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August 17, 1982 · Enstrom F-28F · N5698E

Near Sutton, AK

Overview

Report Status
Preliminary report
Event Type
Accident
Date
August 17, 1982
Injury Outcomes
3 injuries (3 minor injuries)
Location
Near Sutton, AK
Aircraft
Enstrom F-28F
Tail Number
N5698E
Operator
Kean & Associates
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
ANC82DA075

The pilot had approached and landed on a bluff to discharge his two passengers. However, before discharging the passengers, he decided to takeoff and find a better landing area. When the helicopter was about 10 to 20 ft from the takeoff point, but approximately 200 ft AGL, there was a decrease in RPM. Initially, the pilot thought he was settling with power. He lowered the nose and collective, but was unable to regain the RPM, but he felt the helicopter yaw to the left. He felt mast-bumping and realized he must be cross-controlling with too much right pedal and left cyclic. He then entered an autorotation. The helicopter collided with trees on the side of the bluff and rolled to the bottom of the hill. An examination revealed that the No-2 cylinder compression was low. The No-2 intake valve had become tuliped and was leaking. There was evidence that it had been pounding. Also, there were indications of high engine RPM and temperature. The helicopter had been flown 38 hrs since the last inspection.

Full Narrative

THE PILOT HAD APPROACHED AND LANDED ON A BLUFF TO DISCHARGE HIS TWO PASSENGERS. HOWEVER, BEFORE DISCHARGING THE PASSENGERS, HE DECIDED TO TAKEOFF AND FIND A BETTER LANDING AREA. WHEN THE HELICOPTER WAS ABOUT 10 TO 20 FT FROM THE TAKEOFF POINT, BUT APPROXIMATELY 200 FT AGL, THERE WAS A DECREASE IN RPM. INITIALLY, THE PILOT THOUGHT HE WAS SETTLING WITH POWER. HE LOWERED THE NOSE AND COLLECTIVE, BUT WAS UNABLE TO REGAIN THE RPM, BUT HE FELT THE HELICOPTER YAW TO THE LEFT. HE FELT MAST-BUMPING AND REALIZED HE MUST BE CROSS-CONTROLLING WITH TOO MUCH RIGHT PEDAL AND LEFT CYCLIC. HE THEN ENTERED AN AUTOROTATION. THE HELICOPTER COLLIDED WITH TREES ON THE SIDE OF THE BLUFF AND ROLLED TO THE BOTTOM OF THE HILL. AN EXAMINATION REVEALED THAT THE NO-2 CYLINDER COMPRESSION WAS LOW. THE NO-2 INTAKE VALVE HAD BECOME TULIPED AND WAS LEAKING. THERE WAS EVIDENCE THAT IT HAD BEEN POUNDING. ALSO, THERE WAS INDICATIONS OF HIGH ENGINE RPM AND TEMPERATURE. THE HELICOPTER HAD BEEN FLOWN 38 HRS SINCE THE LAST INSPECTION.

Flight

Event TypeAccident
Event Time09:05 AHDT
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftEnstrom F-28F
Tail NumberN5698E
Aircraft CategoryHeli
DamageSubstantial
OperatorKean & Associates
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360-F1AD · Reciprocating · 225
Seats3

People & Injuries

Injury Summary3 injuries (3 minor injuries)
Fatal0
Serious0
Minor3
Uninjured0
Total3
Crew 1Age 25 · Second Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility20 sm
CeilingNone
Temperature / Dew Point14 C / 0 C
Altimeter0

Appendix: Source Data