20241224021159A

Accident · Substantial damage

FAA accident report · Cessna 337G · Athens, GA · December 24, 2024

Date
December 24, 2024 · 17:00 local
Place
Athens, GA
Airport
Athens/Ben Epps
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N868MT
Reported as
Cessna 337G
Reported engine
Continental IO-360 series
People aboard
1
Fatal injuries
0
Other injuries
0

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Pilot reported that shortly after takeoff, he retracted the landing gear. The retraction process stopped about halfway through its cycle. The pilot attempted to manually retract the gear but the gear did not move. He returned to the airport and landed with the gear partially extended. The nose gear did lock and prevented damage to the front propeller. Upon completing a gear swing test, it was discovered that the right main gear actuating cylinder ruptured, causing a loss of hydraulic fluid, and failure of the gear actuating system. Upon landing, the main gear were partially retracted, causing damage to the rear engine, propeller, and main gear doors.

As the FAA filed it

PILOT REPORTED THAT SHORTLY AFTER TAKEOFF, HE RETRACTED THE LANDING GEAR. THE RETRACTION PROCESS STOPPED ABOUT HALFWAY THROUGH ITS CYCLE. THE PILOT ATTEMPTED TO MANUALLY RETRACT THE GEAR BUT THE GEAR DID NOT MOVE. HE RETURNED TO THE AIRPORT AND LANDED WITH THE GEAR PARTIALLY EXTENDED. THE NOSE GEAR DID LOCK AND PREVENTED DAMAGE TO THE FRONT PROPELLER. UPON COMPLETING A GEAR SWING TEST, IT WAS DISCOVERED THAT THE RIGHT MAIN GEAR ACTUATING CYLINDER RUPTURED, CAUSING A LOSS OF HYDRAULIC FLUID, AND FAILURE OF THE GEAR ACTUATING SYSTEM. UPON LANDING, THE MAIN GEAR WERE PARTIALLY RETRACTED, CAUSING DAMAGE TO THE REAR ENGINE, PROPELLER, AND MAIN GEAR DOORS.