LAX08CA003

NTSB accident investigation · Let Blanik L-13 · Hemet, CA · October 6, 2007

Accident · No injuriesData collectionFinal report
Date
October 6, 2007, 14:00 local (21:00 UTC)
Place
Hemet, CA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N510CSLet Blanik L-13
Weather
Visual (VMC) · Day
Status
Completed · report November 29, 2007
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20071006823839A
Case key
66854

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The pilot's failure to maintain a proper descent rate due to his failure to close the air brake and/or partially retract the flaps during an encounter with lost lift on final approach.

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.

In flight collision with objectApproach - vfr pattern - final approach
Object - fence
Proper descent rate - not maintainedPilot in commandFactor
Speed brakes - improper use ofPilot in commandCause
Raising of flaps - not performedPilot in commandCause

Analysis

The pilot encountered a loss of lift during the latter part of the pattern and subsequently collided with the airport boundary fence on final approach. The pilot stated that during the downwind leg, he partially deployed the flaps, and partially opened the air brake. He encountered a significant loss of lift on the final leg, but could not recall whether he closed the air brake. A photograph taken immediately after the accident by the pilot's flight instructor showed the air brake to be open, with the flaps deployed. The pilot was checked out by his flight instructor to fly the L-13 glider earlier that day. The accident flight was his first solo flight in this glider type.

Factual narrative

On October 6, 2007, about 1400 Pacific daylight time, a LET Blanik L-13, N510CS, collided with an airport boundary fence during final approach near Hemet, California. Orange County Soaring Association was operating the glider under the provisions of 14 CFR Part 91. The private pilot, the sole occupant, was not injured; the glider sustained substantial damage. The local area personal flight departed Hemet-Ryan Airport about 1300. Visual meteorological conditions prevailed, and no flight plan had been filed.

In a written report, the pilot stated that he encountered a significant loss of lift during the latter part of the pattern, and subsequently collided with the airport boundary fence.

An FAA investigator interviewed the pilot after the accident. The pilot stated that during the downwind leg, he partially deployed the flaps, and partially opened the air brake. He stated that he encountered a significant loss of lift on the final leg, but could not recall whether he closed the air brake.

A photograph taken immediately after the accident by the pilot's flight instructor showed the air brake to be open. The flaps were deployed.

The pilot was checked out by his flight instructor to fly the L-13 glider earlier that day. The accident flight was his first solo flight since the checkout.

Aircraft

Registration
N510CS
Reported as
Let Blanik L-13
Category
Glider
Serial number
025423
Airframe hours
1,975
Engine
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Orange County Soaring Association
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 1, 2007
Departed
HMT · Hemet, CA
Destination
HMT
Airport
HMT · Hemet-Ryan, runway 22, 2,045 × 25 ft, asphalt

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
None
Certificate
Private
Airplane ratings
Single-engine land
Last flight review
October 1, 2007
Seat
Front
Flight hours
1,263 total · 2 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
320° at 12 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
72 °F, dew point 39 °F
Altimeter
30.04 inHg
Observed at
RIV, 15 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.