GAA17CA526

NTSB accident investigation · Cessna 172 · Coolin, ID · September 10, 2017

Accident · Serious injuriesData collectionFinal report
Date
September 10, 2017, 14:44 local (21:44 UTC)
Place
Coolin, ID
Injuries
1 serious, 3 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N5703ACessna 172
Defining event
Initial climb: Loss of lift
Weather
Visual (VMC) · Day
Status
Completed · report November 27, 2017
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA/ FSDO
FAA report
20170910011269A
Case key
95979

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 take off in high-density altitude and gusting quartering tailwind conditions, which resulted in a loss of lift and an inability to gain altitude during the initial climb.

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.

Performance/control parameters: altitudeAircraft › Aircraft oper/perf/capability · Attain/maintain not possibleCessna 172: 8 casesAll aircraft: 1,310 casesProbable cause
Wind: tailwindEnvironmental issues › Conditions/weather/phenomena · Decision related to conditionCessna 172: 3 casesAll aircraft: 594 cases
Wind: crosswindEnvironmental issues › Conditions/weather/phenomena · Decision related to conditionCessna 172: 3 casesAll aircraft: 1,008 cases
Wind: gustsEnvironmental issues › Conditions/weather/phenomena · Decision related to conditionCessna 172: 2 casesAll aircraft: 1,199 cases
Temp/humidity/pressure: high density altitudeEnvironmental issues › Conditions/weather/phenomena · Decision related to conditionCessna 172: 1 caseAll aircraft: 278 cases
Object/animal/substance: tree(s)Environmental issues › Physical environment · Contributed to outcomeCessna 172: 8 casesAll 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 pilot reported that he completed a normal landing to the south at a grass airstrip near a lake that was surrounded by 75-ft-tall pine trees. He added that he and his passengers ate lunch at the airstrip, and during that time, he noticed "mostly calm" wind with an "occasional gust from the south." The pilot further reported that, due to the runway gradient, he decided to take off downhill to the north because the wind sock was indicating a calm wind. He reported that, during the soft field takeoff, the takeoff roll was normal, but that, about 100 ft above ground level, he noticed that the "climb had slowed" and the "airspeed was dropping." The pilot lowered the nose, the airplane "descended quickly," and then touched down on the runway with about 30 ft remaining. Subsequently, the airplane overran the runway, crossed a road, and impacted a dumpster and trees. The fuselage and both wings sustained substantial damage. The pilot reported that the airplane was 25 lbs under maximum gross weight. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. An automated weather observation station (AWOS) 13 nautical miles from the accident site, reported, about the time of the accident, wind from 240° at 6 knots. A review of four hourly AWOS recordings, south and east of the accident site, around the time of the accident, revealed that the wind was variable from the southwest to west at 5 to 10 knots, gusting 15 to 18 knots. The pilot reported that the takeoff was on runway 33. The calculated density altitude was 3,700 ft. According to the Federal Aviation Administration (FAA) density altitude Koch Chart, the airplane would have likely experienced a 32% decrease in the normal climb rate and a 50% increase in the normal takeoff distance. The FAA's Pilot's Handbook of Aeronautical Knowledge, FAA-H-8083-25B, contained a section titled, "Effect of Obstructions on Wind," which stated in part: "Another atmospheric hazard exists that can create problems for pilots. Obstructions on the ground affect the flow of wind and can be an unseen danger. Ground topography and large buildings can break up the flow of the wind and create wind gusts that change rapidly in direction and speed. These obstructions range from man-made structures, like hangars, to large natural obstructions, such as mountains, bluffs, or canyons. 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 intensity of the turbulence associated with ground obstructions depends on the size of the obstacle and the primary velocity of the wind. This can affect the takeoff and landing performance of any aircraft and can present a very serious hazard." It is likely that, during the initial climb in high-density altitude conditions, the airplane encountered a quartering tailwind gust as the airplane climbed above thetrees, which resulted in a loss of lift and an inability to gain altitude during the initial climb.

Factual narrative

The pilot reported that he completed a normal landing to the south at a grass airstrip, near a lake and surrounded by 75 ft. tall pine trees. He added that he and his passengers ate lunch at the airstrip, and during that time, he noticed "mostly calm" wind with an "occasional gust from the south." The pilot further reported that, due to the runway gradient, he decided to takeoff downhill to the north, as the wind sock was indicating a calm wind. During the soft field takeoff, he reported that the take-off roll was normal, but about 100 ft. above ground he noticed that the "climb had slowed" and the "airspeed was dropping." The pilot lowered the nose, the airplane "descended quickly," and touched down on the runway with about 30 ft. remaining. Subsequently, the airplane overran the runway, crossed a road, and impacted a dumpster and trees. The fuselage and both wings sustained substantial damage. The pilot reported that the airplane was 25 lbs. under maximum gross weight. The pilot did not report that there were any preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. An automated weather observation station (AWOS), about the time of the accident, 13 nautical miles from the accident site, reported wind from 240° at 6 knots. A review of four, hourly AWOSs, south and east of the accident site, around the time of the accident, recorded wind variable from the southwest to westerly direction, at 5 to 10 knots, gusting 15 to 18 knots. The pilot reported that the takeoff was on runway 33. The calculated density altitude was 3,700 ft. According to the Federal Aviation Administration density altitude Koch Chart, the airplane would have likely experienced a 32% decrease to the normal climb rate, and a 50% increase to the normal takeoff distance. The Federal Aviation Administration's Pilot's Handbook of Aeronautical Knowledge, FAA-H-8083-25B, contains a section titled "Effect of Obstructions on Wind" which stated in part: "Another atmospheric hazard exists that can create problems for pilots. Obstructions on the ground affect the flow of wind and can be an unseen danger. Ground topography and large buildings can break up the flow of the wind and create wind gusts that change rapidly in direction and speed. These obstructions range from man-made structures, like hangars, to large natural obstructions, such as mountains, bluffs, or canyons. 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 intensity of the turbulence associated with ground obstructions depends on the size of the obstacle and the primary velocity of the wind. This can affect the takeoff and landing performance of any aircraft and can present a very serious hazard."

Aircraft

Registration
N5703A
Reported as
Cessna 172 (UNDESIGNAT)
Category
Airplane
Serial number
28303
Built
1956
Airframe hours
2,810
Engine
Cont Motor O-300, 145 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 8, 2017
Departed
66S · Coolin, ID
Destination
SFF · Spokane, WA
Airport
66S · Cavanaugh Bay, runway 33, 3,100 × 120 ft, grass/turf
Equipment
Stall warning system, Electronic flight bag or handheld device

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
63
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, With waivers/limitations
Last flight review
April 5, 2016
Seat
Left
Restraint
4-point
Flight hours
325 total · 176 in this make and model · 289 as pilot in command · 21 in the last 90 days · 9 in the last 30 days · 3 in the last 24 hours
Role
Pilot-rated passenger
Age
71
Injuries
None
Certificate
Private
Last flight review
January 1, 1987
Seat
Right
Restraint
4-point
Flight hours
1,008 total · 115 in this make and model · 945 as pilot in command · 0 in the last 90 days · 0 in the last 30 days · 0 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
73 °F, dew point 37 °F
Altimeter
30.20 inHg
Observed at
KSZT, 16 nm away

Docket · 3

The files NTSB released with the investigation on November 6, 2017, on NTSB’s docket system: statements, records, photos and specialists’ reports. 888 KB 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.