N9410

Substantial
None

DEHAVILLAND TIGER MOTH DH 82AS/N: DE-941

Accident Details

Date
Saturday, December 12, 2015
NTSB Number
ERA16LA065
Location
Modena, NY
Event ID
20151214X04724
Coordinates
41.662776, -74.074447
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A partial loss of engine power due to a stuck No. 1 cylinder exhaust valve.

Aircraft Information

Registration
Make
DEHAVILLAND
Serial Number
DE-941
Engine Type
Reciprocating
Year Built
1940
Model / ICAO
TIGER MOTH DH 82ADH82
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
TIGER MOTH DH 82A

Registered Owner (Current)

Name
MANIATIS MICHAEL
Address
12 SANDS DOCK RD
City
MILTON
State / Zip Code
NY 12547-5502
Country
United States

Analysis

On December 12, 2015, about 1200 eastern standard time, a DeHavilland Tiger Moth DH-82A, N9410, was substantially damaged during a forced landing after takeoff from Old Orchard Airpark (2NK9), Modena, New York. The pilot and a passenger were not injured. Visual meteorological conditions prevailed and no flight plan had been filed for the personal flight that was conducted under the provisions of Title 14 Code of Federal Regulations Part 91.

The pilot reported that he conducted a pre-takeoff engine run, which included an operational check of the magnetos with no anomalies noted. The airplane subsequently experienced a 200-rpm reduction in engine power during the initial climb after takeoff from runway 18. The pilot attempted to return to the runway; however, the airplane was not able to maintain altitude and struck tress about 1/4-mile from the airport.

The airplane was manufactured in 1940 and equipped with a DeHavilland Gipsy Major 1C, 145-horsepower engine

Postaccident examination of the airplane by a Federal Aviation Administration inspector revealed that the airplane sustained substantial damage to both wings, the empennage, and the fuselage. When the inspector rotated the engine crankshaft, continuity was observed to the accessory section and compression was attained on all cylinders with exception of the forward (No. 1) cylinder, which produced "little to no compression." Due to the engine's disposition, the inspector was unable to check the ignition system for proper operation. No further examination of the engine was performed.

The pilot further reported that subsequent teardown of the engine revealed that the No. 1 cylinder exhaust value was stuck in the open position. In addition, disassembly of the left magneto revealed that the "breaker spring" was fractured. The pilot stated that the loss of compression to one of the four engine cylinders alone would have resulted in a forced landing; however, he believed that the combination of the loss of compression on the No. 1 cylinder and the failure of the left magneto resulted in the loss of engine power that the airplane experienced during the accident flight.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA16LA065