Ground accident of a Boeing KC-135R Stratotanker in Bishkek

Date & Time: Sep 26, 2006 at 2010 LT
Type of aircraft:
Operator:
Registration:
63-8886
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Bishkek - Bishkek
MSN:
18734
YOM:
1964
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On Sept. 26, at approximately 8:03 p.m. local time, a KC-135R landed at Manas International Airport following a combat mission over Afghanistan. After landing, the KC-135R was parked at the intersection of the active runway and a taxiway while the crew awaited clarification on instructions from the air traffic control tower. The KC-135R was struck by a host nation TU-154 that was taking off. The TU-154's right wing struck the fairing of the KC-135R's No. 1 engine. The force of the impact nearly severed the No. 1 engine from KC-135R and destroyed a portion of the aircraft's left wing. The TU-154 lost approximately six feet of its right wingtip, but was able to get airborne and return to the airport for an emergency landing with no additional damage to the aircraft. The three aircrew members on board the KC-135R, as well as the nine aircrew members and 52 passengers aboard the TU-154, survived the accident. None of the aircrew or passengers on board the TU-154 sustained any injuries. One KC-135 crew member sustained minor abrasions while evacuating the aircraft.
Probable cause:
The collision between the TU-154 and KC-135R aircraft was clearly an accident and not the result of any intentional conduct. The Accident Investigation Board, convened by AMC, determined that the accident was caused by the Kyrgyzaeronavigation air traffic controller who cleared a civilian airliner for takeoff without verifying that the KC-135R was clear of the runway. In addition to the air traffic controller, the AIB found evidence of several contributing factors involving the KC-135R aircrew, conflicting published airport notices, and a tower liaison employed by the U.S. Government to facilitate communication between the tower and U.S. aircrews. Although the AIB found the air traffic controller primarily at fault, the U.S. KC-135R crew and tower liaison shared responsibility for ensuring the KC-135R cleared the runway to a safe location following landing. The accident might have been avoided had any of them exercised better awareness of their situation.
In conclusion, the AIB determined the principal cause of the mishap was the Kyrgyzaeronavigation controller clearing the TU-154 for takeoff without verifying that KC-135R was clear of the runway, there was evidence the following factors also contributed to the mishap:
- The Kyrgyz air traffic controller's instruction to vacate at taxiway Golf after dark conflicted with a published Notice to Airmen (NOTAM) that limited that taxiway's use to daylight hours. The contractor safety liaison (LNO) employed by the U.S. Air Force to facilitate communication between its aircrews and Kyrgyz controllers did not clarify the apparent discrepancy.
- After questioning the Kyrgyz controller's instruction to vacate the runway at taxiway Golf, the LNO instructed the KC-135R crew to hold short of Alpha. The mishap KC-135R crew misperceived the LNO's instructions and responded "holding short of Golf." The LNO failed to catch the read-back error.
- The Kyrgyz controller failed to maintain awareness of the KC-135R's location.
- The LNO failed to maintain situational awareness and intervene when the controller's actions endangered the KC-135R and aircrew.
The KC-135R is assigned to the 92nd Air Refueling Wing, Fairchild Air Force Base, Wash. While deployed at Manas AB, the KC-135R and its aircrew were assigned to U.S. Central Command's 376th Air Expeditionary Wing, flying missions supporting coalition aircraft over Afghanistan.
Final Report:

Crash of a Dornier DO228-212 in Vande Ikya: 13 killed

Date & Time: Sep 17, 2006
Type of aircraft:
Operator:
Registration:
NAF033
Flight Type:
Survivors:
Yes
Site:
Schedule:
Abuja - Obudu
MSN:
8229
YOM:
1994
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
13
Circumstances:
The twin engine aircraft departed Abuja on a flight to Obudu, carrying 15 passengers and a crew of three. The pilots started the descent in poor weather conditions when the aircraft impacted hilly terrain near Vande Ikya, about 29 km northwest of Obudu. Five occupants were injured while 13 others were killed, among them several high ranking officers who were flying to Obudu to proceed to an inspection of the military equipments. At the time of the accident, the visibility was poor due to low ceiling.
Probable cause:
Controlled flight into terrain after the crew initiated the descent prematurely, causing the aircraft to descend below the minimum prescribed altitude.

Crash of a BAe Nimrod MR.2 near Kandahar: 14 killed

Date & Time: Sep 2, 2006 at 1547 LT
Type of aircraft:
Operator:
Registration:
XV230
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Muscat - Muscat
MSN:
8005
YOM:
1969
Country:
Region:
Crew on board:
14
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
14
Circumstances:
The aircraft departed at 13:43 for a mission over Afghanistan, in support of coalition forces engaging the Taliban. At 15:30 the airplane rendezvoused with an RAF Lockheed TriStar tanker and received fuel in an air-to-air refuelling procedure that lasted 10 minutes. Air-to-air refuelling appeared to pass without incident and XV230's crew prepared to turn east, towards their operational area. Eleven minutes later a bomb bay fire warning, either coincident with, or followed immediately by, an elevator bay underfloor smoke warning, was reported. The crew also reported smoke entering the aircraft’s cabin, from both elevator and aileron bays. Within a minute the aircraft depressurised as the fire breached the aircraft’s pressure hull requiring the crew to don their oxygen masks. The captain began to turn the aircraft towards Kandahar, declared a MAYDAY and began a descent. Meanwhile a crew member reported a fire 'from the rear of the starboard engines'. Another crew member reported a fire within the aileron bay. Last radio contact was at 15:46 when the crew acknowledged the Kandahar weather for landing. About the same time, a Harrier GR7 pilot, who was several thousand feet above, reported an intense fire close to the starboard fuselage and stretching out between where the wing joins the aircraft fuselage to the starboard engine; there was a second fire that stretched behind the aircraft from a point on the side of the rear body of the aircraft. At 15:47 the Harrier pilot reported that he saw the Nimrod explode. It broke into 4 sections, at a height of between 750 feet and 1000 feet. All 14 crew members were killed.
Crew:
F/Sgt Gary Wayne Andrews,
F/Sgt Stephen Beattie,
F/Sgt Gerard Martin Bell,
F/Sgt Adrian Davies,
L/Cpl Oliver Simon Dicketts,
F/Lt Steven Johnson,
Sgt Benjamin James Knight,
F/Lt Leigh Anthony Mitchelmore,
F/Lt Gareth Rodney Nicholas,
Sgt John Joseph Langton,
Sgt Gary Paul Quilliam,
F/Lt Allan James Squires,
F/Lt Steven Swarbrick,
Mne Joseph David Windall.
Probable cause:
As the Board was unable to investigate XV230's wreckage at the crash site and it proved impossible to recover more than a few small components from the aircraft, the Board has been unable to determine positively the source or cause of the fire which led to the loss of XV230 and its crew. Nonetheless, through investigation of the limited data available, the Board was able to deduce the most probable location of the fire, a number of probable causes of that event and factors which possibly contributed to it:
a. The escape of fuel during AAR, occasioned by an overflow from No 1 tank, or a leak from the fuel system (fuel coupling or pipe), led to an accumulation of fuel within the No 7 tank dry bay. Although of a lower probability, the fuel leak could have been caused by a hot air leak damaging fuel system seals.
b. The ignition of that fuel following contact with an exposed element of the aircraft's crossfeed/ SCP pipe work.
Contributory factors:
a. The age of the Nimrod MR2's non-structural system components.
b. Nimrod MR2 maintenance policy in relation to fuel and hot air systems.
c. The lack of a fire detection and suppression system within the No 7 tank dry bay.
d. The fact that hazard analysis did not correctly categorize the potential threat to the aircraft caused by the collocation of fuel and hot air system components within the No 7 tank dry bay.
e. The formal incorporation of AAR capability within the Nimrod did not identify the full implications of successive changes to the fuel system and associated procedures.
Aggravating factor:
a. The loss of flying controls through fire damage to the hydraulic systems or cables and pulleys.

Crash of an Antonov AN-26 in Al Fashir

Date & Time: Aug 7, 2006
Type of aircraft:
Operator:
Registration:
ST-ZZZ
Flight Type:
Survivors:
Yes
MSN:
10407
YOM:
1980
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After touchdown on runway 05, the aircraft went out of control, veered off runway and came to rest. There were no injuries while the aircraft was damaged beyond repair as the left engine and the undercarriage were torn off.

Crash of an Antonov AN-12 in Geneina

Date & Time: Jul 14, 2006
Type of aircraft:
Operator:
Flight Type:
Survivors:
Yes
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was completing a flight to Geneina, carrying an unknown number of people and a load consisting of 30 tons of ammunitions. After touchdown at Geneina Airport, the four engine aircraft was unable to stop within the remaining distance. It overran and came to rest few dozen metres further in a field, broken in several pieces. There were no casualties.

Crash of a Tupolev TU-134AK at Simferopol-Gvardeyskoye AFB

Date & Time: Jul 10, 2006
Type of aircraft:
Operator:
Registration:
05 red
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Gvardeyskoye AFB - Moscow-Chkalovsky
MSN:
63875
YOM:
1981
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
22
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll from Simferopol-Gvardeyskoye AFB, the captain started the rotation and the nose gear lifted up. At the same time, the left engine exploded. The captain decided to abandon the takeoff procedure and started an emergency braking procedure. Few seconds were necessary for the nose to land back on runway then the aircraft was unable to stop within the remaining distance. It overran, lost its undercarriage and came to rest, bursting into flames. All 28 occupants were rescued, among them 3 were slightly injured. The aircraft was totally destroyed by a post crash fire. Among those on board was the Admiral Vladimir Masorin of the Russian Navy who was flying back to Moscow following a general inspection of the military installations in Simferopol.
Probable cause:
Failure and explosion of the left engine at takeoff following a bird strike.

Crash of a Lockheed C-130H Hercules in Abéché: 5 killed

Date & Time: Jun 11, 2006 at 1830 LT
Type of aircraft:
Registration:
TT-PAF
Flight Type:
Survivors:
Yes
Schedule:
N’Djamena – Abéché
MSN:
5141
YOM:
1988
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
In unknown circumstances, the aircraft crashed upon landing at Abéché Airport and came to rest about 200 metres past the runway end, bursting into flames. At least five passengers were killed and several others were injured. The aircraft was destroyed. The accident occurred 30 minutes after the airport closing time at 1800LT.

Crash of a Shaanxi Y-8 in Yao: 40 killed

Date & Time: Jun 3, 2006 at 1500 LT
Type of aircraft:
Operator:
Flight Phase:
Flight Type:
Survivors:
No
Location:
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
35
Pax fatalities:
Other fatalities:
Total fatalities:
40
Circumstances:
While cruising at an altitude of 8,000 metres, the crew encountered icing conditions. In unclear circumstances, the aircraft entered an uncontrolled descent, partially disintegrated in the air and eventually crashed in a bamboo forest located near Yao. The aircraft was totally destroyed and all 40 occupants were killed.

Crash of a Lockheed C-130 Hercules C.1P in Lashkar Gah

Date & Time: May 24, 2006 at 1530 LT
Type of aircraft:
Operator:
Registration:
XV206
Flight Type:
Survivors:
Yes
Schedule:
Kabul - Lashkar Gah
MSN:
4231
YOM:
1967
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
20
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The RAF Hercules was on a routine operational flight providing support to the Provincial Reconstruction Team (PRT) at Lashkar Gar, Afghanistan at the time of the accident. The LKG Tactical Landing Zone (TLZ) is 6,800 feet long by 150 feet wide with a surface of compacted sand and gravel located on the south side of LKG town. The TLZ is used by UK forces and other agencies including the UN and Red Cross. The aircraft took off at 08:50 UTC from Kabul International Airport (KBL) to fly a routine logistics sortie to deliver cargo and personnel to LKG TLZ. After an uneventful medium level transit the aircraft landed at LKG at 10:20 UTC. Using a standard tactical landing technique the aircraft touched down some 500ft in from the runway threshold, reverse thrust was selected and speed reduced without the need for wheel braking. After 3 seconds, as the speed was nearing 70 kts there was a loud bang from the port side of the aircraft in the vicinity of the port main landing gear, the force of which was felt throughout the aircraft. At the same time the flight deck crew saw tyre debris flying up in front of the aircraft and then became aware of structural damage to the number 2 engine. The captain ordered the Emergency Engine Shutdown Drill (EESD) on the number 2 engine. He maintained directional control with nosewheel steering. Immediately after the shutdown of number 2 engine crew members observed a large amount of fuel leaking from the port wing area in the vicinity of the external tank pylon and that there was a fire in the vicinity of No.1 engine. The captain ordered the shut down of the No.1 engine using the EESD. Whilst this drill was carried out crew members observed that the fire was spreading across the whole wing. Realising the severity of the situation the captain brought the aircraft to a halt near the northern end of the landing zone some 6,400 feet from the touchdown point. He ordered the passengers and crew to immediately carry out the Emergency Evacuation Drill. Once all personnel had evacuated the aircraft, fire rapidly destroyed the aircraft and cargo.
Probable cause:
The Board concluded that XV206 was destroyed after detonating an explosive device that was buried in the surface of the LKG TLZ. After extensive investigation the Board concluded that the device was an anti-tank landmine. This resulted in aircraft debris puncturing the port wing fuel tanks, causing a major leak of fuel that ignited, leading to an uncontrollable fire originating in the port wing in the vicinity of the n°1 engine.
The Board concluded that the following contributed to the loss of XV206:
a. The lack of permanent force protection at LKG TLZ allowed uncontrolled access to persons wishing to carry out a hostile act;
b. The TLZ clearance procedures proved to be inadequate for detecting subsurface mines.

Crash of a Gavilán 358 in Nueva Antioquia: 3 killed

Date & Time: May 24, 2006
Type of aircraft:
Operator:
Registration:
ARC-416
Flight Type:
Survivors:
No
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
On final approach to Nueva Antioquia Airport, the single engine aircraft went out of control and crashed, killing all three occupants, two pilots and one passenger.