20110731017569A

Accident · Substantial damage

FAA accident report · T&T FALCON LS · Lee'S Summit, MO · July 31, 2011

Date
July 31, 2011 · 21:00 local
Place
Lee'S Summit, MO
Airport
Lee'S Summit Municipal
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N785TT
NTSB investigation
NTSBCEN11LA542
Reported as
T&T Falcon LS
Reported engine
Lycoming O235N2C
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
815 total10 in this make and model9 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.

The pilot was unable to maintain runway heading while rolling out on runway 18. The aircraft departed the runway to the left, struck runway edge lights and crossed taxiway crossover A3, which collapsed the nosegear. The aircraft then continued across the taxiway and struck the taxiway sign, sustaining substantial damage to the right wing. Post accident investigation revealed that the left rudder teleflex cable required excessive pressure to move. This prevented the pilot from being able to apply right rudder or nosewheel steering to correct the aircraft's path.

As the FAA filed it

THE PILOT WAS UNABLE TO MAINTAIN RUNWAY HEADING WHILE ROLLING OUT ON RUNWAY 18. THE AIRCRAFT DEPARTED THE RUNWAY TO THE LEFT, STRUCK RUNWAY EDGE LIGHTS AND CROSSED TAXIWAY CROSSOVER A3, WHICH COLLAPSED THE NOSEGEAR. THE AIRCRAFT THEN CONTINUED ACROSS THE TAXIWAY AND STRUCK THE TAXIWAY SIGN, SUSTAINING SUBSTANTIAL DAMAGE TO THE RIGHT WING. POST ACCIDENT INVESTIGATION REVEALED THAT THE LEFT RUDDER TELEFLEX CABLE REQUIRED EXCESSIVE PRESSURE TO MOVE. THIS PREVENTED THE PILOT FROM BEING ABLE TO APPLY RIGHT RUDDER OR NOSEWHEEL STEERING TO CORRECT THE AIRCRAFT'S PATH.

NTSB investigation

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