Aviation Crash Map

De Havilland DHC-6-100 N121PM

9 December 1990 · Perris Valley, California, United States · Minor injuries

Summary

On 9 December 1990 at about 22:00 local time, a De Havilland DHC-6-100 registered N121PM, operated by One Papa Mike Corp., was involved in an accident near Perris Valley, California, United States. 21 people were on board and one had minor injuries. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 22:00
Classification
Accident
Location
Perris Valley, California, United States
Nearest airport
Perris Valley (L65)
Coordinates
Not recorded
Aircraft
De Havilland DHC-6-100
Registration
N121PM
Category
Airplane
Engines
2
Operator
One Papa Mike Corp.
Operating rule
Part 91: General Aviation
Purpose of flight
Unknown
Phase of flight
Not recorded
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
LAX91FA052

People

1 person had minor injuries.

On board Died Serious Minor Uninjured
21 0 0 1 20

Probable cause

A LOSS OF POWER ON THE LEFT ENGINE DUE TO A FATIGUE FAILURE OF A COMPRESSOR TURBINE BLADE LEADING TO FURTHER COMPRESSOR BLADE DAMAGE; A WORN POWER TURBINE GOVERNOR THROTTLE CAM ASSEMBLY WHICH LED TO LOSS OF POWER ON THE RIGHT ENGINE; AND INADEQUATE MAINTENANCE AND INSPECTION BY THE OPERATOR.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

AFTER LIFT-OFF, AT ABOUT 100 FT AGL AND 85 KTS, THE LEFT ENG DECELERATED AND THE AIRPLANE BEGAN TO YAW AND ROLL LEFT. THE PIC ABORTED THE TAKEOFF, TURNED LEFT AND LANDED ON A FLAT LEVEL FIELD. THE AIRPLANE STRUCK A FENCE, THEN TREES. EXAMINATION OF THE LEFT ENG REVEALED THE LOSS OF POWER WAS ATTRIBUTED TO A FATIGUE FRACTURE OF A COMPRESSOR TURBINE BLADE, WHICH LED TO SUBSEQUENT BLADE FRACTURES. THE RIGHT ENG WAS EXAMINED AND FOUND TO HAVE ADVANCE WEAR ON THE THROTTLE CAM ASSEMBLY OF THE POWER TURBINE GOVERNOR. IN A TEST CELL, ONLY APRX 28% OF TAKEOFF POWER COULD BE ACHIEVED. THE CAM LOBE WEAR HAD PROGRESSED OVER AN EXTENDED PERIOD OF TIME. THE RIGHT ENGINE PROP GOVERNOR WAS REPLACED 11/18/90, FOLLOWED BY A TEST RUN.

Quoted verbatim from the NTSB record.

Other De Havilland DHC-6 accidents

Date Aircraft Location Operator Outcome Died
29 Mar 1990 De Havilland DHC-6
N200EH
Chevak, Alaska, United States - No injuries -
27 Sep 1989 De Havilland DHC-6-300
N75GC
Grand Canyon, Arizona, United States - Fatal 10
29 Oct 1989 De Havilland DHC-6-300
N707PV
Halawa, Molokai, Hawaii, United States
no coordinates
- Fatal 20
19 Sep 1989 De Havilland DHC-6
N851TB
Sleepy Bay, Alaska, United States
no coordinates
Sound Adventures No injuries -
14 Apr 1989 De Havilland DHC-6-100
N100AP
Barrow, Alaska, United States - No injuries -
26 Oct 1991 De Havilland DHC-6
N724CA
Chevak, Alaska, United States Markair Express Inc. No injuries -

All 133 records for this type

Other accidents in this area

Date Aircraft Location Operator Outcome Died
15 Apr 1990 Cessna 180
N9394C
Soledad, California, United States - No injuries -
10 Oct 1990 Cessna 150
N68350
Riverside, California, United States PAR Flight No injuries -
17 Apr 1990 Piper PA46
N4387S
Paso Robles, California, United States Piper Aircraft Corp. No injuries -
7 Oct 1990 Cessna 182M
N70892
Bakersfield, California, United States - No injuries -
1 Apr 1990 Piper J-3
N7363H
Creston, California, United States - Minor injuries -
11 Oct 1990 Bell 47G4
N477JM
Merced, California, United States John W. Myers Serious injuries -

All 170,864 records in United States