DOOR APERTURE. COMPLIED WITH LUBRICATION AND OPS CHECK OF DOOR HANDLE IAW MM 52-11-00-700-802. OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS RMar 19, 2012 · N430QX · Bombdr DHC8402 · Passenger/Crew DoorsSDR QXEA2012030600217Door · noneDOOR VERY DIFFICULT TO OPEN FROM INSIDE. COMPLIED WITH FUNCTIONAL CHECK OF THE AIRSTAIR DOOR HANDLE FORCES IAW AMM 52-11-00-720-802, NO DEFECTS NOTED. RETURNED TO SERVICE.Mar 2, 2012 · N430QX · Bombdr DHC8402 · Passenger/Crew DoorsSDR QXEA2012020300149Controller · malfunctioned"A/F TEST FAILED" CAUTION MESSAGE ON NR 1 ENGINE AFTER A/F TEST. CHECKED CDS, FOUND FAULT 400A ON NR 1 PEX REF FIM 61-20-09-810-806. FOUND NR1 PEC HAS PRIOR HISTORY OF SAME FAULT ON OTHER ACFT. R & R NR1 PEC IAW AMM 61-20-36-000-801/400-801. CHECKS GOOD IAW AFeb 1, 2012 · N430QX · Bombdr DHC8402 · Propeller Controlling SystemSDR QXEA2012012700132Control Unit · malfunctionedON TAKEOFF ROLL WITH POWER LEVERS IN THE RATING DETENT, AUTOFEATHER FAILED TO ARM. AUTOFEATHER SWITCHLIGHT WAS DEPRESSED AND "SELECT" WAS ILLUMINATED. TAKEOFF WAS ABORTED ABOVE 60 KTS BUT LESS THAN 80 KTS. RETURNED TO THE GATE. INTERROGATED CDS FOR FAULTS. Jan 24, 2012 · N430QX · Bombdr DHC8402 · Propeller Feathering/ReversingSDR QXEA2012011700011Autofeather Sys · malfunctionedAUTOFEATHER FAILED TO ARM ON TAKEOFF. ABORTED TAKEOFF AT 60 KNOTS AND RETURNED TO THE GATE. INTERAGATED CDS FOUND FAULT CODES 494 & 422 ON NR 1 ENGINE. C/W FIM 61-20-10-810-826 FOR FAULT 494 FAULT CODE CLEARED. C/W FIM 61-20-09-810-813 FAULT CODE CLEARED OPSJan 10, 2012 · N430QX · Bombdr DHC8402 · Propeller Feathering/ReversingSDR QXEA2011101000982Light · damagedPOSSIBLY ELECTRICAL ODOR EMANATING FROM REAR OF ACFT. INSPECTED CARGO PIT FOUND ODOR TO BE CENTERED AROUND THE FWD LAMP ASSY. BEGAN REMOVAL OF PANEL 251CZ REMOVED ENOUGH OF THE PANEL TO GRANT ACCESS FOR FURTHER INSPECTION REQUIRING THE REMOVAL OF THE AFT CAROct 4, 2011 · N430QX · Bombdr DHC8402 · Cargo Compartment LightingSDR QXEA2011080200640Seat Track · corrodedCORROSION FOUND ON RT INBD SEAT TRACK AT X 1.00. BLENDED SEAT TRACK DAMAGE AND FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED RT INBD FWD SEAT TRACK IAW SRM 51-40-00-02-01. INSTALLED NEW SEAT TRACK IAW SRM 51-40-07-02-01 AND 51-40-15-02-01. APPLIED SEJul 30, 2011 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
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