Owner type
LLC
Serial number
28R-8118011
Year built
1980
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
October 23, 1980
Certificate issued
November 8, 2016
Expires
November 30, 2029
Mode S code
AB520E

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 · 64

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
ADs by the year they took effect: 76 ADs
19641
19661
19672
19691
19721
19732
19751
19772
19781
19793
19803
19811
19822
19862
19892
19911
19921
19931
19941
19951
19964
19971
19983
20001
20011
20021
20032
20041
20052
20066
20071
20083
20091
20103
20111
20123
20131
20151
20171
20182
20212
20222
20242
20261
See all 78 ADs

Information bulletins that may apply · 26

Advisory, not mandatory.

See all 30 bulletins

NTSB investigations

No NTSB investigations matched to N8288LMatched 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-28RT-201 aircraft

FAA incident reports · 2

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 · 5

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

SDR 2020FA0000446Impulse Coupling · jammedDURING AN ENGINE RUN UP THE LEFT MAGNETO WAS OBSERVED TO BE NOT FIRING. UPON REMOVAL OF THE MAGNETO THE IMPULSE COUPLING WAS FOUND FAILED. ONE OF THE PAWLS WAS WEDGED BETWEEN THE PLATE OF THE COUPLING AND THE HOUSING OF THE MAGNETO. IT APPEARS THE RIVET ATTSep 14, 2020 · N8288L · Piper PA28RT201 · Magneto/DistributorSDR 2002FA0000520Impeller · wornDURING ANNUAL INSPECTION, FOUND OIL PUMP ASSEMBLY CONTAINED ALUMINUM DRIVEN IMPELLER AND INTERNAL IRON DRIVEN IMPELLER. AD REQUIRES REPLACEMENT OF THESE IMPELLERS. TBO, HAD MISTAKENLY BEEN CARRIED FORWARD. REPLACEMENT PAST DUE BY 690 HOURS AND 18 MONTHS. MODEApr 16, 2002 · N8288L · Piper PA28RT201 · Engine Oil Distribution (Airframe Furnished)SDR 2002FA0000519Muffler · damagedDURING ANNUAL INSPECTION, CRACK AROUND REAR MUFFLER LEFT HAND STEEL TUBE FOUND. STEEL TUBE AND MUFFLER INTERNAL FLAME TUBE COULD BE PULLED OUT OF MUFFLER END. BOTH MUFFLER INTERNAL FLAME TUBES FOUND DISTORTED, WHEN VIEWED FROM TAIL PIPE. REAR MUFFLER TT INApr 16, 2002 · N8288L · Piper PA28RT201 · Engine Noise SuppressorSDR 2002FA0000518Trunnion · brokenDURING ANNUAL INSPECTION, FOUND NOSE STRUT HOUSING BOSS WHERE LOWER DRAG LINK ATTACHES, BROKEN. HALF OF BOSS WAS MISSING, THE ASSEMBLY WAS SO COVERED WITH GREASE, MISSING PORTION OF BOSS WASNT VISABLE UNTIL CLEANED OFF. UNKNOWN HOW LONG HAD BEEN WHEN, SPECULApr 16, 2002 · N8288L · Piper PA28RT201 · Nose/Tail Landing GearSDR 2002FA0000517Nut · misinstalledDURING ANNUAL INSPECTION, MAIN AXLE NUTS WERE INSTALLED BACKWARDS. ONLY WAY COTTER KEY HOLES WOULD ALIGN, WAS TO BACK OFF NUT TO WHERE MAIN WHEEL WAS NOT TIGHT ON AXLE. ONLY THING RETAINING WHEEL ONTO AXLE WAS BRAKE ASSEMBLY. MAIN AXLE TABS WERE DEEPLY GROOApr 16, 2002 · N8288L · Piper PA28RT201 · Main Landing Gear Strut/Axle/Truck

STCs that may be installed · 345

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

See all 345 STCs