20180211014499A

Accident · Substantial damage

FAA accident report · Shanks V Roger VARI-EZE · Santa Monica, CA · February 11, 2018

Date
February 11, 2018 · 13:00 local
Place
Santa Monica, CA
Airport
Santa Monica Municipal
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N944X
NTSB investigation
NTSBWPR18LA089
Reported as
Shanks V Roger VARI-EZE
Reported engine
Continental 0-200 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
260 total120 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.

On February 11, 2018, at 1258 pacific standard time, an experimental amateur- built roger v Shanks (rutan aircraft factory) varieze, N944X, struck a hangar during its landing rollout at Santa Monica Municipal Airport, Santa Monica, California. The private pilot and pilot rated passenger were not injured. The airplane sustained substantial damage to the nose structure and canard. The airplane was registered to and operated by the pilot under the provisions of 14 code of federal regulations part 91 as a personal flight. The local flight departed brackett field airport, la verne, California about 1240. Visual meteorological conditions prevailed, and no flight plan had been filed.

The pilot reported that the landing approach to runway 21 was uneventful, and that he landed about 200FT beyond the runway numbers. As soon as the nose wheel touched down, the pilot applied brake pressure and the airplane began to swerve to the left. He released the brake and countered with right rudder, and then applied brake pressure again, but the airplane continued to veer left. He then proceeded to alternately cycle the brake and right rudder as the ground roll progressed. The airplane had not appreciably slowed down, and, aware that the terrain dropped off beyond the runway end, he decided to apply full braking. The airplane than veered rapidly to the left, crossed over the adjacent taxiway, and struck a hangar.

The airplane was equipped with a free-castering nose wheel, with ground steering accomplished through differential braking once rudder effectiveness diminished at lower speeds. The design did not incorporate conventional toe-brake, but instead brake pressure was applied directly via the rudder pedals once they had been pushed beyond the pedals rudder travel limits.

Skid marks on the runway indicated that the airplane departed the runway surface just before taxiway where the terrain dropped away. Runway 21 slopes downhill, with a gradient of 1.2%.

As the FAA filed it

ON FEBRUARY 11, 2018, AT 1258 PACIFIC STANDARD TIME, AN EXPERIMENTAL AMATEUR- BUILT ROGER V SHANKS (RUTAN AIRCRAFT FACTORY) VARIEZE, N944X, STRUCK A HANGAR DURING ITS LANDING ROLLOUT AT SANTA MONICA MUNICIPAL AIRPORT, SANTA MONICA, CALIFORNIA. THE PRIVATE PILOT AND PILOT RATED PASSENGER WERE NOT INJURED. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE TO THE NOSE STRUCTURE AND CANARD. THE AIRPLANE WAS REGISTERED TO AND OPERATED BY THE PILOT UNDER THE PROVISIONS OF 14 CODE OF FEDERAL REGULATIONS PART 91 AS A PERSONAL FLIGHT. THE LOCAL FLIGHT DEPARTED BRACKETT FIELD AIRPORT, LA VERNE, CALIFORNIA ABOUT 1240. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND NO FLIGHT PLAN HAD BEEN FILED.

THE PILOT REPORTED THAT THE LANDING APPROACH TO RUNWAY 21 WAS UNEVENTFUL, AND THAT HE LANDED ABOUT 200FT BEYOND THE RUNWAY NUMBERS. AS SOON AS THE NOSE WHEEL TOUCHED DOWN, THE PILOT APPLIED BRAKE PRESSURE AND THE AIRPLANE BEGAN TO SWERVE TO THE LEFT. HE RELEASED THE BRAKE AND COUNTERED WITH RIGHT RUDDER, AND THEN APPLIED BRAKE PRESSURE AGAIN, BUT THE AIRPLANE CONTINUED TO VEER LEFT. HE THEN PROCEEDED TO ALTERNATELY CYCLE THE BRAKE AND RIGHT RUDDER AS THE GROUND ROLL PROGRESSED. THE AIRPLANE HAD NOT APPRECIABLY SLOWED DOWN, AND, AWARE THAT THE TERRAIN DROPPED OFF BEYOND THE RUNWAY END, HE DECIDED TO APPLY FULL BRAKING. THE AIRPLANE THAN VEERED RAPIDLY TO THE LEFT, CROSSED OVER THE ADJACENT TAXIWAY, AND STRUCK A HANGAR.

THE AIRPLANE WAS EQUIPPED WITH A FREE-CASTERING NOSE WHEEL, WITH GROUND STEERING ACCOMPLISHED THROUGH DIFFERENTIAL BRAKING ONCE RUDDER EFFECTIVENESS DIMINISHED AT LOWER SPEEDS. THE DESIGN DID NOT INCORPORATE CONVENTIONAL TOE-BRAKE, BUT INSTEAD BRAKE PRESSURE WAS APPLIED DIRECTLY VIA THE RUDDER PEDALS ONCE THEY HAD BEEN PUSHED BEYOND THE PEDALS RUDDER TRAVEL LIMITS.

SKID MARKS ON THE RUNWAY INDICATED THAT THE AIRPLANE DEPARTED THE RUNWAY SURFACE JUST BEFORE TAXIWAY WHERE THE TERRAIN DROPPED AWAY. RUNWAY 21 SLOPES DOWNHILL, WITH A GRADIENT OF 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.