19980705023879A

Accident · Substantial damage

FAA accident report · Namer AT6G · Longmont, CO · July 5, 1998

Date
July 5, 1998 · 10:50 local
Place
Longmont, CO
Airport
Vance Brand Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8399H
NTSB investigation
NTSBFTW98LA298
Reported as
Namer AT6G
Reported engine
Pratt & Whitney R1340AN1
People aboard
2
Fatal injuries
0
Pilot’s flight hours
11,600 total60 in this make and model250 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.

Lost directional control on 3 point landing. Skidded off rwy. Bent left wing and folded left main gear. (.4)the pilot was given airport advisories on UNICOM. He was told that the active runway was 29 and that the wind was 'light and variable.' He said that the 'windsock's movement was hardly perceptible and the velocity of the indicator indicated less than 5 knots.' The pilot reported that after touchdown, 'the aircraft's rollout path took multiple, short, quick inputs from the rudder to keep properly aligned with the runway centerline as the aircraft proceeded down the runway.' He further reported the rudder inputs became ineffective after approximately 400 to 500 feet of landing roll and the aircraft exited the right side of the runway. The aircraft subsequently impacted an airport taxiway sign, damaging the left main landing gear and the left wing. The aircraft came to rest with its nose down. The pilot said that the tail wheel steering cables had recently been replaced. Postaccident evaluation of the tail wheel steering cables by maintenance personnel found a tension of 5 pounds on these cables; 20 pounds is considered normal (-23)everything seemed normal with the approach to runway 29 at 2V2. Pilot stated he decided a three-point landing was appropriate. When the aircraft touched down, it immediately went inot a skid to the left, departed the runway and across a taxiway onto a grassy area where it came to rest. The wing was bent when the left gear collapsed.

As the FAA filed it

LOST DIRECTIONAL CONTROL ON 3 POINT LANDING. SKIDDED OFF RWY. BENT LEFT WING AND FOLDED LEFT MAIN GEAR. (.4)THE PILOT WAS GIVEN AIRPORT ADVISORIES ON UNICOM. HE WAS TOLD THAT THE ACTIVE RUNWAY WAS 29 AND THAT THE WIND WAS 'LIGHT AND VARIABLE.' HE SAID THAT THE 'WINDSOCK'S MOVEMENT WAS HARDLY PERCEPTIBLE AND THE VELOCITY OF THE INDICATOR INDICATED LESS THAN 5 KNOTS.' THE PILOT REPORTED THAT AFTER TOUCHDOWN, 'THE AIRCRAFT'S ROLLOUT PATH TOOK MULTIPLE, SHORT, QUICK INPUTS FROM THE RUDDER TO KEEP PROPERLY ALIGNED WITH THE RUNWAY CENTERLINE AS THE AIRCRAFT PROCEEDED DOWN THE RUNWAY.' HE FURTHER REPORTED THE RUDDER INPUTS BECAME INEFFECTIVE AFTER APPROXIMATELY 400 TO 500 FEET OF LANDING ROLL AND THE AIRCRAFT EXITED THE RIGHT SIDE OF THE RUNWAY. THE AIRCRAFT SUBSEQUENTLY IMPACTED AN AIRPORT TAXIWAY SIGN, DAMAGING THE LEFT MAIN LANDING GEAR AND THE LEFT WING. THE AIRCRAFT CAME TO REST WITH ITS NOSE DOWN. THE PILOT SAID THAT THE TAIL WHEEL STEERING CABLES HAD RECENTLY BEEN REPLACED. POSTACCIDENT EVALUATION OF THE TAIL WHEEL STEERING CABLES BY MAINTENANCE PERSONNEL FOUND A TENSION OF 5 POUNDS ON THESE CABLES; 20 POUNDS IS CONSIDERED NORMAL (-23)EVERYTHING SEEMED NORMAL WITH THE APPROACH TO RUNWAY 29 AT 2V2. PILOT STATED HE DECIDED A THREE-POINT LANDING WAS APPROPRIATE. WHEN THE AIRCRAFT TOUCHED DOWN, IT IMMEDIATELY WENT INOT A SKID TO THE LEFT, DEPARTED THE RUNWAY AND ACROSS A TAXIWAY ONTO A GRASSY AREA WHERE IT CAME TO REST. THE WING WAS BENT WHEN THE LEFT GEAR COLLAPSED.

NTSB investigation

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