- Owner type
- Co-owned, fractional ownership
- Serial number
- 680A0072
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 7, 2017
- Certificate issued
- July 23, 2026
- Expires
- July 31, 2033
- Mode S code
- A6B1DC
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 N530QSMatched 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 N530QSMatched 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 · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2024121601497Warning Message · false activationFLAPS FAIL AMBER CAS AT FL430 WITH FLAPS INDICATING UP AND FLAP HANDLE IN DETENT. FLAP INDICATOR TURNED AMBER. FLAP RESET BUTTON ILLUMINATED, BUT HAD NO EFFECT. FLAP FAIL LANDING ENSUED. INSPECTED FLAPS, FLAP ACTUATORS, FLAX SHAFTS AND FLAP TRACKS IAW AMM SDR DXTA2024021410892Battery · dischargedDURING POWER ON CHECKLIST EMER LTS DO NOT ILLUMINATE WHILE IN THE ARM POSITION. POWERED UP A/C AND EMER LIGHTS OPS CHECKS GOOD. POWERED UP APU AND CHARGED BATTERIES AS REQUIRED. LIGHTS OPS CHECKS GOOD. WORK DONE IN REF CE680A MM 33-50-00. BATTERIES TOOK EXTRASDR DXTA2023041884500Unknown · unknownENG CNTRL FAULT R AMBER CAS: ENG CTRL FAULT R AMBER CAS MESSAGE DISPLAYED AFTER TAKEOFF. FOLLOWED THE CHECKLIST AND MESSAGE REMAINED. LANDED AS SOON AS PRACTICAL. ACCESED AIRCRAFT AND PERFORMED ENG RUNS. CYCLED T/R'S MULTIPLE TIMES IAW CE680A MM 78-30-00. SDR DXTA2022101271940Harness · brokenMAIN DOOR: MAIN DOOR WILL NOT LOCK. DOOR WILL CYCLE INTO CLOSED POSITION BUT SOLIENOID WILL NOT CYCLE TO LOCK DOOR. REMOVED CHAFFED DOOR THRESHOLD HARNESS AND INST.AILED NEW HARNESS, WNPLETED OPS CHECKS WITH NO DEFECTS NOTED. ALL WORK AANMPLISHE IAW CE680A SDR DXTA2022101171940Door · unknownMAIN DOOR: MAIN DOOR WILL NOT LOCK. DOOR WILL CYCLE INTO CLOSED POSITION BUT SOLIENOID WILL NOT CYCLE TO LOCK DOOR.SDR 2022FA0000331Lug · damagedMAIN CABIN DOOR FORWARD FRAME P/N 7411305-37 LUG DAMAGED.SDR DXTA2022010354640Charger · noneEMERGENCY LIGHTS (FLOOR ILLUMINATION) UNDER SEATS 5 & 8 INOP WHEN CHECKING EMERGENCY LIGHTS. *** CORRECTIVE ACTION *** ALLOWED EMERGENCY BATTERY PACKS TO CHARGE AND ATTEMPTED OPS CHECK THE EMERGENCY LIGHTS AND AGAIN SEATS 5, 8, AND OVERWING EMERGENCY LIGHT WOUSDR 2020F00436Frame · crackedSR-680A-ATA53-25890 MAJOR REPAIR, CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL, FRAME , WEB AND DOUBLERS FS 75.SDR 2020F00434Support Frame · crackedNOSE LANDING GEAR WHEEL WELL FRAME CRACKS.SDR 2020F00257Skin · corrodedREPAIR OF HORIZONTAL STABILIZER LEFT LOWER SKIN DAMAGE (CORROSION). TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ25592M1 DATED APRIL 29, 2020.SDR DXTA2019122323239Software · malfunctionedCABIN ALTITUDE RED CAS ILLUMINATED, ENROUTE AT FLIGHT LEVEL 410. THE PRESSURIZATION FAULT CAS MESSAGE CAME ON. CHECKLIST HAD US GO TO MANUAL THEN AUTO AGAIN. FAULT LIGHT WENT OUT THEN IMMEDIATELY CAME BACK ON. WENT BACK TO MANUAL AND CABIN WAS CLIMBING RAPISDR DXTR2019073001Skin · chafedWING ANTI-ICE CROSS FLOW VALVE IS CHAFFING ON FUSELAGE LOWER SKIN. BLENDED OUT DAMAGE TO PREPARE FOR NDT. NO CRACKS NOTED. COMPLETED STANDARD REPAIR SR-680A-ATA53-22175.SDR DXTA2019062412523Circuit Board · malfunctionedENGINE FIRE R RED CAS INTERMITTENT - DESCENDING THROUGH 7000FT, RED ENGINE FIRE R CAS ILLUMINATED FOR ABOUT 1 SECOND WITH ASSOCIATED AUREL MESSAGE RECOMMEND SWAPPING THE NC208 AND NC108 PCB'S. GAINED ACCESS TO PCB'S AND, REMOVED THE LJH PCB P/N: 6918632-12, SSDR DXTA201709180001Switch · inoperativeDURING CRUISE AT FL 400, RECEIVED AN AMBER CAS MESSAGE FOR FUEL FILTER BYPASS RT. COMPLIED WITH QRH AND DIVERTED. DID NOT EXPERIENCE ANY ENGINE SURGING OR OTHER ANOMALIES. REMOVED AND REPLACED FUEL IMPEDING BYPASS DIFFERENTIAL SWITCH IAW MM 73-10-03.
Reports on N530QS not matched to an aircraft · 2
They name N530QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 98ZZZX4648Line · brokenPILOT'S DISCREPANCY WAS NR 1 ENIGNE IS TEMP LIMITED ABOVE CRUISE DETENT. REMOVED THE OUTER AND INNER BYPASS ACCESS TO CHECK BLEED VALVES. UPON INVESTIGATION, FOUND THE BLEED AIR (P3 LINE) BROKEN AT B-NUT, P/N 3081695. IT APPEARED THE FIT OF THE LINE HAD CAUSDR 98ZZZX4206P3 Line · brokePILOTS DISCREPANCY WAS NR 1 ENGINE TEMPORARILY LIMITED ABOVE CRUISE DETENT. REMOVED THE OUTBOARD INNER BYPASS ACCESS TO CHECK BLEED VALVES. UPON INVESTIGATION, FOUND THE BLEED AIR (P3 LINE) BROKEN AT B-NUT, P/N 3081695. IT APPEARED THE FIT OF THE LINE HAD C
STCs 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