FAA, Fire Safety. This collection contains reports and resources from the Federal Aviation Administration’s Fire Safety Branch research program. Bookmark this collection: https://rosap.ntl.bts.gov/collection_fire_safety.
A commuter category Beechcraft 1900C airliner was subjected to a vertical impact drop test at the FAA William J. Hughes Technical Center, Atlantic City International Airport, New Jersey. The purpose of this test was to measure the impact response of the fuselage, cabin floor, cabin furnishings (including standard and modified seats), and anthropomo
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McGuire, R. J., & Vu, T. (1998). Vertical Drop Test of a Beechcraft 1900C Airliner (Report No. DOT/FAA/AR-96/119). United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research. https://rosap.ntl.bts.gov/view/dot/92727
McGuire, Robert J. and Tong Vu. Vertical Drop Test of a Beechcraft 1900C Airliner. Report no. DOT/FAA/AR-96/119. United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research, 1998. https://rosap.ntl.bts.gov/view/dot/92727.
McGuire, Robert J., and Tong Vu Vertical Drop Test of a Beechcraft 1900C Airliner. United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research, 1998, Report no. DOT/FAA/AR-96/119, ROSA P. https://rosap.ntl.bts.gov/view/dot/92727.
An acoustic emission test for aircraft Halon 1301 bottles has been developed, a prototype acoustic emission test system constructed, and over 200 used bottles tested at the repair facilities of the two manufacturers of these bottles. The system monitors a bottle with six acoustic sensors while the pressure of the bottle is raised by heating it in a
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Beattie, A. (1998). Acoustic Emission Test for Aircraft Halon 1301 Fire Extinguisher Bottles (Report No. DOT/FAA/AR-97/9). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1404587
Beattie, A.G.. Acoustic Emission Test for Aircraft Halon 1301 Fire Extinguisher Bottles. Report no. DOT/FAA/AR-97/9. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1998. https://doi.org/10.21949/1404587.
Beattie, A.G. Acoustic Emission Test for Aircraft Halon 1301 Fire Extinguisher Bottles. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1998, Report no. DOT/FAA/AR-97/9, ROSA P. https://doi.org/10.21949/1404587.
A device was constructed to simulate an exploding aerosol can. The device consisted of a cylindrical pressure vessel for storage of flammable propellants and base product and a high-rate discharge (HRD) valve for quick release of the constituents. Simulator tests were conducted using representative constituents and propellant quantities for compari
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Marker, T. (1998). Initial Development of an Exploding Aerosol Can Simulator (Report No. DOT/FAA/AR-TN97/103). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1404580
Marker, Timothy. Initial Development of an Exploding Aerosol Can Simulator. Report no. DOT/FAA/AR-TN97/103. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1998. https://doi.org/10.21949/1404580.
Marker, Timothy Initial Development of an Exploding Aerosol Can Simulator. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1998, Report no. DOT/FAA/AR-TN97/103, ROSA P. https://doi.org/10.21949/1404580.
A variety of laboratory and full-scale fire tests were conducted on an ethanol-based gel-type hand cleaner currently used in commercial aircraft lavatories. The waterless-type hand cleaner has a relatively low flash point, raising concern over its fire safety when in use in the galley area of commercial transport aircraft where radiant ovens are of
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Marker, T. R., & Do, D. (1998). Fire Testing of Ethanol-Based Hand Cleaner (Report No. DOT/FAA/AR-TN98/15). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1404579
Marker, Timothy R. and Dung Do. Fire Testing of Ethanol-Based Hand Cleaner. Report no. DOT/FAA/AR-TN98/15. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1998. https://doi.org/10.21949/1404579.
Marker, Timothy R., and Dung Do Fire Testing of Ethanol-Based Hand Cleaner. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1998, Report no. DOT/FAA/AR-TN98/15, ROSA P. https://doi.org/10.21949/1404579.
This report presents the results of laboratory round robin flammability testing performed on thermal acoustical insulation blankets and the films used as insulation coverings. This work was requested by the aircraft industry as a result of actual incidents involving flame propagation on the thermal acoustical blankets. Vertical flammability testing
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Cahill, P. (1997). Evaluation of Fire Test Methods for Aircraft Thermal Acoustical Insulation (Report No. DOT/FAA/AR-97/58). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1404584
Cahill, Patricia. Evaluation of Fire Test Methods for Aircraft Thermal Acoustical Insulation. Report no. DOT/FAA/AR-97/58. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1997. https://doi.org/10.21949/1404584.
Cahill, Patricia Evaluation of Fire Test Methods for Aircraft Thermal Acoustical Insulation. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1997, Report no. DOT/FAA/AR-97/58, ROSA P. https://doi.org/10.21949/1404584.
This report contains a summary of the work performed during the development of a minimum performance standard for lavatory trash receptacle automatic fire extinguishers. The developmental work was performed under the direction of the International Halon Replacement Working Group.
Marker, T. (1997). Development of a Minimum Performance Standard for Lavatory Trash Receptacle Automatic Fire Extinguishers (Report No. DOT/FAA/AR-96/122). United States. Department of Transportation. Federal Aviation Administration. https://doi.org/10.21949/1404592
Marker, Timothy. Development of a Minimum Performance Standard for Lavatory Trash Receptacle Automatic Fire Extinguishers. Report no. DOT/FAA/AR-96/122. United States. Department of Transportation. Federal Aviation Administration, 1997. https://doi.org/10.21949/1404592.
Marker, Timothy Development of a Minimum Performance Standard for Lavatory Trash Receptacle Automatic Fire Extinguishers. United States. Department of Transportation. Federal Aviation Administration, 1997, Report no. DOT/FAA/AR-96/122, ROSA P. https://doi.org/10.21949/1404592.
This report provides an overview of the research being conducted by the Federal Aviation Administration (FAA) to develop fire safe cabin materials for commercial aircraft. The objective of the Fire-Resistant Materials program is to eliminate burning cabin materials as a cause of death in aircraft accidents. Long-term activities include the synthesi
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Lyon, R. E. (1996). Fire-Resistant Materials: Research Overview (Report No. DOT/FAA/AR-97-99). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1404581
Lyon, Richard E.. Fire-Resistant Materials: Research Overview. Report no. DOT/FAA/AR-97-99. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://doi.org/10.21949/1404581.
Lyon, Richard E. Fire-Resistant Materials: Research Overview. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA/AR-97-99, ROSA P. https://doi.org/10.21949/1404581.
A British Airtours Boeing 737 experienced an engine failure during takeoff at the Manchester International Airport, in Manchester, England, in 1985 which resulted in 55 fire fatalities. The aircraft's reported initial fuselage burnthrough time of 15 to 20 seconds was inconsistent with previous accidents and Federal Aviation Administration (FAA) lar
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Webster, H. (1996). Fuel Fire Penetration Test and Destruction of a Transport Aircraft (Report No. DOT/FAA/AR-96/48). United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research. https://rosap.ntl.bts.gov/view/dot/92728
Webster, Harry. Fuel Fire Penetration Test and Destruction of a Transport Aircraft. Report no. DOT/FAA/AR-96/48. United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research, 1996. https://rosap.ntl.bts.gov/view/dot/92728.
Webster, Harry Fuel Fire Penetration Test and Destruction of a Transport Aircraft. United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research, 1996, Report no. DOT/FAA/AR-96/48, ROSA P. https://rosap.ntl.bts.gov/view/dot/92728.
Vertical flammability tests specified by the Federal Aviation Administration (FAA) under FAR 25.853 were performed on a variety of interior materials removed from surplus DC-IO, B-707, and B-747 aircraft in order to verify their continued fireworthiness. It was determined that the large majority of materials were in conformance with the test requir
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Cahill, P. (1996). Continued Fireworthiness of Aircraft Interior Materials (Report No. DOT/FAA/AR-TN96/25). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89807
Cahill, Patricia. Continued Fireworthiness of Aircraft Interior Materials. Report no. DOT/FAA/AR-TN96/25. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://rosap.ntl.bts.gov/view/dot/89807.
Cahill, Patricia Continued Fireworthiness of Aircraft Interior Materials. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA/AR-TN96/25, ROSA P. https://rosap.ntl.bts.gov/view/dot/89807.
The characteristics of converging-diverging nozzles are compared to those of converging nozzles for use in aircraft cabin smoke control. The peak flow flight regimes for the two different nozzles are compared by means of test data taken on a Boeing 757. The converging-diverging nozzle is shown as capable of maintaining peak volumetric flow over a w
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Eklund, T. I. (1996). Aircraft Cabin Smoke Control with Converging-Diverging Nozzles (Report No. DOT/FAA/AR-TN96/37). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/90098
Eklund, Thor I.. Aircraft Cabin Smoke Control with Converging-Diverging Nozzles. Report no. DOT/FAA/AR-TN96/37. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://rosap.ntl.bts.gov/view/dot/90098.
Eklund, Thor I. Aircraft Cabin Smoke Control with Converging-Diverging Nozzles. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA/AR-TN96/37, ROSA P. https://rosap.ntl.bts.gov/view/dot/90098.
Flammability testing of aircraft blankets was conducted in order to develop a fire performance test method and performance criteria for blankets supplied to commercial aircraft operators. Aircraft blankets were subjected to vertical Bunsen burner testing, 4-ply vertical testing, full-scale match and cigarette testing, and single- and 4-ply horizont
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Cahill, P. (1996). The Development of a Flammability Test Method for Aircraft Blankets (Report No. DOT/FAA/AR-96/15). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://doi.org/10.21949/1404594
Cahill, Patricia. The Development of a Flammability Test Method for Aircraft Blankets. Report no. DOT/FAA/AR-96/15. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://doi.org/10.21949/1404594.
Cahill, Patricia The Development of a Flammability Test Method for Aircraft Blankets. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA/AR-96/15, ROSA P. https://doi.org/10.21949/1404594.
This report summarizes the findings of Subgroup 4 of the International Materials Fire Test Working Group, which deals with issues involving fire test approval following renovation and repair to interior material systems. The main problem associated with material system renovation is the difficulty in conducting certification tests due to lack of th
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Marker, T. (1996). International Aircraft Materials Fire Test Working Group Material Systems Renovation and Repair Subgroup (Report No. DOT/FAA AR-TN 95/83). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89546
Marker, Timothy. International Aircraft Materials Fire Test Working Group Material Systems Renovation and Repair Subgroup. Report no. DOT/FAA AR-TN 95/83. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://rosap.ntl.bts.gov/view/dot/89546.
Marker, Timothy International Aircraft Materials Fire Test Working Group Material Systems Renovation and Repair Subgroup. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA AR-TN 95/83, ROSA P. https://rosap.ntl.bts.gov/view/dot/89546.
This document describes the methodology for identifying unknown pump motor housing materials suspected of being involved in the propagation of a ramp fire aboard a DC-9 aircraft. The DC-9 was gutted from a fire believed to have originated in the vicinity of this lavatory pump motor. The ramp fire started after power up in Barranquilla, Columbia. Th
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Speitel, L. (1996). Chemical Analysis of Pump Motor Housing Components From DC-9 Ramp Fire at Barranquilla Columbia in March 1995 (Report No. DOT/FAA AR-TN 95/92). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89549
Speitel, Louise. Chemical Analysis of Pump Motor Housing Components From DC-9 Ramp Fire at Barranquilla Columbia in March 1995. Report no. DOT/FAA AR-TN 95/92. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://rosap.ntl.bts.gov/view/dot/89549.
Speitel, Louise Chemical Analysis of Pump Motor Housing Components From DC-9 Ramp Fire at Barranquilla Columbia in March 1995. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA AR-TN 95/92, ROSA P. https://rosap.ntl.bts.gov/view/dot/89549.
The fire response of a potassium aluminosilicate matrix (geopolymer) carbon fiber composite was measured and the results compared to organic matrix composites being used for infrastructure and transportation applications. At irradiance levels of 50 kW/m2, typical of the heat flux in a well-developed fire, glass-or carbon-reinforced polyester, vinyl
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Lyon, R. E. (1996). Fire Response of Geopolymer Structural Composites (Report No. DOT/FAA AR-TN95/22). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89534
Lyon, Richard E.. Fire Response of Geopolymer Structural Composites. Report no. DOT/FAA AR-TN95/22. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996. https://rosap.ntl.bts.gov/view/dot/89534.
Lyon, Richard E. Fire Response of Geopolymer Structural Composites. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1996, Report no. DOT/FAA AR-TN95/22, ROSA P. https://rosap.ntl.bts.gov/view/dot/89534.
This study was undertaken following the completion of a Small Business Innovation Research (SBIR) Phase 2 contract involving the fire hazards of aerosol cans. Tests were conducted on a newly designed aerosol can developed during the SBIR Phase 2 contract as well as two types of currently produced cans. The purpose was to compare the hazards associa
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Hawthorne, C., & Blake, D. (1995). Performance of Improved Aerosol Cans Subjected to an Aircraft Fire (Report No. DOT/FAA AR-TN95/78). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/89533
Hawthorne, Christopher and David Blake. Performance of Improved Aerosol Cans Subjected to an Aircraft Fire. Report no. DOT/FAA AR-TN95/78. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1995. https://rosap.ntl.bts.gov/view/dot/89533.
Hawthorne, Christopher, and David Blake Performance of Improved Aerosol Cans Subjected to an Aircraft Fire. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1995, Report no. DOT/FAA AR-TN95/78, ROSA P. https://rosap.ntl.bts.gov/view/dot/89533.
A review of regulatory actions taken by the Federal Aviation Administration (FAA) over approximately the past thirty years was made to identify which of these actions were preceded by or triggered by research and development (R&D) programs. The focus of this analysis was limited to those actions and R&D that pertained to aircraft safety. Research w
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Westfield, W. T. (1995). The Role of Research and Development on Safety Regulation (Report No. DOT/FAA/AR-95/84). United States. Federal Aviation Administration. Office of Aviation Research. https://rosap.ntl.bts.gov/view/dot/16390
Westfield, William T.. The Role of Research and Development on Safety Regulation. Report no. DOT/FAA/AR-95/84. United States. Federal Aviation Administration. Office of Aviation Research, 1995. https://rosap.ntl.bts.gov/view/dot/16390.
Westfield, William T. The Role of Research and Development on Safety Regulation. United States. Federal Aviation Administration. Office of Aviation Research, 1995, Report no. DOT/FAA/AR-95/84, ROSA P. https://rosap.ntl.bts.gov/view/dot/16390.
A cabin water spray system (CWSS) has been suggested as a means of attenuating the severity of smoke and fire commonly associated with aircraft accidents. All aspects of passenger and cabin safety must be considered when evaluating a new safety system or concept. The purposes of this report are to briefly review the pathophysiological changes occur
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Garner, R. P. (1995). The Potential for Pulmonary Heat Injury Resulting from the Activation of a Cabin Water Spray System to Fight Aircraft Cabin Fires (Report No. DOT/FAA/AM-95/17). Civil Aerospace Medical Institute. https://rosap.ntl.bts.gov/view/dot/21459
Garner, Robert P.. The Potential for Pulmonary Heat Injury Resulting from the Activation of a Cabin Water Spray System to Fight Aircraft Cabin Fires. Report no. DOT/FAA/AM-95/17. Civil Aerospace Medical Institute, 1995. https://rosap.ntl.bts.gov/view/dot/21459.
Garner, Robert P. The Potential for Pulmonary Heat Injury Resulting from the Activation of a Cabin Water Spray System to Fight Aircraft Cabin Fires. Civil Aerospace Medical Institute, 1995, Report no. DOT/FAA/AM-95/17, ROSA P. https://rosap.ntl.bts.gov/view/dot/21459.
The burnthrough resistance of aircraft fuselages to external fuel fires was investigated ln this test series. Three tests were conducted in a wheels-up mode and three in the wheels-down configuration. A comprehensive data base was developed documenting fire entry paths, burnthrough time, and cabin environmental conditions. The overall resistance of
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Webster, H. (1994). Fuselage Burnthrough from Large Exterior Fuel Fires (Report No. DOT/FAA/CT-90-10). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/93177
Webster, Harry. Fuselage Burnthrough from Large Exterior Fuel Fires. Report no. DOT/FAA/CT-90-10. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1994. https://rosap.ntl.bts.gov/view/dot/93177.
Webster, Harry Fuselage Burnthrough from Large Exterior Fuel Fires. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1994, Report no. DOT/FAA/CT-90-10, ROSA P. https://rosap.ntl.bts.gov/view/dot/93177.
Fire tests were conducted on a quarter-scale model of an aircraft cabin to determine ventilation effects on temperature and smoke. The ventilation rates were varied between 1 1/4 and 2 1/2 minutes' time for an air exchange (quarter scale) . The data indicate that there were no significant changes in the cabin temperatures and in the quantity of hea
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Abramowitz, A., & Fann, F. (1993). Ventilation Effects on Smoke and Temperature in an Aircraft Cabin Quarter-Scale Model (Report No. DOT/FAA/CT-89/25). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/93087
Abramowitz, Allan and Franklin Fann. Ventilation Effects on Smoke and Temperature in an Aircraft Cabin Quarter-Scale Model. Report no. DOT/FAA/CT-89/25. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1993. https://rosap.ntl.bts.gov/view/dot/93087.
Abramowitz, Allan, and Franklin Fann Ventilation Effects on Smoke and Temperature in an Aircraft Cabin Quarter-Scale Model. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1993, Report no. DOT/FAA/CT-89/25, ROSA P. https://rosap.ntl.bts.gov/view/dot/93087.
A series of tests were conducted to examine the effect of the ventilation on the environment in an aircraft passenger cabin during an in-flight fire. These tests were run in a reduced scale mockup of an aircraft passenger cabin. A propane burner operating at 10 or 30 kilowatts served as the fire source. The simulated seats and the cabin lining mate
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McCaffrey, B. J., Tu, K. M., Rinkinen, W. J., & Eklund, T. I. (1992). A Model Study of the Aircraft Cabin Environment Resulting from In-Flight Fires (Report No. DOT/FAA/CT-90/22). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/93200
McCaffrey, B. J., King-Mon Tu, W. J. Rinkinen, and Thor I. Eklund. A Model Study of the Aircraft Cabin Environment Resulting from In-Flight Fires. Report no. DOT/FAA/CT-90/22. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1992. https://rosap.ntl.bts.gov/view/dot/93200.
McCaffrey, B. J., et al. A Model Study of the Aircraft Cabin Environment Resulting from In-Flight Fires. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1992, Report no. DOT/FAA/CT-90/22, ROSA P. https://rosap.ntl.bts.gov/view/dot/93200.
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