N5ST1977 Beechcraft 200
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply10 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- De Paz Aviation LLC
- Owner type
- LLC
- City, state
- Coral Gables, FL
- Certificate issued
- May 15, 2023
- Expires
- May 31, 2030
- Airworthiness
- Standard · Normal
- Airworthiness date
- Sep 12, 1977
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
- 200
- Year
- 1977
- Serial number
- BB-289
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 11
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Mode S code
- A636E0
Engine
- Make and model
- P&W Canada Pt6a-60a
- Type
- Turbo-prop
- Power
- 1050 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2023 – nowDe Paz Aviation LLCCoral Gables, FL · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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 (5)
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 |
|---|---|---|---|
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (200)Certain serial numbers: 65-A90, B90, C90, C90A LJ-76; 65-A90, B90, C90, C90A LJ-114–LJ-1691; E90 LW-1–LW-347; F90 LA-2–LA-236; 99, 99A, A99A, B99, C99 U-1–U-239; 100, A100 B-1–B-94; … |
| 2002-23-13 | Pratt & Whitney Canada PT6A Series Turboprop Engines | Dec 31, 2002 | Engine (PT6A-60A)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed. |
| 98-20-38 | Raytheon Aircraft Company 200 Series Airplanes | Sep 29, 1998 | Airframe (200) |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (200) |
| 97-23-17 | Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as… | Dec 29, 1997 | Airframe (200)Certain serial numbers: C90 LJ-683–LJ-1463; C90A LJ-683–LJ-1463; E90 LW-177–LW-347; F90 LA-1–LA-236; H90 LL-1–LL-61; A100 B-228–B-247; … |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (10)
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.
- Wings · skin · crackedSep 26, 2014
REMOVED PREVIOUS REPAIR STRAP THAT WAS INBD OF CRACKED SKIN AT RIVET HOLE & FABRICATED NEW EXTENDED REPAIR STRAP TO INCORPORATE THREE EXTRA RIVET HOLES. THE NEW REPAIR STRIP IS MADE USING 0.050 INCH THICK 2024-T3 ALUMINUM. THE REPAIR STRIP & LE SKIN WERE PREPARED FOR BONDING & ATTACHED USING…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust stack · crackedJul 28, 2009
RIGHT ENGINE OUTBOARD EXHAUST STACK CRACKED. REMOVED RIGHT ENGINE OUTBOARD EXHAUST STACK PART NUMBER 78-00-00-20, SERIAL NUMBER 2203, DUE TO LARGE CRACK RUNNING 80 % AROUND THE CIRCUMFERENCE OF THE EXHAUST STACK AND REPLACED WITH NEW EXHAUST STACK PART NUMBER 78-00-00-20, SERIAL NUMBER 2004.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · fire warning · false activationNov 10, 2006
DURING CRUISE FLIGHT IN THE LATE EVENING, THE RT ENGINE FIRE WARNING LIGHT ILLUMINATED IN FLIGHT. THE FIGHT CREW CHANGED DIRECTION OF FLIGHT TO DETERMINE IF THE SUNLIGHT MIGHT BE CREATING A PROBLEM WITH THE PHOTOCELL. THE FIRE LIGHT DID NOT EXTINGUISH. THE FLIGHT DIVERTED TO THE NEAREST AIRPORT…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuel · fuel cap · leakingSep 5, 2006
AFTER TAKEOFF, THE PILOT NOTICED FUEL EXITING THE AIRCRAFT FROM THE RT WING FUEL CAP AREA. THE PILOT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RT FUEL CAP LANYARD TO BE PINCHED BETWEEN THE FUEL CAP AND THE FUEL INLET OPENING. THE LANYARD WAS PINCHED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · fire detector · shortedAug 9, 2005
AFTER THE PILOT GOT INTO THE AIRCRAFT TO PERFORM A TRIP AND TURNED ON THE MASTER SWITCH, THE ENGINE FIRE WARNING CIRCUIT BREAKER POPPED AND WOULD NOT RESET. THE TRIP WAS CANCELED AND THE AIRCRAFT WAS TURNED OVER TO MAINTENANCE. MAINTENANCE TROUBLESHOT AND FOUND THE LT AFT FIRE PROBE ON THE LEFT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Navigation · coupler · unsecureJul 22, 2005
DURING CLIMB TO ALTITUDE, THE PILOT ATTITUDE INDICATOR DISPLAYED A GYRO FLAG, THEN THE INDICATOR ROLLED TO THE OFF POSITION. THE AIRCRAFT RETURNED TO THE AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE WERE UNABLE TO FULLY DUPLICATE THE PROBLEM. WHILE WORKING ON THE SYSTEM AND MOVING THE 161E-1…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · fire detector · false activationJul 5, 2005
DURING THE AFTER CLIMBING THROUGH ABOUT 18,000 FEET, THE PILOT NOTICED A RED WARNING FLASHED BUT WENT BACK OFF BEFORE CAUSE WAS DETERMINED. A SHORT TIME LATER THE RIGHT ENGINE FIRE WARNING LIGHT CAME ON AND STAYED ON. THE PILOT COMPLIED WITH THE FIRE WARNING CHECKLIST AND DECIDED TO RETURN TO THE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · channel · crackedJul 26, 1999
DURING A PHASE INSPECTION, A CRACK WAS FOUND ON THE AFT END OF THE ENTRY DOOR BOTTOM CHANNEL WHERE THE DOOR HINGE HALF ATTACHES. THE CRACK WAS ABOUT 4 INCHES LONG AND WAS THROUGH THE AFT SET OF RIVETS. THE CHANNEL IS TO BE REPLACED WITH A NEW UNIT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · skin · crackedMar 4, 1999
DURING INSPECTION OF THE AIRCRAFT, DAMAGE TO THE LEFT SIDE OF THE RUDDER AT THE TRIM ACTUATOR CUT-OUT ON THE LEADING EDGE OF THE RUDDER WAS NOTICED. DAMAGE WAS THE RESULT OF WIND BLAST. INSPECTION OF THE DAMAGE REVEALED A .75 INCH CRACK NEAR THE TOP SIDE OF THE CUT-OUT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · rib · crackedDec 6, 1997
RIBS ON THE LEFT WING, ONE STRINGER AFT OF THE LEADING EDGE AT WS 56.50, WS 65.50, AND WS 85.00 ARE CRACKED WHERE THE STRINGER AND RIB ATTACH. THE CRACKS GO FROM THE RIVET HOLE FORWARD TO THE LEADING EDGE OF RIB SECTION. SUSPECT CRACKS ARE DUE TO THE FLEXING OF THE WING OVER TIME. REPAIRED BY…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026