Crash of a Britten Norman BN-2B-21 Islander in Devil's Hole

Date & Time: Nov 3, 2013 at 1020 LT
Type of aircraft:
Operator:
Registration:
G-CIAS
Flight Phase:
Survivors:
Yes
Schedule:
Guernsey - Guernsey
MSN:
2162
YOM:
1982
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
25200
Captain / Total hours on type:
60.00
Circumstances:
At approximately 1830 hrs on 3 November 2013 the operator’s duty pilot received a request that the aircraft should be dispatched to carry out a search. The volunteer crew-members were alerted and made their way to the airport. Weather conditions in the Channel Islands were poor, with a southerly wind gusting up to 41 kt, turbulence, rain, cloud below 1,000 ft aal, and visibility of 3 to 6 km. On arrival at the aircraft’s hangar, the crew was established, consisting of a pilot, search director, and three observers. They donned immersion suits and life jackets and prepared for flight. The search director obtained details of the search request, which was to search for two fishermen near Les Écréhous (a group of rocks in the English Channel approximately 5 nm north-east of the north-eastern corner of Jersey). Some evidence suggested the men were in a small dinghy; other information was that they were in the water. The men were reported to be alive and communicating by mobile telephone. One crew-member carried out pre-flight preparations, although he did not check the fuel quantities or carry out a water drain check. When interviewed, he recalled having reported to the pilot that he had not checked the fuel. The aircraft was then pulled out of its hangar and the search director explained the details of the search request to the pilot and other crew-members. Bearing in mind the weather, the fact that it was dark, and the fishermen’s predicament, the pilot recognized the need for “a lot of urgency” about the task. In the context of the operation, he regarded the task as being routine, but the weather not so. The pilot “walked round” the aircraft, though he did not carry out a formal pre-flight inspection; it was the organization’s custom to ensure that the aircraft was ready for flight at all times. The technical log showed that the aircraft was serviceable, with no deferred defects, and that the wing tanks contained 55 USG each side and the tip tanks, 18 USG each side. The search director recalled asking the pilot whether he was content to fly in the prevailing conditions, and that the pilot stated that he was willing to fly. The crew boarded the aircraft. The observer in the front right-hand seat had recently obtained a Private Pilot’s Licence and this influenced the decision for him to be placed next to the pilot. The pilot reported that he carried out a “fairly rapid” start, although the normal pre-departure sequence was interrupted while a problem with switch selections, affecting the functioning of the search equipment in the aircraft’s cabin, was resolved. The pilot obtained clearance from ATC to taxi, enter the runway, and take off when ready. He described that he carried out engine power checks during a brief back-track, checking the magnetos and propeller controls at 2,100 rpm, before carrying out pre-takeoff checks. He did not refer to the written checklists provided in the aircraft but executed a generic set of checks from memory. Following an unremarkable takeoff, in the strong crosswind , the pilot corrected for drift and established a climb towards a cruising altitude of 900 ft. When interviewed, he described the conditions as being “awful” and “ghastly”, with turbulence from the cliffs contributing to occasional activation of the stall warner, even though the speed was “probably 100 plus knots” . At 900 ft, the aircraft was “in the bottom” of the cloud, which was unhelpful for the observers, so the pilot descended the aircraft to cruise at 500 or 600 ft, flying by reference to the artificial horizon, and making constant control inputs to maintain straight and level flight. He stated that, although he would normally have begun checking fuel flow, mixture settings, etc, shortly after establishing in the cruise, he found that the conditions required him to devote his full attention to flying the aircraft. As the aircraft passed north abeam the western end of Jersey, the rain and low cloud continued and the turbulence worsened, The pilot gained sight of red obstacle lights on a television mast on the north side of the island but had few other visual references. The pilot noticed a change in an engine note. He immediately “reached down to put the hot air on” which made little difference; the observer recalled that the pilot checked that the mixtures were fully rich at this time. The right-hand engine rpm then began surging. The pilot made a quick check of the engine instruments, before applying full throttle on both engines, setting both propellers to maximum rpm and beginning a climb. The observer noticed that the fuel pressure gauge for the right-hand engine was “going up and down” but did not mention this to the pilot; the pilot did not see the gauge indication fluctuating. Around this time the pilot switched the electric fuel pumps on. The pilot turned the aircraft towards Jersey and made a MAYDAY call to ATC; the search director made a similar call on the appropriate maritime frequency. These calls were acknowledged, and a life boat, on its way to Les Écréhous, altered course towards the aircraft’s position. Although the pilot was “amazed” at how few lights he could see on the ground, he perceived what he thought was the runway at Jersey Airport, and flew towards it. The aircraft reached approximately 1,100 ft amsl. The right-hand engine then stopped. The pilot carried out the shut-down checks, feathering the propeller as he did so. The aircraft carried on tracking towards Jersey Airport, descending towards the north side of the island. Some moments later, the left-hand engine’s rpm began to fluctuate briefly before it also stopped. The pilot later recalled being “fairly certain” that he “was trying to change tanks” but acknowledged that he could not recall events with certainty. He trimmed the aircraft for a glide, still heading towards the airport at Jersey, but with very limited visual references outside the cockpit. The crew-members prepared the cabin for a ditching or off-airport landing; the observers in the rear-most seats considered how they might deploy the aircraft’s life raft (stored behind their seats) should a ditching occur. The pilot’s next recollection was that the automated decision height voice call-out activated (he had selected it to announce at 200 ft radio height). He switched the landing lights on and maintained a “reasonable speed” in anticipation of landing or ditching. One crew-member recalled the pilot calling “brace, brace, brace”, while another recalled being instructed to tighten seat belts and brace. No brace position had been set out in the operations manual, or rehearsed in training, and the responses of the crew-members to this instruction varied. The pilot glimpsed something green in front of the aircraft, and flared for landing. The aircraft touched down and decelerated, sliding downhill and passing through a hedge. With the aircraft now sliding somewhat sideways, it came to a halt when its nose lodged against a tree, with significant airframe damage. The pilot made various cockpit selections safe and all the occupants vacated the aircraft, with some difficulty. The search director became entangled in his headset lead as he egressed but freed himself. The front seat occupants experienced difficulty because their door could not be opened. They climbed over the search director’s desk and vacated the aircraft via the door adjacent to the search director’s position (the rear-row observers simultaneously opened the pilot’s door from the outside). The pilot and crew made their way to nearby habitation where they were subsequently assessed by an ambulance crew; none were injured. The search director returned to the aircraft with fire-fighters, to ensure that pyrotechnics and the self-inflating life raft on board the aircraft did not pose a hazard. In his very frank account of the flight, the pilot acknowledged that a decision to turn back soon after departure would have been justified by the weather conditions. He added that before the engine power changed, his workload was already very high, on account of the task and conditions.
Probable cause:
The inspection of the aircraft at the accident site, combined with the crew accounts gathered early in the AAIB accident investigation, indicated that no mechanical or electrical defect had been a factor in the accident. The evidence indicated that the fuel supply to the right-hand engine, and then the left-hand engine, had become exhausted in flight and the engines ceased producing power approximately 15 minutes after the aircraft became airborne. The fuel selector was found in the 'tip tank' position. It appears that the tip tanks had been selected on a flight the previous day and the selection had not been changed. At the commencement of the accident flight, each tip tank contained approximately 5-6 USG.
Final Report:

Crash of a De Havilland DHC-8-202 near Acandí: 4 killed

Date & Time: Oct 5, 2013 at 0100 LT
Registration:
N356PH
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Panama City - Panama City
MSN:
502
YOM:
1997
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The aircraft departed Panama City-Marcos A. Gelabert Airport in the evening on an anti-narcotic survey flight over Colombia, carrying four passengers and two pilots, five US citizens and one Panamanian. En route, while cruising along the border between Panama and Colombia, the aircraft collided with trees and crashed on the slope of a wooded mountain, bursting into flames. All four passengers were killed and both pilots were seriously injured.

Crash of a Cessna T207 Turbo Skywagon in Colorado Springs

Date & Time: Sep 4, 2013 at 0758 LT
Registration:
N211AS
Flight Phase:
Survivors:
Yes
Schedule:
Colorado Springs – Lubbock
MSN:
207-0259
YOM:
1974
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5200
Captain / Total hours on type:
18.00
Aircraft flight hours:
13482
Circumstances:
The pilot reported that he performed the takeoff with the airplane at gross weight and with the flaps up and the engine set for maximum power, which he verified by reading the instruments. During the takeoff, the airplane accelerated and achieved liftoff about 65 to 70 mph and then climbed a couple hundred feet before the pilot began to lower the nose to accelerate to normal climb speed (90 to 100 mph). The airplane then stopped climbing and would not accelerate more than 80 mph. While the pilot attempted to maintain altitude, the airplane decelerated to 70 mph with the engine still at the full-power setting. With insufficient runway remaining to land, the pilot made a shallow right turn toward lower terrain and subsequently made a hard landing in a field. The pilot likely allowed the airplane to climb out of ground effect before establishing a proper pitch attitude and airspeed for the climb, which resulted in the airplane inadvertently entering a “region of reversed command” at a low altitude. In this state, the airplane may be incapable of climbing and would require either more engine power or further lowering of the airplane’s nose to increase airspeed. Because engine power was already at its maximum and the airplane was at a low altitude, the pilot was unable to take remedial action to fly out of the region of reversed command.
Probable cause:
The pilot’s failure to establish the proper pitch attitude and airspeed during takeoff with the engine at maximum power, which resulted in the exceedance of the airplane’s climb performance capability.
Final Report:

Crash of a Beechcraft MC-12W 204 km NE of Kandahar: 4 killed

Date & Time: Apr 27, 2013 at 1243 LT
Type of aircraft:
Operator:
Registration:
09-0676
Flight Phase:
Survivors:
No
Site:
Schedule:
Kandahar - Kandahar
MSN:
FL-676
YOM:
2008
Flight number:
Independence 08
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
1749
Captain / Total hours on type:
242.00
Copilot / Total flying hours:
2434
Copilot / Total hours on type:
38
Circumstances:
On 27 April 2013, at approximately 1243 local time (L) in Afghanistan, an MC-12W, tail number 09-0676 impacted terrain 110 nautical miles northeast of Kandahar Airfield (KAF) while on a combat intelligence, surveillance, and reconnaissance (ISR) mission. The four crewmembers on board were the Mishap Mission Commander (MMC), Mishap Pilot (MP), Mishap Sensor Operator (MSO), and Mishap Tactical Systems Operator (MTSO). The four airmen were killed instantly on impact and the Mishap Aircraft (MA), valued at $19.8 million, was destroyed. The crew and MA were deployed to the 361st expeditionary Reconnaissance Squadron, 451st Air Expeditionary Wing, KAF, Afghanistan. The MA, callsign Independence 08, departed KAF at 1157L and entered orbit at 1229L. The MA encountered deteriorating weather in the orbit and was climbing from 20,000 to 23,000 feet mean sea level (MSL) at 1241L to fly above the weather when the mishap occurred. In addition, the crew had found an enemy combatant and was in the process of adjusting their orbit to enhance mission success.
Probable cause:
Accident Investigation Board was conducted by USAF Brigadier General Donald J. BACON. His conclusion were as follow:
I find by clear and convincing evidence the cause of the mishap was a stall due to insufficient airspeed, while in a climbing left turn, which developed into a left spin followed quickly by a high-speed spiral, from which the crew was unable to recover. Additionally, I find, by a preponderance of evidence, each of the following three factors substantially contributed to the mishap:
orbit weather that impeded visibility and masked the horizon;
pilot inexperience in the MC-12W;
known MC-12W program risks associated with sustaining required combat capability in theater.
Final Report:

Crash of a Partenavia P.68 Observer in Roskilde: 2 killed

Date & Time: Mar 6, 2013 at 1727 LT
Type of aircraft:
Operator:
Registration:
OY-CAG
Survivors:
No
Schedule:
Billund - Roskilde
MSN:
243-03-0B
YOM:
1981
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
13973
Aircraft flight hours:
8370
Aircraft flight cycles:
8400
Circumstances:
The aircraft was engaged in a bird control mission over the center of Denmark and departed Billund Airport in the afternoon with one passenger and one pilot on board. While returning to Roskilde, on approach to runway 03, the pilot initiated a go-around procedure due to the presence of a slower aircraft on the runway. While climbing, the twin engine aircraft stalled and crashed near runway 03. Both occupants were killed.
Probable cause:
The final approach and the go-around procedures were non-standard. The accident was caused by a stall during the climb, and the distance between the aircraft and the ground was insufficient to expect recovery. Weather conditions were not considered as a contributing factor.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain near Bontang: 4 killed

Date & Time: Aug 24, 2012 at 0810 LT
Operator:
Registration:
PK-IWH
Flight Phase:
Survivors:
No
Schedule:
Samarinda - Bontang
MSN:
31-7852065
YOM:
1978
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
17547
Captain / Total hours on type:
4250.00
Aircraft flight hours:
16743
Aircraft flight cycles:
14830
Circumstances:
On 24 August 2012, a Piper Chieftain PA-31-350 aircraft, registered PK-IWH, was being operated by PT. Intan Angkasa Airservice to conduct an aerial survey (aero magnetic) flight at a survey area located north of Bontang, East Kalimantan. There were 4 persons on board; one pilot, one security officer and two surveyors. Based on the flight plan submitted by the Pilot in Command (PIC) to the Briefing Office, the flight was planned with an altitude of 3,000 feet AMSL en-route and 500 feet AGL while surveying the area. The fuel endurance was for 6 hours flight time and the aircraft equipped with an Emergency Locator Transmitter (ELT). The aircraft departed from Temindung Airport (WALS), Samarinda at 0751 local time (LT - 2351 UTC). At 0004 UTC, the pilot informed to the Temindung Control Tower controller (Temindung Tower) that the aircraft was abeam Tanjung Santan descending from 3,000 feet and established contact with Bontang Info officer (Bontang Info). At 0005 UTC, the pilot informed the Bontang Info that the aircraft altitude was 300 feet and estimated over Bontang at 0011 UTC. Bontang info acknowledged this transmission and advised the pilot to report when the flight left the Bontang Area. At 0010 UTC, the SureTrack (flight following system) stopped receiving data from the aircraft. The last recorded information was an aircraft speed of 138 knots, heading 352°, latitude 0°8’33” N and longitude 117°12’54” E. At 0600 UTC, the engineer of the PK-IWH aircraft asked the Temindung Tower about the flight as the fuel endurance had been exceeded. The Temindung Tower contacted Bontang Info to get information about the aircraft. After receiving the request, Bontang Info tried to contact the pilot twice and there was no reply. Bontang Info also contacted the Tanjung Bara Airstrip to request information about the aircraft but there was no information. The Temindung Tower reported that:
• at 0610 UTC declared INCERFA (Uncertainty phase);
• at 0630 UTC declared ALERFA (Alert phase);
• at 0700 UTC declared DETRESFA (Distress phase).
At 0730 UTC, the search and rescue team was assembled; the team consisted of the Temindung Airport Authority, National Search and Rescue, Indonesian Police, Army and Airforce. The search operation was conducted via ground and air using three helicopters. On 26 August 2012 at 0850 UTC, the aircraft wreckage was located by a ground search team on a ridge of Mayang Hill, Bontang at approximately 1,200 feet AMSL at coordinates 00°12’34.3”N, 117°16’57.3”E, 12 NM from Bontang Aerodrome on bearing of 294°. The accident site was within the planned aircraft survey area. All occupants were fatally injured and the aircraft was destroyed by impact force and post impact fire.
Probable cause:
The accident was typical of a Controlled Flight into Terrain (CFIT). Low altitude VFR flying in a low visibility environment limited the pilot’s visibility and increased the probability of impact with terrain.
Final Report:

Crash of a Piper PA-31-310 Navajo C off Jacarepaguá

Date & Time: Jul 24, 2012 at 1610 LT
Type of aircraft:
Operator:
Registration:
PT-WOT
Survivors:
Yes
Schedule:
Jacarepaguá - Jacarepaguá
MSN:
31-7912021
YOM:
1979
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine aircraft was engaged in a survey flight off the State of Rio de Janeiro and departed Jacarepaguá-Roberto Marinho Airport in the afternoon. While returning to his base, the pilot encountered problems and decided to ditch the aircraft. The airplane came to rest few hundred metres offshore. All three occupants were rescued and the aircraft sank.

Crash of a PZL-Mielec AN-2R in Padali

Date & Time: Jul 19, 2012
Type of aircraft:
Registration:
RA-40934
Flight Phase:
Survivors:
Yes
Schedule:
Pobeda - Pobeda
MSN:
1G216-14
YOM:
1985
Flight number:
9201
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was engaged in a patrol flight (fire survey) from Pobeda when the engine failed in flight due to low oil pressure. The crew attempted an emergency landing on the road from Komsomolsk-on-Amur to Elban, near Padali (58 km from Komsomolsk). The aircraft suffered damage to the left main gear and the left lower wing and was damaged beyond repair. All three occupants escaped uninjured.
Probable cause:
Engine failure in flight following a loss of oil pressure.

Crash of a Rockwell Shrike Commander 500S off El Loa: 2 killed

Date & Time: May 18, 2012 at 0150 LT
Operator:
Registration:
CC-CGX
Flight Phase:
Survivors:
No
Schedule:
Iquique - Iquique
MSN:
500-3306
YOM:
1978
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
20183
Captain / Total hours on type:
10000.00
Copilot / Total flying hours:
3755
Copilot / Total hours on type:
2137
Aircraft flight hours:
16308
Circumstances:
The twin engine aircraft departed Iquique-General Diego Aracena Airport at 2115LT on May 17 on a fishing survey and prospection mission over the Pacific Ocean, carrying two pilots. There was sufficient fuel on board for a 7,5-hour flight. While cruising by night, the aircraft entered an uncontrolled descent and crashed in the sea about 30 km northwest of El Loa. Few debris were found floating on water the following morning. Both occupants were killed.
Probable cause:
A loss of control in flight for unknown reasons.
Final Report:

Crash of a Cessna 550 Citation II in Manas: 3 killed

Date & Time: Mar 28, 2011 at 1945 LT
Type of aircraft:
Operator:
Registration:
B-7026
Flight Phase:
Survivors:
No
Site:
Schedule:
Korla - Korla
MSN:
550-0305
YOM:
1982
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Owned by the Zhongfei General Aviation Company (CFGAC), the airplane was engaged in a survey flight over the north China province of Xinjiang. It departed Korla Airport at 1600LT with a crew of three. En route, it crashed in unknown circumstances in the Manas County, Hui autonomous prefecture of Changji. SAR did not find any trace of the aircraft nor the crew. Fatal index is presumed.