Owner type
Corporation
Serial number
31-8352028
Year built
1983
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
August 10, 1995
Certificate issued
December 1, 2018
Expires
December 31, 2028
Mode S code
A0233F

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming TI0-540 model are included below.

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Airworthiness directives that may apply · 106

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

1969In forceSuperseded2026
ADs by the year they took effect: 125 ADs
19691
19711
19731
19741
19754
19763
19777
19784
19797
19806
19812
19832
19841
19851
19861
19871
19892
19912
19922
19932
19942
19951
19968
19974
19985
19993
20002
20012
20023
20032
20043
20054
20066
20084
20092
20102
20113
20125
20132
20152
20162
20173
20221
20231
20241
20261
See all 129 ADs

Information bulletins that may apply · 13

Advisory, not mandatory.

Historical bulletins · 2

NTSB investigations

No NTSB investigations matched to N108JLMatched 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-31-350 aircraft

FAA incident reports

No FAA accident or incident reports matched to N108JLMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Piper PA-31-350 aircraft

Service difficulty reports · 5

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

SDR 1SMA20220726001Link Assy · crackedWHILE PERFORMING NOSE LANDING GEAR LINK ASSEMBLY PN:40336-00 INSPECTION 500 HOUR REPETITIVE INSPECTION PER PIPER SERVICE LETTER NO. 1088 A CRACK INDICATION WAS FOUND DURING 10X MAGNIFYING VISUAL INSPECTION. CRACK CONFIRMED DURING LIQUID PENETRANT INSPECTION.Jul 26, 2022 · N108JL · Piper PA31350 · Landing Gear SystemSDR 1SMA20220717001Filter Housing · crackedDURING APPROACH PHASE WHEN ATTEMPTING TO EXTEND THE LANDING GEAR, THE GEAR FAILED TO FULLY EXTEND WITH THE ENGINE DRIVEN PUMPS. PILOT SUCCESSFULLY EXTENDED GEAR USING THE EMERGENCY EXTENSION HANDLE. AFTER LANDING POST FLIGHT REVEALED SIGNIFICANT AMOUNT OF HYDRJul 17, 2022 · N108JL · Piper PA31350 · Hydraulic System, MainSDR 2022F00297Filter Housing · crackedDURING APPROACH PHASE WHEN ATTEMPTING TO EXTEND THE LANDING GEAR, THE GEAR FAILED TO FULLY EXTEND WITH THE ENGINE DRIVEN PUMPS. PILOT SUCCESSFULLY EXTENDED GEAR USING THE EMERGENCY EXTENSION HANDLE. AFTER LANDING POST FLIGHT REVEALED SIGNIFICANT AMOUNT OF HYDRJul 17, 2022 · N108JL · Piper PA31350 · Hydraulic System, MainSDR 1SMA201611250001Piston Ring · brokenDURING DESCENT, LT ENGINE CYLINDER HEAD TEMP FROM 390 DEGREES F TO APPROXIMATELY ONE NEEDLE WIDTH BELOW RED LINE OBSERVED. TO KEEP TEMP BELOW RED LINE, MIXTURE WAS GRADUALLY INCREASED UNTIL FULL RICH JUST BEFORE CHECKS. DURING CHECKS, LEFT ENGINE OIL PRESSURENov 25, 2016 · N108JL · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR 1SMA2015F00028Bearing · seizedDURING APPROACH TO LANDING, PILOT SELECTED LANDING GEAR LEVER TO DOWN POSITION. GEAR POSITION INDICATORS SHOWED NLG AND LT MLG DOWN AND LOCKED. NO DOWN AND LOCKED INDICATION FOR RT GEAR. GEAR UNSAFE "RED" LIGHT REMAINED ILLUMINATED AND LANDING GEAR SELECTORJan 19, 2015 · N108JL · Piper PA31350 · Landing Gear Retraction/Extension System

STCs that may be installed · 300

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

See all 300 STCs