- Registered owner
- Kilo Alpha 438 LLC
- Location
- Edgewater, FL
- Owner type
- LLC
- Serial number
- BB438
- Year built
- 1978
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- January 24, 1997
- Certificate issued
- March 5, 2024
- Expires
- March 31, 2031
- Mode S code
- A54118
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 · 80
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 |
| 1974 | 1 |
| 1975 | 4 |
| 1976 | 5 |
| 1977 | 5 |
| 1978 | 3 |
| 1979 | 1 |
| 1980 | 4 |
| 1983 | 1 |
| 1985 | 1 |
| 1986 | 1 |
| 1987 | 1 |
| 1989 | 2 |
| 1990 | 4 |
| 1991 | 1 |
| 1992 | 3 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 2 |
| 1997 | 4 |
| 1998 | 4 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 3 |
| 2004 | 3 |
| 2005 | 6 |
| 2006 | 1 |
| 2008 | 3 |
| 2011 | 2 |
| 2012 | 1 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 1 |
| 2025 | 1 |
See all 84 ADs
Information bulletins that may apply · 9
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N438CRMatched 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 · 1
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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR A8JA201408080018Switch · defectiveDURING APPROACH, PILOT SELECTED APPROACH FLAPS SETTING. SELECTION OF APPROACH FLAPS CAUSED NO MOVEMENT IN FLAP SYS. PILOT ATTEMPTED FLAP SELECTION ONCE MORE WITH NO LUCK. PILOT REFERRED TO CHECKLIST FOR FAILED FLAPS. PILOT ELECTED TO ABORT APPROACH & LANDISDR A8JA201309280017Clamp · looseDURING CLIMB, EXPERIENCED RED LANDING GEAR DISAGREEMENT LIGHT. DID NOT NOTICE OR HEAR ANY OTHER FACTORS TO ALARM THEM OF ANY MECHANICAL FAILURES. CONTINUED TO DESTINATION. DURING FINAL APPROACH, EXTENDED LANDING GEAR AND RED LIGHT EXTINGUISHED AND ALL THRSDR A8JA201305090016Windshield · crackedAT APPROXIMATELY 2130 CST, ACFT IN DESCENT, PIC HEARD A LOUD "POP" FROM THE COPILOT WINDSHIELD. UPON VISUAL INSPECTION, PIC NOTICED COPILOT WINDOW PANE CRACKED AND SHATTERED. PILOT REQUESTED "PRIORITY HANDLING" WITH ATC FOR ARRIVAL AND WAS INFORMED HE WOULD SDR A8JA201302260015Switch · intermittentAIRCRAFT DEPARTED, ENROUTE, AFTER FLIGHT CREW INITIATED CLIMBOUT AND RETRACTED LANDING GEAR, CREW OBSERVED ALL GREEN LIGHTS WERE EXTINGUISHED BUT THE RED HANDLE LIGHT (GEAR UNSAFE LIGHT) WAS ILLUMINATED. CREW OPTED TO CYCLE GEAR ONCE MORE AND OBSERVED RED LISDR A8JA201206290014Circuit Breaker · trippedON FINAL APPROACH, EXPERIENCED LOSS OF RADIOS, NAVIGATION, TRANSPONDERS, GPS, AND AUTOPILOT. CREW IDENTIFIED A TRIPPED CIRCUIT BREAKER AND DUE TO PROXIMITY OF AIRPORT AND OTHER TRAFFIC, CREW OPTED TO LOAD SHED AND RESET BREAKER TO GET COMM RADIOS BACK. RESETSDR A8JA201202110011Wire · shortedWHILE CLIMBING OUT, CREW NOTICED ACFT CABIN WAS NOT PRESSURIZING. CREW MEMBER REVIEWED CHECKLIST AND VERIFIED SYS WAS NOT FUNCTIONING NORMAL. DIVERTED BACK TO DEPARTURE. ACFT LANDED WITHOUT INCIDENT. MX DISCOVERED WIRES D30A22, AND D26C22 FROM PINS 3 AND SDR A8JA0001Windshield · failedDURING FLIGHT, RT WINDSHIELD MIDDLE PANE SHATTERED (INNER AND OUTER PANE REMAINED INTACT). ACFT WAS 30 MINUTES INTO FLIGHT AT FL270. ACFT CREW RECEIVED CLEARANCE TO LOWER ALTITUDE AND DIVERTED. ACFT REMAINED UNTIL A FERRY PERMIT WAS ACQUIRED. THE ACFT WAS
STCs that may be installed · 466
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 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.