N958CP

Substantial
None

Schweizer 269CS/N: 51710

Accident Details

Date
Thursday, May 19, 2005
NTSB Number
DEN05CA079
Location
Pueblo, CO
Event ID
20050614X00763
Coordinates
38.289165, -104.496391
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

the student pilot's failure to maintain control of the helicopter during the landing. Contributing to the accident was the flight instructor's inadequate supervision of the student pilot.

Aircraft Information

Registration
Make
SCHWEIZER
Serial Number
51710
Engine Type
Reciprocating
Year Built
1996
Model / ICAO
269CH269
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
269C

Registered Owner (Current)

Name
JOSLYN LARRY J
Address
9632 CAMDEN HILLS AVE
City
LAS VEGAS
State / Zip Code
NV 89145-8621
Country
United States

Analysis

On May 19, 2005, approximately 0920 mountain daylight time, a Schweizer 269C helicopter, N958CP, was substantially damaged when it made a hard landing during a short approach at the Pueblo Memorial Airport (PUB), Pueblo, Colorado. Visual meteorological conditions prevailed at the time of the accident. The instructional flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The flight instructor and student pilot on board reported no injures.The local flight departed PUB approximately 0830.

According to the accident report submitted by the flight instructor, they were conducting steep approaches to runway 26L. The first three approaches and landings were uneventful. During the fourth approach, approximately 10 to 15 feet agl, the student noted that the rpm's had dropped into the yellow arc around 2800 rpm. The student stated that he "lowered the collective and rolled on the throttle." The helicopter "dropped dramatically." The student attempted to cushion the landing by adding collective. The helicopter impacted the ground and "spun left" approximately 180 degrees before coming to a rest. During the impact the skids split, the tail boom was bent backwards, the tail rotor drive shaft separated, and the frame of the helicopter was bent. An examination of the helicopter's systems revealed no anomalies.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN05CA079