Fatal Falcon 50 Runway Excursion Accident: Unairworthy with Unqualified Crew
On 27 September 2018 Dassault Falcon 50 N114TD, operated by Air America Flight Services on a Part 135 on-demand air taxi flight, was destroyed in a runway excursion at Greenville Downtown Airport (GMU), South Carolina. The two pilots were fatally injured. The two passengers were seriously injured.
The Accident Flight
The Dassault Falcon 50 is a midsize long-range business jet. According to the cockpit voice recorder (CVR), during the approach to GMU, the flight crew had difficulties understanding the navigation fixes that air traffic control had provided. The CVR also showed that the flight crew did not use any prelanding checklist or discuss that no braking was available with the brake system in the “#1-ON” position (the pilot was the copilot for the previous four flights in the airplane, during which this condition was present).
The “#1-ON” position of the switch selected normal braking utilizing system 1, and provided antiskid protection, while the “2-OFF” position selected emergency braking and did not provide antiskid. According to the pilot who conducted four flights in the airplane before the accident flight, upon application of the brakes with the brake switch in the “#1-ON” position, braking was normal at low speeds (estimated to be 15-20 knots) but at faster speeds, no braking was available. Braking was restored when the brake switch was placed in the “#2-OFF” position.
This pilot [who who commanded the four flights prior] stated that he reported the brake system failure to the company’s Director of Maintenance after the first two flights (in late August and early September 2018) and indicated his belief that the source of the problem was the antiskid system.
In interview with the Director of Maintenance, the son of the accident co-pilot, denied that he had been told. He also stated there were no defects deferred on the aircraft and the NTSB found no maintenance records indicating a brake system issue. However:
Next to the switch, a green sticker was affixed to the panel with the label “ATA # 32-5 “INOP” DATE: 9/27/18”.
The NTSB go on:
At 1345:34, the CVR recorded the sound of the airplane touching down. At 1345:38, the pilot stated that the brakes were not operating. He and the copilot commented about the lack of brakes several more times before the airplane went over an embankment and came to a stop.
Air traffic controllers at GMU reported that the airplane touched down “normally” at a standard touchdown point on the runway. They saw the airplane’s thrust reverser deploy and watched as the airplane continued down the runway without decelerating.
An airport security video captured the airplane’s touchdown and showed that the thrust reverser and the airbrakes were deployed. The video [below as stills with time in lower left corner] also showed the airplane as it continued to the end of the runway and went over the embankment.
A second video:
[The aircraft had] departed the left edge of the runway  near the departure end, traveled across the flat grassy area at the end of the runway, continued down a 50-foot embankment, and came to rest on the airport perimeter road about 425 ft from the runway.
The wreckage was oriented on a heading of about 160°.
Aviation Safety Network reports that:
First responders reported that all three engines were operating at full power for at least 20 minutes after the accident with, one engine running until about 40 minutes after the accident.
According to the operator’s Director of Maintenance, the aircraft had been kept in storage for about 4 years.
In June 2018, a work order was generated to return the airplane to a serviceable status. The work order included a 12-month inspection, a 12-month or 500-hour inspection, a 24-month inspection, and a 36-month inspection. The work order also indicated that 1C, 3C, and 5C checks were to be completed and that a total of 103 discrepancies found during the ongoing inspections needed to be addressed.
Amazingly (emphasis added):
The work order was about 60% complete at the time of the accident, and there were no maintenance log entries made indicating that the airplane was airworthy and returned to service.
The work order did not include removal of the landing gear for overhaul. The last overhaul of the landing gear (main and nose) was completed on July 23, 2002. During the overhaul, the electrical harness for the landing gear position sensors and antiskid transducers was removed and replaced. The overhaul interval was 12 years (plus a grace period of 5 months) or 6,000 landings, whichever came first. As a result, a landing gear overhaul should have been performed no later than December 23, 2014.
There was an extensive examination of the aircraft’s brakes:
Computed tomography [CT scans] performed on the antiskid system components revealed a broken solder joint on the left-side inboard transducer and a bent pin connection on the right-side inboard transducer. Functional tests of the antiskid wheel speed transducers revealed a failure in the operation of the left-side inboard wheel speed transducer; the other three transducers passed their respective functional tests. Visual inspection of the wiring for the right-side wheel speed transducers found that the wiring to the right outboard transducer was reversed.
In relation to the crew, the NTSB discovered (emphasis added):
The pilot[-in-command] held an airline transport pilot certificate and a type rating for the Dassault Falcon 50 with a limitation for second-in-command privileges only. He also held type ratings for Learjet and Westwind business jets.
The co-pilot [the second-in-command and owner of the company] [only] held a private pilot certificate with ratings for airplane single and multiengine land. He did not hold any type ratings nor did he hold an instrument rating.
The NTSB give little further background on the operator or the FAA‘s regulatory oversight but it is noticeable that the NTSB preliminary report described this flight as a Part 91 Personal flight, which suggests there was some initial uncertainty on the status of the flight.
NTSB disappointingly also do not talk about emergency response, cabin safety or survivability matters. There is no comment whether any FDR data was available.
NTSB also does not discuss the airport layout. Runway 1 is long and has an Engineered Materials Arresting System (EMAS) bed to protect the adjacent road. EMAS beds contain high energy absorbing materials of selected strength which will reliably and predictably crush under the weight of an aircraft.
EMAS therefore provides and alternative to having an adequate Runway End Safety Area (RESA).
However, downward sloping Runway 19 that the accident occured on lacks EMAS but has a large embankment, up to 50 feet high around most of the last quarter of the runway.
NTSB Probable Cause
The operator’s decision to allow a flight in an airplane with known, unresolved maintenance discrepancies, and the flight crew’s failure to properly configure the airplane in a way that would have allowed the emergency or parking brake systems to stop the airplane during landing.
A number of other accidents question safety standards in the US business aviation sector:
- Business Aviation Compliance With Pre Take-off Flight Control Checks
- Gulfstream G-IV Take Off Accident & Human Factors
- Fatal US G-IV Runway Excursion Accident in France – Lessons
- Execuflight Hawker 700 N237WR Akron Accident: Casual Compliance
- Unstabilised Approach Accident at Aspen
- Disorientated Dive into Lake Erie
- G-III Attempted Takeoff Using Runway Edge Lights as Centerline
- Wait to Weight & Balance – Lessons from a Loss of Control
- Business Jet Collides With ‘Uncharted’ Obstacle During Go-Around
- Director of Maintenance Pleads Guilty To Obstructing an NTSB Air Accident Investigation
- G200 Leaves Runway in Abuja Due to “Improper” Handling
- Cockpit Tensions and an Automated CFIT Accident
- Aborted Take Off with Brakes Partially On Results in Runway Excursion
- Global 6000 Crosswind Landing Accident – UK AAIB Report
- Luftwaffe VVIP Global 5000 Written Off After Flying Control Assembly Error
- Falcon 7X LOC-I Due To Solder Defect
- Impromptu Flypast Leads to Disaster
- UPDATE 13 June 2020: Visual Illusions, a Non Standard Approach and Cockpit Gradient: Business Jet Accident at Aarhus
We also have covered this braking related maintenance error: NTSB Confirms United Airlines Maintenance Error After 12 Years
UPDATE 10 June 2020: An accident after a maintenance error during storage: B767 Fire and Uncommanded Evacuation After Lockwire Omitted