Landing (descent or approach)

While on an IFR clearance, the pilot reported to approach control that he was unable to maintain 4,000 feet msl, and did not give a reason. Shortly thereafter, the pilot contacted approach control and stated that he had "fuel starvation" in the right engine and the left engine had just quit. Radar data depicted the aircraft at an altitude of 3,400 feet. The controller asked the pilot if they were completely without power, and the pilot responded, "yes, we're now gliding." The controller gave the pilot instructions to the nearest airport, which was approximately 4.5 nautical miles away. After passing 2,100 feet, the pilot informed the controller that he would be landing short. During the forced landing, the airplane struck the top of a tree, crossed over a house, struck another tree, struck a telephone wire which crossed diagonally over a street, and then cleared a set of wires which paralleled the street. The airplane then impacted a private residence within a residential area, and a fire erupted damaging the airplane and the private residence. Ten gallons of fuel were drained from the left locker tank, which supplements the left main fuel tank. Examination of the airframe and engines did not disclose any structural or mechanical anomalies that would have prevented normal operation. Examination of the propeller revealed that neither propeller had been
feathered.

On final approach to Nassau-Lynden Pindling Airport, the crew encountered engine problems. The aircraft lost height and crashed in the Lake Killarney near the airport. All five occupants were rescued while the aircraft was damaged beyond repair.

On January 16, 2002, at approximately 09:24 UTC, a Boeing 737-300, PK-GWA, ditched into the waters of the Bengawan Solo River, Central Java during a forced landing, following loss of power on both engines as the aircraft was descending through 19,000 ft. The dual engine flame out occurred shortly after the aircraft entered severe cumulonimbus cloud formations with turbulence and heavy rain and ice. The aircraft, owned and operated by PT Garuda Indonesia as Flight GA 421, had departed Ampenan at 08:32 UTC, on a regular scheduled commercial flight with destination Yogyakarta. At departure VMC conditions prevailed. The flight from Ampenan was reported uneventful until its arrival in the Yogyakarta area. The crew stated that they observed cumulonimbus cloud formations on their weather radar. The aircraft descended from cruise altitude of 31,000 ft to 28,000ft as instructed by BALI ATC at 09.08 UTC due to traffic on eastbound at FL290. As they began their descent from FL 280 at 09.13 UTC, prior to entering the clouds at 23,000 feet, the crew noted at the radar screen red cells with two green and yellow areas to the left and right of their intended flight path. The Pilot Flying decided to take the left opening above PURWO NDB. The flight crew prepared to enter turbulence by setting turbulence speed at 280 knots, seatbelt on, engine ignitions on FLT and anti-ice on. Then the Pilot Flying requested to BALI ATC to descend to FL 190 and was cleared by Semarang APP at 09.13 UTC. Shortly after the aircraft entered the area covered by Cumulonimbus cells, the crew noted severe turbulence and heavy precipitation. According to the flight crew interview, the crew noted aircraft electrical power generators loss and they were only having primary engine instrument indications and captain flight instruments, which finally identified both engines flame-out. While in the precipitation, the flight crew attempted at least two engine relights, and one attempt of APU start. As the APU start was initiated, the crew noted total electrical loss of the aircraft. The aircraft descended into VMC conditions at about 8,000 ft altitude. The PIC spotted the Bengawan Solo River and decided to land the aircraft on the river. The crew announced to the flight attendant to prepare emergency landing procedure. The aircraft landed successfully between two iron bridges in the upstream direction, and came to a stop with its nose pointing to the right of the landing path. The aircraft settled down on its belly, with the wings and control surfaces largely intact, and was partially submerged. The evacuation following the landing was successful. Twelve passengers suffered injuries, the flight crew and two flight attendants were uninjured, one flight attendant suffered serious injuries, and another flight attendant was found in the waters of the river and fatally injured.

After touchdown on runway 15 at Chilpancingo-Doctor Alfonso G. Alarcón Airport, the aircraft went out of control, veered off runway to the right, struck several earth mounds and eventually collided with a concrete wall, coming to rest upside down. Four passengers were killed and 14 other occupants were injured. It was reported that the aircraft' speed was excessive at touchdown.

The twin engine airplane departed Madrid-Barajas at 0635LT on a cargo service (flight IBT1278) to Bilbao, carrying one company mechanic, two pilots and a load of cargo consisting of 2,873 kilos of various goods. Following an uneventful flight, the crew was cleared to start the descent to Bilbao-Sondica Airport for an ILS approach to runway 30. During the descent, the crew encountered control problems which he attributed to an autopilot malfunction. While trying to identify the problem, the crew failed to realized that the rate of descent increased when the GPWS alarm sounded three times. Shortly later, while attempting to gain height, the aircraft struck the slope of Mt Santa Marina Vieja located 33 km from Bilbao Airport. The aircraft was destroyed by impact forces and all three occupants were killed. The wreckage was found near the village of Zaldíbar.

Following an uneventful flight from Jacobabad, the crew started a night approach to Shamsi AFB. While descending in limited visibility at the altitude of 3,200 feet, the four engine aircraft struck the slope of a mountain located few km from the airfield. All seven occupants were killed.

The pilot stated that on the day of the accident he ordered fuel only on the first flight of the day. He said he did not add additional fuel during subsequent flights. He said he flew the accident airplane from Fort Lauderdale Executive Airport, Fort Lauderdale, Florida, to Chubb Cay, Bahamas, to Big Whale Cay, Bahamas, back to the Fort Lauderdale Executive Airport. He said he then departed Fort Lauderdale Executive Airport with his next load of passengers and flew to the North Eleuthera Airport, North Eleuthera, Bahamas, without having refueled, and was returning from North Eleuthera, Bahamas, to the Fort Lauderdale International Airport, when he ditched the airplane off Dania Beach, Florida, in the Atlantic Ocean. When asked whether the fuel on board the airplane had been exhausted, the pilot stated, " the way the engines were acting, it seemed like the airplane ran out of fuel." On scene examination of the airplane, as well as follow on examination of its engines revealed no pre accident anomalies with the airplane or its systems. Information obtained from the FAA showed that at 1757, the pilot contacted FAA Miami Approach Control and advised "minimum fuel, further stating that he was not declaring an emergency at that time. At 1758, the controller responded, passing communications control to the FAA Fort Lauderdale Air Traffic Control Tower (ATCT). In response to the pilot's initial communications call to the Fort Lauderdale ATCT, the pilot was given a clearance to land on runway 09R, and told that he was number one. At 1758:43, the pilot replied, asking if there was any chance of getting runway 27L, and at 1759:17, the controller instructed the pilot to descend at his discretion and remain slightly south of final for landing on runway 27L, and to expect 27L. At 1800:07, the pilot contacted the controller and stated, "two five yankee would like to declare an emergency at this time." At 1800:10, the controller responded, "two five yankee yes sir runway two seven left you are cleared to land the wind zero one zero at six." At 1800:16 the pilot responded acknowledging the wind report, and at 1800:27, the controller asked whether the nature of the emergency was minimum fuel, to which the pilot responded, "exactly two five yankee may be coming in dead stick. At 1800:40, the pilot stated that he had the airport in sight and will try to glide, and at 1801:32, the pilot said "two five yankee I'm going to be short of the shore." At 1802, the pilot ditched the airplane about 300 yards from the Dania Beach shoreline, in the area of John Lloyd State Park, in about 15 feet of water. The occupants of the airplane consisted of the pilot and four passengers. All exited the airplane and one passenger drowned in the Atlantic Ocean when according to the pilot "he was in a state of panic" when he tried to instruct him in the use of the life vest while they was in the water, and subsequently tried to use him for flotation when he tried to help him. All remaining passengers confirmed that the pilot had not given them any pre departure safety related briefing prior to or during the accident flight.

The private pilot was accompanied by his wife and his two daughters on a flight from Port Elizabeth to his farm in the Cradock district. On arrival at Cradock, the pilot apparently over-flew the runway for inspection and was on the downwind leg when the aircraft started to roll and yaw to the left. All engine indications were normal and the pilot had to decrease power on the right-hand engine in order to maintain control of the aircraft. With the reduction in power of the right-hand engine, the pilot was unable to maintain height and executed a forced landing on an open field. The aircraft was extensively damaged during the forced landing but no injuries were sustained. An on-site investigation was carried out on 24 December 2000 after which the aircraft was recovered to Lanseria aerodrome for further inspection. On inspection of the Left-hand propeller it was noted that the carbon block of the low pitch proximity sensor, which normally runs inside the Low-Pitch stop collar, was bent down at an angle, which would have rendered the secondary Low-Pitch stop inoperative. Due to the fact that the aircraft sustained damage to it's electronic circuitry it was not possible to verify the proper operation of the propeller pitch control system.

After landing at Lhokseumawe-Malikussaleh Airport, the four engine aircraft went out of control, veered off runway and came to rest in a marshy area, bursting into flames. All 95 occupants were rescued, among them seven passengers were injured. The aircraft was destroyed by a post crash fire.

The flight was cleared for the ILS approach to runway 5R. The flight was at mid runway, at 2,100 feet, heading 049 degrees, at a speed of 163 knots, when the pilot stated "...missed approach." He was instructed to maintain 2,000, and to fly runway heading. Radar showed N41003 started a right turn, was flying away from the airport/VOR, descending. At a point 0.57 miles from the airport/VOR, the flight had descended to 1,500 feet, was turning right, and increasing speed. The flight had descended 400 feet, and had traveled about 0.32 miles in 10 seconds. When radio and radar contact were lost, the flight was 2.35 miles from the airport/VOR, level at 1,600 feet, on a heading of 123 degrees, and at a speed of 169 knots. The published decision height (DH) was 620 feet mean sea level (msl). The published minimum visibility was 1/2 mile. The published Missed Approach in use at the time of the accident was; "Climb to 1,000 [feet], then climbing right turn to 2,500 [feet] via heading 130 degrees, and RDU R-087 [087 degree radial] to ZEBUL Int [intersection] and hold." A witness stated that the aircraft was flying low, power seemed to be in a cruise configuration, and maintaining the same sound up until the crash. The reported weather at the time was: Winds 050 at 5 knots, visibility 1/2 statute mile, obscuration fog and drizzle, ceiling overcast 100, temperature and dew point 11 C, altimeter 30.30 in HG. At the time of the accident the pilot had 10 total flight hours in this make and model airplane; 33 total night flight hours; and 59 total instrument flight hours.