Incident Overview

Date: Sunday 22 July 2001
Aircraft Type: Boeing 737-430
Owner/operator: Euralair International
Registration Number: F-GRNZ
Location: Monastir – ÿ Tunisia
Phase of Flight: Landing
Status: Substantial
Casualties: Fatalities: 0 / Occupants: 178
Component Affected: Lower lob skin, tail skid, 15 stringers, and 2 fuselage websLower lob skin, tail skid, 15 stringers, and 2 fuselage webs
Category: Accident
A Boeing 737-400, F-GRNZ operated by Euralair experienced a tail strike during landing at Monastir, Tunisia. No injuries were reported. Weather conditions were CAVOK with a wind of 110ø/8 and a temperature of 28øC. Upon touchdown, the crew reported an unusual sound and subsequent inspection revealed damage to the lower lob skin, tail skid, 15 stringers, and 2 fuselage webs. The maintenance inspection identified the cause as insufficient thrust reduction during the initial touchdown and pilot attitude introduced by the flight.A Boeing 737-400, F-GRNZ operated by Euralair experienced a tail strike during landing at Monastir, Tunisia. No injuries were reported. Weather conditions were CAVOK with a wind of 110ø/8 and a temperature of 28øC. Upon touchdown, the crew reported an unusual sound and subsequent inspection revealed damage to the lower lob skin, tail skid, 15 stringers, and 2 fuselage webs. The maintenance inspection identified the cause as insufficient thrust reduction during the initial touchdown and pilot attitude introduced by the flight.

Description

A Boeing 737-400, F-GRNZ, operated by Euralair experienced a tail strike while landing on runway 08 at Monastir, Tunisia. There were no reported injuries. Weather was CAVOK, wind 110/8, temp. 28C. The crew heard an unusual sound upon touchdown from a bounced landing. Subsequent crew inspection with a flashlight did not detect any damage. Upon return to CDG, maintenance personnel were redirected to inspect. The maintenance inspection revealed damage to the lower lob skin, tail skid, 15 stringers and 2 fuselage webs. Probable Causes The hard landing resulted from insufficient thrust reduction at the time of the first touchdown and the absence of a go-around after the bounce. The extension of the lift dumpers at the time of the thrust reduction and the additional attitude introduced by the pilot caused the fuselage to rub on the runway. The non-detection of the damage to the aircraft was not a factor in the accident but was a risk factor for the following flight.

Primary Cause

Insufficient thrust reduction during the initial touchdown and pilot attitude caused the fuselage to rub against the runway.Insufficient thrust reduction during the initial touchdown and pilot attitude caused the fuselage to rub against the runway.

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