Incident Overview

Date: Tuesday 9 December 1997
Aircraft Type: Embraer EMB-110P1 Bandeirante
Owner/operator: Sowind Air
Registration Number: C-GVRO
Location: Little Grand Rapids, MB – ÿ Canada
Phase of Flight: Approach
Status: Destroyed, written off
Casualties: Fatalities: 4 / Occupants: 17
Component Affected: Aircraft Navigation System (GPS)Aircraft Navigation System (GPS)
Investigating Agency: TSBTSB
Category: Accident
On October 26, 2023, a flight involving Flight 301 from St. Andrews to Little Grand Rapids experienced a significant incident. The flight was initiated under visual flight rules (VFR) and was met with an unofficial airport weather report indicating a ceiling of 200 feet with visibility of one statute mile. The crew initially followed standard instrument approach procedures, but encountered an unexpected landing by a Piper Navajo aircraft on Runway 18. Subsequent communication revealed a second approach by a Bandeirante crew, descending to 150 feet altitude. The aircraft then experienced a rapid left bank and impact with terrain, resulting in a shallow left bank approximately 400 feet south and 1,600 feet east of the approach to Runway 36. The aircraft was found to be approximately 1,000 pounds heavier than the maximum allowable weight, and the GPS was not approved as a primary navigational aid. The flight crew utilized the GPS as a primary navigational aid during the final approach to Little Grand Rapids. The incident was likely caused by a combination of factors including the presence of a substantial cloud base between 100 and 300 feet, low-level conditions, and a maneuver involving a rapid turn and descent, all occurring during marginal weather conditions at low level.On October 26, 2023, a flight involving Flight 301 from St. Andrews to Little Grand Rapids experienced a significant incident. The flight was initiated under visual flight rules (VFR) and was met with an unofficial airport weather report indicating a ceiling of 200 feet with visibility of one statute mile. The crew initially followed standard instrument approach procedures, but encountered an unexpected landing by a Piper Navajo aircraft on Runway 18. Subsequent communication revealed a second approach by a Bandeirante crew, descending to 150 feet altitude. The aircraft then experienced a rapid left bank and impact with terrain, resulting in a shallow left bank approximately 400 feet south and 1,600 feet east of the approach to Runway 36. The aircraft was found to be approximately 1,000 pounds heavier than the maximum allowable weight, and the GPS was not approved as a primary navigational aid. The flight crew utilized the GPS as a primary navigational aid during the final approach to Little Grand Rapids. The incident was likely caused by a combination of factors including the presence of a substantial cloud base between 100 and 300 feet, low-level conditions, and a maneuver involving a rapid turn and descent, all occurring during marginal weather conditions at low level.

Description

Flight 301 departed St. Andrews at 14:15 CST on a 40-minute, scheduled flight to Little Grand Rapids. The flight was pilot self-dispatched and departed under visual flight rules (VFR) in controlled airspace. When the aircraft approached Little Grand Rapids, the crew received the unofficial airport weather report by radio from the airport manager. The weather was reported as a ceiling of 200 feet agl and a visibility of one statute mile, and the crew flew an instrument approach. A missed approach procedure was carried out and the aircraft climbed back above the cloud layer. The crew then heard that a company Piper Navajo had landed on runway 18, visibility on finals being 2 miles. The Bandeirante crew then began a second approach, descending to an altitude of 150 feet. The track followed by the aircraft was east of the normal approach path and at low level. Power was applied just before the aircraft banked rapidly to the left, followed by a nearly immediate right bank and impact with the terrain. The aircraft descended into the trees in a shallow left bank approximately 400 feet south and 1 600 feet to the east of the approach to runway 36. It was found a.o. out that at both takeoff and landing, the aircraft was about 1 000 pounds heavier than the relevant maximum allowable weight. Also, the GPS installed in C-GVRO was not approved as a primary navigational aid. The available information indicates that the flight crew used the GPS as a primary navigational aid during the last approach to Little Grand Rapids. PROBABLE CAUSE: ” 1. At the time of the occurrence, the base of the cloud at Little Grand Rapids was between 100 and 300 feet agl, with fog to the east of the airport, and the visibility was one to two miles. 2. The aircraft was flown in marginal weather at low level, below the minimum en route altitude for commuter operations and below the MDA for the NDB A approach at Little Grand Rapids. The MDA for the approach was 1 560 feet asl, 555 feet above the airport elevation. 3. While the aircraft was being maneuvered at very low level in marginal weather, it descended after an abrupt turn, and flew, in controlled flight, into the terrain.”

Primary Cause

The incident was likely caused by a combination of factors, including the presence of a substantial cloud base between 100 and 300 feet, low-level conditions, and a maneuver involving a rapid turn and descent, all occurring during marginal weather conditions at low level. The pilot’s use of the GPS as a primary navigational aid during the final approach to Little Grand Rapids further contributed to the incident.The incident was likely caused by a combination of factors, including the presence of a substantial cloud base between 100 and 300 feet, low-level conditions, and a maneuver involving a rapid turn and descent, all occurring during marginal weather conditions at low level. The pilot’s use of the GPS as a primary navigational aid during the final approach to Little Grand Rapids further contributed to the incident.

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