3-48 FAA APPROVED 4-30-76
REISSUED 2-25-81, CHANGE 14
ABORTED TAKEOFF
1. Thrust Levers — IDLE.
2. Wheel Brakes — Apply.
3. Spoilers — EXT.
4. Drag Chute or Thrust Reversers (if installed) — Deploy, if
necessary.
5. • If rejected takeoff was made at a speed of less than 40 knots,
one subsequent takeoff attempt may be made without any waiting
period.
• If rejected takeoff was made at a speed of between 40 and 80
knots, a 20-minute waiting period must be observed, and the main
gear tires, wheels and brakes must be visually inspected before a
subsequent takeoff attempt is made.
• If rejected takeoff was made at a speed of greater than 80 knots,
but with the airplane below the maximum landing brake energy
weight (see applicable LANDING WEIGHT LIMITS chart in Sec-
tion V), a 1-hour waiting period must be observed, and the main
gear tires, wheels and brakes must be visually inspected before a
subsequent takeoff attempt is made.
• If a rejected takeoff was made at a speed of greater than 80
knots and with the airplane at or above the maximum landing
brake energy weight (see applicable LANDING WEIGHT LIMITS
chart in Section V), see maintenance personnel to perform the
High Energy Stop inspection.
• If the stop was conducted above the landing maxi-
mum brake energy limit, it is recommended that the
PARKING BRAKE be released and chocks used.
This will increase the brake cooling efficiency and re-
duce the possibility of wheel fuse plug release and
brake/tire fire.
• Do not attempt a third takeoff after two rejected
takeoffs without a 4-hour waiting period and another
visual inspection of the main gear tires, wheels, and
brakes.
NOTE
3-48 FAA APPROVED 4-30-76
REISSUED 2-25-81, CHANGE 14
ABORTED TAKEOFF
1. Thrust Levers — IDLE.
2. Wheel Brakes — Apply.
3. Spoilers — EXT.
4. Drag Chute or Thrust Reversers (if installed) — Deploy, if
necessary.
5. • If rejected takeoff was made at a speed of less than 40 knots,
one subsequent takeoff attempt may be made without any waiting
period.
• If rejected takeoff was made at a speed of between 40 and 80
knots, a 20-minute waiting period must be observed, and the main
gear tires, wheels and brakes must be visually inspected before a
subsequent takeoff attempt is made.
• If rejected takeoff was made at a speed of greater than 80 knots,
but with the airplane below the maximum landing brake energy
weight (see applicable LANDING WEIGHT LIMITS chart in Sec-
tion V), a 1-hour waiting period must be observed, and the main
gear tires, wheels and brakes must be visually inspected before a
subsequent takeoff attempt is made.
• If a rejected takeoff was made at a speed of greater than 80
knots and with the airplane at or above the maximum landing
brake energy weight (see applicable LANDING WEIGHT LIMITS
chart in Section V), see maintenance personnel to perform the
High Energy Stop inspection.
• If the stop was conducted above the landing maxi-
mum brake energy limit, it is recommended that the
PARKING BRAKE be released and chocks used.
This will increase the brake cooling efficiency and re-
duce the possibility of wheel fuse plug release and
brake/tire fire.
• Do not attempt a third takeoff after two rejected
takeoffs without a 4-hour waiting period and another
visual inspection of the main gear tires, wheels, and
brakes.
NOTE
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