Repairing Damaged Aircraft

Repairing Damaged Aircraft Is a Difficult and Expensive Business

Aircraft damage is becoming more difficult to detect and repair, as well as becoming more than ever critical to aircraft safety, and the world’s airworthiness authorities are increasingly concerned at the diminishing resources available to monitor properly the maintenance practices of the airlines.

These are problems which are concerning airworthiness authorities and both civil and military operators worldwide, given that, for example, a third of the US civil aircraft fleet is now beyond its original design life of 20 years. The Aloha 737 accident in April 1988, where the top of the fuselage “unzipped”, indicated that a close hard look at damage mechanisms was needed. Matters being examined are the regulation of airworthiness, structural integrity, damage tolerance versus fail safe versus safe life philosophies, detection and repair techniques, use of composite materials and maintenance practices – topics of great concern to safety and economics for all operators. As well, there seem to be some political pressures emerging, seeking to reduce the costs of ensuring airworthiness.

The US Federal Aviation Administration has its “Initiatives in Aging Aircraft Research for Assurance of Continuing Airworthiness”, a program mandated by the US Aviation Safety Research Act of 1988. The intent is to develop technologies needed to ensure continued airworthiness of older US civil aircraft. The program investigates the implications of: the increasing frequency of small simultaneous structural cracks linking to “unzip” into a catastrophic break (Multiple Site Damage, MSD, as in the Aloha 737 incident): the increasing frequency of cracks in inaccessible places and the decreasing chances of detection; interaction of fatigue and corrosion; and the stress problems induced by improperly designed or applied repairs. The program covers both metallic and composite structures and examines past and present structural design practices, maintenance and inspection, corrosion control, human factors and a concept of using intelligent networks to search and correlate maintenance data from diverse sources to increase the maintenance database.

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Both metallic and composite structures present their own particular problems, not the least of which is actually finding cracks and defects before catastrophe occurs. Non Destructive Testing (NDT) is still the basic tool for detection, but there are limitations. Even improved methods still need some idea of position to be fully effective in discovering faults and the complexity of modern faults makes life very difficult. Considerable research is in hand in the US on new techniques.

Delamination is also a major problem in composite materials, where large loss of compressive strength can occur with little or no surface indication. An interesting new technique is emerging, in which fibre optic cables are embedded in new composites, and, when damage occurs, the resulting signals are read off and analysed externally.

Another new method, under development at the Australian Defence Force Academy in Canberra, is the use of holography to find very small cracks about 3 microns long. Perhaps operators would still like to have the old time inspectors who could smell invisible cracks from a hundred metres away on a wet and windy night!

Once having located the defects, there is the problem of devising repairs. Badly designed repairs are often worse than no repairs, since they give false security and make inspection more difficult. Things are even more difficult where an old aircraft, designed on safe life principles but with an unknown life remaining, needs repairs. Both the Australian and UK Civil Aviation Authorities have been involved in various international talks on the matter, and the UK CAA has produced its requirements for the design and approval of repairs, particularly where the manufacturer gives little guidance. The essence of all such requirements is the prescription of analysis, materials, components, incorporation and documentation. Some elegant theoretical methods of stress analysis and life prediction are being developed, and the bad old days of rivetting on a thicker patch over the crack are long since gone (although this writer well remembers doing so in a previous incarnation forty-odd years ago).

For composite materials, an International Air Transport Association Task Force has published its “Guidance Material for Design, Maintenance and Repair of Thermo-setting Epoxy Matrix Composite Aircraft Structures”. Composite repairs have the advantage over metallic ones in that, if they are properly done, they do not cause stress concentration, they give stiffer load paths and they generally do not inhibit future inspections. They can be used on thick structures as well as skins.

Air forces have a special interest in repair techniques for Aircraft Battle Damage Repair work. This is the practice of making the best use of combat aircraft by doing just enough repairs to make them fit for the next missions when they have received damage, or, where damage is severe, making them flyable to move them from the operational areas to bases where deep repairs can be done. The UK Royal Air Force views ABDR as a “force multiplier”, based on its Gulf experiences. Effective ABDR depends on meticulous pre-planning, experienced staff and the right repair kits and practices already in place.

Civil Aviation Authorities and airlines, as major players in the airworthiness business, need to work closely together to maintain standards, in the face of reduced funding by Governments and sharply rising maintenance costs. The Australian Government has said that, while standards are to be maintained, it will not continue funding aviation safety regulation after 1992. The burden of proof has shifted: those who wish to maintain existing standards now have to argue their case for retention, not those seeking relaxation of standards.

Airlines find it difficult to obtain and keep the qualified and experienced staffs needed to uphold the maintenance and safety requirements, and the maintenance load is increasing faster than the number of staff. There is no doubt that some costs can be cut, but maintenance of safety is inherently a costly business, and there is the old saying that “if you think safety is expensive, try having an accident!”.

 

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