# N699QS: 2019 Textron 680A - Status: Valid registration - Airframe: [Textron 680A](https://openairdocs.org/model/textron-680a) (registry code 2076814, 10 seats) - Engine: [Pratt & Whitney Canada PW306D1](https://openairdocs.org/engine/pratt-whitney-canada-pw306d1) (registry code 51850) - Data sheets: [TCDS T00012WI](https://openairdocs.org/tcds/T00012WI) (Textron Aviation Inc.), [TCDS E35NE](https://openairdocs.org/tcds/E35NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: 680A0230 - Year built: 2019 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 9, 2019 - Certificate issued: September 9, 2025 - Expires: September 30, 2032 - Mode S code: A94D94 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=699QS - Page: https://openairdocs.org/aircraft/N699QS 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): 3 in force ### Matched by airframe (Textron 680A) - [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 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 2018-07-13](https://openairdocs.org/ad/2018-07-13): Landing Gear · Textron 510, 680 and 680A. Effective May 15, 2018 ### Matched by engine (Pratt & Whitney Canada PW306D1) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N699QS. ## NTSB investigations on N699QS not matched to an aircraft (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 CHI05LA277](https://openairdocs.org/ntsb/CHI05LA277), Sep 26, 2005: Cessna 560XL (N699QS), Columbus, OH, substantial damage. Probable cause: The collapse of the nose landing gear for undetermined reasons. ## FAA accident and incident reports None matched to N699QS. ## Reports on N699QS not matched to an aircraft (3) They name N699QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20130703013249I](https://openairdocs.org/incident/20130703013249I), Jul 3, 2013: Cessna 560XL (N699QS), Mesa, AZ, No damage. During takeoff roll crew observed display controller loose on instrument panel. Takeoff was aborted. - [Accident 20050926026089A](https://openairdocs.org/incident/20050926026089A), Sep 26, 2005: Cessna 560XL (N699QS), Columbus, OH, Substantial damage. (-23) Netjets aircraft N699QS was on the taxiway in a hold position. After being cleared to the hold short position, the aircraft started taxiing forward and… - [Incident 20030223008809I](https://openairdocs.org/incident/20030223008809I), Feb 23, 2003: Cessna 560XL (N699QS), Rochester, NY. (-23) After landing on runway 4 at Rochester airport, the aircraft was taxiing on taxiway "j". Taxiway "j" was ice and snow covered and is oriented… ## Service difficulty reports (19) 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 DXTA2025040702982](https://openairdocs.org/sdr/DXTA2025040702982), Apr 7, 2025: BATTERY PACK. INOPERATIVE. CABIN EMERG LIGHT: EMERGENCY LIGHT BATTERY PACK # 2 INOP. CORRECTIVE ACTION: SWAPPED EMERGENCY LIGHT CBS28-1 S/N 000150 FROM POSITION #2 TO POSITION #3 AND EMER - [SDR DXTA2024091900574](https://openairdocs.org/sdr/DXTA2024091900574), Sep 16, 2024: BATTERY PACK. FAILED. DURING THE EMERGENCY LIGHT PREFLIGHT CHECK THE AISLE LIGHTS UNDER SEAT 5 AND 8 AND THE OVERHEAD LIGHT ON SEAT 7 DID NOT ILLUMINATE. THE EMERGENCY LIGHTS FAIL TE - [SDR DXTA2024070612265](https://openairdocs.org/sdr/DXTA2024070612265), Jul 4, 2024: BATTERY. NO TEST. ON PREFLIGHT; EMER LIGHTS FAILED PREFIGHT TEST. COMPLETED TWO CHARGE CYCLES EACH OF 30 MINUTES. EMER LIGHTS STILL FAIL PREFLIGHT TEST. WAITED FOR THE APART TO A - [SDR DXTA2024042411586](https://openairdocs.org/sdr/DXTA2024042411586), Apr 23, 2024: BATTERY PACK. FAILED. AFT CABIN EMER EXIT LIGHTS DO NOT ILLUMINATE AT BEGINNING OF DUTY DAY. BATTERY PACKS ACCEPT 30 MINUTE CHARGING CYCLE AND AND ILLUMINATE NORMALLY AT END OF DAY O - [SDR 2024F00031](https://openairdocs.org/sdr/2024F00031), Feb 14, 2024: STINGER. CORRODED. CORROSION UNDER VORTEX GENERATORS ON THE RH AND LH SIDE OF THE P/N 6912610-6 STINGER. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ42984M1 REV A DATED FEB - [SDR DXTA2023101197680](https://openairdocs.org/sdr/DXTA2023101197680), Oct 10, 2023: UNKNOWN. UNKNOWN. WHEN DOOR IS UNLATCHED TO OPEN POSITION DOOR REMAINS UPRIGHT AND DOES NOT FALL OPEN. IN ORDER TO OPEN THE DOOR HAD TO PULL DOWN ON HANDLE TO GET IT TO FALL. ARR - [SDR DXTA2023082893990](https://openairdocs.org/sdr/DXTA2023082893990), Aug 26, 2023: UNKNOWN. UNKNOWN. FLOOR EMERG EXIT LIGHT: TOE KICK LIGHT IN LAV IS INOP REMOVED LAV FWD FASCLA TOEKICK PANEL TO GAIN ACCESS TO EMERGENCY TOEKICK LIGHT. FOUND ONE PIN ON THE LIGHT - [SDR DXTA2022102472560](https://openairdocs.org/sdr/DXTA2022102472560), Oct 21, 2022: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: LIGHT UNDER THE SEAT #10 . TOW KICK LIGHT A.KA AISLE LIGHT OPPOSITE OF THE MED STAYS ON WHEN BATTERIES ARE OFF AND DISCONNECTED . REMOVED THE - [SDR DXTA2022101371990](https://openairdocs.org/sdr/DXTA2022101371990), Oct 12, 2022: NONE. NONE. MAIN DOOR VISUAL INDICATOR: DOOR CLOSES AND "CLICKS" LOCKED WITH NO CAS MESSAGE OF DOOR OPEN. ALL 6 SIGHT GLASS WINDOWS DO NOT SHOW GREEN OR WHITE STRIPES. PERF - [SDR DXTA2022082969060](https://openairdocs.org/sdr/DXTA2022082969060), Aug 27, 2022: NONE. NONE. EMERG EXIT SIGN/LIGHT: MAIN CABIN DOOR EXIT LIGHT WILL NOT GO OFF SUSPECT G SWITCH TRIPPED // SIGNOFF // RESET INERTIA SWITCH PER CE 680A AMM 33·50·00. EMERGENC - [SDR DXTA2022081668180](https://openairdocs.org/sdr/DXTA2022081668180), Aug 17, 2022: HINGE FITTING. OUT OF RIG. MAIN DOOR: MAIN CABIN DIOR WILL NOT OPEN.//CORRECTIVE ACTION// ADJUSTED CABIN DOOR HINGE RIGGING IAW CE-680A AMM 52-10-00 OPS CHECK GOOD. - [SDR 2022FA0000044](https://openairdocs.org/sdr/2022FA0000044), Jan 25, 2022: NONE. NONE. LH AND RH HORIZONTAL CUFF PANEL LE, AND AREA ABOVE LH CUFF PANEL, EXPOSED COMPOSITE. REPAIRED IAW TEXTRON AVIAITON ENGINEERING REPORT NO: DQ33272 DATED JAN 23, - [SDR 2022F00103](https://openairdocs.org/sdr/2022F00103), Jan 24, 2022: AXLE. NICKED. LH MLG AXLE NICK. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ33273 DATED: 01/23/2022, 680A-0230, N699QS LH MLG AXLE NICK REPAIR RECOMMENDATION. - [SDR DXTA2021112952720](https://openairdocs.org/sdr/DXTA2021112952720), Nov 29, 2021: APU. DAMAGED. APU SMOKE: AFTER RUNNING THE APU FOR ABOUT 10 MINUTES WE SELECTED BLEED AIR ON. SMOKE BEGAN TO FILL THE COCKPIT AND CABIN. // SIGNOFF// REMOVED AND REPLACED INO - [SDR DXTA2021111651980](https://openairdocs.org/sdr/DXTA2021111651980), Nov 16, 2021: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: REPEAT WRITEUP. WITH POWER OFF AND BATTERIES DISCONNECTED, BOTH OVERWING EMER LIGHTS, SEATS 5,7,&8 EMER LIGHTS SND LAV EXIT LIGHTS REMAIN ON. - [SDR DXTA2021111551950](https://openairdocs.org/sdr/DXTA2021111551950), Nov 14, 2021: BATTERY. DEFECTIVE. EMERGENCY LIGHTING: NORMAL LANDING. BATTERIES DISCONECTED. STILL HAVE EMERGENCY LIGHTS BOTH OVERWING, SEAT 5 AND 8 PATHS, SEAT 7 AND LAV OVERHEAD - ALL REMAIN. - [SDR DXTA2021110351360](https://openairdocs.org/sdr/DXTA2021110351360), Nov 2, 2021: NONE. NONE. 1) CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS 2 FLOOR LEVEL REAR LIGHTS ALONG WITH UPPER LEFT REAR CABIN EMERGENCY LIGHT INOP. SEE VIDEO [T2PL6D008REUA]. 2) RIGH - [SDR DXTA2021072245590](https://openairdocs.org/sdr/DXTA2021072245590), Jul 21, 2021: SEAL. DEFECTIVE. MAIN DOOR: MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN/LOCK FROM INSIDE THE AIRCRAFT. TO SEEMS TO BE THE SAME WITH APU ON OR OFF. WORKS MUCH BETTER FROM OUTSIDE T - [SDR DXTA2021032940240](https://openairdocs.org/sdr/DXTA2021032940240), Mar 28, 2021: STRUT. DIRTY. MAIN DOOR: THE MAIN CABIN DOOR IS VERY HARD TO OPEN . WHEN YOU CLOSE THE DOOR YOU CAN HEAR A VERY DISTINCTIVE CLUNK. THE DOOR IS BINDING ON THE RIGHT SIDE OF TH ## Service difficulty reports on N699QS not matched to an aircraft (34) They name N699QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR CWQR2015022707](https://openairdocs.org/sdr/CWQR2015022707), Feb 27, 2015: FITTING. CRACKED. DURING A SCHEDULED INSPECTION WE FOUND CLIP PAN 6622034-8 CRACKED ONE INCH IN LENGTH. IT IS LOCATED ON THE OTBD SIDE OF RT WING STATION 188.88 AT THE FLAP AILER - [SDR CWQR20150227006](https://openairdocs.org/sdr/CWQR20150227006), Feb 27, 2015: FITTING. CRACKED. DURING A SCHEDULED INSPECTION WE FOUND CLIP PN 6622034-6 CRACKED ONE INCH IN LENGTH. IT IS LOCATED ON THE INBD SIDE OF RT WING STATION 188.88 AT THE FLAP AILERO - [SDR DXTA2012081305093](https://openairdocs.org/sdr/DXTA2012081305093), Aug 13, 2012: TRIM SYSTEM. MALFUNCTIONED. AFTER TAKEOFF, MORE THAN USUAL FORWARD PRESSURE ON YOKE WAS REQUIRED PRIOR TO FLAPS 0 DEGREES. AFTER LEVELING OFF AT FL190 (AUTO PILOT ON), AIRPLANE WAS USING M - [SDR DXTA2011053104597](https://openairdocs.org/sdr/DXTA2011053104597), May 30, 2011: UNKNOWN. VAPOR. AFTER LIFTOFF, THE COCKPIT FILLED WITH A NOXIOUS, VAPOR, THAT BURNED THE EYES. THE PRESSURIZATION SOURCE KNOB WAS SELECTED TO OFF AND THE CONDITION DID NOT WORS - [SDR DXTA2011051204577](https://openairdocs.org/sdr/DXTA2011051204577), May 12, 2011: SEAL. FAILED. LEFT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED DURING FLIGHT. LT OIL PRESSURE GAUGE READ 0. SHUT LT ENGINE DOWN IAW EMERGENCY CHECKLISTS. SUSPECT NR 4 BEARING S - [SDR DXTA2011030704493](https://openairdocs.org/sdr/DXTA2011030704493), Mar 6, 2011: RELAY. ERODED. AT POWER UP PRIOR TO TAKE OFF ANTISKID LIGHT ILLUMINATED. THE POWER BRAKE CB POPPED. RETURNED TO RAMP. POWER BRAKE HAD BLED DOWN SUFFICIENTLY AND PNUEMATIC BRAK - [SDR DXTA2010081604190](https://openairdocs.org/sdr/DXTA2010081604190), Aug 13, 2010: ENGINE. SMOKE. ABOUT 3 MINUTES AFTER DEPARTING AND CLIMBING TO 10,000 FT WE GOT A MASTER WARNING LIGHT AND A R OIL PRESSURE ANNUNCIATOR. ALSO, OBSERVED THAT THE OIL PRESSURE T - [SDR DXTA2010042604076](https://openairdocs.org/sdr/DXTA2010042604076), Apr 23, 2010: BRAKE ASSY. WEAK. CAPTAINS LT BRAKE PEDAL GOES ABOUT HALF WAY TO FLOOR BEFORE BRAKES BEGIN TO TAKE EFFECT. ONCE THAT POINT IS REACHED, BRAKES SEEMS TO WORK OK, BUT LT AND RT PEDA - [SDR DXTA2010041904072](https://openairdocs.org/sdr/DXTA2010041904072), Apr 16, 2010: B-NUT. LOOSE. LT BRAKE PEDAL ON THE CAPTAIN'S SIDE GOES ALL THE WAY TO THE STOP WITH LITTLE TO NO BRAKING EFFECT. FOUND LOOSE B-NUT ON LOW SIDE OF SYS. TIGHTENED B-NUT; BLED - [SDR DXTA2010040604061](https://openairdocs.org/sdr/DXTA2010040604061), Apr 5, 2010: BRAKE SYS. WEAK. CAPTAIN SIDE, LT BRAKE FEELS MUSHY AND TRAVELS TO THE FLOOR BEFORE ENGAGING THE BRAKE. COPILOTS BRAKES APPEAR NORMAL. PERFORMED BLEEDING PROCEDURE FOR THE BRAKE - [SDR DXTA2010032904055](https://openairdocs.org/sdr/DXTA2010032904055), Mar 28, 2010: MASTER CYLINDER. LEAKING. BRAKES IN LT SEAT FEEL MUSHY. THERE IS EXCESSIVE TRAVEL IN THE BRAKE PEDAL BEFORE YOU FEEL BRAKE PRESSURE. FOUND SIGNS OF FLUID LEAKING FROM PILOTS LT BRAKE MAS - [SDR DXTA2010030104007](https://openairdocs.org/sdr/DXTA2010030104007), Mar 1, 2010: BRAKE. WEAK. LT BRAKE PEDAL FROM BOTH LT AND RT VERY MUSHY AND VERY LITTLE BRAKING ACTION. FROM LT SEAT, LT PEDAL ALMOST GOES ALL THE WAY TO THE FLOOR BEFORE ANY BRAKING ACT - [SDR DXTA2009122103904](https://openairdocs.org/sdr/DXTA2009122103904), Dec 20, 2009: MASTER CYLINDER. INOPERATIVE. LT BRAKE PEDAL ON CAPTAINS SIDE FADES TO THE STOP. T/S FOUND LT SIDE OTBD MASTER CYLINDER BAD. REMOVED AND REPLACED MASTER CYLINDER WITH A OVERHAULED UNIT. BLED - [SDR DXTA2009102603826](https://openairdocs.org/sdr/DXTA2009102603826), Oct 23, 2009: BRAKE SYS. MALFUNCTIONED. TOTAL BRAKE FAILURE: WHEN WE BROUGHT THE GEAR DOWN THE BREAK LOW PSI AND ANTI SKID STAYED ON FOR A LONG TIME. WE STOPPED THE PLANE WITH THE EMERENCY BRAKES. INS - [SDR DXTA200702624](https://openairdocs.org/sdr/DXTA200702624), Nov 21, 2007: WINDSHIELD. FAILED. CAPTAINS WINDSHIELD SHATTERED AT FL400 - OUTSIDE ONLY, NO PRESSURIZATION LOSS. REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW MM 56-11-00 OPS CHECK GOOD. - [SDR DXTA200702553](https://openairdocs.org/sdr/DXTA200702553), Oct 19, 2007: COUPLING. DISCONNECTED. LOSS OF NORMAL CABIN PRESSURIZATION OCCURRED IN FLIGHT. FOUND THE FWD COUPLING AT THE WATER SEPARATOR ASSY, TO HAVE COME DISCONNECTED FROM THE AIR DUCT ASSY PN - [SDR DXTA200701892](https://openairdocs.org/sdr/DXTA200701892), Jan 30, 2007: UNKNOWN. UNKNOWN. AFTER GEAR RETRACTION, ALL GREEN LIGHTS WENT OUT BUT THE RED UNLOCK STAYED ON. PULLED THE GEAR CONTROL CB AND THE RT MAIN WENT TO DOWN AND LOCKED. THE LT MAIN A - [SDR DXTA200701885](https://openairdocs.org/sdr/DXTA200701885), Jan 28, 2007: ACTUATOR. INOPERATIVE. UPON LANDING GEAR RETRACTION, GEAR DOWN GREEN LIGHTS GO OUT BUT RED LIGHT AND HYD PRESS LIGHTS REMAIN ON. REPLACED UPLOCK ACTUATOR AND RIGGED UPLOCK SWITCH IAW - [SDR DXTA200701866](https://openairdocs.org/sdr/DXTA200701866), Jan 19, 2007: UPLOCK SWITCH. MALFUNCTIONED. UPON RAISING GEAR , GEAR UNLOCK REMAINED ON HYD PRESS REMAINED ON, STAB MISCOMPARE ILLUMINATED . UPON PULLING HYD CONTROL CB, RT MAIN GEAR LIGHT ILLUMINATED. TR - [SDR DXTA200701858](https://openairdocs.org/sdr/DXTA200701858), Jan 16, 2007: UPLOCK SWITCH. MALFUNCTIONED. AFTER RAISING LANDING GEAR ON TAKEOFF GEAR UNLOCK LIGHT REMAINED ON. ((3) OTHER GEAR INDICATORS BLANK). HYD PRESS ANNUN ILLUMINATED. UPON RAISING FLAPS TO 0 DEG - [SDR DXTA200601790](https://openairdocs.org/sdr/DXTA200601790), Dec 8, 2006: UPLOCK SWITCH. OUT OF ADJUST. GEAR SEEMED TO RETRACT NORMALLY, BUT UNLOCK LIGHT REMANED ILLUMINATED. STAB MISCOMPARE + HYD PRESS LIGHT ALSO ON AFTER 30 SECONDS. ALL INDICATIONS NORMAL ONCE G - [SDR DXTA200601773](https://openairdocs.org/sdr/DXTA200601773), Dec 3, 2006: UPLOCK SWITCH. FAILED. LANDING GEAR WILL NOT FULLY RETRACT UNLOCK LIGHT ILLUMINATED. TROUBLESHOT TO FAILED LT MLG UPLOCK SWITCH REMOVED AND REPLACED SWITCH. PERFORMED LANDING GEAR FUN - [SDR DXTA200601695](https://openairdocs.org/sdr/DXTA200601695), Oct 29, 2006: RESERVOIR. LOW. AFTER TAKEOFF WHEN RETRACTING LANDING GEAR ALL GREEN LIGHTS EXTINGUISHED AND RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. HYD PRESS CAUTION LIGHT REMAINED ON. GE - [SDR DXTA200601577](https://openairdocs.org/sdr/DXTA200601577), Aug 25, 2006: DISPLAY. LOOSE. UPON HITTING A POTHOLE DURING T/O ACCELERATION ON RUNWAY, LEFT PFD SLIDED TOWARD YOKE ABOUT 2 INCHES AND WENT BLANK. T/O WAS ABORTED. PUSHED BACK THE PFD IN PLA - [SDR DXTA200601546](https://openairdocs.org/sdr/DXTA200601546), Aug 9, 2006: MASTER CYLINDER. UNKNOWN. ON LANDING, DURING GEAR EXTENSION "LO BRAKE PRESS" CAUTION LIGHT ILLUMINATED MOMENTARILY. CAPTIANS RIGHT BRAKE PEDAL REQUIRES MORE TRAVEL TO ACTIVATE BRAKES WIT - [SDR DXTA200601515](https://openairdocs.org/sdr/DXTA200601515), Jul 21, 2006: CONTROL VALVE. INOPERATIVE. WHILE TURNING LEFT INTO PARKING, HAD A SIGNIFICANT LOSS OF EFFECTIVENESS ON THE RIGHT BRAKE. AIRCRAFT PIN-WHEELED 45 DEGREES LEFT BEFORE COULD GET IT STOPPED US - [SDR DXTA200601345](https://openairdocs.org/sdr/DXTA200601345), Apr 16, 2006: CLIP. FAULTY. DURING TAKEOFF ROLL (NO TAKEOFF) LIGHT ILLUMINATED AND WARNING HORN SOUNDED. TAKEOFF WAS ABORTED. DURING TROUBLESHOOTING NOTICED THAT EXTENDING THE SPEED BRAKES - [SDR DXTA200500987](https://openairdocs.org/sdr/DXTA200500987), Sep 28, 2005: LANDING GEAR. COLLAPSED. NOSE GEAR RETRACTED WHILE TAXIING, AIRCRAFT SUSTAINED DAMAGE TO THE NOSE STRUCTURE AREA. DAMAGE TO AIRCRAFT IS BEING TEMPORARILY REPAIRED FOR A ONE TIME FERRY F - [SDR DXTA200500599](https://openairdocs.org/sdr/DXTA200500599), Feb 18, 2005: PUMP. FAILED. LOW BRAKE PRESSURE AND ANTI-SKID INOP. ANNUNCIATORS ILLUMINATED WITH MASTER CAUTION. BRAKE PUMP WOULD NOT RUN. SMELL OF ELECTRICAL BURN IN COCKPIT. AFTER APPROX - [SDR DXTA200500520](https://openairdocs.org/sdr/DXTA200500520), Jan 7, 2005: CYLINDER. MALFUNCTIONED. RED UNLOCK LIGHT ON GEAR FLASHED (OR CYCLED) AFTER GEAR RETRACTION. UPON EXTENDING GEAR, HAD 2 "BUMPS" LIKE HYDRAULIC ACTUATION RESULTING IN MOMENTARY LOSS OF D - [SDR DXTA200400322](https://openairdocs.org/sdr/DXTA200400322), Jun 12, 2004: POSITION SWITCH. MALFUNCTIONED. AFTER TAKEOFF NOSE WHEEL LANDING GEAR GREEN LIGHT REMAIN ILLUMINATED, DID NOT EXTINGUISH AFTER GEAR WAS RECYCLED. REMAINED ON FOR THE DURATION OF FLIGHT, UPON L - [SDR DXTA200300187](https://openairdocs.org/sdr/DXTA200300187), Nov 15, 2003: CONTROL CABLE. CHAFED. PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT - [SDR DXTA200300067](https://openairdocs.org/sdr/DXTA200300067), Jul 14, 2003: HUB CAP. OUT OF POSITION. ABORTED TAKE-OFF DUE TO ANTI SKID LIGHT THEN BRAKES FAILED, USED EMERGENCY BRAKE TO STOP AIRCRAFT. - NOTED LEFT WHEEL HUB CAP TRANSDUCER CLIP POSITIONED INCORRE - [SDR DXTA200300033](https://openairdocs.org/sdr/DXTA200300033), May 13, 2003: ODOR. DETECTED. WHILE ENROUTE AT FL280 NOTICED STRONG ODOR IN COCKPIT + CABIN. PIC + SIC DEVELOPED HEADACHE + BURNING EYES. USED O2. ONCE AT 3000' , SELECTED OFF ON PRESSURIZAT ## STCs that may be installed (OpenAirDocs) (16) 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 (Textron 680A) - [STC ST04765NY](https://openairdocs.org/stc/ST04765NY): Unprepared (Grass/Sod) Runway Operations. Textron Aviation Inc - [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems - [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 ST122244IB](https://openairdocs.org/stc/ST122244IB): Installation of Gogo Galileo system, including HDX Antenna. Alamo Engineering GmbH - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc - [STC ST11983SE](https://openairdocs.org/stc/ST11983SE): Installation of Starlink Aviation System. AeroMech Incorporated - [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 ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine - [STC ST02037WI](https://openairdocs.org/stc/ST02037WI): Installation of Gogo Business Aviation AVANCE L5 System with MB 13 Antennas. Duncan Aviation Inc - [STC ST04736NY](https://openairdocs.org/stc/ST04736NY): True Blue TS28 Emergency Battery Power Supply Replacement. Aerospace Design and Compliance LLC - [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC - [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc - [STC ST04367CH](https://openairdocs.org/stc/ST04367CH): Installation of a Medical Interior in accordance with LifePort Master Data List EGR-887-000-001, Revision (B), dated April 18, 2019 or later FAA approved revision and LifePort Master Drawing List MDL-887-00, Revision (D), dated April 11, 2019 or later FAA approved revision.". LifePort LLC - [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 ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc - [STC ST11168SC](https://openairdocs.org/stc/ST11168SC): Installation of a Pratt & Whitney Flight Data Acquisition, Storage, and Transmission System (FAST). Pratt & Whitney Engine Services Inc ## Related - Other Textron 680A aircraft: https://openairdocs.org/model/textron-680a/aircraft.md - The Pratt & Whitney Canada PW306D1 engine: https://openairdocs.org/engine/pratt-whitney-canada-pw306d1.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.