LAX97LA005

NTSB accident investigation · North American F-86 · Salinas, CA · October 6, 1996

Accident · No injuriesLimited investigationFinal report
Date
October 6, 1996, 11:45 local (18:45 UTC)
Place
Salinas, CA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N186SENorth American F-86
Weather
Visual (VMC) · Day
Status
Completed · report September 30, 1997
Report
Approved by Office Director
FAA report
19961006030939A
Case key
29653

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

an internal failure of a hydraulic pump, which resulted in contamination in the hydraulic system and subsequent loss of the braking system. Factors related to the accident included the proximity of a fence and rough/uneven terrain adjacent to the runway.

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.

Airframe/component/system failure/malfunctionLanding - roll
Hydraulic system,auxiliary pump - failureCause
Hydraulic system - contamination,other than waterCause
Landing gear,normal brake system - inoperativeCause
OverrunLanding - roll
On ground/water collision with objectLanding - roll
Object - fenceFactor
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - rough/unevenFactor

Analysis

During an air show, the pilot made several uneventful flybys, then landed near the beginning of the runway. During rollout, the pilot noted a hydraulic brake system failure. Unable to stop with only unboosted brakes, the airplane overran the departure end of the 5,005 foot runway and collided with a fence and rough terrain. Investigation revealed the engine driven #3 system auxiliary hydraulic boost pump had failed internally. Metal particles were found in its screen.

Factual narrative

On October 6, 1996, at 1145 hours Pacific daylight time, a North American F-86, N186SE, landed in the touchdown zone on runway 26 during an air show at the Salinas Municipal Airport, Salinas, California. The pilot reported that during rollout he experienced hydraulic brake system failure. The airplane overran the departure end of the 5,005-foot-long runway and collided with a fence and rough terrain which resulted in substantial airframe damage. The airline transport pilot was not injured. Visual meteorological conditions prevailed. The flight originated from Salinas at 1135.

According to the pilot, during the flight he had performed several flybys without incident. On final approach the airplane lost all utility hydraulic pressure. During rollout he shut down, but was unable to stop with the unboosted brakes.

The FAA coordinator reported its investigation revealed that the engine driven No. 3 system auxiliary hydraulic boost pump internally failed. Metal particles were found in its screen.

Aircraft

Registration
N186SE
Reported as
North American F-86
Category
Airplane
Serial number
001
Engine
GE J47-27, 6,010 lbs thrust, turbo jet
Damage
Substantial damage
Flight
Part 91
Operator
Clyde S. Eberhardt
Registered owner
Stuart & Marilyn Eberhardt
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · August 12, 1996 · 7 hours before
Departed
SNS
Airport
SNS · Salinas Municipal, runway 26, 5,005 × 150 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
60
Certificates
Airline transport, Flight engineer, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Front
Flight hours
27,043 total · 435 in this make and model · 16,183 as pilot in command · 25 in the last 90 days · 18 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 5 knots
Visibility
50 statute miles
Lowest ceiling
None
Temperature
72 °F, dew point 55 °F
Altimeter
30.00 inHg
Observed at
SNS, 1 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.