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Printed page 135. PDF page 149.
maximum load to be expected in service, and ultimate load is limit load multiplied by a safety factor of 1.5. During public hearing testimony, an FAA airframe engineer stated that airplanes are expected to experience limit load only once inOpen final at PDF page 149In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 32. PDF page 46.
determining those loading conditions are shown to be reliable.” Section 25.303, “Factor of safety,” was at amendment level 44 (enacted in December 1978) at the time that the A300-600 was certificated. This section stated the following: Unless otherwise specified, aOpen final at PDF page 46In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587