Premium research interface

The modern interface for aviation safety intelligence.

Search investigations, review source evidence, monitor watched reports, and trace long-term patterns from one calm, data-first workspace.

63k+
Reports indexed
1940-2026
Coverage
Recent
Last data refresh
Featured Report

Loading…

Loading featured report…

Loading…
Open Report

Safety trends by operating rule

Track fatal and non-fatal accident patterns across Part 91, Part 135, and Part 121 operations.

Loading trend charts…

Browse the aviation graph

Move quickly by aircraft, airport, operator, and time with indexes built for research, not wandering.

Last Data Update

By Decade

By Month

Aircraft Manufacturer

More manufacturers

Airports

More airports

Operators

More operators

About

Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

The goal is practical safety education: make it faster to find relevant investigations, compare similar events, review factual records, and understand the evidence behind probable-cause and preliminary reports.

The investigative work and source records belong to the National Transportation Safety Board and the published investigation record. This site is not affiliated with or endorsed by the NTSB.

FAQs

NTSB Report

March 27, 1997 · Enstrom F-28C · N294SB

Sacaton, AZ

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 27, 1997
Injury Outcomes
No injuries (2 uninjured)
Location
Sacaton, AZ
Aircraft
Enstrom F-28C
Tail Number
N294SB
Operator
Steve Bates
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX97LA133

During a confined area takeoff, the aircraft passed through effective translational lift (ETL) when the pilot noticed a reduction in engine noise. Both the engine and rotor rpm needles were still joined at a position just below the bottom of the green arc. He lowered collective and rolled the throttle full on without obtaining an increase in engine rpm. He initiated a straight-in autorotation, and during the ground slide, a skid contacted a rock and the tail boom yawed. The tail boom then struck a tree and separated from the aircraft. The main rotor drive belt was disconnected and a run-up check was performed the engine. The engine ran throughout the normal operating range and magneto checks were within tolerances. The engine air cleaner was removed and exhibited trapped dirt and grass.

NTSB Probable Cause

the pilot's improper use of the collective by not maintaining rotor rpm during takeoff from a confined area.

Full Narrative

On March 27, 1997, at 1515 hours mountain standard time, an Enstrom F-28C, N294SB, collided with the terrain after experiencing a loss of power on takeoff near Sacaton, Arizona. The aircraft sustained substantial damage; however, neither the instructor nor his student was injured. The aircraft was being operated as an instructional flight by Sunbird Aviation when the accident occurred. The flight originated at 1420 in Chandler, Arizona. Visual meteorological conditions prevailed at the time and no flight plan was filed. The instructor stated that he was demonstrating a confined area takeoff to his student. As the aircraft passed through effective translational lift (ETL) and reached about 20 to 25 feet agl, he noticed a reduction in engine noise. When he checked his gauges he noticed that both the engine and rotor rpm needles were still joined at a position just below the bottom of the green arc. He lowered his collective and rolled the throttle full on, with no corresponding increase in engine rpm. At this point, he initiated a straight-in autorotation, cushioning the touchdown with remaining collective and sliding about 5 to 6 feet. During the ground slide, the left skid contacted a rock and the tail boom yawed to the right. The tail boom then struck a Palo Verde tree and separated from the aircraft. A Safety Board investigator estimated that density altitude was approximately 3,000 feet at the time of the accident. After the aircraft was recovered, the main rotor drive belt was disconnected and the engine was started and run. A run-up check was also performed on the right and left magnetos with less than a 100 rpm drop on each. The engine ran smoothly throughout the normal operating range. The engine air cleaner was removed and examined. The element exhibited trapped dirt and grass.

Flight

Event TypeAccident
Event Time15:15 MST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftEnstrom F-28C
Tail NumberN294SB
Aircraft CategoryHeli
DamageSubstantial
OperatorSteve Bates
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360-E1AD · Reciprocating · 205
Seats3

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 50 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind3 kt
Visibility30 sm
CeilingNone
Temperature / Dew Point0 C
Altimeter29.00 inHg
Observation Time21:49
Weather SourceWFAC

Appendix: Source Data