GAA16CA382

NTSB accident investigation · Gonzalez Manuel A RV 7 · Langley, WA · July 16, 2016

Accident · Minor injuriesData collectionFinal report
Date
July 16, 2016, 15:00 local (22:00 UTC)
Place
Langley, WA
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N228MGGonzalez Manuel A RV 7
Defining event
Landing-landing roll: Runway excursion
Weather
Visual (VMC) · Day
Status
Completed · report December 5, 2016
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA
FAA report
20160716006649A
Case key
93628

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 decision to land with a tailwind, which resulted in, landing long, a runway overrun, and impact with a berm and nose over.

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.

Performance/control parameters: descent/approach/glide pathAircraft › Aircraft oper/perf/capability · Not attained/maintainedGonzalez Manuel A RV-7A: 1 caseAll aircraft: 809 casesProbable cause
Wind: tailwindEnvironmental issues › Conditions/weather/phenomena · Effect on operationGonzalez Manuel A RV-7A: 1 caseAll aircraft: 594 cases
Terrain: mountainous/hilly terrainEnvironmental issues › Physical environment · Contributed to outcomeGonzalez Manuel A RV-7A: 1 caseAll aircraft: 329 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

The pilot of a tailwheel equipped airplane reported that due to the tall trees that surrounded the airport he elected to land to the north with a tailwind because of "less tree obstacles". He further reported that the airplane "touched down too far down the runway". He attempted to stop the airplane from over running the runway, but was unsuccessful. The airplane over ran the runway, impacted a grass berm, and nosed over. The airplane sustained substantial damage to the empennage. According to the pilot there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The Federal Aviation Administration has published the Advisory Circular (AC) 91-79A. This AC discusses the hazards associated with runway overruns and the effect of a tailwind on landing distance and states in part: The pilot must be aware of airspeed during the approach and of the targeted reference landing airspeed (VREF)/airspeed, plus wind gust adjustments, over the runway threshold. An excessive approach speed may result in an excessive speed over the runway's threshold, which may result in landing beyond the intended touchdown point as well as a higher speed from which the pilot must bring the airplane to a stop. The effect of a tailwind on landing distance is significant and is a factor in determining the landing distance required. Given the airplane will land at a particular airspeed, independent of the wind, the principal effect of a tailwind on operational landing distance is the change in the ground speed at which the airplane touches down.

Factual narrative

The pilot of a tailwheel equipped airplane reported that due to the tall trees that surrounded the airport he elected to land to the north with a tailwind because of "less tree obstacles". He further reported that the airplane "touched down too far down the runway". He attempted to stop the airplane from over running the runway, but was unsuccessful. The airplane over ran the runway, impacted a grass berm, and nosed over. The airplane sustained substantial damage to the empennage. According to the pilot there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The Federal Aviation Administration has published the Advisory Circular (AC) 91-79A. This AC discusses the hazards associated with runway overruns and the effect of a tailwind on landing distance and states in part: The pilot must be aware of airspeed during the approach and of the targeted reference landing airspeed (VREF)/airspeed, plus wind gust adjustments, over the runway threshold. An excessive approach speed may result in an excessive speed over the runway's threshold, which may result in landing beyond the intended touchdown point as well as a higher speed from which the pilot must bring the airplane to a stop. The effect of a tailwind on landing distance is significant and is a factor in determining the landing distance required. Given the airplane will land at a particular airspeed, independent of the wind, the principal effect of a tailwind on operational landing distance is the change in the ground speed at which the airplane touches down.

Aircraft

Registration
N228MG
Reported as
Gonzalez Manuel A RV 7 (A)
Category
Airplane, amateur-built
Serial number
71045
Built
2005
Airframe hours
465.4
Engine
Lycoming IO-360, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · March 8, 2016
Departed
AWO · Arlington, WA
Destination
W10 · Langley, WA
Airport
W10 · Whidbey Air Park, runway 34, 2,470 × 25 ft, asphalt
Equipment
Electronic primary flight display, Electronic multifunction display, Auto-pilot, ADS-B, Satellite tracking device, Onboard weather, Handheld GPS

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
76
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, With waivers/limitations
Last flight review
April 15, 2015
Seat
Left
Restraint
5-point
Flight hours
2,498 total · 465 in this make and model · 2,948 as pilot in command · 15 in the last 90 days · 2 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 6 knots
Visibility
10 statute miles
Lowest ceiling
7,500 ft overcast
Temperature
66 °F, dew point 52 °F
Altimeter
30.07 inHg
Observed at
KPAE, 9 nm away

Docket · 2

The files NTSB released with the investigation on October 19, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.2 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.