ERA14CA270

NTSB accident investigation · Wonder Michael S Harmon Rocket · Winston Salem, NC · May 21, 2014

Accident · No injuriesData collectionFinal report
Date
May 21, 2014, 12:25 local (16:25 UTC)
Place
Winston Salem, NC
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N85TPWonder Michael S Harmon Rocket
Defining event
Landing-landing roll: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed · report July 30, 2014
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20140521007629A
Case key
89313

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 failure to maintain directional control during landing in a gusty crosswind which resulted in a runway excursion and collision with terrain.

Findings · 4

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.

Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Not attained/maintainedWonder Michael S HARMON ROCKET: 1 caseAll aircraft: 3,958 casesProbable cause
Wind: crosswindEnvironmental issues › Conditions/weather/phenomena · Effect on operationWonder Michael S HARMON ROCKET: 1 caseAll aircraft: 1,008 cases
Wind: gustsEnvironmental issues › Conditions/weather/phenomena · Effect on operationWonder Michael S HARMON ROCKET: 1 caseAll aircraft: 1,199 cases

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

According to the pilot's written statement, while on approach for a straight in landing to runway 33 the tower reported "winds at 250 at 13 or 14 with gusts." The pilot elected to abandon the approach to runway 33 and requested a landing on runway 22. The pilot entered a left downwind for runway 22. On final approach the pilot stated he saw a quartering right crosswind at 18 to 19 knots on his onboard system. Upon touchdown the aircraft "began a weathervane" and the pilot elected to go around. After circling the airport the pilot attempted another approach to runway 22. On this approach the pilot used partial flaps and lined up on the left side of the runway. The pilot stated that upon touchdown the aircraft required almost full left rudder to maintain directional control. The pilot stated that he believed he "got an additional right wind gust." At that time the aircraft swerved sharply to the right where it exited the paved surface and rolled onto the grass. The airplane sustained substantial damage to the engine mount and left wing. The calculated cross wind component at the time of the accident, using the AWOS reported winds, was 13 knots. The pilot reported no preimpact mechanical malfunctions or anomalies that would have precluded normal operation.

Factual narrative

According to the pilot's written statement, while on approach for a straight in landing to runway 33 the tower reported "winds at 250 at 13 or 14 with gusts." The pilot elected to abandon the approach to runway 33 and requested a landing on runway 22. The pilot entered a left downwind for runway 22. On final approach the pilot stated he saw a quartering right crosswind at 18 to 19 knots on his onboard system. Upon touchdown the aircraft "began a weathervane" and the pilot elected to go around. After circling the airport the pilot attempted another approach to runway 22. On this approach the pilot used partial flaps and lined up on the left side of the runway. The pilot stated that upon touchdown the aircraft required almost full left rudder to maintain directional control. The pilot stated that he believed he "got an additional right wind gust." At that time the aircraft swerved sharply to the right where it exited the paved surface and rolled onto the grass. The airplane sustained substantial damage to the engine mount and left wing. The calculated cross wind component at the time of the accident, using the AWOS reported winds, was 13 knots. The pilot reported no preimpact mechanical malfunctions or anomalies that would have precluded normal operation.

Aircraft

Registration
N85TP
Reported as
Wonder Michael S Harmon Rocket
Category
Airplane, amateur-built
Serial number
2828
Built
1996
Airframe hours
942
Engine
Lycoming IO-540B4B5, 260 hp, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · July 30, 2013 · 67 hours before
Departed
SSI · Saint Simons, GA
Destination
INT · Winston Salem, NC
Flight plan
IFR
Airport
INT · Smith Reynolds Airport, runway 22, 3,938 × 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

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
66
Injuries
None
Certificates
Flight instructor, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Without waivers/limitations
Last flight review
February 27, 2013
Seat
Front
Restraint
3-point
Flight hours
6,540 total · 444 in this make and model · 6,100 as pilot in command · 75.4 in the last 90 days · 27.5 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
280° at 5 knots, gusting 17
Visibility
10 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 57 °F
Altimeter
30.07 inHg
Observed at
INT

Docket · 5

The files NTSB released with the investigation on June 26, 2014, on NTSB’s docket system: statements, records, photos and specialists’ reports. 5.3 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.

Other investigations on N85TP · 1

Matched to the same aircraft by N-number and date.