pavimento rigido normas faa

8/4/2019 Pavimento Rigido Normas Faa

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Program Date 04/30/04

Rigid Pavement Design For AC Method Airport Name: Any Airport Date: today's date

Associated City: Anywhere, USADesign Firm: Engineer's Are Us Designer: Joe Engineer AIP Number: 3-XX-XXX-XX

New Pavement Section Required Stabilized Subbase Is Not Required 0.0 PCC Thickness 650 psi New Concrete Flexural Strength6.0 Stabilized Base0.0 Subbase0.0 Non-Frost Layer (free draining material)

Large Aircraft Parallel to Joints (standard design)Overlay Sections

N/A Asphalt Overlay Thickness N/A Existing Slab Thickness N/A N/A PCC needed for existing section N/A N/A Existing Stabilized Subbase N/A Bonded PCC N/A Existing Aggregate Subbase

N/A Existing Slab Flexural Strength N/A F- Factor used in design

N/A Cr Factor N/A Cb Factor

Dry Unit Weight of Soil (lb/cf ) 100Degree Days F 250Soil Frost Code Non-Frost Subgrade k-value was not modified for frost

Frost Depth Penetration (in) 22.53

k value on top of stabilized layer 215k value on top of subbase layer 100

Original subgrade k value 100

Design Aircraft Information None 20 Design Life (years)

0 lbs Gross Aircraft Weight

Unbonded PCC without leveling courseUnbonded PCC with leveling course

Frost Considerations (for new pavement section)


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Design Pavement Section

FAA Rigid Pavement Design AC 150/5320-6D

PCC PavementStabilized Subbase Layer Aggregate Subbase Layer

SubgradeL

ayer

To assure correct answers - complete each step innumerical order. If data is changed in any given scomplete each step below that step.

This software may be used as noted in Appendix 5 of AC 150/5320-6D, Airport Pavement Design and Evaluation.


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ep,


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Enter up to 21 aircraft (in any order) See right for Large Aircraft Optional design

3 0 0 0.002 0 0 0.00

0 0 0.002 0 0 0.00

0 0 0.002 0 0 0.00

0 0 0.00

0 0 0.000 0 0.000 0 0.000 0 0.00

2 0 0 0.000 0 0.000 0 0.000 0 0.00

0 0 0.000 0 0.000 0 0.000 0 0.000 0 0.00

0 0 0.00

U s e r ' s n a m e

f o r

A i r c r a f

t

( o p t

i o n a

l )

e . g . C

i t a t i o n

I V

A i r c r a f

t g r o u p

i n g

- - - -

G e a r t y p e

A C 1 5 0 / 5 3 2 0 - 6

D

.

.

D e f a u

l t

W e i g h

t

M a x

T a k e o

f f

w e i g h

t M T O W

A n n u a

l

D e p a r

t u r e s

T h i c k n e s s

R e q u i r e

d f o r

E a c

h I n d i v i

d u a l

A i r c r a f

t

Step 4 ENTER AIRCRAT DATA(below)

None

None

None

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NoneNone

None

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None

None

None

None

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None

None

None

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None


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Recommended Critical Aircraft







Recommended Critical AircraftRecommended Critical Aircraft







Recommended Critical AircraftRecommended Critical Aircraft





Gear Parallel to Joints (standard)

Gear Skew to Joints (optional)

Large Aircraft Design


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15

15.5

16

16.5

17

17.5

18

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16

15.99

16.11

16.2216.32

16.4116.5

16.5716.64

16.7116.77

16.8316.89

16.9416.99

17.04 17.08

thickness for DUAL WH-100 at 100000 lbs k on top of all subbase = 215 psi PCC Flexural Stren

ANNUAL DEPARTURES

PCCTHICKN

ESS(in)


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From Aircraft TableAircraft Gross Load GL 0 1

Factor RGL 0 Initial thickness guess 10.000000% load on gear WLP 0 Final thickness 0.000000

Coverage Factor RCA 0Gear Type IGEAR 0 this variable used to determine load configuration (edge or center)

# wheels per gear ITW 0 1 find RC valuesRC0 0 0 0RC1 0 0 0RC2 0 0 0

RC0-2 0 0 Allowable Sig75 = 666.6667RC1-2 0 0 B= #DIV/0!RC2-2 0 0

annual departures 0 CONS = 1586.0743years design 20 CT4 = 1586074.2679

CT4 check 1586074.2679DF 1.3 Radius of Relative thickness RR= 35.4879

Flex Strength 650 650


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if check for zero 100 Frost k Thickness of stabThickness of aggregate layer 0.0 0.00

type of aggregate material FALSEK 50 S =

Y = 1 175 7.5X = 2

sk for 50 100

Final SK to use 500 or less 100100

0.0


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departure thickness rounded x-grid xgridLOOKUP AIRCRAFT DATA 3000 3000 15.99 15 15.99 3000 15

0 3400 16.11 16.11 3000 180 3800 16.22 16.22 3400 180 4200 16.32 16.32 3400 150 4600 16.41 16.41 3800 150 5000 16.5 16.5 3800 180 5400 16.57 16.57 4200 180 5800 16.64 16.64 4200 150 6200 16.71 16.71 4600 150 6600 16.77 16.77 4600 18

0 7000 16.83 16.83 5000 180 7400 16.89 16.89 5000 150 7800 16.94 16.94 5400 15

8200 16.99 16.99 5400 188600 17.04 17.04 5800 18

9000 9000 17.08 18 17.08 5800 15USED TO MAKE CHART 6200 15

Required thickness for None at 0 lbs k 6200 186600 18

0.00 6600 157000 157000 187400 187400 157800 157800 188200 18

8200 158600 15

0.00000000 8600 189000 18

r new design 9000 15


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ilized layer 6.0

K 50 S =Y = 0.7 195 10X = 2.26

sk for 50 215

Final SK to use 500 or less 215215

6.0


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xlabels PSI PSI thickness rounded x-grid xgrid xlabels15 500 500 19.55 14 19.55 500 14 1415 520 19.05 19.05 500 20 1415 540 18.57 18.57 520 20 1415 560 18.12 18.12 520 14 1415 580 17.7 17.7 540 14 1415 600 17.3 17.3 540 20 1415 620 16.92 16.92 560 20 1415 640 16.56 16.56 560 14 1415 660 16.22 16.22 580 14 1415 680 15.89 15.89 580 20 14

15 700 15.58 15.58 600 20 1415 720 15.29 15.29 600 14 1415 740 15 15 620 14 1415 760 14.73 14.73 620 20 1415 780 14.47 14.47 640 20 1415 800 800 14.22 20 14.22 640 14 14

USED TO MAKE CHART 660 14Required thickness for None at 0 lbs 660 20

680 20680 14700 14700 20720 20720 14740 14740 20760 20

760 14780 14780 20800 20800 14


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14

15

16

17

18

19

20

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16

19.55

19.05

18.57

18.12

17.7

17.3

16.92

16.56

16.22

15.89

15.58

15.29

1514.73

14.47

14.22

kness for DC 10-30WING at 600000 lbs k on top of all subbase = 100 psi 10851 departures -- sub

PCC Flexural Strength

PCCTHICKNESS(in)


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Any Airport AIP Number AC Method

Anywhere, USA 3-XX-XXX-XX today's date

Engineer's Are Us Joe Engineer INPUT VALUES

W i d e b o d y ?

G e a r T y p e

( c o d e )

% l o a d o n m a

i n g

n 3 0 0 0 0.00 0 0 0 0

n 2 0 0 0 0.00 0 0 0 0

n 0 0 0 0.00 0 0 0 0n 2 0 0 0 0.00 0 0 0 0

n 0 0 0 0.00 0 0 0 0n 2 0 0 0 0.00 0 0 0 0

n 0 0 0 0.00 0 0 0 0n 0 0 0 0.00 0 0 0 0n 0 0 0 0.00 0 0 0 0n 0 0 0 0.00 0 0 0 0n 0 0 0 0.00 0 0 0 0n 2 0 0 0 0.00 0 0 0 0n 0 0 0 0.00 0 0 0 0

n 0 0 0 0.00 0 0 0 0n 0 0 0 0.00 0 0 0 0n 0 0 0 0.00 0 0 0 0n 0 0 0 0.00 0 0 0 0n 0 0 0 0.00 0 0 0 0n 0 0 0 0.00 0 0 0 0n 0 0 0 0.00 0 0 0 0

n 0 0 0 0.00 0 0 0 0Equivalent Annual Departures of the None 0

Design Aircraft --- /---Additional aircraft A

i r c r a

f t g r o u p

i n g

- - - -

G e a r t y p e

A C 1 5 0 / 5 3 2 0 - 6

D

M a x

T a k e o f f

w e i g h

t M T O W

A n n u a

l

D e p a r

t u r e s

M T O W

u s e d

b y

d e s i g n

D e p a r

t u r e s o f

e q u i v g e a r

C o m p u

t e d w h e e

l

L o a d o f a i r c r a

f t

E q u i v . a n n u a l

d e p a r t u r e s o f

d e s i g n

A i r c r a

f t

None

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pavimento rigido normas faa

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