GAA19CA387

NTSB accident investigation · Piper PA32 · Seldovia, AK · July 7, 2019

Accident · No injuriesData collectionFinal report
Date
July 6, 2019, 19:05 local (Jul 7, 2019, 03:05 UTC)
Place
Seldovia, AK
Injuries
5 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N3556WPiper PA32
Defining event
Takeoff: Collision during takeoff/land
Weather
Visual (VMC) · Day
Status
Completed · report May 21, 2020
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA
FAA report
20190706009339A
Case key
99779

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 attain a sufficient climb following a short-field takeoff, which resulted in collision with trees.

Findings · 3

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 · PilotPiper PA-32-260: 18 casesAll aircraft: 9,295 casesProbable cause
Object/animal/substance: tree(s)Environmental issues › Physical environment · Effect on operationPiper PA-32-260: 3 casesAll aircraft: 933 casesProbable cause
Performance/control parameters: climb rateAircraft › Aircraft oper/perf/capability · Not attained/maintainedPiper PA-32-260: 1 caseAll aircraft: 265 casesProbable cause

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 the airplane's gross takeoff weight was 300 lbs less than the maximum allowable takeoff weight. He performed a short-field takeoff from the 1,800-ft-long gravel surface, and the initial climb continued as expected. However, the climb performance then degraded and became insufficient to clear 80-ft-tall trees located about 1,000 ft from the departure end of the runway. The airplane collided with treetops, descended, and subsequently impacted a lake and became submerged. The airplane sustained substantial damage to the stabilator. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

Factual narrative

The pilot reported that the airplane's takeoff gross weight was 300 pounds less than the maximum. He performed a short-field takeoff from the 1,800ft gravel surface, and the initial climb continued as he expected. He recalled that the climb performance degraded and became insufficient to clear the 80ft tall trees located about 1,000ft from the departure end of the runway. The manufacturer's Pilot Operating Handbook (POH) stated that, short field takeoff's that require obstacle clearance will, after breaking ground accelerate to best angle of climb speed, 95 MPH and climb past obstacles. The airplane collided with treetops, descended and subsequently impacted the lake and became submerged. The airplane sustained substantial damage to the stabilator. Additionally, the POH denotes that the minimum runway distance required for the airplane to takeoff over a 50ft barrier was 1,360ft. According to the manufacturer, the minimum runway distance of 1,360ft represents a takeoff from a hard surface runway. Further, the POH specifies the use of a soft-field, obstacle clearance takeoff, as the increase flap setting of 25°, airspeed acceleration and pull nose gear off the ground as soon as possible and at the lowest possible airspeed. Accelerate just above the ground to best angle of climb speed, 95 MPH to climb past obstacle clearance height. Continue to climb while accelerating to best rate of climb, 105 MPH while slowly retracting flaps. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

Aircraft

Registration
N3556W
Reported as
Piper PA32 (260)
Category
Airplane
Serial number
32-444
Built
1966
Airframe hours
6,643.47
Engine
Lycoming O-540-E4B5, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · July 1, 2019
Departed
ASP · Seldovia, AK
Destination
AWS · Wasilla, AK
Airport
SOV · Seldovia, runway 34, 1,845 × 80 ft, gravel
Equipment
Handheld GPS, Stall warning system, Auto-pilot, Electronic flight bag or handheld device, Electronic multifunction display, Electronic primary flight display

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
54
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
BasicMed
Last flight review
August 3, 2018
Seat
Left
Restraint
3-point
Flight hours
1,229 total · 671 in this make and model · 1,194 as pilot in command · 27 in the last 90 days · 10 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
68 °F, dew point 55 °F
Altimeter
30.22 inHg
Observed at
PASO

Docket · 3

The files NTSB released with the investigation on December 5, 2019, 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.

Other investigations on N3556W · 1

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