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Printed page 3. PDF page 17.
longitudinal load factor, a 0.07 G shift to the left in lateral load factor, and about a 0.3 G drop in normal (vertical) load factor.12 The airplane performance study found that these excursions were consistent with a wake turbulence encounter.Open final at PDF page 17In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 138. PDF page 152.
flight 47. The effect of the turbulence was typical of a minor wake encounter-a momentary 0.3 G drop in normal load factor, a 0.04 G drop in longitudinal load factor, and a 0.07 G shift in lateral load factor. However,Open final at PDF page 152In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page label not indexed. PDF page 133.
shock during drop along the slope on the side of the third branch of Sugeno Dale. 3.2.10.3 Four persons survived this accident, but they were all seriously injured. All of them were seated at the aft portion of the aftOpen official document at PDF page 133AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119