20240712012449A

Accident · Substantial damage

FAA accident report · Air Tractor 602 · Dectur, IL · July 12, 2024

Date
July 12, 2024 · 14:00 local
Place
Dectur, IL
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Operator
9FRG
Damage
Substantial damage
Aircraft
N528JC
NTSB investigation
NTSBCEN24LA261
Reported as
Air Tractor 602
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
22,000 total

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.

Aircraft was conducting a normal approach to landing at kdec on runway 18. On touchdown, the aircraft experienced oscilations of the tailwheel as evidenced by the marks left on the runway. The tail of the aircraft eventually swung FAR to the right of the aircraft collapsing the right main landing gear near the edge of the runway and struck the propellor and right wing tip. Inertia carried the aircraft off the left side of runway 18 into the grass. The aircraft continued its roation and came to a rest upright on a heading of approximately 290.

Post accident investigation discovered that the tail wheel lock handle was engaged in the cockpit, but the pin that locks the tailwheel was not engaged. Examination of the tail wheel lock pin found that the pin was protruding through the housing approximately 1/16".

The handle was operated several times with no change of positon of the locking pin. Continuity of the controls proved that the handle and cable mechanism was complete but that the spring that locks the pin into the tail wheel receptacle did not have enough tension to overcome the resistance of the housing through which it passed. The pin and spring were eventually freed and successive operation of the cockpit handle provided positive engagement of the tail wheel lock and extension of the pin through the housing of approximately 1/2".

As the FAA filed it

AIRCRAFT WAS CONDUCTING A NORMAL APPROACH TO LANDING AT KDEC ON RUNWAY 18. ON TOUCHDOWN, THE AIRCRAFT EXPERIENCED OSCILATIONS OF THE TAILWHEEL AS EVIDENCED BY THE MARKS LEFT ON THE RUNWAY. THE TAIL OF THE AIRCRAFT EVENTUALLY SWUNG FAR TO THE RIGHT OF THE AIRCRAFT COLLAPSING THE RIGHT MAIN LANDING GEAR NEAR THE EDGE OF THE RUNWAY AND STRUCK THE PROPELLOR AND RIGHT WING TIP. INERTIA CARRIED THE AIRCRAFT OFF THE LEFT SIDE OF RUNWAY 18 INTO THE GRASS. THE AIRCRAFT CONTINUED ITS ROATION AND CAME TO A REST UPRIGHT ON A HEADING OF APPROXIMATELY 290.

POST ACCIDENT INVESTIGATION DISCOVERED THAT THE TAIL WHEEL LOCK HANDLE WAS ENGAGED IN THE COCKPIT, BUT THE PIN THAT LOCKS THE TAILWHEEL WAS NOT ENGAGED. EXAMINATION OF THE TAIL WHEEL LOCK PIN FOUND THAT THE PIN WAS PROTRUDING THROUGH THE HOUSING APPROXIMATELY 1/16".

THE HANDLE WAS OPERATED SEVERAL TIMES WITH NO CHANGE OF POSITON OF THE LOCKING PIN. CONTINUITY OF THE CONTROLS PROVED THAT THE HANDLE AND CABLE MECHANISM WAS COMPLETE BUT THAT THE SPRING THAT LOCKS THE PIN INTO THE TAIL WHEEL RECEPTACLE DID NOT HAVE ENOUGH TENSION TO OVERCOME THE RESISTANCE OF THE HOUSING THROUGH WHICH IT PASSED. THE PIN AND SPRING WERE EVENTUALLY FREED AND SUCCESSIVE OPERATION OF THE COCKPIT HANDLE PROVIDED POSITIVE ENGAGEMENT OF THE TAIL WHEEL LOCK AND EXTENSION OF THE PIN THROUGH THE HOUSING OF APPROXIMATELY 1/2".

NTSB investigation

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