- Registered owner
- Pa1 208b-0632 LLC
- Location
- Fort Lauderdale, FL
- Owner type
- LLC
- Serial number
- 208B0632
- Year built
- 1997
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- September 22, 1997
- Certificate issued
- September 13, 2026
- Expires
- September 30, 2033
- Mode S code
- A4D4CA
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 · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20230908015199ILanding: Approach · Manokotak, AKA passenger was sitting in the front right seat of a grant aviation CE-208 [privacy data omitted]. The passenger was asleep and started leaning forward touching the control yoke. The pilot pushed him backwards and tried to wake him. They were on approach to…Accident 20030709036369ANormal Cruise · Kotzebue, AK(-23) Airman harris stated that while in cruise flight at approximately 4,500 feet he removed his seatbelt and went to the rear of the aircraft to "stretch his legs and check the cargo." The SIC was seated at the controls. Harris stated that an encounter with…Incident 20000915031659IRoll-Out (Fixed Wing) · Kasigluk, AK(-23)During rollout at Kasigluk, AK (Z09) found minimal braking on rmlg and no breaking on lmlg. Pilot pulled power lever into reverse while maintaining directional control, attempting to stop on the runway. The aircraft drifted right and hit runway end…
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ENHA 20250521862Regulator · stickingPILOT OBSERVED THE PILOT DOOR POST GETTING HOT. MECHANICS REPLACED THE BLEED AIR PRESSURE REGULATOR AND PROBLEM WAS RESOLVED.SDR ENHA202310160002Unknown · unknownPILOT NOTED "I OBSERVED A RUNAWAY ENGINE CONDITION, MY TORQUE AND NG GUAGES CLIMBED TO REDLINE WITH MY POWER LEVER IN IDLE POSITION. I DECIDED TO CLIMB TO 9500 FT AND CONTINUE TOWARDS KING SALMON ALASKA. MY ITT GUAGE SLOWLY CLIMBED TO A MAXIMUM OF 900C. ONSDR ENHA202208300001Autopilot Sys · faultedPILOT REPORTED: I WAS ENROUTE TO BET FROM AKN. I WAS IN SOME ICING AND TRYING TO FIND AN ALTITUDE THAT WAS GOING TO WORK. I HAD A BLOCK 8,000-12,000. I WAS AT 12,000 WHEN I NOTICED THAT MY AIRSPEED WAS DECAYING FASTER THAN SEEMED NORMAL. I LOOKED OUT TO THE WISDR ENHA202108150071Circuit Breaker · trippedAFTER TAKEOFF, AT APPROXIMATELY 200FT, THE G600 AUTOPILOT ENVELOPE STALL PROTECTION (ESP) SYSTEM ENGAGED AND NOSED THE AIRCRAFT INTO A DESCENT. THE PILOT PUSHED THE AUTOPILOT DISCONNECT SWITCH WHICH BRIEFLY DISCONNECTED THE AUTOPILOT SYSTEM. THE PILOT REPORTEDSDR EPUA20170409003Longeron · crackedDURING SCHEDULED INSPECTION, A CRACK WAS FOUND ON RT LONGERON AT RBL 8.00 WAS FOUND TO BE AND NEEDED TO BE REPLACED. IN ORDER TO REMEDY THIS CONDITION A SPLICE WAS DESIGNED PER DER APPROVAL ON 8110-3 DATED 28 MARCH 2017.SDR EPUA20170409002Attach Fitting · crackedDURING SCHEDULED INSPECTION THE NOSE LANDING GEAR ATTACH FITTING WAS FOUND TO BE CRACKED. IN ORDER TO REMEDY THIS CONDITION THE ATTACH FITTING HAD TO BE REPLACED.SDR EPUA20170409001Floor Panel · damagedDURING SCHEDULED INSPECTION FLOOR SECTION FROM FUSELAGE STA 122.00 TO 159.00 WAS FOUND TO BE DAMAGED BEYOND ALLOWABLE LIMITS. IN ORDER TO REMEDY THIS CONDITION A SPLICE FROM NEW FLOOR SECTION WAS INSTALLED.SDR EPUA20151015001Brake Assy · brokenRIGHT BRAKE WAS NOTED BY FLIGHT CREW AS BEING INOPERATIVE. MX DETERMINED THAT THE RT HAND BRAKE ASSEMBLY BROKE A GUIDE PIN, CAUSING IT TO CONTACT THE RT HAND TIRE ASSEMBLY. REPLACED THE DEFECTIVE BRAKE ASSEMBLY & DAMAGED TIRE ASSEMBLY IN ORDER TO FERRY THE ASDR 98ZZZX156Line · chafedFORWARD FUEL LINE COMING FROM THE WING AS IT ENTERS RESERVOIR TANK COMPARTMENT. THERE ARE THREE AN3 BOLTS RETAINING A SEAL IN THE SIDE WALL OF COMPARTMENT. FORWARD BOLT CHAFING LINE, BOLT TURNED OUT TO BE AN3-4A, PARTS MANUAL CALLS FOR AN3-3A. BOTH SIDES OF
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.