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Aviation safety reports, made easier to study

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April 16, 2000 · Bell 407 · N175PA

Grand Canyon, AZ

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 16, 2000
Injury Outcomes
No injuries (6 uninjured)
Location
Grand Canyon, AZ
Aircraft
Bell 407
Tail Number
N175PA
Operator
Papillon Airways
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX00LA156

About 5 minutes after takeoff, while in cruise flight, the pilot felt a few short 'clunks' and then heard grinding noise and felt violent shaking. The pilot elected to perform a precautionary, autorotative, off-airport landing. During the landing flare, the tail rotor and tail stinger contacted the ground. The tail rotor blades were damaged, the stinger broken, and the tail rotor gearbox was fractured. The vibration that the pilot felt was traced to a failed bearing at the oil cooler fan forward hanger. The bearing was sent to the helicopter manufacturer for examination; however, a fracture mode could not be identified due to damage to the fracture surfaces. An airworthiness directive applied to the bearing and was complied with 11 flight hours prior to the accident.

NTSB Probable Cause

The failure and subsequent disintegration of the oil cooler fan forward hanger bearing.

Full Narrative

On April 16, 2000, at 1208 hours mountain standard time, a Bell 407, N175PA, was substantially damaged during a precautionary, autorotative, off-airport landing near Grand Canyon, Arizona. The commercial certificated pilot and five passengers were not injured. The local area sightseeing flight was operated under 14 CFR Part 135 by Papillon Airways, Inc. A company VFR flight plan was filed. Visual meteorological conditions prevailed for the flight that departed from the Grand Canyon National Park airport at 1205. The pilot reported he felt a few short "clunks" while in cruise flight about 5 minutes after takeoff. Next there was "a very loud grinding noise and the aircraft began to SHAKE VIOLENTLY." The pilot decided to autorotate to a nearby clearing. During the landing flare, the tail rotor and tail stinger contacted the ground. The tail rotor blades were damaged, the stinger broken, and the tail rotor gearbox was fractured. The vibration that the pilot felt was traced to a failed bearing at the oil cooler fan forward hanger. The bearing was sent to Bell Helicopter/Textron for examination; however, the laboratory report states that a fracture mode could not be identified due to damage to the fracture surfaces. Airworthiness Directive 2000-02-12 applied to the bearing and was complied with 11 flight hours prior to the accident.

Flight

Event TypeAccident
Event Time12:08 MST
Nearest Airport0nm
Runway0
Flight Plan FiledCvfr
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 407
Tail NumberN175PA
Aircraft CategoryHeli
DamageSubstantial
OperatorPapillon Airways
Operating RulePart 135
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C47B · Turboshaft · 647
Seats7

People & Injuries

Injury SummaryNo injuries (6 uninjured)
Fatal0
Serious0
Minor0
Uninjured6
Total6
Crew 1Age 39 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind230° @ 15 kt, gusting 20 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point61 F / 18 C
Altimeter30.00 inHg
Observation Time18:54
Weather SourceWFAC

Appendix: Source Data