- Owner type
- Co-owned, fractional ownership
- Serial number
- 680A0229
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 2, 2019
- Certificate issued
- May 8, 2026
- Expires
- May 31, 2033
- Mode S code
- A94626
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 3
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2018 | 1 |
|---|---|
| 2023 | 1 |
| 2026 | 1 |
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N697QSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Textron 680A aircraft
FAA incident reports
No FAA accident or incident reports matched to N697QSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Textron 680A aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026100510014Elec Connector · disconnectedRT VANITY SEAT LIGHT INOP. TESTED WITH EMER LIGHTS ON ARMED AND WITH SHIPS BATTERIES. PERFORMED OPS CHECK OF RT VANITY SEAT LIGHT WAS ABLE TO DUPLICATED SQUAWK. GAINED ACCESS TO LIGHT ASSY FOUND BOTH LIGHT ASSY ABOVE VANITY SEAT ELECTRICAL PLUG NOT INSTALLEDSDR DXTA2026052908250Pressure Switch · faultedSELECTED FUEL CROSSFEED L TANK TO R ENGINE INFLIGHT AND RECIEVED FUEL PRES LOW L CAS AS WELL AS AN AMBER FUEL BST PUMP ON L. RAN QRH AND FUEL BST PUMP L MESSAGE REMAINED AMBER. REMOVED LH SUSPECTED DEFECTIVE FUEL PRESSURE SWITCH P/N:9914488-2, S/N:2423753 ANSDR DXTA2025110705572Battery Pack · defectiveUPON SHUTDOWN, ONE OF US NOTICED THAT THE EMER LIGHTS WERE ALL OFF BEFORE THE OTHER ONE TURNED OFF THE SWITCH. UPON TROUBLESHOOTING, IT SEEMS THAT THE EMER LIGHTS DO NOT ILLUMINATE WITH THE MAIN BATTERIES TURNED OFF, AND THE EMER LIGHT SWITCH IN THE ARM POSITISDR DXTA2025030602563Engine · bird ingestionWE FELT AND HEARD A VERY NOTICABLE "CLUNK" AT 200' AGL ON APPROACH. DURING POSTFLIGHT, FOUND EVIDENCE OF BIRD STRIKE ON RIGHT WING LEADING EDGE DIRECTLY IN FRONT OF ENGINE. LARGE BLOOD SPATTERS ON UNDERSIDE OF COWLING, AND BLOOD SCATTERED ON SPINNER AND INSIDESDR 2025F00044Skin · debondedDISBOND AND CONTOUR DEVIATIONS, LH AND RH WING, UPPER SKIN BOND ASSEMBLIES, STRINGER ENDS. ACCOMPLISHED FR-680A-0229-14754 REV - DATED 2-13-2025 AND FAA FORM 8110-3 DATED 02/13/2025; FIELD REPAIR - DISBOND AND CONTOUR DEVIATIONS, WING, UPPER SKIN BOND ASSEMBLISDR DXTA2024021510905Wire · looseDURING PREFLIGHT INSPECTION FOUND LAV EMERGENCY FLOOR FLOOD LIGHT INOP AND LOSE WIRE IN PROXIMITY. RECONNECTED THE CONNECTOR AT THE TOE KICK OF THE RIGHT LAV SEAT AND OPS CHECKED GOOD REF CE 680A AMM 33-50-00SDR 2022F00064None · chippedLH INBOARD AXLE PLATING DAMAGE. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ33428M1 DATED: FEBRUARY 3, 2022, LEFT MAIN LANDING GEAR AXLE PLATING DAMAGE (CHIPPED).SDR DXTA2021122754290None · noneMAIN DOOR: MAIN CABIN DOOR BINDS SLIGHTLY AT TOP OF TRAVEL. NEEDS SMALL PUSH TO OPEN FROM INSIDE AIRCRAFT. // SIGNOFF// FOUND MED RUBBING AGAINST THE FORWARD RUB BLOCK. ADJUSTED THE FORWARD THE FORWARD RUB BLOCK IAW CESSNA 680A AMM CH 52-10-00 OPS CHECK IS GOSDR DXTA2021091448810Oil System · leakingCABIN SMOKE: WHILE ON GROUND WITH APU ON, A FINE MIST WITH AN ODOR OF ENGINE OIL BEGAN TO APPEAR & THICKENED UNTIL BLEED AIR TURNED OFF.
COMPLIED WITH TC-68A-21-181006M ENVIRON CONTROL SYS BLEED DUCT BURN PROCEDURE & NOTED SMOKE WHILE DOING PROCEDURE. FOUSDR DXTA2021031539370Wire · disconnectedMAIN DOOR: MAIN CABIN ENTRY DOOR WOULD NOT OPEN AFTER LANDING. DOOR LEVER WOULD NOT DISENGAGE AFTER PRESSING RED HANDLE RELEASE BUTTON. TURNING OFF APU HAD NO EFFECT. MED WAS OPENED BY GROUND PERSONNEL BEING INSTRUCTED VIA TELEPHONE USING NORMAL DOOR OPENING PSDR DXTA2021021504737Switch · malfunctionedMAIN EXIT SIGN/LIGHT: EXIT SIGN OVER MAIN ENTRY DOOR WILL NOT EXTINGUISH WITH EMERGENCY LIGHT SWITCH SELECTED OFF. RESET #1 INERTIA SWITCH AND EXTINGUISHED EXIT SIGN OVER MAIN ENTRY DOOR. IAW 680A AMM 33-50-00.
Reports on N697QS not matched to an aircraft · 18
They name N697QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2015082806068Pressure Switch · unserviceableBRAKE PUMP FAILED, CREW USED THE EMER BRAKING SYS DURING TAXI IN. ANTISKID LIGHT CAME ON IN FLIGHT , ALSO POWER BRAKE C/B POPPED. AS PER THE CHECKLIST PWR/BRKS C/B WAS RESET BEFORE LANDING AND THE C/B POPPED AGAIN. THE LANDING WAS UNEVENTFUL AND AFTER WE CONTSDR DXTA2014120805943Apu · contaminatedSMOKE FILLED COCKPIT & CABIN AFTER ACTIVATION OF BLEED AIR ON APU. BORESCOPED APU INLET AREA AND IMPELLER. HEAVY AMOUNTS OF OIL THROUGHOUT THE AREA. REMOVED APU IAW MM 498-10-00 AND DRAINED OIL. CLEANED OUT APU CONTAINMENT BOX AS REQUIRED. INSTALLED THE APUSDR DXTR20130717002Bracket · crackedLEFT ACM BRACKET CRACKED AT RUDDER BIAS CONTROL VALVE. R & R LT ACM BRACKET REF SRM 51-40-03.
See all 18 unmatched reportsSTCs that may be installed · 16
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Textron 680A
STC ST04765NYUnprepared (Grass/Sod) Runway OperationsSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST12344IBReplacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher