N736YU

HISTORY OF FLIGHTOn January 11, 2020, at 1801 mountain standard time, a Cessna TR182 airplane, N736YU, was destroyed when it was involved in an accident near Billings, Montana. The pilot and three passengers were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 instructional flight.

The pilot’s wife reported that her husband planned to fly about 1630 and was expected to return to his home about 1730. According to Automatic dependent surveillance-broadcast (ADS-B) data, following its departure from Billings Logan International Airport (BIL), Billings, Montana, the airplane landed at Big Horn County Airport (00U), Hardin, Montana about 1715 and subsequently departed about 1740. Flight data retrieved from a multi-function display (MFD) on the airplane showed that the airplane began an immediate climb after it departed 00U and established its cruise altitude, about 4,796 ft msl at 1747:43 and maintained a similar altitude and a height above terrain (between 1,400 and 2,100 ft agl) for the remainder of the flight.

According to ADS-B data, the airplane then flew a straight track northwest towards Roundup, Montana (about 269° magnetic) until about 1753:53 when the airplane made a slight left turn to 257° and continued along this heading for the remainder of the recording. MFD data showed rising terrain about 40 seconds before the airplane crashed. The airplane was at an altitude of 4,954 ft msl (35 ft agl) when the data ended at 1801:22 about 1/2 nautical mile from the airplane’s initial impact point. The pilot’s wife contacted local law enforcement about 2000 when he did not return home.

According to the participants who flew with the accident pilot, he normally flew about 1,000 ft agl level over terrain and would use the autopilot “altitude hold” function for many flights. They also observed that he did not fly with a Federal Aviation Administration sectional chart as he relied mostly on the map on his MFD for terrain and chart information.

According to the accident pilot’s business partner, based on a photograph taken by one of the rear seat passengers that had been sent to her during the accident flight, the accident pilot was in the right seat of the airplane during the accident flight. According to those who flew with the pilot, during these flights he would allow his passengers to fly the airplane from the left seat if they chose to and they would typically fly anywhere between 4,000 and 5,000 ft msl to destinations south, east, and north of the airport.

A passenger who flew with the accident pilot about one week prior to the accident reported that they flew to 00U, but then flew south and circled a landmark before returning to BIL. During the flight, they maintained an altitude of about 1,000 ft agl and used the autopilot for one leg of the flight. A review of other flight data retrieved from the MFD showed that the pilot typically flew at altitudes between about 1,000 and 2,000 ft agl during these flights.

The MFD flight data also showed that the pilot completed a leg from 00U to Roundup Airport (RPX), Roundup, Montana, several days before the accident. This track showed the airplane depart 00U about 1653 and flew a similar course as the accident flight. During cruise flight, the airplane passed within 0.3 nautical mile of the 185-ft radio tower that it impacted on the day of the accident. This part of the flight occurred at 1716 during cruise flight at an altitude of 4,680 ft msl (580 ft agl). The flight landed at RPX about 15 minutes later.

PERSONNEL INFORMATIONThe co-owner of the accident airplane, who knew the accident pilot for 47 years, stated that the pilot started flying in 1972, that he did most of his flying and flight instructing in Billings, and was familiar with the area.

According to the pilot’s wife, the pilot was well rested on the day of the accident and did not exhibit any abnormal behavior that day or in the days that preceded the accident.

AIRCRAFT INFORMATIONThe airplane was equipped with an Aspen Evolution primary flight display (PFD and a Garmin GTN750 MFD. The Aspen Evolution was installed in front of the left seat occupant and drew barometric altitude information from its own internal air data computer, displaying that information on a digital tape on the right side of the display. The barometric altitude was adjustable by altimeter setting, which was displayed below the altitude tape. According to the Aspen installation manual, the altitude tape display should be within 40 ft of the calibrated test altitude. The altimeter setting at the time of the accident could not be determined as the Aspen unit did not record data. An Aspen MFD was located next to the PFD that was mounted to the instrument panel in front of the left seat occupant. Likewise, this unit did not record data.

The GTN750 was a touchscreen MFD mounted on the center instrument panel that was equipped with an obstacle range option and topography overlay available on the unit’s map page. According to a representative of the MFD manufacturer, the GPS altitude or “GSL” altitude, which is computed by satellite geometry, would have been displayed in the top left corner of the MFD’s map page. According to the Garmin pilot’s guide, the obstacle range could display unlighted obstacles below 1,000 ft agl. A representative from Garmin stated that the obstacle range would not have displayed obstructions below 200 ft agl.

The GTN750 also recorded pressure altitude and barometric altitude that was taken from the Aspen air data computer. The last data point recorded showed the barometric altitude was 4,954 ft msl and the GPS altitude was 4,747 ft GSL about the time of the accident.

AIRPORT INFORMATIONThe airplane was equipped with an Aspen Evolution primary flight display (PFD and a Garmin GTN750 MFD. The Aspen Evolution was installed in front of the left seat occupant and drew barometric altitude information from its own internal air data computer, displaying that information on a digital tape on the right side of the display. The barometric altitude was adjustable by altimeter setting, which was displayed below the altitude tape. According to the Aspen installation manual, the altitude tape display should be within 40 ft of the calibrated test altitude. The altimeter setting at the time of the accident could not be determined as the Aspen unit did not record data. An Aspen MFD was located next to the PFD that was mounted to the instrument panel in front of the left seat occupant. Likewise, this unit did not record data.

The GTN750 was a touchscreen MFD mounted on the center instrument panel that was equipped with an obstacle range option and topography overlay available on the unit’s map page. According to a representative of the MFD manufacturer, the GPS altitude or “GSL” altitude, which is computed by satellite geometry, would have been displayed in the top left corner of the MFD’s map page. According to the Garmin pilot’s guide, the obstacle range could display unlighted obstacles below 1,000 ft agl. A representative from Garmin stated that the obstacle range would not have displayed obstructions below 200 ft agl.

The GTN750 also recorded pressure altitude and barometric altitude that was taken from the Aspen air data computer. The last data point recorded showed the barometric altitude was 4,954 ft msl and the GPS altitude was 4,747 ft GSL about the time of the accident.

WRECKAGE AND IMPACT INFORMATIONThe airplane wreckage was located in mountainous terrain at an elevation of about 4,252 ft msl. All major sections of the airplane were accounted for at the accident site. The initial impact point was marked by several bent cross members and a broken guy wire about 65 ft high (4,809 ft msl) on an about 185-ft-tall radio tower, which was located on a peak with a field elevation of about 4,744 ft msl. Several sections of the outboard left wing (not shown in figure 1) were located about 100 ft north of the tower, and two pieces displayed longitudinal signatures consistent with impacting a wire. The remaining section of the left wing was found in the debris path about 350 ft from the main wreckage. Several airframe and engine fragments were distributed along the energy path, which was oriented on a heading of about 295º. The main wreckage was found about 1,450 ft northwest of the initial impact point in a coulee and included the right wing, fuselage, empennage, and engine. A 5-ft intermediate ground scar was located about 250 ft beyond the main wreckage.

Figure 1: Wreckage diagram and photograph of impacted tower

The left wing was fragmented, and some sections were found near the tower. The control cables to the rudder, aileron, and elevator were recovered but exhibited multiple overload failures. The flap motor actuator measured 0.1 inch, consistent with a retracted flap position.

The engine crankshaft could only be partially rotated due to damage sustained during the impact. The ignition system displayed signatures consistent with normal operation and wear. Internal inspection of the case did not reveal any indications of oil starvation. The cylinder combustion chambers remained mechanically undamaged, and there was no evidence of foreign object ingestion or detonation.

ADDITIONAL INFORMATIONTower

According to FAA Advisory Circular 70/7460-1L, under Chapter 2.1 “Structures to be Marked or Lighted”:

“Any temporary or permanent structure, including all appurtenances, that exceeds an overall height of 200 feet above ground level or exceeds any obstruction standard contained in 14 CFR Part 77 should be marked and/or lighted. However, an FAA aeronautical study may reveal that the absence of marking and/or lightning will not impair aviation safety. Conversely, the object may present such an extraordinary hazard potential that higher standards may be recommended for increased conspicuity to ensure aviation safety.”

The excerpt continues to describe FAA action on struct...