# N686QS: 2006 Cessna 560XL

- Status: Valid registration
- Airframe: [Cessna 560XL](https://openairdocs.org/model/cessna-560xl) (registry code 2076702, 13 seats)
- Engine: [Pratt & Whitney Canada PW545B](https://openairdocs.org/engine/pratt-whitney-canada-pw545b) (registry code 52186)
- 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: 560-5661
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 9, 2006
- Certificate issued: June 29, 2019
- Expires: June 30, 2029
- Mode S code: A91AF0
- Registered owner: [Netjets Sales Inc](https://openairdocs.org/faa-owner/NETJETS%20SALES%20INC)
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Corporation
- Owner's area on the map: 35.5467° N, 97.5646° W: Placed by OpenAirDocs at the center of ZIP code 73116, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=686QS
- Page: https://openairdocs.org/aircraft/N686QS

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.

## ADs that may apply (OpenAirDocs): 19 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 PW545B)

- [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

### 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 N686QS.

## FAA accident and incident reports

None matched to N686QS.

## Service difficulty reports (42)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DXTA2025120805968](https://openairdocs.org/sdr/DXTA2025120805968), Dec 4, 2025: BELLCRANK. WORN. MAIN CABIN DOOR REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE AND SEEMS TO BE BINDING INTERNALLY. OPERATION IS NOT NORMAL COMPARED TO OTHER MAIN CABIN DOORS ON XLS
- [SDR DXTA2025060203716](https://openairdocs.org/sdr/DXTA2025060203716), May 31, 2025: LANDING GEAR. FAULTED. AFTER A NORMAL TAKE OFF GEAR WOULD NOT RETRACT. HANDLE WAS LOCKED IN THE DOWN POSITIONS. ALSO NOTICE THE GND IDLE AND NO TAKE OFF ANNC WERE ILLUMINATED AT THIS 
- [SDR DXTA2025012002014](https://openairdocs.org/sdr/DXTA2025012002014), Jan 17, 2025: G SWITCH. NO TEST. CABIN EMERG LIGHT: WITH THE BATTERY SWITCH ON, AND THE EMER LTS SWITCH TO ARM, THE AFT EMERGENCY LIGHTS STAY ON. CORRECTIVE ACTION: RESET AFT EMERGENCY INTERTIA
- [SDR DXTA2023081693170](https://openairdocs.org/sdr/DXTA2023081693170), Aug 15, 2023: UNKNOWN. UNKNOWN. MAIN CABIN DOOR IS EXTREMELY DIFFICULT TO OPEN AND CLOSE, BOTH FROM THE INSIDE AND THE OUTSIDE OF THE AIRCRAFT. ADJUSTED MAIN CABIN DOOR LATCH PLATE DUE TO MAIN
- [SDR DXTA2023050985650](https://openairdocs.org/sdr/DXTA2023050985650), May 8, 2023: UNKNOWN. UNKNOWN. WHILE TOUCHING DOWN AT LANDING, PWR BRKS CB TRIPPED. LOW BRK PRESS & ANTISKID INOP MESSAGES ILLUMINATED. BRAKE PRESSURE COMPLETELY FAILED & ACFT HAD TO BE STOPP
- [SDR DXTA2022112374630](https://openairdocs.org/sdr/DXTA2022112374630), Nov 23, 2022: APU. SMOKE. COCKPIT FILLS WITH THICK SMOKE, APU ON, BLEED ON NORMAL. REMOVED AND REPLACED THE APU IAW AMM 49-10-00
- [SDR DXTA2022111573990](https://openairdocs.org/sdr/DXTA2022111573990), Nov 14, 2022: G SWITCH. TRIPPED. CABIN EMERG LIGHT: FORWARD HALF OF EMERGENCY LIGHTING IS STUCK ON, REGARDLESS OF PASS SAFETY SWITCH POSITION. FOUND FORWARD EMERGENCY BATT G SITCH TRIPPED. RESE
- [SDR DXTA2022061664000](https://openairdocs.org/sdr/DXTA2022061664000), Jun 15, 2022: PRESSURE SWITCH. INTERMITTENT. MAIN DOOR PRIMARY SEAL: AFTER STARTING APU WITH MAIN CABIN DOOR OPEN NOTICED THE DOOR SEAL ANNUNCIATOR WAS NOT ILLUMINATED. FOUND MAIN CABIN DOOR SEAL INFLATED.
- [SDR DXTA2022051061530](https://openairdocs.org/sdr/DXTA2022051061530), May 9, 2022: DOOR SEAL. MALFUNCTIONED. MAIN DOOR: WITH APU RUNNING AND BLEED AIR ON THE MAIN CABIN DOOR WOULD NOT CLOSE. THE DOOR SEAL WAS INFLATED. SHUT OFF THE BLEED AIR WITH NO CHANGE. WHEN WE SHU
- [SDR DXTA2022010654810](https://openairdocs.org/sdr/DXTA2022010654810), Jan 5, 2022: MANIFOLD. LEAKING. APU BLEED AIR: AFTER APU START, WHEN THE BLEED AIR WAS SELECTED ON, THE CABIN FILLED WITH A STRONG EXHAUST/FUEL SMELL. REMOVED APU ACCESS PANEL AND INSPECTED IN
- [SDR DXTA2021112952560](https://openairdocs.org/sdr/DXTA2021112952560), Nov 26, 2021: HEAT EXCHANGER. DEFECTIVE. APU BLEED AIR: WITH THE APU RUNNING AND ENGINES OFF, WITH THE APU BLEED AIR ON, THERE IS AN OIL SMELL IN THE CABIN. THE BLEED AIR SWITCH WAS CYCLED SEVERAL TIME
- [SDR DXTA20210104649](https://openairdocs.org/sdr/DXTA20210104649), Jan 27, 2021: LINK. OUT OF ADJUST. THE MAIN CABIN DOOR OVER CENTER HANDLE IS EXTREMELY LOOSE AND HITS THE DOOR WHEN THE DOOR IS CLOSED. IT TAKES MINIMUM EFFORT ON THE OVER CENTER HANDLE FOR THE D
- [SDR DXTA202101024544](https://openairdocs.org/sdr/DXTA202101024544), Jan 2, 2021: MECHANISM. DIRTY. MAIN CABIN DOOR PRECATCH WORKS, DOOR PINS OUT OF SYNC WITH DOOR HANDLE POSITION. OPERATIONS CHECKED, DOOR COULD NOT DUPLICATE FAILURE. PER MX CONTROL GAINED ACC
- [SDR DXTA2019022502069](https://openairdocs.org/sdr/DXTA2019022502069), Feb 23, 2019: HANDLE. FAILED. LEFT MLG MLG - NO MLG LIGHTS ON EXTENSION. LANDING GEAR WILL NOT EXTEND QRH COMPLETED. "CORRECTIVE ACTION" REMOVED LANDING GEAR CONTROL BOX P;N 9912550-1 S/N 04
- [SDR DXTR2017060901](https://openairdocs.org/sdr/DXTR2017060901), Jun 9, 2017: SERVICE DOOR. CORRODED. APU OIL SERVICE DOOR CORRODED AT FWD AND AFT LATCH POINTS. REPAIRED IAW ERO-897650, THIS IS A MINOR REPAIR OF LEVEL 1 CORROSION.
- [SDR DXTA2017022206374](https://openairdocs.org/sdr/DXTA2017022206374), Feb 22, 2017: LIGHT. MELTED. DURING DESCENT, THERE WAS SMOKE COMING FROM THE LEFT CIRCUIT PANEL. AN EMERGENCY DESCENT WAS PERFORMED AND ELECTRICAL FIRE OR SMOKE CHECKLIST G1 WAS INITIATED A
- [SDR DXTA2016101106316](https://openairdocs.org/sdr/DXTA2016101106316), Oct 11, 2016: CONTROL UNIT. FAILED. ON DEPARTURE, LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION. UNABLE TO RETRACT GEAR. UNABLE TO RETRACT GEAR. WITH A MULTI METER CHECK FOR 28VDC AND GROUND A
- [SDR CWQR20160216004](https://openairdocs.org/sdr/CWQR20160216004), Feb 16, 2016: AIR DUCT. CRACKED. DURING AN INSPECTION WE FOUND THE APU AIR DUCT MOUNTING FLANGE CRACKED WHERE IT ATTACHES TO THE DUCT ASSEMBLY. REPLACED AIR DUCT WITH UPGRADED 6655600-49 ASSEMB
- [SDR DXTA2015070206038](https://openairdocs.org/sdr/DXTA2015070206038), Jul 1, 2015: UNKNOWN. MALFUNCTIONED. WHILE USING BRAKES AT ANY TIME, BRAKES THUMP & MOMENTARILY LOCK UP. PIN LENGTH IS GOOD & NO ANNUNCIATION WAS NOTICED. REMOVED LT & RT WHEEL ASSEMBLIES, INSPECTE
- [SDR CWQR20141015008](https://openairdocs.org/sdr/CWQR20141015008), Oct 15, 2014: HINGE. CORRODED. DURING A SCHEDULED INSPECTION WE FOUND THE LOWER AFT MAIN CABIN DOOR HINGE HALF CORRODED. THE HINGE HALF MATERIAL HAD SWELLED FROM INTERGRANULAR CORROSION FROM 
- [SDR DXTA2013111105561](https://openairdocs.org/sdr/DXTA2013111105561), Nov 7, 2013: APU. FAILED. ACFT ON GROUND, APU RUNNING, COCKPIT & CABIN SUDDENLY FILLED WITH ELECTRICAL SMOKE ODOR. NO INDICATIONS OF FIRE, RAN SMOKE CHECKLIST. APU SHUTDOWN ON ITS OWN. C
- [SDR DXTA2013050205367](https://openairdocs.org/sdr/DXTA2013050205367), May 2, 2013: POINTER. BENT. PITCH TRIM IS HARD TO MOVE AND BINDING AS IT IS MOVED NOSE UP THROUGH THE TAKEOFF RANGE. BINDING CAN BE FELT WHILE USING MANUAL TRIM. WHILE USING ELECTRIC TRIM 
- [SDR DXTA2013041105352](https://openairdocs.org/sdr/DXTA2013041105352), Apr 10, 2013: ACTUATOR. BINDING. TRIM WHEEL VERY DIFFICULT TO TRIM MANUALLY. WHEN TRIMMING WITH ELECTRIC TRIM IT STOPS/BINDS FOR A MOMENT APPROX EVERY INCH OF ROTATION. WHEN IN AUTOPILOT IT DID
- [SDR CWQR20120523033](https://openairdocs.org/sdr/CWQR20120523033), May 23, 2012: CHANNEL. CRACKED. DURING A SCHEDULED INSPECTION, FOUND FWD BAGGAGE DOOR HINGE ASSY CRACKED IN SEVERAL PLACES. 2 CRACKS IN SUPPORT CHANNEL 66120720-2 AND 1 CRACK ON CHANNEL 661206
- [SDR DXTA2011091204726](https://openairdocs.org/sdr/DXTA2011091204726), Sep 8, 2011: BRAKE ASSY. MALFUNCTIONED. WHEN APPLYING THE LEFT BRAKE, IT DOESN'T DO ANYTHING FOR A WHILE THEN GRABS SUDDENLY CAUSING ABRUPT TURN TO THE LEFT. PERFORMED TAXI CHECK OF BRAKES. NO DEFECTS
- [SDR DXTA2010102604271](https://openairdocs.org/sdr/DXTA2010102604271), Oct 25, 2010: COMPUTER. FAILED. DURING CLIMB OUT OF 28,000 FT, WITH RT SEAT PILOT FLYING, THE ATTITUDE AND HEADING FAILURE MESSAGE ILLUMINATED IN THE LT SIDE PFD AND THE MFD. THE AUTO-PILOT AL
- [SDR DXTA2010080904187](https://openairdocs.org/sdr/DXTA2010080904187), Aug 8, 2010: UNKNOWN. SMOKE. HAD VISIBLE SMOKE IN COCKPIT ON TAKEOFF, THRU ABOUT 2K FT, WITH APU RUNNING. SMOKE SEEMED TO BE ISOLATED TO COCKPIT AREA. SMOKE DISSIPATED ON ITS OWN IN A VERY 
- [SDR DXTA2009081403758](https://openairdocs.org/sdr/DXTA2009081403758), Aug 13, 2009: BRAKE ASSY. CHATTERING. BRAKES CHATTER AND PLANE SUTTER WHEN APPLYING THE RT BRAKE DURING TAXI AND LANDING, REPLICATED ON BOTH SETS OF BRAKE PEDALS. T/S SYS TO DEFECTIVE ANTISKID VALVE
- [SDR DXTA2009061503686](https://openairdocs.org/sdr/DXTA2009061503686), Jun 14, 2009: BRAKE ASSY. WEAK. ON LANDING, "LO BRAKE PRESSURE" AND "ANTI SKID INOP" LIGHTS ILLUMINATED; ANTI-SKID BITE LIGHTS ARE NORMAL. ACFT PULLS TO THE RT WHEN BRAKES ARE APPLIED ON THE G
- [SDR DXTA2009042703620](https://openairdocs.org/sdr/DXTA2009042703620), Apr 24, 2009: METERING VALVE. MALFUNCTIONED. DURING TAXI THERE WAS A HEAVY VIBRATION HEARD AND FELT WHEN BRAKES WERE APPLIED. THE VIBRATION CAME FROM RT BRAKE ONLY. LT SIDE OK. REMOVED AND REPLACED BRAKE M
- [SDR DXTA2009021303503](https://openairdocs.org/sdr/DXTA2009021303503), Feb 12, 2009: BRAKE SYS. WEAK. BRAKE PEDALS FEEL SPONGY. BLED ANTI-SKID BRAKE SYS IAW CH 32-44-00 OF AMM. LEAK CHECK OF BLEEDER PLUGS GOOD. TAXI CHECK OF BRAKES GOOD. ALL WORK IAW MM 32-44-00
- [SDR DXTA2009020103486](https://openairdocs.org/sdr/DXTA2009020103486), Feb 1, 2009: ACTUATOR. INOPERATIVE. REMOVED AND REPLACED LT MLG ACUATOR WITH REPAIRED UNIT. PERFORMED ALL OPS CHECKS AND LEAK CHECKS. OPS AND LEAK CHECKS GOOD. ALL ACTUATOR HARDWARE REPLACED WITH 
- [SDR DXTA2009020103483](https://openairdocs.org/sdr/DXTA2009020103483), Feb 1, 2009: PUMP. INOPERATIVE. FOUND FAULT RELATED TO GEAR/HYD ISSUE WITH ACFT. AFTER COMPLETION OF HYD PUMP REPLACEMENT PERFORMED SEVERAL OPS CHECKS OF STAB AND FLAP SYS WITH NO DEFECTS NOTE
- [SDR DXTA2009020303486](https://openairdocs.org/sdr/DXTA2009020303486), Feb 1, 2009: WARNING LIGHT. ILLUMINATED. ON DESCENT INTO KASE. AT APPROX 195 KIAS, GOT STAB MISCOMPARE CAUTION LIGHT.
- [SDR DXTA2009020303483](https://openairdocs.org/sdr/DXTA2009020303483), Feb 1, 2009: UNKNOWN. UNKNOWN. SELECTED LANDING GEAR DOWN. GOT GEAR DOWN INDICATION ON NOSE AND RT MAIN. UNLOCK LIGHT ILLUMINATED LT MAIN LIGHT DID NOT ILLUMINATE.
- [SDR DXTA200803150](https://openairdocs.org/sdr/DXTA200803150), Jun 28, 2008: OIL SYSTEM. LEAKING. DURING TAKEOFF ROLL, APPROX 60 KTS, LT ENG OIL PRESS DROPPED TO 0. LT LOW OIL PRESS LIGHT ILLUMINATED FOR 20 SEC & EXTINGUISHED. RAN ENG TO T/O POWER & PRESS DR
- [SDR DXTA200803013](https://openairdocs.org/sdr/DXTA200803013), Apr 23, 2008: RELAY. INOPERATIVE. UNCOMMANDED EMERGENCY DESCENT WITH AUTOPILOT ENGAGED AT FL400. REPLACED RELAY KC009 AND CONNECTOR. IAW MFG WIRING DIAGRAM MAN 20-10-04. OPS CHECK GOOD. RELAY P/
- [SDR DXTA20082952](https://openairdocs.org/sdr/DXTA20082952), Mar 20, 2008: LATCH. OBSTRUCTED. AC DOOR LIGHT (TAIL) ILLUMINATED ON TAKEOFF. FOUND BAGGAGE AFT UPPER LATCH STIFF. CLEANED SLIDE (BAYONET) AND HINGE POINTS AND LUBED. REMOVED UNIT FROM BAYONET 
- [SDR DXTA200802777](https://openairdocs.org/sdr/DXTA200802777), Jan 19, 2008: FIRE LOOP. OUT OF POSITION. LT ENGINE FIRE WARNING LIGHT FLASHES INTERMITTENT IN CRUISE FLIGHT. NO SECONDARY INDICATIONS OBSERVED. REMOVED BOTH UPPER AND LOWER COWLINGS, INSPECTED FIRE LOO
- [SDR DXTA200702234](https://openairdocs.org/sdr/DXTA200702234), Jun 1, 2007: ACTUATOR. INOPERATIVE. STAB MISCOMPARE LIGHT ILLUMINATES ON FLAP RETRACTION AFTER T/O. REMOVED HORIZONTAL STAB ACTUATOR AND INSTALLED AN INSPECTED ACTUATOR. OPS AND LEAK CHECKS GOOD. 
- [SDR DXTA200702161](https://openairdocs.org/sdr/DXTA200702161), Apr 29, 2007: UNKNOWN. MALFUNCTIONED. DURING START BRAKE LOW PRESS AND ANTI SKID INOP LIGHT CAME ON. IT WENT OUT AS RPM INCREASED, CAME ON AGAIN AS TAXI STARTED. BRAKE PRESS REMAINED OK. EMER BRAKE 
- [SDR DXTA200702065](https://openairdocs.org/sdr/DXTA200702065), Apr 1, 2007: UNKNOWN. CHATTERING. UPON RELEASING BRAKES FOR TAKEOFF AT SJC, (4) LOUD KNOCKS IN RAPID SUCCESSION WERE HEARD FROM REAR OF AIRCRAFT. ABORTED TAKEOFF AND RETURNEDTO RAMP. INSPECTED B

## 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/N686QS/stcs.md

## Related

- Other Cessna 560XL aircraft: https://openairdocs.org/model/cessna-560xl/aircraft.md
- The Pratt & Whitney Canada PW545B engine: https://openairdocs.org/engine/pratt-whitney-canada-pw545b.md

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