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N3327M

Open the Markdown

1977 Piper PA-28R-201 · Lycoming I0360 series

Open in FAA registry

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Registered owner
Nearhoof Jeremy R
Location
The Woodlands, TX
Owner type
Individual
Serial number
28R-7837112
Year built
1977
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
January 5, 1978
Certificate issued
September 23, 2020
Expires
September 30, 2027
Mode S code
A3A096
Piper PA-28R-201Airframe model · 4 seats · 1 engine · 352 registeredTCDS 2A13Airframe · Piper PA-28R-201TCDS 1E10Engine · Lycoming I0360 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming I0360 model are included below.

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Airworthiness directives that may apply · 72

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1964In forceSuperseded2026
See all 89 ADs

Information bulletins that may apply · 29

Advisory, not mandatory.

See all 33 bulletins

NTSB investigations

No NTSB investigations matched to N3327MMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Piper PA-28R-201 aircraft

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.

Incident 19850114012529ILevel Off Touchdown · Niles, INNose wheel failed to extend for landing. Ice accumulation on leading edges.Jan 14, 1985 · Minor damage

Service difficulty reports · 3

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 20001109SH029Lifter · wornAFTER FINDING FINE FERROUS METAL IN OIL FILTER , FURTHER INVESTIGATION LED TO THE FAILED CAMSHAFT AND TAPPETS. BOTH TAPPETS RIDE ON THE SAME LOBE. SUBMITTER STATED THESE WERE RECONDITIONED PARTS. (X)Oct 17, 2000 · N3327M · Piper PA28R201 · Reciprocating Engine Power SectionSDR 20001109SH028Camshaft · wornAFTER FINDING FINE FERROUS METAL IN OIL FILTER , FURTHER INVESTIGATION LED TO THE FAILED CAMSHAFT AND TAPPETS. BOTH TAPPETS RIDE ON THE SAME LOBE. SUBMITTER STATED THESE WERE RECONDITIONED PARTS. (X)Oct 17, 2000 · N3327M · Piper PA28R201 · Reciprocating Engine Power SectionSDR 99ZZZX2637Plug · failedTHIS ENGINE EXPERIENCED A PROPELLER OVERSPEED REQUIRING REDUCTION TO 18 INCHES OF MP TO RETURN TO MAXIMUM RPM. INSTALLING AN OVERHAULED GOVERNOR DID NOT CORRECT THE PROBLEM. PRESSURIZING THE OIL PASSAGE TO THE PROPELLER IAW LYC SI 1462 GAVE AN ACCEPTABLE DIFJun 28, 1999 · N3327M · Piper PA28R201 · Propeller Controlling System

STCs that may be installed · 361

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 361 STCs