Accident Boeing 737-2K9 TJ-CBE,
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ASN Wikibase Occurrence # 324571
 

Date:Sunday 3 December 1995
Time:22:44
Type:Silhouette image of generic B732 model; specific model in this crash may look slightly different    
Boeing 737-2K9
Owner/operator:Cameroon Airlines
Registration: TJ-CBE
MSN: 23386/1143
Year of manufacture:1985
Total airframe hrs:18746 hours
Cycles:23233 flights
Engine model:Pratt & Whitney JT8D-15A
Fatalities:Fatalities: 71 / Occupants: 76
Aircraft damage: Destroyed, written off
Category:Accident
Location:1,7 km S of Douala Airport (DLA) -   Cameroon
Phase: Approach
Nature:Passenger - Scheduled
Departure airport:Cotonou Airport (COO/DBBB)
Destination airport:Douala Airport (DLA/FKKD)
Investigating agency: CCAA
Confidence Rating: Accident investigation report completed and information captured
Narrative:
A Boeing 737-2K9 passenger plane, operated by Cameroon Airlines, was destroyed in an accident at Douala, Cameroon. Five of the 76 occupants survived the accident.
The Boeing 737, named "Nyong", operated on a passenger flight from Cotonou, Benin to Douala, Cameroon. The flight departed at 20:22 UTC and climbed to the cruising altitude of FL330. The en route and descent were uneventful. At 21:32 UTC the flight was cleared for an approach to runway 30. Nine minutes later the flight reported 3,5 NM out at 1100 feet with runway in sight. The tower controller then cleared the flight to land. The aircraft overflew the runway threshold and started to climb. The flight radioed that they were 'having problems' and that they would report back. The tower controller then saw the aircraft in a sharp left hand turn. The airplane descended until it impacted a mangrove swamp.

PROBABLE CAUSES (translated from French):
The probable cause of the accident is a of loss of control during a go-around attempt made during a maneuver to reach the runway with degraded performance.
Seriously contributing to this:
1 - The detachment by structural fatigue of a first stage compressor blade of the No. 1 engine which resulted in a loss of power and destabilization of the trajectory when landing
2 - The late or slow execution of the go-around procedure with an unidentified single-engine configuration, leading to irreversible loss of speed.

Accident investigation:
cover
  
Investigating agency: CCAA
Report number: Final report
Status: Investigation completed
Duration:
Download report: Final report

Sources:

ICAO Adrep Summary 1/96

Location

Revision history:

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