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Printed page 136. PDF page 150.
right rear lug while the vertical stabilizer was exposed to aerodynamic loads that were about twice the certified limit load design envelope and wereOpen final at PDF page 150In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 159. PDF page 173.
right rear lug while the vertical stabilizer was exposed to aerodynamic loads that were about twice the certified limit load design envelope and were more than the certified ultimate load design envelope. 7. The first officer had a tendency toOpen final at PDF page 173In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587