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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

June 10, 1999 · Bell 47G3B2A · N24MP

Pendleton, OR

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 10, 1999
Injury Outcomes
No injuries (1 uninjured)
Location
Pendleton, OR
Aircraft
Bell 47G3B2A
Tail Number
N24MP
Injuries
None
Aircraft Damage
Substantial
NTSB Number
SEA99LA098

The helicopter was applying dry fertilizer from an external bucket. While taking off after refilling the bucket, the external load cable became entangled in the auger of the fertilizer truck. The pilot reported he then attempted to release the load, but the quick-disconnect hydraulic lines would not release. In the process of attempting to get the helicopter to the ground, the helicopter suffered a blade strike and impacted the ground. The pilot reported the hydraulic lines were routed over the skid or cross tube, as opposed to down the release hook and cable. The hydraulic lines were approved for a spray system installation installed per FAA Supplemental Type Certificate (STC) on the helicopter in 1993; however, the operator furnished no substantiation of FAA approval of the external bucket installation, and no record of FAA approval of the bucket installation on the helicopter was on file with the FAA.

NTSB Probable Cause

A fouled external load cable, and the pilot's operation of the helicopter with a non-approved external bucket installation, resulting in misrouted hydraulic lines and consequent malfunction of the external load release system.

Full Narrative

On June 10, 1999, approximately 1400 Pacific daylight time, a Bell 47G3B2A helicopter, N24MP, registered to Columbia Basin Helicopters Inc. of Pendleton, Oregon, collided with terrain while performing a 14 CFR 133/14 CFR 137 external-load agricultural aerial application flight in or near Pendleton, and was substantially damaged. The commercial pilot-in-command, who was the aircraft's sole occupant, was not injured. Visual meteorlogical conditions existed and no flight plan had been filed for the flight, which departed from the job site in or near Pendleton. At the time of the accident, the helicopter was performing agricultural operations utilizing an external bucket to drop dry fertilizer. The pilot reported that while taking off after refilling the fertilizer bucket, the external load cable to the bucket became entangled with the auger of the fertilizer truck. The pilot reported that he attempted to release the load, but that the quick-disconnect hydraulic lines did not release. The pilot reported that while attempting to get the helicopter to the ground, he had a blade strike. The helicopter subsequently impacted the ground. The pilot expressed a belief to an FAA inspector assigned to investigate the accident that "because the hydraulic lines were routed over the skid or cross tube the helicopter was thrown out of lateral C.G. when the hydraulic lines failed to disconnect properly." According to the FAA inspector, the pilot further stated to him that "during conversations with other industry folks regarding his accident, he learned that routing lines over the skid or cross tube is a known problem and that the fix is to route the lines down the release hook and cable...." Subsequent investigation revealed that the hydraulic pump and lines involved were approved as part of FAA Supplemental Type Certificate (STC) SH891NW for installation of a Simplex model 5600 spray system, which according to FAA aircraft records was installed on the accident helicopter on January 15, 1993. However, the accident helicopter was not configured with the Simplex spray system at the time of the accident. Despite repeated requests, the operator did not furnish any substantiation of FAA approval of the external bucket installation to FAA investigators. The FAA aircraft registry records on the accident helicopter also contained no record of FAA approval of the external bucket installation. The pilot, who held a commercial pilot certificate with rotorcraft-helicopter rating and private privileges for single-engine land airplanes, reported he had 650 hours of single-engine airplane time, but did not provide any information to the NTSB regarding his total pilot time or helicopter time. The pilot reported that his most recent biennial flight review was conducted on March 3, 1998, in a Cessna TU206.

Flight

Event TypeAccident
Event Time14:00 PDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 47G3B2A
Tail NumberN24MP
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 137
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · V0-435 · Reciprocating · 285
Seats3

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 33 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind240° @ 4 kt, gusting 12 kt
Visibility50 sm
CeilingNone
Temperature / Dew Point70 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data