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

September 11, 2003 · Schweizer 269C-1 · N6147Q

Homestead, FL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 11, 2003
Injury Outcomes
2 injuries (2 minor injuries)
Location
Homestead, FL
Aircraft
Schweizer 269C-1
Tail Number
N6147Q
Operator
Helicenter International Academy
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
MIA03LA181

The certified flight instructor (CFI) stated that after departure the flight proceeded to the Homestead General Airport where he advised the student that the lesson would continue with "running landing" and "running take off" training from the previous day. The flight continued in the traffic pattern for runway 36, and when on short final approach to the runway at 5 feet above ground level, the helicopter was at 25 knots indicated airspeed. The helicopter contacted the runway with the skids parallel to the runway centerline, and the CFI allowed the helicopter to continue sliding. The CFI advised the student that the lesson would conclude with a "running takeoff", and upon lifting off the runway at an indicated airspeed of 35 knots, he noticed a vibration from the main rotor system. He noticed the rpm was decreasing and touched down again on the runway, at which time the helicopter began to "shake violently." He realized the flight had encountered ground resonance, and noticed that there was insufficient main rotor rpm to lift off the ground to stabilize the vibrating rotor blade system. He lowered the collective but felt a force when he attempted to reduce throttle input; he felt the force was the student pilot applying throttle input. At that point he was contacted in the head, lost consciousness, which he regained in the hospital. The student pilot advised a Federal Aviation Administration (FAA) inspector that when the flight was approximately 30 feet above ground level prior to performing a running landing, the CFI took the controls from him. The flight continued and while sliding on the runway, the CFI started screaming and froze on the controls. He (student pilot) then braced for impact. Following recovery of the helicopter, the landing gear and main rotor dampers were removed for further examination at the manufacturer's facility with FAA oversight. Examination of the main rotor blade dampers revealed all three exhibited damage associated from lead lag motions encountered in ground resonance. Examination of the four landing gear dampers which had been installed when the helicopter was manufactured revealed all tested out of limits for charge pressure (low). The helicopter was last inspected in accordance with a 100-Hour inspection on August 11, 2003; the helicopter had accumulated 87.9 hours since the inspection at the time of the accident. Review of the 100-Hour inspection guide revealed the landing gear dampers are required to be inspected for operation and condition, and for damper extension with a full fuel tank. Review of Section 12 of the Basic Handbook of Maintenance Instructions manual indicates the landing gear dampers will experience a decrease in pressure with subsequent use of the helicopter, and they should be extension checked during a 100-Hour inspection, or every six months, whichever occurs first. According to a memorandum from the Director of Flight Training to all flight instructors dated August 25, 2003, with respect to the Dominican Republic Flight Training Program, running landings were prohibited to be demonstrated and practiced until a new order was given.

NTSB Probable Cause

the inadequate 100-hour inspection of the helicopter by other maintenance personnel who failed to discover that the landing gear dampers had low pressure, which resulted in ground resonance and subsequent substantial damage during a run-on landing.

Full Narrative

On September 11, 2003, about 1445 eastern daylight time, a Schweizer 269C-1, N6147Q, registered to Caribbean Helicopter Leasing, Inc., operated by Helicenter International Academy, was substantially damaged during a run-on landing at the Homestead General Aviation Airport, Homestead, Florida. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 91 instructional flight from the Kendall-Tamiami Executive Airport, Miami, Florida, to the Homestead General Aviation Airport, Homestead, Florida. The certified flight instructor (CFI) and student sustained minor injuries. The flight originated at 1430, from the Kendall-Tamiami Executive Airport. The CFI stated that after departure the flight proceeded to the Homestead General Airport where he advised the student that the lesson would continue with "running landing" and "running take off" training from the previous day. The flight continued in the traffic pattern for runway 36, and when on short final approach to the runway at 5 feet above ground level, the helicopter was at 25 knots indicated airspeed. The helicopter contacted the runway with the skids parallel to the runway centerline, and the CFI allowed the helicopter to continue sliding. The CFI advised the student that the lesson would conclude with a "running takeoff", and upon lifting off the runway at an indicated airspeed of 35 knots, he noticed a vibration from the main rotor system. He noticed the rpm was decreasing and touched down again on the runway, at which time the helicopter began to "shake violently." He realized the flight had encountered ground resonance, and noticed that there was insufficient main rotor rpm to lift off the ground to stabilize the vibrating rotor blade system. He lowered the collective but felt a force when he attempted to reduce throttle input; he felt the force was the student pilot applying throttle input. At that point he was contacted in the head, lost consciousness, which he regained in the hospital. The student pilot advised a Federal Aviation Administration (FAA) inspector that when the flight was approximately 30 feet above ground level prior to performing a running landing, the CFI took the controls from him. The flight continued and while sliding on the runway, the CFI started screaming and froze on the controls. He (student pilot) then braced for impact. Following recovery of the helicopter, the landing gear and main rotor dampers were removed for further examination at the manufacturer's facility with FAA oversight. Examination of the main rotor blade dampers revealed all three exhibited damage associated from lead lag motions encountered in ground resonance. Examination of the four landing gear dampers which had been installed when the helicopter was manufactured revealed all tested out of limits for charge pressure (low). The helicopter was last inspected in accordance with a 100-Hour inspection on August 11, 2003; the helicopter had accumulated 87.9 hours since the inspection at the time of the accident. Review of the 100-Hour inspection guide revealed the landing gear dampers are required to be inspected for operation and condition, and for damper extension with a full fuel tank. Review of Section 12 of the Basic Handbook of Maintenance Instructions manual indicates the landing gear dampers will experience a decrease in pressure with subsequent use of the helicopter, and they should be extension checked during a 100-Hour inspection, or every 6 months, whichever occurs first. According to a memorandum from the Director of Flight Training to all flight instructors dated August 25, 2003, with respect to the Dominican Republic Flight Training Program, running landings were prohibited to be demonstrated and practiced until a new order was given. The helicopter minus the retained main rotor and landing gear dampers was released to the president and CEO of the owner of the helicopter on November 18, 2003. The retained main rotor and landing gear dampers were released to the president and CEO of the owner of the helicopter on March 23, 2004.

Flight

Event TypeAccident
Event Time14:45 EDT
Nearest AirportHomestead General Aviation (0nm)
Runway36
Runway Length4000 ft
Runway Width100 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftSchweizer 269C-1
Tail NumberN6147Q
Aircraft CategoryHeli
DamageSubstantial
OperatorHelicenter International Academy
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HO-360-C1A · Reciprocating · 180
Seats2

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 32 · Second Class · Minor
Crew 2Age 20 · Third Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind5 kt
Visibility10 sm
CeilingNone
Altimeter29.93 inHg
Observation Time18:53
Weather SourceWFAC

Appendix: Source Data