- Registered owner
- Ttc Aircraft Leasing Inc
- Location
- Decatur, TX
- Owner type
- Corporation
- Serial number
- 441-0051
- Year built
- 1978
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- May 10, 1978
- Certificate issued
- April 1, 2021
- Expires
- April 30, 2028
- Mode S code
- A9B7C3
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every AiResearch TPE331 model are included below.
On this page
Airworthiness directives that may apply · 65
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 1 |
|---|---|
| 1974 | 2 |
| 1975 | 2 |
| 1976 | 1 |
| 1979 | 6 |
| 1980 | 3 |
| 1983 | 1 |
| 1984 | 3 |
| 1986 | 2 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1992 | 2 |
| 1993 | 4 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 2 |
| 1997 | 1 |
| 1998 | 5 |
| 2001 | 3 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 2 |
| 2008 | 2 |
| 2009 | 2 |
| 2011 | 1 |
| 2012 | 1 |
| 2015 | 2 |
| 2016 | 2 |
| 2018 | 4 |
| 2023 | 1 |
See all 77 ADs
Information bulletins that may apply · 9
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N725SVMatched 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
No FAA accident or incident reports matched to N725SVMatched 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 Cessna 441 aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2009FA0000410Mount Bracket · crackedDURING THE SID INSP THE NLG WAS REMOVED FOR INSP. THE RETRACT ACTUATOR UPPER MOUNT WAS FOUND CRACKED WHICH ALLOWED THE DOWNLOCK OVER-CENTER TENSION TO BE REDUCED. THERE IS NO REEQUIREMENT TO REMOVE THE NLG EXCEPT DURING THE SID INSP CALLED OUT IN THE LATEST SDR 2009FA0000405Hinge · corrodedDURING THE SID INSP THE UPPER CABIN DOOR WAS REMOVED FOR INSP. THE HINGE PIVOT BOLTS COULD NOT BE REMOVED BECAUSE THE BOLTS, BUSHINGS AND BRGS WERE ALL RUSTED SOLID. THIS CAUSED THE BOLTS TO PIVOT IN THE FUSELAGE STRUCTURE INSTEAD OF THE BRGS CAUSING EXCESSISDR 2009FA0000404Skin Panel · debondedDURING THE SID INSP, WITH THE HORIZONTAL STABILIZER REMOVED, DEBONDING WAS FOUND USING ULTRASOUND INSP ON THE BOTTOM CENTER WHERE THE LT AND RT PANELS ARE JOINED TOGETHER WITH FINGER DOUBLERS.SDR 2009FA0000403Pivot Assy · corrodedDURING THE SID INSP OF MLG TRAILING LINK THE PIVOT PIN WAS FOUND TO HAVE EXCESSIVE AMOUNTS OF RUST.SDR 2009FA0000401Drag Brace · damagedDURING THE SID INSP THE NLG WAS REMOVED FOR INSP. THE DRAG BRACE LT AND RT BRG PLATE HOLES WERE ALL FOUND EXCESSIVLY ELONGATED REQUIRING STRUCTURAL REPAIR. SUSPECT DAMAGE WAS CAUSED BY NORMAL TOWING OVER THE LIFE OF THE ACFT. THIS WOULD NOT BE DETECTED UNLESDR 2009FA0000400Bearing · looseWITH THE LT MAIN GEAR REMOVED FROM THE WING FOR SID INSP, THE AFT TRUNNION BRG WAS FOUND VERY LOOSE IN THE AFT TRUNNION SUPPORT.
STCs that may be installed · 200
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