19990224001729A

Accident · Substantial damage

FAA accident report · Bell 206L-1 · Barrow, AK · February 24, 1999

Date
February 24, 1999 · 17:30 local
Place
Barrow, AK
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N785SR
NTSB investigation
NTSBANC99TA029
Reported as
Bell 206L1
Reported engine
Allison 250C30
Fatal injuries
0
Pilot’s flight hours
17,000 total314 in this make and model99 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.

1980 Bell Textron 206L-1 helicopter crashed on landing and sustained substantial damage. Other circumstances are unknown. (.19) on February 24, 1999, about 1730 Alaska standard time, a high skid equipped Bell 206L-1 helicopter, N785SR, sustained substantial damage during landing, about 4 miles south of Barrow, Alaska. The helicopter was being operated as a public use, visual flight rules (VFR) local area search and rescue flight under title 14, CFR part 91, when the accident occurred. The helicopter was registered to the north slope borough, and was operated by the north slope borough search and rescue of Barrow. The airline transport pilot and the two passengers aboard received minor injuries. Visual meteorological conditions prevailed, and VFR company flight following procedures were in effect. During a telephone conversation with the national transportation safety board investigator-in-charge on February 24, the chief pilot reported that the accident helicopter was being utilized to search for a missing person. He said that shortly after initiating the search, the pilot was able to locate the missing person on a frozen lake. The chief pilot indicated that as the pilot approached the lake for landing, the pilot became disoriented due to whiteout conditions. The helicopter struck the frozen lake, and rolled over onto its right side. The helicopter sustained substantial damage to the fuselage, tail boom, and drive train components. The closest oficial weather observation station is Barrow, located about 4 nautical miles north of the accident site. On February 24, at 1753, an aviation routine weather report (METAR) was reporting in part: wind, 070 degrees at 13 knots; visibility, 3 miles with light snow; clouds, 2,400 feet scattered, 3,800 feet broken, 10,000 feet overcast; temperature, minus 7 degrees f; dew point, minus 13 degrees f; altimeter, 29.81 inhg. The pilot reported that there were no preaccident mechanical anomalies with the helicopter. (-23) during landing to an area without visual references in a large snow covered field, the pilot encountered flat light conditions. He attempted a go-around too late. The helicopter contacted the ground and rolled onto it's side. (.4) the pilot reported that the public use helicopter was being utilized to search for a missing person. He said that shortly after initiating the search, he was able to locate the missing person on a frozen lake. He indicated that as he approached the lake for landing, he became disoriented due to whiteout conditions. The helicopter struck the frozen lake, and rolled onto its right side. The helicopter sustained substantial damage to the fuselage, tail boom, and drive train components. The closest official weather observation station is Barrow, located about 4 nautical miles north of the accident site. On February 24, at 1753, an aviation routine weather report (METAR) was reporting in part: wind, 070 degrees at 13 knots; visibility, 3 miles with light snow; clouds, 2,400 feet scattered, 3,800 feet broken, 10,000 feet overcast; temperature, minus 7 degrees f; dew point, minus 13 degrees f; altimeter, 29.81 inhg. The pilot reported that there were no preaccident mechanical anomalies with the helicopter.

As the FAA filed it

1980 BELL TEXTRON 206L-1 HELICOPTER CRASHED ON LANDING AND SUSTAINED SUBSTANTIAL DAMAGE. OTHER CIRCUMSTANCES ARE UNKNOWN. (.19) ON FEBRUARY 24, 1999, ABOUT 1730 ALASKA STANDARD TIME, A HIGH SKID EQUIPPED BELL 206L-1 HELICOPTER, N785SR, SUSTAINED SUBSTANTIAL DAMAGE DURING LANDING, ABOUT 4 MILES SOUTH OF BARROW, ALASKA. THE HELICOPTER WAS BEING OPERATED AS A PUBLIC USE, VISUAL FLIGHT RULES (VFR) LOCAL AREA SEARCH AND RESCUE FLIGHT UNDER TITLE 14, CFR PART 91, WHEN THE ACCIDENT OCCURRED. THE HELICOPTER WAS REGISTERED TO THE NORTH SLOPE BOROUGH, AND WAS OPERATED BY THE NORTH SLOPE BOROUGH SEARCH AND RESCUE OF BARROW. THE AIRLINE TRANSPORT PILOT AND THE TWO PASSENGERS ABOARD RECEIVED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND VFR COMPANY FLIGHT FOLLOWING PROCEDURES WERE IN EFFECT. DURING A TELEPHONE CONVERSATION WITH THE NATIONAL TRANSPORTATION SAFETY BOARD INVESTIGATOR-IN-CHARGE ON FEBRUARY 24, THE CHIEF PILOT REPORTED THAT THE ACCIDENT HELICOPTER WAS BEING UTILIZED TO SEARCH FOR A MISSING PERSON. HE SAID THAT SHORTLY AFTER INITIATING THE SEARCH, THE PILOT WAS ABLE TO LOCATE THE MISSING PERSON ON A FROZEN LAKE. THE CHIEF PILOT INDICATED THAT AS THE PILOT APPROACHED THE LAKE FOR LANDING, THE PILOT BECAME DISORIENTED DUE TO WHITEOUT CONDITIONS. THE HELICOPTER STRUCK THE FROZEN LAKE, AND ROLLED OVER ONTO ITS RIGHT SIDE. THE HELICOPTER SUSTAINED SUBSTANTIAL DAMAGE TO THE FUSELAGE, TAIL BOOM, AND DRIVE TRAIN COMPONENTS. THE CLOSEST OFICIAL WEATHER OBSERVATION STATION IS BARROW, LOCATED ABOUT 4 NAUTICAL MILES NORTH OF THE ACCIDENT SITE. ON FEBRUARY 24, AT 1753, AN AVIATION ROUTINE WEATHER REPORT (METAR) WAS REPORTING IN PART: WIND, 070 DEGREES AT 13 KNOTS; VISIBILITY, 3 MILES WITH LIGHT SNOW; CLOUDS, 2,400 FEET SCATTERED, 3,800 FEET BROKEN, 10,000 FEET OVERCAST; TEMPERATURE, MINUS 7 DEGREES F; DEW POINT, MINUS 13 DEGREES F; ALTIMETER, 29.81 INHG. THE PILOT REPORTED THAT THERE WERE NO PREACCIDENT MECHANICAL ANOMALIES WITH THE HELICOPTER. (-23) DURING LANDING TO AN AREA WITHOUT VISUAL REFERENCES IN A LARGE SNOW COVERED FIELD, THE PILOT ENCOUNTERED FLAT LIGHT CONDITIONS. HE ATTEMPTED A GO-AROUND TOO LATE. THE HELICOPTER CONTACTED THE GROUND AND ROLLED ONTO IT'S SIDE. (.4) THE PILOT REPORTED THAT THE PUBLIC USE HELICOPTER WAS BEING UTILIZED TO SEARCH FOR A MISSING PERSON. HE SAID THAT SHORTLY AFTER INITIATING THE SEARCH, HE WAS ABLE TO LOCATE THE MISSING PERSON ON A FROZEN LAKE. HE INDICATED THAT AS HE APPROACHED THE LAKE FOR LANDING, HE BECAME DISORIENTED DUE TO WHITEOUT CONDITIONS. THE HELICOPTER STRUCK THE FROZEN LAKE, AND ROLLED ONTO ITS RIGHT SIDE. THE HELICOPTER SUSTAINED SUBSTANTIAL DAMAGE TO THE FUSELAGE, TAIL BOOM, AND DRIVE TRAIN COMPONENTS. THE CLOSEST OFFICIAL WEATHER OBSERVATION STATION IS BARROW, LOCATED ABOUT 4 NAUTICAL MILES NORTH OF THE ACCIDENT SITE. ON FEBRUARY 24, AT 1753, AN AVIATION ROUTINE WEATHER REPORT (METAR) WAS REPORTING IN PART: WIND, 070 DEGREES AT 13 KNOTS; VISIBILITY, 3 MILES WITH LIGHT SNOW; CLOUDS, 2,400 FEET SCATTERED, 3,800 FEET BROKEN, 10,000 FEET OVERCAST; TEMPERATURE, MINUS 7 DEGREES F; DEW POINT, MINUS 13 DEGREES F; ALTIMETER, 29.81 INHG. THE PILOT REPORTED THAT THERE WERE NO PREACCIDENT MECHANICAL ANOMALIES WITH THE HELICOPTER.

NTSB investigation

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