WPR14CA365

NTSB accident investigation · Ealand Charles Lionheart · Santa Maria, CA · September 5, 2014

Accident · Minor injuriesData collectionFinal report
Date
September 5, 2014, 13:00 local (20:00 UTC)
Place
Santa Maria, CA
Injuries
3 minor
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N15TEEaland Charles Lionheart
Defining event
Landing-landing roll: Runway excursion
Weather
Visual (VMC) · Day
Status
Completed · report December 5, 2014
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Administration FSDO
FAA report
20140905016239A
Case key
90032

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The pilot's inadequate landing flare and subsequent loss of directional control during the landing roll.

Findings · 5

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The owner/builder of the experimental amateur-built, tailwheel-equipped biplane was seated in the front left seat, with another pilot seated in the right seat, and a passenger in the rear seat. The intent of the flight was to prepare both pilots for a flight review, with both trading off flight duties as necessary. They planned to initially perform touch-and-go landings at their home base airport, with the pilot in the right seat acting as pilot-in-command. The first takeoff and landing was uneventful, but the airport was busy, so they diverted to the accident airport to practice further. The landing approach was normal, with the airplane touching down slightly to the right of centerline and then bouncing. The pilot made corrective control inputs, but the airplane did not fully respond, bouncing again on the runway. He applied forward elevator pressure and the airplane landed a third time, this time remaining on the ground. The airplane began to drift to the right, but would not respond to the pilot's rudder inputs. The owner/builder then applied left rudder, but the airplane continued to drift towards a runway sign. As they passed to the right of the sign the airplane pitched down violently, and nosed over. The airplane sustained substantial damage during the accident sequence to the left upper wing and the vertical stabilizer. Postaccident examination of the airplane revealed no mechanical malfunctions or failures which would have precluded normal operation. The owner stated that this was the first flight since he had completed the airplane's conditional inspection, and no flight control malfunctions were discovered at that time. He subsequently stated that he did not find any mechanical malfunctions or failures during a post-accident examination. He further surmised that the design of the braking system was such that simultaneous application of the left and right side brake pedals by both pilots may have resulted in excessive brake pressure, and this may have been the reason the airplane nosed over so unexpectedly.

Factual narrative

The owner/builder of the experimental amateur-built, tailwheel-equipped biplane was seated in the front left seat, with another pilot seated in the right seat, and a passenger in the rear seat. The intent of the flight was to prepare both pilots for a flight review, with both trading off flight duties as necessary. They planned to initially perform touch-and-go landings at their home base airport, with the pilot in the right seat acting as pilot-in-command. The first takeoff and landing was uneventful, but the airport was busy, so they diverted to the accident airport to practice further. The landing approach was normal, with the airplane touching down slightly to the right of centerline and then bouncing. The pilot made corrective control inputs, but the airplane did not fully respond, bouncing again on the runway. He applied forward elevator pressure and the airplane landed a third time, this time remaining on the ground. The airplane began to drift to the right, but would not respond to the pilot's rudder inputs. The owner/builder then applied left rudder, but the airplane continued to drift towards a runway sign. As they passed to the right of the sign the airplane pitched down violently, and nosed over.The airplane sustained substantial damage during the accident sequence to the left upper wing and the vertical stabilizer. Postaccident examination of the airplane revealed no mechanical malfunctions or failures which would have precluded normal operation. The owner stated that this was the first flight since he had completed the airplane's conditional inspection, and no flight control malfunctions were discovered at that time. He subsequently stated that he did not find any mechanical malfunctions or failures during a post-accident examination. He further surmised that the design of the braking system was such that simultaneous application of the left and right side brake pedals by both pilots may have resulted in excessive brake pressure, and this may have been the reason the airplane nosed over so unexpectedly.

Aircraft

Registration
N15TE
Reported as
Ealand Charles Lionheart (NO SERIES)
Category
Airplane, amateur-built
Serial number
GA-LH-008
Built
2006
Airframe hours
237
Engine
P&W R-985 SERIES, 450 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · September 9, 2013 · 1 hours before
Departed
SBP · San Luis Obispo, CA
Destination
SMX · Santa Maria, CA
Airport
SMX · Santa Maria Pub/Capt G Allan H, runway 30, 8,004 × 150 ft, asphalt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew · 2

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
80
Injuries
Minor
Certificates
Flight instructor, Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, With waivers/limitations
Last flight review
March 31, 2012
Seat
Right
Restraint
4-point
Flight hours
30,000 total · 80 in this make and model
Role
Pilot
Age
73
Injuries
Minor
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, With waivers/limitations
Last flight review
February 1, 2014
Seat
Left
Restraint
4-point
Flight hours
18,007 total · 237 in this make and model · 16,143 as pilot in command · 4 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
310° at 5 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
73 °F, dew point 57 °F
Altimeter
29.89 inHg
Observed at
KSMX

Docket · 4

The files NTSB released with the investigation on November 19, 2014, on NTSB’s docket system: statements, records, photos and specialists’ reports. 4.2 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.