- Registered owner
- Pa1 208b-0616 LLC
- Location
- Fort Lauderdale, FL
- Owner type
- LLC
- Serial number
- 208B0616
- Year built
- 1997
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- June 20, 1997
- Certificate issued
- September 12, 2026
- Expires
- September 30, 2033
- Mode S code
- A4C74C
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 · 47
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 |
| 1977 | 1 |
| 1978 | 2 |
| 1980 | 2 |
| 1986 | 1 |
| 1988 | 1 |
| 1990 | 3 |
| 1992 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 2 |
| 2001 | 2 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 3 |
| 2009 | 3 |
| 2011 | 2 |
| 2012 | 1 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 54 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
NTSB investigations · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB ANC21LA025Accident · No injuriesClass 4 · LimitedFinal reportChevak, AKThe pilot’s loss of directional control during the back-taxi for departure in strong crosswind conditions which resulted in a runway excursion. Contributing to the accident was the snow-and-ice-covered runway.NTSB ANC00LA033Accident · No injuriesLimited investigationFinal reportHoly Cross, AKAn in-flight separation of a main landing gear tire mud flap, and subsequent impact with the horizontal stabilizer.
FAA incident reports · 5
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20251101016059ICruise/Level Flight · Bethel, AKOn November 1, 2025, approximately 1210 local time, during cruise flight and headed for Bethel Airport; the PIC stated that he experienced several primary bus circuit breakers pop. Then the aircraft’s primary flight display flickered and suddenly shutoff.…Incident 20240615005659ITaxi · Hooper Bay, AKThe pilot was taxiing with attention diverted away from the ramp looking at the runway. The aircraft propeller struck a stack of cargo boxes on the ramp while taxing to the runway.Accident 20210312002319ATaxi · Chevak, AK1) On 03/12/2021 the airman was dispatched to take a flight to hooper bay and Chevak Alaska. 2) A flight risk assessment log was filled out and initialed by the pilot and the [privacy data omitted] dispatch agent. 3)The [privacy data omitted] weather sheet…Accident 20000304038779ANormal Cruise · Holy Cross, AK(.4) The commercial certificated pilot departed on a scheduled flight. During cruise, abour fifteen minutes after takeoff, he heard a bang. After landing at the destination airport, damage was discovered to the horizontal stabilizer. The left mud flap,…Incident 19981028041309IRoll-Out (Fixed Wing) · Pilot Station, AKM&d initiated for failure of left hand landing gear. FSDO id #IAL39102801.
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ENHA20251101002Screw · looseAFTER SECURING LOOSE SCREW ON BUS 2 STANDBY POWER CIRCUIT BREAKER (LOG PAGE 263019)AND SUCCESSFUL CHECK FLIGHT THE AIRCRAFT WAS RETURNED TO SERVICE.SDR ENHA20251103001Electrical Sys · malfunctionedPILOT NOTE DISCREPANCY AS AN ELECTRICAL POWER LOSS/MULTIPLE BUS BREAKERS POP/PFD LOSS. MAINTENANCE INSPECTED ELECTRICAL SYSTEM AND COULD NOT DUPLICATE. AIRCRAFT IS SCHEDULED TO PERFORM AN OPERATIONAL CHECK FLIGHT FOR THE ELECTRICAL SYSTEM.SDR ENHA202310160001Unknown · unknownLEFT WING MOVES DURING FLIGHT /FLAP OPERATION. MAINTENANCE INSPECTED LEFT WING AND DETERMINED AFT ATTACH FITTINGS WERE DAMAGED AND REQUIRE REPLACEMENT. THE FOLLOWING FITTINGS WERE REPLACED: 2622021-9,2622021-1,2611139-1,2611139-2.SDR EPUA092007ASkin · crackedDURING ROUTINE INSPECTION, DISCOVERED 4" CRACK ON UPPER RT AFT WING SKIN 18" FROM WING ROOT AT WS 53.00. DAMAGE WAS REPAIRED IAW CESNNA MM 51-75-00. AIRCRAFT WAS RETURNED TO SERVICE.SDR EPUA300104ASupport · crackedPILOT REPORTED WHEN RETRACTING FLAPS ON ROLL-OUT THE FLAP CIRCUIT BREAKER TRIPPED. MX INSPECTED AND FOUND THE FLAP TRANSMISSION SUPPORT ASSY. CRACKED AND BUCKLED. THERE WAS NO EVIDENCE OF THE STANDBY FLAP SYSTEM BEING ACTIVATED.
STCs that may be installed · 357
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.