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Aircraft record

N125CD2023 Textron Aviation INC 525B

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply4 service difficulty reports

Registration
Valid
expires Mar 31, 2033
Based in
Pleasant Grove, UT
owner city / state
Owners
1
since 2026
NTSB events
None
since 1982
ADs may apply
6
confirm with A&P
Service reports
4
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Aero Dynamic Medical LLC
Owner type
LLC
City, state
Pleasant Grove, UT
Certificate issued
Mar 24, 2026
Expires
Mar 31, 2033
Airworthiness
Standard · Commuter
Airworthiness date
Dec 12, 2023

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 data

Airframe

Manufacturer
Textron Aviation INC
Model
525B
Year
2023
Serial number
525B0710
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
A0667B

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
  1. 2026 – nowAero Dynamic Medical LLCPleasant Grove, UT · current
  2. 1990 – 2018Helicopter Applicators INCGettysburg, PA · different airframe: 1968 Bell 47g-3b-1 S/N 3762

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs 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.

ADSubjectEffectiveApplies to
2026-03-06Vertical Stabilizer Structure; 5415, Nacelle/Pylon, Attach FittingsMar 13, 2026Airframe (525B)
2024-15-09Gust Lock/ Damper SystemOct 22, 2024Airframe (525B)Only with: Tamarack ATLAS winglets installed in accordance with STC No. SA03842NY.
2020-24-06Flight ControlsDec 28, 2020Airframe (525B)Only with: With Tamarack active load alleviation system (ATLAS) winglets installed in accordance with STC SA03842NY.
2008-03-10Cessna Aircraft Company Models 525, 525A, and 525B AirplanesMar 11, 2008Airframe (525B)Certain serial numbers: 525 0001–0637; 525A 0001–0347; 525B 0001–0152. Only with: Cockpit mounted pilot relief tube installed.
2007-23-16Cessna Aircraft Company, Model 525B AirplanesDec 19, 2007Airframe (525B)Certain serial numbers: 525B 0001–0013
Show all 6 ADs
ADSubjectEffectiveApplies to
2005-17-11The Cessna Aircraft Company Models 525, 525A, and 525B AirplanesOct 7, 2005Airframe (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.

  • Flight controls · flap system · asymetricMay 14, 2026

    INITIAL SQUAWK WAS FOR FLAPS NOT LOCKING IN THE UP POSITION. THE FLAPS WERE DROOPING WHILE TAXING OR PARKED. DURING SERVICE THE TECHNICIANS REPORTED THE FLAP ACTUATORS WERE UNLOCKING AT DIFFERENT PRESSURES. THIS WOULD CAUSE A MOMENTARY ASYMMETRIC DEPLOYMENT OF THE FLAPS. TEXTRON ENGINEERING…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · flap system · asymetricMay 14, 2026

    INITIAL SQUAWK WAS FOR FLAPS NOT LOCKING IN THE UP POSITION. THE FLAPS WERE DROOPING WHILE TAXING OR PARKED. DURING SERVICE THE TECHNICIANS REPORTED THE FLAP ACTUATORS WERE UNLOCKING AT DIFFERENT PRESSURES. THIS WOULD CAUSE A MOMENTARY ASYMMETRIC DEPLOYMENT OF THE FLAPS. TEXTRON ENGINEERING…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · flap system · asymetricMay 14, 2026

    INITIAL SQUAWK WAS FOR FLAPS NOT LOCKING IN THE UP POSITION. THE FLAPS WERE DROOPING WHILE TAXING OR PARKED. DURING SERVICE THE TECHNICIANS REPORTED THE FLAP ACTUATORS WERE UNLOCKING AT DIFFERENT PRESSURES. THIS WOULD CAUSE A MOMENTARY ASYMMETRIC DEPLOYMENT OF THE FLAPS. TEXTRON ENGINEERING…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reports
  • Flight controls · flap system · asymetricMay 14, 2026

    THE INITIAL SQUAWK WAS FOR THE FLAP ACTUATORS NOT LOCKING IN THE FULLY RETRACTED POSITION. THE FLAPS WOULD DROOP DURING TAXI AND/OR WHILE PARKED. DURING THE SERVICE EVENT. THE TECHNICIANS REPORTED THE FLAP ACTUATORS WERE UNLOCKING AT DIFFERENT PRESSURES. THIS WOULD CAUSE A MOMENTARY ASYMMETRIC…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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