- Registered owner
- Mob Aviation USA LLC
- Location
- Auburndale, FL
- Owner type
- LLC
- Serial number
- 2837009
- Year built
- 1988
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- December 19, 1988
- Certificate issued
- December 20, 2024
- Expires
- December 31, 2031
- Mode S code
- AAF957
From the FAA registry file of October 24, 2026.
On this page
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.
| 1977 | 1 |
|---|---|
| 1979 | 4 |
| 1980 | 3 |
| 1981 | 1 |
| 1982 | 1 |
| 1986 | 1 |
| 1989 | 1 |
| 1994 | 1 |
| 1996 | 2 |
| 1998 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2021 | 1 |
| 2022 | 1 |
| 2024 | 2 |
Airframe · Piper PA-28R-201
AD 2024-14-03Autopilot SystemAD 2024-10-04Wing, Attach FittingsAD 2022-03-15Fuel Quantity IndicatorInformation bulletins that may apply · 18
Advisory, not mandatory.
See all 19 bulletins
NTSB investigations
No NTSB investigations matched to N806NDMatched 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-28R-201 aircraft
FAA incident reports
No FAA accident or incident reports matched to N806NDMatched 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-28R-201 aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 98ZZZX1720Mount · crackedFOUND CRACK IN CLUSTER JUST BELOW LOWER LEFT ENGINE TO MOUNT ATTACH POINT. CRACK ORIGINATED FROM UNDERCUT WELD. MOUNT IS ORIGINAL ONE INSTALLED. INSTALLED NEW MOUNT (MOUNT REMOVED FOR REPAIR). CRACK FOUND DURING SCHEDULED INSPECTION.SDR 95ZZZX2178Rod End · wrong partDURING RAMP CHECK, FOUND SHIMMY DAMPER SHAFT ROD END BENT. FOUND CAUSE TO BE INCORRECT SHAFT INSTALLED. SHAFT LENGTH SHOULD BE APPROXIMATELY 6.450 INCHES WITHOUT ROD END. SHAFT INSTALLED WAS APPROXIMATELY 6.950 INCHES (LONGER SHAFTS ARE FOR PA-28-161 SHIMMYSDR 95ZZZX2185Bushing · wornFOUND FLAP HANDLE HORN HOLE AND BUSHING WORN. BUSHING WAS INSTALLED PER PIPER SB 965 ON 11-14-93. BUSHING STILL WEARS ON HORN REQUIRING HORN/HANDLE REPLACEMENT. SUGGEST BALL BEARING OR SWAGABLE BUSHING TO PREVENT HORN DAMAGE.
STCs that may be installed · 306
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-28R-201
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