20170802010269A

Accident · Substantial damage

FAA accident report · Air Tractor AT-402B · San Angelo, TX · August 2, 2017

Date
August 2, 2017 · 17:38 local
Place
San Angelo, TX
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N38HT
NTSB investigation
NTSBGAA17CA469
Reported as
Air Tractor AT-402B
Reported engine
Pratt And Whitney T74-GP-702
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
6,960 total240 in this make and model88 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

This was a research flight related to weather modification. The aircraft had a spray system that put an electrical charge on the water as it exited the spray boom. There were researchers on the ground collecting real time data from the aircraft. The flight began with 350 gallons (400 gallon capacity) of water in the hopper and the intent was to find uplifting conditions (thermals) to spray the water. Uplifting conditions for this flight which had lasted 2.0 hours, were not good, so pilot decided to return to the airport. The hopper still had 281 gallons of water which weighed approximately 2250 pounds. Pilot took this into consideration during the approach knowing that the aircraft was heavier than normal landings with an empty hopper. The remaining fuel on board was approximately 50 gallons. Beginning fuel load was 164 gallons. Pilot used 100 mph as approach speed and set 10 degrees flaps. There was a right crosswind of about 30 degrees at approximately 10 KTS. Pilot had right wing down and left rudder to keep the fuselage straight with runway. As pilot flared for landing, pilot leveled the wings, reduced power to idle, and touched down in a three-point attitude in a full stall with the fuselage straight down the runway. The touch down was right at the end of the threshold and beginning of the runway. The landing was harder than usual, aircraft did not bounce and continued straight down the runway for about 500 feet. The aircraft then began an un-commanded slow turn to the right. I applied heavy left braking and left rudder with no effect. The turn continued to the point where it entered a classic ground loop with fuselage making a reversal of less than 180 degrees. The side load broke the left landing gear off and the left wing settled to the ground and the prop hit the asphalt. The tailwheel did not break off.

As the FAA filed it

THIS WAS A RESEARCH FLIGHT RELATED TO WEATHER MODIFICATION. THE AIRCRAFT HAD A SPRAY SYSTEM THAT PUT AN ELECTRICAL CHARGE ON THE WATER AS IT EXITED THE SPRAY BOOM. THERE WERE RESEARCHERS ON THE GROUND COLLECTING REAL TIME DATA FROM THE AIRCRAFT. THE FLIGHT BEGAN WITH 350 GALLONS (400 GALLON CAPACITY) OF WATER IN THE HOPPER AND THE INTENT WAS TO FIND UPLIFTING CONDITIONS (THERMALS) TO SPRAY THE WATER. UPLIFTING CONDITIONS FOR THIS FLIGHT WHICH HAD LASTED 2.0 HOURS, WERE NOT GOOD, SO PILOT DECIDED TO RETURN TO THE AIRPORT. THE HOPPER STILL HAD 281 GALLONS OF WATER WHICH WEIGHED APPROXIMATELY 2250 POUNDS. PILOT TOOK THIS INTO CONSIDERATION DURING THE APPROACH KNOWING THAT THE AIRCRAFT WAS HEAVIER THAN NORMAL LANDINGS WITH AN EMPTY HOPPER. THE REMAINING FUEL ON BOARD WAS APPROXIMATELY 50 GALLONS. BEGINNING FUEL LOAD WAS 164 GALLONS. PILOT USED 100 MPH AS APPROACH SPEED AND SET 10 DEGREES FLAPS. THERE WAS A RIGHT CROSSWIND OF ABOUT 30 DEGREES AT APPROXIMATELY 10 KTS. PILOT HAD RIGHT WING DOWN AND LEFT RUDDER TO KEEP THE FUSELAGE STRAIGHT WITH RUNWAY. AS PILOT FLARED FOR LANDING, PILOT LEVELED THE WINGS, REDUCED POWER TO IDLE, AND TOUCHED DOWN IN A THREE-POINT ATTITUDE IN A FULL STALL WITH THE FUSELAGE STRAIGHT DOWN THE RUNWAY. THE TOUCH DOWN WAS RIGHT AT THE END OF THE THRESHOLD AND BEGINNING OF THE RUNWAY. THE LANDING WAS HARDER THAN USUAL, AIRCRAFT DID NOT BOUNCE AND CONTINUED STRAIGHT DOWN THE RUNWAY FOR ABOUT 500 FEET. THE AIRCRAFT THEN BEGAN AN UN-COMMANDED SLOW TURN TO THE RIGHT. I APPLIED HEAVY LEFT BRAKING AND LEFT RUDDER WITH NO EFFECT. THE TURN CONTINUED TO THE POINT WHERE IT ENTERED A CLASSIC GROUND LOOP WITH FUSELAGE MAKING A REVERSAL OF LESS THAN 180 DEGREES. THE SIDE LOAD BROKE THE LEFT LANDING GEAR OFF AND THE LEFT WING SETTLED TO THE GROUND AND THE PROP HIT THE ASPHALT. THE TAILWHEEL DID NOT BREAK OFF.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.