- Registered owner
- Johnson Scott M
- Location
- Seminole, TX
- Owner type
- Individual
- Serial number
- 34-7770313
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- June 29, 1977
- Certificate issued
- August 7, 2019
- Expires
- August 31, 2029
- Mode S code
- AAF845
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 32
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1975 | 3 |
|---|---|
| 1977 | 1 |
| 1978 | 1 |
| 1979 | 1 |
| 1980 | 2 |
| 1986 | 2 |
| 1988 | 1 |
| 1992 | 2 |
| 1994 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 3 |
| 1999 | 2 |
| 2000 | 1 |
| 2003 | 1 |
| 2005 | 5 |
| 2006 | 1 |
| 2008 | 1 |
| 2010 | 1 |
| 2013 | 1 |
| 2022 | 1 |
| 2023 | 1 |
See all 34 ADs
Information bulletins that may apply · 13
Advisory, not mandatory.
Airframe · Piper PA-34-200T
SAIB AIR-21-10Wing, Attach Fittings (JASC 5740)SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-11-12R1Wings - PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach FittingSAIB CE-14-23Powerplant; Air IntakeSAIB CE-11-42Flight Controls: Control Cable/Pulley InspectionsSAIB CE-11-14Stabilizers- Vertical Stabilizer on Piper PA-28, PA-32, PA-34 Forward Attach Point CorrosionSAIB CE-11-13Wings - Piper PA-28, PA-32, PA-34 Forward Spar CorrosionSAIB CE-11-11Wings - Piper PA-28, PA-32, and PA-34 Aileron Hinge Fitting CorrosionSAIB CE-11-10Piper PA-28, PA-32, PA-34, and PA-44 Corrosion on Flap Hinges, Brackets, and RibsSAIB CE-11-01Stabilizers -Horizontal Stabilator TurnbuckleSAIB CE-09-23Fuel: Piper PA-28, PA-32, PA-34SAIB CE-09-15Landing Gear - Nose Gear Centering Attach BoltSAIB CE-08-13Electrical PowerHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N806BEMatched 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-34-200T aircraft
FAA incident reports
No FAA accident or incident reports matched to N806BEMatched 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-34-200T aircraft
Reports on N806BE not matched to an aircraft · 3
They name N806BE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Incident 19911118058179IBeech 1900 · New York, NYLanding gear relay circuit breaker popped. Gear lowered manually. Landed safely. Found a burned out pc board.Incident 19911118058169IBeech 1900 · Binghamton, NYLanding gear relay circuit breaker popped. Gear lowered manually. Found broken and shorted wire in wing root area.Incident 19910208005769IBeech 1900 · Philadelphia, PARed intransit light remained on after departure. Returned. Landed safely. Replaced landing gear uplock switch.
Service difficulty reports
No reports matched to N806BEGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Piper PA-34-200T aircraft
Reports on N806BE not matched to an aircraft · 4
They name N806BE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR PLG102195G2Py Line · crackedLGA - FLT 4727 - EN ROUTE, THE LEFT ENGINE SPOOLED TO 40 PERCENT N1. THE FLIGHT CREW SECURED THE ENGINE AND DIVERTED TO SWF LANDING WITHOUT INCIDENT. MAINTENANCE WAS NOTIFIED AND DISPATCHED TO THE AIRCRAFT. MAINTENANCE FOUND THE PY LINE BETWEEN THE FCU AND SDR PLGA316951Servo · malfunctionedAIRCRAFT HAD RUDDER CONTROL PROBLEMS. THE YAW DAMP COMPUTER AND SERVO WERE BOTH SENT OUT FOR REPAIR AND TESTING. THE COMPUTER WAS RETURNED FROM REPAIR WITH NO FAULT FOUND. THE SERVO WAS RETURNED FROM REPAIR WITH BEARINGS AND DRIVE TRAIN CLEANED AND GREASED.SDR 95ZZZZ227Servo Computer · malfunctionedBOS - AFTER T/O THE ACFT EXPERIENCED RUDDER CONTROL PROBLEMS. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED, LANDING WITHOUT INCIDENT. MX INSPECTION WAS PERFORMED WITH NO DEFECTS NOTED. ALL FLIGHT CONTROLS WERE CHECKED, NO DEFECTS WERE FOUND. BOTH ENGINE
STCs that may be installed · 280
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 280 STCs