- Registered owner
- Seas To See LLC
- Location
- Nacogdoches, TX
- Owner type
- LLC
- Serial number
- 42-5527004
- Year built
- 1984
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- February 14, 1985
- Certificate issued
- July 9, 2026
- Expires
- July 31, 2033
- Mode S code
- A4D7F7
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 11
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1986 | 2 |
|---|---|
| 1994 | 1 |
| 1996 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2009 | 1 |
| 2011 | 1 |
Airframe · Piper PA-42-1000
AD 2009-13-06 R1DoorsAD 2005-01-19Mode S transpondersAD 2004-08-15TAWS8000 terrain awareness warning systems (TAWS)AD 2000-14-08Pneumatic Deicing BootsAD 99-14-01AFM - Limitations Section - IcingAD 98-25-02Top-mounted AntennaAD 97-26-12AFM - Limitations Section - Power LeversAD 96-21-03Aileron Spar Crack InspectionAD 94-06-04Mask RegulatorsAD 86-21-10Pilots Operating Handbook/AFM ChangesAD 86-18-10Tip Tank Vent LinesSuperseded and historical ADs · 1
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Piper PA-42-1000
SAIB CE-01-30NTSB investigations
No NTSB investigations matched to N411BGMatched 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-42-1000 aircraft
FAA incident reports · 1
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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2020F00118Brace · crackedDURING A ROUTINE EVENT INSPECTION ON N411BG , 42-5527004 THE RIGHT
MAIN LANDING GEAR SIDE BRACE P/N 75245-015 WAS FOUND CRACKED, SEE PHOTOS
ATTACHED.
THIS PART HAS A LIFE LIMIT OF 3,000 HOURS , THE TIME IN SERVICE ON
THIS PART IS 2,601.6 THE PARTSDR 2007FA0000657Roll Pin · shearedPILOTS RT RUDDER PEDAL ROLL PINS SHEARED. REFERENCE IPC PN 761792, FIG. 103, INDEX 14, PN 480572. FAILURE MAY CAUSE LOSS OF DIRECTIONAL CONTROL OR BRAKING ACTION DURING GROUND OPERATION. (K)
STCs that may be installed · 86
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-42-1000
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