DANA PLANE CRASH: How Captain battled with failed engines mid-air – Report
Preliminary report on the Dana plane that crashed on 3rd June 2012
at Iju-Ishaga, Lagos released yesterday by the Accident Investigation
Bureau, AIB, said that the Captain tried starting the failed two engines
mid-air when the engines packed up and after several failed attempt
‘’the Capt informed the Flight Officer, FO, “we just lost everything,
we lost an engine. I lost both engines”.
This is coming as the report said the crash was not caused by
contaminated fuel. The plane, a Boeing MD-83, with registration no
5N-RAM on a domestic scheduled commercial flight, operated by Dana
Airlines Limited as flight 992 (DAN 992), crashed into a densely
populated area during a forced landing following a total loss of power
in both engines while on approach to Muhammed Murtala Airport (LOS),
Lagos, Nigeria.
According to the report, ‘’the airplane was on the fourth flight
segment of the day, consisting of two round-trips between Lagos and
Abuja. The accident occurred during the return leg of the second trip.
DAN 992 was on final approach for runway 18R at LOS when the crew
reported the total loss of power.
‘’According to interviews, the flight arrived in ABV as Dana Air
flight 993 about 1350. According to Dana Air ground personnel, routine
turn-around activities occurred, including refueling of the airplane.
DAN 992 initiated engine startup at 1436, taxied to the runway and was
later airborne at 1458 after the flight had reported that it had a fuel
endurance of 3.5 hours.
“Shortly after takeoff, DAN 992 reported 1545 as the estimated time
of arrival at LOS as the flight climbed to a cruise altitude of 26,000
ft. DAN0992 made contact with Lagos Area Control Center at 1518 hours.
‘’According to the report,the cockpit voice recorder (CVR) retained
about 31 minutes of the flight and starts about 1515 at which time the
captain and first officer were in a discussion of a non-normal condition
regarding the correlation between the engine throttle setting and an
engine power indication.
“However, they did not voice concerns then that the condition would
affect the continuation of the flight. The flight crew continued to
monitor the condition and became increasingly concerned as the flight
transition through the initial descent from cruise altitude at 1522 and
the subsequent approach phase.
‘’DAN 992 reported passing through 18,100 and 7,700 ft, respectively,
at 1530 and 1540 hours. After receiving a series of heading and
altitude assignments from the controller, DAN 992 was issued the final
heading to intercept the final approach course for runway 18R.

Wreckage of Dana Airline which crashed at Iju Isaga area of Lagos, recently.
‘’During the period of 1537 and 15:41 the flight crew engaged in
pre-landing tasks including deployment of the slats, and extension of
the flaps and landing gear. At 15:41:16 the first officer (FO) inquired,
“both engines coming up?” and the captain (Capt) replied “negative.”
‘’The flight crew subsequently discussed and agreed to declare an
emergency. At 1542:10, DANA 992 radioed an emergency distress call
indicating “dual engine failure . . . negative response from throttle.”
‘’At 1542:35, the flight crew lowered the flaps further and continued
with the approach and discussed landing alternatively on runway 18L. At
1542:45, the Capt reported the runway in sight and instructed the FO to
raise the flaps up and 4 seconds later to raise the landing gear.
“At 1543:27 hours, the Capt informed the FO “we just lost everything,
we lost an engine. I lost both engines”. During the next 25 seconds
until the end of the CVR recording, the flight crew was attempting to
restart the engines.
‘’The airplane crashed in a residential area about 5.8 miles north of
LOS. The airplane wreckage was on approximately the extended centerline
of runway 18R. During the impact sequence, the airplane struck an
incomplete building, two trees and three buildings. The wreckage was
confined, with the separated tail section and engines located at the
beginning of the debris field.
‘’The airplane was mostly consumed by post crash fire. The tail
section, both engines and portions of both wings, representing only
about 15% of the airplane were recovered from the accident site for
further examination.
‘’The two flight recorders, the Cockpit Voice Recorder (CVR) and the
flight data recorder (FDR) were analysed at the facilities of the
National Transportation Safety Board (NTSB), Washington, D.C., USA. The
solid state based memory in the CVR was in good condition and retained
31 minutes of audio information. The digital tape based memory in the
FDR succumbed to the post crash fire and melted, consequently no data
could be recovered.
“The captain, age 55, held an airline transport pilot license with
type ratings in the A-320, DC-9, FK-28, and SF-340. He had over 18,116
hours of total time, including 16,416 hours of pilot-in-command time
(PIC). The captain had 7,461 hours in the accident model airplane all of
which was as PIC. He was employed with Dana Air on 14 March 2012.
“He began flying line operations for the company in late May 2012 and
had since accrued over 120 hours of flight time. The captain had
acquired about 3, 78, and 116 flight hours, respectively, in the
preceding 24 hours, 30 and 90 days.
‘’The first officer, age 34, held a commercial pilot license he was
type rated in MD-83. He had 1,143 hours of total time, including about
200 hours as pilot-in-command. The first officer had 808 hours in the
accident model airplane all of which was second-in-command.
“He had been previously employed with Dana Air as the Director of
Cabin Service before he was hired as a pilot about January 2011. The
first officer had accrued about 3, 42, and 154 flight hours,
respectively, during the preceding 24 hours, 30 and 90 days.
‘’The airplane was manufactured in 1990 and according to maintenance
records it had accumulated 60,846 hours (35,219 cycles) of total time.
The left and right engines respectively had 54,322 (30,933 cycles) and
26,025 (12,466 cycles) hours of total time since new.
“A review of the aircraft technical logs did not reveal of the
previous 30 days did not indicate a condition. The airplane had last
undergone maintenance on 1st June 2012, and after a return to service
flight on 2nd June 2012, it was operated on four revenue flights (two
round trips between LOS and ABV) and another four flights on 3rd June
2012.
Fueling records indicated the airplane was uplifted with 8000 lbs of
fuel before departure from ABV. The flight crew reported to ATC they had
26,000 lbs of total fuel. Preliminary analysis of fuel samples from the
refueling truck and the supply tank at ABV were negative for
contamination.
The investigative activities have included, in part, visual
examination of the aircraft wreckage, review of maintenance records and
other historical information of the aircraft, documentation of the
training and experience of the flight crew, determination of the
chronology of the flight, review of recorded data, reconstructing the
aircraft refueling, and collection of related fuel samples, and
interviews of relevant personnel.
‘’Future investigative activities will include, but is not limited
to, the detailed examination of the engines, further testing of fuel
samples, continued factual gathering of relevant historical,
operational, maintenance and performance information of the accident
airplane in addition to other similar airplane models, further
development of the background of the flight crew, further analysis of
the CVR audio recording and review of pertinent issues associated with
regulatory oversight.
‘’As the State of Occurrence, the Accident Investigation Bureau (AIB)
has instituted an investigation in accordance with the standards and
recommendations specified in the provisions of Annex 13 of the
International Civil Aviation Organization.
“As the State of manufacture of the airplane and engine, a US
Accredited Representative has been appointed and assisted by US
technical advisors from the NTSB, US Federal Aviation Administration,
Boeing Airplane Company, and Pratt & Whitney Engines. In accordance
with Annex 13, “the sole objective of the investigation of an accident
or incident shall be the prevention of accidents and incidents. It is
not for the purpose of this activity to apportion blame or liability.”
source: vanguard news