2000 Queensland Beechcraft King Air crash
Central Air Beechcraft 200 Super King Air · Crew incapacitation due to uncontrolled decompression; cause unknown
From Perth International Airport (PER) to Leonora Airport (LNO)
Event
- NTSB case
- DCA00WA092
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Unknown · led by another country; figures from NTSB notifications
- Event fatalities
- 8 · all aircraft and ground
- Ground fatalities
- Unknown
- Occupants
- 8
- Survivors
- 0
- InjuriesFatal: death within 30 days. Serious: over 48 hours in hospital within a week, most broken bones, severe bleeding, nerve or organ damage, or serious burns. Minor: anything less. Glossary
- 0 serious · 0 minor (NTSB)
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- Charter & commuter
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Unknown
Beechcraft 200 Super King Air
- Aircraft type
- Beechcraft 200
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- VH-SKC
- Operator
- Central Air
- Onboard fatalities
- 8
- Route
- From Perth International Airport (PER)To Leonora Airport (LNO)
- Aircraft age
- Not recorded
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Non-U.S., Commercial
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- Not recorded
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Not recorded
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Destroyed
Cause areas
- Personnel issues › Physical
- Personnel issues › Psychological
- Aircraft › Fluids/misc hardware
From the investigation findings the Wikipedia article reports, sorted into the NTSB's cause areas with AI assistance.
Approximate · Coordinates from the Wikipedia article; not checked against an investigation report.
From the Wikipedia article
On 4 September 2000, a chartered Beechcraft 200 Super King Air departed Perth for a flight to the mining town of Leonora, Western Australia. The aircraft crashed near Burketown, Queensland, Australia, resulting in the deaths of all eight occupants. During the flight, the aircraft climbed above its assigned altitude. When air traffic control (ATC) contacted the pilot, the pilot's speech had become significantly impaired, and he was unable to respond to instructions. Three aircraft intercepted the Beechcraft, but were unable to make radio contact. The aircraft continued flying on a straight north-easterly heading for five hours, before exhausting its fuel and crashing 65 km south-east of Burketown. The crash became known in the media as the "ghost flight".
A subsequent investigation by the Australian Transport Safety Bureau (ATSB) concluded that the pilot and passengers had become incapacitated and had been suffering from hypoxia, a lack of oxygen to the body, meaning the pilot would have been unable to operate the aircraft. Towards the end of the flight, the left engine stopped due to fuel exhaustion, and the aircraft crashed into the ground. The investigation report said that, due to extensive damage to the aircraft, investigators were unable to conclude if any of the eight aboard had used the oxygen system. The final report stated that the ATSB could not determine what incapacitated the occupants. A number of safety recommendations were made following the crash.
Background
The aircraft involved in the crash was a Beechcraft 200 Super King Air, registration VH-SKC, manufactured in 1975. The aircraft had about 19,000 hours of service before the crash. The amount of air passed into the cabin is controlled by bleed air valves on the engines. The positions of the bleed air valves can be altered by the pilot. According to the investigation report, "The aircraft was not fitted with a high cabin altitude aural warning device, nor was it required to be." The aircraft was fitted with an emergency oxygen system—an oxygen tank which could supply oxygen to the crew through two masks located in the cockpit, and to passengers through masks which drop from the ceiling of the cabin.
Investigators concluded the aircraft was airworthy at the time of the crash, and a pilot who flew the aircraft earlier in the day said the aircraft functioned normally. The investigation report stated that "the maintenance release was current, and an examination of the aircraft's maintenance records found no recurring maintenance problems that may have been factors in the accident."
Crash
On Monday 4 September 2000, the Beechcraft, chartered by mining company Sons of Gwalia, departed Perth, Western Australia, for the town of Leonora, Western Australia. On board were seven mine workers travelling to Gwalia Gold Mine. The aircraft took off from Perth at 6:09 pm local time (10:09 Coordinated Universal Time (UTC)), and was cleared by ATC to climb to FL130 (13000 ft). Five minutes later, at 10:15, it was further cleared to its cruising altitude of FL250 (25000 ft); and instructed to be at FL160 (16000 ft) by 36 nmi from Perth. The pilot acknowledged this transmission.
Five minutes later, at 10:20, as the aircraft climbed through FL156 (15600 ft), it was cleared to waypoint DEBRA. The pilot again acknowledged. At approximately 10:33, the aircraft passed through its cleared level, and at FL256 (25600 ft), ATC asked the pilot to confirm his altitude. "Sierra Kilo Charlie—um—standby," the pilot replied. This was the final spoken transmission from the aircraft, and its climb continued. According to the investigation report, several open-microphone transmissions followed, with the sound of background noise from the engines, a person breathing, "one unintelligible syllable," and "two chime-like tones, similar to those generated by electronic devices." During this time, ATC attempted to regain contact with the pilot. At 10:40, the controller called out, "Sierra Kilo Charlie Sierra Kilo Charlie, Melbourne Centre, if receiving this transmission squawk ident." At 10:41, the controller asked again, "Sierra Kilo Charlie, only receiving open mike from you. Would you contact me on one two five decimal two."
The aircraft continued to climb, and left radar coverage at 11:02, passing FL325 (32500 ft). Thirty-one minutes later, Australian Search and Rescue asked the crew of a business jet to approach the Beechcraft. They reported that it was in level flight at FL343 (34300 ft), and they could see no movement on the flight deck or in the cabin. However, the conditions made it difficult to observe closely.
Two other aircraft which were asked to monitor the Beechcraft intercepted it over the Northern Territory, north-west of Alice Springs. The pilots reported that it was now in a steady descent, and both aircraft followed it as its airspeed increased. The investigation report stated that the pilots observed that "although its external lights were on, nothing could be seen inside the cabin." The investigation report then describes how "the crews of the chase aircraft attempted to contact the pilot of the Beechcraft by radio, but they did not receive a response." At 15:10, the aircraft turned left through 90 degrees as it descended through 5000 ft. About 65 km south-east of Burketown, Queensland, it hit the ground and disintegrated. The pilot and seven passengers were killed.
Investigation and cause
Investigation
The crash was investigated by the Australian Transport Safety Bureau (ATSB), a federal body responsible for investigating transportation accidents in Australia. The final report was published in March 2001. The report was unable to make a definitive conclusion as to the cause of the crash.
The report found all those aboard the aircraft, including the pilot, had likely become incapacitated and begun suffering from hypoxia.
The report stated, "After the aircraft climbed above the assigned altitude of FL250, the speech and breathing patterns of the pilot, evidenced during the radio transmissions, displayed changes consistent with hypoxia." Investigators were, however, unable to conclusively dismiss toxic fumes as the cause. "The incapacitation of the pilot and passengers was probably due to hypobaric hypoxia because of the high cabin altitude and their not receiving supplemental oxygen" the report said, adding, "The reasons for the pilot and passengers not receiving supplemental oxygen [from the oxygen tank aboard the aircraft] could not be determined."
The ATSB found it likely that the autopilot was engaged, and this caused the aircraft to fly on a straight heading; the vertical path of the aircraft indicated climb power had been set before the occupants of the aircraft were incapacitated. According to the report, "the design of the aircraft systems were such that, with the autopilot engaged, the engines would continue to operate, and the aircraft would continue to fly without human input until it was disrupted by other events, such as collision or fuel exhaustion." It was suggested that, towards the end of the flight, the fuel tank for the left engine was almost empty. "The near exhaustion of fuel in the left wing tanks may have produced at least one, and probably several, momentary losses of left engine power shortly before all power was lost," the report said. "The aircraft yawed and rolled towards the left engine, as was observed shortly before the aircraft collided with the ground."
The report said due to the damage to the aircraft upon impact with the ground, investigators were unable to conclude if any of the eight aboard used the oxygen system. However, the report stated "The absence of a distress radio call, or an attempt to descend the aircraft, and the likelihood that the pilot did not don his oxygen mask, suggested that the pilot was unaware that the aircraft was unpressurised or depressurising." The passengers, the report added, were also likely not wearing their oxygen masks, as there was no noise recorded on the ATC transmissions indicating they were attempting to assist the pilot.
Investigators were not able to determine what caused the depressurisation of the aircraft, but stated likely causes included either an incorrect switch selection due to pilot error, or a mechanical failure in the aircraft pressurisation system. The air traffic control recordings suggested it was unlikely that a rapid decompression had occurred. The report explains how "during an explosive or rapid depressurisation of a pressurised aircraft, however, the noise, pressure changes, temperature changes, and draughts within the cabin would have alerted the occupants that a substantial failure had occurred." The document listed the two main factors in the crash as:
Text from the Wikipedia article “2000 Queensland Beechcraft King Air crash” (revision 1373733526, retrieved 2026-09-18) by its authors, under CC BY-SA 4.0. Extracted as plain text: references, tables, images and some sections are left out. Read the article
Sources
Wikipedia article: 2000 Queensland Beechcraft King Air crash
- Revision
- 1373733526 · 2026-09-07 · retrieved 2026-09-18
- Wikidata
- Q4597179
- Licence
- Text CC BY-SA 4.0, by the article's authors; Wikidata CC0; town positions GeoNames (CC BY 4.0)
NTSB record DCA00WA092
- Event ID
- 20010108X00055
- Case number
- DCA00WA092
- Dataset
- historical-pre2008
- Source SHA-256
- 89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Where each value comes from
- Record
- Wikipedia article "2000 Queensland Beechcraft King Air crash" (page 19488498, revision 1373733526); merged with NTSB case DCA00WA092 (events / aircraft)
- Date
- Wikipedia infobox: date
- Place and country
- Wikipedia infobox: site
- Map position
- Wikipedia: Wikipedia article coordinates
- Aircraft, operator and route
- Wikipedia infobox: aircraft type, registration, operator, origin and destination; route airports from the linked airport articles' Wikidata codes (OurAirports); gaps and aircraft details from NTSB record DCA00WA092
- Operation
- Reviewed correction (2026-09-26): A chartered King Air carrying passengers to a mining town: a small charter flight. The article: "a chartered Beechcraft 200 Super King Air departed Perth for a flight to the mining town of Leonora"
- Fatalities
- Wikipedia: Wikipedia infobox: aircraft fatalities
- Ground fatalities
- Wikipedia: not stated in the Wikipedia infobox
- Summary
- Wikipedia infobox: summary
Source notes (2)
- One occurrence in two sources, merged: the Wikipedia article "2000 Queensland Beechcraft King Air crash" and NTSB case DCA00WA092, matched by the same aircraft registration and date. For this event outside the United States Wikipedia's values are used where the two differ; each value names its source.
- No bulk values were replaced by the NTSB case API.