# N678QS: 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: 560-5616
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 13, 2006
- Certificate issued: June 22, 2021
- Expires: June 30, 2028
- Mode S code: A8FADF
- 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=678QS
- Page: https://openairdocs.org/aircraft/N678QS

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 N678QS.

## FAA accident and incident reports

None matched to N678QS.

## Service difficulty reports (46)

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 DXTA2026091409665](https://openairdocs.org/sdr/DXTA2026091409665), Sep 11, 2026: HANDLE. DAMAGED. MAIN CABIN DOOR TAKES EXCESSIVE FORCE TO OPEN AND CLOSE THE DOOR HANDLE. THE PRECATCH IS STUCK IN THE PULLED POSITON AND WILL NOT ENGAGE. THE DOOR IS HAVING THE
- [SDR 2026FA0000171](https://openairdocs.org/sdr/2026FA0000171), Mar 11, 2026: SKIN. CORRODED. RH WINGTIP SKIN UNDER OTBD STATIC WICK BASE IS HEAVILY CORRODED. COMPLIED WITH NETJETS RFTS-116596 REV.0 TITLE: N678QS (560-5616) WING TIP STATIC WICK BASE CORR
- [SDR 2026FA0000170](https://openairdocs.org/sdr/2026FA0000170), Mar 11, 2026: DECK PLATE. CORRODED. POTTY DECK CORRODED. REPAIRED POTTY DECK PER NETJETS RFTS-116581 REV.0 TITLE: N678QS (560-5616) TOILET DECK SKIN CORROSION DATED 10MAR26. THIS IS A PERMANENT MI
- [SDR DXTA2026020306745](https://openairdocs.org/sdr/DXTA2026020306745), Jan 30, 2026: LIGHT. INOPERATIVE. EMERGENCY EGRESS LIGHTS REMAIN ON THE RIGHT SIDE OF THE FUSELAGE WITH THE BATTERY OFF, PASSENGER SAFETY OFF AND THE EMERGENCY LIGHT SWITCH OFF. INSIDE THE CABIN
- [SDR DXTA2026012806685](https://openairdocs.org/sdr/DXTA2026012806685), Jan 26, 2026: BATTERY PACK. DEFECTIVE. EMERGENCY LIGHTS REMAIN ON, RIGHT SIDE OF FUSELAGE WITH THE BATTERY OFF, PASSENGER SAFETY OFF AND EMERGENCY LIGHT SWITCH OFF. INSIDE THE CABIN TWO EXIT LIGHTS R
- [SDR DXTA2026012606667](https://openairdocs.org/sdr/DXTA2026012606667), Jan 24, 2026: SWITCH. OUT OF POSITION. EMERGENCY EGRESS LIGHTS ON THE RIGHT SIDE OF FUSELAGE REMAINED ILLUMINATED WITH THE BATTERY OFF AND PASSENGER SAFETY OFF AND EMERGENCY LIGHTS OFF. INSIDE THE CA
- [SDR DXTA2025061903930](https://openairdocs.org/sdr/DXTA2025061903930), Jun 17, 2025: TRANSDUCER. FAULTY. DURING TAXI, ANTI-SKID INOP ANNUNCIATOR ILLUMINATED FOR APPROXIMATELY 10 SECONDS THEN EXTINGUISHED. THE SKID CONTROL CIRCUIT BREAKER AND THE POWER BRAKES CIRCUI
- [SDR DXTA2025052303575](https://openairdocs.org/sdr/DXTA2025052303575), May 21, 2025: CIRCUIT BREAKER. FAILED. DURING PREFLIGHT INSPECTION AFT, EQUIPMENT BAY FOUND CIRCUIT BREAKER HT043 POPPED. REPLACED HT043 CB. ALL OPS CHECKS GOOD. ALL WORK PERFORMED IN ACCORDANCE WITH
- [SDR DXTA2025051903539](https://openairdocs.org/sdr/DXTA2025051903539), May 18, 2025: WIRE. BROKEN. EMERGENCY LIGHTING: REPEAT, FRONT HALF OF THE EMERGENCY LIGHTS WILL NOT TURN ON (TRIED: EMER LIGHTS ON, EMER LIGHTS ARM DC POWER OFF AND EMER LIGHTS ON PASS SAF
- [SDR DXTA2025022502452](https://openairdocs.org/sdr/DXTA2025022502452), Feb 21, 2025: SHIMMY DAMPENER. WORN. VIOLENT NOSE WHEEL SHIMMY ON TAKEOFF ROLL. ABORTED TAKEOFF BETWEEN 40 - 50 KNOTS. INSPECTED NOSE LANDING GEAR AND NOSE WHEEL TIRE. FOUND NLG TIRE TO BE OUT OF R
- [SDR DXTA2025021002262](https://openairdocs.org/sdr/DXTA2025021002262), Feb 6, 2025: VALVE. DEFECTIVE. CENTRAL WARNING SYSTEMS: CABIN DOOR SEAL WILL NOT DEFLATE WITH APU RUNNING. UNABLE TO CLOSE MSIN CABIN DOOR. CORRECTIVE ACTION: REPLACED VALVE. OPS CHECK GOOD. 
- [SDR DXTA2025021002261](https://openairdocs.org/sdr/DXTA2025021002261), Feb 6, 2025: VALVE. DEFECTIVE. CENTRAL WARNING SYSTEMS: CABIN DOOR SEAL WILL NOT DEFLATE WITH APU RUNNING. UNABLE TO CLOSE MSIN CABIN DOOR. CORRECTIVE ACTION: REPLACED INFLATION/DEFLATION VAL
- [SDR DXTA2024121101439](https://openairdocs.org/sdr/DXTA2024121101439), Dec 8, 2024: LATCH. OUT OF ADJUST. MAIN DOOR: CABIN DOOR WILL NOT OPEN WITH MAIN DOOR HANDLE. VERIFIED THE FAUL TY WAS ACTIVE. WE ADJUSTED THE POSTION OF THE LATCH PLATE AND PERFORMED MULTIPLE SU
- [SDR DXTA2024121101434](https://openairdocs.org/sdr/DXTA2024121101434), Dec 7, 2024: PRECATCH. OUT OF ADJUST. CABIN DOOR WILL NOT OPEN WITH MAIN DOOR HANDLE. PERFORMED MAIN CABIN DOOR PRECATCH ADJUSTMENT IN REF TO CESSNA 560XL AMM 52-10-01. MAIN CABIN DOOR OPENS NORMALL
- [SDR DXTA2024062012116](https://openairdocs.org/sdr/DXTA2024062012116), Jun 20, 2024: HANDLE. LACK OF LUBE. WHEN OPENING CABIN DOOR, DOOR HANDLE WAS EXTREMELY STIFF ROTATING TO THE 10 O'CLOCK POSITION, BECAME MORE DIFFICULT TO REACH UNLATCH POINT. AFTER UNLATCHING DOO
- [SDR DXTA2024042411588](https://openairdocs.org/sdr/DXTA2024042411588), Apr 23, 2024: PRESSURE SWITCH. FAILED. DURING TAXI THE LO BRK PRESS AND ANTISKD INOP ANNUNCIATORS FLASHING ALONG WITH A FLASHING MASTER CAUTION. NORMAL BRAKING INEFFECTIVE & ACFT BROUGHT TO A STOP US
- [SDR 2024FA0000294](https://openairdocs.org/sdr/2024FA0000294), Apr 5, 2024: WEB. CHAFED. DURING THE 96 MONTH INSPECTION FOUND THE RH WEB FORWARD OF E-EXIT TO HAVE 3 EACH CHAFE LOCATIONS. REPAIR 3 CHAFFED AREAS ROUND E-EXIT PER AQRD ERO-979437. REPAI
- [SDR JGVR202404050002](https://openairdocs.org/sdr/JGVR202404050002), Apr 5, 2024: STRAKE. CORRODED. DURING THE VENTRAL STRAKE COIN TAP TEST FOUND MULTIPLE SPOT OF SURFACE LEVEL CORROSION. PERFORM REPAIR TO RH STRAKE CORROSION. COMPLIED WITH RFTS-110419 REV.0 D
- [SDR JGVR202404050001](https://openairdocs.org/sdr/JGVR202404050001), Apr 5, 2024: STRAKE. CORRODED. DURING THE VENTRAL STRAKE COIN TAP TEST FOUND MULTIPLE SPOT OF SURFACE LEVEL CORROSION. PERFORM REPAIR TO LH STRAKE CORROSION. COMPLIED WITH RFTS-110424 REV.0 D
- [SDR DXTA2023101097660](https://openairdocs.org/sdr/DXTA2023101097660), Oct 10, 2023: MOTOR. FAULTED. WHEN TAXIING OUT, CREW HEARD A POP AND ANTI-SKID ANNUNCIATOR ILLUMINATED. CREW WAS ABLE TO BRING AIRCRAFT TO A STOP. SOON AFTER LOW BRAKE PRESS FLASHING ANNUNCI
- [SDR DXTA2023091895640](https://openairdocs.org/sdr/DXTA2023091895640), Sep 17, 2023: LIGHT. BROKEN. FLOOR EMERG EXIT LIGHT: LEFT SIDE (FWD) EMER FLOOR LIGHTING INOP. POWERED ON EMERGENCY LIGHTING AND DUPLICATED DISCREPANCY. PERFORMED POWER AND GROUND CHECK TO 
- [SDR DXTA2023070690370](https://openairdocs.org/sdr/DXTA2023070690370), Jul 5, 2023: HANDLE. DEFECTIVE. LEFT MLG LANDING GEAR RETRACTION: AFTER TAKEOFF, SELECTED GEAR HANDLE UP. THE GEAR REMANDED DOWN AND LOCKED, 3 GREEN INDICATION. USED THE CESSNA CHECKLIST: LAND
- [SDR DXTA2021060142890](https://openairdocs.org/sdr/DXTA2021060142890), Jun 1, 2021: UNKNOWN. ODOR. AT 37,000 FT BOTH CREWMEMBERS NOTED A BOLD ACRYLIC ODOR IN THE COCKPIT. RAN ENVIRONMENTAL SMOKE/ODOR CHECKLIST. AFTER ABOUT A MINUTE, ODOR SEEMED TO DISSIPATE. 
- [SDR DXTA2021051341940](https://openairdocs.org/sdr/DXTA2021051341940), May 12, 2021: FAN. DEFECTIVE. WHILE IN CRUISE FLIGHT AT 39,000FT, WE HAD A STRONG ODOR FILL THE COCKPIT AND CABIN. THE CREW AND PAX BOTH NOTICED THE SMELL AND IT WAS ON THE SIDE OF AN ELECTR
- [SDR DXTA2021041340760](https://openairdocs.org/sdr/DXTA2021041340760), Apr 13, 2021: SOCKET. OUT OF ADJUST. MAIN DOOR: MAIN CABIN DOOR VERY DIFFICULT TO CLOSE FROM OUTSIDE OF CABIN . SOUNDS LIKE METAL GRINDING. ADJUSTED AFT BOTTOM PIN SOCKET, GAINED SUBSTANTIAL EASE O
- [SDR DXTA2020081703988](https://openairdocs.org/sdr/DXTA2020081703988), Aug 17, 2020: SERVO. DEFECTIVE. WHILE DEPARTING GED WE LEVELED OFF AT 2000 FEET WITH AUTOPILOT ON. WE WERE THEN GIVEN A CLIMB TO 7000 AND A RIGHT TURN TO 090, WE WERE ALSO MAINTAINING AROUND 2
- [SDR DXTA2019093002908](https://openairdocs.org/sdr/DXTA2019093002908), Sep 29, 2019: WATER SEPARATOR. ODOR. COCKPIT ODOR - DESCENDING FROM CRUISE ALT OF FL400. STARTED GETTING A STRONG ORDER SIMILAR TO JET EXHAUST. IT SMELLED DIFFERENT THAN WHEN THE HEAT IS TURNED UP.
- [SDR DXTA2019070302565](https://openairdocs.org/sdr/DXTA2019070302565), Jul 2, 2019: FIRE LOOP. OUT OF POSITION. WHILE ENROUTE AT FL220 AND LESS THAN 10C JUST PRIOR TO ENTERING CLOUDS THE WING ENGINE ANTI ICE WAS TURNED ON. WITHIN APPROXIMATELY 2-4 SECONDS THE LEFT ENGINE 
- [SDR DXTA2019062802547](https://openairdocs.org/sdr/DXTA2019062802547), Jun 28, 2019: COALESCER BAG. CONTAMINATED. CABIN ODOR OIL ODOR. BEGINNING OF DECENT FROM 41,000 FEET WITH THE APU OFF, PASSENGER CAME FORWARD COMPLAINING OF AN ODOR IN THE CABIN. CREW MEMBER WENT BACK AN
- [SDR 2019F00206](https://openairdocs.org/sdr/2019F00206), May 16, 2019: SKIN. CHAFED. LEFT AND RIGHT LOWER SKINS DAMAGE (CHAFE). REFERENCE REPAIR MEMO DQ19462M1, DATED MAY 13, 2019.
- [SDR DXTA2018071601174](https://openairdocs.org/sdr/DXTA2018071601174), Jul 11, 2018: TRUNNION. LACK OF LUBE. LANDING GEAR WARNING HORN ACTIVATED, RT MLG BULB DID NOT ILLUMINATE UPON GEAR EXTENSION AND THE RED UNLOCK LIGHT REMAINED ILLUMINATED. WHEN TESTED, THE RT LG BU
- [SDR DXTA2018052951004](https://openairdocs.org/sdr/DXTA2018052951004), May 25, 2018: EEC. MALFUNCTIONED. RIGHT ENGINE LOW POWER, ENGINE DID NOT MAKE TAKE OFF POWER BY 4 OR 5 %, RIGHT ITT WAS HIGHER THAN THE LEFT, ALL THE REST THE ENGINE PARAMETERS WERE MATCHED. AT 
- [SDR DXTA201805250991](https://openairdocs.org/sdr/DXTA201805250991), May 23, 2018: ENGINE. POWER LOSS. RIGHT ENGINE NOT DEVELOPING FULL POWER DURING CLIMB. COULD NOT DUPLICATE DISCREPANCY. REMOVED AND REPLACED EEC INTERFACE PCB AS A PRECAUTIONARY IAW MM 24-51-01.
- [SDR CWQR20160725026](https://openairdocs.org/sdr/CWQR20160725026), Jul 25, 2016: SKIN. CORRODED. CORROSION WAS DISCOVERED ON THE VERTICAL STABILIZER SKIN. THE CORROSION WAS REMOVED AND VERTICAL STABILIZER SKINS WERE REPAIRED IAW ERO-850036, REV IR.
- [SDR CWQR20160725025](https://openairdocs.org/sdr/CWQR20160725025), Jul 25, 2016: SKIN. CORRODED. CORROSION WAS DISCOVERED ON THE VERTICAL STABILIZER SKIN. THE CORROSION WAS REMOVED AND VERTICAL STABILIZER SKINS WERE REPAIRED IAW ERO-850036, REV IR.
- [SDR DXTR20121015002](https://openairdocs.org/sdr/DXTR20121015002), Oct 15, 2012: AXLE. CORRODED. RIGHT MLG AXLE CORRODED UNDER BRAKE ASSY. R & R AXLE ASSY BY REPLACING TRAILING LINK ASSY IAW COMPONENT MM 32-10-01. TRAILING LINK ASSY, NR 6641648-14, SN 3911.
- [SDR DXTR 20121015001](https://openairdocs.org/sdr/DXTR%2020121015001), Oct 15, 2012: BRACKET. CRACKED. DURING A ROUTINE A/B INSPECTION, DISCOVERED THE AUTOPILOT RUDDER CABLE BRACKET LOCATED AFT OF THE CANTED BULKHEAD IS CRACKED IN 2 PLACES. REPLACED RUDDER AUTO P
- [SDR CWQR20110901017](https://openairdocs.org/sdr/CWQR20110901017), Sep 1, 2011: CONTROL CABLE. FRAYED. FRAYED ELEVATOR TRIM CABLE WAS FOUND DURING A SCHEDULED INSPECTION. CABLE WAS FRAYED A QUARTER OF THE CABLE'S DIAMETER AND TENTION WAS 2 POUNDS BELOW MM LIMITS.
- [SDR DXTA2010090804226](https://openairdocs.org/sdr/DXTA2010090804226), Sep 7, 2010: SERVO VALVE. SURGES. LEFT EEC ANNUNCIATOR ILLUMINATED DURING FLIGHT. LT ENGINE RESPONDED TO THROTTLE INPUT. COMPLETED ABNORMAL CHECKLIST. LT N1 & N2 WOULD NOT REMAIN CONSTANT, FLUCT
- [SDR 2009F00119](https://openairdocs.org/sdr/2009F00119), Nov 24, 2009: HYDRAULIC SYSTEM. WARNING MESSAGE. ON TAKE OFF; RT ENG "LO HYD FLOW R" CAME ON STEADY, L - FLASHING. AFTER 30 SECONDS "LO HYD LEVEL" ON STEADY. GEAR, FLAPS, T/R'S ALL DEPLOYED NORMAL BUT SLOWLY. 
- [SDR DXTA2009082103763](https://openairdocs.org/sdr/DXTA2009082103763), Aug 20, 2009: PUSHROD. OUT OF ADJUST. AFTER TAKEOFF ACFT ROLLED LEFT. EXCESSIVE PRESSURE NEEDED TO FLY STRAIGHT. A/P WAS OFF AND TRIMS WERE NEUTRAL. YOKE TURNED APPROX 45 DEG TO THE RT TO MAINTAIN H
- [SDR DXTA200808163231](https://openairdocs.org/sdr/DXTA200808163231), Aug 16, 2008: COMPRESSOR. STALLED. LT ENGINE EXPERIENCED COMPRESSOR STALL AS THROTTLES WERE ADVANCED FOR TAKEOFF. N1 WAS APPROX 70 PERCENT WHEN STALL OCCURRED. ACCOMPLISHED TROUBLESHOOT FOR COMPR
- [SDR DXTA200803231](https://openairdocs.org/sdr/DXTA200803231), Aug 16, 2008: COMPRESSOR. STALLED. LEFT ENG EXPERIENCED COMPRESSOR STALL AS THROTTLES WERE ADVANCED FOR TAKEOFF. ABORTED TAKEOFF. (S)
- [SDR DXTA200807183182](https://openairdocs.org/sdr/DXTA200807183182), Jul 18, 2008: AILERON. OUT OF RIG. DURING OCF FLIGHT FOR CONTROL CABLE CHANGE, WITH THE AILERON AND RUDDER TRIM WHEELS CENTERED, THE PLANE ROLLED LT AGGRESSIVELY ON TAKEOFF AND AT CRUISE SPEED. T
- [SDR DXTA200803182](https://openairdocs.org/sdr/DXTA200803182), Jul 17, 2008: TRIM SYSTEM. OUT OF ADJUST. DURING OCF FLIGHT FOR CONTROL CABLE CHANGE, WITH THE AILERON AND RUDDER TRIM WHEELS CENTERED, THE PLANE ROLLED LT AGGRESSIVELY ON TAKEOFF AND AT CRUISE SPEED. T
- [SDR DXTA200702623](https://openairdocs.org/sdr/DXTA200702623), Nov 21, 2007: SWITCH. OUT OF ADJUST. CRUISING AT FL 270 AND 270 KIAS, THE CABIN DOOR LIGHT ILLUMINATED. ADJUSTED SWITCH. LIGHT EXTINGUISHES WHILE PRESSURIZED AND UNPRESSURIZED. IAW CE560 XL MM 52-7

## 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/N678QS/stcs.md

## Earlier aircraft with N678QS

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N678QS before.

- [Cancelled 2003-11-07](https://openairdocs.org/deregistered/N678QS-2003-11-07): Cessna 560XL, S/N 560-5353. Exported to Spain. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## 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

---
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.