Plane Crash List

Piper PA-28-161 N91338

20 July 1987 · Milpitas, California, United States · Minor injuries

Summary

On 20 July 1987 at about 19:30 local time, a Piper PA-28-161 registered N91338, operated by Flying Country Club, Inc., was involved in an accident near Milpitas, California, United States. One person was on board and one had minor injuries. The aircraft was substantially damaged. No probable cause statement is available for this record.

The record

Date
at 19:30
Classification
Accident
Location
Milpitas, California, United States
Nearest airport
Reid Hillview (RHV)
Coordinates
37.4397, -121.8697
Aircraft
Piper PA-28-161
Registration
N91338
Category
Airplane
Engines
1
Operator
Flying Country Club, Inc.
Operating rule
Part 91: General Aviation
Purpose of flight
Instructional
Phase of flight
Not recorded
Route
San Jose → Concord
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
LAX87LA275

People

1 person had minor injuries.

On board Died Serious Minor Uninjured
1 0 0 1 0

Probable cause

The NTSB has not published a probable cause for this record. No probable cause statement is present in the source data.

Nothing about the cause is stated here that is not in the source record.

Read the full NTSB narrative

WHILE CLIMBING TO CRUISE PLT HEARD A LOUD KNOCKING NOISE FOLLOWED BY 'VIOLENT VIBRATIONS' & A LOSS OF POWER. PLT MADE A FRCD LNDING IN A NEWLY EXCAVATED CONSTRUCTION SITE & WENT OVER AN EMBANKMENT. INVES REVEALED DEFORMATION OF THE #4 CYLINDER VALVE COVER. #4 EXHAUST VALVE ROCKER ARM WAS FOUND TO BE BROKEN. REVIEW OF ACFT MAINTENANCE RECORDS REVEALED THAT AD 87-10-06 WHICH INCORPORATES LYCOMING SERVICE BULLETIN (SB) 477A WAS ACCOMP 78.7 HRS PRIOR TO THE ACCIDENT. THE SB REQUIRES ROCKER ARMS THAT DO NOT HAVE A WALL THICKNESS OF.075 BE REPLACED. IF THE ROCKER ARM PASSES THE THICKNESS EXAM THE ROCKER ARM OIL DRIP HOLE OUTER EDGE MUST BE 'BURRED' TO THE APPROX .030 RADIUS PRIOR TO REASSEMBLY. THE ROCKER ARM WAS MEASURED USING A ROUND ANVIL MICROMETER. THE MEASUREMENT MET THE MIN DIMENSION OF .075. AFTER THE ACCIDENT, MET LAB EXAM REVEALED FRACTURE FEATURES OF HIGH CYCLE FATIGUE & OVERSTRESS. THE ORIGIN OF THE FATIGUE WAS TRACED TO THE REWORKED OIL DRIP HOLE WHICH DID NOT MEET .030 RADIUS. THE WALL THICKNESS MEASURED .055 USING A MEASURING MICROSCOPE.

Quoted verbatim from the NTSB record.

Other Piper PA-28 accidents

Date Aircraft Location Operator Outcome Died
20 Mar 1987 Piper PA-28-140
N726FL
Miami, Florida, United States - Fatal 2
4 Aug 1987 Piper PA-28-161
N8363H
N. Andover, Massachusetts, United States
no coordinates
- No injuries -
7 Nov 1987 Piper PA-28-161
N8253E
Detroit, Michigan, United States - No injuries -
4 Aug 1987 Piper PA-28
N33791
Prospectville, Pennsylvania, United States - No injuries -
17 Apr 1987 Piper PA-28-181
N6505C
Florida City, Florida, United States American Aviation, Inc. Fatal 1
14 Nov 1987 Piper PA-28-181
N47622
Manitowoc, Wisconsin, United States - No injuries -

All 9,402 records for this type

Other accidents in this area

Date Aircraft Location Operator Outcome Died
1 Nov 1987 Durbin MONNETT MONI
N190PJ
Ramona, California, United States Lipner, Robert M. Serious injuries -
24 Dec 1987 Bede BD-5
N29DT
Chula Vista, California, United States
no coordinates
Teufel, Armin U. Fatal 1
25 Oct 1987 Stits ELKINS 85
N72P
Camarillo, California, United States - Fatal 1
21 Nov 1987 Isgrigg ELITE
N333JE
Tehachapi, California, United States Isgrigg, John Minor injuries -
27 Dec 1987 Rolladen-Schneider LS-3
N75FE
Santa Ynez, California, United States - Serious injuries -
1 Jan 1987 Cessna 152
N5540H
San Dimas, California, United States King Aviation Minor injuries -

All 170,864 records in United States