# N622QS: 2021 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: 680A0268 - Year built: 2021 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 5, 2021 - Certificate issued: July 7, 2026 - Expires: July 31, 2033 - Mode S code: A81F1A - Owner type: Co-owned - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=622QS - Page: https://openairdocs.org/aircraft/N622QS 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 N622QS. ## FAA accident and incident reports None matched to N622QS. ## Reports on N622QS not matched to an aircraft (1) They name N622QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20101019050609I](https://openairdocs.org/incident/20101019050609I), Oct 19, 2010: Cessna 560XL (N622QS), Sedona, AZ, Minor damage. During initial landing into sez, landing on rwy 21 nose wheel bounced three times, on third bounce pilot executed a go-around, regained control and landed on… ## Service difficulty reports (18) 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 DXTA2026101910200](https://openairdocs.org/sdr/DXTA2026101910200), Oct 15, 2026: PROXIMITY SWITCH. FAULTED. AMBER CABIN DOOR OPEN AND CHECK DOORS CAS MESSAGES CAME ON IN CRUISE AT FL410. COMPLETED QRH AND CAS MESSAGES REMAINED FOR DURATION OF FLIGHT AND AFTER LANDING. - [SDR DXTA2026101310119](https://openairdocs.org/sdr/DXTA2026101310119), Oct 10, 2026: PCB. FAULTED. CABIN DOOR OPEN AMBER CAS IN FLIGHT. REPLACED PCB. OPS CHECK GOOD. IAW CE680A AMM 24-60-40 - [SDR DXTA2026091009626](https://openairdocs.org/sdr/DXTA2026091009626), Sep 9, 2026: WIRE HARNESS. DAMAGED. DURING CRUISE AT 43000 THE CHECK DOORS AND CABIN DOOR OPEN CAUTION MESSAGES APPEARED. WE COMPLIED WITH QRH PROCEDURES AND LANDED UNEVENTFULLY. MESSAGES STAYED T - [SDR 2026F00184](https://openairdocs.org/sdr/2026F00184), Aug 25, 2026: FITTING. CORRODED. REMOVED NOSE LANDING GEAR ACTUATOR FITTING ASSEMBLY DUE TO LEVEL 2 CORROSION. INSTALLED NEW FITTING PER SR-680A-ATA53-33739 REV. A, STANDARD REPAIR - NLG ACTUAT - [SDR DXTA202608030169](https://openairdocs.org/sdr/DXTA202608030169), Aug 3, 2026: SKIN. CORRODED. FOUND SEVERAL AREAS WITH EVIDENCE OF CORROSION ON THE LT UPPER AND LOWER HORIZONTAL STABILIZER. PERFORM NJA WC: TEXTRON 680/680A HORIZONTAL STABILIZER LOWER SKI - [SDR 2026F00140](https://openairdocs.org/sdr/2026F00140), Jul 6, 2026: STRINGER. CORRODED. FOUND EVIDENCE OF CORROSION ON THE APU STINGER ASSY, LOWER AREA, AFT OF PANEL 330BBC. MECHANICALLY REMOVED SEVERAL AREAS OF CORROSION LOCATED ON APU STINGER, LO - [SDR DXTA2026061608432](https://openairdocs.org/sdr/DXTA2026061608432), Jun 13, 2026: PCB. FAULTY. AMBER CAS MESSAGE CABIN DOOR OPEN AND ASSOCIATED CHECK DOORS CAME ON AT CRUISE 39000. RAN QRH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CED MONITOR PCB - [SDR DXTA2025082604706](https://openairdocs.org/sdr/DXTA2025082604706), Aug 23, 2025: FLAP SYSTEM. FAILED. FLAPS FAIL AMBER CAS MSG ON APPROACH. RESET 1X & MSG REMAINED. FLAPS FAILED IN NR 1. INSPECT, BITES 2, 5, 6, & 8 SET ON FLAP CONTROLLER. FLAPS OPS. CLEARED FAUL - [SDR DXTA2025051003435](https://openairdocs.org/sdr/DXTA2025051003435), May 10, 2025: TEE FITTING. LEAKING. OXYGEN PRESSURE INDICATION: REPEAT WRITE UP. RETURNED TO AC THIS MORNING AFTER AOG OF 02 INDICATING SYSTEM LAST NIGHT. INITIAL INDICATION WAS 1700 PSI. INDICATI - [SDR DXTA2024032511306](https://openairdocs.org/sdr/DXTA2024032511306), Mar 24, 2024: BATTERY. DISCHARGED. LAV EXIT SIGN/LIGHT: REPEAT WRITE UP. LOWER LAV EXIT SIGN WILL NOT ILLUMINATE WITH BATTERIES OFF AND EMER SWITCH IN ARM POSITION. POWERED AIRCRAFT AND PERFQRRNE - [SDR DXTA2024032511305](https://openairdocs.org/sdr/DXTA2024032511305), Mar 24, 2024: BATTERY. FAILED. EXIT SIGN ABOVE SEAT 7 WONT ILLMINATE WITH THE BATTERIES OFF AND EMER LIGHT SWITCH IN ARM POSITION. R & R NR 4 BATTERY PACK IAW MM 33-50-06. - [SDR DXTA2024032111268](https://openairdocs.org/sdr/DXTA2024032111268), Mar 21, 2024: SWITCH. OUT OF POSITION. EMERG EXIT SIGN/LIGHT: EMERGENCY EXIT SIGN ABOVE SEAT 7 DOES NOT ILLUMINATE. LAV EXIT SIGN/LIGHT: EMERGENCY EXIT SIGN LIGHT BELOW THE LAV SEAT DOES NOT ILLUMINA - [SDR DXTA2023071790910](https://openairdocs.org/sdr/DXTA2023071790910), Jul 14, 2023: UNKNOWN. DEFECTIVE. GEA FAIL 2 AMBER CAS: DURING CRUISE AT FL400 AMBER CAS MESSAGES ENG CTRL FAULT L AND PRESSURIZATION FAULT ILLUMINATED WITH LOSS OF INDICATION FOR L EBGINE OIL P - [SDR DXTA2022101772240](https://openairdocs.org/sdr/DXTA2022101772240), Oct 16, 2022: FUSE. BLOWN. CABIN EMERG LIGHT: SEAT #3: READ LIGHT AND TOE KICK LIGHT ASSOCIATED WITH THE SEAT DO NOT ILLUMINATE WITH EMER LIGHTS SWITCH SELECTED TO ON. REMOVED AND REPLACE - [SDR DXTA2022090669690](https://openairdocs.org/sdr/DXTA2022090669690), Sep 5, 2022: NONE. NONE. FUEL IMBALANCE: BEFORE TAKEOFF, FUEL WAS BALANCED AT 4500 A SIDE. DURING TAKEOFF, RIGHT FUEL INDICATED AN INCREASE OF OVER 1000 POUNDS AND THE FUEL IMBALANCE CA - [SDR DXTA2022040759830](https://openairdocs.org/sdr/DXTA2022040759830), Apr 6, 2022: NONE. NONE. CABIN EMERG LIGHT: THE EXIT LIGHTS AND SEAT 10 TOE KICK LIGHTS WILL NOT EXTINGUISH WITH EMER LIGHTS SWITCH IN OFF POSITION. SUSPECT TRIPPED G SWITCH. // SIGNOFF - [SDR DXTA2022011355100](https://openairdocs.org/sdr/DXTA2022011355100), Jan 12, 2022: NOT REPORTED. NOT REPORTED. MAIN DOOR: MAIN DOOR HAS BEEN GETTING PROGRESSIVELY MORE DIFFICULT TO OPEN. IT IS STILL FUNCTIONAL BUT NEEDS EVALUATION FOR LUBRICATION AND/OR POSSIBLE ADJUSTME - [SDR DXTA2021080246170](https://openairdocs.org/sdr/DXTA2021080246170), Jul 31, 2021: BRAKE ASSY. DEFECTIVE. LEFT MLG BRAKE: LEFT INBOARD BRAKE HAS LEAKING FLUID AND BRAKE WAS SMOKING AT SHUT DOWN BRAKING WAS NOT AS GOOD AS USUAL. // SIGNOFF // CLEANED PRESSURIZED-AND ## Service difficulty reports on N622QS not matched to an aircraft (14) They name N622QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA2017070706424](https://openairdocs.org/sdr/DXTA2017070706424), Jul 7, 2017: COALESCER BAG. ODOR. CONDITIONED AIR HAS A STRONG MILDEW ODOR ESPECIALLY WHEN DEMANDING HEAT. CONDITIONED AIR THROUGH DUCT WORK DOES NOT HAVE A STRONG MILDEW ODOR. REMOVED WATER SEP - [SDR CWQR20160217005](https://openairdocs.org/sdr/CWQR20160217005), Feb 17, 2016: BRACKET. CRACKED. DURING A SCHEDULED INSPECTION WE FOUND THE AVIONICS SHELF BRACKET, PN 9256023-16, CRACKED MORE THAN HALF ITS LENGTH. REPLACED BRACKET & SENT SCR 745615 TO MFG. - [SDR CWQR20160106001](https://openairdocs.org/sdr/CWQR20160106001), Jan 6, 2016: ATTACH BRACKET. CRACKED. DURING SCHEDULED INSPECTION, FOUND THE RT FWD AVIONICS SHELF ATTACHED BRACKET CRACKED. REPLACED WITH NEW. - [SDR DXTA2015060506024](https://openairdocs.org/sdr/DXTA2015060506024), Jun 4, 2015: APU. LEAKING. DURING PREFLIGHT, WITH APU BLEED RUNNING, CABIN FILLED WITH BLUE SMOKE. FIRST OFFICER INDICATED CABIN WAS VERY HOT EVEN THOUGH TEMP SETTING WAS VERY LOW. REMOVE - [SDR DXTA2014041505731](https://openairdocs.org/sdr/DXTA2014041505731), Apr 14, 2014: ENGINE. LEAKING. DURING CLIMB OUT, HAD A CHEMICAL ODOR IN THE COCKPIT. RETURNED TO DEPARTURE. APU WAS OFF AFTER ENGINE START & NOT USED ON THE GROUND FOR BLEED AIR. THERE WAS NO - [SDR CWQR20110831016](https://openairdocs.org/sdr/CWQR20110831016), Aug 31, 2011: CONTROL CABLE. FRAYED. DURING A SCHEDULED INSPECTION FOUND ELEVATOR TRIM CABLE FRAYED AT LEAST HALF WAY THROUGH. THIS CABLE IS A PART OF A LARGER CABLE ASSY, PN 6660003-1. THIS CABLE - [SDR DXTA2011042504560](https://openairdocs.org/sdr/DXTA2011042504560), Apr 23, 2011: UNKNOWN. UNKNOWN. INTERMITTENTLY AFTER TAKEOFF AND GEAR RETRACTION, A VERY LOUD BANGING SOUND AND VIBRATION COMES FROM THE FWD RT SIDE OF ACFT. SLOW CYCLED GEAR. FOUND NOSE GEAR - [SDR DXTA2010102004268](https://openairdocs.org/sdr/DXTA2010102004268), Oct 19, 2010: TIRE. FAILED. NOSE TIRE BLEW OUT DURING LANDING. R & R NOSE WHEEL/TIRE ASSY IAW MM 32-41-01. - [SDR DXTA200702579](https://openairdocs.org/sdr/DXTA200702579), Oct 28, 2007: WINDSHIELD. FAILED. WHILE DESCENDING THROUGH 12000 FT AT 250 KTS, THE RT SIDE FORWARD COCKPIT WINDSHIELD SHATTERED AND THE RT W/S FAULT LIGHT ILLUMINATED. 30-60 SECONDS LATER, THE - [SDR DXTA200601670](https://openairdocs.org/sdr/DXTA200601670), Oct 18, 2006: ENGINE. MALFUNCTIONED. ON TAKEOFF ROLL, LEFT ENGINE ITT WENT STRAIGHT TO 780 (DEG)A/ INITIAL POWER UP. NO DELAY IN ABORTING. ABORTED LESS THAN 20 KNOTS AND TEMP WAS ONLY MOMENTARY. PE - [SDR DXTA200601286](https://openairdocs.org/sdr/DXTA200601286), Mar 10, 2006: BULB. BURNED OUT. RIGHT MAIN LANDING GEAR INDICATOR LIGHT WOULD NOT ILLUMINATE AFTER LOWERING THE GEAR. USING THE ABNORMAL CHECKLIST MANUALLY (BLEWDOWN) THE GEAR. SEVERAL MINUTES - [SDR DXTA200501073](https://openairdocs.org/sdr/DXTA200501073), Nov 10, 2005: GROUND STUD. DAMAGED. INFLIGHT UNLOCK LIGHT ILLUMINATED WITH 3 GREEN LIGHTS LEFT, GEAR WAS FLICKERING ON/OFF. ACCOMPLISHED CHECK LIST AND BLEW GEAR DOWN. T/S TO BAD GROUND ON LEFT MA - [SDR DXTA200400311](https://openairdocs.org/sdr/DXTA200400311), May 11, 2004: BRAKE. FIRE. PERFORMED HIGH SPEED TAXI AFTER BRAKE MAINTENANCE, TAXIED BACK USING NORMAL BRAKING PROCEDURE. UPON RETURN TO RAMP, LEFT WHEEL/BRAKE ASSEMBLY WAS ON FIRE, RIGHT - [SDR DXTA200300198](https://openairdocs.org/sdr/DXTA200300198), Dec 14, 2003: WARNING LIGHT. ILLUMINATED. AFTER TAKEOFF OUT OF IAD FOR BCT, WITH GEAR HANDLE SELECTED UP GOT GEAR UNLOCKED WARNING LIGHT BUT GEAR STAYED DOWN. ACCOMPLISHED AIR TURNBACK TO IAD AND LANDED ## 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.