Location
Savoy, IL
Owner type
Government
Serial number
2843160
Year built
1998
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
July 31, 1998
Certificate issued
September 28, 1998
Expires
April 30, 2028
Mode S code
A4E636

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O&VO-360 model are included below.

On this page

Airworthiness directives that may apply · 70

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: 79 ADs
19631
19641
19661
19671
19692
19774
19794
19806
19811
19821
19862
19881
19893
19911
19921
19951
19964
19971
19982
19991
20001
20011
20021
20042
20053
20067
20071
20083
20091
20103
20122
20131
20151
20161
20172
20182
20212
20222
20243
20261
See all 80 ADs

Information bulletins that may apply · 26

Advisory, not mandatory.

See all 35 bulletins

NTSB investigations

No NTSB investigations matched to N4146RMatched 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

No FAA accident or incident reports matched to N4146RMatched 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-28-181 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 2008FA0000034Support · crackedFOUND CRACKED AFT ZEE ASSY PN 62664-000. THE ZEE ASSY IS RIVETED TO THE TOP FWD END OF TUNNEL PLATE PN 62601-003 AND AS AN ATTACHMENT POINT FOR THE RUDDER BAR SUPPORT ASSY PN 63451-000 USING 4 STANDARD AN3-4A BOLTS, WHICH ARE SECURED THROUGH NUTPLATES THAT AROct 12, 2007 · N4146R · Piper PA28181 · Rudder Control SystemSDR 2002FA0000374Cable · wornDURING A ROUTINE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLES WERE FOUND WORN. THE LEFT AILERON BALANCE CABLE WAS ALSO FOUND IN A SIMILAR CONDITION. THE WORN PARTS OF THE CABLE WERE FOUND AT PULLEYS, FAIRLEADS.Feb 27, 2002 · N4146R · Piper PA28181 · Aileron Control SystemSDR 2002FA0000373Cable · wornDURING A ROUTINE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLES WERE FOUND WORN. THE LEFT AILERON BALANCE CABLE WAS ALSO FOUND IN A SIMILAR CONDITION. THE WORN PARTS OF THE CABLE WERE FOUND AT PULLEYS, FAIRLEADS. PROBABLE CAUSE: SUBSTANDARD CABLE Feb 27, 2002 · N4146R · Piper PA28181 · Elevator Control SystemSDR 2002FA0000372Cable · wornDURING A ROUTINE INSPECTION THE RIGHT AND LEFT FORWARD STABILATOR CABLES WERE FOUND WORN. THE LEFT AILERON BALANCE CABLE WAS ALSO FOUND IN A SIMILAR CONDITION. THE WORN PARTS OF THE CABLE WERE FOUND AT PULLEYS, FAIRLEADS. PROBABLE CAUSE: SUBSTANDARD CABLE Feb 27, 2002 · N4146R · Piper PA28181 · Elevator Control SystemSDR 99ZZZX34Fan · malfunctionedCOOLING FAN PIPER P/N 460-105 PRODUCED NOISE THAT INTERFERES WITH THE PROPER OPERATION OF THE MARKER BEACON RECEIVER IN THE ACFT. THE PROBLEM SHOWS UP AS NOISE ON THE MARKER BEACON RECEIVER THAT LIGHTS THE IM LIGHT. THIS NOISE IS ALSO PRESENT ON THE NAVIGATIJul 12, 1998 · N4146R · Piper PA28181 · Air Distribution Fan

STCs that may be installed · 383

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

See all 383 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N4146R before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.