Accident BAC One-Eleven 320AZ 5N-AOT, Thursday 7 September 1989
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Date:Thursday 7 September 1989
Time:19:05
Type:Silhouette image of generic BA11 model; specific model in this crash may look slightly different    
BAC One-Eleven 320AZ
Owner/operator:Okada Air
Registration: 5N-AOT
MSN: 133
Year of manufacture:1968
Total airframe hrs:42575 hours
Engine model:Rolls-Royce Spey 511-14
Fatalities:Fatalities: 0 / Occupants: 92
Other fatalities:0
Aircraft damage: Destroyed, written off
Category:Accident
Location:Port Harcourt Airport (PHC) -   Nigeria
Phase: Landing
Nature:Passenger - Scheduled
Departure airport:Lagos-Murtala Muhammed International Airport (LOS/DNMM)
Destination airport:Port Harcourt Airport (PHC/DNPO)
Investigating agency: AIPB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
Okada Air Flight OKJ 307 originated from Lagos (LOS), at about 17:10 hours UTC en-route to Port-Harcourt (PHC).
By 17:40 hours, at FL250, the crew established contact with Port Harcourt Tower and was cleared to the "PR" Radio Beacon. The 1700 hours weather report was passed onto the crew with the assurance not to expect any delay for an ILS approach to runway 21.
At 75 nm from Port Harcourt, the aircraft was cleared down to FL90 and the crew reviewed their approach briefings. The First Officer was still flying when the airplane was further cleared to 2000 feet with the instructions to report when established on the localizer.
At 700 feet, the Commander had the field-in-sight but the flying pilot had not. Then the Commander took over control from the First Officer. The captain requested the tower to increase approach lights intensity because of drizzling rain. The BAC 1-11 passed an area of heavy downpour. It entered a high sink rate and made a hard landing. The airplane bounced and made the second touchdown on its nose-wheel. The right nose wheel shattered instantaneously while the second nose wheel fractured at the hub. It rolled for about 90 metres and crumbled under the weight of the aircraft. When both wheels of the nose gear had broken away, the wheel axle made contact with runway to cut grooves onto the runway surface for about 25 metres before the nose strut finally gave way. The aircraft now scooped forward on the nose fuselage section and continued off the runway on to the left shoulder. On the shoulder, the aircraft ran into the wide trench which was covered up with loose soil and the impact severed off the right main gear from the attachment point. The aircraft eventually came to a stop 735 meters after touchdown.

CAUSE OF ACCIDENT: "The probable cause of this accident is the poor handling of the controls at the critical movement of final approach and landing phases, probably due to the sudden loss of azimuth in the heavy down pour of rain. The contributory factor to the accident is the excavation and improper refilling of the outrageous trenches of wide dimensions along the length of runway 03/21."

Accident investigation:
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Investigating agency: AIPB
Report number: CIA 148
Status: Investigation completed
Duration: 8 months
Download report: Final report

Sources:

Flight International 17-23 January 1989 (46)

Location

Images:


photo (c) AIPB Nigeria; Port Harcourt Airport (PHC); September 1989


photo (c) AIPB Nigeria; Port Harcourt Airport (PHC); September 1989


photo (c) via Werner Fischdick; London-Gatwick Airport (LGW); April 1982

Revision history:

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