- Registered owner
- Garmin International Inc
- Location
- Olathe, KS
- Owner type
- Corporation
- Serial number
- E-3763
- Year built
- 2007
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- March 7, 2007
- Certificate issued
- April 10, 2007
- Expires
- January 31, 2030
- Mode S code
- A1E910
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 28
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1987 | 1 |
|---|---|
| 1988 | 3 |
| 1991 | 1 |
| 1993 | 3 |
| 1996 | 1 |
| 1999 | 1 |
| 2000 | 1 |
| 2004 | 1 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 3 |
| 2010 | 1 |
| 2012 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2022 | 3 |
| 2023 | 6 |
See all 34 ADs
Information bulletins that may apply · 15
Advisory, not mandatory.
Airframe · Raytheon G36
SAIB CE-15-22Wing Leading Edge Hinge-Pin CorrosionSAIB CE-12-36Flight Controls: AileronSAIB CE-12-18Flight Controls: Elevator Control Cable ConditionSAIB CE-11-21Flight Controls: Trailing Edge Flaps; Flap Nose Rib CrackingSAIB CE-09-12Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 InstallationsEngine · Continental IO-550-B
SAIB NE-20-05POWERPLANT - Engine Camshaft Gear Tooth FractureSAIB NE-18-16POWERPLANT Alternator Drive CouplingSAIB NE-17-11POWERPLANT Engine damage as a result of kickbackSAIB NE-16-13Powerplant - Prohibited use of sealantSAIB NE-13-15Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control LeversSAIB NE-13-04Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing InspectionSAIB NE-10-09Reciprocating Engine Power Section: Hydraulic Valve LiftersSAIB NE-10-07Reciprocating Engine Cylinder: Identification Information for Superior Air Parts, PMA Cylinder Heads for Teledyne Continental Motors (TCM) IO-520, TSIO-520,and IO-550 Series Engines.SAIB NE-09-08Reciprocating Engine Cylinder SectionSAIB NE-07-09R1Periodic Inspections of ECi Cylinder Assemblies for Cracks in the Aluminum HeadNTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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 · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2012FA0000827Cylinder Head · crackedNR 1 CYLINDER HEAD CRACKED FROM THE SPARK PLUG HOLE TO THE INTAKE VALVE SEAT AND LEAKING EXHAUST EXTERNALLY.SDR 2008FA0000317Bolt · shearedTHE PILOT REPORTED A "POP" AS HE WAS GROUND HANDLING THE AIRCRAFT ON THE RAMP (IN A STRAIGHT DIRECTION USING AN AIRTUG). FURTHER INVESTIGATION REVEALED 1 NUT/BOLT COMBINATION HAD SHEARED ON THE INBOARD WHEEL HALF OF THE RIGHT MAIN LANDING GEAR ASSEMBLY. THE SDR 20080506FA001Bolt · shearedTHE PILOT REPORTED A "POP" AS HE WAS GROUND HANDLING THE AIRCRAFT ON THE RAMP (IN A STRAIGHT DIRECTION USING AN AIRTUG). FURTHER INVESTIGATION REVEALED 1 NUT/BOLT COMBINATION HAD SHEARED ON THE INBOARD WHEEL HALF OF THE RIGHT HAND MAIN LANDING GEAR ASSEMBLY.
STCs that may be installed · 176
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.