Crash of a PZL-Mielec C-145A Skytruck in Walan Rabat

Date & Time: Dec 18, 2011 at 1502 LT
Type of aircraft:
Operator:
Registration:
08-0319
Flight Type:
Survivors:
Yes
Schedule:
Kandahar - Qalat - Walan Rabat - Qalat - Kandahar
MSN:
AJE003-19
YOM:
2009
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3546
Captain / Total hours on type:
434.00
Copilot / Total flying hours:
982
Copilot / Total hours on type:
677
Aircraft flight hours:
1164
Aircraft flight cycles:
1273
Circumstances:
At 0939 hours Zulu time on 18 December 2011, an M-28, Tail Number 08-0319, departed Kandahar Air Base, Afghanistan on a mission to pick up four passengers at Qalat, Afghanistan, transport them to Walan Rabat short takeoff and landing zone, transport two additional personnel from Walan Rabat back to Qalat, then return to Kandahar Air Base. The mishap aircraft and crew were assigned or attached to the 318th Special Operations Squadron, 27th Special Operations Wing at Cannon Air Force Base, New Mexico, and were deployed to the 318th Expeditionary Special Operations Squadron at Kandahar Air Base, Afghanistan. After an uneventful stop at Qalat to onload four passengers and their bags, the mishap crew flew a 20-minute leg to Walan Rabat. Surface winds at Walan Rabat were 190 degrees at 14 knots gusting to 17 knots, 30 degrees off a direct tailwind for runway 34. Because the landing zone has a three percent upslope for runway 34, and a 1,500-foot mountain exists 1½ miles to the north, the pilot elected to land with a tailwind on runway 34, the preferred landing direction. Walan Rabat Landing Zone is a 1,756-foot long, 31-foot wide, semi-prepared dirt strip with poorly defined boundaries. The landing zone was marked with AMP-3 markings, commonly called a “box-and-one” with colored panels. The mishap pilot consulted a wind component chart and incorrectly calculated the tailwind component, mistakenly believing it was within the allowable limit for landing the M-28. The pilot flew a shallow 2½-3 degree approach due to the upsloping landing zone. At approximately 1,000 feet short of the landing zone, the mishap pilot visually acquired the AMP-3 markings and landed the mishap aircraft at 1032 zulu. After a firmer than normal landing, the aircraft veered to the right and departed the prepared surface. The nose gear encountered uneven terrain and collapsed, causing the mishap aircraft to flip tail-over-nose. The mishap crew and passengers then egressed the aircraft through the copilot’s window. There were no serious injuries to crew or passengers. The mishap aircraft, which was valued at approximately $12,300,000 was destroyed. There were no civilian casualties.
Probable cause:
The AIB president found no clear and convincing evidence of the primary cause of the accident. He determined by a preponderance of evidence that the Landing Zone Condition, Cross-Monitoring Performance, Task/Mission-in-Progress Re-planning, Landing with an Excessive Tailwind, and Aircraft Engine Anomalies substantially contributed to the mishap, ultimately causing the mishap aircraft to veer off the prepared surface into rough terrain, resulting in the collapse of the nose landing gear and destruction of the aircraft.
Final Report:

Crash of a McDonnell Douglas C-17A Globemaster III at Elmendorf AFB: 4 killed

Date & Time: Jul 28, 2010 at 1822 LT
Operator:
Registration:
00-0173
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Elmendorf AFB - Elmendorf AFB
MSN:
P-73
YOM:
2000
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The crew was engaged in a training exercise in preparation to the 'Thunder Air Show' taking part at Elmendorf-Richardson AFB on 31JUL2010. Shortly after take off from runway 06, the pilot-in-command initiated a first turn to the left then a steep turn to the right when the aircraft entered an uncontrolled descent and crashed in a huge explosion in a wooded area located some 3 km northwest of the airbase. The aircraft was totally destroyed by impact forces and a post crash fire and all four crew members were killed.
Probable cause:
The board president found clear and convincing evidence that the cause of the mishap was pilot error. The pilot violated regulatory provisions and multiple flight manual procedures, placing the aircraft outside established flight parameters at an attitude and altitude where recovery was not possible. Furthermore, the copilot and safety observer did not realize the developing dangerous situation and failed to make appropriate inputs. In addition to multiple procedural errors, the board president found sufficient evidence that the crew on the flight deck ignored cautions and warnings and failed to respond to various challenge and reply items. The board also found channelized attention, overconfidence, expectancy, misplaced motivation, procedural guidance, and program oversight substantially contributed to the mishap.

Crash of a Learjet C-21A at Talil AFB

Date & Time: Nov 2, 2009 at 1430 LT
Type of aircraft:
Operator:
Registration:
84-0094
Flight Type:
Survivors:
Yes
MSN:
35-540
YOM:
1985
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a positioning flight to Talil AFB (Imam Ali), Iraq. On approach, the aircraft was too high and descended with an excessive speed and a tailwind component of 10 knots. The crew failed to initiate a go-around and the aircraft landed about two-third down the runway. Unable to stop within the remaining distance, the aircraft overran, lost its undercarriage and came to rest in a sandy area about 60 metres past the runway end. Both pilots escaped uninjured while the aircraft was damaged beyond repair and later destroyed by soldiers from the 68th Transportation Company.
Probable cause:
The accident investigation board (AIB) president found clear and convincing evidence that the mishap crew failed to sufficiently reduce speed and altitude during their approach to execute a normal landing, failed to complete the appropriate checklist for a high speed partial flap landing, and failed to recognize that there was insufficient runway remaining to safely land. Finally, the mishap crew failed to initiate a 'Go-Around' to correct the aforementioned deviations. Additionally, the AIB president also found sufficient evidence that skill-based errors, judgment and decision-making errors, cognitive factors, psycho-behavioural factors, coordination, communication and planning factors, and planning inappropriate operations all were substantially contributing factors to the mishap.

Crash of a Boeing E-3C Sentry at Nellis AFB

Date & Time: Aug 28, 2009 at 1800 LT
Type of aircraft:
Operator:
Registration:
83-0008
Flight Type:
Survivors:
Yes
Schedule:
Tinker AFB - Nellis AFB
MSN:
22836/962
YOM:
1983
Crew on board:
4
Crew fatalities:
Pax on board:
28
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following a Red Flag exercice from Tinker AFB, the aircraft was returning to Nellis AFB. Upon landing, the nose gear collapsed and the aircraft slid on the runway for few dozen metres before coming to rest, bursting into flames. All 32 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The nose gear collapsed upon landing for unknown reasons.

Crash of a Boeing B-52H-155-BW Stratofortress off Guam Island: 6 killed

Date & Time: Jul 21, 2008 at 0945 LT
Type of aircraft:
Operator:
Registration:
60-0053
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Andersen AFB - Andersen AFB
MSN:
464418
YOM:
1960
Flight number:
Raider 21
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The aircraft departed Andersen AFB on a flight around the Guam Island under call sign 'Raider 21' with 6 crew members on board, taking part to the Guam Liberation Day celebrations. About 15 minutes into the flight, while descending from 14,000 to 1,000 feet, the aircraft became uncontrollable and crashed in the sea about 50 km north of Guam Island. The aircraft disintegrated on impact and only few debris were found. All six crew members were killed.
Crew:
Maj Chris Cooper, pilot,
Cpt Michael Dodson, copilot,
1st Lt Robert Gerren, electronic warfare officer,
1st Lt Joshua Shepherd, navigator,
Maj Brent Williams, radar navigator,
Col George Martin, flight surgeon.
Probable cause:
Malfunctioning parts and late recognition of spiraling problems likely led to the fatal crash of a B-52H Stratofortress in July, an Air Force accident investigation board concluded in a report issued Feb. 13. The problem parts, investigators decided, were the bomber’s rear stabilizers — the large horizontal fins at the jet’s tail that help angle the B-52H up or down. Although the inquiry could not determine what led to the stabilizer problem, the board said it believed the stabilizers malfunctioned while the bomber was in a fast descent from 14,000 feet to 1,000 feet. “Even an experienced aircrew could have found it difficult to recognize, assess and recover from the very rapidly developing situation involving the rear stabilizer trim,” board president Brig. Gen. Mark Barrett concluded. The bomber did not carry a flight data recorder, so the investigation team pieced together events leading up to the crash from air traffic control radar information and from parts recovered from the ocean floor by remote-controlled Navy submarines. One recovered part was a component called a jackscrew that helps control the stabilizers. The jackscrew revealed the stabilizer trim was set at 4.5 to 5 degrees nose down, but parts that could have helped determine why the stabilizers were pointed down were not recovered. Based on flight simulations, the investigative team determined the flight was normal until the jet turned left and began to descend about 33 miles west of Guam. As the 48-year-old bomber dove toward the Pacific at a speed of more than 240 mph, the stabilizers suddenly unhinged, putting the jet into a dive with the nose pointed down 30 degrees and more. One of the pilots likely tried to level the stabilizers manually using a control wheel in the cockpit that moves the stabilizer 1 degree every two to three seconds, the report said. However, because the plane was already low, there wasn’t enough time to level the stabilizers. At least three crew members tried to bail out seconds before the plane hit the water, but the plane’s speed, altitude and angle already were past the point where they could survive the ejection.