Cessna 414 Chancellor

Aircraft was substantially damaged when it veered off the runway while landing at Hammonton Municipal Airport (N81), Hammonton, New Jersey. The private pilot was not injured and the commercial pilot-rated passenger received minor injuries. Visual meteorological conditions prevailed, and an instrument flight rules flight plan was filed for the flight. The flight originated from Montgomery County Airpark (GAI), Gaithersburg, Maryland about 1105 and was destined for N81. The personal flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. The airplane was being repositioned to N81 in order for the owner's insurance adjuster and a local mechanic to physically inspect previous claim work for damage done during ground handling following Hurricane Sandy. The pilot reported lowering the landing gear during the approach to runway 03, and confirmed that they were extended by observing the landing gear position indicator lights. Immediately after touchdown, the airplane veered to the left. The pilot applied full right rudder, but the airplane continued to veer to the left. After departing the left side of the runway, the airplane struck several trees and was subsequently engulfed in a post-crash fire. According to FAA records, the pilot held a private certificate, with ratings for airplane single- and multiengine land. His most recent FAA third class medical certificate was issued on January 2, 2013. As of April 5, 2013, the pilot reported a total of 587 total hours of flight experience, of which 120 hours were in the same make and model as the accident airplane. The seven-seat, twin-engine, low-wing, retractable tricycle-gear airplane was manufactured in 1977 and was equipped with two Continental Motors TSIO-520, 520-hp engines. Review of the airplane's maintenance logbooks revealed that its most recent annual inspection was completed on October 26, 2012. At the time of inspection, the airplane had accumulated 9,335 total hours in service. The number one and two engines accumulated approximately 735 and 157 total hours of operation since overhaul, respectively. The airplane had flown about three hours since the most recent annual inspection. The 1154 recorded weather observation at Atlantic City International Airport (ACY), Atlantic City, New Jersey, located about 15 miles southeast of the accident site, included wind from 330 degrees at 13 knots, 10 miles visibility, few clouds at 1,600 feet, temperature 11 degrees C, dew point 4 degrees C, and a barometric altimeter setting of 29.83 inches of mercury. N81 was a non-tower-controlled airport equipped with one asphalt runway, oriented in a 03/21 configuration. The runway was 3,601 feet in length and 75 feet wide. The field elevation for the airport was 65 feet mean sea level.

The twin engine aircraft departed Innsbruck-Kranebitten Airport at 0654LT on a private flight to Valencia, Spain, carrying seven passengers and one pilot. VFR conditions prevailed at the time of departure. After takeoff from runway 26, the pilot turn to the south when he encountered limited visibility due to foggy conditions. In IMC conditions, the aircraft contacted trees, lost height and crashed in a wooded area located near the village of Ellbögen, about 15 km southeast of Innsbruck Airport, bursting into flames. The wreckage was found at an altitude of 1,612 metres. Two passengers were seriously injure while six other occupants were killed. The aircraft was totally destroyed by a post impact fire.

The pilot performed an instrument approach to the runway with an approaching winter storm. A review of on-board global positioning system (GPS) data indicated that the airplane flew through the approach course several times during the approach and was consistently below the glideslope path. The airplane continued below the published decision height altitude and drifted to the right of the runway’s extended centerline. The GPS recorded the pilot’s attempt to perform a missed approach, a rapid decrease in ground speed, and then the airplane descend to the ground, consistent with an aerodynamic stall. Further, the airplane owner, who was also a passenger on the flight, stated that, after the pilot made the two “left turning circles” and had begun a third circle, he perceived that the airplane “just stalled.” An examination of the airframe and engine did not detect any preimpact anomalies that would have precluded normal operation. The airplane’s anti-ice and propeller anti-ice switches were found in the “off” position. A review of weather information revealed that the airplane was operating in an area with the potential for moderate icing and snow. Based on the GPS data and weather information, it is likely that the airframe collected ice during the descent and approach, which affected the airplane’s performance and led to an aerodynamic stall during the climb.

The privately owned Cessna 414A departed Toronto/Buttonville Municipal Airport, Ontario, en route to Sydney, Nova Scotia. The flight was operating under an instrument flight rules flight plan with the pilot-in-command and the aircraft owner on board. Nearing Sydney, the aircraft was cleared to conduct an instrument approach. At the final approach waypoint the pilot was advised to discontinue the approach due to conflicting traffic. While manoeuvring for a second approach, the aircraft departed from controlled flight, entered a rapid descent and impacted the water at 2335 Atlantic Daylight Time. The aircraft wreckage was located using a side-scan sonar 11 days later, in 170 feet of water. The aircraft had been destroyed and both occupants were fatally injured. No signal was detected from the emergency locator transmitter.

The twin engine aircraft departed San Salvador-Ilopango Airport on a private flight to Barranquilla with an intermediate stop in San Andrés Island, carrying one passenger and one pilot. On final approach to San Andrés-Gustavo Rojas Pinilla Airport runway 06, the left engine failed. The pilot increased power on the right engine but the aircraft continued to lose height. The pilot ditched the aircraft near the coast. Both occupants evacuated safely and were quickly rescued while the aircraft was damaged beyond repair.

According to witnesses, the airplane departed runway 35 and was observed flying in and out of the clouds. Several of the witnesses observed the airplane initiate a turn to the west. One witnesses commented that it was dark but he could still see the silhouette of the airplane. He observed the airplane descend below the trees. All of the witnesses reported flames and "fireballs." On scene evidence was consistent with the airplane impacting trees in a left turn. The airplane was destroyed. An examination of the airplane, flight controls, engines, and remaining systems revealed no anomalies. Weather observations and radar data depicted low clouds, and restricted visibility due to rain and mist, in the vicinity of the airport. Toxicological examination revealed cetirizine, an antihistamine, consistent with use within the previous 12 hours. Most studies have not found any significant impairment from the medication, though it is reported to cause substantial sedation in some individuals.

The 2,212-hour instrument rated commercial pilot collided with terrain while circling to land after completing an instrument approach to an uncontrolled non-towered airport. The airport had two instrument approaches to Runway 14; a VOR and a RNAV(GPS). The published minimums for a circling approach to Runway 32 are a 500 foot ceiling and one mile visibility (VOR14) and a 700 foot ceiling and one mile visibility for RNAV(GPS) to Runway 14. The weather at the airport at the time of the accident was reported as 300 overcast, visibility of 3/4 of a mile in mist, with winds from 020 degrees at 10 knots gusting to 14 knots. Two witnesses reported that the airplane circled over the airport and then descended straight to the ground. Radar data revealed that after the airplane made the instrument approach to Runway 14, at approximately 2,800 feet mean sea level (msl), the airplane initiated a circling turn to the left and a slight descent. The last radar hit showed the airplane at 2,600 feet at a groundspeed of 186 knots. A post impact fire consumed some of the airframe. The pilot's logbooks were not located during the course of the investigation and his instrument experience and currency could not be determined. The pilot was reported to be very familiar with the airport and the 2 instrument approaches. A detailed examination of the wreckage of the airplane failed to reveal any anomalies with the airframe, structure, or systems. Flight control continuity was established at the accident site. The engines were examined, and no mechanical anomalies were found. The propellers were shipped to the manufacturer's facility for examination and teardown. Both propellers were rotating at the time of ground impact. Neither of the two propellers was found in the feathered position. Blade damage was consistent with both propellers operating under power at the time of impact. No mechanical defects were noted with either propeller.

The airplane encountered in-flight icing, and the pilot diverted to an airport to attempt to knock the ice off at a lower altitude. During the instrument approach, the pilot advised the tower controller of the ice, and that it depended on whether or not the ice came off the airplane if she would land. As the airplane broke out of the clouds, it appeared to tower personnel to be executing a missed approach; however, it suddenly "dove" for the runway. The tower supervisor noticed that the landing gear were not down, and at 75 to 100 feet above the runway, advised the pilot to go around. The airplane continued to descend, and by the time it impacted the runway, the landing gear were only partially extended, and the propellers and airframe impacted the pavement. The pilot then attempted to abort the landing. The damaged airplane became airborne, climbed to the right, stalled, and nosed straight down into the ground.