DEN88FA033

NTSB accident investigation · Piper PA-28R-200 · San Jose, CA · December 5, 1987

Accident · FatalField investigationFinal report
Date
December 5, 1987, 09:55 local (17:55 UTC)
Place
San Jose, CA
Injuries
3 fatal, 1 serious
Damage
Destroyed
Phase of flight
Approach
Aircraft
N9309NPiper PA-28R-200
Weather
Visual (VMC) · Day
Status
Completed · report March 31, 1989
Report
Approved by Office Director
FAA report
19871205069159A
Case key
17343

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

On this page

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/malfunctionGo-around (vfr)
Lubricating system - leakCause
Fluid,oil - pressure too lowCause
Precautionary landing - initiated
Loss of engine power(total) - mech failure/malfGo-around (vfr)
Weather condition - tailwindFactor
Airspeed - excessivePilot in commandFactor
Proper touchdown point - not attainedPilot in commandFactor
Go-around - attemptedPilot in command
Fluid,oil - exhaustionCause
Engine assembly,connecting rod - failure,totalCause
In flight collision with objectLanding
Object - utility poleFactor
Object - residenceFactor

Analysis

Several min after takeoff, the plt noted a loss of oil pressure & elected to return to the arpt. As he was returning, the eng began to overspeed, but he controlled the RPM by retarding the throttle. The wind was from 150 deg at 10 KTS. The plt was clrd to enter traffic for rwy 13L, but he elected to land in the opposite direction with a tail wind. While on a short final apch to land on rwy 31R, the acft ballooned & the plt decided to go around. Drg the go-around, the eng lost power. Subsequently, the acft collided with a utility pole, then crashed into a multi-family dwelling & burned. Oil residue was fnd on the left side & bottom of the fuselage. A teardown of the eng revealed the #4 connecting rod had failed. Only about 1/2 pint of oil was fnd in the eng. Due to impact & fire damage, the reason for the loss of oil was not determined.

Aircraft

Registration
N9309N
Reported as
Piper PA-28R-200
Category
Airplane
Serial number
28R35009
Airframe hours
3,285
Engine
Lycoming IO-360-C1C, 200 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Personal · Part 91
Registered owner
Christopher J. Verbil
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 30, 1987 · 56 hours before
Departed
RHV
Destination
308 · Coalinga, CA
Flight plan
VFR
Airport
RHV · Reid-Hillview, runway 31R, 3,101 × 75 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
32
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
802 total · 105 in this make and model · 584 as pilot in command · 48 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
150° at 10 knots
Visibility
20 statute miles
Lowest ceiling
3,000 ft broken
Temperature
55 °F, dew point 48 °F
Altimeter
30.00 inHg
Observed at
RHV, 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.

Other investigations on N9309N · 2

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