SEA01LA153

NTSB accident investigation · Let Blanik L-13 · Enumclaw, WA · August 19, 2001

Accident · Serious injuriesLimited investigationFinal report
Date
August 19, 2001, 12:35 local (19:35 UTC)
Place
Enumclaw, WA
Injuries
1 serious, 1 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N82ASLet Blanik L-13
Weather
Visual (VMC) · Day
Status
Completed · report June 3, 2002
Report
Approved by Office Director
Parties
FAA - FSDO
FAA report
20010819023969A
Case key
53083

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 premature release of the towline and the pilot's improper selection of a landing area following the release. Factors include improper preflight planning.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Miscellaneous/otherTakeoff - initial climb
Glider launch/tow equipment - unlatchedCause
Loss of control - in flightManeuvering - turn to landing area (emergency)
Unsuitable terrain or takeoff/landing/taxi area - improperPilot in commandCause
Preflight planning/preparation - improperPilot in commandFactor

Analysis

The glider pilot reported that the towline prematurely released from the tow plane (Piper PA-18). He reported that this occurred shortly after takeoff from runway 28, about 200 feet above ground level (AGL). After the unscheduled disconnect, the glider pilot initiated a turn to the right in an effort to reach the departure runway. He reported that during the turn, the glider "pitched down" and did not respond to control inputs. Shortly thereafter, the glider impacted trees and terrain. This was the second failed attempt to launch the glider; the first attempt resulted in an unscheduled release immediately following the initiation of the tow. Following the first unscheduled release, the "Field Manager" reconnected to towline to the PA-18, and the second tow was initiated. In both cases, the towline prematurely released from the release hook on the tow aircraft, but remained attached to the latching mechanism on the glider. The handle for the tow-hitch is located on the floorboard of the tow plane's forward cockpit. To open the hitch, the handle is moved from the forward position to the aft position. According to the tow plane pilot, the handle had not been actuated and was in the forward position when the unscheduled releases occurred. Postaccident examination and testing of the tow-hitch revealed no discrepancies or anomalies that would explain the unscheduled release. In a written statement, the glider pilot indicated that he had not been briefed on potential emergency landing sites near the departure field. Additionally, he stated that had he been briefed, he would have "...made the decision to fly to such a site given my altitude at release." The elevation at Bergseth Field is approximately 1,100 feet mean sea level (MSL). Runway 10/28 is a 2,100 by 60 foot turf runway, with rising terrain to the east and sloping terrain to the west The terrain to the west slopes down to an elevation of approximately 500 feet MSL.

Factual narrative

On August 19, 2001, about 1235 Pacific daylight time, a LET Blanik L-13 glider, N82AS, sustained substantial damage during a forced landing at a private airstrip near Enumclaw, Washington. The glider is registered to Puget Sound Soaring Association, Kent, Washington, and was being operated as a visual flight rules (VFR) personal/pleasure flight under the provisions of Title 14, CFR Part 91. The private pilot sustained minor injuries and his passenger sustained serious injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the local flight. The flight originated from Bergseth Field shortly before the accident.

In a written statement dated September 4, 2001, the pilot of the glider reported that the towline prematurely released from the tow plane (Piper PA-18). The report indicated this occurred shortly after takeoff from runway 28, about 200 feet above ground level (AGL). After the unscheduled disconnect, the pilot initiated a turn to the right in an effort to reach the departure runway. He reported that during the turn, the glider "pitched down" and did not respond to control inputs. Shortly thereafter, the glider impacted trees and terrain. In his written statement, the pilot indicated that he had not been briefed on potential emergency landing sites near the departure field. Additionally, he stated that had he been briefed, he would have "...made the decision to fly to such a site given my altitude at release."

This was the second failed attempt to launch the glider; the first attempt resulted in an unscheduled release immediately following the initiation of the tow. Following the first unscheduled release, the "Field Manager" reconnected the towline to the PA-18, and the second tow was initiated. In both cases, the towline prematurely disconnected from the release hook on the tow aircraft, but remained attached to the latching mechanism on the glider.

The elevation at Bergseth Field is approximately 1,100 feet mean sea level (MSL). Runway 10/28 is a 2,100 by 60 foot turf runway, with rising terrain to the east and sloping terrain to the west. The terrain to the west slopes down to an elevation of approximately 500 feet MSL.

The handle for the release hook is located on the floorboard of the tow plane's forward cockpit. To open the tow-hitch, the handle is moved from the forward position to the aft position. According to the tow plane pilot, the handle had not been actuated and was in the forward position when the unscheduled releases occurred.

A review of the maintenance records indicated that the Schweizer Aircraft tow-hitch was installed on the tow airplane on September 4, 1999. A representative from the Puget Sound Soaring Association reported that between September 12, 1999, and September 19, 2001, approximately 705 tow cycles were completed without previous incidents.

Postaccident examination and testing of the tow-hitch revealed no discrepancies or anomalies that would explain the unscheduled release.

Aircraft

Registration
N82AS
Reported as
Let Blanik L-13
Category
Glider
Serial number
026651
Airframe hours
2,643
Engine
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Puget Sound Soaring
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 2, 2001
Departed
WN76 · Enumclaw, WA
Destination
WN76 · Enumclaw, WA
Airport
WN76 · Bergseth Field, runway 27, 2,100 × 60 ft, grass/turf

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
58
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Last flight review
July 7, 2000
Seat
Rear
Flight hours
450 total

Weather

Conditions
Visual (VMC) · Day
Wind
302° at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
63 °F, dew point 52 °F
Altimeter
30.19 inHg
Observed at
SEA, 287 nm away

Docket · 4

The files NTSB released with the investigation on January 23, 2026, on NTSB’s docket system: statements, records, photos and specialists’ reports. 701 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.

Other investigations on N82AS · 1

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