Owner type LLC
Year built 1979
Type Fixed wing single engine
Engine Reciprocating
Airworthiness Standard, normal
Airworthiness date October 23, 1979
Certificate issued October 20, 2016
Expires October 31, 2029 From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming IO-540 model are included below.
On this page Registration Potential ADs 92 Information bulletins 30 NTSB investigations 1 FAA incident reports 1 Difficulty reports 7 Potential STCs 388 Related links Airworthiness directives that may apply · 92 Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
1963 2026 ADs by the year they took effect: 105 ADs 1963 1 1964 1 1966 1 1967 3 1968 2 1969 3 1970 2 1971 2 1972 3 1973 1 1974 3 1975 4 1976 1 1977 5 1978 3 1979 2 1980 4 1981 1 1982 1 1983 1 1986 1 1989 2 1992 1 1995 1 1996 5 1997 2 1998 4 1999 2 2000 1 2002 3 2003 2 2004 2 2005 3 2006 6 2007 1 2008 3 2009 1 2010 3 2011 1 2012 3 2013 1 2015 2 2017 2 2020 1 2021 1 2022 2 2023 1 2024 2 2026 2
See all 108 ADs NTSB investigations · 1 Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 1 FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 7 Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2004F00146 Points · failed INVESTIGATION OF MAGNETO FAILURE FOUND THAT THE CONTACT ARM OF THE PRIMARY POINT SET HAD SNAPPED OFF. THE BREAK OCCURED AT THE AREA WHERE THE STIFFENER FLANGES FLATEN OUT. JUST AT THE EDGE OF THE NYLON BLOCK. UNABLE TO DETERMINE CAUSE OF FAILURE. (AL0520040 May 17, 2004 · N8127K · Piper PA32300 · Magneto/Distributor SDR 2004F00144 Breaker Points · broken SLICK MAG MODEL NUMBER M3637 CONTACT POINTS BROKE. 10 HOURS SINCE NEW. May 17, 2004 · N8127K · Piper PA32300 · Magneto/Distributor SDR 2004FA0000836 Receiver · malfunctioned THIS RECEIVER WAS INSTALLED AS PART OF THE EFIS-SV SYSTEM. AFTER APPROXIMATELY 30 HOURS OF OPERATION FOLLOWING THE INSTALLATION, AN LOI MESSAGE DISPLAYED ON THE INTEGRATED DISPLAY UNIT (IDU). THE RECEIVER WAS REPLACED, AND THE ERROR MESSAGE WAS NO LONGER DIS Mar 29, 2004 · N8127K · Piper PA32300 · Global Positioning System SDR 98ZZZX3869 Blade · snapped WHILE AT CRUISE RPM, PILOT HEARD LOUD BANG FOLLOWED BY A SEVERE VIBRATION. REDUCING RPM MADE VIBRATION WORSE. A HIGHER RPM SETTING WAS USED AND AIRCRAFT RETURNED TO LAND SAFELY. UPON EXAMINATION, FOUND APPROXIMATELY 8 INCHES OF ONE PROPELLER BLADE SEPARATED Sep 1, 1998 · N8127K · Piper PA32300 · Propeller Blade Section SDR 98ZZZX3566 Impulse Coupling · loose SUBMITTER FOUND IMPULSE COUPLING RETAINER NUT LOOSE ON SHAFT WITH COTTER PIN STILL IN PLACE. THE IMPULSE ASSY COULD BE PULLED FROM TAPERED SHAFT WITH ONLY SLIGHT PRESSURE. A BLUEING COMPOUND WAS APPLIED TO THE TAPERED SHAFT AND THE IMPULSE ASSY WAS RESEATED. Aug 10, 1998 · N8127K · Piper PA32300 · Magneto/Distributor SDR 98ZZZX2986 Impulse Coupling · loose REMOVED MAGNETO FOR 400-HOUR IMPULSE INSPECTION. FOUND BOTH PAWL PINS HAD BECOME LOOSE ON IMPULSE BODY WITH ONE PIN NEARLY READY TO COME OUT OF ITS MOUNT HOLE. THIS WAS A NEW MAGNETO ASSY INSTALLED ON ENGINE AS A UNIT. Jul 17, 1998 · N8127K · Piper PA32300 · Magneto/Distributor SDR 98ZZZX9 Impulse Coupling · defective MAGNETO REMOVED AT 500 HOURS TIS DUE TO IMPULSE COUPLING DEFECT. Nov 1, 1997 · N8127K · Piper PA32300 · Magneto/Distributor STCs that may be installed · 388 Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piper PA-32-300 See all 388 STCs