FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N354PH and the event date: up to this one’s cancellation.
Incident 20020713025289IClimb · Portland, OR(-23) Aircraft experienced roll control binding in flight. Pilot returned to field without incident. Maintenance troubleshot system and discovered safety wire pigtail rubbing on aileron servo motor cable guard assembly. Maintenance cut pigtail shorter and…Incident 19971109041439IGround Taxi, Other Airplane · Portland, ORAircraft was marshalled into a parked aircraft. Failure in communication between marshaller/wingwalker.
Service difficulty reports · 224
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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. INSDR 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 CORROSIONSDR 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 AND
See all 224 reportsOther aircraft with N354PH · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N354PH now.