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Tail Strike Briefing Tail Strike Briefing
- Capt. Ray Craig
Airplane Validation & Flight Operations
Boeing Commercial Airplanes May 2004
- Capt. Ray Craig
Airplane Validation & Flight Operations
Boeing Commercial Airplanes May 2004
Tail Strike Briefing Tail Strike Briefing Capt. Ray Craig Capt. - - PowerPoint PPT Presentation
Tail Strike Briefing Tail Strike Briefing Capt. Ray Craig Capt. Ray Craig Airplane Validation & Flight Operations Airplane Validation & Flight Operations Boeing Commercial Airplanes Boeing Commercial Airplanes May 2004 May 2004
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Airplane Validation & Flight Operations
Boeing Commercial Airplanes May 2004
Airplane Validation & Flight Operations
Boeing Commercial Airplanes May 2004
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The Boeing Company
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The Boeing Company
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The Boeing Company
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The Boeing Company
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landing therefore has higher damage
body for landing. However, 737-800/900 have adequate aft body landing clearance
all Boeing models due to increased deliveries and/or new pilots
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The Boeing Company
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The Boeing Company
– 3 without damage (not listed) – 10 with damage – 3 occurred during takeoff – 7 occurred during landing – limited damage occurred during takeoff tailstrikes – the 737-800/900 tailskid protects the aircraft on takeoff not on landing
– 3 without damage (not listed) – 10 with damage – 3 occurred during takeoff – 7 occurred during landing – limited damage occurred during takeoff tailstrikes – the 737-800/900 tailskid protects the aircraft on takeoff not on landing
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The Boeing Company
gusty/crosswind conditions
gusty/crosswind conditions
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– Wrong weights – Incorrect center of gravity (CG)
– Normal recommended rotation rate is 2 to 3 dps – Nose up mis-trim can rotate 5 dps or more – Aircraft may try to fly off runway without any pilot input
– Wrong weights – Incorrect center of gravity (CG)
– Normal recommended rotation rate is 2 to 3 dps – Nose up mis-trim can rotate 5 dps or more – Aircraft may try to fly off runway without any pilot input
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setting
setting
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height at runway end
performance
strike
height at runway end
performance
strike
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The Boeing Company
guidance only after the aircraft is airborne, nominally passing 35 feet
degrees and a speed of V2 + 10 (V2 + 15 on some models)
the tail into the ground
guidance only after the aircraft is airborne, nominally passing 35 feet
degrees and a speed of V2 + 10 (V2 + 15 on some models)
the tail into the ground
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The Boeing Company
technique for -600 thru -900
excessive attitude
for actual thrust used
additional tail clearance
conditions
technique for -600 thru -900
excessive attitude
for actual thrust used
additional tail clearance
conditions
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The Boeing Company
Note: Tail strikes on landing generally cause more
gear damaging the aft pressure bulkhead.
Note: Tail strikes on landing generally cause more
gear damaging the aft pressure bulkhead.
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will never get the approach stabilized – Excessive or insufficient airspeed in the flare – Long on runway touch down
changes in the flare
will never get the approach stabilized – Excessive or insufficient airspeed in the flare – Long on runway touch down
changes in the flare
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touch down causing a tail strike
flare does not reduce the sink rate, but may increase it
touch down causing a tail strike
flare does not reduce the sink rate, but may increase it
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flare resulting in high pitch attitude
landing flair
an attempt to make an extremely smooth touchdown
main gear touchdown
flare resulting in high pitch attitude
landing flair
an attempt to make an extremely smooth touchdown
main gear touchdown
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The Boeing Company
especially in gusty conditions
rates of 700 to 900 feet are required
increases drag, and may increase rate of descent
plus turbulence, can increase tail strikes
especially in gusty conditions
rates of 700 to 900 feet are required
increases drag, and may increase rate of descent
plus turbulence, can increase tail strikes
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bounced landing, can cause tail strikes
consider a go-around
bounced landing, can cause tail strikes
consider a go-around
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landing attitude and add thrust as necessary to control rate of descent
skip
around procedures. A second touchdown may
landing attitude and add thrust as necessary to control rate of descent
skip
around procedures. A second touchdown may
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flare
the flare or after touchdown
excessively smooth landing
back pressure on control wheel and fly the nose wheel
– Do not allow pitch attitude to increase after touchdown – Do not attempt to use aero braking - it does not work !
flare
the flare or after touchdown
excessively smooth landing
back pressure on control wheel and fly the nose wheel
– Do not allow pitch attitude to increase after touchdown – Do not attempt to use aero braking - it does not work !
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briefings in all initial, transition and recurrent training
briefing tool during training
briefings in all initial, transition and recurrent training
briefing tool during training
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during training
sessions
during training
sessions
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proper training
continuous
proper training
continuous
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