20160204007319I

Incident · Minor damage

FAA incident report · Cessna 310N · Griffin, GA · February 4, 2016

Date
February 4, 2016 · 17:30 local
Place
Griffin, GA
Airport
Griffin - Spalding County
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N395MC
Reported as
Cessna 310N
Reported engine
Continental I0-470 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
3,200 total50 in this make and model5 in the last 90 days

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 February 4, 2016 at approximately 1700 hours, while test flying N395MC, a Cessna 310N, sn 310N-064, to do an autopilot test flight, the pilot noticed the gear lights would not remain on when landing gear was deployed. Coming in for the landing, the pilot would lower the landing gear and would get three green lights. After a few seconds, the two main lights would go out. The gear was recycled several times which never corrected the problem. The pilot then pulled the gear circuit breaker and hand cranked the gear down with the same results. The pilot radioed a second pilot who was about to take off and asked him if he would fly alongside the aircraft and look at the landing gear. The second pilot said that the gear appeared to be down but the right landing gear door looked like it was not completely closed. The pilot then proceeded to land. Upon landing and having rolled approximately 50 yards it appeared that the right gear collapsed. When the plane starting to veer off to the right side of the runway the slide loaded the left gear and it collapsed as well. The no. 2 propeller struck the ground but did not stop spinning. Minor damage to the right and left gear door and the foot stand was bent no other damage noted until aircraft was moved. When the aircraft was moved from the runway to the hanger, damage was done to the strap area when the aircraft was lifted during transit.

After moving the aircraft to a hanger and placing it on jacks for testing, further investigation determined that a down lock limit switch and or down lock relay on the right gear failed and would not allow the gear to lock in place. The gear would move into an over-center position not allowing it to lock in place.

Pilot was not injured during this landing. No other injuries reported.

As the FAA filed it

ON FEBRUARY 4, 2016 AT APPROXIMATELY 1700 HOURS, WHILE TEST FLYING N395MC, A CESSNA 310N, SN 310N-064, TO DO AN AUTOPILOT TEST FLIGHT, THE PILOT NOTICED THE GEAR LIGHTS WOULD NOT REMAIN ON WHEN LANDING GEAR WAS DEPLOYED. COMING IN FOR THE LANDING, THE PILOT WOULD LOWER THE LANDING GEAR AND WOULD GET THREE GREEN LIGHTS. AFTER A FEW SECONDS, THE TWO MAIN LIGHTS WOULD GO OUT. THE GEAR WAS RECYCLED SEVERAL TIMES WHICH NEVER CORRECTED THE PROBLEM. THE PILOT THEN PULLED THE GEAR CIRCUIT BREAKER AND HAND CRANKED THE GEAR DOWN WITH THE SAME RESULTS. THE PILOT RADIOED A SECOND PILOT WHO WAS ABOUT TO TAKE OFF AND ASKED HIM IF HE WOULD FLY ALONGSIDE THE AIRCRAFT AND LOOK AT THE LANDING GEAR. THE SECOND PILOT SAID THAT THE GEAR APPEARED TO BE DOWN BUT THE RIGHT LANDING GEAR DOOR LOOKED LIKE IT WAS NOT COMPLETELY CLOSED. THE PILOT THEN PROCEEDED TO LAND. UPON LANDING AND HAVING ROLLED APPROXIMATELY 50 YARDS IT APPEARED THAT THE RIGHT GEAR COLLAPSED. WHEN THE PLANE STARTING TO VEER OFF TO THE RIGHT SIDE OF THE RUNWAY THE SLIDE LOADED THE LEFT GEAR AND IT COLLAPSED AS WELL. THE NO. 2 PROPELLER STRUCK THE GROUND BUT DID NOT STOP SPINNING. MINOR DAMAGE TO THE RIGHT AND LEFT GEAR DOOR AND THE FOOT STAND WAS BENT NO OTHER DAMAGE NOTED UNTIL AIRCRAFT WAS MOVED. WHEN THE AIRCRAFT WAS MOVED FROM THE RUNWAY TO THE HANGER, DAMAGE WAS DONE TO THE STRAP AREA WHEN THE AIRCRAFT WAS LIFTED DURING TRANSIT.

AFTER MOVING THE AIRCRAFT TO A HANGER AND PLACING IT ON JACKS FOR TESTING, FURTHER INVESTIGATION DETERMINED THAT A DOWN LOCK LIMIT SWITCH AND OR DOWN LOCK RELAY ON THE RIGHT GEAR FAILED AND WOULD NOT ALLOW THE GEAR TO LOCK IN PLACE. THE GEAR WOULD MOVE INTO AN OVER-CENTER POSITION NOT ALLOWING IT TO LOCK IN PLACE.

PILOT WAS NOT INJURED DURING THIS LANDING. NO OTHER INJURIES REPORTED.