- Registered owner
- Bird Acquisition LLC
- Location
- Phoenix, AZ
- Owner type
- LLC
- Serial number
- 2843499
- Year built
- 2001
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- November 19, 2001
- Certificate issued
- September 25, 2007
- Expires
- June 30, 2028
- Mode S code
- A55708
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O-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.
| 1963 | 1 |
|---|---|
| 1964 | 1 |
| 1966 | 1 |
| 1967 | 1 |
| 1969 | 2 |
| 1977 | 4 |
| 1979 | 4 |
| 1980 | 6 |
| 1981 | 1 |
| 1982 | 1 |
| 1986 | 2 |
| 1988 | 1 |
| 1989 | 3 |
| 1991 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 7 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2021 | 2 |
| 2022 | 2 |
| 2024 | 3 |
| 2026 | 1 |
Airframe · Piper PA-28-181
AD 2024-14-03Autopilot SystemAD 2024-10-04Wing, Attach FittingsAD 2022-03-15Fuel Quantity IndicatorInformation bulletins that may apply · 26
Advisory, not mandatory.
See all 35 bulletins
NTSB investigations · 1
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.
Incident 20170917019539ILanding: Touchdown · Deer Valley, AZAircraft operated by trans-pac (bird acquisition LLC) 141 pilot school (fqas) at Deer Valley Airport (dvt). Student was on solo flight with 38 hours total time. Third class medical student certificate #4023898. During a hard landing at Deer Valley Airport…Accident 20110104000079ATaxi · Wickenburg, AZDuring first solo cross country from deer valley airport (dvt) to deer valley airport (dvt) with landings in gila bend AZ, (E63) and Wickenburg, AZ (E25). The pilot completed a landing and full stop in Wickenburg AZ (E25). Pilot needed to exit the aircraft at…
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FQAR20180919049Wire · deterioratedDURING A SCHEDULED INSPECTION, FOUND THE POWER WIRE FOR THE START BADLY DETERIORATED WITH NUMEROUS BARE SECTIONS OF WIRE EXPOSED. THE WIRE APPEARS TO BE AUTOMOTIVE TYPE WIRE AND WAS SUPPLIED AS PART OF THE INSTALLATION KIT.SDR FQAR2018083003047Pan · crackedDURING A SCHEDULED INSPECTION, THE OUTER DOOR PAN WAS FOUND TO BE CRACKED ABOVE THE WING SPAR CUT OUT, WHEN THIS HAS BEEN FOUND BEFORE, WE ALSO FIND THE FOREWARD SPAR CARRY THRU CRACKED INSIDE THE FUSELAGESDR FQAR20180830046Rib · crackedDURING AN INSPECTION, FOUND TWO WING RIBS CRACKED, IN THE LT WING AT WS 106.19, AND 86.03. THE RIBS WERE REMOVED AND REPLACED.SDR FQAR20180830045Rib · crackedDURING AN INSPECTION, FOUND TWO WING RIBS CRACKED IN THE LT WING AT WS 86.03 AND 106.19, THE RIBS REMOVED AND REPLACED.SDR FQAR20180315022Channel · crackedDURING A REPAIR FOR ANOTHER ISSUE, CRACKS WERE FOUND IN THE FWD DOOR CHANNEL LOCATED AT BS 72.6, CRACKS WERE LOCATED ON THE AFT SIDE OF THE EYE BOLT BUSHINGS, BUSHINGS ARE LOCATED INSIDE THE CHANNEL. THIS AREA IS VERY HARD TO INSPECT DUE TO RESTRICTED ACCESS, SDR FQAR20180315021Pan · crackedDURING AN EVENT INSPECTION, FOUND A CRACK ON INSIDE AFT CORNER OF THE DOOR PAN ABOVE THE SPAR CARRY THRU AT BS 108, WL 30, REPLACED BOTH INNER AND OUTER DOOR PANS, DURING THE REPAIR OF THE DOOR PAN, THE FORWARD DOOR CHANNEL AT BS 72.6 WAS FOUND TO BE CRACKED SDR FQAR20170607034Bracket · crackedDURING A PROGRESSIVE INSPECTION, 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 ASSY. IT CONTAINS NUT PLATES TO ALLOW TSDR FQAR20161027046Bracket · crackedDURING A ROUTINE INSPECTION, AN ANGLE IN THE LEFT WING THAT IS LOCATED WITH THE OUTBOARD FLAP MOUNTING BRACKET WAS FOUND TO BE CRACKED THROUGH THE RIVETS.SDR FQAR20151003100Oil Cooler · leakingDURING A ROUTINE INSPECTION, FRESH OIL WAS FOUND SPRAYED AROUND ON THE INSIDE OF THE ENGINE COWLING. INSPECTION REVEALED THE OIL COOLER WAS THE SOURCE OF THE LEAKAGE. IT HAD BEEN INSTALLED ON THE ACFT 5 MONTHS AT THE TIME OF FAILURE.SDR FQAR20150528063Tappet · flattenedDURING THE REMOVAL OF A CYLINDER, THE TECH WAS TRYING TO REMOVE THE HYDRAULIC LIFTER ASSY WHEN HE FELT SOMETHING ROUGH INSIDE THE CRANKCASE. VISUAL INSPECTION REVEALED THE CYLINDER-FACING END OF THE NR 4 CYLINDER EXHAUST TAPPET WAS IN PIECES. THERE HAD BEEN SDR FQAR20150119006Tube · leakingWHEN THE ACFT LANDED WITH THE INTENTION OF PERFORMING A TOUCH AND GO, THE PILOTS BECAME AWARE OF A VIBRATION THAT INCREASED TO A SEVERE RATTLING OF THE AIRFRAME. THE IP DECIDED TO BRAKE, ABORTING THE TAKEOFF, AND REALIZED THE ACFT WAS SUFFERING FROM A DEFLATEDSDR FQAR20141222050Bracket · 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 P
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.
Airframe · Piper PA-28-181
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller