Fort Myers

The pilot reported visually checking the main fuel tanks during his preflight inspection of the airplane and later reported there was enough fuel for the intended flight which would be less than 1 hour, plus a 45-minute reserve amount of fuel. He estimated the fuel level in the main fuel tanks was 2-3 inches from the top. He also reported that before the accident flight he had never flown the accident make and model airplane, and that he had not had any flight training in the airplane. The passengers were boarded, the flight departed and climbed to between 4,500 and 6,500 feet msl. He leaned the mixture during cruise, and the flight continued. He began descending when the flight was 12 miles from the destination airport, and he performed the pre landing checks when the flight was 3 miles from the destination airport. The flight entered left downwind where he lowered the landing gear and turned on the fuel pumps. When abeam the landing point he reduced power, lowered the flaps 10 degrees, and turned onto base leg. During the base leg while rolling out of the turn and flying at 600 feet, "the right engine suddenly came to a stop...." He banked to the left to maintain zero sideslip, pushed the mixture, propeller, and throttle controls full forward, and identified the right engine had failed. He reportedly pulled the right propeller control to the feather position but during the postaccident investigation, the right propeller blades were not in the feather position and there was no evidence of preimpact failure or malfunction of the propeller. The pilot further reported that while pulling the right propeller control to the feather position, the airplane, "began to yaw right and simultaneously bank right...." He moved the left throttle control to idle, and they were on the ground in a span of 6 seconds from the time the right engine quit. No fuel leakage was noted at the scene, and no fuel contamination was noted in a nearby pond. Additionally, only residual fuel was noted in the fuel lines in each engine compartment. A total of 4.0 and 1.5 gallons of fuel were drained from the left and right auxiliary fuel tanks, respectively. No evidence of preimpact flight control failure or malfunction was noted. Neither propeller was at or near the feather range at the time of impact. Both engines were removed from the airplane, placed on a test stand with a "club" propeller, and both engines were noted to operate normally during the engine run. Examination of the right seat in the third row of the airplane revealed the seat frame was bent down on the left side, and all seat feet were in position but distorted; no fracture of the seat feet were noted. Examination of the seat of the passenger who sustained minor injuries (left seat in the third row) revealed the seatpan was compressed down, and the lapbelt was unbuckled. The inboard arm rest was bent inward, and the outboard arm rest was bent outward. The seat frame indicated displacement to the left. The seat back was twisted counter clockwise, and the left forward seat foot was in place. The seat and attach structure was certificated for a maximum forward g loading of 9 g's, and a maximum sideward g loading of 1.5 g's. This does not include a 1.33 margin of safety factor. The seat and attach structure was tested to ultimate loads in a combined forward, sideward, and upward directions in accordance with CAR 3.390-2. The same loads were also applied in a downward direction by itself. The empennage was separated just aft of the aft pressure bulkhead but remained secured by flight control cables. According to personnel from the airplane manufacturer, the tested load (150 percent limit) for the empennage in negative shear translates to 14.0 g loading. Based on Cessna Engineering rough calculations, they believe the empennage is capable of sustaining an additional 30 percent beyond what it was tested to, or an estimated 18.2 g's in negative shear loading.

At 1623:41, the pilot requested taxi clearance. The Green Bay (GRB) tower (ATCT) told the pilot to taxi to runway 18. At 1626:47 the pilot said that he was ready for takeoff. The ATCT local controller (LC) told the pilot, "proceed on course, cleared for takeoff". At 1627:33, radar showed the airplane began to accelerate down runway 18. At 1628:17 the LC told the pilot to contact departure control. The pilot responded, "ah papa charlie we have a little problem here we're going to have to come back." The LC asked the pilot, "what approach would you like?" The pilot responded, "like to keep the vis." At 1628:35, the LC asked the pilot, "like the contact approach that what you're saying?" There was no response from the pilot. At 1628:50, GRB radar showed the airplane on a heading of 091 degrees, at an altitude of 855 feet msl (160 feet agl), and at an airspeed of 206 knots. The airplane was 1.28 miles southeast of the airport radar. Radar contact with the airplane was lost at 1628:55. A witness to the accident said, "It was snowing moderately at that time. The road was wet but not slippery. Crossing the intersection of Morning Glory Rd. & Main St., I noted a white private jet flying from the south. It was flying at approximately a 75-80 degree angle perpendicular to the ground with its left wing down & teetering slightly." The witness said, "It then crossed Main Street with the lower wing tip approximately 20 to 30 feet above the power wires. The plane became more perpendicular to the ground at a 90 degree angle with the left wing down & (and) lost altitude crashing into the Morning Glory Dairy warehouse building." An examination of the airplane revealed no anomalies. At 1638, GRB weather was reported as ceilings of 200 feet broken, 800 feet overcast, visibility 1/2 statute mile with snow and fog, temperature 32 degrees F, dew point 32 degrees F, winds 120 degrees at 3 knots, and an altimeter setting of 29.99 inches Hg. Witnesses at the FBO said the pilot arrived to pick up the airplane after 1600. The pilot was briefed by the mechanic as he did his walk around inspection of the airplane. The pilot then
got into the airplane. The airplane was towed out and the tow bar removed. About two minutes later, the engines started. Less than five minutes after the engines started, the airplane taxied. The NTSB Audio Laboratory reviewed radio communications between ATCT and the pilot to determine from the speech evidence the pilot's level of psychological stress and workload. The examination indicated the pilot's speech characteristics were consistent with an increased stress/workload that might accompany a developing emergency. Referring to the pilot's final transmissions, "His unusually long reaction time suggests that he was distracted by competing cockpit priorities and/or was having a difficult time determining his answer, while his fast speech and microphone keying provide further evidence of an urgency to return to other cockpit activities." The report states that the pilot's statements remained rational and showed good word choice and grammar. "These factors, along with the relatively small change in fundamental frequency, suggest that the pilot did not reach an extreme level of stress."

The aircraft departed Miami at night on an on-demand, air taxi flight to Fort Myers, FL. During arrival at the destination, the flight encountered IFR conditions. The pilot obtained clearance for an ILS runway 06 approach and was told to report at the outer marker (om). At 0152:25 est, he reported to Miami center that he was over the om. This was his last transmission to an ATC facility. At about 0203 est, he made a transmission on unicom frequency to inform airport operations personnel that he could not get the approach lights to operate. He was asked if he had used the proper frequency and had keyed the mike the required number of times. The pilot indicated that he had properly keyed the mike; however, unicom personnel did not hear any keying of the mike except for 2 clicks. The aircraft contacted the ground in a nearly level attitude and with the gear extended, approximately 1.5 mile short of runway 06. It then skidded about 90 feet and hit a tree before coming to rest. No preimpact part failure/malfunction was found with the aircraft, engine or approach/runway lights. The 0149 est weather at Fort Myers was in part: sky obscured, visibility 1/4 mile with fog. While the pilot was seriously injured, the passenger was killed.

Witnesses observed the aircraft taxi to the end of runway 27R and positioned so the tail was out in the overrun area. Witnesses further stated the aircraft appeared to take an overly long takeoff roll before lifting off. After lift off, the aircraft pitched up vertically, climbed to about 100 feet, rolled left inverted, crashed to the ground in a dive on a heading of 035° and burst into flames. The aircraft was 955 pounds over maximum gross weight and the cg was 14.5 inches aft of the most rearward limit. The weight and balance form had been altered to indicate the aircraft was within limits for weight and balance prior to departure. Examination of faa records revealed Air Cargo America had been cited for numerous breaches of federal air regulations and the pilot-in-command had a history of suspensions/revocations of his pilot airman in certificate. A pilot of Air Cargo America reported the company pressured their pilots to operate the aircraft outside the requirements of the federal air regulations. FAA was notified of these practices in 1985. Both occupants were killed.

The aircraft collided with trees and the ground during flight in adverse weather. There is no record of the pilot receiving a pre-flight briefing and no flight plan was filed. Witnesses heard an aircraft flying low followed by a loud thud. About 16 miles north at Sarasota, FL, the 2128 est weather was: 200 feet partial obscuration, visibility 3 miles with fog. Persons in the vicinity of the accident stated that the area had heavy, patchy ground fog. All four occupants were killed.

While in normal cruise on a flight from Panama City to Fort Myers, the twin engine airplane entered an uncontrolled descent. Due to overload failure, it partially disintegrated in the air, losing its left wing and tail section before crashing in an uninhabited area located near Wilma. Both occupants were killed.

The crew was completing a local training flight at Fort Myers Airport. During a simulated single engine approach, the crew initiated a steep turn when the airplane stalled and crashed close to the runway. The aircraft was destroyed by a post crash fire and both occupants were killed.

Lehigh Acres Development, Inc., Flight 701, a Martin 404, N40412, departed from Runway 02R at DeKalb-Peachtree Airport, Chamblee, Georgia, at 0916 e.d.t. on an Instrument Flight Rules flight plan to Fort Myers, Florida. Two pilots, two cabin attendants and 29 passengers were on board. The aircraft had been fueled to approximately 800 gallons prior to departure. The weather at the time of takeoff was: Measured 400 feet overcast, visibility 1 mile with very light rain and fog. Atlanta Departure Control established radar and radio contact with the flight one minute after takeoff. .During the climb, there was a loss of power from the No. 2 engine. This loss rapidly deteriorated to the extent that little useful power was being developed. While the crew was working to correct the discrepancy with the No. 2 engine, the No. 1 engine lost power. The crew declared an emergency and reported that they were going down. Departure Control attempted to vector the aircraft to the Atlanta International Airport for an emergency landing. When the aircraft descended below the overcast, the pilot observed Interstate Highway 285 just below and decided to make an emergency landing on the median strip, heading west. Touchdown on the highway occurred at approximately 0930. The aircraft skidded along the highway for approximately one-half mile, struck the side of the Moreland Avenue bridge, and came to rest on top of the bridge. As the aircraft proceeded along the highway, it struck an automobile that was traveling east and inflicted fatal injuries to the five occupants. One passenger in the aircraft received fatal injuries. The two pilots and one flight attendant received serious injuries. Twenty-seven passengers received injuries requiring medical treatment or hospitalization. The aircraft was destroyed by impact; no fire developed.

An engine failed in flight. All nine crew members decided to bail out and abandoned the aircraft that dove into the ground and crashed in a prairie located two miles north of Fort Myers. Eight crews were found uninjured while one was killed as his parachute failed to open.

Crashed on landing at Fort Myers Airport for unknown reasons. As there was no injury among the occupants, the aircraft was damaged beyond repair.