- Registered owner
- Sedrak Michael
- Location
- Corona, CA
- Owner type
- Individual
- Serial number
- 2303
- Year built
- 2006
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- December 22, 2006
- Certificate issued
- October 22, 2018
- Expires
- October 31, 2028
- Mode S code
- ADD130
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 34
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1988 | 1 |
|---|---|
| 1991 | 1 |
| 1993 | 2 |
| 1996 | 1 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 3 |
| 2008 | 4 |
| 2009 | 3 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 2 |
| 2014 | 1 |
| 2016 | 1 |
| 2020 | 1 |
| 2022 | 1 |
| 2023 | 5 |
| 2024 | 1 |
Airframe · Cirrus Design SR22
AD 2024-24-11Power LeverAD 2023-09-09Exhaust Turbine System (Recip)AD 2022-03-15Fuel Quantity IndicatorInformation bulletins that may apply · 28
Advisory, not mandatory.
See all 31 bulletins
NTSB investigations
No NTSB investigations matched to N99KEMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cirrus Design SR22 aircraft
FAA incident reports
No FAA accident or incident reports matched to N99KEMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cirrus Design SR22 aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR M8VR2026020300001Brake Disc · crackedDURING 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.SDR 2013FA0000223Spark Plug · damagedAFTER 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 RUNNINGSDR 2013FA0000222Exhaust Duct · crackedTHE LT EXHAUST SYS DEVELOPED CRACKS DURING A RECENT INSPECTION AT 825 HRS TT. THE NEW STYLE EXHAUST KIT WAS INSTALLED.SDR 2013FA0000221Drive Gear · brokenNYLON 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.SDR 2011FA0000099Gear · fracturedWHILE THE ACFT WAS IN FOR MX, WHILE ATTEMPTING TO START THE ENGINE, A METAL GRINDING NOISE WAS HEARD BY THE MECHANIC. SUBSEQUENT REMOVAL OF THE STARTER ADAPTER REVEALED AT LEAST 2 TEETH MISSING ON THE CRANKSHAFT GEAR AND MARRED TEETH ON THE ADAPTER. THIS CONSDR 2011FA0000098Sensor · inaccurateTHE MANIFOLD PRESSURE SENSOR WOULD GIVE ERRONEOUS READINGS IN FLIGHT, BUT ON THE GROUND WOULD BE ACCURATE. THE REMEDY IS TO REPLACE THE SENSOR.SDR 2011FA0000097Seal · failedTHE ENGINE SEAL THAT SEALS ENGINE OIL OUT OF ALTERNATOR NR2 FAILED. THE RESULT WAS ENGINE OIL PASSING INTO THE ALTERNATOR AND DOWN THE BELLY OF THE ACFT. THE REMEDY IS TO REPLACE THE SEAL AND REBUILD THE ALTERNATOR.SDR 2011FA0000096Controller · failedUNABLE TO SET ENGINE IDLE AND MIXTURE SETUP. REMEDY WAS TO REPLACE THROTTLE CONTROLLER.SDR 2011FA0000095Check Valve · failedOIL FOUND IN INTAKE MANIFOLD. REMEDY WAS TO REPLACE TURBO INLET CHECK VALVE.SDR 2011FA0000094Adapter · failedSTARTER 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 ADASDR 2011FA0000093Module · failedTHE OXYGEN SYS WOULD NOT TURN ON IN FLIGHT BUT WORKED ON THE GROUND. REMEDY WAS TO REPLACE THE SWITCH, WIRE HARNESS, AND LOGIC MODULE.SDR 2011FA0000092Support Bracket · chafedTHE 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 SDR 2011FA0000091Exhaust Duct · crackedTHE 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. R
STCs that may be installed · 147
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cirrus Design SR22
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller