Commercial aircraft wreckage, composed of 70 to 80 percent aluminum by structural weight in narrowbody types like the Boeing 737 and Airbus A320, does not enter any disposal or recycling stream until an extensive, legally codified investigative process has run its full course. In the United States, 49 CFR Part 831 grants the NTSB exclusive jurisdiction over accident sites and all physical evidence within them, effectively elevating debris field material to the legal status of evidence in a criminal proceeding rather than industrial scrap. Internationally, ICAO Annex 13 mirrors this framework, assigning investigative authority to the State of Occurrence and mandating preservation of all physical evidence until formal authorization for removal is granted. These two instruments operate in parallel and are binding on operators, manufacturers, and governments alike, meaning that no part of an aircraft — from a fuselage barrel section to a fractured floor beam — can be legally disturbed, relocated, or disposed of before competent authority has documented and released it.
The NTSB's Go Team, which deploys within hours of a major accident, organizes its work around functional groups covering structures, powerplants, systems, flight operations, air traffic control, meteorology, and human performance — more than 100 specialists in major investigations, coordinated across as many as a dozen parties and multiple federal and local agencies. Structures specialists and materials engineers begin not by moving wreckage but by building a complete spatial record of it, using GPS positioning, photogrammetry, and high-resolution video to produce a georeferenced map of every fragment before collection begins. The position, orientation, and separation distances of pieces relative to one another encode information about the in-flight or ground-impact breakup sequence that is permanently destroyed the moment a fragment is displaced without documentation. This phase is not procedural formality — it is the primary means by which investigators reconstruct whether a structural failure preceded impact, whether a fatigue crack propagated from a specific joint, or whether the breakup pattern is consistent with a particular flight regime or control state.
Component priority during physical extraction reflects investigative value rather than mass or accessibility. Flight Data Recorders and Cockpit Voice Recorders — encased in titanium and designed to survive 3,400 g of impact force and 2,012 degrees Fahrenheit of sustained flame — are recovered first. High-value structural components follow: actuators, control surfaces, engine fan blades, turbine sections, and primary structural joints where fatigue or corrosion may have initiated failure. Only after these items are extracted and tagged does the bulk aluminum proceed toward the industrial removal phase, where fuselage barrel sections, wing skins, and floor beams — typically mangled, folded, and fused with soil and fuel residue — are reduced by excavators into transportable fragments and loaded into roll-off containers. The January 2025 mid-air collision between an American Eagle CRJ700 and a US Army Black Hawk helicopter over the Potomac River illustrated the additional complexity of aquatic recovery, requiring six days of diving operations in cold, dark, current-affected water before all human remains were recovered, with structural debris removal extending well beyond that timeline.
For airline operations departments, flight safety officers, and Part 135 and Part 91K operators, the forensic lifecycle of wreckage aluminum is directly relevant because the findings extracted from that material shape the airworthiness directives, structural inspection requirements, and maintenance program modifications that follow every major accident. The detailed reconstruction of large-scale accidents — physically reassembling fragments to map fracture propagation and failure sequencing — has driven some of the most consequential airworthiness actions in modern aviation, including corrosion detection programs, lap joint inspection requirements, and composite structure monitoring protocols. The pace at which this process can be completed also affects how quickly an aircraft type can return to unrestricted service following a systemic finding, a factor that fleet operators and schedulers must account for when similar accident signatures emerge. Understanding the governed, sequential nature of wreckage disposition reinforces why aircraft accident investigation timelines run on the order of months to years rather than weeks, and why premature release of physical evidence — however operationally inconvenient — would undermine the integrity of the causal findings on which future safety actions depend.