Registered owner
Bird Acquisition LLC
Location
Phoenix, AZ
Owner type
LLC
Serial number
2843307
Year built
1999
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
December 13, 1999
Certificate issued
September 25, 2007
Expires
June 30, 2028
Mode S code
ACB5A9

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 30

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

1977In forceSuperseded2026
ADs by the year they took effect: 35 ADs
19772
19793
19803
19862
19891
19962
19991
20001
20011
20041
20052
20062
20082
20091
20101
20131
20151
20161
20171
20182
20211
20221
20242
See all 35 ADs

Information bulletins that may apply · 17

Advisory, not mandatory.

See all 18 bulletins

NTSB investigations

No NTSB investigations matched to N918PAMatched 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 · 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 · 7

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

SDR FQAR201807313044Wire · chafedDURING A SCHEDULED INSPECTION, FOUND THE POWER WIRE FOR THE SLICK START, BADLY DETERIATED WITH NUMEROUS BARE SECTIONS OF WIRE EXPOSED. THE WIRE APPEARS TO BE AUTOMOTIVE TYPE WIRE AND WAS SUPPLIED BY CHAMPION AS PART OF THE INSTALLATION KIT.Jul 30, 2018 · N918PA · Piper PA28181 · Electrical Power System WiringSDR FQAR20170702061Sensor · failedPILOTS REPORTED THE FUEL LEVEL WOULD INDICATE FULL EVEN WHEN TANK WAS HALF EMPTY. TESTING OF SENSOR REVEALED THAT AT CERTAIN FUEL LEVELS THE SENSOR WOULD INDICATE FULL; WHEN AT/NEAR ZERO.Jul 1, 2017 · N918PA · Piper PA28181 · Fuel Quantity SensorSDR FQAR20170331012Support Channel · crackedDURING AN INSPECTION, STRUCTURE THAT HOLDS THE PARKING BRAKE AND HANDLE WAS FOUND CRACKED. STRUCTURE IN QUESTION IS A CHANNEL THAT RUNS BETWEEN THE FIREWALL AFT FACE AND INSTRUMENT PANEL FWD FACE. CRACKING WAS SEEN IN THIS CASE ON THE AFT END OF THE CHANNEL, IMar 31, 2017 · N918PA · Piper PA28181 · Fuselage Miscellaneous StructureSDR FQAR20161019037Bracket · crackedWHEN THE ELT WAS REMOVED, THE TECH DETERMINED THE ELT MOUNTING BRACKET WAS CRACKED IN FOUR PLACES. THE CRACKS WERE ON EITHER SIDE OF TWO NUTPLATES USED TO MOUNT THE ELT MOUNTING TRAY. THE ELT MOUNTING TRAY HIDES THE CRACKS FROM VISUAL DETECTION.Oct 19, 2016 · N918PA · Piper PA28181 · Fuselage Main, Attach FittingsSDR FQAR20150105003Bracket · crackedDURING A PROGRESSIVE INSPECTION EVENT, A BRACKET WAS FOUND 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 IS USED TO MOUNT THE FLAP HANDLE ASSEMBLY. IT CONTAINS NUT PLATES TJan 3, 2015 · N918PA · Piper PA28181 · Fuselage Main, Attach FittingsSDR FQAR201307102385Throttle Arm · bindingON INSPECTION OF THROTTLE LEVER ON CARBURETOR, FOUND TO STICK INTERMITTENTLY. NO EXTERNAL DAMAGE OR CONDITION WAS FOUND TO BE CAUSE OF THIS FAILURE.Apr 16, 2013 · N918PA · Piper PA28181 · Fuel Control/Reciprocating EnginesSDR FQA2003F00002Channel · crackedDURING A HARD LANDING INSPECTION, A MECHANIC NOTED THE AFT STIFFENING CHANNEL, PN 62086-003 CRACKED ON THE LEFT, LOWER, SKIN NEAR THE WING ROOT. THE CRACK APPEARS OLD. THE LEFT WING FORWARD STIFFENING CHANNEL WAS NOT DAMAGED.Feb 13, 2003 · N918PA · Piper PA28181 · Fuselage Miscellaneous Structure

STCs that may be installed · 333

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

See all 333 STCs