Incident Overview

Date: Sunday 1 November 1987
Aircraft Type: Boeing 737-2A8
Owner/operator: Indian Airlines
Registration Number: VT-EDS
Location: Bangalore-Hindustan Airport (BLR) – ÿ India
Phase of Flight: Landing
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 61
Component Affected: Nose landing gear actuator attachment point.Nose landing gear actuator attachment point.
Category: Accident
During takeoff from Madras, the crew reported an unusual noise from the nose landing gear during retraction. The flight continued to Bangalore. Upon approach, the nose gear appeared to be not locked down, and a low pass was performed. Air traffic control confirmed the undercarriage was fully down. Upon landing, the crew maintained the nose up as far as possible. The nose contacted the runway after a ground run of 4000 feet, resulting in a stop 1300 feet further on. A probable cause was non-locking of the nose landing gear in down position, likely due to downward shifting of the nose landing gear actuator attachment point following fatigue and ‘T’ section longitudinal beam under stress corrosion cracking.During takeoff from Madras, the crew reported an unusual noise from the nose landing gear during retraction. The flight continued to Bangalore. Upon approach, the nose gear appeared to be not locked down, and a low pass was performed. Air traffic control confirmed the undercarriage was fully down. Upon landing, the crew maintained the nose up as far as possible. The nose contacted the runway after a ground run of 4000 feet, resulting in a stop 1300 feet further on. A probable cause was non-locking of the nose landing gear in down position, likely due to downward shifting of the nose landing gear actuator attachment point following fatigue and ‘T’ section longitudinal beam under stress corrosion cracking.

Description

During takeoff from Madras, the crew heard an unusual noise from the nose landing gear during retraction. The flight continued to Bangalore. While on approach it appeared that the nose gear was not locked down. A low pass at 300 feet was performed. Air traffic control confirmed that the undercarriage was fully down. Upon landing the crew kept the nose up as far as possible. The nose contacted the runway after a ground run of 4000 feet and the aircraft stopped 1300 feet further on. PROBABLE CAUSE: “Non-locking of the nose landing gear in down position which was most probably due to downwards shifting of the nose landing gear actuator attachment point subsequent to failure of failure of vertical leg of its attachment fitting under fatigue and ‘T’ section longitudinal beam under stress corrosion cracking.”

Primary Cause

Non-locking of the nose landing gear in down position, likely due to downward shifting of the nose landing gear actuator attachment point following fatigue and ‘T’ section longitudinal beam under stress corrosion cracking.Non-locking of the nose landing gear in down position, likely due to downward shifting of the nose landing gear actuator attachment point following fatigue and ‘T’ section longitudinal beam under stress corrosion cracking.

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