ADC Airlines Flight 053 (ADK053) was a scheduled passenger flight operated by ADC Airlines from Nigeria's capital of Abuja to Sokoto. On 29 October 2006, the Boeing 737-200 crashed onto a corn field shortly after take-off from Nnamdi Azikiwe International Airport in Abuja, killing 96 out of 105 people on board.
The investigation of the crash, conducted by Nigeria's Accident Investigation Bureau, blamed the pilot's decision to take off in unsuitable weather as the primary cause of the crash, as presence of windshear at the time posed serious risk to the aircraft's ability to fly. Further investigation revealed inadequate company oversights on windshear recovery training and lack of teamwork among the pilots of Flight 053.
The crash killed several prominent figures in Nigeria, particularly the Sultan of Sokoto, Muhammadu Maccido, the leader of Sokoto and spiritual leader of Nigeria's 70 million Muslims, and his son, Senator Badamasi Maccido. It highlighted Nigeria's poor aviation safety record as it was the third major aviation disaster in less than a year, after Bellview Airlines Flight 210 and Sosoliso Airlines Flight 1145 in 2005, with a combined death toll of 321 people. The crash led to the creation of an independent aviation regulatory body of the Nigerian Civil Aviation Authority. Since then, the nation's aviation safety has significantly improved. There were no more major aviation accidents in Nigeria until Dana Air Flight 992.
The aircraft involved in the crash was a 23-year-old Boeing 737-2B7. It was built in 1983 with a manufacturer serial number of 22891. The aircraft was equipped with 2 Pratt & Whitney JT8D-15 engines. Prior to its acquisition by ADC Airlines, the aircraft was delivered to USAir with a registration of N323AU. In 1988, the aircraft changed its registration code as N279AU. In 1997, it was delivered to US Airways and in 1999 it was operated by the company's MetroJet subsidiary. ADC Airlines acquired the aircraft in September 2003 and its registration was changed to 5N-BFK.
The aircraft had been maintained according to its maintenance schedule and its engines had been installed in new condition in November 2005. The technical logbook did not indicate any known defects on the aircraft.
The flight carried 100 passengers and 5 crew. The Sultan of Sokoto and spiritual leader of Nigeria's Muslims, Muhammadu Maccido, the sultan's son, Senator Badamasi Maccido, the Deputy Governor of Sokoto, Garba Muhammed, the first ever female West African ENT surgeon, Dr Nnennia Mgbor, and Abdulrahman Shehu Shagari, son of former president Shehu Shagari, were on the passenger list. Spokesman of Sokoto Government Mustapha Shehu also stated that the state's education commissioner and another unidentified senator were also on board. The three daughters of Ibrahim Idris, governor of Kogi State, were also on the passenger list.
The captain was 50-year-old Charles Kolawole Atanda, and the first officer was 54-year-old Celestine Okkoneh, who had logged 8,545 and 6,497 flight hours (their experience on the Boeing 737 was not available), respectively.
Flight 053 was a scheduled domestic passenger flight from Nnamdi Azikiwe International Airport in the country's capital of Abuja to Sadiq Abubakar III International Airport in Sokoto. The aircraft was refueled in Lagos, carrying more than 11,000 liters of fuel. The aircraft was carrying 100 passengers and 5 crew members, consisting of 2 flight crew and 3 cabin crew. The aircraft was flown by Captain Atanda with First Officer Okonneh as his co-pilot.
The flight crew received start-up clearance at 11:15 a.m and later received the taxiing permit at 11:21 a.m. Immediately after, the flight crew asked the ATC about the wind condition. The control tower stated that the recorded wind speed was eight knots with varying wind direction. The controller later warned the flight crew that wind gusts were present in the vicinity. The wind started to intensify, as the speed increased to 15 knots (28 km/h; 17 mph) and 35 knots (65 km/h; 40 mph), before it slowed down a bit to 28 knots (52 km/h; 32 mph).
As the aircraft arrived on the runway, the controller stated that the wind was blowing at 15 knots (28 km/h; 17 mph). A pilot of a Virgin Nigeria Airways stated that he would wait for the weather to improve as he stated that the wind was actually closer to 35 knots (65 km/h; 40 mph). Flight 053, however, decided to request a take-off clearance from the airport. The controller re-emphasized the deteriorating weather condition and gave the latest wind check, which the flight crew acknowledged. The flight was cleared for take-off and the crew began the take-off roll.
Flight 053 took off from Abuja at 11:29 a.m. Immediately after takeoff from Runway 22, the Boeing 737 entered into a headwind-shift to-tailwind windshear. Captain Atanda added a small amount of power and pulled up the yoke while First Officer Okonneh kept asking Captain Atanda to pull up. Thus, the nose rose further, reaching an angle of 30-35 degrees. As the nose was pulled up with a high pitch, airflow to the engines was disrupted, causing both engines to experience compressor stall. Following the compressor stall, the aircraft lost its thrust, causing it to enter an aerodynamic stall, followed by a roll to the left of over 90 degrees and a steep descent into the ground. The GPWS warning sounded and the aircraft's left wing struck a tree. It then crashed into a corn field with its nose hitting the ground and with a violent left roll. The aircraft's 11,000-kilogram (24,000 lb) of fuel then ignited, causing a massive explosion. Flight 053 crashed just 76 seconds after it had taken off from Runway 22.
After three unsuccessful attempts to contact the aircraft, the controller advised the Approach Control to call Flight 053. Other aircraft on the apron were also asked to assist in contacting the aircraft but all attempts were unsuccessful. Kano and Lagos Area Controls were requested to contact Flight 053, but there was no response from the aircraft. Abuja Flight Communication Centre was then advised to inform National Emergency Management Agency (NEMA) in Kano about the loss of contact with Flight 053.
At 11:38 a.m, Flight Communication Centre called the controller that someone came from a nearby village near the radar site where Flight 053 was last seen and reported that a plane had crashed in their village. A search party from the airport was dispatched and they confirmed that the plane had crashed shortly after takeoff. The front and middle part were obliterated by the impact and post-crash fire that followed, while a portion of the back of the plane managed to stay intact, saving the lives of a flight attendant and 8 passengers. The other 96 people were killed in the crash.
The Nigerian Aircraft Investigation Bureau (AIB) started an investigation for the cause of the crash with representatives from the U.S. National Transportation Safety Board (NTSB) representing the country where the aircraft was manufactured.
The flight recorders were recovered in good condition and were sent to the NTSB for further analysis. The FDR recorded a total of 18 parameters, of which 14 were able to be converted into "usable engineering units". According to the FDR data, rotation was initiated at 143 knots (265 km/h; 165 mph). The aircraft then reached a peak speed of 162 knots (300 km/h; 186 mph) before it started to decay. The aircraft had been struck by a horizontal and vertical wind shear. A nose-down input was initially applied by the flight crew, recovering the airspeed. However, four seconds later the flight crew applied a nose-up input. The aircraft reached a very high angle of attack and the altitude of the aircraft became erratic.
According to the CVR, just before takeoff the flight crew had acknowledged the presence of windshear in the area, as Captain Atanda had warned his First Officer to "be ready for windshear". The landing gear was retracted and the V2 callout was given by the first officer. Two seconds after the V2 callout, a wind shear warning was triggered, as the aircraft experienced a rapid change in wind direction. The crew then pitched the nose up to between 30° and 35°, thereby greatly exceeding the critical angle of attack, activating the stick-shaker. As a result of the high pitch attitude, the airflow to the engines was disrupted, causing both engines to experience compressor stall. Flight control inputs by the crew resulted in an aerodynamic stall, altitude loss, and subsequent ground impact.