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NTSB Report

September 25, 2025 · Textron Aviation 525C · N361MB

Baton Rouge, LA

Overview

Report Status
Probable Cause
Event Type
Accident
Date
September 25, 2025
Injury Outcomes
No injuries (2 uninjured)
Location
Baton Rouge, LA
Aircraft
Textron Aviation 525C (2021)
Tail Number
N361MB
Operator
Pacifia
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CEN25LA402

About 10,000 ft mean sea level during a repositioning flight, the flight crew felt a bump/thud in the back of the airplane, which they thought was caused by something falling into the aisle from the lavatory. The flight crew observed that the landing gear unsafe light was illuminated. The flight crew stated that they followed emergency/abnormal airplane checklist items and reset the landing circuit breaker, which did not retract the landing gear. Then, the crew lowered the landing gear, which resulted in three green landing gear position lights. They continued the flight to the destination with the landing gear extended where they landed the airplane. During landing rollout and after applying moderate braking, they felt the right main landing gear collapse, which then punctured the right wing and resulted in substantial damage to right wing. Postaccident examination revealed the aft main landing gear trunnion pin for the right main landing gear was not properly installed during the recent maintenance as the aft trunnion pin was not installed far enough to allow the retaining roll pin to engage and retain the trunnion pin. The pilot reported and maintenance records showed that maintenance performed by the aircraft manufacturer’s service center, which included the reinstallation of the main landing gear trunnion pin, occurred 2.9 hours before the accident. According to the manufacturer’s maintenance manual installation procedures, maintenance personnel are required to make sure the aft end of the trunnion pin is at least 2.0 inches (50.8 mm) forward of the aft spar fitting to verify proper installation. The Civil Aviation Accident and Incident Investigation Commission (CIAIAC) of Spain investigated a similar accident that occurred on May 4, 2018, as documented in CIAIAC Report A-012/2018. As a result of the investigation, the aircraft manufacturer published a mandatory service letter (SL525C-32-12) to do an inspection of the aft main landing trunnion pins for proper installation.

NTSB Probable Cause

The improper installation of the trunnion pin, which resulted in a failure of the right main landing gear. Contributing to the accident was the failure of maintenance personnel to follow the aircraft manufacturer’s maintenance procedures.

Full Narrative

About 10,000 ft mean sea level during a repositioning flight, the flight crew felt a bump/thud in the back of the airplane, which they thought was caused by something falling into the aisle from the lavatory. The flight crew observed that the landing gear unsafe light was illuminated. The flight crew stated that they followed emergency/abnormal airplane checklist items and reset the landing circuit breaker, which did not retract the landing gear. Then, the crew lowered the landing gear, which resulted in three green landing gear position lights. They continued the flight to the destination with the landing gear extended where they landed the airplane. During landing rollout and after applying moderate braking, they felt the right main landing gear collapse, which then punctured the right wing and resulted in substantial damage to right wing. Postaccident examination revealed the aft main landing gear trunnion pin for the right main landing gear was not properly installed during the recent maintenance as the aft trunnion pin was not installed far enough to allow the retaining roll pin to engage and retain the trunnion pin. The pilot reported and maintenance records showed that maintenance performed by the aircraft manufacturer’s service center, which included the reinstallation of the main landing gear trunnion pin, occurred 2.9 hours before the accident. According to the manufacturer’s maintenance manual installation procedures, maintenance personnel are required to make sure the aft end of the trunnion pin is at least 2.0 inches (50.8 mm) forward of the aft spar fitting to verify proper installation. The Civil Aviation Accident and Incident Investigation Commission (CIAIAC) of Spain investigated a similar accident that occurred on May 4, 2018, as documented in CIAIAC Report A-012/2018. As a result of the investigation, the aircraft manufacturer published a mandatory service letter (SL525C-32-12) to do an inspection of the aft main landing trunnion pins for proper installation.

Flight

Event TypeAccident
Event Time18:25 CDT
Nearest AirportBaton Rouge Metropolitan Airpo (0.2nm NW)
Runway31
Runway Length7005 ft
Runway Width150 ft
Flight Plan FiledIFR
Flight Plan ActivatedYes
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftTextron Aviation 525C
Tail NumberN361MB
Aircraft CategoryAir
DamageSubstantial
OperatorPacifia
Operating RulePart 91
Engines2
Engine TypeTurbofan
Engine DetailsWilliams · FJ44-4A · Turbofan · 3621 | Williams · FJ44-4A · Turbofan · 3621
Seats11

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 22 · First Class · None
Crew 2Age 50 · First Class · None

Conditions

ConditionsVMC
LightDaylight
Wind260° @ 3 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point70 F
Altimeter29.89 inHg
Observation Time17:53
Weather SourceWFAC

Appendix: Source Data