# N442JS: 2024 Cirrus Design SR20 - Status: Valid registration - Airframe: [Cirrus Design SR20](https://openairdocs.org/model/cirrus-design-sr20) (registry code 2130000, 4 seats) - Engine: [Lycoming IO-390-C3B6](https://openairdocs.org/engine/lycoming-io-390-c3b6) (registry code 42710) - Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH) (Cirrus Design Corporation), [TCDS E00006NY](https://openairdocs.org/tcds/E00006NY) (Lycoming Engines) (OpenAirDocs) - Serial number: 9948 - Year built: 2024 - Type: Fixed wing single engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: June 2, 2024 - Certificate issued: February 28, 2026 - Expires: February 28, 2033 - Mode S code: A552E4 - Registered owner: [Prelude Aviation LLC](https://openairdocs.org/faa-owner/PRELUDE%20AVIATION%20LLC) - Location: [Rockledge, FL](https://openairdocs.org/faa-place/FL/Rockledge) - Owner type: LLC - Owner's area on the map: 28.2888° N, 80.7914° W: Placed by OpenAirDocs at the center of ZIP code 32955, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=442JS - Page: https://openairdocs.org/aircraft/N442JS From the FAA registry file of October 21, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 15 in force ### Matched by airframe (Cirrus Design SR20) - [AD 2024-24-11](https://openairdocs.org/ad/2024-24-11): Power Lever · Cirrus Design SR20, SR22 and SR22T. Effective Dec 23, 2024 - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI). Effective Mar 21, 2022 - [AD 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009 - [AD 2008-14-13](https://openairdocs.org/ad/2008-14-13): Upper door hinge · Cirrus Design SR20 and SR22. Effective Aug 14, 2008 - [AD 2008-11-18](https://openairdocs.org/ad/2008-11-18): Heat exchanger · Cirrus Design SR20. Effective Jul 7, 2008 - [AD 2008-03-16](https://openairdocs.org/ad/2008-03-16): Rudder, aileron, and rudder-aileron interconnect rigging · Cirrus Design SR20 and SR22. Effective Mar 11, 2008 - [AD 2007-14-03](https://openairdocs.org/ad/2007-14-03): Cirrus Airplane Parachute System (CAPS) · Cirrus Design SR20 and SR22. Effective Aug 16, 2007 - [AD 2006-21-03](https://openairdocs.org/ad/2006-21-03): Brake caliper piston O-ring seals · Cirrus Design SR20 and SR22. Effective Nov 17, 2006 - [AD 2006-19-10](https://openairdocs.org/ad/2006-19-10): Adjust crew seat break-over bolts · Cirrus Design SR20 and SR22. Effective Oct 24, 2006 - [AD 2006-07-06](https://openairdocs.org/ad/2006-07-06): Wire harness · Cirrus Design SR20 and SR22. Effective May 11, 2006 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2002-24-08](https://openairdocs.org/ad/2002-24-08): Cable clamp · Cirrus Design SR20 and SR22. Effective Jan 24, 2003 - [AD 2002-21-02](https://openairdocs.org/ad/2002-21-02): Self-locking retaining nut · Cirrus Design SR20 and SR22. Effective Nov 8, 2002 - [AD 2001-25-03](https://openairdocs.org/ad/2001-25-03): Rivets In Elevator and Rudder · Cirrus Design SR20 and SR22. Effective Dec 17, 2001 ### Matched by engine (Lycoming IO-390-C3B6) - [AD 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026 ### Historical (superseded or no longer in force) - [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008 - [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008 - [AD 2005-17-19](https://openairdocs.org/ad/2005-17-19) (historical): Crew seat recline locks · Cirrus Design SR20 and SR22. Effective Oct 13, 2005 - [AD 2002-05-05](https://openairdocs.org/ad/2002-05-05) (historical): Limitation Section - Cirrus Aircraft Parachute System (CAPS) Activation Cable · Cirrus Design SR20 and SR22. Effective Mar 19, 2002 ## Information bulletins (advisory) (16 in force) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-11-50](https://openairdocs.org/saib/CE-11-50): Flight Controls, Flaps. Issued Aug 26, 2011 - [SAIB CE-08-12R1](https://openairdocs.org/saib/CE-08-12R1): Electrical Power. Issued Mar 16, 2011 - [SAIB CE-11-09](https://openairdocs.org/saib/CE-11-09): Navigation Flight Management Computing Software System. Issued Jan 5, 2011 - [SAIB CE-09-46](https://openairdocs.org/saib/CE-09-46): Landing Gear, Nose. Issued Jul 31, 2009 - [SAIB CE-09-32](https://openairdocs.org/saib/CE-09-32): Navigation: Cirrus Aircraft Under-Glareshield GPS/WAAS Antenna Mount. Issued May 29, 2009 - [SAIB CE-09-01](https://openairdocs.org/saib/CE-09-01): Equipment - Emergency. Issued Oct 21, 2008 - [SAIB CE-07-08](https://openairdocs.org/saib/CE-07-08): Avidyne Primary Flight display (PFD). Issued Oct 31, 2006 - [SAIB CE-06-30](https://openairdocs.org/saib/CE-06-30): . Issued Feb 9, 2006 - [SAIB CE-06-07](https://openairdocs.org/saib/CE-06-07): . Issued Nov 4, 2005 - [SAIB CE-05-88](https://openairdocs.org/saib/CE-05-88): . Issued Sep 30, 2005 - [SAIB CE-05-77](https://openairdocs.org/saib/CE-05-77): . Issued Jul 27, 2005 - [SAIB CE-04-74](https://openairdocs.org/saib/CE-04-74): . Issued Aug 3, 2004 - [SAIB CE-03-09](https://openairdocs.org/saib/CE-03-09): . Issued Dec 16, 2002 - [SAIB CE-02-34](https://openairdocs.org/saib/CE-02-34): . Issued Jun 19, 2002 - [SAIB NE-19-08](https://openairdocs.org/saib/NE-19-08): Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve Cylinders. Issued May 2, 2019 - [SAIB CE-08-12](https://openairdocs.org/saib/CE-08-12) (historical): Electrical Power. Issued Feb 27, 2008 ## NTSB investigations None matched to N442JS. ## FAA accident and incident reports None matched to N442JS. ## Reports on N442JS not matched to an aircraft (2) They name N442JS, but no registry record covers the event date, or the aircraft registered then was built later. - [Incident 20010603012439I](https://openairdocs.org/incident/20010603012439I), Jun 3, 2001: Dorner DO328100 (N442JS), Pittsburgh, PA. (-23)On June 3, 2001, at 1335E, a DO-328-100, registered as N442JS and operating as vnaa flight #4021 landed at "pit" after reporting a nose landing gear… - [Incident 20000605032459I](https://openairdocs.org/incident/20000605032459I), Jun 5, 2000: Dorner DO328100 (N442JS), Binghamton, NY. (-23)On June 5, 2000, N442JS, dornier 328, operated by psa (vnvaa), declared an emergency and LANDE3D at Binghamton airport (kbgm). The flight was enroute from… ## Service difficulty reports (77, newest 50) As reported by operators and repair stations. - [SDR VNAA0403004](https://openairdocs.org/sdr/VNAA0403004), Mar 2, 2004: SMOKE DETECTOR. FAILED. THE CREW REPORTED RECEIVING A LAV SMOKE DETECT FAIL. MAINTENANCE INSPECTED AND DEFERRED THE APU IN ACCORDANCE WITH MEL 49-1 CODE C. - [SDR VNAA0403001](https://openairdocs.org/sdr/VNAA0403001), Mar 1, 2004: SMOKE DETECTOR. FAILED. THE CREW REPORTED RECEIVING A SMOKE LAV CAS MESSAGE. MAINTENANCE THEN DEFERRED THE LAVATORY SMOKE DETECTOR PER MEL 26-3 CODE C. THE AIRCRAFT WAS THEN RELEASED F - [SDR VNAA0402012](https://openairdocs.org/sdr/VNAA0402012), Feb 29, 2004: SMOKE DETECTOR. FAILED. THE CREW REPORTED RECEIVING A LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND FOUND A LOOSE BACKSHELL TO THE LAV SMOKE DETECTOR AND TIGHTENED IN ACCORDANCE WIT - [SDR VNAA0402011](https://openairdocs.org/sdr/VNAA0402011), Feb 28, 2004: SMOKE DETECTOR. FAILED. THE CREW REPORTED RECEIVING AN INTERMITTENT LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENA - [SDR VNAA0310018](https://openairdocs.org/sdr/VNAA0310018), Oct 22, 2003: POWER LEVER. FAILED. DURING TAKEOFF, THE CREW EXPERIENCED A LEFT HAND POWER LEVER BEING STIFF AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND LUBED THE POWER LEVER IN ACCORDANCE WITH - [SDR VNAA0310016](https://openairdocs.org/sdr/VNAA0310016), Oct 22, 2003: ROD. FAILED. DURING FLIGHT, THE CREW RECEIVED A PASSENGER OPEN INDICATION IN FLIGHT AND RETURNED TO DAY. MAINTENANCE INSPECTED AND ADJUSTED THE PASSENGER DOOR ROD IN ACCORDA - [SDR VNAA0305007](https://openairdocs.org/sdr/VNAA0305007), May 12, 2003: EJECTOR. FAILED. DURING CLIMBOUT, THE CREW RECEIVED AN AIRFOIL DE-ICE FAIL INDICATION. FLIGHT 4176 THEN RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE 17HH EJECTOR FLOW - [SDR VNAA0303006](https://openairdocs.org/sdr/VNAA0303006), Mar 6, 2003: GENERATOR. FAILED. DURING TAKE OFF, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND ABORTED TAKE OFF. THE GENERAOR WAS RESET AND THE FLIGHT WAS CLEARED FOR ANOTHER TA - [SDR VNAA0212028](https://openairdocs.org/sdr/VNAA0212028), Dec 22, 2002: POWER SUPPLY. FAILED. THE CREW REPORTED THAT THE EMERGENCY BACK UP BATTERY FAILS TO TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAI - [SDR VNAA0212003](https://openairdocs.org/sdr/VNAA0212003), Dec 3, 2002: VALVE. FAILED. WHILE ENROUTE TO DCA, THE CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE AND DIVERTED TO PHL. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY - [SDR VNAA0211004](https://openairdocs.org/sdr/VNAA0211004), Nov 5, 2002: WINDSHIELD. FAILED. ENROUTE, THE CREW RECEIVED A WINDSHIELD HEAT FAIL CAS MESSAGE. FLIGHT 4039 WAS IN ICING CONDITIONS AND AFTER REVIEWING THE WEATHER FOR THE REST OF THE ROUTE, MA - [SDR VNAA0208028](https://openairdocs.org/sdr/VNAA0208028), Aug 19, 2002: WARNING SYSTEM. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A FUEL FEED TEMPERATURE CAS MESSAGE AND ABORTED TAKEOFF. WHEN FLIGHT 4150 CLEARED THE RUNWAY THE MESSAGE CLEARED. THE CREW CAL - [SDR VNAA0208029](https://openairdocs.org/sdr/VNAA0208029), Aug 19, 2002: SENSOR. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A FUEL FEED TEMPERATURE CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE CONTROL DISPATCHED DAY MAINTENANCE. MAINTENANCE IN PHL IN - [SDR VNAA0208005](https://openairdocs.org/sdr/VNAA0208005), Aug 5, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY BATTERY AT THE 7LK LOCATION WAS NOT WORKING PROPERLY. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 7LK P - [SDR VNAA0207043](https://openairdocs.org/sdr/VNAA0207043), Jul 29, 2002: POWER SUPPLY. FAILED. THE CREW REPORTED THAT THE EMERGENCY BACK UP BATTERY WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MA - [SDR VNAA0207034](https://openairdocs.org/sdr/VNAA0207034), Jul 24, 2002: BATTERY. DISCHARGED. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING AT ROW 10A. MAINTENANCE INSPECTED AND REPLACED THE 7LK EMERGENCY BATTERY IN ACCORDANCE - [SDR VNAA0206018](https://openairdocs.org/sdr/VNAA0206018), Jun 25, 2002: ECU. FAILED. DURING TAKE OFF, THE CREW RECEIVED A RIGHT HAND ENGINE CONTROL UNIT AND GENERATOR FAIL INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAG - [SDR VNAA0206003](https://openairdocs.org/sdr/VNAA0206003), Jun 4, 2002: CONTROL UNIT. MALFUNCTIONED. DURING THE TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE CONTROL UNIT LAT MODE FAIL CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY THE MESSAGE CLEARED - [SDR VNAA0205019](https://openairdocs.org/sdr/VNAA0205019), May 29, 2002: FLIGHT DIR. MALFUNCTIONED. DURING TAKEOFF, THE FLIGHT DIRECTOR FAILED AND THE CREW ABORTED TAKEOFF. FLIGHT 4124 RETURNED TO THE GATE AND MAINTENANCE DEFERRED THE FLIGHT DIRECTOR, 22-5 COD - [SDR VNAA0205018](https://openairdocs.org/sdr/VNAA0205018), May 29, 2002: FLIGHT DIR. MALFUNCTIONED. DURING TAKEOFF, THE FLIGHT DIRECTOR FAILED AND THE CREW ABORTED TAKEOFF. THE CREW EXITED THE RUNWAY AND THE MESSAGE CLEARED. FLIGHT 4124 WAS THEN CLEARED FOR AN - [SDR VNAA0204023](https://openairdocs.org/sdr/VNAA0204023), Apr 25, 2002: LEAD. BROKEN. WHILE PASSING THROUGH 19,000 FEET, THE CREW RECEIVED A RIGHT HAND PROP HEAT FAIL MESSAGE. THE CREW RESET THE SYSTEM BUT IT FAILED AGAIN. THE CREW WAS ADVISED TH - [SDR VNAA0204004](https://openairdocs.org/sdr/VNAA0204004), Apr 11, 2002: MECHANISM. STUCK. DURING TAKEOFF THE CREW HEARD AIR RUSHING. THE CREW DETERMINED THAT THE NOSE GEAR DOOR REMAINED OPEN AFTER THE GEAR WAS SELECTED UP. THE FLIGHT RETURNED TO PHL - [SDR VNAA0203026](https://openairdocs.org/sdr/VNAA0203026), Mar 16, 2002: SENSOR. FAILED. THE FLIGHT CREW WAS CLIMBING OUT OF PIT WHEN THE RIGHT ENGINE FUEL FEED TEMPERATURE WENT TO 78 DEGREES C. THE FLIGHT CREW FOLLOWED THE QRH PROCEDURES BUT THE TE - [SDR VNAA0203025](https://openairdocs.org/sdr/VNAA0203025), Mar 16, 2002: COMPUTER. MALFUNCTIONED. THE FLIGHT WAS ON THE TAKEOFF ROLL WHEN THE FLIGHT CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL WARNING MESSAGE ON THE EICAS DISPLAY. THE FLIGHT CREW ABORTED T - [SDR VNAA0202025](https://openairdocs.org/sdr/VNAA0202025), Feb 25, 2002: WARNING SYSTEM. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL INDICATION AND ABORTED TAKEOFF. AS THE AIRCRAFT CLEARED THE RUNWAY THE INDICATION EXTINGUISHED - [SDR VNAA0201018](https://openairdocs.org/sdr/VNAA0201018), Jan 21, 2002: DISPLAY. MALFUNCTIONED. DURING TAKEOFF, THE CAPTAIN'S HEADING MODE ROLLED ON THE MULTI FUNCTION DISPLAY UNIT AND THE CREW ABORTED TAKEOFF. THE MULTI FUNCTION DISPLAY UNIT CLEARED ITSEL - [SDR VNAA0201004](https://openairdocs.org/sdr/VNAA0201004), Jan 3, 2002: DAU. FAILED. DURING THE TAKE OFF ROLL, THE CREW RECEIVED AN AMBER BOXED NL EICAS AND ABORTED TAKE OFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND RERACKED THE DATA A - [SDR VNAA0112006](https://openairdocs.org/sdr/VNAA0112006), Dec 8, 2001: WARNING SYSTEM. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A AMBER GPWS CAS MESSAGE AND ABORTED TAKEOFF. AS THE AIRCRAFT TAXIED OFF THE RUNWAY THE MESSAGE CLEARED. FLIGHT 4048 WAS CLEAR - [SDR VNAA0109010](https://openairdocs.org/sdr/VNAA0109010), Sep 16, 2001: COMPUTER. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL MESSAGE AND ABORTED TAKEOFF. AS FLIGHT 4065 EXITED THE RUNWAY THE MESSAGE CLEARED. THE CREW CO - [SDR VNAA0108018](https://openairdocs.org/sdr/VNAA0108018), Aug 27, 2001: FAN. FAILED. DURING THE TAXI FROM THE GATE, THE CREW NOTICED A LEFT HAND PACK OVERHEAT LIGHT. THE FLIGHT ATTENDANT THEN REPORTED THERE WAS SMOKE IN THE CABIN. THE CREW RETUR - [SDR VNAA0108009](https://openairdocs.org/sdr/VNAA0108009), Aug 16, 2001: COMPUTER. MALFUNCTIONED. DURING THE TAKEOFF ROLL, THE CREW RECEIVED A FGC HEADING HOLD FAIL AMBER CAS MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE SYSTEM AND WAS CLEARED FOR ANOTHER - [SDR VNAA0106002](https://openairdocs.org/sdr/VNAA0106002), Jun 3, 2001: BULB. FAILED. DURING DESCENT, THE CREW RECEIVED NO GEAR DOWN INDICATION FOR THE NOSE GEAR. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK. THE CREW DECLARED A EMERGENCY AND - [SDR VNAA0105005](https://openairdocs.org/sdr/VNAA0105005), May 8, 2001: WARNING SYSTEM. ACTIVATED. DURING THE TAKEOFF ROLL, THE CREW RECEIVED A FGC LATERAL MODE FAIL CAS MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK AND ABORTED TAKEOFF. THE MESSAG - [SDR VNAA0103018](https://openairdocs.org/sdr/VNAA0103018), Mar 30, 2001: LIGHT. INOPERATIVE. THE FLIGHT CREW REPORTED THAT THE EMERGENCY FLOOR PATHWAY LIGHT WOULD NOT ILLUMINATE ADJACENT TO THE CABIN SEAT ROW 4 POSITION. MAINTENANCE REPLACED THE FLOOR P - [SDR VNAA0103002](https://openairdocs.org/sdr/VNAA0103002), Mar 3, 2001: BATTERY. DISCHARGED. THE FLIGHT CREW REPORTED THAT A SECTION OF THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE 5LK BATTERY IN ACCORDANCE WITH DORNIER MA - [SDR VNAA0102015](https://openairdocs.org/sdr/VNAA0102015), Feb 22, 2001: PUMP. FAILED. ON LANDING IN EVV THE FLIGHT CREW REPORTED A LEFT ENGINE ELECTRONIC CONTROL UNIT FAILED. MAINTENANCE INSPECTED AND CLEANED THE CONNECTOR FOR THE ELECTRONIC CONT - [SDR VNAA0101010](https://openairdocs.org/sdr/VNAA0101010), Jan 15, 2001: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING AT ROWS 4 AND 7 WERE NOT WORKING. THE AIRCRAFT WAS FERRIED TO PIT WERE MAINTENANCE INSPECTED AND REPLACED THE EMER - [SDR VNAA0101007](https://openairdocs.org/sdr/VNAA0101007), Jan 10, 2001: POWER SUPPLY. FAILED. THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY WILL NOT TEST. THE AIRCRAFT WAS FERRIED TO PIT WHERE MAINTENANCE INSPECT AND REPLACED THE EMERGENCY POWER SUPP - [SDR VNAA0012017](https://openairdocs.org/sdr/VNAA0012017), Dec 20, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY TRACK LIGHTING AT ROWS 3 TO 6 WERE NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 5LK PO - [SDR VNAA0012013](https://openairdocs.org/sdr/VNAA0012013), Dec 14, 2000: ESCAPE HATCH. DIRTY. PIT - FLIGHT 4123 - DURING CLIMB-OUT, THE CAPTAIN HAD WATER DRIPPING ON HIM FROM THE CREW EMERGENCY DOOR ON TOP OF THE FUSELAGE. RETURNED TO PIT WHERE MAINTENAN - [SDR VNAA0011028](https://openairdocs.org/sdr/VNAA0011028), Nov 26, 2000: FACE PLATE. THE CREW REPORTED THAT THE FACE PLATE OF THE EMERGENCY EXIT SIGN ABOVE THE PASSENGER DOOR WAS MISSING. MAINTENANCE FOUND THE FACE PLATE BEHIND THE FLIGHT ATTEND - [SDR VNAA0011016](https://openairdocs.org/sdr/VNAA0011016), Nov 17, 2000: WARNING SYSTEM. ACTIVATED. DURING THE TAKEOFF ROLL, FLIGHT 4027 HAD A ICE CAS MESSAGE AND ABORTED TAKEOFF. AFTER CLEARING THE RUNWAY THE MESSAGE CLEARED AND FLIGHT 4027 WAS CLEARED FOR AN - [SDR VNAA0010014](https://openairdocs.org/sdr/VNAA0010014), Oct 20, 2000: DOOR. OPEN. AFTER TAKE OFF, THE AIRCRAFT WAS CLIMBING THROUGH 3000 FEET THE CREW NOTICED A LOSS OF PRESSURIZATION FOLLOWED BY A DOOR LIGHT AND VIBRATION IN THE RUDDER PEDAL - [SDR VNAA0009006](https://openairdocs.org/sdr/VNAA0009006), Sep 12, 2000: SENSOR. FAILED. WHEN FLIGHT 4169 BEGAN THE TAKEOFF ROLL, THE CREW RECEIVED A LEFT HAND ANGLE OF ATTACK FAIL AND NUMBER TWO PROBE FAIL MESSAGE. THE CREW ABORTED TAKEOFF AND EXIT - [SDR VNAA0008001](https://openairdocs.org/sdr/VNAA0008001), Aug 2, 2000: SENSOR. FAILED. DURING TAKEOFF, AN ANGLE OF ATTACK SENSOR FAILED AND THE CREW ABORTED TAKEOFF. MAINTENANCE PERFORMED OPERATIONAL CHECKS WITH THE CREW IN ACCORDANCE WITH DORNIER - [SDR VNAA0006002](https://openairdocs.org/sdr/VNAA0006002), Jun 5, 2000: WARNING SYSTEM. ACTIVATED. WHILE EN ROUTE, THE CREW RECEIVED A EMERGENCY PARK ACCUMULATOR AMBER CAS MESSAGE. THE CREW FOLLOWED THE PROCEDURES IN THE QUICK REFERENCE HANDBOOK AND COULD NOT - [SDR VNAA0005001](https://openairdocs.org/sdr/VNAA0005001), May 1, 2000: WARNING SYSTEM. ACTIVATED. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND SHAKER FAIL CAS MESSAGE. THE CREW ABORTED TAKEOFF AND CONTACTED MAINTENANCE CONTROL. MAINTENANCE CONTROL HAD THE C - [SDR VNAA0003013](https://openairdocs.org/sdr/VNAA0003013), Mar 12, 2000: POWER SUPPLY. FAILED. THE FLIGHT CREW REPORTED THAT THE EMERGENCY EXIT PATHWAY LIGHTS WOULD NOT ILLUMINATE AT CABIN SEAT ROWS 7 THROUGH 9. MAINTENANCE REPLACED THE EMERGENCY BATTERY - [SDR 20000329SH036](https://openairdocs.org/sdr/20000329SH036), Mar 4, 2000: TIRE. FAILED. DEFECT: TREAD/SIDEWALL FAILURE. CAUSE: UNDER INVESTIGATION. PREVENTIVE ACTION: PENDING COMPLETION OF INVESTIGATION. (X) - [SDR VNAA0003003](https://openairdocs.org/sdr/VNAA0003003), Mar 2, 2000: POWER SUPPLY. FAILED. FLIGHT CREW REPORTED A SECTION OF THE EMERGENCY TRACK LIGHTING OUT AT ROW 5, 6 AND 7. MAINTENANCE INSPECTED AND RERACKED THE POWER SUPPLY AT 6LK IN ACCORDANCE W All 77: https://openairdocs.org/aircraft/N442JS/reports.md ## Related - Other Cirrus Design SR20 aircraft: https://openairdocs.org/model/cirrus-design-sr20/aircraft.md - STCs for the Cirrus Design SR20: https://openairdocs.org/model/cirrus-design-sr20/stcs.md - The Lycoming IO-390-C3B6 engine: https://openairdocs.org/engine/lycoming-io-390-c3b6.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.