- Registered owner
- Bird Acquisition LLC
- Location
- Phoenix, AZ
- Owner type
- LLC
- Serial number
- 2843116
- Year built
- 1998
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- January 6, 1998
- Certificate issued
- September 25, 2007
- Expires
- June 30, 2028
- Mode S code
- ACE32E
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
No FAA accident or incident reports matched to N9299BMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FQAR20171214101Battery · dischargedON RAMP WHEN STARTER BUTTON PUSHED, BATTERY WAS TOO LOW TO CRANK ENGINE. BATTERY WAS REMOVED AND CAPACITY TESTED; TEST REVEALED 84% CAPACITY. BATTERY INSTALLED NEW 3 WEEKS PRIOR.SDR FQAR20161020042Bracket · 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 FQAR20150527058Cylinder Head · crackedBORESCOPE EXAMINATION REVEALED THE NR 3 CYLINDER HEAD WAS CRACKED. AFTER THE CYLINDER WAS REMOVED, CRACKING WAS SEEN AT THE LOWER SPARK PLUG HOLE.SDR FQAR20150108003Indicator · inaccurateAFTER TAKEOFF, THE IP NOTED THE ACFT DID NOT PERFORM AS EXPECTED. THE IP AND STUDENT PROCEEDED TO THE PRACTICE AREA TO PERFORM SLOW FLIGHT AND STALLS. DURING SLOW FLIGHT WITH THE FLAPS FULLY EXTENDED, THE ACFT STALLED AT 55 KTS, 10 KTS HIGHER THAN SHOULD BE ESDR FQAR20140303026Carburetor · bindingDURING A GROUND ENGINE RUN, THE THROTTLE WAS OBSERVED TO GET STUCK DURING THROTTLE ADVANCEMENT. THIS KEPT THE OPERATOR FROM BEING ABLE TO BRING THE ENGINE PAST IDLE-1000 RPM. FURTHER INSPECTION REVEALED THE ISSUE TO BE FROM THE CARBURETOR ITSELF RATHER THAN TSDR VJ32002F00055Pump · failedDURING FLIGHT OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE. CHECKED SYSTEM FOR LEAKS AND CHECKED REGULATOR FOR PROPER OPERATION, ALL CHECKED WELL. SUSPECT PROBABLE CAUSE IS HEAT. NO RECOMMENDATION FOR CORRECTIVE ACTION AT THIS TIMESDR 2002FA0000717Magneto · failedROUGH ENGINE ON GROUND RUN, A MAGNETO CHECK WAS PERFORMED AND THE LEFT MAGNETO HAD EXCESSIVE MAGNETO DROP. MAGNETO WAS REMOVED AND A REPAIRED MAGNETO INSTALLED. MAGNETO OPERATION CHECK OF THE ENGINE WAS PERFORMED AND CHECKED NORMAL.SDR VJ32002F00046Magneto · inoperativeROUGH ENGINE ON GROUND RUN, A MAGNETO CHECK WAS PERFORMED AND THE LEFT MAGNETO HAD EXCESSIVE MAGNETO DROP. MAGNETO WAS REMOVED AND A REPAIRED MAGNETO INSTALLED. MAGNETO OPERATION CHECK OF THE ENGINE WAS PERFORMED AND CHECKED NORMAL.SDR 20000809SH020Control Cable · frayedLEFT AILERON BALANCE CABLE FRAYED, LOCATED UNDER THE REAR SEATS. (X)
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
Earlier aircraft with this N-number · 1
This aircraft carried N9299B before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.