# N630QS: 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: 680A0179
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 7, 2019
- Certificate issued: September 30, 2025
- Expires: September 30, 2032
- Mode S code: A83F2B
- Owner type: Co-owned
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=630QS
- Page: https://openairdocs.org/aircraft/N630QS

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 N630QS.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20230824008859I](https://openairdocs.org/incident/20230824008859I), Aug 24, 2023: Textron Aviation Inc 680A (N630QS), Atlanta, GA, Minor damage. On August 24, 2023, at approximately 1644 LCL while on approach to kpdk airport, Atlanta, GA, at 4,000', hit a large bird. Aircraft continued to a safe landing…

## Reports on N630QS not matched to an aircraft (1)

They name N630QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20120604010149I](https://openairdocs.org/incident/20120604010149I), Jun 4, 2012: Cessna 560XL (N630QS), Teterboro, NJ, Minor damage. Upon landing on runway 6, the right main gear tire failed and disintegrated. Aircraft taxied off runway to taxiway r and awaited for ground personnel to tow…

## Service difficulty reports (28)

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 DXTA2026090809551](https://openairdocs.org/sdr/DXTA2026090809551), Sep 3, 2026: BRAKE. ABNORMAL. BRAKE SHUTTER DURING LOW SPEED TAXI IN TO A FULL STOP. SOUNDS MORE PROMINENT ON RIGHT SIDE, BUT CAN FEEL IT IN BOTH PEDALS. VISUALLY INSPECTED BRAKES. NO DEFECT
- [SDR DXTA2026081009188](https://openairdocs.org/sdr/DXTA2026081009188), Aug 7, 2026: DOOR SEAL. DAMAGED. DURING DESCENT, A LOUD PRESSURIZATION SQUEAL OCCURS STARTING AT 2.6 PSID AND CONTINUES UNTIL PRESSURE FALLS BELOW 2.2 PSID. REMOVED DAMAGED CABIN DOOR SEAL AND 
- [SDR DXTA2026052608214](https://openairdocs.org/sdr/DXTA2026052608214), May 24, 2026: PRESSURE SWITCH. FAULTY. AT CRUISE ALTITUDE FL410 ATTEMPTED TO CROSSFEED L TANK TO R ENG IMMEDIATLEY RECEIVED AMBER FUEL BST PUMP ON L R RAN QRH MESSAGE REMAINED BUT TURNED WHITE AS QRH
- [SDR DXTA2025022602506](https://openairdocs.org/sdr/DXTA2025022602506), Feb 25, 2025: DOOR. BINDING. MAIN DOOR: MAIN DOOR BINDING. WHEN RELEASED FROM THE INTERIOR OR EXTERIOR DOOR REQUIRES EXCESSIVE PUSH PULL TO CLEAR THE TOP OF THE DOOR FRAME BEFORE IT WILL FA
- [SDR DXTA2024111101090](https://openairdocs.org/sdr/DXTA2024111101090), Nov 8, 2024: DOOR. OUT OF RIG. MAIN DOOR: REPEAT WRITEUP. MAIN CABIN DOOR STICKS AND REQUIRES FORCE TO OPEN. CORRECTIVE ACTION; ADJUSTED MAIN CABIN DOOR RIGGING IAW CE680A AMM 52-10-00. OPS C
- [SDR DXTA2024110801068](https://openairdocs.org/sdr/DXTA2024110801068), Nov 5, 2024: DOOR. BINDING. MAIN DOOR: MAIN CABIN DOOR DOES NOT OPEN ON IT'S OWN AS NORMAL. THE DOOR SEEMS TO BE BINDING ON THE FORWARD SIDE AND NEEDS TO BE PUSHED TO GET IT TO OPEN. CORRE
- [SDR DXTA202401100786](https://openairdocs.org/sdr/DXTA202401100786), Oct 7, 2024: STEERING SYS. DEFECTIVE. GEAR DISAGREE N AMBER CAS: AFTER TAKEOFF THE NOSE GEAR DID NOT RETRACT. THE MAIN GEAR CAME UP AND INDICATED UP. THE QRH DIRECTED THE HANDLE TO BE PLACED IN THE 
- [SDR DXTA2024051311746](https://openairdocs.org/sdr/DXTA2024051311746), May 11, 2024: DOOR. SLOW. MAIN CABIN DOOR SLOW TO OPEN. FROM OUTSIDE PULL DOOR HANDLE AND THE DOOR DID NOT OPEN IMMEDIATELY. IT CRACKED OPEN THEN HAD TO PULL WITH HAND AND THE DOOR CAME 
- [SDR DXTA2023100597270](https://openairdocs.org/sdr/DXTA2023100597270), Oct 4, 2023: UNKNOWN. UNKNOWN. THE PRIMARY DOOR HAS BEEN STICKING THE PAST FEW USES, AND TODAY IT HAS BEEN STICKING IN THE FULLY CLOSED/UP POSITION NEEDING A PHYSICAL PUSH OR PULL TO OPEN THE
- [SDR DXTA2023071791140](https://openairdocs.org/sdr/DXTA2023071791140), Jul 17, 2023: MOTOR. DEFECTIVE. MAIN DOOR: UPON ARRIVAL AT AIRCRAFT MAIN CABIN DOOR DID NOT FREE FALL OPEN. DIFFICULT TO OPEN. STARTED APU AND DOOR WASN'T AS DIFFICULT BUT STILL REQUIRED SMALL
- [SDR DXTA2023052687110](https://openairdocs.org/sdr/DXTA2023052687110), May 25, 2023: UNKNOWN. UNKNOWN. AFTER TAKEOFF, THE NOSE GEAR DID NOT RETRACT. NOSE FEAR RETRACTED AFTER 2D ATTEMPT. UPON LANDING, NOSE GEAR WHEEL WELL WAS INSPECTED AND EVERYTHING LOOKED NORMA
- [SDR 2023F00084](https://openairdocs.org/sdr/2023F00084), Mar 17, 2023: SKIN. UNKNOWN. STINGER SKIN OVERSIZED HOLES. ACCOMPLISHED TEXTRON AVIATION REPAIR LETTER DQ38629M1 DATED MARCH 14, 2023 "680A-0179 STINGER SKIN OVERSIZED HOLE"
- [SDR 2023FA0000146](https://openairdocs.org/sdr/2023FA0000146), Mar 17, 2023: FAIRING. CRACKED. LH WIPER FARING CRACK. ACCOMPLISHED TEXTRON AVIATION REPAIR LETTER DQ38608M1 DATED MARCH 14, 2023 "680A-0179 LH WIPER FARING CRACK. "
- [SDR DXTA2023022781250](https://openairdocs.org/sdr/DXTA2023022781250), Feb 27, 2023: NONE. NONE. EMERGENCY LIGHTS BATTERY: EMERGENCY EXIT LIGHT AT MAIN CABIN DOOR STAYS ON. APPEARS G SWITCH WAS TRIPPED.//CORRECTIVE ACTION// RESET THE #1 EMERGENCY LIGHT INTE
- [SDR DXTA2023021580500](https://openairdocs.org/sdr/DXTA2023021580500), Feb 14, 2023: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: WITH THE EMER LIGHT SWITCH IN THE OFF POSITION, THE EXIT LIGHT AND THE TWO EXITS SIGNS AROUND THE MAIN CABIN DOOR, AS WELL AS THE LIGHT UNDER
- [SDR DXTA2022122376950](https://openairdocs.org/sdr/DXTA2022122376950), Dec 23, 2022: BATTERY PACK. DEFECTIVE. EMERG EXIT SIGN/LIGHT: ZONE 1 EMER LIGHTS REMAIN ON AFTER SWITCHED OFF. REMOVED AND REPLACED THE #1 FWD EMERGENCY LIGHT BATTERY PACK. RESET THE FWD EMERGENCY LI
- [SDR 2022FA0000643](https://openairdocs.org/sdr/2022FA0000643), Oct 24, 2022: NONE. NONE. CORROSION ON THRUST REVERSER ATTACH FLANGE. NORDAM FIELD ENGINEERING DISPOSITION LETTER DOCUMENT NUMBER NTRSD-22TP-283 DATED OCTOBER 21, 2022. THRUST REVERSER C
- [SDR 2022F00411](https://openairdocs.org/sdr/2022F00411), Oct 24, 2022: NONE. NONE. CORROSION ON THRUST REVERSER ATTACH FLANGE. NORDAM FIELD ENGINEERING DISPOSITION LETTER DOCUMENT NUMBER NTRSD-22TP-282 DATED OCTOBER 21, 2022. THRUST REVERSER C
- [SDR DXTA2022092671140](https://openairdocs.org/sdr/DXTA2022092671140), Sep 26, 2022: NONE. NONE. EMERG LIGHT SWITCH: WITH BATTERIES CONNNECTED AND BATT SWITCHES OFF, EMER LIGHTS WERE NOT OPERATIONAL WITH THE EMER LTS SWITCH IN THE ARM POSITION. // SIGNOFF//
- [SDR DXTA2022061964100](https://openairdocs.org/sdr/DXTA2022061964100), Jun 17, 2022: PUSHROD. DEFECTIVE. MAIN DOOR HANDLE: MAIN CABIN DOOR HANDLE WILL NOT MOVE AFTER MOTOR CLOSES DOOR. DOOR STUCK IN OPEN POSITION.//CORRECTIVE ACTION//REMOVED AND REPLACED PUSHROD. D
- [SDR DXTA2022060663250](https://openairdocs.org/sdr/DXTA2022060663250), Jun 3, 2022: PIN. BINDING. MAIN DOOR: DOOR HANDLE CANNOT BE CLOSED. THE MIDDLE FORWARD LOCKING PIN IS NOT ALIGNED WITH THE GUIDE HOLE. REPEAT WRITE-UP. // SIGNOFF// CABIN DOOR LATCH/LOCK 
- [SDR DXTA2022053163000](https://openairdocs.org/sdr/DXTA2022053163000), May 31, 2022: PIN. OUT OF ALIGNMENT. MAIN DOOR: DOOR HANDLE CANNOT BE CLOSED. THE MIDDLE FORWARD LOCKING PIN IS NOT ALIGNED WITH THE GUIDE HOLE. DOOR OPERATING MECHANISM ADJUSTED AND TESTED IAW AMM
- [SDR DXTA2022040459510](https://openairdocs.org/sdr/DXTA2022040459510), Apr 1, 2022: NONE. NONE. MAIN DOOR: MAIN CABIN DOOR WILL NOT LATCH. HANDLE STUCK IN THE OPEN POSITION // SIGNOFF// REMOVED TRIM AND STAIRS FROM THE MAIN ENTRANCE DOOR TO GAIN ACCESS TO 
- [SDR DXTA2021122754150](https://openairdocs.org/sdr/DXTA2021122754150), Dec 25, 2021: APU. DAMAGED. COCKPIT SMOKE: AFTER SHUTDOWN AND APU AIR APPLIED COCKPIT AND CABIN FILLED WITH SMOKE // SIGNOFF// REPLACED APU WITH RENTAL APU IN ACCORDANCE WITH 680A MM CH 49
- [SDR DXTA2021070644750](https://openairdocs.org/sdr/DXTA2021070644750), Jul 5, 2021: DOOR. BINDING. MAIN DOOR: WHEN ATTEMPTING TO CLOSE THE MAIN CABIN DOOR, THE LIFT BUTTON INSIDE THE ACFT WAS PUSHED AND HELD UNTIL THE DOOR CLOSED TIGHT INTO FUSELAGE; HOWEVER,
- [SDR DXTA2020120404430](https://openairdocs.org/sdr/DXTA2020120404430), Dec 3, 2020: TRIM SYSTEM. OUT OF RIG. EXCESSIVE BACK PRESSURE NEEDED FOR ROTATION. THE HORIZONTAL STAB INDICATIONS SEEMS TO NOT MATCH COCKPIT INDICATIONS. ALL OTHER FLIGHT CONDITIONS ARE NORMAL AND 
- [SDR DXTA2020100304162](https://openairdocs.org/sdr/DXTA2020100304162), Oct 3, 2020: DOOR. BINDING. WHEN OPENING THE MAIN CABIN DOOR THE DOOR TEMPORARILY HANGS UP BEFORE FALLING TO THE FULL OPEN POSITION. SEEMS TO BE RUBBING ON THE BLACK GUILD BLOCK ON THE INS
- [SDR DXTA2020081703981](https://openairdocs.org/sdr/DXTA2020081703981), Aug 14, 2020: PIN. BINDING. AFTER CLOSING THE MAIN CABIN DOOR THE DOOR LATCHING HANDLE WILL NOT MOVE TO THE CLOSED POSITION. RAN THE QRH WHILE PUSHING THE DOOL LIFT CANCEL BUTTON, WE NEVER

## Service difficulty reports on N630QS not matched to an aircraft (26)

They name N630QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2014121605949](https://openairdocs.org/sdr/DXTA2014121605949), Dec 15, 2014: MOTOR. FAILED. MAIN BRAKE SYS FAILED WITH LOW BRAKE PRESSURE & ANTI-SKID INOPERATIVE LIGHTS ON LANDING. POWERED ACFT UP, AND RAN THE BRAKE SYSTEM SEVERAL TIMES AND COULD NOT F
- [SDR EBVR20140923002](https://openairdocs.org/sdr/EBVR20140923002), Sep 23, 2014: FITTING. CRACKED. FOUND 2 HORIZONTAL STAB PIVOT FITTING ASSEMBLY CRACKED PN 6631102-15 DURING OUR INSPECTION. MECHANICS NEED TO PAY CLOSE ATTENTION TO THIS AREA WHILE DOING INSPE
- [SDR 2014FA0000483](https://openairdocs.org/sdr/2014FA0000483), Aug 18, 2014: FITTING. CRACKED. FOUND A CRACKED HORIZONTAL STAB PIVOT BOLT FITTING ASSY. WHICH WAS POSSIBLY CAUSED BY IMPROPER INSTALLATION OF THE LOWER SUPPORT CLIP. UPON REMOVING THE LOWER S
- [SDR DXTA2014033005702](https://openairdocs.org/sdr/DXTA2014033005702), Mar 27, 2014: WIRE. CHAFED. DURING ROUTINE COCKPIT INSPECTION WITH MAIN BATTERY ON, AILERON TRIM BOUND DURING CHECK, AUTOPILOT SERVO CIRCUIT BREAKER TRIPPED & SMOKE WAS DETECTED. TRIM KNOB
- [SDR DXTA2012060504989](https://openairdocs.org/sdr/DXTA2012060504989), Jun 4, 2012: TIRE. FAILED. RT MAIN TIRE TREAD SEPARATED FROM TIRE ON LANDING ROLLOUT. R & R RT MLG WHEEL & TIRE ASSY IAW MM 32-41-02.
- [SDR DXTA2012021004867](https://openairdocs.org/sdr/DXTA2012021004867), Feb 9, 2012: CONTROL HANDLE. MALFUNCTIONED. GEAR WOULD NOT RETRACK WHEN GEAR HANDLE WAS PULLED UP, HAD ALL 3 GREEN INDICATORS, GROUND CONFIRMED GEAR WERE WAS DOWN AND EMERGENCY WAS NOT DECLARED. HANDLE WA
- [SDR DXTA2011111404784](https://openairdocs.org/sdr/DXTA2011111404784), Nov 11, 2011: TRIM SYSTEM. FROZEN. ELEVATOR TRIM STUCK. FROZE UP INFLIGHT. IT WOULD NOT OPERATE ELECTRICALLY OR MANUALLY. IT COULD NOT BE MOVED ANY AT ALL MANUALLY. IT CREATED POSITIVE FORWARD FO
- [SDR CWQR2001101824](https://openairdocs.org/sdr/CWQR2001101824), Oct 18, 2011: ANGLE. CRACKED. DURING A SCHEDULED MX CHECK, ANGLE WAS FOUND CRACKED THROUGH THE FREE FLOATING LEG INTO THE ANGLE RADIUS, THIS CRACK WAS 4.2 INCHES FROM THE END OF THE PART. TH
- [SDR DXTA2011080104675](https://openairdocs.org/sdr/DXTA2011080104675), Jul 31, 2011: AHRS. MALFUNCTIONED. LEFT PFD: "HEADING FAILURE - SINGLE" AT ALTITUDE. R & R LT AHRS COMPUTER. OPS CHECKED GOOD. WORK DONE IAW MM 34-21-01.
- [SDR DXTA2010062504131](https://openairdocs.org/sdr/DXTA2010062504131), Jun 24, 2010: WIRE HARNESS. FAULTY. LEFT ENGINE ITT SPIKED TO 800° IN FLIGHT. TRIED TO CONTROL TEMP WITH THROTTLE, BUT WHEN WE DESCENDED TO 5000', ITT EXCEEDED 760°. SHUTDOWN ENGINE, BUT ITT NEVER
- [SDR DXTA2010052504101](https://openairdocs.org/sdr/DXTA2010052504101), May 24, 2010: BULB. INOPERATIVE. AFTER LANDING GEAR EXTENSION, GREEN NLG LIGHTS FAILED TO ILLUMINATE. COMPLIED WITH THE LANDING GEAR WILL NOT EXTEND CHECKLIST. LANDING WAS NORMAL. AFTER LANDING
- [SDR DXTA2010050304084](https://openairdocs.org/sdr/DXTA2010050304084), May 2, 2010: EEC. MALFUNCTIONED. CLIMBING THROUGH FL280 HAD PARTIAL LOSS OF POWER ON THE RT ENGINE, POWER LEVERS IN CLIMB. MAX POWER WAS 64.5 % WITH FUEL FLOW OF 360. LT ENG APPROX 85 % & FUEL 
- [SDR DXTA2009101903815](https://openairdocs.org/sdr/DXTA2009101903815), Oct 18, 2009: BLEED VALVE. INOPERATIVE. RT ENGINE FAILED TO ATTAIN T/O N1 POWER. AFTER MULIPLE ATTEMTS AND AN A/C "RESET" THE BEST N1 ATTITUDE WAS 68%, N1 WITH 100% N2 INDICATED. ON FINAL ATTEMT A COM
- [SDR DXTA2009031603550](https://openairdocs.org/sdr/DXTA2009031603550), Mar 13, 2009: ACM. SMOKE. WHEN APU BLEED AIR IS SELECTED CABIN AND COCKPIT AREA BEGINS TO FILL WITH BLUE SMOKE. REMOVED ACM DUCTING & SEALS, R&R ACM. BEGAN INSTALLATION OF OVERHAULED ACM
- [SDR DXTA2009030503529](https://openairdocs.org/sdr/DXTA2009030503529), Mar 5, 2009: OIL SYSTEM. LEAKING. BORESCOPED EXHAUST AND INLET OF APU. FOUND OIL IN INLET. REMOVED AND REPLACED APU AND ECU IAW MM CH 49-10-00 LEAK AND FUNCTIONAL CHECKED GOOD.
- [SDR DXTA2009030603529](https://openairdocs.org/sdr/DXTA2009030603529), Mar 5, 2009: ECU. LEAKING. AFTER TURNING ON APU BLEED AIR, EXCESSIVE FUMES AND ODOR ENTERED THE CABIN. REMOVED AND REPLACED APU AND ECU IAW MM CH 49-10-00 LEAK AND FUNCTIONAL CHECKED GOOD
- [SDR DXTA2008122403434](https://openairdocs.org/sdr/DXTA2008122403434), Dec 24, 2008: ELEVATOR SYSTEM. STIFF. ELEVATOR CONTROL FEELS STIFF.
- [SDR DXTA2008122303434](https://openairdocs.org/sdr/DXTA2008122303434), Dec 23, 2008: CONTROL CABLE. LOOSE. DURING CLIMB THROUGH 12,000 FT AT 200 KIAS, AUTO PILOT OFF, ELEVATOR CONTROL FELT STIFF FROM LT SEAT. AN ABNORMAL BUMP COULD BE FELT WHEN MOVING YOKE FORE AND A
- [SDR DXTA200811143357](https://openairdocs.org/sdr/DXTA200811143357), Nov 14, 2008: ACTUATOR. INOPERATIVE. GEAR UNLOCK HYD PRESS AND STAB MISCOMPARE LTS ALL REMAINED ILLUMINATED AFTER GEAR AND FLAP RETRACTION. ALL LIGHTS REMAINED ILLUMINATED UNTIL GEAR / FLAPS WERE P
- [SDR DXTA2008111703357](https://openairdocs.org/sdr/DXTA2008111703357), Nov 14, 2008: WARNING SYSTEM. ACTIVATED. GEAR UNLOCK HYD PRESS REMAINED ILLUMINATED AFTER GEAR AND FLAP RETRACTION.
- [SDR DXTA2008102903326](https://openairdocs.org/sdr/DXTA2008102903326), Oct 28, 2008: RELIEF VALVE. FAULTED. GEAR "UNLOCK" LIGHT, "HYD PRES" LIGHT, AND "STAB MISCOMPARE" LIGHT ALL ILLUMINATED AFTER TAKEOFF. THEY REMAINED ILLUMINATED WHILE RUNNING THE CHECKLIST AND DID 
- [SDR DXTA200702558](https://openairdocs.org/sdr/DXTA200702558), Oct 21, 2007: BRAKE ASSY. MALFUNCTIONED. THE TOE BRAKES ON RT PEDAL GOES TO THE FLOOR. PERFORMED BRAKE BLEED IAW AMM 32-42-01. OPS CHECK GOOD.
- [SDR DXTA200601772](https://openairdocs.org/sdr/DXTA200601772), Dec 1, 2006: DUCT. SEPARATED. WHILE ACCELERATING IN CRUISE FLIGHT FL280 HEARD A THUMP SOUND ACCOMPANIED BY AN INCREASED SLIP STREAM NOISE AND A SLIGHT VIBRATION ON THE CONTROL YOKE. DECREASE
- [SDR DXTA200500951](https://openairdocs.org/sdr/DXTA200500951), Sep 2, 2005: ACM. SEIZED. APU RUNNING ON THE GROUND WITH BLEED AIR ON. SMOKE IN CABIN AND COCKPIT SHUTDOWN BLEED AIR AND APU REMOVED BATTERY POWER FROM AIRCRAFT. ACM WAS FOUND SEIZED UP,
- [SDR DXTA200300189](https://openairdocs.org/sdr/DXTA200300189), Nov 27, 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 DXTA200300044](https://openairdocs.org/sdr/DXTA200300044), Jun 9, 2003: RELAY. INOPERATIVE. LOST BRAKES ON LANDING ROLLOUT. USED EMERGENCY BRAKES TO STOP ACFT. POWER BRAKES AND ANTI SKID ANNUNCIATORS DID COME ON WHEN ACFT LOST BRAKES. POST FLIGHT REVEA

## 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

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