N354PH, cancelled Jul 21, 2011

Service difficulty reports · 224

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 = 'N354PH' AND deregistration_id = 'N354PH-2011-07-21'
  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 QXEA200800285Attach Fitting · corrodedPDX - C5 - MCD LAY SHAFT FWD AND AFT GOOSE NECK ATTACH FITTINGS ARE PITTING AND CORRODED. REMOVED MCD LAY SHAFT REF -8/200 AMM 52-10-00FIG 501 SHEETS (3&4). REMOVED BOTH FWD AND AFT HINGE FITTINGS FROM FWD AND AFT TUBE ASSEMBLIES REF -8/200 SRM 51-40-11. INMar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Main, Attach FittingsSDR QXEA200800284Bracket · corrodedPDX - C5 - MCD SURROUND FWD END OF SILL PLATE BRACKET FOR SILL PLATE CORRODED AGAINST FUSELAGE. REMOVED THE MCD THRESHOLD BY DRILLING OUT THE RIVETS HOLDING THE THRESHOLD TO LOWER SILL PLATE, REMOVED NUTPLATES FROM THE LOWER SILL PLATE. BLENDED OUT CORROSIONMar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Main, Attach FittingsSDR QXEA200800283Sill · corrodedPDX - C5 - MCD SURROUND FWD SIDE OF SILL PLATE AREA, CORROSION AT SEAL INFLATION FEED THROUGH, IPC 52-05-00 FIG 5 ITEM 490. REMOVED MCD SEAL INFLATION TUBE AND REMOVED CORROSION AROUND HOLE REF RD8-53-8921. HFEC INSPECTION IAW -8/200 NDTM PART 6 51-00-01 ANDMar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800282Sill · corrodedPDX- C5 - CORROSION ON LOWER SURFACE OF MCD SILL PLATE STATION X250 AT AFT NUT PLATE. BLENDED TO REMOVE CORROSION IAW RD8-53-8921. HFEC INSPECTION OF BLENDED AREA IAW -8/200 NDTM PART 6 51-00-01, NO CRACKS NOTED. AREA IS WITHIN LIMITS, ETCH, ALODINE AND PRIMar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800272Bracket · crackedPDX - C5 - ANGLE BRACKET FORWARD OF STATION 600 AND INBOARD OF STRINGER 31R WEB UNDER FLOOR PANEL 441CZ IS CRACKED IN UPPER RADIUS. DRILLED OUT RIVETS IN THE ANGLE BRACKET. REMOVED IAW D8 200 SRM 51-10-21 PG 2 FIG 1. HFEC INSPECTED CUT AWAY FOR REMOVAL OF CMar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800270Attach Angle · corrodedPDX - C5 - CARGO BAY ENTRYWAY THRESHOLD ATTACHMENT ANGLE AT APPROXIMATELY STA 580.5 HAS CORROSION AROUND NUT PLATES. REMOVED CARGO BAY THRESHOLD PLATE BY REMOVING BOLTS AND SCREWS. REMOVED ANGLE BRACKET AND NUT PLATES BY REMOVING SOLID RIVETS. BLENDED CORROMar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800277Skin · chafedPDX - C5 - UPPER SURFACE OF LEFT INBOARD FLAP 5" AFT OF THE LEADING EDGE AT STATION YW139.00 IS CHAFED APPROXIMATELY .30" BY .35". BLENDED OUT CHAFE IAW -8 200 SRM 57-50-16 PG 2 TABLE 1. HFEC INSPECTED BLEND IAW-8 200 NDTM PART 6 51-00-01. NO CRACKS NOTED, Mar 6, 2008 · N354PH · Dhav DHC8202 · Trailing Edge FlapsSDR QXEA200800276Channel · dentedPDX - C5 - LOWER FORWARD EMERGENCY EXIT THRESHOLD CHANNEL PN 85320693 REQUIRES REPLACEMENT IN ACCORDANCE WITH EA 2-53-733 PERMANENT REPAIR FOR DENT IN CHANNEL. REMOVED FLOORBOARD SUPPORT CHANNEL ASSEMBLY AFT OF EMERGENCY EXIT AND EXIT THRESHOLD COVER PLATE. Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800275Floor Support · corrodedPDX - C5 - CORROSION ON FLOOR BOARD NUT PLATE FLANGE UNDER PANEL 144BZ AT STATION 199.5 INBOARD OF SEAT TRACK. REMOVED NUTPLATE, BLENDED OUT CORROSION IAW DASH 8 200 CPM CHAPTER 4, FOUND TO BE WITHIN LIMITS IAW DASH 8 200 SRM 51-20-11. ALODINED AND PRIMED BLEMar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800274Floorboard · corrodedPDX - C5 - CORROSION ON FLOORBOARD FLANGE UPPER SURFACE AT STATION 599.5 OUTBOARD OF STRINGER 28R TO END OF FLANGE. REMOVED NUT PLATE, BLENDED OUT CORROSION IAW DASH 8 200 CPM CHAPTER 4, BLENDED AREA WITHIN LIMITS IAW DASH 8 200 SRM 51-20-11. ALODINED AND PRMar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Floor PanelSDR QXEA200800269Threshold · chafedPDX - C5 - CARGO BAY ENTRYWAY THRESHOLD HAS SEVERAL AREAS OF LIGHT CHAFING. REPAIRED CHAFE BY BLENDING, MAX MATERIAL REMOVED WAS .005" WITHIN LIMITS REFERENCE TO D-8 200 SRM 51-20-11 .Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200701902Rod · brokenFLIGHT 2035. LT MAIN GEAR DOORS WERE OPEN WITH NO INDICATION FROM THE COCKPIT, ONLY THE LT SIDE OF THE DOOR IS OPEN. MAINTENANCE REPLACED THE SPRING, CONNECT ROD WHICH WERE BROKEN. AIRCRAFT RETURNED TO SERVICE.Dec 14, 2007 · N354PH · Dhav DHC8202 · Landing Gear Door Retract SectionSDR QXEA200701586Outflow Valve · malfunctionedSEA FLIGHT NR 2190 AT LEVEL FLIGHT CABIN DIFFERENTIAL PRESSURE GRADUALLY DECREASED FROM 5.4 PSID TO 0 PSID. UNABLE TO CONTROL CABIN PRESSURE IN MANUAL MODE. MAINTENANCE REPLACED THE FORWARD OUTFLOW VALVE. PRESSURIZED AIRCRAFT IN MANUAL. OPERATIONAL CHECK GOct 20, 2007 · N354PH · Dhav DHC8202 · Pressure Regulator/Outflow ValveSDR QXEA200701504Generator · malfunctionedYVR FLIGHT NR 2450, NR 1 AC GENERATOR CAUTION LIGHT WOULD NOT RESET PER CHECKLIST. FERRIED TO PDX. REPLACED NR 1 AC GENERATOR IAW 24-21-00-400-801. ALSO, REPLACED TRANSFORMERS, BOTH GCU'S AND RELAYS 2421-K1 AND K2. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNESep 25, 2007 · N354PH · Dhav DHC8202 · AC Generation SystemSDR QXEA200701410Pressure Switch · malfunctionedPDX FLIGHT NR 2107, 18 PSI BLEED AIR INDICATES 10 PSI WITH POWER LEVERS AT FLIGHT IDLE. INSTALLED NEW 55 AND 65 PSI SWITCHES IN BOTH RIGHT AND LEFT NACELLES IAW AMM 30-10-00-720-001. GROUND RAN BOTH ENGINES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERSep 10, 2007 · N354PH · Dhav DHC8202 · Airfoil Anti/De-ice SystemSDR QXEA200701166Smoke Detector · inoperativeSEA FLIGHT NR 2064, NR 1 ENGINE START SMOKE MASTER WARNING ILLUMINATED. NR 2 SMOKE DETECTOR INOP. PLACED ON MEL 372270. AIRCRAFT RETURNED TO SERVICE.Jul 18, 2007 · N354PH · Dhav DHC8202 · Smoke DetectionSDR QXEA200700963Lens · dislodgedSEA FLIGHT NR 2026 PLASTIC PIECE FELL OFF FROM CEILING ABOUT 6" LONG. REPORTED BY FLIGHT ATTENDANT. MAINTENANCE RESECURED SIDE WALL LIGHT LENS. PERFORMED GUI OF LENS. NO DEFECT NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Jun 14, 2007 · N354PH · Dhav DHC8202 · Passenger Compartment LightingSDR QXEA200700393Wire · chafedSEA FLIGHT 2070 SHORTLY AFTER LIFTOFF NR 2 DC GENERATOR DC GEN HOT CAUTION ILLUMINATED. CAUTION REMAINED ON FOR ENTIRE DURATION OF FLIGHT EVEN AFTER TURNING OFF NR 2 DC GENERATOR. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND WIRES, 77A20N, 715D20, 78A20, 76A16, Mar 18, 2007 · N354PH · Dhav DHC8202 · Electrical Power System WiringSDR QXEA200700361Generator · overheatedSEA FLIGHT NR 2116 - DURING TAXI, NR 2 DC GEN HOT CAUTION ILLUMINATED. AFTER TURNING OFF NR 2 DC GENERATOR (AS PER CHECKLIST) CAUTION EXTINGUISHED AFTER APPROXIMATELY 2 MINUTES. MAINTENANCE REPLACED NR 2 DC GENERATOR IAW MTC 9801001. PERFORMED FUNCTIONAL TEMar 11, 2007 · N354PH · Dhav DHC8202 · DC Generating SystemSDR QXEA200602066Galley · odiferousSEA FLIGHT NR 2054 ON DESCENT, AIRCRAFT SMELLS LIKE A DIRTY LAV. LAV FLUID HAS BEEN EXCHANGED TWICE, WARDROBE CLOSET HAS BEEN CLEANED. AIRCRAFT STILL SMELLS LIKE DIRTY LAV. REQUESTING BELLY DRAIN BR OPEN WS FOR ANY OVER FLOW FLUID TO ESCAPE. MAINTENANCE FOUNAug 13, 2006 · N354PH · Dhav DHC8202 · Buffet/GalleysSDR QXEA200600999Stop · wornPDX - C4 LEFT HAND UNDERWING EMERGENCY EXIT AFT UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126.Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200601000Stop · wornPDX - C4 LEFT UNDER WING EMERGENCY EXIT AFT LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126.Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200600998Stop · wornPDX - C4 LEFT UNDER WING EMERGENCY EXIT FORWARD UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126.Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200600997Stop · wornPDX - C4 LEFT UNDER WING EMERGENCY EXIT FORWARD LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126.Apr 7, 2006 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200600996Stop · wornPDX - C4 RIGHT UNDERWING EMERGENCY EXIT AFT LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126.Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200600995Stop · wornPDX - C4 RIGHT UNDERWING EMERGENCY EXIT AFT UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126.Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200600992Stop · wornPDX - C4 LEFT UNDER WING EMERGENCY EXIT AFT LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-52-350.Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200600991Stop · wornPDX - C4 LEFT UNDER WING EMERGENCY EXIT AFT UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-52-350.Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200600990Stop · wornPDX - C4 LEFT HAND UNDER WING EMERGENCY EXIT FORWARD LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-350.Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200600993Stop · wornPDX - C4 RIGHT HAND UNDERWING EMERGENCY EXIT FORWARD UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126.Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200600994Stop · wornPDX - C4 RIGHT HAND UNDER WING EMERGENCY EXIT FORWARD LOWER STOP WORN ON CONTACT. REPAIRED IAW RD 8-53-126.Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200600989Stop · wornPDX - C4 LEFT UNDER WING EMERGENCY EXIT FORWARD UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-350.Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200601001Stringer · corrodedPDX - C4 CORROSION FOUND ON STRINGER 32R ON AFT SIDE OF FRAME X151.600. REPAIRED IAW DHC-8-200 SRM 51-40-11 AND HORIZON AIR EA 2-53-375.Apr 6, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Longeron/StringerSDR QXEA200601003Skin · corrodedPDX - C4 CORROSION ON INTERNAL SKIN BAGGAGE COMPARTMENT JUST AFT OF DOOR CUTOUT FLOOR LEVEL. SEVERAL AREAS OF SURFACE CORROSION APPROXIMATELY X600-X535 AND STRINGER 23P. REPAIRED IAW RD 8-53-8998.Apr 5, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR QXEA200600938Threshold · dentedPDX - C4 DENT IN FORWARD EMERGENCY EXIT THRESHOLD HAS TRANSFER THROUGH TO INSIDE LYING STRUCTURE AT X248-249, YW40. REPAIRED IAW HORIZON AIR EA 2-53-733.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200600921Frame · corrodedPDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 31L AND 32L. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-21-10 AND SRM 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600925Frame · corrodedPDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 30R AND 31R. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND SRM 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600931Frame · corrodedPDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 30L AND 31L. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600924Frame · corrodedPDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 28L AND 29L. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600932Frame · corrodedPDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 29L AND 30L. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND SRM 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600930Frame · corrodedPDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 31L AND 32L. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600929Frame · corrodedPDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 32L AND 33L. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-21-10, 51-25-10 AND SRM 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600928Frame · corrodedPDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 30R AND 31R. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600923Frame · corrodedPDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 29L AND 30L. REPAIRED IAW DHC-82 SRM 51-00-02, 51-21-10, 51-25-10 AND 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600934Stringer · corrodedPDX - C4 STRINGER 31R APPEARS CORRODED WHERE PAINT IS MISSING AT STATION 175.0. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-00-04, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Longeron/StringerSDR QXEA200600926Frame · corrodedPDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 32R AND 33R. REPAIRED IAW DHC-8-200 SRM 51-40-11, 51-20-10 AND SRM 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600922Frame · corrodedPDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 30L AND 31L. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-20-11, 51-25-10 AND SRM 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600927Frame · corrodedPDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 31R AND 32R. REPAIRED IAW DHC-8-200 SRM 51-70-16, 51-40-11, 51-21-10, 51-25-10 AND SRM 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600933Frame · corrodedPDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 28L AND 29L. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200600915Sill · dentedPDX - C4 RIGHT FORWARD EMERGENCY EXIT LOWER SILL HAS DENT BY FORWARD DOOR LUG RECEPTACLE. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND HORIZON AIR EA 2-53-729.Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
Back to N354PH, cancelled Jul 21, 2011