N428CS2007 Cessna 525B
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply4 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Altc LLC
- Owner type
- LLC
- City, state
- Sun Valley, CA
- Certificate issued
- Sep 14, 2021
- Expires
- Sep 30, 2028
- Airworthiness
- Standard · Commuter
- Airworthiness date
- Jun 23, 2007
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Cessna
- Model
- 525B
- Year
- 2007
- Serial number
- 525B0165
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 8
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Mode S code
- A5199A
Engine
- Make and model
- Williams Fj44-3a
- Type
- Turbo-fan
- Power
- 2,820 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2021 – nowAltc LLCSun Valley, CA · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (6)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2026-03-06 | Vertical Stabilizer Structure; 5415, Nacelle/Pylon, Attach Fittings | Mar 13, 2026 | Airframe (525B) |
| 2024-15-09 | Gust Lock/ Damper System | Oct 22, 2024 | Airframe (525B)Only with: Tamarack ATLAS winglets installed in accordance with STC No. SA03842NY. |
| 2020-24-06 | Flight Controls | Dec 28, 2020 | Airframe (525B)Only with: With Tamarack active load alleviation system (ATLAS) winglets installed in accordance with STC SA03842NY. |
| 2008-03-10 | Cessna Aircraft Company Models 525, 525A, and 525B Airplanes | Mar 11, 2008 | Airframe (525B)Certain serial numbers: 525 0001–0637; 525A 0001–0347; 525B 0001–0152. Only with: Cockpit mounted pilot relief tube installed. |
| 2007-23-16 | Cessna Aircraft Company, Model 525B Airplanes | Dec 19, 2007 | Airframe (525B)Certain serial numbers: 525B 0001–0013 |
Show all 6 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2005-17-11 | The Cessna Aircraft Company Models 525, 525A, and 525B Airplanes | Oct 7, 2005 | Airframe (525B)Certain serial numbers: 525 525-0001–525-0600; 525A 525A-0001–525A-0234; 525B 525B-0001–525B-0035 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (4)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Landing gear · bulb · inoperativeFeb 2, 2012
ON 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 DIVERTED FOR MX. CREW DID NOT DECLARE AN…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · valve · inoperativeDec 7, 2011
DURING 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 UNEVENTFUL. MX TROUBLESHOT SYS TO A FAULTY…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · bulb · burned outJan 13, 2011
ON 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. ACFT LANDING WAS UNEVENTFUL. MX REPLACED…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reportsShow fewer reports
- Engine fuel and control · fuel control · defectiveDec 5, 2010
DESCENDING 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 ACFT DIRECT FCM AND DECLARED AN…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026