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

December 16, 2004 · Bell UH-1H · N51AG

Rockford, AL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 16, 2004
Injury Outcomes
No injuries (1 uninjured)
Location
Rockford, AL
Aircraft
Bell UH-1H
Tail Number
N51AG
Operator
Agrotors
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ATL05LA035

According to the pilot, during a turn while applying fertilizer over pine trees he heard a "loud bang"; at the same time he lost tail rotor authority. The pilot attempted to level the helicopter and settled into the trees. Post accident examination revealed the helicopter was upright and on its skids. Flight control continuity was established with the cyclic and the collective controls. Examination of the tail rotor blades revealed leading edge damage on both blades. Examination of the helicopter revealed the lower fuselage was buckled and the tail rotor rear housing of the tail rotor gearbox transmission was broken and cracked. The tail rotor assembly was examined and revealed that the fracture features on the case assembly indicated an overload event. The wear patterns on the teeth of the bevel gears within the gearbox indicated that they were forced apart. There were no indications of any pre-existing conditions on the components examined that would suggest a failure before the tail rotor strike.

NTSB Probable Cause

The pilot's failure to maintain adequate obstacle clearance, which resulted in an in-flight collision with a tree.

Full Narrative

On December 16, 2004, at 1620 central standard time, a Bell UH-1, N51AG, registered to and operated by AG Rotors, collided with trees during a spraying operation five miles west of Rockford, Alabama. The agricultural flight was operated under the provisions of Title 14 Part 137 with no flight plan filed. Visual meteorological conditions prevailed at the time of the accident. The pilot was not injured and the helicopter sustained substantial damage. The flight departed from a field site located in the vicinity of Rockford, Alabama, on December 16, 2004, at 1600. According to the pilot, during a turn while applying fertilizer over pine trees he heard a "loud bang"; at the same time he lost tail rotor authority. The pilot attempted to level the helicopter and settled into the trees. Post accident examination reveal the helicopter was upright and on its skids. Flight control continuity was established with the cyclic and the collective controls. Examination of the tail rotor blades revealed leading edge damage on both blades. Examination of the helicopter revealed the lower fuselage was buckled and the tail rotor rear housing of the tail rotor gearbox transmission was broken and cracked. The tail rotor assembly was examined and revealed that the fracture features on the case assembly revealed an overload event. The wear patterns on the teeth of the bevel gears within the gearbox showed that they were forced apart. There was no evident of any pre-exiting condition on the components examined that would suggest a failure before the tail rotor strike.

Flight

Event TypeAccident
Event Time16:20 CST
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell UH-1H
Tail NumberN51AG
Aircraft CategoryHeli
DamageSubstantial
OperatorAgrotors
Operating RulePart 137

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1None

Conditions

ConditionsVMC
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point46 / 45 C
Altimeter30.47 inHg
Observation Time16:20
Weather SourceWFAC

Appendix: Source Data