N349PH

Service difficulty reports · 220

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 = 'N349PH' 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 QXEA200701879Trim Panel · failedLWS - FLIGHT 2027 - WHILE BOARDING PASSENGERS WITH GROUND POWER ON, SMOKE STARTED TO COME FROM THE TRIM INDICATOR PANEL IN THE COCKPIT. POWER TURNED OFF AND BATTERIES TURNED OFF. SMOKE STOPPED. NO INDICATION OF FIRE. FOUND CIRCUIT BREAKER POPPED. MAINTENDec 12, 2007 · N349PH · Dhav DHC8202 · Rudder Control SystemSDR QXEA200701631Tscu · failedPDX - ON FLIGHT 2048, NR 2 PROPELLER FAILED AUTOFEATHER TEST. FEATHER LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED AUTOFEATHER CONTROL RELAYS 6121-K6, 6121-K8. COMPLIED WITH AUTOFEATHER TEST BUT FEATHER STILL FAILED TO ILLUMINATE. REPLACED NROct 30, 2007 · N349PH · Dhav DHC8202 · Propeller Feathering/ReversingSDR QXEA200701486Unknown · unknownPDX FLIGHT NR 2156 - MULTIPLE NO AIII WARNINGS ON CAT III APPROACH. PERFORMED INDEX COMPENSATION ADJUSTMENT FOR NR 1 AND NR 2 FLUX VALVES, PERFORMED OPERATIONAL TEST IAW -8 200 TC 9340021, ALL CHECKS GOOD. PERFORMED OPERATIONAL TEST OF HGS RETURN TO SERVICESep 26, 2007 · N349PH · Dhav DHC8202 · Central WarningSDR QXEA200701343Connector · loosePDX FLIGHT NR 2093, AFTER TAKEOFF AIRCRAFT BEGAN PRESSURIZATION AT HIGH RATE, CABIN DIFF OF 5.75 REACHED BY 4000 FEET MSL. SWITCHED TO MAIN MODE, NO CONTROL. ATTEMPTED TO DUMP CABIN WOULDN'T DUMP. FINALLY DUMPED CABIN PRESSURE FOR LANDING BY OPENING FORWARDAug 18, 2007 · N349PH · Dhav DHC8202 · Air Conditioning System WiringSDR QXEA200701231Contactor · damagedSEA FLIGHT NR 2070 WITH NR 1 FEATHERED AND NR 2 UNFEATHERED THE LEFT TRU CAUTION ILLUMINATED. WITH NR 2 FEATHERED AND NR 1 UNFEATHERED THE LIGHT WAS NOT ILLUMINATED. FOUND NO AC POWER ON LEFT BUSS WHILE NR 1 AC GENERATOR OFF LINE AND NR 2 GENERATOR ON LINE. Aug 2, 2007 · N349PH · Dhav DHC8202 · Electrical Power System WiringSDR QXEA200701146Connector · misalignedSEA FLIGHT NR 2104 - DURING TAKEOFF ROLL AUTO FEATHER FAILED TO ARM THROUGH 80 PERCENT. TORQUE ON BOTH NR 1 AND NR 2. FOUND CONNECTOR 6121-P9 TO BE ASKEW. RESEATED CONNECTOR 6121-P9. FUNCTIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Jul 16, 2007 · N349PH · Dhav DHC8202 · Propeller/Propulsor System WiringSDR QXEA200701021Limit Switch · out of adjustSEA FLIGHT NR 2104 AUTOFEATHER DID NOT ARM. MAINTENANCE ADJUSTED THE NR 1 POWER LEVER LIMIT SWITCH. OPERATIONAL CHECK GOOD. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE.Jun 24, 2007 · N349PH · Dhav DHC8202 · Propeller Controlling SystemSDR QXEA200701008Autofeather Sys · malfunctionedYVR FLIGHT NR 2025 - AUTOFEATHER FAILED TO ARM ON TAKEOFF ROLL WITH POWER SET ABORTED TAKEOFF, AUTOFEATHER SYSTEM INOP. MAINTENANCE PERFORMED AUTO FEATHER SYSTEM ADJUSTMENT AND TEST IAW DHC-8-200 ENGINE RIGGING MANUAL. RT ER 10, PARAGRAPH 5-1-A 1 38. PERFORMJun 19, 2007 · N349PH · Dhav DHC8202 · Propeller Controlling SystemSDR QXEA200700526Tscu · malfunctionedPDX AUTO FEATHER ARM SWITCH LIGHT DOES NOT EXTINGUISH, LIGHT FLICKERS ON AND OFF EN ROUTE AND EXTINGUISHES IN DESCENT. REPLACED 6121-K5 RELAY AND NR 1 AND NR 2 TSCU UNITS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Apr 9, 2007 · N349PH · Dhav DHC8202 · Propeller Controlling SystemSDR QXEA200700394Potentiometer · out of adjustSEA FLIGHT NR 2243 WHEN NOSE WHEEL STEERING SELECTED ON, WITH TILLER CENTERED, NOSE WHEEL TURNS FULL LEFT, NOSE WHEEL STEERING INOP. MAINTENANCE RESECURED LINKAGE BETWEEN TILLER HANDLE AND RVDT ADJUSTED POT NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Mar 16, 2007 · N349PH · Dhav DHC8202 · Landing Gear Steering SystemSDR QXEA200603149Ahrs · malfunctionedSEA FLIGHT NR 2084 ADI ROLL MISMATCH ON ADVISORY DISPLAY. FIRST OFFICER ADI SHOWS 5 DEGREE ROLL TO LEFT. MAINTENANCE REPLACED NR 2 AHRS AS PER T/C 9340019. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Dec 8, 2006 · N349PH · Dhav DHC8202 · Attitude and Direction Data SystemSDR QXEA200602957Switch · malfunctionedSEA FLIGHT NR 2203 DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED. MAINTENANCE REPLACED 65 PSI SWITCHES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Nov 15, 2006 · N349PH · Dhav DHC8202 · Airfoil Anti/De-ice SystemSDR QXEA200602634Hydraulic System · malfunctionedPDX FLIGHT 2228 NR 2 AUXILARY POWER CAUTION. MAINTENANCE REPLACED NR 2 SPU IAW DHC-8 AMM 29-*11-17-00-062 AND 29-11-17-00-802. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Oct 6, 2006 · N349PH · Dhav DHC8202 · Hydraulic System, AuxiliarySDR QXEA200602372Bulb · inoperativeSEA FLIGHT NR 2053 NR 2 AUXILLARY PUMP LIGHT INOP. MAINTENANCE RELAMPED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Aug 31, 2006 · N349PH · Dhav DHC8202 · Instrument PanelSDR QXEA200602071Cowl Door · openPDX FLIGHT 2149 COWL DOOR OPEN. MAINTENANCE CLOSED THE COWL DOOR. OPERATION CHECK GOOD, NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Aug 15, 2006 · N349PH · Dhav DHC8202 · Engine Cowling SystemSDR QXEA200601141Battery Pack · malfunctionedSEA - FORWARD CENTER CEILING EMERGENCY LIGHTS INOP AND NR 1 EMERGENCY EXIT EGRESS LIGHTS AT STATION X 324.1 INOP. MAINTENANCE REPLACED EMERGENCY BATTERY PACK PS3 IAW DASH 8 200 AMM 33-51-00, OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Apr 28, 2006 · N349PH · Dhav DHC8202 · Emergency LightingSDR QXEA200600661Frame · corrodedPDX-C4 CHECK, FUSELAGE FRAME WEB HAS SPOTS OF CORROSION ON TOP SURFACE AND AROUND 4 RIVETS AT AFT END OF WEB, LOCATED BETWEEN FS X425 AND X436, WEB IS ON TOP OF STRINGER 23R AT FLOOR LEVEL Z100.032. REPAIRED IAW SRM 51-40-11.Mar 3, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600659Frame · corrodedPDX-C4 CHECK, FUSELAGE FRAME WEB HAS SPOTS OF CORROSION ON TOP SURFACE AND AROUND 4 RIVETS AT AFT END OF WEB, LOCATED BETWEEN FS X424 AND X436, WEB IS ON TOP OF STRINGER 23R AT FLOOR LEVEL. REPAIRED IAW SRM 51-20-11 AND SRM 51-40-11Mar 3, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600658Frame · corrodedPDX - C4 CHECK, FUSELAGE FRAME X424 TO STRINGER 23R TIE CLIP IS CORRODED ON TOP SURFACE, LOWER EDGE AND MOUNTING RIVETS. REPAIRED IAW SRM 51-40-11 AND SRM 51-20-36.Mar 3, 2006 · N349PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200600660Intercostal · bentPDX-C4 CHECK, OUTBOARD INTERCOSTAL IS BENT AND BROKEN AT FS X424 AND STRINGER 23R. REPAIRED IAW SRM 51-40-11.Mar 3, 2006 · N349PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200600639Skin · dentedPDX - C4 CHECK, LEFT HAND AFT FUSELAGE SKIN AND STRINGER DENTED BETWEEN RPB AND FRAME NR 1, STRINGER 13P - 15P. REPAIRED IAW RD 8-55-1651 AND EA 2-55-111.Mar 3, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR QXEA200600636Panel · corrodedPDX - C4 CHECK, ROOT FAIRING PANEL 262PT HAS CORRODED FASTENERS. REPAIRED IAW SRM 53-50-01.Mar 2, 2006 · N349PH · Dhav DHC8202 · Aerodynamic FairingsSDR QXEA200600657Seat Track · corrodedPDX-C4 CHECK. CONTINUATION CARD RIGHT HAND INBOARD SEAT TRACK HAS CORROSION/CHAFE MARKS AT THESE LOCATIONS X405, X375 - X379, X313 - X316, AND X281 - 284. REPAIRED IAW RD 8-53-4473.Feb 27, 2006 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA20060618Seat Track · corrodedPDX C4 CHECK, LEFT HAND INBOARD SEAT TRACK NR 4 HAS PITTING CORROSION INSIDE TRACK AT STATION X266, X280 AND X298. REPAIRED IAW RD 8-53-1339 AND RD 8-51-1102.Feb 27, 2006 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA20060623Seat Track · corrodedPDX-C4 CHECK, RIGHT HAND INBOARD SEAT TRACK HAS CORROSION/CHAFE MARKS AT X409, X375 - 379, X313 - 316, AND X281 - 284. REPAIRED IAW RD 8-53-1339 AND SRM 51-40-00, SRM 51-40-11.Feb 27, 2006 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200600655Skin · chafedPDX-C4 CHECK, RIGHT OUTBOARD FLAP HAS A 4" CHAFE ON TOP EXTERIOR SKIN AT WS YW236.000 AND FORWARD OF TRAILING EDGE. REPAIRED IAW RD 8-57-1022 AND SRM 51-20-36, SRM 51-20-16, AND SRM 51-20-26.Feb 26, 2006 · N349PH · Dhav DHC8202 · Trailing Edge FlapsSDR QXEA200600654Frame · crackedPDX-C4 CHECK, FRAME CRACKED APPROX STATION X253.4, BLR 24R Z100.8. REPAIRED IAW EA 2-53-690.Feb 25, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600656Stringer · corrodedPDX-C4 CHECK, CORROSION ON STRINGER 31R TOP SURFACE OF LOWER FLANGE BETWEEN FSX151 AND X167. REPAIRED IAW EA 2-53-689 AND SRM 51-40-11.Feb 24, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, Longeron/StringerSDR QXEA200600646Skin · corrodedPDX - C4 CHECK, JACK PAD (NOSE) IS CORRODED, AS SEEN FROM INSIDE AIRCRAFT. REPAIRED IAW SRM 51-40-11.Feb 24, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR QXEA200600645Stringer · corrodedPDX - C4 CHECK, STRINGER 31R IS CORRODED BETWEEN PILOTS BULKHEAD AND FRAME AT X167. REPAIRED IAW EA 2-53-689, SRM 51-20-16 AND SRM 51-40-11.Feb 24, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, Longeron/StringerSDR QXEA200600628Galley Track · corrodedPDX - C4 CHECK, GALLEY OUTBOARD MOUNT FLANGE IN AIRCRAFT IS CORRODED ON AFT END. REPAIRED IAW SRM 51-20-11 AND SRM 51-20-16, RD 8-53-8936.Feb 24, 2006 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200600617Bulkhead · chafedPDX C4 CHECK, RIGHT HAND NACELLE WHEEL WELL AFT BULKHEAD HAS CHAFED BETWEEN GRAVEL GUARD AND RECEPTACLES. REPAIRED IAW SRM 51-20-11, RD 8-54-2139 AND EA 2-54-253.Feb 24, 2006 · N349PH · Dhav DHC8202 · Nacelle/Pylon, Bulkhead/FirewallSDR QXEA200600652Frame · corrodedPDX - C4 CHECK, FRAME X151 IS CORRODED AT CASTELLATION BETWEEN STRINGER 31R AND 32R. REPAIRED IAW SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-11.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600651Frame · corrodedPDX - C4 CHECK, FRAME X167 IS CORRODED AT CASTELLATION BETWEEN STRINGER 30R AND 31R. REPAIRED IAW SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-11.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600650Frame · corrodedPDX - C4 CHECK, FRAME X167 IS CORRODED AT CASTELLATION BETWEEN STRINGER 32L AND 33L. REPAIRED IAW SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-11.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600649Frame · corrodedPDX-C4 CHECK, FRAME X167 IS CORRODED AT CASTELLATION BETWEEN STRINGER 28L AND 29L. REPAIRED IAW SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-11.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600648Frame · corrodedPDX-C4 CHECK, FRAME X167 HAS SMALL AREA OF CORROSION ON FORWARD SIDE JUST OUTBOARD OF STRINGER 29L. REPAIRED IAW SRM 51-20-16, SRM 51-00-04, SRM 51-20-36 AND SRM 51-20-11.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600653Frame · corrodedPDX - C4 CHECK, FRAME X167 IS CORRODED AT CASTELLATION BETWEEN STRINGER 31R AND 32R. REPAIRED IAW SRM 51-20-16, SRM 51-20-36 AND SRM 51-20-11.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600640Frame · corrodedPDX - C4 CHECK, FRAME AT X167 HAS CORRODED CASTELATION BETWEEN STRINGER 31L - 32L. REPAIRED IAW SRM 51-20-11, SRM 51-20-16, SRM 51-20-36 AND SRM 51-40-11.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600643Frame · corrodedPDX - C4 CHECK, FRAME AT X151 HAS CORRODED CASTELATION BETWEEN STRINGER 31L - 32L. REPAIRED IAW SRM 51-20-11, SRM 51-20-26, SRM 51-20-36 AND SRM 51-40-11.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600625Seat Track · corrodedPDX - C4 CHECK, RIGHT INBOARD SEAT TRACK INBOARD FLANGE HAS SCREW HOLES CORRODED AT X597, X580. REPAIRED IAW RD 8-53-4936.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200600626Seat Track · corrodedPDX - C4 CHECK, RIGHT HAND OUTBOARD SEAT TRACK CORRODED ON LUGS AND IN BOTTOM OF CHANNEL AT X266 - X269, X279, X299, AND X330. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200600627Stringer · corrodedPDX - C4 CHECK, STRINGER 33 UPPER AND LOWER FLANGES CORRODED BETWEEN X152 - X202. REPAIRED IAW SRM 51-20-11.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage Main, Longeron/StringerSDR QXEA20060624Seat Track · corrodedPDX-C4 CHECK, RIGHT HAND INBOARD SEAT TRACK AFT MOST SEGMENT CORRODED ON TOP AND INSIDE LUGS AT X597. REPAIRED IAW RD 8-53-4936.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA20060622Seat Track · corrodedPDX-C4 CHECK, RIGHT HAND INBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION IN CHANNEL AT X530 - X542. REPAIRED IAW RD 8-53-4936 AND SRM 51-20-16.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA20060619Seat Track · corrodedPDX-C4 CHECK, RIGHT HAND OUTBOARD SEAT TRACK HAS CORROSION AT X437 - X439, AND X501 - 505. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA20060620Seat Track · chafedPDX C4 CHECK, RIGHT OUTBOARD SEAT TRACK HAS CHAFE DAMAGE ON TOP OF LUGS AT X470. REPAIRED IAW RD 8-53-1342 AND SRM 51-20-16.Feb 23, 2006 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200600647Sill · gougedPDX-C4 CHECK, TWO GOUGES ON UPPER CARGO DOOR SILL, LOCATED BETWEEN TWO UPPER CARGO STEP PADS. REPAIRED IAW RD 8-53-7447.Feb 22, 2006 · N349PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200600631Flap Track · corrodedPDX - C4 CHECK, RIGHT HAND NR 3 FLAP TRACK HAS PITTING CORROSION ALONG THE LENGTH OF THE TRACKS, ALONG THE PATHS OF THE ROLLERS. REPAIRED IAW RD 8-57-987.Feb 22, 2006 · N349PH · Dhav DHC8202 · Trailing Edge FlapsSDR QXEA200600630Spar Cap · chafedPDX - C4 CHECK, RIGHT HAND WING FRONT SPAR, LOWER CAP IS CHAFED AT INBOARD ATTACH POINT FOR 611AR. REPAIRED IAW SRM 51-20-16, SRM 51-40-00 AND RD 8-57-811.Feb 22, 2006 · N349PH · Dhav DHC8202 · Wing Spar
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