20240325005209A

Accident · Substantial damage

FAA accident report · Parmelee M/Parmelee N COZY MARK IV · Gonzales, TX · March 25, 2024

Date
March 25, 2024 · 18:44 local
Place
Gonzales, TX
Airport
Roger M Dreyer Memorial
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N20MN
NTSB investigation
NTSBCEN24LA141
Reported as
Parmelee M/Parmelee N Cozy Mark IV
Reported engine
Lycoming 0-360-A1D
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot

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.

On 03/25/2024, the pilot of the accident aircraft contacted san antonio ATC declaring an emergency due to loss of engine. He advised ATC that he would attempt to glide into the gonzalez airport (T20) for landing. Houston center later advised that they were in contact with the pilot and there were no reported injuries. The aircraft landed short of the runway and sustained substantial damage to the left wing, left aileron torque tube, left elevator and collapsed the nose landing gear. Primary field investigation revealed that the engine still contained approximately five quarts of oil. The normal operating range is 4-6 quarts. However, there was presence of an oil leak that resulted in an oil puddle between the #2 and #4 cylinders. Additionally, the #1 and #3 cylinders had no compression. An engine teardown was conducted later and revealed the left idler stud mount for the gear that drives the engine driven fuel pump was shimmed and the studs in the engine block for the hold down nuts were not tight. This allowed movement of the idler stud leading to abnormal wear and eventual failure of the hardware. Once this occurred, the gear mounted on this idler became disengaged with the magneto drive gear which also drives the cam. This caused the valves to stop being driven when the cam was no longer turning.

As the FAA filed it

ON 03/25/2024, THE PILOT OF THE ACCIDENT AIRCRAFT CONTACTED SAN ANTONIO ATC DECLARING AN EMERGENCY DUE TO LOSS OF ENGINE. HE ADVISED ATC THAT HE WOULD ATTEMPT TO GLIDE INTO THE GONZALEZ AIRPORT (T20) FOR LANDING. HOUSTON CENTER LATER ADVISED THAT THEY WERE IN CONTACT WITH THE PILOT AND THERE WERE NO REPORTED INJURIES. THE AIRCRAFT LANDED SHORT OF THE RUNWAY AND SUSTAINED SUBSTANTIAL DAMAGE TO THE LEFT WING, LEFT AILERON TORQUE TUBE, LEFT ELEVATOR AND COLLAPSED THE NOSE LANDING GEAR. PRIMARY FIELD INVESTIGATION REVEALED THAT THE ENGINE STILL CONTAINED APPROXIMATELY FIVE QUARTS OF OIL. THE NORMAL OPERATING RANGE IS 4-6 QUARTS. HOWEVER, THERE WAS PRESENCE OF AN OIL LEAK THAT RESULTED IN AN OIL PUDDLE BETWEEN THE #2 AND #4 CYLINDERS. ADDITIONALLY, THE #1 AND #3 CYLINDERS HAD NO COMPRESSION. AN ENGINE TEARDOWN WAS CONDUCTED LATER AND REVEALED THE LEFT IDLER STUD MOUNT FOR THE GEAR THAT DRIVES THE ENGINE DRIVEN FUEL PUMP WAS SHIMMED AND THE STUDS IN THE ENGINE BLOCK FOR THE HOLD DOWN NUTS WERE NOT TIGHT. THIS ALLOWED MOVEMENT OF THE IDLER STUD LEADING TO ABNORMAL WEAR AND EVENTUAL FAILURE OF THE HARDWARE. ONCE THIS OCCURRED, THE GEAR MOUNTED ON THIS IDLER BECAME DISENGAGED WITH THE MAGNETO DRIVE GEAR WHICH ALSO DRIVES THE CAM. THIS CAUSED THE VALVES TO STOP BEING DRIVEN WHEN THE CAM WAS NO LONGER TURNING.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N20MN · 3

Matched to the same aircraft by N-number and date.