# N588QS: 2007 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: 560-5721
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 23, 2007
- Certificate issued: July 28, 2022
- Expires: July 31, 2029
- Mode S code: A7950F
- Registered owners: [Netjets Sales Inc](https://openairdocs.org/faa-owner/NETJETS%20SALES%20INC), [Netjets Aviation Inc](https://openairdocs.org/faa-owner/NETJETS%20AVIATION%20INC)
- Location: [Columbus, OH](https://openairdocs.org/faa-place/OH/Columbus)
- Owner type: Co-owned, fractional ownership
- Owner's area on the map: 40.0074° N, 82.9207° W: Placed by OpenAirDocs at the center of ZIP code 43219, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=588QS
- Page: https://openairdocs.org/aircraft/N588QS

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ERA11IA184](https://openairdocs.org/ntsb/ERA11IA184), Mar 10, 2011: Cessna 560XL (N588QS), Haynesville, VA, incident, no damage. Probable cause: The manufacturer's inadequate design fix for previously known tailcone stinger water ingestion and retention.

## FAA accident and incident reports

None matched to N588QS.

## Service difficulty reports (34)

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 DXTA2026091709713](https://openairdocs.org/sdr/DXTA2026091709713), Sep 14, 2026: BATTERY PACK. FAULTED. WITH THE EMERGENCY LIGHT SWITCH SET TO ARM AND THE PASSENGER SAFETY SWITCH SET TO OFF THE EMERGENCY LIGHT SYSTEM REMAINS ILLUMINATED BOTH INTERIOR AND EXTERIOR.
- [SDR DXTA2026072708979](https://openairdocs.org/sdr/DXTA2026072708979), Jul 23, 2026: SWITCH. OUT OF ADJUST. DURING TAKEOFF AT APPROXIMATELY 10 KTS THE ACC DOOR UNLOCK TAIL ANNUNCIATOR ILLUMINATED. AFTER RETURNING TO THE FBO VERIFIED ALL DOORS WERE IN THE CLOSED AND LO
- [SDR DXTA2026050507920](https://openairdocs.org/sdr/DXTA2026050507920), May 3, 2026: DOOR SEAL. CUT. AT ALTITUDES ABOVE 16,500' AN ULTRA-HIGH PIERCING FREQUENCY SOUND CAN BE HEARD IN THE CABIN. TOUGH TO PINPOINT, BUT SEEMS TO COME FROM AREA AROUND MAIN CABIN DO
- [SDR DXTA2026030607131](https://openairdocs.org/sdr/DXTA2026030607131), Mar 5, 2026: G SWITCH. TRIPPED. EMERGENCY LIGHTS STAY ON WHEN EMERGENCY LIGHTING SWITCH PLACED IN THE ARMED POSITION. RECYCLED POWER ON AIRCRAFT WITH SAME RESULTS. ACCESSED AFT EMERGENCY LIGHT
- [SDR DXTA2026021306862](https://openairdocs.org/sdr/DXTA2026021306862), Feb 11, 2026: BATTERY PACK. DEFECTIVE. THE FRONT EMERGENCY BATTERY PACK IS DEAD. WITH BATTERY SWITCH ON AND EMER LIGHT SWITCH ON, ALL EMERGENCY LIGHTS CHECK NORMAL. TURNING THE BATTERY SWITCH TO OFF,
- [SDR DXTA2025041003031](https://openairdocs.org/sdr/DXTA2025041003031), Apr 10, 2025: SOLENOID. FAULTED. AFTER CLOSING AND SECURING MAIN CABIN DOOR, THE CABIN DOOR ANNUNCIATOR LIGHT REMAINED ILLUMINATED. AFTER A COUPLE OF UNSUCCESFUL ATTEMPTS TO PROPERLY SECURE THE
- [SDR DXTA2024121601541](https://openairdocs.org/sdr/DXTA2024121601541), Dec 15, 2024: SOLENOID. DEFECTIVE. AIRCRAFT WOULD NOT PRESSURIZE AFTER DEPARTURE. VENT DOOR LATCH FEELS LIKE THERE IS SOME RESISTANCE PREVENTING IT FROM FULLY CLOSING. GAINED ACCESS AND REMOVED M
- [SDR DXTA2024072212439](https://openairdocs.org/sdr/DXTA2024072212439), Jul 22, 2024: G SWITCH. TRIPPED. EXIT LIGHT ABOVE MAIN CABIN DOOR,¿ EXIT SIGN LEFT AND RIGHT OF MAIN CABIN DOOR AND READING LIGHT AT SEAT NR. 3 AND NR. 10 ARE STEADY ILLUMINATED. THEY WILL EXTI
- [SDR DXTA2024060711982](https://openairdocs.org/sdr/DXTA2024060711982), Jun 6, 2024: CONDENSER. DIRTY. INTERMITTENT HOT ELEC ODOR COMES FROM WEMAC VENTS WITH ENGS RUNNING. NO SMOKE OBSERVED. HAPPENED SEVERAL TIMES BEGINNING AFTER TAKEOFF TO SHUTDOWN. ON POST FLIG
- [SDR DXTA2024040211379](https://openairdocs.org/sdr/DXTA2024040211379), Apr 1, 2024: BATTERY. INOPERATIVE. WITH THE MAIN BATTERY OFF AND EMER LIGHTS ON THE FORWARD LEFT AISLE EMER LIGHTS AND THE THREE EXIT SIGNS AT MAIN ENTRY DOOR WERE INOP. REMOVED INOP FWD EMER LIG
- [SDR DXTA2024022110970](https://openairdocs.org/sdr/DXTA2024022110970), Feb 19, 2024: SIGN. NO TEST. MAIN DOOR EXIT LIGHT DOES NOT CHECK WHEN EMER LIGHTS TEST. VERIFY THAT THE MAIN CABIN EXIT DOOR LIGHT IS INOP. C/W RSA OF THE MAIN CABIN EXIT DOOR LIGHT PN ON A
- [SDR DXTA2024013110760](https://openairdocs.org/sdr/DXTA2024013110760), Jan 30, 2024: SEAL. MALFUNCTIONED. MAIN DOOR PRIMARY SEAL: WHEN YOU START THE APU THE GREY PRIMARY DOOR SEAL INFLATES. UNABLE TO CLOSE MAIN CABIN DOOR. PERFORMED A DETAIL INSPECTION. RAN APU AGAI
- [SDR DXTA2023121310326](https://openairdocs.org/sdr/DXTA2023121310326), Dec 13, 2023: UNKNOWN. UNKNOWN. MAIN CABIN DOOR MOVES FORCEFULLY TO CLOSE WHEN HAND RAIL IS LIFTED OUT OF OVER CENTER OPEN POSITION. LAST HALF OF DOOR CLOSING OCCURS VERY RAPIDLY. ADJUSTED MAI
- [SDR DXTA2023111310029](https://openairdocs.org/sdr/DXTA2023111310029), Nov 11, 2023: UNKNOWN. UNKNOWN. MAIN DOOR PRECATCH: CABIN DOOR WAS LOCKED AND DOOR WOULD NOT OPEN WITH OUT PUSHING THE PRECATCH. DID THIS TWICE DOOR WOULD NOT OPEN. LUBRICATED PRECATCH AS REQU
- [SDR DXTA2023090594500](https://openairdocs.org/sdr/DXTA2023090594500), Sep 3, 2023: UNKNOWN. UNKNOWN. MAIN DOOR VISUAL INDICATOR: MAIN DOOR ANNUNCIATOR ILLUMINATED ON GROUND. RAN QRH. DOOR HANDLE AND VENT DOOR LIGHTS REMAINED ILLUMINATED. //SIGNOFF//
- [SDR DXTA2023081793240](https://openairdocs.org/sdr/DXTA2023081793240), Aug 16, 2023: UNKNOWN. UNKNOWN. FLOOR EMERG EXIT LIGHT: DROP ISLE LED EMERGENCY LIGHT STRIP UNDER CABIN ENTRY DOOR AND UNDER SEAT #8 IS NOT SECURED AND LAYING ON FLOOR. LED LIGHTS ARE OPERATIV
- [SDR DXTA2023080792430](https://openairdocs.org/sdr/DXTA2023080792430), Aug 7, 2023: UNKNOWN. UNKNOWN. WHILE OBSERVING THE MAIN CABIN DOOR, LOCKED FROM THE OUTSIDE, THE VENT DOOR PROTRUDES OUTWARD AND DOES NOT SEAT WITH THE AIRFRAME. AT LEAST A 1/4" GAP EXISTS. C
- [SDR DXTA2023061488710](https://openairdocs.org/sdr/DXTA2023061488710), Jun 14, 2023: UNKNOWN. UNKNOWN. MAIN CABIN DOOR, INTERMITTENT THE DOOR WILL NOT OPEN UNLESS THE PRECATCH RELEASE IS BEING UTILIZED
- [SDR DXTA2022053163020](https://openairdocs.org/sdr/DXTA2022053163020), May 31, 2022: BATTERY PACK. DEFECTIVE. CABIN EMERG LIGHT: APPEARS FRONT EMERGENCY BATTERY IS INOP. FRONT AISLE LIGHTS OUT OVERHEAD EXIT LIGHT OUT AND BOTH SIDE ON MAIN DOOR EXIT LIGHT OUT. REMOVED AN
- [SDR DXTR2022022801](https://openairdocs.org/sdr/DXTR2022022801), Feb 28, 2022: AUTOPILOT SYS. BROKEN. YAW DAMPER: YAW DAMPER DOESN'T SEEM TO WORK IN TURBULENT AIR. PLANE FISH TAILS AND DUTCH ROLLS IN UNSTABLE AIR, BUT IS FINE IN SMOOTH AIR. THE YAW DAMP ENGAGE S
- [SDR DXTA2021112252210](https://openairdocs.org/sdr/DXTA2021112252210), Nov 19, 2021: SEAL. DEFECTIVE. MAIN DOOR: WHEN THE APU IS RUNNING THE MAIN CABIN DOOR ACCUSTIC SEAL IS INFLATING ON IT'S OWN. THE SEAL INHIBITS THE USE OF THE MAIN CABIN DOOR. COULD BE A SAFT
- [SDR DXTA2021092049090](https://openairdocs.org/sdr/DXTA2021092049090), Sep 19, 2021: BATTERY PACK. DEFECTIVE. CABIN EMERG LIGHT: BACK HALF OF FLOOR PROXIMITY EMERGENCY LIGHTS ARE INOP . REMOVED FAULTY AFT EMERGENCY BATTERY PN 8813-1 SN# 1094 AND INSTALLED OVERHAULED BAT
- [SDR DXTA2020101604217](https://openairdocs.org/sdr/DXTA2020101604217), Oct 16, 2020: SLEEVE. WORN. THE MAIN CABIN DOOR WHEN OPENED FROM THE OUTSIDE CAUSES THE INSIDE CABIN DOOR HANDLE TO POP UP AND BE PARTIALLY BETWEEN THE OPEN AND CLOSE STOWED POSITION. REPL
- [SDR DXTA2020071503866](https://openairdocs.org/sdr/DXTA2020071503866), Jul 14, 2020: CABLE. DAMAGED. ON SHORT FINAL, THE LT ENGINE FIRE DETECTION LIGHT ILLUMINATED. ABOUT 5 SECONDS LATER THE LT ENGINE FIRE WARNING LIGHT ILLUMINATED FOR ABOUT 2 SECONDS & EXTINGU
- [SDR DXTA2015082606065](https://openairdocs.org/sdr/DXTA2015082606065), Aug 25, 2015: FIRE LOOP. FALSE ACTIVATION. AT 22,000 FT DURING CLIMB OUT, THE RT ENGINE FIRE LIGHT CAME ON. WHEN THE THROTTLE WAS REDUCED TO IDLE THE LIGHT EXTINGUISHED. DURING TROUBLESHOOTING, FOUND NO 
- [SDR CWQR20150119001](https://openairdocs.org/sdr/CWQR20150119001), Jan 19, 2015: TUBE. CRACKED. DURING A SCHEDULED INSPECTION WE FOUND THE BLEED AIR, AIR TUBE MOUNTING FLANGE CRACKED 1/3 THE WAY AROUND THE BLEED AIR TUBE ASSEMBLY. ABOUT 2.5 INCHES LONG. TH
- [SDR DXTA2014101305910](https://openairdocs.org/sdr/DXTA2014101305910), Oct 10, 2014: WHEEL. FAILED. DURING ROTATION, ACFT PITCHED UP VIOLENTLY REQUIRING SIGNIFICANT FWD PRESSURE ON THE YOKE TO AVOID OVER ROTATION. REMOVED ELEVATOR TRIM WHEEL & FOUND TRIM INDIC
- [SDR DXTA2013090405493](https://openairdocs.org/sdr/DXTA2013090405493), Sep 3, 2013: UPLOCK SWITCH. BROKEN. ON LANDING GEAR RETRACTION, RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED. TROUBLESHOT LANDING GEAR UNLOCK LIGHT, INSPECTED GEAR, FOUND LT MLG UPLOCK SWITCH BROK
- [SDR CWQR20110901019](https://openairdocs.org/sdr/CWQR20110901019), Sep 1, 2011: CONTROL CABLE. FRAYED. FRAYED ELEVATOR TRIM CABLE WAS FOUND DURING A SCHEDULED INSP. CABLE WAS FRAYED ONE THIRD OF THE CABLE'S DIAMETER. AND CABLE TENSION WAS WITHIN MM LIMITS.
- [SDR CWQR2011081515](https://openairdocs.org/sdr/CWQR2011081515), Aug 15, 2011: HINGE BRACKET. CRACKED. DURING AN INSPECTION, FOUND INBD ELEVATOR HINGE BRACKET CRACKED. IT WAS CRACKED IN THE UPPER BRACKET RADIUS AREA THAT ATTACHES TO THE UPPER SKIN OF THE HORIZ ST
- [SDR CWQR2011081514](https://openairdocs.org/sdr/CWQR2011081514), Aug 15, 2011: HINGE BRACKET. CRACKED. DURING AN INSPECTION, FOUND THE OTBD ELEVATOR HINGE BRACKET CRACKED. IT WAS CRACKED IN THE UPPER BRACKET RADIUS AREA THAT ATTACHES TO THE UPPER SKIN OF THE HORI
- [SDR DXTA2011031004502](https://openairdocs.org/sdr/DXTA2011031004502), Mar 10, 2011: DRAIN. OBSTRUCTED. ON CLIMB OUT, PASSING FL 220, RUDDER EFFECTIVENESS LOST. RUDDER FELT FROZEN. FREEZING LEVEL FL160. ON DESCENT REGAINED RUDDER EFFECTIVENESS AT FL140, JUST BELOW
- [SDR DXTA2010112402421](https://openairdocs.org/sdr/DXTA2010112402421), Nov 23, 2010: WINDSHIELD. FAILED. RT WINDSHIELD STARTED ARCHING AT 43,000 FT. COMPLETED THE EMERGRNCY CHECKLIST AND DESCENDED TO 10,000 FT. AROUND 20,000 FT THE WINDSHEILD SHATTERED.
- [SDR DXTA200803213](https://openairdocs.org/sdr/DXTA200803213), Aug 3, 2008: WARNING SYSTEM. ACTIVATED. ON A VISUAL APPROACH SELECTED GEAR DOWN AND GOT ONLY TWO GREEN INDICATORS. (S)

## 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/N588QS/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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