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 19, 2008 · Hawker Beechcraft 99 · N118SF

Moline, IL

Overview

Report Status
Final with probable cause
Event Type
Incident
Date
February 19, 2008
Injury Outcomes
No injuries (1 uninjured)
Location
Moline, IL
Aircraft
Hawker Beechcraft 99
Tail Number
N118SF
Injuries
None
Aircraft Damage
Minor
NTSB Number
CHI08IA085

The pilot said that during descent he "smelled electrical smoke and saw flames behind the power quadrant." He declared an emergency and removed the fire extinguisher from its holder. In the time it took to do this, the flames were no longer visible and the burning smell was not getting any stronger. The pilot landed at his destination without further incident. An examination revealed that a 10 ohm, 1/2 watt, resistor contacted the ground lug of a silicon controlled rectifier in the flap control circuit. The manufacturer indicated that manufacturing practices require component leads to be covered with a sleeve. The 100 hour inspection listed in the airplane's maintenance manual indicated that the instrument plumbing and wiring should be inspected for "condition, attachment, chafing, etc."

NTSB Probable Cause

The arcing of the resistor and silicone controlled rectifier in the flap control circuit.

Full Narrative

On February 18, 2008, about 2030 central standard time, a Hawker Beechcraft Corp. 99, N118SF, operated by Suburban Air Freight Inc., as a cargo airplane, received minor damage during cruise when an in-flight fire occurred about 30 miles west of the Quad City International Airport (MLI), near Moline, Illinois. Visual meteorological conditions prevailed at the time of the accident. The unscheduled domestic 14 CFR Part 135 cargo flight had a filed and activated an instrument flight rules flight plan. The pilot was uninjured. The flight originated about 1930 from the Eppley Airfield, near Omaha, Nebraska, and was destined for MLI. The pilot said that during the descent to MLI he "smelled electrical smoke and saw flames behind the power quadrant." He declared an emergency and removed the fire extinguisher from its holder. In the time it took to do this, the flames were no longer visible and the burning smell was not getting any stronger. The pilot elected to continue to MLI. A Federal Aviation Administration Inspector examined the airplane. The inspector found that a 10 ohm, 1/2 watt, resistor contacted the ground lug of a silicon controlled rectifier. The components were mounted to a terminal strip located on the aft side of the center pedestal. The components were part of the flap control circuit. The circuit was protected by a five-amp circuit breaker manufactured in 1967. The circuit breaker was checked multiple times to verify what amperage it tripped and the initial test required 17 amps to trip the breaker. The airplane's last inspection was completed on December 28, 2007. The airplane accumulated 14,079 hours of total time at the time of that inspection. The manufacturer indicated that manufacturing practice requires electrical wires and leads of resistors and capacitors to be covered with sleeve insulation. The manufacturer indicated that periodic visual inspections of this wire harness per the Model 99 Maintenance Manual should detect sleeve damage that would allow the 10 ohm, 1/2 watt, resistor to contact the ground lug of a silicon controlled rectifier. The 100 hour inspection listed in the Model 99 Airliner Series Maintenance Manual, Chapter 5-20-00, indicated that the instrument plumbing and wiring should be inspected for "condition, attachment, chafing, etc."

Flight

Event TypeIncident
Event Time20:30 CST
Nearest AirportQuad-City (30nm)
Flight Plan FiledIFR
Flight Plan ActivatedYes
Aircraft FireIflt
Aircraft ExplosionNo

Aircraft

AircraftHawker Beechcraft 99
Tail NumberN118SF
Aircraft CategoryAir
DamageMinor
Operating RulePart 135
Engines2
Engine TypeTurboprop
Engine DetailsPratt & Whitney Canada · PT6A-20 · Turboprop · 550 | Pratt & Whitney Canada · PT6A-20 · Turboprop · 550

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 47 · First Class · None

Conditions

ConditionsVMC
LightNight
Wind270° @ 10 kt, gusting 21 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point7 C / -2 C
Altimeter30.01 inHg
Observation Time01:52
Weather SourceWFAC

Appendix: Source Data