Registered owner
Bird Acquisition LLC
Location
Phoenix, AZ
Owner type
LLC
Serial number
2843299
Year built
1999
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
November 23, 1999
Certificate issued
September 25, 2007
Expires
June 30, 2028
Mode S code
ACE0DF

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.

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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 N929PAMatched 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 N929PAMatched 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 FQAR20150520041Cylinder · crackedDURING A ROUTINE INSPECTION, A CRACK WAS SEEN AT THE LOWER SPARK PLUG HOLE OF THE NR 4 CYLINDER. AFTER THE CYLINDER WAS REMOVED, THE CRACK COULD BE SEEN IN THE INSIDE OF CYLINDER HEAD TO ONE SIDE OF THE LOWER SPARK PLUG HOLE. THE CYLINDER SHOWED NO INDICATIOMay 20, 2015 · N929PA · Piper PA28181 · Reciprocating Engine Cylinder SectionSDR FQAR20150520040Cylinder · crackedDURING A ROUTINE INSPECTION, SEVERAL CRACKS WERE SEEN AT THE LOWER SPARK PLUG HOLE OF THE NR 1 CYLINDER. AFTER THE CYLINDER WAS REMOVED, NUMEROUS CRACKS COULD BE SEEN IN THE INSIDE OF CYLINDER HEAD TO EITHER SIDE OF THE LOWER SPARK PLUG HOLE. THE CYLINDER SHMay 20, 2015 · N929PA · Piper PA28181 · Reciprocating Engine Cylinder SectionSDR FQAR20141222049Bracket · crackedDURING A PROGRESSIVE INSPECTION EVENT, A BRACKET WAS FOUND TO BE CRACKED BELOW WHERE THE FLAP HANDLE IS MOUNTED. THE BRACKET IN QUESTION IS LOCATED IN THE TUNNEL IN THE CENTER OF THE CABIN FLOOR AND USED TO MOUNT THE FLAP HANDLE ASSEMBLY. IT CONTAINS 2 NUT PDec 20, 2014 · N929PA · Piper PA28181 · Fuselage Main, Attach FittingsSDR FQAR20140417033Pump · low pressureDURING CLIMBOUT, NGINE SPUTTERED AND STOPPED. INSTRUCTOR PILOT WAS ABLE TO RESTART THE ENGINE AND THE ACFT RETURNED TO ITS DEPARTURE WITHOUT INCIDENT. MAINTENANCE RAN THE ENGINE ON THE GROUND AND NOTED THE FUEL PRESSURE TO BE LOW. REPLACING THE ELECTRIC FUApr 11, 2014 · N929PA · Piper PA28181 · Fuel Boost PumpSDR FQAR20140310028Housing · contaminatedDURING CRUISE FLIGHT, PILOT NOTED ENGINE RUNNING ROUGH AND LOST 50 RPM. LANDED. MAINTENANCE INSPECTED THE ACFT AND FOUND THE MAGNETO TIMING HOUSING TO BE CONTAMINATED WITH ENGINE OIL. REPLACED AND ENGINE RUNS REVEALED NO DEFECTS.Mar 6, 2014 · N929PA · Piper PA28181 · Magneto/Distributor

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