N3333P

Substantial
Serious

PIPER PA-23-160 S/N: 23-1284

Accident Details

Date
Thursday, May 27, 1993
NTSB Number
CHI93LA184
Location
ELY, MN
Event ID
20001211X12363
Coordinates
47.900753, -91.849716
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
2
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

the pilot's decision to continue flight with a known deficiency in the airplane's hydraulic system. Factors associated with the accident are the loss of power in the left engine due to fuel contamination, and a leak in the hydraulic system.

Aircraft Information

Registration
N3333P
Make
PIPER
Serial Number
23-1284
Engine Type
Reciprocating
Model / ICAO
PA-23-160 PA23
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
CRYSTAL SHAMROCK INC
Address
6000 DOUGLAS DRIVE NORTH
Status
Deregistered
City
MINNEAPOLIS
State / Zip Code
MN 55429
Country
United States

Analysis

On May 27, 1993, about 1320 central daylight time, a Piper PA-23-160 airplane, N3333P, operated by Crystal Shamrock, Inc., sustained substantial damage when it collided with trees approximately four miles north of Ely, Minnesota. The commercial pilot and the sole passenger aboard were seriously injured. The flight departed Hallock, Minnesota about 1100, with an intended destination of Cook County Airport, Grand Marias, Minnesota. Instrument meteorological conditions prevailed for 14 CFR Part 91 flight, and an instrument flight plan was filed.

The pilot reported a relatively slow loss of power from the left engine while in cruise at 7,000' MSL. He said the power loss developed over several seconds. The pilot wrote in his report to the NTSB that he feathered the left engine and made a diversion to Ely, Minnesota. He was unable to maintain altitude, and complained of excessive drag from an unknown source on the airplane. He wrote that it became apparent that the airplane would not reach Ely due to his inability to maintain altitude, and he elected to make a forced landing into the tree tops.

During the flight, the pilot said the main landing gear kept creeping down and he had to keep "snugging" it up by putting the gear handle in the up position. Once the left engine ceased to run, he said he used the emergency hydraulic hand pump to accomplish the same task. According to the pilot's written statement, he was aware of the sagging gear problem prior to the flight, and that it was necessary for him to bring the gear up every 3 to 5 minutes. He said that the main landing gear system apparently had a slow leak, and it was scheduled for repair soon. He also wrote: "In retrospect, I believe this seemingly minor problem may have been of critical significance in causing this accident. I think given a few more seconds of time, I may have been able to recognize this as the source of drag and eliminate it and avoid the crash-landing."

The airplane's left engine was examined in the field by an FAA inspector. His report (appended) notes that all of the left engine spark plugs were very blackened, and that the fuel sample taken between the fuel pump and carburetor was dirty and watery.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI93LA184