Location
Savoy, IL
Owner type
Government
Serial number
2843152
Year built
1998
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
June 22, 1998
Certificate issued
September 8, 1998
Expires
April 30, 2028
Mode S code
A4E619

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 60

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

1963In forceSuperseded2026
ADs by the year they took effect: 69 ADs
19631
19641
19661
19671
19692
19774
19793
19804
19821
19862
19893
19911
19921
19951
19964
19971
19982
19991
20001
20011
20042
20052
20065
20071
20083
20091
20103
20122
20131
20151
20161
20172
20182
20212
20221
20243
20261
See all 69 ADs

Information bulletins that may apply · 22

Advisory, not mandatory.

See all 24 bulletins

NTSB investigations

No NTSB investigations matched to N4145XMatched 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-28-181 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.

Service difficulty reports · 5

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

SDR 2002FA0000286Control Cable · wornDURING A ROUTINE INSPECTION THE RT AND LT FORWARD STABILATOR CABLE WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMILAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS FAIRLEADS OR ANY PLFeb 19, 2002 · N4145X · Piper PA28181 · Flight Control SystemSDR 2002FA0000285Control Cable · wornDURING A ROUTINE INSPECTION THE RT AND LT FORWARD STABILATOR CABLES WERE FOUND WORN AND FRAYED. THE AILERON RIGHT AND LEFT BALANCE CABLES WERE ALSO FOUND IN A SIMILAR CONDITION. THE WORN AND FRAYED PARTS OF THE CABLES WERE FOUND AT PULLEYS FAIRLEADS OR ANY PFeb 19, 2002 · N4145X · Piper PA28181 · Flight Control SystemSDR 20001017SH002Control Cable · frayedDURING A ROUTINE INSPECTION, THE LEFT AILERON BALANCE CABLE WAS FOUND FRAYED BY THE LEFT WING ROOT RIB. (X)Sep 14, 2000 · N4145X · Piper PA28181 · Aileron Control SystemSDR 20000504SH004Sensor · leakingSTATIC SYSTEM LEAK GREATER THAN 100 FEET/MINUTE TRACED TO THIS UNIT. AR850 ONLY TWO YEARS IN SERVICE SINCE AIRCRAFT WAS NEW. AR850''S ARE NOT KNOWN TO BE FAULTY IN THIS MANNER. SUBMITTER STATED POSSIBLE NARCO FACTORY DEFECT IN ASSEMBLY OF SENSOR. (X)Mar 9, 2000 · N4145X · Piper PA28181 · Altimeter, Barometric/EncoderSDR 20000407SH027Encoder · leakingINTERNAL LEAK IN ALTITUDE ENCODER GREATER THAN THE ALLOWED 100 FEET/MINUTE NON- PRESSURIZED AIRCRAFT. THESE ENCODERS ARE NORMALLY VERY REALIABLE, YET RECERTIFICATION SINCE PIPER AIRCRAFT INSTALLATION. POSSIBLE NARCO MANUFACTURE DEFECT IN ASSEMBLY OF PRESSUREMar 9, 2000 · N4145X · Piper PA28181 · Altimeter, Barometric/Encoder

STCs that may be installed · 369

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

See all 369 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N4145X before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.