- Registered owner
- De Paz Aviation LLC
- Location
- Coral Gables, FL
- Owner type
- LLC
- Serial number
- BB-289
- Year built
- 1977
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- September 12, 1977
- Certificate issued
- May 15, 2023
- Expires
- May 31, 2030
- Mode S code
- A636E0
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 56
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 1 |
|---|---|
| 1975 | 3 |
| 1976 | 5 |
| 1977 | 4 |
| 1978 | 1 |
| 1979 | 1 |
| 1980 | 2 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 1 |
| 1992 | 2 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 4 |
| 1998 | 4 |
| 2003 | 3 |
| 2004 | 3 |
| 2005 | 6 |
| 2006 | 1 |
| 2008 | 3 |
| 2022 | 1 |
| 2023 | 1 |
| 2025 | 1 |
See all 58 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N5STMatched 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 Beech 200 aircraft
FAA incident reports · 2
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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CIER2014092601Skin · crackedREMOVED 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 PRESDR CIEA200900010Exhaust Stack · crackedRIGHT 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 SDR CIEA200600009Fire Warning · false activationDURING 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 SDR CIEA200600006Fuel Cap · leakingAFTER 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 INSDR CIEA200500017Tach Generator · defectiveSHORTLY AFTER TAKEOFF, THE PILOT NOTICED THE LT PROP RPM DROPPING. THE OTHER ENGINE INSTRUMENTS DID NOT SEEM TO BE AFFECTED, BUT THE PILOT THOUGHT THE ENGINE WAS LOOSING POWER. THE AIRCRAFT RETURNED AND LANDED AT THE SAME AIRPORT AS THE TAKEOFF. THE AIRCRAFSDR CIEA200500014Fire Detector · shortedAFTER 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 FOSDR CIEA200500010Coupler · unsecureDURING 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 WORKSDR CIEA200500009Fire Detector · false activationDURING 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 WARNINGSDR CIEA200500002Connector · bentSHORTLY AFTER TAKEOFF, THE ENGINE INSTRUMENT AND AUDIO PANEL CIRCUIT BREAKER POPPED. THE AIRCRAFT WAS FLYING AT NIGHT. THE AIRCRAFT RETURNED TO THE AIRPORT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A STUD FOR THE LIGHT PANEL ON THE AVIONICS OVERLAY TO BSDR CIEA200500001Connector · bentSHORTLY AFTER TAKEOFF, THE ENGINE INSTRUMENT AND AUDIO PANEL CIRCUIT BREAKER POPPED. THE AIRCRAFT WAS FLYING AT NIGHT. THE AIRCRAFT RETURNED TO THE AIRPORT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A STUD FOR THE LIGHT PANEL ON THE AVIONICS OVERLAY TO BSDR 99ZZZX3394Channel · crackedDURING 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.SDR 99ZZZX3417Skin · crackedDURING 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 SDR 98ZZZX626Rib · crackedRIBS 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
STCs that may be installed · 415
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 200
STC SA4175NMInstallation of fully enclosed main landing gear door system for high-flotation- gear-equipped aircraft.STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller