- Registered owner
- Surdex Corp
- Location
- Chesterfield, MO
- Owner type
- Corporation
- Serial number
- 441-0358
- Year built
- 1986
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Restricted, aerial surveying
- Airworthiness date
- April 12, 2007
- Certificate issued
- October 5, 2005
- Expires
- September 30, 2028
- Mode S code
- A54B09
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 41
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1979 | 4 |
|---|---|
| 1980 | 1 |
| 1983 | 1 |
| 1984 | 1 |
| 1986 | 2 |
| 1992 | 2 |
| 1993 | 2 |
| 1995 | 2 |
| 1996 | 2 |
| 1997 | 1 |
| 1998 | 4 |
| 2001 | 3 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 1 |
| 2008 | 2 |
| 2009 | 2 |
| 2011 | 1 |
| 2012 | 1 |
| 2016 | 1 |
| 2018 | 4 |
| 2023 | 1 |
See all 48 ADs
Information bulletins that may apply · 7
Advisory, not mandatory.
Airframe · Cessna 441
SAIB CE-14-11R1Landing Gear; Nose Landing Gear TrunnionsSAIB CE-13-22Electrical Power System Circuit Breaker SwitchSAIB CE-10-01Fuel: Fuel Tank Selector Valve SystemsSAIB CE-06-46R1SAIB ACE-99-05Engine · Honeywell TPE331-10N
SAIB NE-16-19Turbine Engine Compressor Section Stator Nozzle DistressSAIB NE-16-18Power Lever Loss of Power ControlHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N440EHMatched 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 Cessna 441 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 2026FA0000788Engine · failedDURING CRUISE FLIGHT AT FL290, ONE HOUR AFTER TAKEOFF, RIGHT ENGINE TORQUE QUICKLY FELL TO ZERO AND REMAINED, NO OSCILLATIONS. SIMULTANEOUSLY, RIGHT ENGINE EGT INCREASED TO BEYOND RED LINE AND REMAINED, NO OSCILLATIONS. AIRCRAFT YAWED AND BEGAN TO LOSE ALTITUDSDR 2009FA0000481Line · crackedHYDRAULIC FLUID DEPLETION HAVE OCCURRED. (TWO WERE FLAP FAILURE TO EXTEND AND ONE THE LANDING GEAR HAD TO BE EXTENDED USING THE EMERGENCY EXTENSION SYS. THESE FAILURES WERE CAUSED BY A CRACK AND LEAK FORMING IN A .3750 ALUM ALLOY HYDRAULIC LINE AT A BEND RAD
STCs that may be installed · 182
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 441
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