- Serial number
- 525B0165
- Year built
- 2007
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- June 23, 2007
- Certificate issued
- September 14, 2021
- Expires
- September 30, 2028
- Mode S code
- A5199A
- Registered owner
- Altc LLC
- Location
- Sun Valley, CA
- 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 N428CSMatched 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 N428CSMatched 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 · 4
SDR Z5FA2012020200001Bulb · inoperativeON APPROACH, CREW SELECTED GEAR DOWN, THE RT MAIN GEAR LIGHT DID NOT ILLUMINATE. CREW FOLLOWED CHECKLIST, BLEW DOWN GEAR AND STILL DID NOT RECEIVE PROPER INDICATIONS. CREW USED ROTARY TEST AND GEAR WARNING SYS, NO INDICATION OF UNSAFE CONDITION. CREW DIVERTSDR Z5FA2011120900001Valve · inoperativeDURING FLIGHT, FLAPS DID NOT MOVE WITH HANDLE SELECTED TO 15 DEGREES. UNABLE TO LOWER LANDING GEAR AND SPEED BRAKES WERE INOPERATIVE. AN EMERGENCY WAS DECLARED. LANDING GEAR WAS EXTENDED USING THE EMERGENCY BLOW DOWN PROCEDURE. ACFT DIVERTED. LANDING WAS SDR Z5FA011311N428CS1Bulb · burned outON APPROACH, GEAR SELECTED DOWN, THE LT MAIN GEAR LIGHT DID NOT ILLUMINATE. ROTARY TEST CONFIRMED LT MAIN GEAR INDICATOR LIGHTS WERE INOPERATIVE. CREW RAN THE CHECK LIST PROCEDURE FOR EMERGENCY GEAR EXTENSION. TOWER CONFIRMED ALL 3 LANDING GEARS WERE DOWN. ACSDR Z5FA120510N428CS1Fuel Control · defectiveDESCENDING ENROUTE, CREW PULLED BACK BOTH THROTTLES TO FLIGHT IDLE AND THE LT ENGINE ROLLED BACK AND SHUT DOWN. AFTER GOING THROUGH AFM CHECK LIST CREW ATTEMPTED AN UNSUCCESSFUL RESTART, AT 24,00 FT. AT 15,000 FT A WINDMILL RESTART WAS SUCCESSFUL AND ATC GAVE