19990617007179A

Accident · Substantial damage

FAA accident report · Bell 206B3 · Erwinna, PA · June 17, 1999

Date
June 17, 1999 · 10:00 local
Place
Erwinna, PA
Phase of flight
Low Level Operations
Operating rules
Agricultural (Part 137)
Operator
NDBG
Damage
Substantial damage
Aircraft
N94WF
NTSB investigation
NTSBNYC99LA147
Reported as
Bell 206B3
Reported engine
Allison 250C20B
Fatal injuries
0
Pilot’s flight hours
10,000 total160 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.

1979 Bell 206B-III helicopter was involved in aerial application over the Delaware river and was flying low over the river when the skids contacted the water, the nose of the acft subsequently dipped into the water, and the main rotor blades then struck the water, other circumstances are unknown. (From .19) on June 17, 1999, about 1012 eastern daylight time, a Bell 206B-III, N94WF, was substantially damaged during a collision with water at tinicum, Pennsylvania. The certificated commercial pilot sustained minor injuries. Visual meteorological conditions prevailed for the local flight that originated from Erwinna, Pennsylvania. No flight plan was filed for the aerial application flight conducted under 14 CFR part 137. According to the pilot, he departed from "landing zone 5," an open field adjacent to the Delaware river. He intended to perform aerial application for 20 minutes, and return to the landing zone. He stated that while spraying for blackfly over the Delaware river, his attention was momentarily diverted, as he was looking at a flow gauge inside the cockpit. The pilot further stated that he flew too low, causing the skids to contact the water. The main rotor blades subsequently struck the water, and the helicopter came to rest on its side, in approximately 3 feet of water, about 2 to 3 miles from the landing zone. Examination of the wreckage by a federal aviation administration inspector did not reveal any pre-impact mechanical malfunctions, nor did the pilot report any. (-23) pilot looked inside the cockpit to check a flow meter at which time a skid contacted the water. (.4) the pilot was performing aerial application over the Delaware river. He stated that his attention was momentarily diverted, as he was looking at a flow gauge inside the cockpit. The pilot further stated that he flew too low, causing the skids to contact the water. The main rotor blades subsequently struck the water, and the helicopter came to rest in the river.

As the FAA filed it

1979 BELL 206B-III HELICOPTER WAS INVOLVED IN AERIAL APPLICATION OVER THE DELAWARE RIVER AND WAS FLYING LOW OVER THE RIVER WHEN THE SKIDS CONTACTED THE WATER, THE NOSE OF THE ACFT SUBSEQUENTLY DIPPED INTO THE WATER, AND THE MAIN ROTOR BLADES THEN STRUCK THE WATER, OTHER CIRCUMSTANCES ARE UNKNOWN. (FROM .19) ON JUNE 17, 1999, ABOUT 1012 EASTERN DAYLIGHT TIME, A BELL 206B-III, N94WF, WAS SUBSTANTIALLY DAMAGED DURING A COLLISION WITH WATER AT TINICUM, PENNSYLVANIA. THE CERTIFICATED COMMERCIAL PILOT SUSTAINED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE LOCAL FLIGHT THAT ORIGINATED FROM ERWINNA, PENNSYLVANIA. NO FLIGHT PLAN WAS FILED FOR THE AERIAL APPLICATION FLIGHT CONDUCTED UNDER 14 CFR PART 137. ACCORDING TO THE PILOT, HE DEPARTED FROM "LANDING ZONE 5," AN OPEN FIELD ADJACENT TO THE DELAWARE RIVER. HE INTENDED TO PERFORM AERIAL APPLICATION FOR 20 MINUTES, AND RETURN TO THE LANDING ZONE. HE STATED THAT WHILE SPRAYING FOR BLACKFLY OVER THE DELAWARE RIVER, HIS ATTENTION WAS MOMENTARILY DIVERTED, AS HE WAS LOOKING AT A FLOW GAUGE INSIDE THE COCKPIT. THE PILOT FURTHER STATED THAT HE FLEW TOO LOW, CAUSING THE SKIDS TO CONTACT THE WATER. THE MAIN ROTOR BLADES SUBSEQUENTLY STRUCK THE WATER, AND THE HELICOPTER CAME TO REST ON ITS SIDE, IN APPROXIMATELY 3 FEET OF WATER, ABOUT 2 TO 3 MILES FROM THE LANDING ZONE. EXAMINATION OF THE WRECKAGE BY A FEDERAL AVIATION ADMINISTRATION INSPECTOR DID NOT REVEAL ANY PRE-IMPACT MECHANICAL MALFUNCTIONS, NOR DID THE PILOT REPORT ANY. (-23) PILOT LOOKED INSIDE THE COCKPIT TO CHECK A FLOW METER AT WHICH TIME A SKID CONTACTED THE WATER. (.4) THE PILOT WAS PERFORMING AERIAL APPLICATION OVER THE DELAWARE RIVER. HE STATED THAT HIS ATTENTION WAS MOMENTARILY DIVERTED, AS HE WAS LOOKING AT A FLOW GAUGE INSIDE THE COCKPIT. THE PILOT FURTHER STATED THAT HE FLEW TOO LOW, CAUSING THE SKIDS TO CONTACT THE WATER. THE MAIN ROTOR BLADES SUBSEQUENTLY STRUCK THE WATER, AND THE HELICOPTER CAME TO REST IN THE RIVER.

NTSB investigation

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