- Serial number
- 525B0270
- Year built
- 2008
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- September 16, 2008
- Certificate issued
- December 28, 2021
- Expires
- December 31, 2028
- Mode S code
- A9CBE4
- Registered owner
- Gold Canyon Aviation LLC
- Location
- Richmond, MO
- Owner type
- LLC
From the FAA registry file of October 20, 2026.
On this page
Airworthiness directives that may apply · 11
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment. Not a compliance determination.
| 1998 | 1 |
|---|---|
| 2005 | 1 |
| 2007 | 1 |
| 2008 | 1 |
| 2014 | 1 |
| 2019 | 2 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
| 2026 | 1 |
Airframe · Cessna 525B
AD 2026-03-06Vertical Stabilizer Structure, Nacelle/Pylon, Attach FittingsAD 2024-15-09Gust Lock/Damper SystemAD 2023-10-02Indicating/Recording System, NavigationAD 2021-05-17NAVIGATION SYSTEMAD 2020-24-06Flight ControlsAD 2014-18-01NavigationAD 2008-03-10Lower wing skin structureAD 2007-23-16Electrical power relay circuit protection kitAD 2005-17-11Fire extinguisher bottlesAD 98-25-02Top-mounted AntennaEngine · Williams FJ44-3A
AD 2022-13-15Turbine SectionSuperseded and historical ADs · 2
Information bulletins that may apply · 1
Advisory, not mandatory. Matched the same way as ADs.
Airframe · Cessna 525B
SAIB CE-10-49R1Equipment/Furnishings Drain Mast HeaterHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N730JSMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 525B aircraft
FAA incident reports
No FAA accident or incident reports matched to N730JSMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 525B aircraft
Service difficulty reports · 2
SDR 3EJA7304/05/22None · noneRUDDER PEDALS HAVE BINDING / GRINDING FEELING DURING TAXI. T/S TO COPILOT RUDDER PEDALS CHAFING AGAINST R/H KICK PANEL. REPOSITIONED KICK PANEL AS REQUIRED FOR PROPER CLEARANCE IAW AMM 25-12-01SDR 3EJA202104070001Valve · leakingON TAKE-OFF RUDDER FULL DEFLECTION AFTER TRIMMING, CONTINUED ACTUATING RUDDER INPUTS-NOT BY HUMAN INTERACTION. AFFECTED AILERON EFFICIENCY. REMOVED AND REPLACED RUDDER BIAS VALVE. OPS CK GOOD REF MM 27-20-01