N7281M1999 Cessna 206H
This N-number isn't registered right now. Below is its last known registration, canceled Oct 19, 2022.
Safety record in brief:No NTSB accidents or incidents since 198212 ADs may apply5 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- South Regional Aviation Enterprise INC
- Owner type
- Non Citizen Corporation
- City, state
- Boynton Beach, FL
- Certificate issued
- Aug 25, 2022
- Canceled
- Oct 19, 2022
- Airworthiness
- Standard · Normal
- Airworthiness date
- Mar 24, 2006
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
- 206H
- Year
- 1999
- Serial number
- 20608048
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 6
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A9C3CB
Engine
- Make and model
- Lycoming Io-540-Ac1a5
- Type
- Reciprocating
- Power
- 300 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2022South Regional Aviation Enterprise INCBoynton Beach, FL
- until 1958Cessna Aircraft CoWichita, KS · different airframe: Cessna 175 S/N 55581
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 |
|---|---|---|---|
| 2026-17-10 | Reciprocating Engine Cylinder Section | Sep 14, 2026 | Engine (IO-540-AC1A5)Serial numbers per Table 2 or Table 3 of Lycoming Mandatory Service Bulletin No. 667A, dated March 12, 2026. Only with: Installed piston pin P/N LW-13445 with an OEM FAA Form 8130-3 production dated between January 7, 2021 and December 15, 2025, or where the production date cannot be determined or the form is unavailable. |
| 2013-11-11 | Engine Oil Pressure | Aug 1, 2013 | Airframe (206H)Certain serial numbers: 172R 17280001–17281618; 172S 172S8001–172S11256; 182S 18280001–18280944; 182T 18280945–18282357; T182T T18208001–T18209089; 206H 20608001–20608349; … |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (206H)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. |
| 2008-05-09 | Cessna Aircraft Company 172, 182, and 206 Series Airplanes | Apr 8, 2008 | Airframe (206H)Certain serial numbers: 172R 17281211–17281356; 172S 172S9621–172S10310; 172S 172S10312–172S10324; 172S 172S10327–172S10332; 172S 172S10334–172S10349; 172S 172S10351–172S10374; … |
| 2007-08-03 | Cessna Aircraft Company Models 172R, 172S, 182T, T182T, 206H, and T206H Airplanes | May 2, 2007 | Airframe (206H)Certain serial numbers: 172R 17281244–17281364; 172R 17281366–17281372; 172R 17281374–17281376; 172R 17281379; 172S 172S9809–172S10349; 172S 172S10351–172S10374; … |
Show all 12 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2007-05-10 | Cessna Aircraft Company Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H Airplanes | Apr 11, 2007 | Airframe (206H)Certain serial numbers: 172R 17280001–17281262; 172S 172S8001–172S9994; 182S 18280001–18280944; 182T 18280945–18281701; T182T T18208001–T18208453; 206H 20608001–20608250; … |
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (IO-540-AC1A5)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999. |
| 2005-13-10 | Cessna Aircraft Company Models 172R, 172S, 182T, T182T, 206H, and T206H Airplanes | Aug 9, 2005 | Airframe (206H)Certain serial numbers: 172R 17281186–17281232; 172S 172S9476–172S9689; 172S 172S9691–172S9770; 182T 18281242–18281502; 182T 18281506; 182T 18281507; … |
| 2004-15-18 | Cessna Aircraft Company Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H Airplanes | Sep 12, 2004 | Airframe (206H)Certain serial numbers: 172R 17280001–17281073; 172R 17281075–17281127; 172R 17281130; 172S 172S8001–172S9195; 172S 172S9197; 172S 172S9198; …. Only with: Equipped with a KAP 140 autopilot computer system P/N 065-00176-2501, -2602, -5001, -5101, -5201, -5402, or -7702 (all serial numbers). |
| 2004-05-24 | Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and… | Mar 30, 2004 | Engine (IO-540-AC1A5)Only with: Engines with crankshaft gear retaining bolts P/N STD-2209 installed; excludes O-540-F series engines subject to AD 99-03-05 with bolt not since replaced, engines with bolt installed at original assembly or replaced by Lycoming per SB 554 after November 10, 1998, engines with bolt from replacement kits 05K19987, 05K23325, 05K23326, 05K23327, 05K23335 or 05K23336, and engines with single-drive dual magnetos. |
| 2001-09-06 | Cessna Aircraft Company Models 206H and T206H Airplanes | May 18, 2001 | Airframe (206H)Certain serial numbers: 206H 20608001–20608053; 206H 20608055–20608086; 206H 20608088; 206H 20608089; T206H T20608001–T20608093; T206H T20608095–T20608145; … |
| 99-13-04 | Cessna Aircraft Company Models 206H and T206H Airplanes | Jul 13, 1999 | Airframe (206H)Certain serial numbers: 206H 20608002–20608026; T206H T20608002–T20608015; T206H T20608017–T20608023; T206H T20608025–T20608028 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (5)
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.
- Flight controls · cable housing · inadequateSep 20, 2000
DURING INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANTS (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE INTERCONNECT CABLE FOUND ONLY MINIMAL…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · cable guard · inadequateSep 20, 2000
DURING INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANTS (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE INTERCONNECT CABLE FOUND ONLY MINIMAL…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · engine · failedJun 5, 2000
PILOT REPORTED ENGINE SURGING ON TAKEOFF WITH SIGNIFICANT FUEL FLOW FLUCTUATION WHICH WAS CORRECTED WITH A DECREASE IN ENGINE POWER BY ADJUSTMENT OF THE PROP CONTROL AND ACTIVATION OF THE STANDBY ELECTRIC FUEL PUMP. POST-GROUND RUNS DUPLICATED THE PROBLEM, BUT NORMAL SYSTEMS CHECKS SATISFACTORY.…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Fuel · line · damagedFeb 23, 2000
DURING THE AIRCRAFT''S FIRST 100-HOUR INSPECTION, DISCOVERED FUEL LEAK AT FUEL SELECTOR VALVE AROUND FITTING ON FUEL LINE FROM SELECTOR TO LT HEADER TANK. UPON REMOVAL OF LINE, DISCOVERED DAMAGED FLARE. TOTAL AIRCRAFT TIME: 98.6 HRS. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · shroud · crackedFeb 1, 2000
DISCOVERED OIL LEAK IN ENGINE COMPARTMENT COMING FROM RIGHT SIDE PUSH ROD TUBE SHROUD ON NR 5 CYLINDER ASSEMBLY. ON FURTHER INSPECTION, TUBE WAS FOUND CRACKED APPROXIMATELY ONE INCH DIAGONALLY THEN EXTENDING AROUND THE CIRCUMFERENCE OF THE TUBE (APPROX HALF WAY AROUND). CRACK WAS LOCATED DIRECTLY…
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