Cirrus Design SR22

Service difficulty reports · 438

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'SR22'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR J4PA2663Alternator · openWHILE AT CRUISE, ALT 1 LIGHT ILLUMINATED. PILOT DIVERTED TO PDK. ONE PASSENGER WAS ONBOARD. LAND WITH INCIDENT. MAINTENANCE REPLACED THE NR 1 ALTERNATOR AND FIELD CONTROL MODULE.Aug 17, 2007 · N134AJ · Cirrus SR22 · AC Generation SystemSDR 2618Sensor · malfunctionedFLYING FROM GSP TO LRO APPROXIMATELY 1500 HOURS LOCAL DEVELOPED A HIGH OIL TEMP. MADE AN UNSCHEDULED LANDING AT CAE WITHOUT INCIDENT. THERE WAS TWO PASSENGERS ON BOARD. IT WAS DETERMINED THAT THE OIL TEMP SENSOR WAS MALFUNCTIONING. REPLACED SENSOR AND FLEWAug 8, 2007 · N134AJ · Cirrus SR22 · Engine Oil TemperatureSDR J4PA200702558Alternator · openAIRCRAFT DEPARTED KCAE TO KHXD WITH 1 PASSENGER. DURING CRUISE NR 1 ALT FAIL LIGHT ILLUMINATED. PILOT RETURNED TO KCAE WITHOUT INCIDENT. MAINTENANCE DROVE TO KCAE, REMOVED AND REPLACED THE NR 1 ALTERNATOR AND NR 1 FIELD CONTROL MODULE.Jul 26, 2007 · N675CD · Cirrus SR22 · AC Generation SystemSDR 02541Alternator · openDURING DESCENT INTO KPDK FROM KJZI, WITH ONE PASSENGER THE NR 1 ALT WARNING LIGHT COME ON. TRIED RESETTING THE SYSTEM DID NOT HELP. PERFORMED LOAD SHEDDING AND LANDED WITHOUT INCIDENT. FOUND NR 1 ALT HAD AN OPEN FIELD IN THE ALTERNATOR ITSELF.Jul 23, 2007 · N675CD · Cirrus SR22 · AC Generation SystemSDR 2502Module · brokenAT 0900, DURING CLIMB OUT FROM GMU TO 60J THE ALT, NR 1 AND NR 2 FAIL LIGHT CAME ON. RETURNED TO GMU WITH OUT INCIDENT. HAD ONE PASSENGER ONBOARD. GROUND RAN AIRCRAFT COULD NOT DUPLICATED PROBLEM. PERFORM A AROUND THE PATTERN FLIGHT AND PROBLEM CAME BACK. Jul 14, 2007 · N695CD · Cirrus SR22 · Electrical Power SystemSDR 2007FA0000635Alternator · failedUPON RECEIPT OF CURRENT ALTERNATOR, NOTICED THAT SLIP-RING HOUSING WAS CLOCKED 180 DEGREES OUT OF ALIGNMENT OUT OF THE BOX. THIS PLANE HAS HAD SEVERAL REPAIRED ALTERNATORS INSTALLED ON IT. THE MOST RECENT ALTERNATOR HAD ONLY 131.1 HOURS BEFORE IT FAILED AND Jun 29, 2007 · N769PC · Cirrus SR22 · AC Generation SystemSDR J4PA062907002Control Unit · failedWHILE FLYING FROM KRIC TO KGGE A NR 1 ALT WARNING LIGHT COME ON. FOLLOWED PROCEDURES AND FAILED AGAIN. MADE AN UNSCHEDULED LANDING AT KRDU. TWO PASSENGERS WERE ONBOARD. NO PROBLEMS DURING LANDING.Jun 28, 2007 · N134AJ · Cirrus SR22 · Altimeter, Barometric/EncoderSDR J4PA062807001Spark Plug · crackedAT APPROXIMATELY 1600 LOCAL FLYING FROM KPDK TO KGSO AT CRUISE DEVELOPED AN ENGINE VIBRATION AND ROUGH RUNNING. DIVERTED INTO KGMU WITH 1 PASSENGER, WITHOUT INCIDENT. AFTER GROUND CHECKS FOUND THAT A SPARK PLUG FIRING SIDE INSULATOR WAS CRACKED CAUSING THE MJun 27, 2007 · N851CD · Cirrus SR22 · Spark Plug/IgniterSDR 2393Control Unit · failedAT APPROXIMATELY 1300 LOCAL AND DURING CLIMB-OUT FROM KGSP GOING TO KSAV THE ALT 2 WARNING LIGHT CAME ON AND SHOW A BATTERY DISCHARGE. ACTION TAKEN WAS TO DIVERT TO KGMU FOR TROUBLESHOOT AND REPAIR. 1 PASSENGER ON BOARD AND LANDED WITHOUT INCIDENT. FOUND THJun 15, 2007 · N695CD · Cirrus SR22 · DC Generating SystemSDR 2007FA0000517Hinge · corrodedFLAP HINGE ASSEMBLY HAS INTERGRANULAR CORROSION ON THE FORWARD EDGE OF THE HINGE JUST BELOW THE BOTTOM WING SKIN ABOVE THE HINGE FAIRING.Jun 12, 2007 · N122GH · Cirrus SR22 · Trailing Edge FlapsSDR 2007FA0000516Hinge · corrodedFLAP HINGE ASSEMBLY HAS INTERGRANULAR CORROSION ON THE FORWARD EDGE OF THE HINGE JUST BELOW THE BOTTOM WING SKIN ABOVE THE HINGE FAIRING.Jun 12, 2007 · N122GH · Cirrus SR22 · Trailing Edge FlapsSDR 2350Probe · shortedDURING CRUISE FLIGHT, THE NR 2 CHT READS 380*-420*. AIRCRAFT MADE AN UNSCHEDULED LANDING AT KCAE AT APPROXIMATELY 2010 LOCAL. ONE PASSENGER ON BOARD. AIRCRAFT LANDED WITHOUT INCIDENT OR INJURIES. THE NR 2 CHT READ HOTTER THAN THE OTHERS AND SPIKED INTO THEMay 31, 2007 · N851CD · Cirrus SR22 · Cylinder Head Temperature (CHT) Indicating SystemSDR 2007FA0000477Bungee · misriggedDURING INSPECTION FOUND RUDDER AILERON INTERCONNECT BUNGEE MISRIGGED AND INTERTFERING WITH THE AILERON CONTROLS. THERE IS NO EVIDENCE THAT THIS AIRCRAFT HAS HAD ANY MAINTENANCE TO THIS SYSTEM SINCE LEAVING THE FACTORY. ANOTHER AIRCRAFT WITH THIS CONDITION HAD May 7, 2007 · N519SR · Cirrus SR22 · Rudder Control SystemSDR 2007FA0000476Air Filter · debondedAPPEARS THAT THE FOAM AIR FILTER ELEMENT, THAT IS CYLINDER SHAPED AND BONDED TOGETHER, DID NOT HAVE SUFFICIENT GLUEUU OR CAME UNBONDED AND WAS ALLOWING UNFILTERED AIR TO ENTER THE ENGINE INTAKE.May 4, 2007 · N711KW · Cirrus SR22 · Engine Air Intake SystemSDR 050207Rod End · brokenCABIN DOOR DEPARTED AIRCRAFT IN FLIGHT DUE TO THE ROD END HINGE FAILURE. IT APEARS THE ROD END FAILED DUE TO FATIGUE. THE ROD END SHOULD BE MADE OF A STRONGER MATERIAL.May 2, 2007 · N299JW · Cirrus SR22 · Passenger/Crew DoorsSDR 001101Wire · brokenAT APPROXIMATELY 1420 AND DURING CLIMBOUT FROM KHXD TO KLRO, THE NR 1 ALT LIGHT CAME ON. TURNED THE MFD TO ENGINE PAGE WHEN SIGN FOR CHECK ALT 1 CAME ON. RETURNED TO KHXD AND LANDED WITH NO INCIDENT. ALTITUDE WAS APPROXIMATELY 2200 FEET WITH 1 PASSENGER ON May 1, 2007 · N301SR · Cirrus SR22 · Electrical Power System WiringSDR 2007FA0000375Control Cable · interferenceDURING INSPECTION FOUND INTERFERENCE BETWEEN RUDDER/AILERON INTERCONNECT SYSTEM AND RT AILERON CABLE. CHECKED RIGGING AND FOUND CABLE CLAMP ON RT AILERON CABLE OUT OF POSITION. VISUAL INSPECTION INDICATES NO MOVEMENT BETWEEN CABLE AND CLAMP AND RECORDS REVIEW Apr 27, 2007 · N220SR · Cirrus SR22 · Rudder Control SystemSDR 2007FA0000339Arm · misriggedEACH AC THAT CAME INTO THE SHOP WAS INSPECTED FOR THE SAME CONDITION WITH THE AILERON/RUDDER INTERFERENCE. INSPECTION FOUND RUDDER/AILERON INTERCONNECT MISRIGGED RESULTING IN THE BOLT CONNECTING THE BUNGEE TO THE RUDDER/AILERON INTERCONNECT ARM HITTING THE FOApr 19, 2007 · N927SE · Cirrus SR22 · Rudder Control SystemSDR 2007FA0000337Control System · out of rigDURING INSPECTION, FOUND AILERON RUDDER INTECONNECT OUT OF RIG AND CAUSING INTERFERENCE BETWEEN RUDDER AND AILERON. THIS IS THE FOURTH AIRCRAFT WE'VE FOUND WITH THIS PROBLEM AND ONE ACTUALLY HAD THE RUDDER AND AILERON LOCK IN FULL OPPOSITE DEFLECTIONS JUST PRIApr 18, 2007 · N636ST · Cirrus SR22 · Aileron Control SystemSDR 2007FA0000341Relay · failedDURING A TRAINING FLIGHT, THE FLAPS BECAME STUCK IN THE DOWN POSITION. THE AIRCRAFT RETURNED TO THE AIRPORT WITHOUT INCIDENT AND THE AIRCRAFT WAS SENT TO MAINTENANCE FOR TROUBLESHOOTING. MAINTENANCE DISCOVERED THE FLAPS DOWN RELAY FAILED.Apr 16, 2007 · N105SR · Cirrus SR22 · Trailing Edge Flap Control SystemSDR ODAR15DR1Alternator · destroyedOWNER REPORTED NR2 ALTERNATOR LIGHT ILLUMINATED. REMOVED TOP COWLING TO INSPECT NR2 ALTERNATOR. FOUND NR2 ALTERNATOR BROKEN OFF AT MOUNTING PLATE BY (3) STUDS. ONE STUD STILL ATTACHED WITH NUT, BUT LOOSE. REMOVED P/N BC410-1, S/N 0921403.Apr 11, 2007 · N15DR · Cirrus SR22 · AC Generator-AlternatorSDR 15DRAlternator · destroyedOWNER REPORTED NR2 ALTERNATOR LIGHT ILLUMINATED. REMOVED TOP COWLING TO INSPECT NR2 ALTERNATOR. FOUND NR2 ALTERNATOR BROKEN OFF AT MOUNTING PLATE BY (3) STUDS. ONE STUD STILL ATTACHED WITH NUT, BUT LOOSE. REMOVED P/N BC410-1, S/N 0921403.Apr 11, 2007 · N15DR · Cirrus SR22 · AC Generator-AlternatorSDR ODAR3Alternator · destroyedOWNER REPORTED NR 2 ALTERNATOR LIGHT ILLUMINATED. REMOVED TOP COWLING TO INSPECT NR 2 ALTERNATOR. FOUND NR 2 ALTERNATOR BROKEN OFF AT MOUNTING PLATE BY (3) STUDS. ONE STUD STILL ATTACHED WITH NUT, BUT LOOSE. REMOVED P/N BC410-1, S/N 0921403. PICTURES AVAILApr 11, 2007 · N15DR · Cirrus SR22 · AC Generator-AlternatorSDR 02118Pressure Switch · fluctuatesOIL PRESSURE DROPPED TO 20 PSI IN CRUISE FLIGHT, DURING CRUISE OIL GAUGE FLUCTUATED +- 4 PSI, BETWEEN 33-37 OTHER INDICATIONS NORMAL, REMOVED AND CLEANED OIL PRESSURE SENDING UNIT REINSTALLED AND OPERATIONAL CHECKED GOOD.Apr 6, 2007 · N509SR · Cirrus SR22 · Engine Oil PressureSDR J4PA2095Control Unit · malfunctionedALT NR 1 INFLIGHT, COULD NOT RESET, AMMETER FOR ALT NR 1 SHOWED NORMAL CHARGE SOMETIME AND 0 CHARGE OTHER TIMES. ALT NR 2 SHOWED + 100 THEN -100 AFTER NR 1 SHUTOFF. BOTH WARNING LIGHTS CAME ON. AFTER LANDING, SHUT ENGINE COMPLETELY, RESTARTED FOR GROUND RUN UPApr 2, 2007 · N584CD · Cirrus SR22 · Electrical Power SystemSDR BUW2007F00000Wheel · disintegratedEVAPORATOR BLOWER WHEEL DISINTEGRATED IN HOUSING. (K)Apr 1, 2007 · N927SE · Cirrus SR22 · Cabin Cooling SystemSDR R022366Seal Ring · debondedTEFLON (BLADE SEAL) DEBONDED FROM THE SHANK OF BLADE SN A0336 CAUSING GREASE LEAK.Mar 16, 2007 · Cirrus SR22 · Propeller AssemblySDR J4PA200701772Control Module · failedFLIGHT FROM BGF TO JZI AT 7000, 30 TO 45 MINUTES INTO FLIGHT, ALT NR 2 FAIL LIGHT CAME ON AND BATT NR 2 CB POPPED. TRIED TO RESET BUT WOULD NOT RESET. CONTINUED ONTO JZI WITH NO OTHER PROBLEMS. DID NOT LOOSE ANY OTHER SYSTEMS. TROUBLE SHOT DISCREPANCY AND FJan 21, 2007 · N121SR · Cirrus SR22 · AC Generator-AlternatorSDR 2007FA0000010Battery · leakingDURING ANNUAL INSPECTION, FOUND BATTERY COMPARTMENT CONTAMINATED BY LEAKAGE FROM D CELLS AND BATTERY TERMINALS CORRODED. BATTERIES FOUND DEAD. BATTERIES WERE INSTALLED MARCH 2004 AND HAVE A EXPIRATION DATE OF MARCH 2008. THE MODEL ELT IS CERTIFIED BY THE MFDec 18, 2006 · N910JR · Cirrus SR22 · Emergency Locator BeaconSDR 2007FA0000009Drive Assy · crackedSTARTER DRIVE WAS REMOVED FROM AIRCRAFT DUE TO SLIPPING. INSPECTION AFTER REMOVAL FOUND A CRACK EMANATING FROM THE STUD BOSS LOCATED AT APPROXIMATELY THE 7:00 POSITION. (K)Dec 18, 2006 · N249CK · Cirrus SR22 · Engine StarterSDR J4PA200601772Alternator · failedDEPARTED KMGM ON LEG2 OF TRIP 5794 DESTINATION KGMU ON 12/10 AT 11AM. OUR ROUTE OF FLIGHT WAS DIRECT SINCA INTERSECTION DIRECT GMU. THAT ROUTE KEEPS SOUTH AND CLEAR OF ATLANTA CLASS B AIRSPACE. IN LEVEL CRUISE FLIGHT AT 7000 FEET, THE ALT 1 ANNUNCIATOR LIGHDec 10, 2006 · N820CD · Cirrus SR22 · AC Generator-AlternatorSDR J4PA0001572Control Circuit · faultyAT TAKEOFF FROM LBE ON AN IFR FLT PLAN EN ROUTE TO RDU. DURING CLIMB, APPROXIMATELY 5 MINUTES AFTER TAKEOFF, THE AIRPLANE’S ALT 1 ANNUNCIATOR ILLUMINATED NR 1 ALTERNATOR FAILED. NOTICED CIRCUIT BREAKER POPPED (ALT 1). NOTIFIED ATC OF NR 1 ALTERNATOR FAILUREOct 9, 2006 · N134AJ · Cirrus SR22 · DC Generating SystemSDR 2006FA0000976Exhaust Header · crackedNR 5 EXHAUST STACH/HEADER WAS FOUND TO BE CRACKED AT THE CYLINDER FLANGE AT THE WELD.Oct 3, 2006 · N253SR · Cirrus SR22 · Reciprocating Engine Cylinder SectionSDR 2006FA0000979Exhaust Header · crackedNR 5 EXHAUST HEADER CRACKED AT CYLINDER FLANGE AT THE WELD. (K)Sep 15, 2006 · N253SR · Cirrus SR22 · Reciprocating Engine Cylinder SectionSDR 2006FA0000858Muffler · damagedLT AND RT MUFFLER FLAME ARRESTERS FOLDED OVER FROM EXHAUST GAS HEAT COMPOUNDED OVER THE 609 HOURS OF THEIR SERVICE LIFE. (K)Jul 18, 2006 · N948AH · Cirrus SR22 · Engine Collector/Tailpipe/NozzleSDR 2006FA0000677Muffler · deterioratedREPLACED LT MUFFLER ON AIRCRAFT DO TO THE DETERIORATED CONDITION OF THE SPARK ARRESTER INSIDE OF THE MUFFLER. LT SIDE SPARK ARRESTER MELTED AND FOLDED OVER. LT MUFFLER, PN 14836001. THE FIRST DETECT REPORT WAS FILED WHEN AC HAD A TT 682 HRS. BOTH LT AND RTJul 1, 2006 · N752C · Cirrus SR22 · Engine Noise SuppressorSDR 2006FA0000576Nut · splitTHRU STUD NUT SPLIT ON NR 4 CYLINDER TOP THRU STUD. (K)Jun 6, 2006 · N746C · Cirrus SR22 · Reciprocating Engine Power SectionSDR 2006FA0000504Rivet · looseBOTH LT AND RT ELEVATOR OB HINGE BRACKETS ARE RIVETED TO THE ELEVATORS WITH FLUSH HEAD BLIND RIVETS AND FLUSH HEAD SOLID DRIVE RIVETS. AT 121 HOURS TT. DURING A 100 HOUR INSPECTION, THE RIVETS ON THE OB HINGE BRACKETS, LT AND RT ELEVATORS, WERE FOUND TO BE SMay 8, 2006 · N5226R · Cirrus SR22 · Elevator Miscellaneous StructureSDR 2006FA0000518Solenoid · intermittentTHE STARTER ON THIS AIRCRAFT FAILED. THIS IS THE THIRD FAILURE OF THIS TYPE STARTER HAS A SOLENOID ATTACHED AND THE PROBLEM NOTED IS THAT THIS SOLENOID BECOMES INTERMITTENT. (K)May 5, 2006 · N343CD · Cirrus SR22 · Engine StarterSDR 2006FA0000512Flight Dir · failedPFD WAS JUST UPDATED TO REV 6. 2 DAYS AFTERWARDS, SCREEN WOULD FAIL IN FLIGHT. DISPLAY WOULD FLICKER AND NOT BE USABLE. UNIT WOULD ALSO FAIL TO BOOT UP IN HANGAR. CUSTOMER WAS GIVEN EXCHANGE. (K)Apr 21, 2006 · N629LF · Cirrus SR22 · Integrated Flight SystemSDR AVI000021Elevator · out of toleranceDURING SA 06-05 ELEVATOR GAP VISUAL INSPECTION IT WAS NOTED THAT THE GAP BETWEEN ELEVATOR TIP AND HORIZONTAL STABILIZER WAS LESS THEN 0.10 INCH, UPON FURTHER INVESTIGATION IT WAS NOTED THAT PN 11626-002 ELEVATOR HINGE, OB WAS RUBBING ON HORIZONTAL STABILIZER OApr 19, 2006 · N753CD · Cirrus SR22 · Elevator StructureSDR AMCR200600001Battery · corrodedDURING ANNUAL INSP, ELT DID NOT TEST. FOUND 2 D-CELL BATTERIES CORRODED. THESE 2 BATTERIES WERE AT THE BOTTOM OF THE STACK AND THE CORROSION WAS NOT EVIDENT AT FIRST. THERE WERE 2 YEARS REMAINING BEFORE BATTERY REPLACEMENT WAS DUE. THESE ARE THE ORIGINAL BATTEApr 5, 2006 · N679DV · Cirrus SR22 · Emergency Locator BeaconSDR 2006FA0000513Flight Dir · failedTHIS PARTICULAR PFD HAD 3 BACK TO BACK FAILURES THAT COULD ONLY BE DETECTED AFTER 1 HOUR + OF FLIGHT. DISPLAY WOULD LIGHTEN UP, TURN GREEN AND FLICKER. WOULD NOT BE USABLE. THIS UNIT WAS UPGRADED TO REV 6 SOFTWARE FOR FLIGHT DIRECTOR. FAILURES HAPPENED AFTApr 4, 2006 · N623KT · Cirrus SR22 · Integrated Flight SystemSDR 2006FA0000239Relief Valve · restrictedLOSS OF OIL PRESSURE, INSPECTED OIL PRESSURE RELIEF VAVLE AND FOUND TIP OF DRILL BIT LODGED IN RELIEF VALVE. REMOVED TIP OF DRILL BIT AND REASSEMBLED RELIEF VALVE. GROUND RAN, OPS CHECKED GOOD. (K)Mar 15, 2006 · N216N · Cirrus SR22 · Reciprocating Engine Oil SystemSDR 2006FA0000236Flight Dir · intermittentJUST GOT 2003 SR22 BACK FROM GETTING REVISION 6 COMPLETED. PUT ABOUT 10 HOURS ON THE AIRPLANE. TWICE DURING THIS TRIP, THE PFD DISPLAY ROTATED OR ROLLED LIKE THE OLD TELEVISION SETS DID. ONCE FOR ONLY 2 OR 3 SECONDS AND ANOTHER TIME FOR MAYBE 10 TO 20 SECONFeb 27, 2006 · N56FS · Cirrus SR22 · Flight Management Computing Hardware SystemSDR 2006FA0000186Torque Tube · wornINSPECTED THE FLIGHT CONTROL SYSTEM IAW SB AND FOUND FREE PLAY AT THE TORQUE TUBE/ END FITTING INTERFACE ON BOTH SIDES. THE RIGHT SIDE WAS MORE PORNOUNCED THAN THE LEFT. MFG CONSIDERS THIS SB TO BE OPTIONAL, HOWEVER THE CONTINUED USE WITH THIS DEFECT WILL REFeb 15, 2006 · N150X · Cirrus SR22 · Flight Control SystemSDR 2006FA0000185Torque Tube · wornINSPECTED THE FLIGHT CONTROL SYS IAW SB AND FOUND FREE PLAY AT THE TORQUE TUBE/ END FITTING INTERFACE ON BOTH SIDES. THE RT SIDE WAS MOR PRONOUNCED THAN THE LT. MFG CONSIDERS THIS SB TO BE OPTIONAL, HOWEVER THE CONTINUED USE WITH THIS DEFECT WILL RESULT IN TFeb 15, 2006 · N150X · Cirrus SR22 · Flight Control SystemSDR 2006FA0000198Electrical Box · faultyOPERATOR REPORTS THREE CASES OF UNCOMMANDED ENGINE STARTER ENGAGEMENT. IN TWO CASES, STARTER ENGAGED WHEN THE BATTERY MASTER WAS TURNED ON. IN THE THIRD CASE, OPERATOR STATES THAT THE SHIP'S BATTERY CAME ON LINE UNCOMMANDED AND THAT STARTER CONCURRENTLY ENGAFeb 10, 2006 · Cirrus SR22 · DC Power Distribution SystemSDR 2006FA0000004Dipstick · brokenDURING PREFLIGHT WHILE CHECKING OIL LEVEL ON DIPSTICK, THE ENTIRE ROD PORTION OF THE DIPSTICK CAME APART IN MY HANDS UPON LIFTING IT OUT OF THE OIL FILLER TUBE. BARELY CAUGHT IT WITH MY HAND BEFORE IT WOULD'VE FALLEN DOWN INSIDE THE ENGINE CRANK CASE WITH POTEJan 4, 2006 · N5175L · Cirrus SR22 · Reciprocating Engine Oil SystemSDR 2006FA0000003Dipstick · brokenDURING PREFLIGHT WHILE CHECKING OIL LEVEL ON DIPSTICK, ENTIRE ROD PORTION OF DIPSTICK CAME APART IN MY HANDS UPON LIFTING IT OUT OF OIL FILLER TUBE. BARELY CAUGHT IT WITH MY HAND BEFORE IT WOULD'VE FALLEN DOWN INSIDE THE ENGINE CRANKCASE WITH POTENTIALLY CATAJan 4, 2006 · N5175L · Cirrus SR22 · Reciprocating Engine Oil System
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