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 QXEA2011080200639Tray · corrodedSTANDBY BATTERY TRAY NEEDS CLEANED PAINTED. CLEANED TRAY IAW SRM 51-26-00. REMOVED CORROSION IAW SRM 51-21-00. TREATED AND PRIMED IAW RD 8/4-53-3833. PERFORMED ECI ON TRAY, NO CRACKS FOUND IAW NDTM PSM 1-84-7A.Jul 29, 2011 · N430QX · Bombdr DHC8402 · Battery Box StructureSDR QXEA2011080100634Angle · corrodedCORROSION FOUND AT FS 32.400, Z100.032 WEB AT AFT SIDE OF FWD PASSENGER DOOR FLOOR LEVEL Y EQUALS 27L TO 38L. REMOVED ANGLE .013" MATERIAL REMOVED IAW SRM 51-21-00-00-02 AND 51-42-05-00-01. FABRICATED NEW ANGLE FROM 2024-T3 .050 IAW DWG 824844, SRM 51-21-10-Jul 29, 2011 · N430QX · Bombdr DHC8402 · Passenger/Crew DoorsSDR QXEA2011080100631Threshold · corrodedCORROSION FOUND AT FORWARD PASSENGER DOOR THRESHOLD MEMBER. REMOVED THRESHOLD MEMBER IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW 51-21-00-00-02. LOCATED FASTENER HOLED FOR NEW THRESHOLD MEMBER IAW SRM 51-40-05-00-01 AND 51-40-07-02-01. INSTALLED ANGLE IAJul 28, 2011 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011080100630Frame · corrodedCORROSION FOUND AT X1.0 LT AND Z100 BETWEEN STR 23 & 24. REMOVED CORROSION IAW SRM 51-21-00. TREATED AFFECTED AREAS IAW SRM 51-21-10-02-01 PRIMED IAW SRM51-25-10-02-01, TOP COATED IAW SRM 51-25-25-02-01, APPLIED CIC IAW SRM 51-21-10-02-01. ALL WORK DONE INJul 28, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011080100629Panel · corrodedFOUND CORROSION AROUND 2 PANEL SCREW HOLES AT FS X 784.102 FLOOR LEVEL Z100.032 Y6.250 AND Y20. BLENDED OUT CORROSION AND FOUND IN LIMITS IAW SRM 51-21-00 AND RD 8/4-53-3835.. ALODINED IAW SRM 51-21-10-01. ENGINEERING REQUEST SENT TO MFG. PERFORMED ECI ON Jul 28, 2011 · N430QX · Bombdr DHC8402 · Fuselage Floor PanelSDR QXEA2011080100636Threshold · corrodedCHANNEL BELOW MAIN DOOR THRESHOLD CORRODED. BLENDED OUT CORROSION IAW SRM 51-21-00-00-02. SENT TO ENGINEERING. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-1660. PERFORMED LPI IAW QX CHAP 8.2 NO DEFECTS NOTED. PERFORMED ECI ON ALL BLENDED AREAS IAW NDTM PSM 1-Jul 28, 2011 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011080100635Structure · corrodedCORROSION AT X 32.400 AND 2100 LT BETWEEN STR 23&24. REMOVED CORROSION IAW SRM 51-21-00-00-02. MAX MATERIAL REMOVED .021". TREATED, PRIMED AND PAINTED IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND 51-25-25-02-01. APPLIED CORROSION INHIBITING COMPOUND IAW SRMJul 28, 2011 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011080100633Frame · corrodedFOUND CORROSION ON FRAME FS 281 BETWEEN STR 30 AND 32 RT SIDE. REMOVED CORROSION IAW 51-21-00-00-02. MAX MATERIAL REMOVED .003" IS WITHIN LIMITS IAW RD 8/4-53-2344. TREATED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. APPLIED TOP COAT AND CIC TO WJul 28, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011072800624Frame · corrodedCORRODED RIVETS FOUND AT FS 196 BETWEEN STR 30 & 32 LT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .039, ORIGINAL THICKNESS .040", .001 MATERIAL REMOVED IAW SRM 53-20-15-00-01. ALL WORK ACCEPTABLE RD 8/4-53-2344. TREATED WORKEDJul 27, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011072800623Frame · corrodedCORRODED RIVETS FOUND AT FS 216 BETWEEN STR 30 & 32 LT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038, ORIGINAL THICKNESS .040", .002 MATERIAL REMOVED IAW SRM 53-20-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED WOJul 27, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011072800618Floor Panel · corrodedCORROSION AROUND FLOOR PANEL SCREW HOLE AT FS X714.062 Z 100.032 Y23.5. BLENDED AREA IAW 51-21-00-00-02. FOUND OUT OF LIMITS IAW 53-40-43-00-01. ENGINEERING REQUEST SENT TO MFG. PAINTED AREA IAW SRM 51-25-15-02-01. PERFORMED ECI IAW NDTM PSM 1-84-7A. WORKJul 27, 2011 · N430QX · Bombdr DHC8402 · Fuselage Floor PanelSDR QXEA2011072800616Frame · corrodedCORRODED RIVETS FOUND AT F/S 156 BETWEEN STR 30 & 32 RT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038. ORIGINAL THICKNESS .040". .002" MATERIAL REMOVED IAW SRM 53-23-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED Jul 27, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011072800615Structure · corrodedCORRODED RIVETS FOUND AT FS 176 BETWEEN STR 30 & 32 RT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038. ORIGINAL THICKNESS .040". .002" MATERIAL REMOVED IAW SRM 53-23-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED Jul 27, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, StructureSDR QXEA2011072800614Skin · corrodedFOUND CORROSION ON FUSELAGE BELLY UNDER FWD DRAIN MAST ATTACH POINT. REMOVED SURFACE CORROSION FROM DRAIN MAST MOUNT IAW SRM 51-21-00. ALODINED IAW SRM 51-21-10-02-01. PAINTED IAW SRM 51-25-25-02-01.Jul 27, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, Plate/SkinSDR QXEA2011072800613Structure · corrodedCORRODED RIVETS FOUND AT FS 136 BETWEEN STR 30 & 32 LT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038. ORIGINAL THICKNESS .040". .002" MATERIAL REMOVED IAW SRM 53-23-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED IJul 27, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, StructureSDR QXEA2011072800625Frame · corrodedCORRODED RIVETS FOUND AT FS 321 BETWEEN STR 30 & 32 RT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038, ORIGINAL THICKNESS .040", .002 MATERIAL REMOVED IAW SRM 53-20-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED WOJul 26, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011072800622Frame · corrodedCORRODED RIVETS FOUND AT FS 258 BETWEEN STR 30 & 32 LT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION, TOLERANCE .038, ORIGINAL THICKNESS .040", .002 MATERIAL REMOVED IAW SRM 53-20-15-00-01. ALL WORK ACCEPTABLE IAW RD 8/4-53-2344. TREATED WOJul 26, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011072800621Seat Track · corrodedCORROSION ON FLOOR SEAT TRACK LT SIDE INBD FS X644.5 TO X668.9. BLENDED CORROSION FOUND TO EXCEED MAX LIMITS IAW RD 8/4-53-884. REMOVED THE SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. PREPARED SEAT TRACK FOR INSTALL AND INSTALLED SEAT TRACK IAW 5Jul 26, 2011 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2011072800620Sill · corrodedAFT SERVICE DOOR SILL PLATE CORRODED. CORROSION REMOVED IAW 51-21-00-00-02. SENT ENGINEERING REQUEST. AREA OUT OF LIMITS IAW SDR 53-40-21-00-01. LOCATED HOLES AND ROUGH CUT NEW SEAL PLATE IAW SRM 51-24-35-02-01. FABRICATED NEW SILL IAW EC 6-53-999. TREATJul 26, 2011 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011072800619Frame · corrodedCORROSION FOUND FROM FRAME X47.975 - X32.400 ON ATTACH FLANGE ON RT STR 31. REMOVED 4 RIVETS IAW SRM 51-42-06-00-01. BLENDED AREA IAW SRM 51-21-00-00-02. ENGINEERING REQUEST SENT. ULTRA SONIC THICKNESS EXAMINATION PERFORMED, MINIMUM REMAINING THICKNESS .06Jul 26, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011072800617Sill · corrodedLIGHT CORROSION FOUND UNDER AFT SERVICE DOOR SILL. REMOVED CORROSION IAW SRM 51-21-00. ENGINEERING REQUEST SENT. RECEIVED RD 8/4-53-3828. AREA IS OK AS IS. TREATED AND PRIMED AREA WORKED IAW SRM 51-25-10-02-01.Jul 26, 2011 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011072700612Frame · corrodedCORRODED RIVETS ON FRAME AT X116.00 BETWEEN LT STR 31&30. REMOVED 5 RIVETS IAW SRM 51-42-05-00-01. REMOVED LIGHT CORROSION IAW SRM 51-21-00-02-01. BLENDED AREA WITHIN LIMITS OF RD 8/4-53-2344. ALL WORK DONE IAW RD 8/4-53-2344. TREATED AND PRIMED IAW SRM 51Jul 26, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011072700611Attach Fitting · corrodedCORRODED RIVETS ON ATTACH FLANGE OF RT STG 26 FROM X116.00 - X216.00. REMOVED 42 RIVETS IAW SRM 51-42-05-00-01. FOUND NO OTHER CORROSION. INSTALLED 42 NEW RIVETS IAW SRM 51-42-05. PRIMED AND PAINTED IAW AMM 51-25-26 AND 51-25-31-302-801. APPLIED LPS NR 3 Jul 26, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, Attach FittingsSDR QXEA2011072700610Frame · corrodedCORRODED RIVETS FOUND AT F/S 156 BETWEEN STR 30 AND 32 LT. REMOVED RIVETS IAW SRM 51-42-05-02-01. BLENDED OUT CORROSION IAW SRM 51-26-10-02-01. ALL BLENDS WITHIN LIMITS RD 8/4-53-2344. TREATED BLENDED AREAS IAW SRM 51-21-10-02-01 AND 51-25-10-02-01. INSTAJul 26, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, FrameSDR QXEA2011072700609Structure · corrodedCORRODED RIVETS ON FOUND AT F/S 176 BETWEEN STR 30&32 LT. REMOVED 6 RIVETS IAW SRM 51-42-05-00-01. FOUND CORROSION UNDER BUCK TAILS ON FRAME, BLENDED OUT CORROSION IAW SRM 51-26-10-02-01. ALL BLENDS WITHIN LIMITS RD 8/4-53-2344. TREATED BLENDED AREAS IAW SJul 26, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, StructureSDR QXEA2011072700608Structure · corrodedCORRODED RIVETS ON ATTACH FLANGE OF RT STG 25, FROM X116.00 - X156.00. REMOVED 13 CORRODED RIVETS IAW SRM 51-42-05-00-01. AFTER FURTHER INSP, NO DAMAGE FOUND TO STRINGER. INSTALLED 13 NEW RIVETS IAW SRM 51-42-05-02-01. PRIMED AND PAINTED FRAME IAW SRM 51-2Jul 26, 2011 · N430QX · Bombdr DHC8402 · Fuselage Miscellaneous StructureSDR QXEA2011072500596Attach Fitting · corrodedCORROSION ALONG INBD ATTACH FLANGE ON LT STG 31 FROM X584.00 - X644.50. REMOVED CORROSION IAW SRM 51-21-00-00-02. TREATED AND PRIMED IAW SRM 51-25-10-02-01.Jul 22, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, Attach FittingsSDR QXEA2011072000514Attach Fitting · corrodedC2 - CORRODED RIVETS ON RT STG 31 ATTACH FLANGE BETWEEN X1.00 AND 19.400. REMOVED 19 EA RIVETS IAW SRM 51-42-05. FOUND NO EVIDENCE OF CORROSION UNDER RIVET HEADS IAW SRM 51-14-00. INSTALLED 19 EA RIVETS IAW SRM 51-42-05. TREATED, PRIMED AND PAINTED AREA IAJul 19, 2011 · N430QX · Bombdr DHC8402 · Fuselage Main, Attach FittingsSDR QXEA2010122700935Brake Sys · malfunctionedEXCESSIVE BRAKING REQUIRED TO STOP. C/W BLEEDING OF THE BRAKE SYS. IAW AMM 32-42-00-870-801. C/W FUNCTIONAL TEST OF BRAKE SYS IAW AMM 32-42-00-720-801. CHECKS GOOD. C/W FUNCTIONAL TEST OF ANTI-SKID SYS IAW AMM 32-46-00-720-802. TESTS GOOD. C/W ANTI-SKID BUILTDec 21, 2010 · N430QX · Bombdr DHC8402 · Landing Gear Brake SystemSDR QXEA2010102800671Actuator · malfunctionedWITH GEAR RETRACTION NOSE WHEEL REMAINED DOWN AND LOCKED FOR 23 SEC AFTER MAINS WERE UP AND LOCKED. NOSEWHEEL AMBER, RED AND UNSAFE LIGHTS REMAINED ILLUMINATED. GEAR CAME UP BY ITSELF AND LIGHTS WENT DARK. ALTERNATE GEAR EXT. ACCOMPLISHED. LANDING UNEVENTFUL.Oct 24, 2010 · N430QX · Bombdr DHC8402 · Landing Gear ActuatorSDR QXEA2010080200457Blade · crackedNR 2 PROPELLER BLADES HAVE CUFF CRACKS, ALL BLADES. REPAIRED CUFF CRACKS ON ALL 6 BLADES OF THE 2 PROPS IAW MFG PUB 1105 BLADE REPAIR MANUAL MINOR BLADE REPAIR NR 3 (F10). PLACED ON DMI. RETURNED TO SERVICE.Jul 28, 2010 · N430QX · Bombdr DHC8402 · Propeller Blade SectionSDR QXEA2010040200211Transceiver · failedWEATHER RADAR DOES NOT PAINT GROUND CLUTTER OR WEATHER CORRECTLY. DUE TO THUNDERSTORMS, DIVERTED, LANDING UNEVENTFUL. R & R RADAR TRANSCEIVER IAW AMM 34-41-01, PGS 401-406. OPS TEST CKS GOOD IAW 34-41-00, PGS 516-520. RETURNED TO SERVICE.Mar 29, 2010 · N430QX · Bombdr DHC8402 · Weather Radar SystemSDR QXEA2010020100071Selector Valve · malfunctionedGEAR DID NOT EXTEND WHEN GEAR HANDLE SELECTED. 3 RED LIGHTS ILLUMINATED, NO OTHERS ILLUMINATED. PERFORMED ALTERNATE GEAR EXTENSION IAW E/A CHECKLIST PROCEDURE GEAR EXTENDED OK. LANDING UNEVENTFUL. FAULTS NOTED IN PSEU FLIGHT LEG 00" DIN01A FAULT UNREASON TRJan 28, 2010 · N430QX · Bombdr DHC8402 · Landing Gear Retraction/Extension SystemSDR QXEA2010011900044Door · unsecureMASTER WARNING FUSELAGE DOORS - REJECTED T/O AT 96KTS. UPON RETURN TO GATE BAG AFT DOOR HANDLE POPPED OPEN. DOOR STILL CLOSED. WT 48,000 LBS. NO BRAKES APPLIED. C/W INSP AND OPS TEST OF AFT CARGO DOOR HANDLE IAW AMM TASK 52-31-00-710-801. OPS TEST GOOD, TASJan 13, 2010 · N430QX · Bombdr DHC8402 · Cargo/Baggage DoorsSDR QXEA2010010700020Control Panel · malfunctionedLANDING GEAR DID NOT EXTEND NORMALLY- NO INDICATION THAT GEAR DOORS OPENED PERFORMED EMERGENCY CHECK LIST UTILIZED ALTERNATE GEAR EXTENSION. GEAR EXTENDED UTILIZING ALTERNATE GEAR EXTENSION. LANDING UNEVENTFUL. RETRIEVED PSEU FAULT CODES IAW AMM TASK 32-61-00-Jan 3, 2010 · N430QX · Bombdr DHC8402 · Landing Gear Retraction/Extension SystemSDR QXEA2010010600016Elevator System · malfunctioned"ELEVATOR FEEL" CAUTION MESSAGE IN CRUISE AT 25,000 REMAINED ON FOR ENTIRE FLIGHT. DIVERTED. LANDING UNEVENTFUL. INTEROGATED CDS FOUND FAULT "LT FEEL ACTUATOR FAIL MESSAGE" ALSO FOUND CB H4 TRIPED. RE-SET H4 REF GMM 9.2.2. AND C/W FIM TASK 27-30-00-810-802 CLEJan 2, 2010 · N430QX · Bombdr DHC8402 · Elevator Control SystemSDR QXEA200901006Warning Light · illuminatedON T/O ROLL AT 70KTS, GOT THE NR 1 AND NR 2 BLEED HOT CAUTION LIGHT, AFTER FOLLOWING ABNORMAL CHECKLIST, BLEED, PRESSURIZATION ALL WORKING NORMALLY. INTERIGATED CDS, NO FAULTS FOUND, C/W OPS TEST OF THE BLEED AIR SYS IAW AMM TASK 36-11-00-710-802, OPS TEST GNov 23, 2009 · N430QX · Bombdr DHC8402 · Pneumatic Distribution SystemSDR QXEA2009112000973Solenoid Valve · malfunctionedATTEMPTED TO START APU, APU AUTO SHUTDOWN. RAMP REPORTED ALOT OF SMOKE. PLACED ON MEL 49-00-1. RETURNED TO SERVICE. MEL CLOSED ON 11-18-09. INTERROGATED CDS, FOUND CODE 102-3 ( UNDERSPEED) REMOVED AND REPLACED MAIN FUEL SOLENOID VALVE IAW AMM TASK 49-30-07-000Nov 16, 2009 · N430QX · Bombdr DHC8402 · APU Engine Fuel and ControlSDR QXEA2009102600875Warning Message · illuminatedPOWERPLANT MESSAGE ON T/O ROLL AT 40KTS. INSPECTED AND FOUND FAULT 794 ON NR 1 ENG. PERFORMED FIM TASK 73-20-00-810-850 AND AMM TASK 71-00-00-868-806 WITH 2 SEPRATE STARTS. FAULT DID NOT RETURN. AIRCRAFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.Oct 22, 2009 · N430QX · Bombdr DHC8402 · Central WarningSDR QXEA2009091000669Unknown · odorAN ELECTRICAL ODOR IN BACK BAGGAGE COMPARTMENT NEAR NR 1 SMOKE DETECTOR. REMOVED AND REPLACED NR 1 SMOKE DETECTOR AS A PRECAUTION IAW AMM 26-12-01-000-801 / 400-801 OPS TEST GOOD. ELECTRICAL ODOR STILL EXISTS. REMOVED FORWARD AFT BAGGAGE COMPARTMENT LIGHT ASSYSep 7, 2009 · N430QX · Bombdr DHC8402 · Air Distribution SystemSDR QXEA2009090800653Display · failedSTRONG ODOR IN FLIGHT DECK EXTENDS BACK TO APPROXIMATELY ROW 5. INVESTIGATED ODOR, FOUND NR 1 ARCDU FAILED., REMOVED AND REPLACED NR 1 ARCDU IAW MTC 9238101. RETURNED TO SERVICE.Sep 2, 2009 · N430QX · Bombdr DHC8402 · Communications SystemSDR QXEA2009042400289Handle · dislodgedSEA - UPON ROTATION FUSELAGE DOOR WARNING LIGHT ILLUMINATED AND AIRCRAFT DID NOT PRESSURIZE. AFTER RETURN TO FIELD BAGGAGE DOOR HANDLE WAS STICKING OUT. MAINTENANCE PERFORMED A INSPECTION OF THE AFT CARGO DOOR AND OPERATIONAL TEST IAW AMM TASK 52-31-00-710-8Apr 20, 2009 · N430QX · Bombdr DHC8402 · Cargo/Baggage DoorsSDR QXEA2009042200285Door · unknownPDX - L2 - AFT SERVICE DOOR WILL NOT OPEN. MAINTENANCE OPERATED DOOR, NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.Apr 18, 2009 · N430QX · Bombdr DHC8402 · Service DoorsSDR QXEA2009040100209Skin · chafedPDX - C1 RT OTBD FLAP HAS TOP SKIN CHAFE APPROX 47 INCHES FROM THE INBD EDGE 34 INCHES LONG. BLENDED AREA OF CHAFE IAW SRM 57-52-30-02 TO REMOVE DAMAGE AND FOUND BLENDED AREA TO BE OUT OF LIMITS IAW SRM 57-52-30-01. HFEC IAW NDTM PART 6 51-00-01, NO CRACKS NMar 29, 2009 · N430QX · Bombdr DHC8402 · Trailing Edge FlapsSDR QXEA2009040100208Skin · damagedPDX - C1 - THERE ARE THREE DENTS IN THE UPPER OUTBOARD SKIN OF THE MCD THAT REQUIRE A PERMANENT REPAIR. MAPPED AREA OF DENTS FOR ENGINEERING STARTED THE REPAIR ON THE MCD SHELL ASSY IAW RD 8/4-52-456 STEPS (1) AND (2). CONTINUED REPAIR OF MCD SHELL BY COMPLYMar 29, 2009 · N430QX · Bombdr DHC8402 · Cargo/Baggage DoorsSDR QXEA2009040100207Skin · damagedPDX - C1 - LT OTBD FLAP AT APPROX 30 INCHES FROM INBOARD END AND APPROX 14 INCHES UP FROM TRAILING EDGE ON THE TOP SURFACE HAS A CHAFE FORMING, CHAFE IS APPROX 3 INCHES IN LENGTH AND .100 INCH WIDE IN CENTER OF CHAFED AREA. BLENDED AREA IAW SRM 57-52-30-02 TMar 29, 2009 · N430QX · Bombdr DHC8402 · Trailing Edge FlapsSDR QXEA2009033100206Seat Track · corrodedPDX - C1 CHECK, CORROSION PITS ON TOP OF RT INBOARD SEAT TRACK AT STATION 644.5. BLENDED AREA, MATERIAL REMOVED WAS 0.37 INCH AND OUT OF LIMITS. REPLACED SEAT TRACK.Mar 27, 2009 · N430QX · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2009031100175Unknown · odorPDX - APU AIR HAS UNUSUAL AND PERSISTANT ODOR. PLACED APU ON MEL 49-00-1. MEL CLEARED 3/11/09 INSPECTED APU COMPARTMENT. NO DEFECTS NOTED. RAN APU. NO UNUSUAL ODOR FOUND. SYSTEM OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.Mar 7, 2009 · N430QX · Bombdr DHC8402 · Air Distribution SystemSDR QXEA2009020500164Boot · failedGEG- "DEICE PRESS" LIGHT ILLUMINATED IN FLT. RAN CHECKLIST LIGHT CONTINUED TO ILLUMINATE. PSI LOOKED GOOD. LEFT INBOARD DE-ICE BOOT/HORIZONTAL STAB, LIGHT ON THE ICE PROTECTION PANEL CONTINUED TO FLICKER WHILE CHECKLIST WAS BEING DONE. DIVERTED TO GEG. LAMar 1, 2009 · N430QX · Bombdr DHC8402 · Airfoil Anti/De-ice SystemSDR QXEA2009021200114Computer · malfunctionedSEA - DURING APPROACH IN SEA A3 ARM WOULD CYCLE OFF THEN COME BACK ON AT LOC INTERCEPT, THEN AT GLIDESLOPE INTERCEPT IT WOULD GO NO A3. ATTEMPTED 2 APPROACHES ON 16C AND 1 APPROACH ON 16L AND SETUP AGAIN AT PDX 10R ALL RESULTS THE SAME. EVENT MARKER PUSHED. Feb 8, 2009 · N430QX · Bombdr DHC8402 · Ground Proximity System
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