- Registered owners
- David Aviation Inc DBAKing Air Nation
- Location
- Brandon, MS
- Owner type
- Corporation
- Serial number
- BC-61
- Year built
- 1978
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- May 8, 2000
- Certificate issued
- July 17, 2024
- Expires
- July 31, 2031
- Mode S code
- A8541F
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.
On this page
Airworthiness directives that may apply · 54
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1975 | 1 |
| 1976 | 2 |
| 1977 | 1 |
| 1978 | 2 |
| 1980 | 4 |
| 1985 | 1 |
| 1986 | 1 |
| 1987 | 1 |
| 1989 | 1 |
| 1990 | 2 |
| 1992 | 3 |
| 1994 | 2 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 3 |
| 1998 | 5 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 3 |
| 2004 | 2 |
| 2005 | 6 |
| 2008 | 1 |
| 2011 | 2 |
| 2012 | 1 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 60 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Beech A200
SAIB CE-12-36Flight Controls: AileronNTSB investigations
No NTSB investigations matched to N636BMatched 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 A200 aircraft
FAA incident reports
No FAA accident or incident reports matched to N636BMatched 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 Beech A200 aircraft
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR K5L2014F00001Indicator · failedDURING CLIMB THROUGH 4000 FT, THE CAPTAIN SIDE ATTITUDE INDICATOR FLAGGED "GYRO", THEN STARTED INDICATING A BANK TO THE LEFT. CAPTAIN CALLED THE FAILURE AND POSITIVE EXCHANGE OF CONTROLS OCCURRED BETWEEN PILOT AND CO PILOT. CO PILOTFLEW THE RETURN , INTERCEPSDR K5L20140110000001Flap Track · tornAIRCRAFT WAS CLEARED TO LAND AND ON A CLOSE LT DOWNWIND, CIRCLING AT 140 KNOTS FROM A GPS13 APPROACH, CONFIGURED WITH FLAPS SET AT APPROACH AND GEAR SELECTED DOWN. CAPTAIN`S COMMANDED FULL FLAPS. WHEN THEY WERE SELECTED THE FLAPS EXTENDED ONLY TO APPROXIMATESDR K5L2012F00002Fire Detector · failedON SHORT FINAL APPROACH THE LEFT ENGINE FIRE DETECTOR T-HANDLE LIGHT ILLUMINATED. PILOT MADE A NORMAL LANDING AND NO SMOKE WAS NOTICED. PULLED AND RESET CIRCUIT BREAKER AND LIGHT EXTINGUISHED. MADE NORMAL SHUTDOWN. MX OPENED COWLS AND NO SIGN OF ANY FIRE SDR K5L2012F00001Fire Detector · failedON SHORT FINAL APPROACH, THE LT ENGINE FIRE DETECTOR T HANDLE LIGHT ILLUMINATED. PILOT MADE NORMAL LANDING AND NO SMOKE WAS NOTICED, PULLED AND RESET CIRCUIT BREAKER AND LIGHT EXTINGUISHED. MADE NORMAL SHUTDOWN. MX OPENED COWLS AND NO SIGN OF ANY FIRE WAS NSDR 2009FA0000292Flow Valve · failedDURING CLIMB TO ALTITUDE CABIN FAILED TO MAKE MAXIMUM DIFFERENTIAL PRESSURE AND HAD A HIGHER THAN NORMAL CABIN. FOUND A P3 AIR TUBE DISSCONNECTED AT RT HEAT EXCHANGER IN RT WING. ON MX FLIGHT FOUND LT FLOW CONTROL VALVE WEAK. REPLACED DUCT AND FLOW CONTROL VALSDR K5LA050908001Bellcrank · twistedDRUING A ROUTINE PHASE 3 INSPECTION, IT WAS FOUND THAT THE MAIN CABIN DOOR AFT UPLOCK BELLCRANK WAS TWISTED ABOUT 10 DEGREES FROM WHAT A NEW ONE IS.. ALSO THE BOLT PN NAS110321D THAT THE UPLOCK BRACKET PIVOTS ON WAS DEFORMED SLIGHTLY. THIS WAS PROBABLY CAUSED SDR K5L2007F00002Power Supply · failedAWAITING TAKEOFF, PILOT TURNED ON CABIN LIGHTS AND NOTICED SMOKE FUMES IN COCKPIT AND CABIN. TURNED OFF VENT BLOWED AND CABIN LIGHTS AND RETURNED TO RAMP. IT WAS DETERMINED THAT THE POWER SUPPLY (BALLAST) HAD FAILED AND CAUSED THE SMOKE. POWER SUPPLY WAS RESDR K5L2007F00001Actuator · inoperativeDESCENDING, PILOT SELECTED ICE VANES EXTENDED AND ONLY THE LT ONE EXTENDED. PULLED CIRCUIT BREAKER AND SLOWED AIRCRAFT AND EXTENDED RT ICE VANE WITH THE MANUAL EXTENSION HANDLE. REPLACED RT ICE VANE ACTUATOR MOTOR. (K)SDR 2007FA0000785Sensor · faultyAT APPROXIMATELY 1635 LOCAL, IN CLOUDY CONDITIONS, ON A MAINTENANCE TEST FLIGHT, THE NR 1 ENGINE FIRE LIGHT BRIEFLY ILLUMINATED, THEN EXTINGUISHED. ALL ENGINE GAUGES INDICATED NORMALLY. ALREADY IN DESCENT, THROUGH 4,500 FT, AND CONTINUED TO A SAFE LANDING. SDR K5L2007F00000Windshield · failedWHEN IN CRUISE FLIGHT AT FL210 AND -42 DEGREES C, THE INNER PANE ON THE CO-PILOTS WINDSHIELD SHATTERED. NO PIECES BROKE LOOSE AND NORMAL DESCENT AND SAFE LANDING WERE MADE AT KLEB. THERE WAS NO LOSS OF CABIN PRESSURE. LAST INSPECTION WAS 3 MONTH AND 100 HOUSDR K5L2005F00002Shutoff Valve · failedAFTER NORMAL ENGINE START, DURING RUN UP NOTICED THAT THE LEFT INSTRUMENT SHUTOFF VALVE PN 101381000-9 WOULD NOT CLOSE WHEN SELECTED OFF. FOUND VALVE SOLENOID TO BE AT FAULT AND INSTALLED OVERHAULED VALVE. RUN UP AND OPS CHECKED NORMAL. (K)SDR K5L2005F00001Fuse · failedSELECTED APPROACH FLAPS DESCENDING, FLAPS FAILED TO EXTEND. RESET CIRCUIT BREAKER AND CYCLED FLAP SELECTOR BUT STILL NO FLAP MOVEMENT. MADE UNEVENTFUL NO FLAP LANDING. AFTER LANDING, FLAPS WORKED FINE A COUPLE OF TIMES, UP AND DOWN. TROUBLESHOT AND FOUND LSDR K5L2005F00000Uplock Switch · failedON TAKEOFF, RETRACTED GEAR AND IN TURBULENCE, GEAR HANDLE LIGHTS FLICKERED ON AND OFF. PULLED BACK ON YOKE AND LIGHTS STAY ON, PUSH FWD AND LIGHTS GO OFF. REMOVED GEAR UP LIMIT SWITCH AND FOUND IT WAS GOING OFF BEHIND AUDIAL CLICK OFF SWITCH. REPLACED SWITCSDR K5LA620JSWindshield · crackedCLIMBING THROUGH 14000 FT IN THE CLOUDS WITH W/S HEAT ON, OAT-5C PILOTS WINDSHIELD OUTER PLY CRACKED ACROSS ENTIRE WINDSHIELD. RETURNED TO AIRPORT AND LANDED. REPLACED WINDSHIELD, NO OTHER DAMAGE NOTED.SDR K5LA620JSafety Switch · brokenAFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. GEAR REMAINED DOWN AND LOCKED. AFTER LANDING IT WAS DETERMINED A WIRE ON THE LANDING GEAR EMERGENCY SAFETY SWITCH HAD BEEN BROKEN OFF DURING INSPECTION AND LUBE OF NOSE GEAR CHAIN. JACKING THE AIRCRAFT AND DOIN
STCs that may be installed · 267
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech A200
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).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.