| Accident summary | |
|---|---|
| Date | December 19, 2005 |
| Type | Structural failure |
| Site | Miami Beach, Florida, United States |
| Passengers | 18 |
| Crew | 2 |
| Injuries | 0 |
| Fatalities | 20 (all) |
| Survivors | 0 |
| Aircraft type | Grumman G-73T |
| Operator | Chalk's Ocean Airways |
| Tail number | N2969 |
| Flight origin | Fort Lauderdale, Florida, United States |
| Stopover | Watson Island, Miami, Florida, United States |
| Destination | Bimini, Bahamas |
Chalk's Ocean Airways Flight 101 was an aircraft crash that occurred off Miami Beach, Florida, in the United States on December 19, 2005. All 20 passengers and crew on board the 1947 Grumman G-73T Turbine Mallard died in the crash, which was attributed to metal fatigue on the starboard wing resulting in separation of the wing from the fuselage.
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On December 19, 2005, Chalk's Ocean Airways Flight 101 from Fort Lauderdale, Florida, United States to Bimini, Bahamas, with an unscheduled stop at Watson Island, Miami, Florida, crashed off Miami Beach, Florida.[1] Witnesses saw white smoke billowing from the plane, before the right wing ripped off and the plane plunged into the ocean. Twenty people — 18 passengers and two crew members — were on board. There were no survivors. Three of the passengers were lap-held infants under the age of two. Just over half of the passengers were from Bimini and returning from Christmas shopping in Florida.
The plane crashed and sank in Government Cut channel, a waterway which connects the Port of Miami with the Atlantic Ocean. Government Cut was closed to shipping until 6:30 p.m. on December 20, stranding at least three cruise ships.[2]
The plane was a Grumman G-73T Turbine Mallard manufactured in 1947. It was the first fatal passenger incident for Chalk's Ocean Airways.[3] The pilot and copilot were, respectively, Michele Marks, 37, of Boynton Beach, Florida, and Paul DeSanctis, 34, of Wyomissing, Pennsylvania.[4]
Sergio Danguillecourt, a member of the board of directors of Bacardi Ltd. (and a great-great-grandson of the rum company's founder Facundo Bacardi), and wife, Jacqueline Kriz Danguillecourt, were on board. Sergio Danguillecourt undid his seatbelt likely as an effort to escape the aircraft; he either jumped or fell out of the aircraft; his body, the last one found, was recovered by a fisherman near Key Biscayne, four miles from the crash site. The bodies of all the other passengers were found still strapped in their seats.[5]
On December 22, 2005 the NTSB issued a press release which included pictures showing metal fatigue on the wing that broke off.[6] On May 30, 2007, Reuters reported that "The National Transportation Safety Board asserted Chalk Ocean Airways failed to identify and properly repair fatigue cracks on the 1947 Grumman Turbo Mallard. The plane lost its right wing a few minutes after take-off for the Bahamas at 500 ft (152 m) and plunged into the shipping channel adjacent to the Port of Miami on December 19, 2005." The safety board, in its final report on the probable cause of the crash, noted numerous maintenance-related problems on the plane and another company aircraft, raising questions about Chalk Ocean's aircraft maintenance practices. "The signs of structural problems were there but not addressed," safety board chairman Mark Rosenker said. The safety board also said the Federal Aviation Administration (FAA) failed to detect and correct the airline's maintenance shortfalls. Regulations exempt older seaplanes from rigorous structural oversight. Chalk Ocean had no comment on the safety board's findings. The FAA said it had no indication Chalk Ocean's maintenance program was in question. "The regulations are crystal clear that the carrier has primary responsibility for the airworthiness of (its) fleet and that includes making appropriate structural repairs," the agency said in a statement.[7]
The cause of the accident was a fatigue failure in the right wing initiated by a crack in a span-wise stringer close to the wing root. The crack had been detected running through a slosh hole (an aperture in the wall of the stringer that allows fuel to flow from one side of the stringer to the other) and seemingly repaired earlier, but the repair was eventually to prove ineffective.
The Mallard was designed in the 1940s with a so-called 'wet wing' where the fuel tanks instead of being separate items within the wing, are constructed from sealed-off portions of the wing structure itself. This eliminates the additional weight of the tanks and also allows more fuel to be contained within a given wing-size. The drawback of this form of construction is that all the joints around the tank seams have to be sealed, so as to make a fuel-tight tank. In addition, as the wing flexes to some extent during flight, the movement has a tendency over extended periods of time to open seams leading to fuel leaks. Grumman, the manufacturer, had issued warnings as early as 1963 about fuel leaks from the Mallard's wing being indicative of possible structural problems, however for unknown reasons the airline did not consider this particularly relevant to its own aircraft.
The accident aircraft had, over a period of several years, developed chronic fuel leakage problems from both wings that had been remedied by the operator by repeatedly applying a sealant to the inside seams of the fuel tanks. Unfortunately, in applying the sealant inside the right wing tank the operator had inadvertently applied the material over a damaged lower stringer - an important, load-bearing structural member of the wing - in such a way as to conceal a fatigue crack, which had earlier been discovered during maintenance and an attempt to repair made by grinding the crack out. In applying the sealant the operator was required to access the inside of the fuel tank using small removable inspection hatches in the top surface of the wing, and of necessity, this resulted in poor visibility and awkward conditions for working inside the tank. Unfortunately the sealant concealed the earlier repair on the stringer and made subsequent checking for further damage to this component, i.e., any crack growth, impossible.
The first outward sign of possible significant problems with the accident aircraft was when a chord-wise (i.e., running from the front of the wing towards the rear) crack was noticed in the skin of the lower surface of the right wing at the root, which, after several failed attempts at stopping the crack by drilling stop-holes, was then repeatedly repaired by affixing doublers - metal patches intended to take over the load from the damaged part, a normal repair procedure for minor skin damage - riveted over the cracked skin, however the crack continued to grow, requiring longer and longer doublers to be fitted. Although the skin crack was slowly getting longer it was not thought to be anything other than a skin problem, which could be dealt with in the normal way, i.e., affixing a doubler.
Like most aircraft of the period the Mallard was built using an aluminium stressed skin construction, in which, unlike earlier fabric covered aircraft where the fabric covering is merely for aerodynamic purposes and contributes little to the overall strength of the airframe, the metal skin itself carries part of the flight loads, i.e., is 'stressed'. Many such aircraft develop minor skin cracks over time and provided appropriate action is taken to repair any cracking then the safety of the aircraft need not be compromised.
Meanwhile the unseen cracked stringer allowed the right wing to flex more during flight which increased the bending forces at the root such that the visible skin crack slowly increased in length with each subsequent flight.
Eventually on the accident flight, the crack in the underside of the wing grew in length until the wing was so weakened it was unable to support the flight loads, and the wing separated. This caused the fuel contained within the wing to be released which then ignited, resulting in the fire that was seen by witnesses.
On examination of the wreckage investigators discovered that in addition to the external ones, internal doublers had also been affixed to the root area of both wings, although maintenance record for these repairs were not available. They also concluded that the cracked stringer that initiated the wing loss had probably failed completely some considerable time prior to the accident, leading to a substantial weakening of the wing structure.
The accident aircraft had been built in 1947 and the manufacturer, Grumman, had produced only 59 examples of this type. When Grumman ceased production of the aircraft in 1951 this eventually left operators with no source of new spare parts, and the airline operator of the accident aircraft, Chalk's Ocean Airways, had had to resort to acquiring several un-airworthy Mallards to cannibalise for spares. In addition, the sort of aircraft used for Chalk's operations, a passenger-carrying flying boat, is of a type no longer manufactured by aircraft companies, so the option of replacing the ageing Mallard fleet with newer designs was not available. At the time of the accident, the accident aircraft was 58 years old, had accumulated 31,226 total flight hours, and had completed 39,743 take-off/landing cycles.
When certificated in 1944 the Mallard design was required to satisfy a static strength analysis, but no fatigue requirement was yet in force as no satisfactory fatigue analysis method had been developed at that time. The Mallard therefore had not been designed with any 'safe life' figure, unlike most civil transport aircraft today which have designed fatigue lives of around 65,000-70,000hrs, or twenty years. In addition, no authorised repair manual for the aircraft type had been issued by the manufacturer, responsibility for authorising repair techniques having been acquired by an outside company after Grumman discontinued support for the type.
The accident aircraft had been acquired by Chalk's in 1980 and had been upgraded to a G-73T Turbo Mallard in July 1981 when its original Pratt & Whitney Wasp H piston engines had been replaced with Pratt & Whitney Canada PT6 turboprops.
Flight 101 (a regularly scheduled flight to Bimini) can be seen in the closing sequence of the pilot episode of Miami Vice titled "Brother's Keeper", where the character of Calderone escapes being arrested by flying off in a Chalk's Grumman G-73 Seaplane with tail number N2969. This episode aired in 1984, many years before the 2005 crash of Chalk's flight 101.
As a result of a number of incidents with aircraft flown by Chalk's pilots, concern had arisen among them about the state of repair of the aircraft, in particular a number of engine failures, and one incident when an elevator control cable snapped in flight, although fortunately the pilot was able to land that aircraft safely. This led to several of Chalk's pilots reconsidering their position in the company, and one, having suffered four engine failures during his period there, and having a wife and new baby to support, resigned his position over what he perceived as persistent maintenance issues with the fleet.
After the accident all remaining Mallards in the Chalk's fleet were grounded. Subsequently all were discovered to be suffering from severe corrosion with many showing signs of sub-standard repair during maintenance.
Most passengers were Bimini locals returning from Christmas shopping.[1][4][8]
| Nationality | Passengers | Crew | Total |
|---|---|---|---|
| Bahamas | 11 | 0 | 11 |
| United States | 7 | 2 | 9 |
| Total | 18 | 2 | 20 |
The story of the disaster was featured on the ninth season of Canadian National Geographic Channel show Mayday (known as Air Emergency in the US, Mayday in Ireland and Air Crash Investigation in the UK and the rest of world). The episode is entitled "Beach Crash."
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