19990929047519A

Accident · Substantial damage

FAA accident report · Enstrm 280C · Longmont, CO · September 29, 1999

Date
September 29, 1999 · 18:40 local
Place
Longmont, CO
Airport
Vance Brand Airport
Phase of flight
Pwr Off Vert Land/Autorotate
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N84DH
NTSB investigation
NTSBDEN99LA173
Reported as
Enstrm 280C
Reported engine
Lycoming HIO360E1AD
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,127 total40 in this make and model91 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.

(.4) While practicing autorotations, the pilot, who was a commercial pilot in single and multiengine aircraft but a student pilot in helicopters, experienced a loss of engine power for unknown reasons. During the full autorotation, which was necessitated by the power loss, the landing was hard and resulted in main rotor flex, which cut off the tail boom. Density altitude at the time was 9,000 feet. (-23) student pilot practicing autorotation. He rolled off throttle to disengage main rotor. Engine quit. Autorotation completed. Main rotor blade contacted top and aft section of tail boom. After landing the engine was run on the ground by student and instructor. There were no engine abnormalities in engine run.

As the FAA filed it

(.4) WHILE PRACTICING AUTOROTATIONS, THE PILOT, WHO WAS A COMMERCIAL PILOT IN SINGLE AND MULTIENGINE AIRCRAFT BUT A STUDENT PILOT IN HELICOPTERS, EXPERIENCED A LOSS OF ENGINE POWER FOR UNKNOWN REASONS. DURING THE FULL AUTOROTATION, WHICH WAS NECESSITATED BY THE POWER LOSS, THE LANDING WAS HARD AND RESULTED IN MAIN ROTOR FLEX, WHICH CUT OFF THE TAIL BOOM. DENSITY ALTITUDE AT THE TIME WAS 9,000 FEET. (-23) STUDENT PILOT PRACTICING AUTOROTATION. HE ROLLED OFF THROTTLE TO DISENGAGE MAIN ROTOR. ENGINE QUIT. AUTOROTATION COMPLETED. MAIN ROTOR BLADE CONTACTED TOP AND AFT SECTION OF TAIL BOOM. AFTER LANDING THE ENGINE WAS RUN ON THE GROUND BY STUDENT AND INSTRUCTOR. THERE WERE NO ENGINE ABNORMALITIES IN ENGINE RUN.

NTSB investigation

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