- Registered owner
- Rempert Erich A
- Location
- Lake Geneva, WI
- Owner type
- Individual
- Serial number
- NAV-4-16
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Experimental, research and development
- Airworthiness date
- January 17, 1968
- Certificate issued
- February 5, 2016
- Expires
- February 28, 2029
- Mode S code
- A03B73
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental O-470 model are included below.
On this page
Airworthiness directives that may apply · 40
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1962 | 1 |
|---|---|
| 1963 | 1 |
| 1967 | 1 |
| 1968 | 1 |
| 1969 | 2 |
| 1973 | 1 |
| 1979 | 2 |
| 1980 | 1 |
| 1981 | 1 |
| 1985 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1991 | 1 |
| 1993 | 2 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 1 |
| 2005 | 1 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 2 |
| 2022 | 3 |
| 2023 | 4 |
Airframe · Navion NAVION D
AD 2022-03-15Fuel Quantity IndicatorAD 2008-05-14Fuel systemAD 2005-01-19Mode S transpondersInformation bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Navion NAVION D
SAIB AIR-22-13Landing Gear ComponentsSAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-06-11R1Fuel system selector valvesEngine · Continental O-470 series
SAIB NE-20-05POWERPLANT - Engine Camshaft Gear Tooth FractureSAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-09-08Reciprocating Engine Cylinder SectionNTSB investigations
No NTSB investigations matched to N114EMatched 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 Navion NAVION D aircraft
FAA incident reports
No FAA accident or incident reports matched to N114EMatched 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 Navion NAVION D aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR N114ELControl Arm · separatedON THE RUDDER PEDAL ASSY, THE RUDDER CONTROL ARM ASSEMBLY, TRIM ARM BROKE OFF AT PARENT METAL SURROUNDING THE WELD POINT. PILOT REPORTED LOSS OF RUDDER TRIM INPUT. NO HISTORY OF PART REPLACEMENT. P/N 63457-003. 2879.3 HOURS TOTAL AIRCRAFT TIME. HAND TOW BASDR N114EL1Control Arm · separatedON THE RUDDER PEDAL ASSY, THE RUDDER CONTROL ARM ASSEMBLY , TRIM ARM BROKE OFF AT PARENT METAL SUROUNDING THE WELD POINT. PILOT REPORTED LOSS OF RUDDER TRIM INPUT. NO HISTORY OF PART REPLACMENT. P/N 63457-003. 2879.3 HOURS TOTAL AIRCRAFT TIME. HAND TOW BAR
Reports on N114E not matched to an aircraft · 2
They name N114E, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2015FA0000218Eec · malfunctionedRIGHT ENGINE ROLLED BACK IN FLIGHT TO FLIGHT IDLE. CREW SHUTDOWN ENGINE, UPON RESTART INFLIGHT THEY RECEIVED ENGINE CONTROL FAIL MESSAGE. ENGINE WOULD REMAIN IN FLIGHT IDLE WHEN THROTTLE WAS ADVANCED. ACFT LANDED WITHOUT INCIDENT. RT ENGINE EEC, FADEC, WAS SDR N114EL2Control Arm · separatedON THE RUDDER PEDAL ASSY, THE RUDDER CONTROL ARM ASSY, TRIM ARM BROKE OFF AT PARENT METAL SURROUNDING THE WELD POINT. PILOT REPORTED LOSS OF RUDDER TRIM INPUT. NO HISTORY OF PART REPLACEMENT. P/N 63457-003. 2879.3 HOURS TOTAL AIRCRAFT TIME. HAND TOW BAR FO
STCs that may be installed · 290
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Navion NAVION D
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 N114E before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.