Page 117 - Planning and Design of Airports

86 Airp o r t Pl anning

TOR = TOD − CL (2-7c)
1 1 1max
FS = TOR (2-7d)
1 1
Engine-failure takeoff case:

FL = FS + CL (2-8)
2 2 2max
where

TOD = D35 (2-8a)
2 2
CL = 0.50(TOD − LOD ) (2-8b)
2max 2 2
TOR = TOD − CL (2-8c)
2 2 2max
FS = TOR (2-8d)
2 2
Engine-failure aborted takeoff:

FL = FS + SW (2-9)
3
where

FL = DAS (2-9a)
3
Landing case:

FL = LD (2-10)
4
where

SD
LD = (2-10a)
.
060
FS = LD (2-10b)
4
To determine the required field length and the various compo-
nents of length which are made up of full-strength pavement, stop-
way, and clearway, the above equations must each be solved for the
critical design aircraft at the airport. This will result in finding each of
the following values:

FL = max [(TOD ), (TOD ), (DAS), (LD)] (2-11)
1 2
FS = max [(TOR ), (TOR ), (LD)] (2-12)
1 2
SW = [(DAS) − max (TOR , TOR , LD)] (2-13)
1 2