General Atomics MQ-9

Palmdale, CA — November 25, 2019

Event Information

DateNovember 25, 2019
Event TypeACC
NTSB NumberDCA20CA028
Event ID20191126X70448
LocationPalmdale, CA
CountryUSA
Coordinates34.57111, -117.66889
AirportGray Butte
Highest InjuryNONE

Aircraft

MakeGeneral Atomics
ModelMQ-9
CategoryAIR
FAR Part091
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious0
Minor0
None0
Total Injured0

Event Location

Probable Cause

Incorrect control inputs by the student pilot during a crosswind landing, resulting in control saturation and a runway excursion.

Full Narrative

On November 25, 2019, at 1052 Pacific standard time (PST), N341HK a General Atomics Aeronautical Systems (GA-ASI) MQ-9 unmanned aircraft system (UAS), sustained substantial damage after departing runway 26 when landing during a training flight at the Gray Butte airport, Palmdale, California. The flight was operated by GA-ASI as a routine pilot and sensor operator training flight. The flight departed Gray Butte, and was conducted under the provisions of 14 CFR Part 91 and an FAA Certificate of Authorization (COA). There were no injuries or other damage.

At 1058 PST, the automated surface observation system at Gray Butte reported clear skies with wind from 260 at 18 knots, variable from 220 degrees to 290 degrees, with a peak wind of 270 degrees at 28 knots.

According to the operator/manufacturer, the student pilot was pilot-flying and the aircraft touched down at 79 knots indicated airspeed (KIAS) crabbed to the left approximately 5 degrees, consistent with a 7 knot crosswind component from the left. Upon touchdown, the aircraft began drifting to the left with the nose wheel off the ground. Over approximately the next 15 seconds, increasing right rudder was applied as the aircraft continued to drift left. Pitch stick position was +9 degrees (with pitch trim set to -5 degrees, pitch command was +4 degrees, 2 degrees above recommended pitch in the Flight Manual). The throttle was not moved to ground idle or reverse. A go-around was initiated, but the aircraft departed the runway before the engine could respond.

Operator/manufacturer examination of data logs systems information revealed that since the autopilot prioritizes pitch control over yaw control for movement of the ruddervators, the atypically high pitch command limited the ruddervator authority available for yaw control. With the ruddervators saturated in pitch, yaw authority from the ventral rudder alone was insufficient to effect a right yaw.

The flight manual did not have any information about the possibility of pitch control prioritization resulting in limited yaw authority.

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

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