N9653F1987 Cessna 208
This N-number isn't registered right now. Below is its last known registration, canceled Apr 16, 2009.
Safety record in brief:No NTSB accidents or incidents since 198212 ADs may apply6 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Atlantic Aero INC
- Owner type
- Corporation
- City, state
- Greensboro, NC
- Certificate issued
- Jul 28, 2004
- Canceled
- Apr 16, 2009
- Airworthiness
- Standard · Normal
- Airworthiness date
- Apr 29, 1987
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Cessna
- Model
- 208
- Year
- 1987
- Serial number
- 20800114
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 10
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- AD7180
Engine
- Make and model
- P&W Canada Pt6a-60a
- Type
- Turbo-prop
- Power
- 1050 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2004 – 2009Atlantic Aero INCGreensboro, NC
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (12)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2021-04-10 | Textron Aviation, Inc. Airplanes | Apr 12, 2021 | Airframe (208)Certain serial numbers: 208 20800564–20800594; 208 20800603–20800605; 208B 208B5141–208B5285; 208B 208B5287–208B5305; 208B 208B5307–208B5312; 208B 208B5314; … |
| 2009-15-05 | Cessna Aircraft Company Models 208 and 208B Airplanes | Jul 27, 2009 | Airframe (208)Certain serial numbers: 208 20800500–20800504; 208B 208B1216; 208B 208B2001; 208B 208B2003–208B2023; 208B 208B2025–208B2029; 208B 208B2031–208B2037; … |
| 2009-05-12 | Cessna Aircraft Company Models 208 and 208B Airplanes | Apr 15, 2009 | Airframe (208)Certain serial numbers: 208 20800001–20800415; 208 20800417–20800419; 208B 208B0001–208B1081; 208B 208B1083–208B1215; 208B 208B1217–208B1257; 208B 208B1259–208B1305; … |
| 2008-13-06 | Cessna Aircraft Company Models 208 and 208B Airplanes | Jul 30, 2008 | Airframe (208)Certain serial numbers: 208 20800001–20800415; 208B 208B0001–208B1299 |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (208)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007. |
Show all 12 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2007-10-15 | Cessna Aircraft Company Models 208 and 208B Airplanes | Jun 21, 2007 | Airframe (208) |
| 2006-01-11 R1 | The Cessna Aircraft Company Models 208 and 208B Airplanes | Feb 22, 2006 | Airframe (208) |
| 2004-08-17 | Cessna Aircraft Company Models 208 and 208B Airplanes | May 17, 2004 | Airframe (208)Certain serial numbers: 208 20800370; 208 20800371; 208B 208B1034–208B1043; 208B 208B1045; 208B 208B1046; 208B 208B1048 |
| 2003-21-04 | Cessna Aircraft Company Models 208 and 208B Airplanes | Oct 21, 2003 | Airframe (208)Certain serial numbers: 208 20800001–20800369; 208B 208B0001–208B1014; 208B 208B1017; 208B 208B1018; 208B 208B1020–208B1024; 208B 208B1026; … |
| 2002-23-13 | Pratt & Whitney Canada PT6A Series Turboprop Engines | Dec 31, 2002 | Engine (PT6A-60A)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed. |
| 2002-22-17 | Cessna Aircraft Company Models 208 and 208B Airplanes | Dec 31, 2002 | Airframe (208) |
| 97-25-04 | Cessna Aircraft Company Models 208, 208A, 208B, 425, and 441 Airplanes | Jan 21, 1998 | Airframe (208) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (6)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Exhaust · cowling · crackedSep 19, 2008
THE SECONDARY EXHAUST COWLING WAS FOUND TO HAVE A 5.5 INCH LONG CRACK NEXT TO THE CENTER EXHAUST HANGER ROD END BRACKET. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · housing · wornMay 12, 2008
RT BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THIS IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTROPHIC DAMAGE TO THE CALIPER ASSEMBLY, TORQUE PLATE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · bearing · corrodedApr 23, 2008
THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reportsShow fewer reports
- Flight controls · bellcrank · damagedApr 23, 2008
THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · bellcrank · damagedApr 23, 2008
THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · bellcrank · damagedApr 23, 2008
THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026