Incident Overview

Date: Monday 12 February 1990
Aircraft Type: Fokker F-27 Friendship 200
Owner/operator: TAM Transportes A‚reos Regionais
Registration Number: PT-LCG
Location: Bauru Airport, SP (BAU) – ÿ Brazil
Phase of Flight: Initial climb
Status: Destroyed, written off
Casualties: Fatalities: 1 / Occupants: 41
Component Affected: Aircraft Engine (specifically, the turbine combustion chambers) ? The engine’s combustion chambers experienced excessive fuel due to low rotation, resulting in a rapid temperature increase, causing engine failure and subsequent loss of control.Aircraft Engine (specifically, the turbine combustion chambers) ? The engine’s combustion chambers experienced excessive fuel due to low rotation, resulting in a rapid temperature increase, causing engine failure and subsequent loss of control.
Investigating Agency: CENIPACENIPA
Category: Accident
On March 15, 2023, a serious aviation incident occurred involving an F-27 Friendship aircraft during a domestic flight from S?o Paulo-Congonhas to Bauru. The aircraft was operating under conditions of reduced frequency and a complex approach sequence. The pilot, flying under instruction, initiated a rapid descent while the airplane was 27 nautical miles (50 kilometers) from Bauru. Due to congestion in the Brasilia ACC, the descent was initiated at a faster rate than the standard 40 nautical mile (74 kilometer) out approach. After a fast descent to 4000 feet, the flight plan was cancelled, and the crew proceeded for a visual straight-in approach to runway 32. The pilot, operating under the instructor?s control, attempted to maintain the approach and landing configuration, including lowering the landing gear and selecting flaps to 16 to 40 degrees. The pilot expressed discomfort with the aircraft’s speed and proximity to the airfield, prompting the instructor to instruct the landing gear to be lowered and flaps to be selected down. The pilot subsequently requested the instructor?s control, leading to a takeover. The aircraft descended at a rate of 2500 feet per minute, and the speed remained at 130 kts. The airplane touched down 775 meters past the runway 32 threshold, floating and alternatingly touching the right and left main landing gear. The instructor, recognizing the aircraft?s inability to be stopped, initiated a go-around maneuver, resulting in a significant increase in turbine gas temperature (TGT). The engine combustion chambers experienced excessive fuel, causing the low rotations of the propellers. This resulted in an extreme rise in turbine gas temperature, leading to engine failure. The aircraft sank, impacting two occupants of a car that was hit, resulting in six fatalities. The incident highlighted a significant lapse in instruction and coordination, compounded by a pilot?s discomfort and a lack of proper control measures.On March 15, 2023, a serious aviation incident occurred involving an F-27 Friendship aircraft during a domestic flight from S?o Paulo-Congonhas to Bauru. The aircraft was operating under conditions of reduced frequency and a complex approach sequence. The pilot, flying under instruction, initiated a rapid descent while the airplane was 27 nautical miles (50 kilometers) from Bauru. Due to congestion in the Brasilia ACC, the descent was initiated at a faster rate than the standard 40 nautical mile (74 kilometer) out approach. After a fast descent to 4000 feet, the flight plan was cancelled, and the crew proceeded for a visual straight-in approach to runway 32. The pilot, operating under the instructor?s control, attempted to maintain the approach and landing configuration, including lowering the landing gear and selecting flaps to 16 to 40 degrees. The pilot expressed discomfort with the aircraft’s speed and proximity to the airfield, prompting the instructor to instruct the landing gear to be lowered and flaps to be selected down. The pilot subsequently requested the instructor?s control, leading to a takeover. The aircraft descended at a rate of 2500 feet per minute, and the speed remained at 130 kts. The airplane touched down 775 meters past the runway 32 threshold, floating and alternatingly touching the right and left main landing gear. The instructor, recognizing the aircraft?s inability to be stopped, initiated a go-around maneuver, resulting in a significant increase in turbine gas temperature (TGT). The engine combustion chambers experienced excessive fuel, causing the low rotations of the propellers. This resulted in an extreme rise in turbine gas temperature, leading to engine failure. The aircraft sank, impacting two occupants of a car that was hit, resulting in six fatalities. The incident highlighted a significant lapse in instruction and coordination, compounded by a pilot?s discomfort and a lack of proper control measures.

Description

The F-27 Friendship departed Sao Paulo-Congonhas (CGH) on a domestic flight to Bauru. Pilot flying was a captain in training, accompanied by an instructor and a commissioner. Due to congestion in the frequency of Brasilia ACC, the descent from FL140 was initiated while the airplane was 27 nm (50 km) from Bauru, instead of the usual 40nm (74 km) out. After a fast descent to 4000 feet the IFR flight plan was cancelled and the crew proceeded for a visual straight-in approach to runway 32. The pilot flying felt uncomfortable because the airplane was flying too fast and was too close to the airfield. The instructor wanted to continue the approach and instructed the landing gear to be lowered and the flaps to be selected down from 16 to 40 degrees. The airplane decelerated to 135 kts, which was still too fast. After asking the instructor, the pilot was told that he was supposed to carry out the approach and landing. Because the instructor also held his control column and due to the improper approach configuration, the pilot again asked who would perform the landing. The instructor now took over control. The F-27 descended at a rate of 2500 fpm and the speed was still 130 kts. The airplane touched down 775 m past the runway 32 threshold. The aircraft floated and alternatingly, touched the runway with the right and left main landing gear. The instructor realized that the plane could not be stopped on the remaining runway, and brusquely added power to initiate a go around. Contrary to the Airplane Flight Manual, power was not added gradually thus causing an extreme rise in the turbine gas temperature (TGT). The engine?s combustion chambers had now received excessive from fuel. The low rotations of the propellers did not provide enough air for a combustive mixture and the high angle of attack on the initial climb provoked the intake of enough air into the engines. Both engines failed to develop enough power and the Fokker began to sank until it collided with some obstacles on the ground, 600 m outside the airport. Two occupants of a car that was hit, didn’t survive. CONCLUS?O: Fator Humano – Aspecto Psicol¢gico – Contribuiu Fator Operacional – Contribuiu (1) Deficiente Instru‡?o. (2) Deficiente Aplica‡?o dos Comandos. (3) Deficiente Coordena‡?o de Cabine. (4) Deficiente Julgamento. (5) Deficiente Planejamento. (6) Deficiente Supervis?o.

Primary Cause

Improper Approach Configuration and Lack of Coordination ? The pilot?s deviation from the standard approach procedure, particularly the rapid descent and insufficient control, combined with the instructor?s over-intervention and lack of proper coordination, led to a critical situation. The rapid descent, combined with the instructor?s insistence on a specific approach configuration, created an unstable and potentially dangerous situation. The failure to properly manage the aircraft?s speed and proximity to the airfield, exacerbated by the pilot?s discomfort, triggered a catastrophic event.Improper Approach Configuration and Lack of Coordination ? The pilot?s deviation from the standard approach procedure, particularly the rapid descent and insufficient control, combined with the instructor?s over-intervention and lack of proper coordination, led to a critical situation. The rapid descent, combined with the instructor?s insistence on a specific approach configuration, created an unstable and potentially dangerous situation. The failure to properly manage the aircraft?s speed and proximity to the airfield, exacerbated by the pilot?s discomfort, triggered a catastrophic event.

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