# N461PS: 2000 Cessna 560XL - Status: Valid registration - Airframe: [Cessna 560XL](https://openairdocs.org/model/cessna-560xl) (registry code 2076702, 13 seats) - Engine: [Pratt & Whitney Canada PW545 series](https://openairdocs.org/engine/pratt-whitney-canada-pw545-series) (registry code 52154) - Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE) (Textron Aviation Inc.), [TCDS E00059EN](https://openairdocs.org/tcds/E00059EN) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: 560-5059 - Year built: 2000 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 8, 2000 - Certificate issued: August 26, 2013 - Expires: August 31, 2029 - Mode S code: A59EA8 - Registered owner: [Omni Air LLC](https://openairdocs.org/faa-owner/OMNI%20AIR%20LLC) - Location: [Chesapeake, VA](https://openairdocs.org/faa-place/VA/Chesapeake) - Owner type: LLC - Owner's area on the map: 36.8004° N, 76.4212° W: Placed by OpenAirDocs at the center of ZIP code 23321, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=461PS - Page: https://openairdocs.org/aircraft/N461PS From the FAA registry file of October 24, 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. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PW545 model are included. ## ADs that may apply (OpenAirDocs): 20 in force ### Matched by airframe (Cessna 560XL) - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2025-11-09](https://openairdocs.org/ad/2025-11-09): Fire Protection · Textron 560 and 560XL. Effective Jul 11, 2025 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2020-26-05](https://openairdocs.org/ad/2020-26-05): POWER LEVER · Textron 560XL. Effective Dec 17, 2020 - [AD 2017-04-14](https://openairdocs.org/ad/2017-04-14): Electrical power · Textron 560XL. Effective Mar 9, 2017 - [AD 2012-26-15 R1](https://openairdocs.org/ad/2012-26-15-R1): Navigation · Agusta AW139, A318-111, A318-112 and 70 more. Effective Dec 3, 2014 - [AD 2014-18-01](https://openairdocs.org/ad/2014-18-01): Navigation · Bombardier ATR42-200, ATR42-300, ATR42-320 and 23 more. Effective Oct 14, 2014 - [AD 2013-09-11](https://openairdocs.org/ad/2013-09-11): Air Conditioning · Cessna 500, 501, 550 and 5 more. Effective Jul 5, 2013 - [AD 2012-09-01](https://openairdocs.org/ad/2012-09-01): Landing Gear · Cessna 560XL. Effective Jun 7, 2012 - [AD 2012-06-01](https://openairdocs.org/ad/2012-06-01): Fuselage · Cessna 560XL. Effective Apr 25, 2012 - [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010 - [AD 2007-11-17](https://openairdocs.org/ad/2007-11-17): Wires for the positive and negative terminal studs of the engine and/or auxiliary power unit (APU) fire extinguishing bottles. · Cessna 500, 501, 550 and 5 more. Effective Jul 6, 2007 - [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001 - [AD 2001-14-09](https://openairdocs.org/ad/2001-14-09): Wiring of the Landing Light Switch and theJ-Box Fairing Light Relays · Cessna 560XL. Effective Jul 26, 2001 - [AD 2000-15-51](https://openairdocs.org/ad/2000-15-51): Aileron Cable Fairlead Tube and Aileron Cable Sector · Cessna 560XL. Effective Aug 14, 2000 - [AD 2000-03-09](https://openairdocs.org/ad/2000-03-09): Residual Ice · Cessna 560 and 560XL. Effective Apr 3, 2000 - [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998 - [AD 94-01-04](https://openairdocs.org/ad/94-01-04): Traffic Alert and Collision Avoidance System · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 136 more. Effective Feb 4, 1994 ### Matched by engine (Pratt & Whitney Canada PW545 series) - [AD 2010-18-09](https://openairdocs.org/ad/2010-18-09): Bleed valve/servo valve · Pratt & Whitney Canada PW545A, PW545B and PW530A. Effective Sep 10, 2010 - [AD 2003-03-21](https://openairdocs.org/ad/2003-03-21): Flexible Fuel Tubes · Pratt & Whitney Canada PW530A, PW535A and PW545A. Effective Feb 20, 2003 ### Historical (superseded or no longer in force) - [AD 2012-26-15](https://openairdocs.org/ad/2012-26-15) (historical): Navigation · Agusta AW139, A318-111, A318-112 and 71 more. Effective Jan 24, 2013 - [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006 - [AD 2006-04-10](https://openairdocs.org/ad/2006-04-10) (historical): Identification sleeves · Cessna Aircraft Company, The 500, 550, 560 and 3 more. Effective Mar 24, 2006 ## Information bulletins (advisory) (4 in force) - [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021 - [SAIB CE-10-29R1](https://openairdocs.org/saib/CE-10-29R1): Lights Aft Side Ledger Divider Light. Issued May 21, 2010 - [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010 - [SAIB 2024-06](https://openairdocs.org/saib/2024-06): Oil Servicing Issues on Pratt & Whitney Canada PW545 Series Engines. Issued Nov 18, 2024 - [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021 - [SAIB CE-10-29](https://openairdocs.org/saib/CE-10-29) (historical): Lights Aft Side Ledger Divider Light. Issued Apr 28, 2010 ## NTSB investigations None matched to N461PS. ## FAA accident and incident reports None matched to N461PS. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N461PS not matched to an aircraft (50) They name N461PS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR VNAA0305005](https://openairdocs.org/sdr/VNAA0305005), May 8, 2003: WARNING LIGHT. ILLUMINATED. DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND AC VOLT FAIL INDICATION AND ABORTED TAKEOFF. WHILE TAXIING TO THE GATE THE INDICATION CLEARED AND THE CREW CALLED - [SDR VNAA0302023](https://openairdocs.org/sdr/VNAA0302023), Feb 25, 2003: CONTROL ROD. ENROUTE, THE CREW RECEIVED A MAIN CABIN DOOR RED WARNING PANEL LIGHT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND LANDED AT THE NEAREST SUITABLE AIRPORT, - [SDR VNAA0301016](https://openairdocs.org/sdr/VNAA0301016), Jan 15, 2003: WARNING SYSTEM. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE CREW CALLED MAINTENANCE CONTROL AND THE MESSAGE HAD CLEARED. MAIN - [SDR VNAA0301013](https://openairdocs.org/sdr/VNAA0301013), Jan 12, 2003: SWITCH. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION HORN AND RED WARNING PANEL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE POWE - [SDR VNAA0301012](https://openairdocs.org/sdr/VNAA0301012), Jan 11, 2003: WARNING SYSTEM. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A PROP SPEED WARNING CAS MESSAGE AND ABORTED TAKEOFF. THE CREW THEN TAXIED OFF THE RUNWAY AND CALLED MAINTENANCE CONTROL. THE - [SDR VNAA0301009](https://openairdocs.org/sdr/VNAA0301009), Jan 9, 2003: RACK. DEFECTIVE. DURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND REPLA - [SDR VNAA0301008](https://openairdocs.org/sdr/VNAA0301008), Jan 8, 2003: PROXIMITY SENSOR. OUT OF ADJUST. EN ROUTE, THE CREW RECEIVED A 9A EMERGENCY DOOR LIGHT INDICATION ON THE RED WARNING PANEL. FLIGHT DESCENDED TO 9000 FEET AND THE LIGHT WENT OUT. MAINTENANCE INS - [SDR VNAA0301004](https://openairdocs.org/sdr/VNAA0301004), Jan 5, 2003: WARNING SYSTEM. MALFUNCTIONED. DURING FLIGHT, THE CREW RECEIVED A 9A EMERGENCY EXIT DOOR OPEN IN FLIGHT INDICATION BUT WAS VERIFIED TO BE CLOSED. UPON LANDING AT CVG, OUTSTATION INSPECTED, CL - [SDR VNAA0211019](https://openairdocs.org/sdr/VNAA0211019), Nov 18, 2002: TIRE. FAILED. DURING TAKE OFF, THE CREW EXPERIENCED A NOSE WHEEL VIBRATION AND ABORTED TAKE OFF. MAINTENANCE AND TIRES WERE THEN SENT TO DCA. MAINTENANCE INSPEECTED AND REPLA - [SDR VNAA0211018](https://openairdocs.org/sdr/VNAA0211018), Nov 15, 2002: CONTROL UNIT. MALFUNCTIONED. DURING TAKEOFF AT 45 KNOTS, THE CREW RECEIVED A FLIGHT GUIDANCE CONTROL UNIT MESSAGE AND ABORTED TAKEOFF. AFTER CLEARING THE RUNWAY THE MESSAGE CLEARED BY ITSEL - [SDR VNAA0211010](https://openairdocs.org/sdr/VNAA0211010), Nov 10, 2002: PUMP. FAILED. DURING CLIMB, THE CREW RECEIVED A MAIN HYDRAULIC INOP BLUE CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK PROCEDURE AND THE MESSAGE DID NOT CLEAR. - [SDR VNAA0209017](https://openairdocs.org/sdr/VNAA0209017), Sep 14, 2002: WARNING SYSTEM. MALFUNCTIONED. DURING TAKEOFF, THE CREW EXPERIENCED A DISPLAY UNIT 5 AND A WEIGHT ON WHEELS 1 FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND HAD THE CREW CYCL - [SDR VNAA0208036](https://openairdocs.org/sdr/VNAA0208036), Aug 24, 2002: WARNING SYSTEM. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A TAKE OFF CONFIGURATION CAS MESSAGE AND ABORTED TAKEOFF. THE MESSAGE THEN EXTINGUISHED BY ITSELF AND FLIGHT 4102 WAS CLEARED - [SDR VNAA0208020](https://openairdocs.org/sdr/VNAA0208020), Aug 12, 2002: COMPUTER. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE CONTROL FAIL MESSAGE AND ABORTED TAKEOFF. WHEN THE FLIGHT TAXIED ONTO THE TAXIWAY, THE MESSAGE CLEARED. THE - [SDR VNAA0207046](https://openairdocs.org/sdr/VNAA0207046), Jul 30, 2002: DRAIN LINE. BROKEN. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND BLEED SHUT OFF VALVE FAIL MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND FOUND A BROKEN DRAIN TUBE ON THE - [SDR VNAA0207007](https://openairdocs.org/sdr/VNAA0207007), Jul 9, 2002: CONNECTOR. DIRTY. EN ROUTE FROM PIT TO CVG, THE CREW RECEIVED A MAIN HYDRAULIC PUMP INOP CAS MESSAGE. THE NOSE WHEEL STEERING AND ANTI SKID WERE TURNED OFF FOR LANDING FOLLOWING - [SDR VNAA0206008](https://openairdocs.org/sdr/VNAA0206008), Jun 17, 2002: DAU. MALFUNCTIONED. DURING TAKEOFF, THE CREW RECEIVED A DATA ACQUISITION UNIT CHANNEL NUMBER 2 FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE SYSTEM AND WAS CLEARED FOR A - [SDR VNAA0205009](https://openairdocs.org/sdr/VNAA0205009), May 15, 2002: LIGHT. INOPERATIVE. THE CREW REPORTED THAT THE FORWARD OVERHEAD EMERGENCY LIGHT WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE BULB IN THE LIGHT ASSEMBLY IN ACCORDANC - [SDR VNAA0205002](https://openairdocs.org/sdr/VNAA0205002), May 2, 2002: SENSOR. FAILED. AFTER DEPARTURE FROM DAY, THE CREW RECEIVED A LEFT HAND EMERGENCY DOOR OPEN INDICATION. FLIGHT 9412 THEN RETURNED TO DAY. MAINTENANCE INSPECTED AND ADJUSTED THE - [SDR VNAA0203045](https://openairdocs.org/sdr/VNAA0203045), Mar 29, 2002: STALL WARNING. MALFUNCTIONED. AFTER TAKING THE RUNWAY THE FLIGHT RECEIVED A PUSHER FAIL WARNING MESSAGE ON THE EICAS DISPLAY. THE FLIGHT CREW EXITED THE RUNWAY AND RETURNED TO THE GATE. MAIN - [SDR VNAA0201002](https://openairdocs.org/sdr/VNAA0201002), Jan 1, 2002: DISPLAY. MALFUNCTIONED. AFTER APPLYING POWER, THE NUMBER 4 AND NUMBER 5 MULTI FUNCTION DISPLAYS UNITS WENT BLANK. THE CREW ABORTED TAKEOFF AND DEPARTED THE RUNWAY. THE MULTI FUNCTION D - [SDR VNAA0111007](https://openairdocs.org/sdr/VNAA0111007), Nov 16, 2001: PANEL. FAILED. WHILE CLIMBING THROUGH 6,000 FEET, THE CREW RECEIVED A LEFT HAND GENERATOR FAIL CAS MESSAGE AND RETURNED TO PIT AFTER THE QUICK REFERENCE HANDBOOK PROCEDURE DID - [SDR VNAA0109019](https://openairdocs.org/sdr/VNAA0109019), Sep 29, 2001: BRAKE. FAILED. THE CREW REPORTED THATTHE FIRST OFFICERS BRAKES WERE INEFFECTIVE. THE AIRCRAFT WAS FERRIED TO PIT. MAINTENANCE INSPECTED AND BLED THE BRAKES IN ACCORDANCE WITH - [SDR VNAA0106006](https://openairdocs.org/sdr/VNAA0106006), May 26, 2001: RUDDER. FAILED. THIS IS A CONTINUATION ODR FOR ODR VNAA0105018. MAINTENANCE INSPECTED AND REPLACED THE RUDDER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONA - [SDR VNAA0103015](https://openairdocs.org/sdr/VNAA0103015), Mar 19, 2001: HARNESS. DEFECTIVE. AFTER BEGINNING THE TAKEOFF ROLL THE FLIGHT CREW RECEIVED A PROXIMITY FAIL WARNING INDICATION. THE FLIGHT CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAI - [SDR VNAA0103009](https://openairdocs.org/sdr/VNAA0103009), Mar 8, 2001: POWER SUPPLY. DISCHARGED. THE FLIGHT CREW REPORTED THAT THE FORWARD SECTION OF THE EMERGENCY FLOOR LIGHTING WOULD NOT OPERATE. MAINTENANCE INSPECTED AND REPLACED THE 4LK POWER SUPPLY IN - [SDR VNAA0102005](https://openairdocs.org/sdr/VNAA0102005), Feb 9, 2001: BATTERY. FAILED. THE CREW REPORTED THAT ROW THREE''S EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY IN ACCORDANCE WITH D - [SDR VNAA0101024](https://openairdocs.org/sdr/VNAA0101024), Jan 27, 2001: CONTROLLER. MALFUNCTIONED. AFTER TAKING THE RUNWAY, THE CREW RECEIVED A FLAP CONTROL FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND RESET THE FLAP CONTROL IN ACCORDANCE W - [SDR VNAA0011007](https://openairdocs.org/sdr/VNAA0011007), Nov 10, 2000: LIGHT. FAILED. PIT - FLT 4064 - THE CREW REPORTED THE EMERGENCY LIGHTING STRIP WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE LIGHTING STRIP IAW DORNIER MM 33-51-01. OPERATION - [SDR VNAA0009002](https://openairdocs.org/sdr/VNAA0009002), Sep 6, 2000: PUMP. FAILED. AFTER TAKEOFF, FLIGHT 4126 RECEIVED A RIGHT HAND ENGINE SURGE AND A RIGHT OIL PRESSURE CAS MESSAGE. THE CREW DECIDED TO RETURN TO THE FIELD AND LANDED WITHOUT I - [SDR VNAA0006014](https://openairdocs.org/sdr/VNAA0006014), Jun 24, 2000: WARNING SYSTEM. FALSE ACTIVATION. THE CREW RECEIVED AN APU BLEED SHUT OFF VALVE FAIL CAS MESSAGE AND ABORTED TAKE OFF, EXITED THE RUNWAY, AND CONTACTED MAINTENANCE CONTROL, WHO ADVISED THE CREW - [SDR VNAA0004020](https://openairdocs.org/sdr/VNAA0004020), Apr 19, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY SIGN AT ROW 9A WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION IN ACCORD - [SDR VNAA0004006](https://openairdocs.org/sdr/VNAA0004006), Apr 4, 2000: BATTERY. FAILED. THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS NOT WORKING AT ROWS 6, 7, AND 8. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 6LK POSITION - [SDR VNAA0003001](https://openairdocs.org/sdr/VNAA0003001), Mar 1, 2000: GENERATOR. MALFUNCTIONED. WHILE TAKING THE RUNWAY, THE CREW RECEIVED SEVERAL CAS MESSAGES. AFTER CLEARING THE RUNWAY THE CREW CONTACTED MAINTENANCE CONTROL AND WERE INSTRUCTED TO DE-SELE - [SDR VNAA0002012](https://openairdocs.org/sdr/VNAA0002012), Feb 14, 2000: BATTERY. INOPERATIVE. THE CREW NOTICED THAT THE EMERGENCY LIGHTS AT THE 4LK POSITION WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION. O - [SDR VNAA0001021](https://openairdocs.org/sdr/VNAA0001021), Jan 31, 2000: BATTERY. DISCHARGED. THE CREW FOUND THAT THE EMERGENCY LIGHTING AT THE 4LK AND 6LK POSITIONS WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE BATTERY AT THE 4LK POSITION IN - [SDR VNAA0001017](https://openairdocs.org/sdr/VNAA0001017), Jan 21, 2000: BATTERY. DISCHARGED. THE CREW FOUND THAT THE EMERGENCY LIGHT AT THE 6LK POSITION WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY AT THE 6LK POSITION IN ACCORDANCE - [SDR VNAA0001013](https://openairdocs.org/sdr/VNAA0001013), Jan 16, 2000: BATTERY. DISCHARGED. THE CREW FOUND THAT THE EMERGENCY LIGHT AT THE 4LK POSITION DID NOT WORK. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK POSITION IN ACCORD - [SDR VNAA9911022](https://openairdocs.org/sdr/VNAA9911022), Nov 27, 1999: BATTERY. DISCHARGED. THE FLIGHT CREW FOUND EMERGENCY LIGHTS AT THE 4LK POSITION NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY AT THE 4LK LOCATION IN ACCORDAN - [SDR VNAA9911010](https://openairdocs.org/sdr/VNAA9911010), Nov 13, 1999: FAIL MESSAGE. ACTIVATED. FLIGHT 4032 WAS ON FINAL WHEN THE CREW RECEIVED A NOSE WHEEL STEERING FAIL CAS MESSAGE AND A NOSE WHEEL POWER UP FAIL CAS MESSAGE. THE CREW EXECUTED A GO-AROUND - [SDR VNAA9910023](https://openairdocs.org/sdr/VNAA9910023), Oct 31, 1999: BATTERY. DISCHARGED. DURING THE APPROACH TO PIT, THE FLIGHT CREW EXPERIENCED A NR 1 BATTERY INDICATION WITH AN OVERHEAT INDICATION STAYING ON AFTER THE TEST BUTTON WAS RELEASED. MAI - [SDR VNAA9904004](https://openairdocs.org/sdr/VNAA9904004), Apr 7, 1999: ACTUATOR. FAILED. VIBRATIONS ORIGINATING FROM THE REAR OF THE AIRCRAFT WERE NOTED BY THE CREW AFTER TAKEOFF. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO THE FIELD - [SDR VNAA9903003](https://openairdocs.org/sdr/VNAA9903003), Mar 2, 1999: PCU. FAILED. THE RIGHT HAND PROPELLER WOULD NOT COME OUT OF FEATHER WHEN SELECTED DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE RIGH - [SDR VNAA9812018](https://openairdocs.org/sdr/VNAA9812018), Dec 31, 1998: BRUSH BLOCK. DIRTY. THE FLIGHT RETURNED TO THE GATE AFTER RECEIVING A LEFT HAND PROPELLER HEAT FAIL WARNING MESSAGE. MAINTENANCE INSPECTED AND CLEANED THE LEFT HAND PROPELLER BRUSH - [SDR VNAA9811022](https://openairdocs.org/sdr/VNAA9811022), Nov 22, 1998: WINDSHIELD. FAILED. DURING THE TAXI FOR TAKEOFF, A RIGHT HAND WINDSCREEN HEAT FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND DEFERRE - [SDR VNAA9809008](https://openairdocs.org/sdr/VNAA9809008), Sep 10, 1998: SKIN. BIRD STRIKE. DURING APPROACH, THE AIRCRAFT TOOK A BIRD STRIKE ON THE LEFT WING. THE AIRCRAFT CONTINUED THE APPROACH AND PERFORMED A NORMAL LANDING WITHOUT ANY FURTHER PROBLE - [SDR VNAA9809001](https://openairdocs.org/sdr/VNAA9809001), Sep 1, 1998: NOSE CONE. BIRD STRIKE. THE CREW REPORTED THAT THEY MAY HAVE TAKEN A BIRD STRIKE ON THE NOSE CONE, DURING SHORT FINAL APPROACH. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED WITHOUT I - [SDR VNAA9801011](https://openairdocs.org/sdr/VNAA9801011), Jan 24, 1998: CONTROL UNIT. TRIPPED. DURING TAXI FOR TAKEOFF, A FLAP CONTROL FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE AND MAINTENANCE WAS CALLED. MAINTENANCE INSPECTED AN - [SDR VNAA9612003](https://openairdocs.org/sdr/VNAA9612003), Dec 16, 1996: SELECTOR. SHORTED. CLT - FLT 4008 - LANDING GEAR GREEN DOWN AND LOCKED LIGHTS DID NOT COME ON WHEN LANDING GEAR WAS SELECTED DOWN. TOWER OBSERVATIONS WERE THAT THE GEAR WAS EXTEND - [SDR VNAA9612002](https://openairdocs.org/sdr/VNAA9612002), Dec 10, 1996: PROX SWITCH. OUT OF ADJUST. WHILE PASSING THROUGH 1700 FEET, THE BAGGAGE COMPARTMENT DOOR LIGHT CAME ON. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE BAGGA ## STCs that may be installed (OpenAirDocs) (114, first 50) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Cessna 560XL) - [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC ST01823WI](https://openairdocs.org/stc/ST01823WI): Installation of Garmin GTS Traffic Sensor with Garmin GTX 3000 Mode S Transponders with ADS-B Out. Blackhawk Aerospace Technologies Inc - [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc - [STC ST12344IB](https://openairdocs.org/stc/ST12344IB): Replacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc - [STC ST02016WI](https://openairdocs.org/stc/ST02016WI): Installation of the Meggitt Wireless Tire Pressure Sensor. 3S Certification LLC - [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC - [STC ST00390BO](https://openairdocs.org/stc/ST00390BO): Installation of a SmartSky Networks Air to Ground Data Link System. Apcela IFC JV, LLC dba Apcela ATG - [STC ST04604CH](https://openairdocs.org/stc/ST04604CH): INSTALL SMARTSKY FLAGSHIP SYSTEM. Apcela IFC JV, LLC dba Apcela ATG - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc - [STC ST02718LA](https://openairdocs.org/stc/ST02718LA): Modification to replace the existing standby instrument. Acron Aviation Inc - [STC ST03292CH](https://openairdocs.org/stc/ST03292CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development, Inc - [STC ST12042WI](https://openairdocs.org/stc/ST12042WI): Upgrade of AirCell High Speed Internet System to Gogo Business Aviation C1 System. Duncan Aviation Inc - [STC ST09854AC](https://openairdocs.org/stc/ST09854AC): Installation of a Lumin Media Server. L2 Aviation - [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc - [STC ST04730NY](https://openairdocs.org/stc/ST04730NY): Installation of Battery Temperature Indicator. Aero-Mach Labs Inc - [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine - [STC ST02804SE](https://openairdocs.org/stc/ST02804SE): Installation of Starlink Aviation System. AeroMech Incorporated - [STC ST01979WI](https://openairdocs.org/stc/ST01979WI): Installation of Gogo Business Aviation AVANCE L5/X3 System or optional AVANCE LX5 System. Gogo Business Aviation LLC - [STC ST04742NY](https://openairdocs.org/stc/ST04742NY): Installation of SkyVue 1000 Cockpit Upgrade including dual Avidyne IFD540 FMS with LPV i. Aerospace Design & Compliance LLC - [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc - [STC ST01918WI](https://openairdocs.org/stc/ST01918WI): Installation of Garmin G5000 Integrated Flight Deck. Garmin International Inc - [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC - [STC ST01083DE](https://openairdocs.org/stc/ST01083DE): Installation of the Aviation Clean Air Airborne Air & Surface Purification System. Lee Aerospace, Inc - [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC - [STC ST02427LA](https://openairdocs.org/stc/ST02427LA): Installation of Dual Garmin GTN 6XX/7XX Series Global Navigation System with Structural Antenna and WAAS approval; Garmin GMA 35 Audio Panel; and Dual Garmin GTX 33 Mode S Transponders, Weather Radar, and ADS-B Link. JETTECH LLC - [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc - [STC ST02029WI](https://openairdocs.org/stc/ST02029WI): Installation of Garmin GI 275 Standby Instrument and GSB 15 USB Port. Blackhawk Aerospace Technologies - [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited - [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine - [STC ST00011WI](https://openairdocs.org/stc/ST00011WI): Installation of Concorde RG380E/40 and 40B battery. Aero-Mach Wilco LLC - [STC ST11285DS](https://openairdocs.org/stc/ST11285DS): An update to the existing Collins Aerospace Integrated Flight Information System (IFIS) FSU-5010 and upgrade the existing XMWR-1000 to a XMWR-1000S (Sirius XM) in Part 25. BHE & Associates Ltd - [STC ST03035NY](https://openairdocs.org/stc/ST03035NY): Replacement of certain Goodrich pneumatic deicer boots. SMR Technologies Inc - [STC ST04258CH](https://openairdocs.org/stc/ST04258CH): Installation of Gogo Business Aviation Avance High Speed Data System. Ross Aviation Flight Maintenance - [STC ST00411BO](https://openairdocs.org/stc/ST00411BO): Installation of Avidyne GPS/Nav/Com. Avidyne Corporation - [STC ST01916WI](https://openairdocs.org/stc/ST01916WI): Installation of Beijing Sky Aviation Chinese Flight Inspection System. Duncan Aviation Inc - [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc - [STC ST00953DE](https://openairdocs.org/stc/ST00953DE): Installation of a cabin emergency lighting. West Star Aviation - [STC ST01027DE](https://openairdocs.org/stc/ST01027DE): Installation of MarathonNorco Aerospace Inc Nickel Cadmium battery in place of existing Nickel Cadmium main aircraft battery/batteries. MarathonNorco Aerospace Inc - [STC ST01859WI](https://openairdocs.org/stc/ST01859WI): Installation of Gogo Business Aviation's Gogo Biz 4G Air-to-Ground System. Textron Aviation Inc Wichita Citation Service Center - [STC ST00158BO](https://openairdocs.org/stc/ST00158BO): Installation of Universal Avionics Systems Corporation (UASC) Flight Management System (FMS). Pro Star Aviation, LLC - [STC ST04416CH](https://openairdocs.org/stc/ST04416CH): Install Mid-Continent Instruments MD-302 Standby Instrument. Elliott Aviation Technical Products Development Inc - [STC ST00934DE](https://openairdocs.org/stc/ST00934DE): Installation of Becker Avionics BXT6553 transponder. Peregrine - [STC ST01780LA](https://openairdocs.org/stc/ST01780LA): Installation of a Patient Loading and Utility System. LifePort LLC - [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS - [STC ST01138CH](https://openairdocs.org/stc/ST01138CH): Install air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed - [STC ST00883DE](https://openairdocs.org/stc/ST00883DE): Installation of Grumman LitefLCR-100 Attitude Heading and Reference System (AHRS) in place of existing LCR-93 AHRS. Peregrine All 114: https://openairdocs.org/aircraft/N461PS/stcs.md ## Related - Other Cessna 560XL aircraft: https://openairdocs.org/model/cessna-560xl/aircraft.md - The Pratt & Whitney Canada PW545 series engine: https://openairdocs.org/engine/pratt-whitney-canada-pw545-series.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.