GAA16CA106

NTSB accident investigation · Piper PA 28RT-201 · Terrell, TX · January 19, 2016

Accident · No injuriesData collectionFinal report
Date
January 19, 2016, 11:15 local (17:15 UTC)
Place
Terrell, TX
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N2119NPiper PA 28RT-201
Defining event
Approach-VFR go-around: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed · report April 5, 2016
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
North Texas FSDO (FAA)
FAA report
20160119004169A
Case key
92602

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 private pilot's exceedance of the airplane's critical angle-of-attack during a go-around in gusting crosswind conditions, which resulted in an aerodynamic stall and a collision with terrain short of the runway.

Findings · 7

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.

Use of equip/info: aircraft controlPersonnel issues › Task performance · Student/instructed pilotPiper PA-28RT-201: 4 casesAll aircraft: 9,295 casesProbable cause
Performance/control parameters: climb rateAircraft › Aircraft oper/perf/capability · Not attained/maintainedPiper PA-28RT-201: 1 caseAll aircraft: 265 casesProbable cause
Performance/control parameters: angle of attackAircraft › Aircraft oper/perf/capability · Capability exceededPiper PA-28RT-201: 1 caseAll aircraft: 990 casesProbable cause
Action: delayed actionPersonnel issues › Action/decision · Instructor/check pilotPiper PA-28RT-201: 1 caseAll aircraft: 894 casesProbable cause
Wind: variable windEnvironmental issues › Conditions/weather/phenomena · Effect on operationPiper PA-28RT-201: 1 caseAll aircraft: 113 cases
Wind: gustsEnvironmental issues › Conditions/weather/phenomena · Effect on operationPiper PA-28RT-201: 1 caseAll aircraft: 1,199 cases
Object/animal/substance: tree(s)Environmental issues › Physical environment · Effect on operationPiper PA-28RT-201: 1 caseAll aircraft: 933 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 flight instructor reported that the private pilot receiving instruction was flying a simulated engine failure approach to an airport in gusty crosswind conditions. When the airplane approached 50 feet above the ground on final, the flight instructor called "go-around." He reported that the instructed pilot "simultaneously pulled back and went full throttle." The flight instructor stated that the airspeed was about 80 knots, and "the airplane fell straight to the ground" short of the runway. After the impact, the airplane bounced forward onto the runway, the left main landing gear collapsed, and the airplane departed the runway to the left about 550 feet from the runway threshold. The flight instructor reported that he verified that the throttle was full forward before the impact. A postaccident examination revealed substantial damage to the right wing. The flight instructor reported there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation. According to the Federal Aviation Administration (FAA) Airport Facility Directory, trees were listed as an obstacle for the runway used. About the time of the accident, 7 nautical miles southeast of the airport, an automated weather observing system reported wind from 190 true at 13 knots, gusting to 21 knots. The tree line was located upwind and parallel to the airplane's final approach. The FAA Pilot's Handbook of Aeronautical Knowledge describes effects of obstructions on wind. The handbook states, "It is especially important to be vigilant when flying in or out of airports that have large buildings or natural obstructions located near the runway." The handbook further states, "During the landing phase of flight, an aircraft may 'drop in' due to the turbulent air and be too low to clear obstacles during the approach."

Factual narrative

The flight instructor reported that the private pilot receiving instruction was flying a simulated engine failure approach to an airport in gusty crosswind conditions. When the airplane approached 50 feet above the ground on final, the flight instructor called "go-around." He reported that the instructed pilot "simultaneously pulled back and went full throttle." The flight instructor stated that the airspeed was about 80 knots, and "the airplane fell straight to the ground" short of the runway. After the impact, the airplane bounced forward onto the runway, the left main landing gear collapsed, and the airplane departed the runway to the left about 550 feet from the runway threshold. The flight instructor reported that he verified that the throttle was full forward before the impact. A postaccident examination revealed substantial damage to the right wing. The flight instructor reported there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation. According to the Federal Aviation Administration (FAA) Airport Facility Directory, trees were listed as an obstacle for the runway used. About the time of the accident, 7 nautical miles southeast of the airport, an automated weather observing system reported wind from 190 true at 13 knots, gusting to 21 knots. The tree line was located upwind and parallel to the airplane's final approach. The FAA Pilot's Handbook of Aeronautical Knowledge describes effects of obstructions on wind. The handbook states, "It is especially important to be vigilant when flying in or out of airports that have large buildings or natural obstructions located near the runway." The handbook further states, "During the landing phase of flight, an aircraft may "drop in" due to the turbulent air and be too low to clear obstacles during the approach."

Aircraft

Registration
N2119N
Reported as
Piper PA 28RT-201 (T)
Category
Airplane
Serial number
28R-7918038
Built
1979
Engine
Lycoming IO-360, 201 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
J. Linn Aviation Inc
Registered owner
J. Linn Aviation Inc
Airworthiness certificate
Standard, Normal
Departed
HQZ · Mesquite, TX
Destination
HQZ · Mesquite, TX
Airport
1F7 · Airpark East, runway 13, 2,630 × 30 ft, asphalt
Equipment
Auto-pilot

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
Flight instructor
Age
38
Injuries
None
Certificates
Commercial, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Without waivers/limitations
Last flight review
June 1, 2014
Seat
Right
Restraint
3-point
Flight hours
6,300 total · 500 in this make and model · 5,500 as pilot in command · 150 in the last 90 days · 40 in the last 30 days · 1.6 in the last 24 hours
Role
Student pilot
Age
19
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land, Multi-engine land
Medical
Class 3, Without waivers/limitations
Seat
Left
Restraint
3-point
Flight hours
300 total · 3 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
190° at 13 knots, gusting 21
Visibility
10 statute miles
Temperature
59 °F, dew point 46 °F
Altimeter
30.17 inHg
Turbulence
Light
Observed at
KTRL, 7 nm away

Docket · 6

The files NTSB released with the investigation on March 18, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 9.4 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.