N440DA1981 Cessna 441
This N-number isn't registered right now. Below is its last known registration, canceled Sep 6, 2019.
Safety record in brief:No NTSB accidents or incidents since 198210 ADs may apply1 service difficulty report
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Texas Turbine Conversions INC
- Owner type
- Corporation
- City, state
- Denison, TX
- Certificate issued
- Mar 1, 2016
- Canceled
- Sep 6, 2019
- Airworthiness
- Standard · Normal
- Airworthiness date
- Mar 27, 2008
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Cessna
- Model
- 441
- Year
- 1981
- Serial number
- 441-0207
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 10
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A54AE9
Engine
- Make and model
- Honeywell Tpe331-8
- Type
- Turbo-prop
- Power
- 715 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2016 – 2019Texas Turbine Conversions INCDenison, TX
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (10)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2018-22-01 | Turbine Section | Dec 10, 2018 | Engine (TPE331-8)Only with: Second stage turbine rotor assemblies P/N 3102106-1, -6, -8 or P/N 3101514-1, -10, -12 installed. |
| 2018-13-05 | Turbine Engine Reduction Gear | Jul 26, 2018 | Engine (TPE331-8)Only with: Hydraulic torque sensor gear assemblies P/Ns 3101726-1, -2, or -3 installed. |
| 2018-02-14 | Turbine Engine Combustion Section | Feb 28, 2018 | Engine (TPE331-8)Only with: Combustion chamber case assemblies P/Ns 869728-x, 893973-x, 3101668-x, or 3102613-x (any dash number) installed. |
| 2016-18-17 | Honeywell International Inc. Turboprop and Turboshaft Engines | Nov 4, 2016 | Engine (TPE331-8)Only with: With 2nd stage compressor impeller P/N 893482-1 through -5 inclusive, or P/N 3107056-1 or 3107056-2, installed. |
| 2005-20-25 | The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411… | Nov 9, 2005 | Airframe (441)Certain serial numbers: 401 655; 401 401-0001–401-0322; 401A 655; 401A 401A0001–401A0132; 401B 401B0001–401B0221; 402 402-0001–402-0322; …. Only with: Equipped with an avionics bus circuit breaker switch P/N CM3589-50, 593-250-101, 593-250-102, W31-X2M5A-50, or W31-X1000-50. |
Show all 10 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2003-09-09 | Cessna Aircraft Company Models 441 and F406 Airplanes | Jun 24, 2003 | Airframe (441)Certain serial numbers: 441 0001–0362; 441 698; F406 0001–0089 |
| 2002-25-02 | Honeywell International Inc. TPE331-3, -5, -6, -8, -10, and -11 Series Turboprop and… | Jan 21, 2003 | Engine (TPE331-8) |
| 98-04-28 | Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414… | Mar 13, 1998 | Airframe (441) |
| 97-25-04 | Cessna Aircraft Company Models 208, 208A, 208B, 425, and 441 Airplanes | Jan 21, 1998 | Airframe (441) |
| 95-25-10 | Cessna Model 441, 500, 550, and 560 Series Airplanes | Jan 22, 1996 | Airframe (441)Serial numbers per Allied Signal Aerospace Service Bulletins 103576-21-4054, 103576-21-4056, and 103648-21-4055. Only with: Equipped with Allied Signal outflow/safety valves identified in Allied Signal Aerospace Service Bulletins 103576-21-4054, 103576-21-4056, and 103648-21-4055. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Fuselage · structure · misoverhauledJul 11, 2013
PERFORMED A PHASE 2, 3, & D, TASK A361004, BLEED AIR LINE EXHIBITED CORROSION WHERE ITS FLANGE FASTENS TO THE FUSELAGE SKIN BS 187.87 RBL 27, AND WL 62.79. ON DISASSEMBLY, FLANGE TO FUSELAGE JOINT FOUND WITH HEAVY DISSIMILAR METAL CORROSION. INVESTIGATION FOUND THAT DURING A PRIOR MX EVENT, DUCT…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026