20240810012779I

Incident · Minor damage

FAA incident report · Lancair LC-40-550FG · San Carlos, CA · August 10, 2024

Date
August 10, 2024 · 16:52 local
Place
San Carlos, CA
Airport
San Carlos Airport
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N141AM
Reported as
Lancair LC-40-550FG
Reported engine
Continental IO-550 series
People aboard
3
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
1,915 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.

Incident occurred on landing rollout. Weather was clear with unrestricted visibility. On initial braking, a “pop” was felt through the left brake pedal during the landing roll. Right brake pressure had to be released to prevent turning to the right at speed. A second application check of the left brake had no effect.

The aircraft has a castering nose wheel and requires differential braking to control steering, so without equal braking only partial right brake could be used to slow the aircraft to prevent a more extreme turn to the right. Given the lack of braking and steering control, the aircraft departed the runway at the

Departure end of the runway while still traveling approximately ~30 KTS. During the runway overrun, right brake was used to avoid direct impact with airport signage, but the right wing impacted a runway end light resulting in visible damage to the composite skin on the underside of the right wing. Once the speed had decreased to less than 15 KTS, full right brake was applied to spin the aircraft twice in a circle until it stopped, avoiding impact with the airport fencing.

As the FAA filed it

INCIDENT OCCURRED ON LANDING ROLLOUT. WEATHER WAS CLEAR WITH UNRESTRICTED VISIBILITY. ON INITIAL BRAKING, A “POP” WAS FELT THROUGH THE LEFT BRAKE PEDAL DURING THE LANDING ROLL. RIGHT BRAKE PRESSURE HAD TO BE RELEASED TO PREVENT TURNING TO THE RIGHT AT SPEED. A SECOND APPLICATION CHECK OF THE LEFT BRAKE HAD NO EFFECT.

THE AIRCRAFT HAS A CASTERING NOSE WHEEL AND REQUIRES DIFFERENTIAL BRAKING TO CONTROL STEERING, SO WITHOUT EQUAL BRAKING ONLY PARTIAL RIGHT BRAKE COULD BE USED TO SLOW THE AIRCRAFT TO PREVENT A MORE EXTREME TURN TO THE RIGHT. GIVEN THE LACK OF BRAKING AND STEERING CONTROL, THE AIRCRAFT DEPARTED THE RUNWAY AT THE

DEPARTURE END OF THE RUNWAY WHILE STILL TRAVELING APPROXIMATELY ~30 KTS. DURING THE RUNWAY OVERRUN, RIGHT BRAKE WAS USED TO AVOID DIRECT IMPACT WITH AIRPORT SIGNAGE, BUT THE RIGHT WING IMPACTED A RUNWAY END LIGHT RESULTING IN VISIBLE DAMAGE TO THE COMPOSITE SKIN ON THE UNDERSIDE OF THE RIGHT WING. ONCE THE SPEED HAD DECREASED TO LESS THAN 15 KTS, FULL RIGHT BRAKE WAS APPLIED TO SPIN THE AIRCRAFT TWICE IN A CIRCLE UNTIL IT STOPPED, AVOIDING IMPACT WITH THE AIRPORT FENCING.