Incident Overview

Date: Saturday 21 July 1979
Aircraft Type: Boeing B-17G
Owner/operator: Black Hills Aviation
Registration Number: N66573
Location: 16 km SW of Superior, MT – ÿ United States of America
Phase of Flight: Manoeuvring (airshow, firefighting, ag.ops.)
Status: Destroyed, written off
Casualties: Fatalities: 2 / Occupants: 2
Component Affected: Airtanker’s flight path and control systems, specifically the left turn and bank angle.Airtanker’s flight path and control systems, specifically the left turn and bank angle.
Category: Accident
An air tanker encountered a challenging situation while fighting forest fires in Montana. After a high pass over a mountainous ridge, it impacted a densely wooded hillside due to a critical left turn and increased bank angle, resulting in a stall.An air tanker encountered a challenging situation while fighting forest fires in Montana. After a high pass over a mountainous ridge, it impacted a densely wooded hillside due to a critical left turn and increased bank angle, resulting in a stall.

Description

The air tanker was engaged in fighting forest fires in Montana, USA. The aircraft was re-loaded with 1,800 gallons of retardant and departed from the airport at 17:48 on the second run in the Lolo National Forest. Upon returning to the fire, the aircraft made a high pass over the fire and then an approach for a second pass. The fire was located near the top of a mountainous ridge on an even slope that provided an easy target for a retardant drop. Once the pass had been made, no retardant had been dropped. Immediately after the airtanker passed over the drop target, it made a steep left turn and impacted a densely timbered hillside. Ground impact occurred in an estimated 5 to 10 degree nose low attitude and approximately a 40-degree left bank. The investigation team determined that during the sequence of events, the airtanker’s flight path during the left turn was taking it too close to the mountainside. This required more bank angle and gravity forces to increase the rate of turn and hold altitude in order to clear the mountainside. Unfortunately, as bank angles and load factors increased, induced drag, which predominates at low speeds, also increased dramatically. These factors would have required significant increases in power to maintain flight and preclude stalling. The airtanker’s situation, already critical because of its low airspeed, low altitude, and the turning space restriction, was compounded by the additional bank angle and increased load factor. The fringe of a stall was entered and aggravated by the addition of aileron and elevator input to increase the rate of turn. Power was insufficient to maintain flight and a few seconds later the airtanker completely stalled when performance demands could not be maintained. Close proximity to the ground precluded the use of normal stall recovery techniques, and the airtanker descended into the trees.

Source of Information

https://www.researchgate.net/publication/2840945_United_States_Department_of_Agriculture_Forest_Servicehttps://www.researchgate.net/publication/2840945_United_States_Department_of_Agriculture_Forest_Service

Primary Cause

Critical left turn and increased bank angle during a maneuver, leading to induced drag and stall.Critical left turn and increased bank angle during a maneuver, leading to induced drag and stall.

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