N933AC1985 Beechcraft 400
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 19829 ADs may apply1 service difficulty report
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 18, 2026- Last registered owner
- Stratos Aircraft INC
- Owner type
- Corporation
- City, state
- Redmond, OR
- Certificate issued
- Mar 2, 2016
- Canceled
- Sep 6, 2019
- Airworthiness
- Standard · Normal
- Airworthiness date
- Sep 17, 1985
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
- Beechcraft
- Model
- 400
- Year
- 1985
- Serial number
- RJ-05
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 9
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Mode S code
- ACF0D1
Engine
- Make and model
- Ama/Expr Unknown Eng
- Type
- Turbo-fan
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2016 – 2019Stratos Aircraft INCRedmond, OR
- 1998 – 2001T & T LLCTucson, AZ · different airframe: 1965 Piper Pa-32-260 S/N 32-164
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 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 (9)
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 |
|---|---|---|---|
| 2014-21-06 | Flight Controls | Nov 28, 2014 | Airframe (400)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–RK-604; 400T TT-1–TT-180; 400T TX-1–TX-13; MU-300 A003SA–A093SA |
| 2014-15-15 | Stabilizers | Sep 5, 2014 | Airframe (400)Certain serial numbers: MU-300 A003SA–A093SA; 400 RJ-1–RJ-65; 400A RK-1–RK-604; 400T TT-1–TT-180; 400T TX-1–TX-13 |
| 2009-07-02 | Hawker Beechcraft Corporation Model MU-300-10 Airplanes and Model 400 and 400A Series… | Apr 30, 2009 | Airframe (400)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–RK-93; MU-300-10 A1001SA–A1011SA; MU-300 A003SA–A091SA |
| 2006-21-02 | Raytheon (Beech) Model 400, 400A, and 400T Series Airplanes; and Raytheon (Mitsubishi)… | Oct 25, 2006 | Airframe (400) |
| 2006-15-16 | Raytheon (Beech) Model 400 and 400A Series Airplanes | Sep 5, 2006 | Airframe (400)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–RK-23. Only with: Kit P/N 128-3004-1 P or 128-3004-3 P (Lucas Aerospace/Goodrich DC Starter Generator) has been incorporated. |
Show all 9 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2002-01-23 | Raytheon Model Beech 400, 400A, and 400T Series Airplanes; Model Beech MU-300-10… | Feb 14, 2002 | Airframe (400)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–on; 400T TT-1–TT-180; 400T-1 TX-1–TX-11; MU-300-10 A1001SA–A1011SA; MU-300 A003SA–A091SA |
| 2001-24-11 | Raytheon Model Beech 400, 400A, and 400T Series Airplanes, Model Mitsubishi MU-300… | Dec 11, 2001 | Airframe (400) |
| 99-21-26 | Raytheon (Beech) Model 400, 400A, 400T, and MU-300-10 Airplanes | Nov 22, 1999 | Airframe (400)Certain serial numbers: 400A RK-1–RK-107 |
| 98-06-30 | Raytheon (Beech) Model 400, 400A, 400T, MU-300, and MU-300-10 Airplanes | Apr 24, 1998 | Airframe (400)Serial numbers per AlliedSignal Aerospace Service Bulletin 103570-21-4012, Revision 1. Only with: Equipped with AlliedSignal outflow/safety valves identified in AlliedSignal Aerospace Service Bulletin 103570-21-4012, Revision 1. |
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.
- Air conditioning and pressurization · clamp · looseFeb 25, 2013
AFTER TAKEOFF. EMERGENCY PRESSURIZATION SYS ACTIVATED. AFTER LANDING, MECHANICS FOUND CLAMP ON RUBBER HOSE JOINT LOOSE ALLOWING AIR TO ESCAPE NEAR DUCT PRESSURE SENSOR. TIGHTENED CLAMP AND GROUND RUN AND TEST FLIGHT GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026