- Registered owner
- Bird Acquisition LLC
- Location
- Phoenix, AZ
- Owner type
- LLC
- Serial number
- 2843304
- Year built
- 1999
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- December 7, 1999
- Certificate issued
- October 1, 2007
- Expires
- September 30, 2028
- Mode S code
- ACAA84
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.
| 1963 | 1 |
|---|---|
| 1964 | 1 |
| 1966 | 1 |
| 1967 | 1 |
| 1969 | 2 |
| 1977 | 4 |
| 1979 | 3 |
| 1980 | 4 |
| 1982 | 1 |
| 1986 | 2 |
| 1989 | 3 |
| 1991 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 5 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 2 |
| 2018 | 2 |
| 2021 | 2 |
| 2022 | 1 |
| 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 · 22
Advisory, not mandatory.
See all 24 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.
Accident 20170814010649AChandler, AZAircraft landed on runway 4L, and lost directional control. Aircraft crossed over to the other runway where the pilot taxied to the taxiway l. he then stopped, shut down the aircraft and ran across an active runway to his instructor.Incident 20061206028709IRoll-Out (Fixed Wing) · Phoenix, AZ(-23) Student pilot was performing landings on rwy 7L. He came in for landing and overshot the landing touch down area. The aircraft was on the ground and slowing as he neared taxiway B9. The pilot attempted to turn off the runway at that taxiway but realized…
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FQAR20180321024Selector Valve · stuckPILOT REPORTED THE FUEL SELECTOR VALVE WAS STUCK IN THE RT TANK POSITION, CHECKED THE VALVE, FOUND CONDITION TO BE INTERMITTENT, REPLACED FUEL VALVE WITH NEW.SDR FQAR20170201006Rib · crackedDURING A ROUTINE INSPECTION, A RIB IN THE RIGHT WING WAS FOUND TO BE CRACKED. RIB IN QUESTION IS BETWEEN MAIN WING SPAR AND WING AFT SPAR, 4TH RIB OUTBOARD FROM THE WING ROOT (WING STA 64.59). CRACK WAS DIFFICULT TO SEE DUE TO LACK OF INSPECTION PANELS IN VICISDR FQAR20170201005Rib · crackedDURING A ROUTINE INSPECTION, A RIB IN THE RIGHT WING WAS FOUND TO BE CRACKED. THE RIB IN QUESTION IS BETWEEN MAIN WING SPAR AND WING AFT SPAR, 5TH RIB OUTBOARD FROM THE WING ROOT (WS 86.03).SDR FQAR20161020041Nut Plate · crackedWHEN THE ELT WAS BEING REMOVED FOR INSPECTION, THE TECH DISCOVERED TWO, TWO INCH CRACKS NEXT TO THE NUTPLATES IN THE ELT MOUNTING BRACKET. THESE CRACKS CAN ONLY BE SEEN WHEN THE ELT TRAY IS REMOVED.SDR FQAR20160908030Angle · crackedDURING A ROUTINE INSPECTION, AN ANGLE IN THE RIGHT WING THAT IS CO-LOCATED WITH THE OUTBOARD FLAP MOUNTING BRACKET WAS FOUND TO BE CRACKED THROUGH THE RIVETS.SDR FQAR2012021500925Distributor Gear · failedRIGHT MAGNETO FAILED AFTER CLIMBING TO ALTITUDE. FOUND RT MAGNETO DISTRIBUTOR GEAR HAD FAILED. METAL PLATE THAT ATTACHES TO THE MIDDLE OF THE GEAR AND EXTENDS TO THE EDGE HAD COME OFF. THIS PIECE WAS LOCATED INSIDE THE MAGNETO. UPON FURTHER INSP, THE MAGNE
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.
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