20000808025709I

Incident · Minor damage

FAA incident report · Enstrm F-28F · Twin Falls, ID · August 8, 2000

Date
August 8, 2000 · 16:40 local
Place
Twin Falls, ID
Airport
Twin Falls-Sun Valley Reg Josl
Phase of flight
Autorot Descent (Rotorcraft)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N8623B
Reported as
Enstrm F28F
People aboard
2
Fatal injuries
0
Pilot’s flight hours
961 total117 in this make and model139 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.

(-23)Instructor stated that prior to training flight fuel gauge was checked and 12 gallons of fuel added to give 2 hours of flight time. The instruction flight was planned to be 1.5 hours. After completing 4 practice auto rotations, the instructor and student confirmed using the fuel gauge they had time and fuel for one more practice auto rotations. During the climb the engine quit, a downwind auto rotation was attempted in minor damage to the helicopter and no injuries to the occupants. Post incident investigation found the fuel sender unit to give an inaccurate reading to the ships fuel gauge. The system was indicating more fuel than was actually in the ship. This false reading lead to fuel depletion and engine stoppage at 1.2 hours of flight time.

As the FAA filed it

(-23)INSTRUCTOR STATED THAT PRIOR TO TRAINING FLIGHT FUEL GAUGE WAS CHECKED AND 12 GALLONS OF FUEL ADDED TO GIVE 2 HOURS OF FLIGHT TIME. THE INSTRUCTION FLIGHT WAS PLANNED TO BE 1.5 HOURS. AFTER COMPLETING 4 PRACTICE AUTO ROTATIONS, THE INSTRUCTOR AND STUDENT CONFIRMED USING THE FUEL GAUGE THEY HAD TIME AND FUEL FOR ONE MORE PRACTICE AUTO ROTATIONS. DURING THE CLIMB THE ENGINE QUIT, A DOWNWIND AUTO ROTATION WAS ATTEMPTED IN MINOR DAMAGE TO THE HELICOPTER AND NO INJURIES TO THE OCCUPANTS. POST INCIDENT INVESTIGATION FOUND THE FUEL SENDER UNIT TO GIVE AN INACCURATE READING TO THE SHIPS FUEL GAUGE. THE SYSTEM WAS INDICATING MORE FUEL THAN WAS ACTUALLY IN THE SHIP. THIS FALSE READING LEAD TO FUEL DEPLETION AND ENGINE STOPPAGE AT 1.2 HOURS OF FLIGHT TIME.

Other reports on N8623B · 1

Matched to the same aircraft by N-number and date.