1969 PIPER PA-28-180
N3331R is a 1969 PIPER PA-28-180 registered to EPIK INDUSTRIAL LLC in TERRE HAUTE, IN. Its FAA registration status is Valid. It has 5 NTSB accident records on file. 2 Airworthiness Directives may apply.
The PIPER PA-28-180 is registered with the FAA under N-number N3331R. This airframe was manufactured in 1969. Its manufacturer serial number is 28-5661. The aircraft was issued its airworthiness certificate on 1969-10-01. The current registered owner is EPIK INDUSTRIAL LLC, based in TERRE HAUTE, IN. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.
Sullivan, IN, USA
Accident — PIPER PA-28-180 (NTSB CEN22LA399)
Valparaiso, IN, USA
Accident — PIPER PA 28-180 (NTSB GAA16CA491)
Valparaiso, IN, USA
Accident — PIPER PA-28-180 (NTSB CEN09CA208)
LAPAZ, IN, USA
Accident — Piper PA-28-180 (NTSB CHI98LA329)
VALPARAISO, IN, USA
Accident — PIPER PA-28-180 (NTSB CHI89LA045)
Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.
N3331R has been involved in 5 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-28-160, PA-28-161, PA-28-180, and PA-28-181 Airplanes
The FAA adopts a new airworthiness directive (AD) for certain The New Piper Aircraft, Inc. (Piper) Models PA-28-160, PA-28-161, PA- 28-180, and PA-28-181 airplanes that incorporate Petersen Aviation, Inc. Supplemental Type Certificate (STC) SA2660CE installed between April 20, 1998, and April 1, 2005, and incorporate Petersen Aviation, Inc. Service Bulletin SB98-1. This AD requires you to replace the AN894-6-4 bushing screw thread expanders on the gascolator and bushing attached to the inlet of the top fuel pump with NAS1564-6-4J reducers and AN818-6 nuts. This AD results from reports of fuel leaks during the post STC installation tests. We are issuing this AD to prevent fuel fittings used in STC SA2660CE from leaking fuel in the engine compartment, which could result in an engine fire. This condition could lead to loss of control of the airplane.
Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N3331R may be affected by 2 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.
+1 more Airworthiness Directive 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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