1981 PIPER PA-31-350
N4105D is a 1981 PIPER PA-31-350 registered to GRANT AVIATION INC in ANCHORAGE, AK. Its FAA registration status is Valid. It has 3 NTSB accident records on file. 7 Airworthiness Directives may apply.
The PIPER PA-31-350 is registered with the FAA under N-number N4105D. This airframe was manufactured in 1981. Its manufacturer serial number is 31-8252027. The aircraft was issued its airworthiness certificate on 1982-02-10. The current registered owner is GRANT AVIATION INC, based in ANCHORAGE, AK. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.
Goodnews, AK, USA
Accident — Piper PA-31-350 (NTSB ANC04LA059)
EMMONAK, AK, USA
Accident — Piper PA-31-350 (NTSB ANC00LA133)
NOME, AK, USA
Accident — Piper PA-31-350 (NTSB ANC97LA041)
Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.
N4105D has been involved in 3 NTSB accidents since 1982. Each record above includes the date, location, severity, and NTSB summary. Buyers should review the full accident narratives and verify repairs in the aircraft's logbooks before purchase.
Airworthiness Directives; The New Piper Aircraft, Inc. Models PA-31, PA-31-300, PA-31-325, PA-31-350, PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, and PA-31P-350 Airplanes
This amendment adopts a new airworthiness directive (AD) that applies to all The New Piper Aircraft, Inc. (Piper) Models PA-31, PA- 31-300, PA-31-325, PA-31-350, PA-31P, PA-31T, PA-31T1, PA-31T2, PA- 31T3, and PA-31P-350 airplanes. This AD requires you to install an inspection hole (or use for inspection the tooling hole in the rudder bottom rib), conduct a detailed visual inspection of the rudder torque tube and associated ribs for corrosion, and, if corrosion is found, replace or repair the rib/rudder torque tube assembly. This AD is the result of reports of rudder tube corrosion. The actions specified by this AD are intended to detect and correct corrosion in the rudder torque tube assembly and rudder rib, which could result in failure of the rudder torque tube. This failure could lead to loss of rudder control.
Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N4105D may be affected by 7 directives. All applicable ADs must be complied with for the aircraft to remain legally airworthy. Buyers should verify AD compliance in the aircraft's logbooks before purchase.
+6 more Airworthiness Directives found for this aircraft
Full list, with effective dates and links to the official Federal Register documents, is included in the paid report.
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