CEN12CA431

NTSB accident investigation · Schweizer 269C · Denton, TX · July 6, 2012

Accident · No injuriesData collectionFinal report
Date
July 6, 2012, 16:22 local (21:22 UTC)
Place
Denton, TX
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N565LHSchweizer 269C
Defining event
Maneuvering: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed · report September 13, 2012
Report
Approved by Office Director
NTSB office
Central Region
Parties
Federal Aviation Administration
FAA report
20120706011979A
Case key
84276

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The flight instructor and student pilot exceeded the helicopter's takeoff performance, which resulted in low rotor rpm and settling.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Aircraft capability: climb capabilityAircraft › Aircraft oper/perf/capability · Capability exceededSchweizer 269C: 2 casesAll aircraft: 183 casesProbable cause
Temp/humidity/pressure: high density altitudeEnvironmental issues › Conditions/weather/phenomena · Effect on operationSchweizer 269C: 3 casesAll aircraft: 278 cases

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The flight instructor and student pilot were practicing takeoffs and landings to confined areas. The student pilot performed a maximum performance takeoff from a confined area to an altitude of about 10 feet above the trees. During the transition to forward flight, the low rotor rpm horn sounded and the helicopter began to settle toward the trees. The instructor applied full throttle and forward cyclic. The helicopter continued to settle and the rotor rpm continued to decay. The instructor leveled the helicopter, applied full collective, and the main rotor blades contacted trees. The helicopter settled into the trees and came to rest nose down. The instructor recommended that the student limit maximum performance takeoffs to large confined areas when operating above 3,000 feet density altitude. The instructor reported no mechanical malfunctions prior to the accident and a calculated density altitude of 3,500 feet.

Factual narrative

The instructor and student were practicing takeoffs and landings to confined areas. The student pilot performed a maximum performance takeoff from a confined area to an altitude of approximately 10 feet above the trees. During the transition to forward flight, the low rotor RPM horn sounded and the helicopter began to settle towards the trees. The instructor applied full throttle and forward cyclic. The helicopter continued to settle and the rotor RPM continued to decay. The instructor leveled the helicopter, applied full collective, and the main rotor blades contacted trees. The helicopter settled into the trees and came to rest nose down. The instructor recommended that he limit maximum performance takeoffs to large confined areas when operating above 3,000 feet density altitude. The instructor reported no mechanical malfunctions prior to the accident, and a calculated density altitude of 3,500 feet.

Aircraft

Registration
N565LH
Reported as
Schweizer 269C
Category
Helicopter
Serial number
S1904
Airframe hours
3,037
Engine
Lycoming HIO-360-D1A, 190 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Longhorn Helicopters Inc
Registered owner
Longhorn Helicopters Inc
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 14, 2012
Departed
DTO · Denton, TX
Destination
DTO · Denton, TX

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
28
Injuries
None
Certificates
Commercial, Flight instructor
Instrument ratings
Helicopter
Medical
Class 1, Without waivers/limitations
Last flight review
June 8, 2012
Seat
Right
Flight hours
1,910 total · 57 in this make and model
Role
Student pilot
Age
30
Injuries
None
Certificates
Student, Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Unknown
Seat
Left
Flight hours
434 total · 39 in this make and model

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
None
Temperature
99 °F, dew point 63 °F
Altimeter
29.97 inHg
Observed at
DTO, 4 nm away

Docket · 1

The files NTSB released with the investigation on July 17, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.9 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.