Asheville

The right main landing gear collapsed on landing. According to the flight crew, after departure they preceded to Mountain Air Airport, where they performed a "touch-and-go" landing. Upon raising the landing gear following the touch-and-go landing, they got an "unsafe gear" light. The crew stated they cycled the gear back down and got a "three green" normal indication. They cycled the gear back up and again got the "gear unsafe" light. They diverted to Greensboro, North Carolina, and upon landing in Greensboro the airplane's right main landing gear collapsed. After the accident, gear parts from the accident airplane were discovered on the runway at Mountain Air Airport. Metallurgical examination of the landing gear components revealed fractures consistent with overstress separation and there was no evidence of fatigue. Examination of the runway at Mountain Air Airport by an FAA Inspector showed evidence the accident airplane had touched down short of the runway.

At about the 3,000-foot marker on the 8,000-foot long runway witnesses saw the airplane at about 100 to 150-feet above the ground with the landing gear retracted when they heard a loud "bang". They said the airplane made no attempt to land on the remaining 5,000 feet of runway after the noise. The airplane continued climbing and seemed to gain a little altitude before passing the end of the runway. At that point the airplane began a right descending turn and was in a 60 to 80 degree right bank, nose low attitude when they lost sight of it. The airplane collided with the ground about 8/10 of a mile from the departure end of runway 34 in a residential area. Examination of the critical left engine found no pre-impact mechanical malfunction. Examination of the right engine found galling on all of the connecting rods. Dirt and particular contaminants were found embedded on all of the bearings, and spalling was observed on all of the cam followers. The oil suction screen was found clean, The oil filter was found contaminated with ferrous and non-ferrous small particles. The number 3 cylinder connecting rod yoke was broken on one side of the rod cap and separated into two pieces. Heavy secondary damage was noted with no signs of heat distress. Examination of the engine logbooks revealed that both engine's had been overhauled in 1986. In 1992, the airplane was registered in the Dominican Republic and the last maintenance entry indicated that the left and right engines underwent an inspection 754.3 hours since major overhaul. There were no other maintenance entries in the logbooks until the airplane was sold and moved to the United States in 2002. All three blades of the right propeller were found in the low pitch position, confirming that the pilot did not feather the right propeller as outlined in the pilot's operating handbook, under emergency procedures following a loss of engine power during takeoff.

The pilot had left the airplane at Asheville on the day before the accident due to low cloud ceilings and visibility at Mountain Air Airport, his destination, and completed the trip by rental car. On the day of the accident the pilot returned the rental car and at 1656 departed Asheville in N396PM, enroute to Mountain Air Airport, 27 miles north of Asheville. The last radio contact with the pilot was at 1701:44, when the pilot told controllers at Asheville that he was in visual flight rule conditions, at 4,000 feet. The last radar contact with the flight was by FAA Atlanta Center, at 1704:00, when the flight was about 5 miles south of the accident site at 3,800 feet. The flight did not arrive at the destination, an emergency locator transmitter signal was received by satellite, and search and rescue operations were begun. The pilot and the wreckage of the airplane was located the next day about 1400. The airplane had collided with 75-foot tall trees, at about the 4,800-foot msl level on the side of Bullhead Mountain, while in a wings level attitude, while on a 170 degree heading. After the initial impact the airplane continued for another 300 feet, causing general breakup of the airplane. The main wreckage came to rest on a northerly heading. All components of the airplane were located at the crash site and there was no evidence of precrash failure or malfunction of the airplane structure, flight controls, airplane systems, engine, or propeller. A witness reported that the weather near the time of the accident on the Blue Ridge Parkway, located about 3/4 mile to the west of the crash site, was very foggy. Satellite images show clouds were present at the crash site and the Asheville airport, located 20 miles south-southwest of the crash site, reported overcast clouds 2,600 feet agl or 4,765 feet msl, and visibility 4 miles in haze, at the time of the accident. An Airmet for mountain obscuration due to clouds, mist, and haze was in effect at the time the pilot departed and the at the time of the accident. No record to show that the pilot received a weather briefing from a FAA Flight Service Station was found.

The pilot and aircraft had been fighting forest fires earlier in the day. A late developing fire necessitated another dispatch. The aircraft arrived on scene and checked in with the lead aircraft circling overhead coordinating the fire fighting efforts. The tanker made two runs over the fire area following the lead aircraft. After the second run, the aircraft banked left in a level turn to make another run without using the lead aircraft. During the third run the tanker struck trees near the top of a 1,800 feet ridgeline. Witnesses on the ground remarked how low the aircraft was. According to the pilot's peers, he took pride in doing his job well and always strove to put the chemical right on target. There had been occasions in the past where this zeal to succeed had resulted in his going lower than the 150 feet agl minimum altitude mandated by forestry service regs. He had, on occasions, returned to base with tree foliage stuck in his aircraft. The pilot, sole on board, was killed.

After a missed approach at Asheville the flight was cleared to the Greenville-Spartanburg Airport at Greer, SC. Enroute to Greer radar contact was lost. In response to a query from Atlanta artcc the pilot verified his position as being on the 235° radial of Spartanburg VOR and 11.9 miles southwest. He was then cleared to descend to 2,700 feet and execute an ILS approach. The aircraft impacted a mountain at the 3,200 feet level. The wreckage was found on the 235° radial of the Sugarloaf mountain vortac and at 24 miles. Review of the aircraft's logbook revealed that mechanical irregularities reported were not corrected for long periods of time. No corrective action was listed for an "outer marker inop aural and visual (needs to be fixed now, since ADF is also inoperative) and 'light in #2 VOR head out'. The marker beacon was described as inoperative on three dates beginning 22 August 1981 and the ADF was described as inoperative on seven dates beginning 8 May 1981. No corrective action was listed for any entry about the marker beacon or ADF. The pilot, sole on board, was killed.

The three engine aircraft departed Asheville Regional Airport at 1158LT and climbed to its assigned altitude. About three minutes later, while climbing to an altitude of 6,132 feet in a limited visibility due to clouds, the aircraft collided with a Cessna 310 registered N3121S. Operated by Lanseair, it was carrying two passengers and a pilot. Following the collision, both aircraft dove into the ground and crashed in a dense wooded area located about nine miles southeast of Asheville Airport. The wreckage of the 727 was found in a forest along a highway located in Hendersonville. All 82 occupants in both aircraft were killed.