19970925028999A

Accident · Destroyed

FAA accident report · Bell 206B · Anahuac, TX · September 25, 1997

Date
September 25, 1997 · 13:30 local
Place
Anahuac, TX
Phase of flight
To Vertical (Helicopter Only)
Operating rules
Rotorcraft external load (Part 133)
Operator
GURL
Damage
Destroyed
Aircraft
N59396
NTSB investigation
NTSBFTW97LA364
Reported as
Bell 206B
Reported engine
Allison 250C20B
Fatal injuries
0
Pilot’s flight hours
12,525 total1,000 in this make and model30 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.

Pilot reported collective and cyclic problems after picking up sling load. Lost control. No anomalies found. (.4) the helicopter impacted in a marshy area at a high rate of descent with very low forward speed approximately 100 feet west of his water pick up point. He helicopter was performing sling load operations transporting water in a 100 gallon bambi bucket suspended by a 100 foot long line. There were no reported eyewitnesses to the accident. A ground impression corresponding to the water bucket was found approximately 200 feet to the west of the resting place of the main wreckage. The 3 to 5 foot tall grass on the southern portion of the hole made by the water bucket was found pushed or laid back in a southerly direction. Deep impressions corresponding to the steel cable being utilized in conjuction with the external load were found aft of the toe for the left skid tube, at the attaching point where it attaches to the crosstube. No similar impressions were found on the other skid or crosstube assemblies. No evidence of pre-impact mechanical failure or malfunction was found within the helicopter or related components. The commercial pilot had accumulated a total of 4 hours operating with a 100 foot sling. (-23) see narrative # FTW97LA364

As the FAA filed it

PILOT REPORTED COLLECTIVE AND CYCLIC PROBLEMS AFTER PICKING UP SLING LOAD. LOST CONTROL. NO ANOMALIES FOUND. (.4) THE HELICOPTER IMPACTED IN A MARSHY AREA AT A HIGH RATE OF DESCENT WITH VERY LOW FORWARD SPEED APPROXIMATELY 100 FEET WEST OF HIS WATER PICK UP POINT. HE HELICOPTER WAS PERFORMING SLING LOAD OPERATIONS TRANSPORTING WATER IN A 100 GALLON BAMBI BUCKET SUSPENDED BY A 100 FOOT LONG LINE. THERE WERE NO REPORTED EYEWITNESSES TO THE ACCIDENT. A GROUND IMPRESSION CORRESPONDING TO THE WATER BUCKET WAS FOUND APPROXIMATELY 200 FEET TO THE WEST OF THE RESTING PLACE OF THE MAIN WRECKAGE. THE 3 TO 5 FOOT TALL GRASS ON THE SOUTHERN PORTION OF THE HOLE MADE BY THE WATER BUCKET WAS FOUND PUSHED OR LAID BACK IN A SOUTHERLY DIRECTION. DEEP IMPRESSIONS CORRESPONDING TO THE STEEL CABLE BEING UTILIZED IN CONJUCTION WITH THE EXTERNAL LOAD WERE FOUND AFT OF THE TOE FOR THE LEFT SKID TUBE, AT THE ATTACHING POINT WHERE IT ATTACHES TO THE CROSSTUBE. NO SIMILAR IMPRESSIONS WERE FOUND ON THE OTHER SKID OR CROSSTUBE ASSEMBLIES. NO EVIDENCE OF PRE-IMPACT MECHANICAL FAILURE OR MALFUNCTION WAS FOUND WITHIN THE HELICOPTER OR RELATED COMPONENTS. THE COMMERCIAL PILOT HAD ACCUMULATED A TOTAL OF 4 HOURS OPERATING WITH A 100 FOOT SLING. (-23) SEE NARRATIVE # FTW97LA364

NTSB investigation

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