- Registered owner
- Szm LLC
- Location
- Laconia, NH
- Owner type
- LLC
- Serial number
- E-3925
- Year built
- 2010
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- February 11, 2010
- Certificate issued
- April 3, 2013
- Expires
- April 30, 2029
- Mode S code
- A15B75
Hawker Beechcraft G36TCDS 3A15Airframe · Hawker Beechcraft G36TCDS E3SOEngine · Continental IO-550-B
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 |
Airframe · Hawker Beechcraft G36
AD 2023-10-02Indicating/Recording System, NavigationAD 2022-03-15Fuel Quantity IndicatorAD 2009-15-01Wire harness/connector(s)Information bulletins that may apply · 15
Advisory, not mandatory.
Airframe · Hawker Beechcraft 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
No NTSB investigations matched to N187JMatched 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 Hawker Beechcraft G36 aircraft
FAA incident reports
No FAA accident or incident reports matched to N187JMatched 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 Hawker Beechcraft G36 aircraft
Service difficulty reports
No reports matched to N187JGeneral 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 Hawker Beechcraft G36 aircraft
Reports on N187J not matched to an aircraft · 2
They name N187J, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 97ZZZX2366Mount · chafedDURING ROUTINE INSPECTION, DISCOVERED THE RIGHT ENGINE MOUNT TRUSS HAD BEEN CHAFED BEYOND ALLOWABLE LIMITS IN TWO PLACES BY A NR 8 STAINLESS STEEL HARD OIL SCAVAGE RETURN LINE. SUBMITTER ADVISES OTHERS WITH KA-B-100'S TO CHECK THIS AREA OF MOUNT TRUSS. THE CSDR 97ZZZX2356Strut · crackedNOSE LANDING GEAR STRUT UPPER BODY CASTING HAS A CRACK FROM THE LEFT LOWER GREASE FITTING TO THE BOTTOM OF THE BODY CASTING. A DISTANCE OF .3125 INCH LONG. SUBMITTER ADVISES OTHERS TO CHECK THIS AREA.
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.