Aerial photography

Carrying one pilot, a navigator and a photographer, the aircraft departed Lae on a photographic survey flight over the Wewak area, but conditions proved unfavourable for photography and it was decided to return to Lae. Lae tower was called five minutes before arrival and landing instructions were passed, in which it was advised that Runway 32 was to be used, the wind velocity being 300 degrees at 15 knots with gusts to 20 knots. Just before turning on to base leg the aircraft was cleared to do a practice asymmetric landing, but was warned to expect turbulence on the final approach. This was acknowledged by the aircraft. Witnesses agree that the aircraft was very low at the time of entering the final approach from a right-hand base leg with the left-hand propeller feathered. They also agreed that, following what sounded to be a marked increase in the power setting when 300 yards from the end of the strip, the aircraft rolled to the left and dived into the water in a partly inverted attitude. All three occupants perished.
Crew:
Allen Motteram, pilot,
Patrick Murphy, navigator,
Passenger:
Gordon Murrell, photographer.

At 0735 hours, the aircraft departed Horn Island with only the normal crew on board to conduct aerial photography over the northern portion of the Cape York Peninsula. The aircraft returned to Horn Island at about midday and was refueled to full tanks. The crew lunched with the crew of World Wide Aerial Surveys Hudson VH-SMM which was also conducting aerial photography in the area. After lunch the three passengers boarded VH-AGO which set course for Weipa Mission at 1516 hours. At 1523 hours, Captain Linfoot advised the communication station on Thursday Island that he was returning to Horn Island with engine trouble and requesting that VH-SMM be held on the ground at Horn Island to render assistance if required. Following a baulked approach at Horn Island, the aircraft crashed on a tidal mud shelf 1.25 miles north-west of Horn Island Aerodrome at approximately 1535 hours. It was subsequently established that the port engine had seized as a result of a master rod bearing failure. The inquiry determined that VH-AGO had a total time of 3083 hours with 260 hours since last overhaul.
The following account of the accident is extracted from "Aviation Safety Digest":
"The aircraft was temporarily based at the Weipa Mission aerodrome, northern Queensland, with the normal crew consisting of a pilot, a navigator and a photographic assistant. On the day before the accident the aircraft was flown on a private flight from Weipa Mission to the Horn Island aerodrome with three non-paying passengers aboard in addition to the crew. The aircraft remained overnight at Horn Island, and early on the following morning took off with the normal crew, and carried out survey work over a period of some four hours. The aircraft returned to Horn lsland at about midday and was refueled. During the same morning another Hudson aircraft (VH-SMM of WWAS. Ed.) engaged on photographic survey work had arrived at the aerodrome and the two crews lunched together. Both aircraft were prepared for departure and the three passengers again boarded the Weipa Mission aircraft, which took-off first and set course at 1518 hours E.S.T. intending to climb to 7,000 feet en route for Weipa, 45 minutes flying time to the south. Five minutes after departure the pilot of this aircraft advised the communication station at Thursday Island that trouble had developed in the port engine and that he was returning, to land at Horn Island. He also asked that the other Hudson aircraft be held on the ground in case some assistance was needed. At the stage that this message was relayed to the captain of the second Hudson the aircraft was lined up for take-oft but immediately vacated the strip. The captain watched the circuit and approach of the other aircraft from a position clear of, but adjacent to, the threshold of Runway 08. The returning aircraft was seen to cross Runway 08 and then turn downwind at a height of 1,500-1,700 feet and proceed with a left-hand circuit towards the threshold of that runway. As the aircraft turned on to final approach at about the normal distance from the threshold but still unusually high, the ground observers noticed that the undercarriage had not been extended. The aircraft continued to descend in this configuration and it seemed likely at this stage that a wheels-up landing would be made well down the strip. When the aircraft had reached a point approximately 600 feet from the threshold and 150 feet above ground level the undercarriage was observed to extend and it was also noticed that the port propeller was feathered. At this point there appeared to be no wing flap extended and the aircraft crossed the strip threshold at a height of more than 100 feet and at a speed estimated to be well in excess of the normal approach speed. Soon after the aircraft had passed the threshold it was seen to roll and turn to port and this motion continued until the aircraft disappeared from view at such a height and angle of bank that an accident seemed imminent. The pilot of the Hudson on the ground immediately took-off and located the wrecked aircraft on a coral mud shelf just beyond the northern shore of the island. Ground parties discovered that the aircraft had been virtually destroyed by very high impact forces and the six occupants had lost their lives."
Those on board at the time of the crash were:
Joseph (Joe) Linfoot (Captain)
Hermione Ivy (Josie) Linfoot (Wife of the Captain)
Graham Holstock (Navigator)
Harold Corrigan (Camera Operator)
William Frank Mitchell (Director of Mitchell Aerial Services Pty Ltd, Cairns)
Lionel Kenneth George Jeffery (a pilot intending to join Adastra).
Source & photos:
http://www.adastron.com/adastra/aircraft/hudson/vh-ago.htm

Crashed while taking off at Manchester-Ringway Airport. All three occupants were killed.

The crew was performing a flight to Ulyanovsk to conduct aerial photography of the airplane on behalf of the UAZ factory. While approaching Ulyanovsk at an altitude of 3,000 meters, the left wing suffered a structural failure and partially detached and struck the tail. Out of control, the aircraft dove into the ground and crashed in a snow covered field located 15 km northeast of Ulyanovsk. The airplane was destroyed and all four crew members were killed.

Owned by Jorgen C. Mortensen, the twin engine aircraft was enroute from Copenhagen-Kastrup Airport to Aarhus, in charge to perform an aerial photography mission. On approach to Tirstrup Airport, the airplane crashed in unknown circumstances and was destroyed. Both occupants were rescued.

The aircraft was carrying two filmmakers and one pilot who were in charge to make a movie of the Heathrow Airport. Following an uneventful mission, the pilot returned to the airport when, on final approach, the right engine suffered technical problems and failed. In a certain confusion, the pilot mistakenly shut down the left engine, causing the aircraft to stall and to crashed short of runway. All three occupants were evacuated while the aircraft was written off.

While descending to Alcañiz, an engine failed. The crew attempted to make an emergency landing when the aircraft crash landed in a field and hit an obstacle before coming to rest. A passenger was killed while three other occupants were injured. They were conducting an aerial photography mission from Madrid.

A first Lisunov LI-2 left Krasnoyarsk Airport at 1755LT bound for Novosibirsk with an assigned altitude of 2,100 meters. At 1840LT, a second Lisunov LI-2T registered CCCP-A4031 left Novosibirsk Airport bound for Kemerovo with a crew of seven who were involved in an aerial photography mission. While approaching Kemerovo, the captain of the first LI-2 modified his route and flight level without prior permission and passed north of Kemerovo. In excellent weather conditions, while cruising at an altitude of 1,800 meters to a heading of 270° and facing the sun, the first LI-2 was hit on its right wing and right engine by the second LI-2 that was flying from the opposite. Following the collision, both aircraft dove into the ground and crashed in a wooded area located 16,5 km west of Barzas. Debris were found on a greater distance than 600 meters and all 27 occupants on both aircraft were killed.

Shortly after takeoff, the twin engine aircraft suffered an engine failure resulting in its crossing the Centre Dandenong Road beneath the 20 feet high telephone wires which were strung along each side of the road before striking an earth embankment and two fences, tearing off the port wing. While all three crew members were slightly injured, the aircraft was damaged beyond repair.

While approaching Santander following an aerial photography mission, the twin engine aircraft crashed on a hilly terrain near Novales. All four occupants were killed.