Greeley

The twin-tubofan airplane overran the runway during an aborted takeoff, impacting two fences before coming to rest. The pilot reported experiencing no anomalies with the airplane during the preflight inspection and taxi portion of the flight. During takeoff roll, at V1 (103 knots), the pilot began to pull aft on the control yoke. The pilot noticed the nose landing gear was not coming off of the runway and at 120 knots, with full aft control input, elected to abort the takeoff. He pulled the power to idle and applied maximum braking. Upon seeing the localizer antennas approaching the airplane at the departure end of the runway, the pilot veered the airplane to the right of centerline. The airplane departed the runway surface and impacted the fences. Post-accident examination of the runway revealed tire skid marks on the runway that led to the airplane's final resting place. The tire skid marks measured 1,765 feet in length. Examination of the wreckage revealed no pre-existing brake system anomalies that would have hindered the airplane's braking capability. Examination of the elevator trim system revealed it was 12 degrees out of trim in the nose down direction. The airplane underwent a Phase B and Phase 1 through 5 inspections approximately 5 months prior to the accident. The manufacturer's inspection manual indicates the elevator system should be examined every Phase 5 inspection. The aircraft's flight manual informs the pilot that the right elevator and trim tab should be inspected during the exterior inspection to ensure the elevator trim tab position matches its indicator.

N3554p was on a maintenance test flight after the right wing was repaired. The pilot lost control of the airplane shortly after liftoff and was unable to regain control prior to the ground impact. The a&p mechanic who performed the repairs, re assembled the right wing aileron control cables per the Piper service manual. Post accident examination of the aileron control system revealed the right wing control cables were reversed on the aileron bellcrank, resulting in both ailerons moving the same direction (either up or down) when the control wheel was turned left or right. Both occupants were seriously injured.

The pilot was on a flight from Greeley to Denver, Colorado to obtain minor maintenance on a cargo door. As the aircraft was being vectored on final approach, the pilot reported that he believed the aircraft had fuel starvation. Subsequently, the aircraft was observed to make a complete roll and crash in a residential area. Only about 1.5 gallon of fuel was found in the right wing tank. The left wing and fuel tank were destroyed, but no odor of fuel was noted on the ground around the left wing. Also, a lack of fuel was noted in the fuel lines. The aircraft had not been refueled after the previous flight. The pilot that had flown the aircraft on a previous flight estimated there was 100 lbs of fuel remaining in each tank after his flight.

The aircraft diverted from Scottsdale to a flight course to Sedona because of thunderstorms and high winds at Scottsdale, but after a radio conversation with Scottsdale tower, the pilot decided to reroute to land at Scottsdale. The pilot did not read back the weather correctly to Scottsdale tower. After descending in rain and turbulence, the pilot reported to Scottsdale at 1857 that 'we think we have the arpt at nine o'clock.' the plt was cleared to make a visual approach to rwy 21. The twr never established visual contact with the acft & was unable to make further radio contact the last recorded radar contact showed the acft at 2200 ft descending, 2 miles from scottsdale on a bearing of 075 degrees. The acft contacted the ground left wing & nose low in a landing configuration on a heading of about 300 degrees. The acft slid about 770 ft, losing the engines, wings & landing gear before stopping. A post accident examination of the wreckage showed no signs of pre-impact conditions that would have affected normal operations.