N99KE2006 Cirrus SR22
Safety record in brief:No NTSB accidents or incidents since 198216 ADs may apply13 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Individual owner
- City, state
- Corona, CA
- Certificate issued
- Oct 22, 2018
- Expires
- Oct 31, 2028
- Airworthiness
- Standard · Normal
- Airworthiness date
- Dec 22, 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
- Cirrus
- Model
- SR22
- Year
- 2006
- Serial number
- 2303
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 4
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Type certificate data sheet
- A00009CH
- Mode S code
- ADD130
Engine
- Make and model
- Cont Motor Io-550-N
- Type
- Reciprocating
- Power
- 310 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2018 – nowIndividual ownerCorona, CA · current
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 (16)
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 |
|---|---|---|---|
| 2024-24-11 | Power Lever | Dec 23, 2024 | Airframe (SR22)Only with: Equipped with upper power lever P/N 19181-001, 19181-002, or 46505-001. |
| 2023-05-16 | Reciprocating Engine Power Section | Mar 15, 2023 | Engine (IO-550-N) |
| 2020-16-11 | Reciprocating Cylinder Section | Sep 21, 2020 | Engine (IO-550-N)Only with: Engines originally manufactured, rebuilt, or modified with a cross-flow cylinder assembly replacement on or after November 1, 2014, with cross-flow cylinder assembly P/N 658538, 658540, 658542, 658591, 658595, 658613, 658624, 658539, 658541, 658590, 658594, 658603, 658623, or 658630 installed. |
| 2012-10-13 | Continental Motors, Inc. (CMI) Reciprocating Engines | Jun 8, 2012 | Engine (IO-550-N)Only with: Starter adapter P/N 642085A17, 642085A18, 642085A19, 642085A20, 642085A22, 642085-1A1, R-642085A17, R-642085A18, R-642085A19, or R-642085A22 installed, where the engine was manufactured, or a new or rebuilt starter adapter installed, before November 20, 2011; IO-550-N only if turbo-normalized per STC SE10589SC. |
| 2009-26-01 | Cirrus Design Corporation Model SR22 Airplanes | Dec 21, 2009 | Airframe (SR22)Certain serial numbers: SR22 3409; SR22 3411–3430; SR22 3432–3441; SR22 3443–3450; SR22 3455–3465; SR22 3467; …. Only with: Equipped with an anti-ice system approved for flight into known icing. |
Show all 16 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO-550-N)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
| 2008-14-13 | Cirrus Design Corporation Model SR20 and SR22 Airplanes | Aug 14, 2008 | Airframe (SR22)Certain serial numbers: SR20 1423–1906; SR22 0795; SR22 0820–2912 |
| 2008-03-16 | Cirrus Design Corporation Models SR20 and SR22 Airplanes | Mar 11, 2008 | Airframe (SR22)Certain serial numbers: SR20 1005–1861; SR22 0002–2333; SR22 2335–2419; SR22 2421–2437 |
| 2007-24-13 | Cirrus Design Corporation Model SR22 Airplanes | Dec 4, 2007 | Airframe (SR22)Certain serial numbers: SR22 2334; SR22 2420; SR22 2438–2749 |
| 2007-14-03 | Cirrus Design Corporation Models SR20 and SR22 Airplanes | Aug 16, 2007 | Airframe (SR22)Certain serial numbers: SR20 1005–1798; SR22 0002–2437. Only with: Applies to airplanes certificated in any category that have not incorporated in their entirety the actions of Cirrus Alert Service Bulletin No. SB A2X-95-10 R1, Revised April 10, 2007. |
| 2006-21-03 | Cirrus Design Corporation Models SR20 and SR22 Airplanes | Nov 17, 2006 | Airframe (SR22)Certain serial numbers: SR20 1005–1600; SR22 0002–1739; SR20 1005–1592; SR22 0002–1727 |
| 2006-19-10 | Cirrus Design Corporation Models SR20 and SR22 Airplanes | Oct 24, 2006 | Airframe (SR22)Certain serial numbers: SR20 1005–1600; SR22 0002–1727 |
| 2006-07-06 | Cirrus Design Corporation Models SR20 and SR22 Airplanes | May 11, 2006 | Airframe (SR22)Certain serial numbers: SR20 1005–1581; SR22 0002–1643; SR22 1645–1662 |
| 2002-24-08 | Cirrus Design Corporation Models SR20 and SR22 Airplanes | Jan 24, 2003 | Airframe (SR22)Certain serial numbers: SR20 1005–1195; SR22 0002–0209 |
| 2002-21-02 | Cirrus Design Corporation Model SR20 and SR22 Airplanes | Nov 8, 2002 | Airframe (SR22)Certain serial numbers: SR20 1005–1234; SR20 1236; SR20 1239–1241; SR22 0002–0308; SR22 0310–0321; SR22 0324–0327; …. Only with: SR20 S/N 1005-1241 except 1235, 1237, 1238; SR22 S/N 0002-0333 except 0309, 0322, 0323, 0328. |
| 2001-25-03 | Cirrus Design Corporation Models SR20 and SR22 Airplanes | Dec 17, 2001 | Airframe (SR22)Certain serial numbers: SR20 1134–1159; SR22 0003–0119 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (13)
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.
- Landing gear · brake disc · crackedJan 22, 2026
DURING ANNUAL INSPECTION, THE BRAKE DISC FAILED MINIMUM THICKNESS CHECK ON THE FRICTION SURFACE. DURING ROTOR REPLACEMENT THREE SEPARATE, SIGNIFICANT CRACKS WERE NOTED IN THE WEB/RADIUS ADJACENT TO EACHOF THE THREE BOLT HOLES.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Ignition · drive gear · brokenApr 2, 2013
NYLON GEAR HAS EIGHT BROKEN TEETH RESULTING IN LOOSING LT MAGNETO ON CLIMBOUT. THE MAGNETO HAD 430 HRS SINCE THE LAST 500 INSPECTION, WITH 865 HRS TT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust duct · crackedApr 2, 2013
THE LT EXHAUST SYS DEVELOPED CRACKS DURING A RECENT INSPECTION AT 825 HRS TT. THE NEW STYLE EXHAUST KIT WAS INSTALLED.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Ignition · spark plug · damagedApr 2, 2013
AFTER HAVING CRACKED INSULATOR ON RHB32S SPARK PLUGS AND SB 11-05, WHICH HAD A MANDATORY REPLACEMENT OF FINE WIRE SPARK PLUGS, INSTALLED MASSIVE SPARK PLUGS. NOW, 13 MONTHS AND 310 HRS LATER, THE ENGINE IS MISFIRING IN CRUISE. ONE CYLINDER AT A TIME RUNNING ON ONE SPARK PLUG. THE ENGINE IS RUN…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust duct · crackedJan 19, 2011
THE RT EXHAUST SYS DEVELOPED GUSSET CRACKS AROUND 250 HRS TT. THE MFG SAID THE CRACKS WERE "NON SAFETY CONCERNS" AND DID NOT ADDRESS THEM AT THE TIME. AT 432 HRS TT THE EXHAUST CRACKED IN 2 DIFFERENT WELD JOINTS ON THE COLLECTORS LEADING FROM 2 CYLINDERS. REMEDY WAS TO REPLACE THE RT EXHAUST SYS.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · support bracket · chafedJan 19, 2011
THE VERTICAL SUPPORT ROD SUPPORTING THE TURBOS WAS BEING CHAFED BY THE SUPPORT BRACKET. THE SUPPORT BRACKET CHANGED PN OLD: ETI-62-103-1, NEW: 22-625-0006 AND 22-625-0005. THE VERTICAL SUPPORT ROD DID NOT CHANGE PN, HOWEVER BOTH LT AND RT RODS WERE REPLACED AS WITH THE BRACKETS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Oxygen · module · failedJan 19, 2011
THE OXYGEN SYS WOULD NOT TURN ON IN FLIGHT BUT WORKED ON THE GROUND. REMEDY WAS TO REPLACE THE SWITCH, WIRE HARNESS, AND LOGIC MODULE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Starting · adapter · failedJan 19, 2011
STARTER ADAPTER WAS SLIPPING. AS A RESULT THE ENGINE WOULD BARELY TURN OVER WHEN STARTING. THE REMEDY WAS TO REPLACE THE STARTER AND STARTER ADAPTER. THESE STARTERS HAVE A LONG HISTORY OF TEARING UP STARTER ADAPTERS. THESE STARTERS WILL NOT RELEASE THE ADAPTER ONCE THE ENGINE FIRES ( CAUSING THE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Reciprocating engine · check valve · failedJan 19, 2011
OIL FOUND IN INTAKE MANIFOLD. REMEDY WAS TO REPLACE TURBO INLET CHECK VALVE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine controls · controller · failedJan 19, 2011
UNABLE TO SET ENGINE IDLE AND MIXTURE SETUP. REMEDY WAS TO REPLACE THROTTLE CONTROLLER.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 13 reports.
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