Registered owner
Chandler Air Service Inc
Location
Chandler, AZ
Owner type
Corporation
Serial number
2843121
Year built
1998
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
February 2, 1998
Certificate issued
June 9, 2016
Expires
June 30, 2029
Mode S code
A4E5EE

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 · 2

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

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 · 6

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

SDR 2012FA0000272Tube · defectiveHAD RIGHT TIRE FLATTEN WHILE ON LANDING, AFTER A TRAINING MISSION. THE ACFT CAME SAFELY TO A STOP AND MX REPLACED THE TIRE/WHEEL ASSY. UPON DISASSEMBLY OF THE AFFECTED TIRE/ WHEEL ASSY, IT WAS DISCOVERED THAT THE TUBE HAD A MFG DEFECT. A SMALL HOLE NOT CREApr 12, 2012 · N4144P · Piper PA28181 · Tire TubeSDR 2003FA0000749Diode · failedPILOT REPORTED ALTERNATOR INOPERATIVE. LIGHT STAYED ON AND AMP METER SHOWED 28 AMPS. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT A DIODE HAD FAILED INSIDE THE ALTERNATOR.Jun 4, 2003 · N4144P · Piper PA28181 · DC Generator-AlternatorSDR 2003FA0000728Oil Cooler · crackedFOUND OIL LEAK DURING PREFLIGHT BY STUDENT PILOT. PRESSURE CHECKED OIL COOLER AND FOUND OIL LEAK AT TOP SEAM. THIS IS A WEAK AREA ON THE COOLER. MAY BE CAUSED BY VIBRATION OR IMPROPER INSTALLATION METHODS.Jun 4, 2003 · N4144P · Piper PA28181 · Engine Oil CoolerSDR 2003FA0000574Oil Cooler · crackedFOUND OIL LEAK ON PREFLIGHT INSPECTION BY STUDENT PILOT. PRESSURE CHECKED OIL COOLER LEAKING AT SEAM ON TOP. THIS IS A WEAK AREA ON THE OIL COOLER, COULD BE CAUSED BY VIBRATION AND NOT USING A BACK UP WRENCH WHEN INSTALLING OIL COOLER HOSES. RECOMMEND FINDIMay 15, 2003 · N4144P · Piper PA28181 · Engine Oil CoolerSDR 20000911SH032Control Cable · frayedTRIM CABLE FRAYED AT REAR DRUM. (X)Aug 21, 2000 · N4144P · Piper PA28181 · Flight Control SystemSDR 20000809SH023Control Cable · frayedRIGHT AILERON BALANCE CABLE FRAYED. LOCATED UNDER THE REAR SEATS. (X)Jul 25, 2000 · N4144P · Piper PA28181 · Aileron Control System

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 N4144P before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.