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

February 25, 2002 · Rotorway Rotorway Exec 90 · N9876D

Phoenix, AZ

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
February 25, 2002
Injury Outcomes
No injuries (2 uninjured)
Location
Phoenix, AZ
Aircraft
Rotorway Rotorway Exec 90
Tail Number
N9876D
Operator
Rotorway International
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX02LA096

The experimental helicopter made a hard landing following a practice autorotation and loss of engine power. During the third practice autorotation, the student informed the instructor that he was unable to reintroduce power during the autorotation recovery. The instructor took control of the helicopter and attempted to roll the throttle up; however, he found it would not rotate any further. The instructor raised the collective at 10 feet agl in an attempt to cushion the landing. The helicopter hit the ground hard, the left skid collapsed, and the helicopter rolled onto its left side. Examination of the helicopter revealed the mechanical stop for the throttle was bent causing a condition in which the engine would stay at ground idle once the throttle was rolled past over center near the ground idle position. Once the linkage was driven over center, the linkage could not be moved by the throttle control. A post accident run of the engine revealed no additional anomalies.

NTSB Probable Cause

The student's inadvertent over control of the throttle mechanism, which resulted in the bending of the throttle mechanical stop and binding the linkage in the idle position. Also causal was the CFI's inadequate supervision. A factor in the accident was the CFI's inability to add engine power due to the bent throttle mechanism during a practice autorotation.

Full Narrative

On February 25, 2002, at 1430 mountain standard time, a Rotorway Exec 90 experimental helicopter, N9876D, made a hard landing following a loss of power during cruise about 5 miles south of Phoenix, Arizona, on the Gila River Indian Reservation. The helicopter was operated by Cobb International, Inc., under the provisions of 14 CFR Part 91 as an instructional flight, and sustained substantial damage. The certified flight instructor (CFI) and student pilot were not injured. Visual meteorological conditions prevailed for the local area flight that departed the Chandler Stellar Airpark (P19), Chandler, Arizona, at 1410. The flight was scheduled to terminate at P19. A flight plan had not been filed. In the CFI's written statement, he stated that he and his student were on a training flight to practice autorotations. During the third practice autorotation from 500 feet agl, the student performed the maneuver "without problems until the aircraft was straight and level after flaring" about 30 feet agl. Attempts were made to reintroduce power without success. The CFI stated he was on the controls "lightly" with the student, when the student told the CFI he could not reintroduce power. The CFI then came fully onto the controls and attempted to roll on the throttle only to discover it would not roll any further. The collective was raised to cushion the landing at 10 feet agl; however, the aircraft made hard contact with the ground, collapsing the left skid, and rolling onto its left side. The Federal Aviation Administration Inspector, who responded to the accident site, informed the National Transportation Safety Board that the mechanical stop for the throttle was bent. He stated once the linkage is driven "over center," it can't be brought back, and it remains at ground idle. The engine was started after the accident and ran "with no problems."

Flight

Event TypeAccident
Event Time14:30 MST
Nearest Airport5nm S
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftRotorway Rotorway Exec 90
Tail NumberN9876D
Aircraft CategoryHeli
DamageSubstantial
OperatorRotorway International
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsRotorway · RI-162 · Reciprocating · 150
Seats2

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 42 · Second Class · None
Crew 2Age 57 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind230° @ 8 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point30 C
Altimeter30.10 inHg
Observation Time21:56
Weather SourceWFAC

Appendix: Source Data