ML20138J152

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Rev 1 to SQUG Walkdown Sample - Floor/Ceiling Cable Tray Supports
ML20138J152
Person / Time
Site: Davis Besse Cleveland Electric icon.png
Issue date: 08/28/1995
From: Osting S
TOLEDO EDISON CO.
To:
Shared Package
ML20138J127 List:
References
C-CSS-100.03-01, C-CSS-100.03-013-R01, C-CSS-100.03-1, C-CSS-100.03-13-R1, NUDOCS 9705080052
Download: ML20138J152 (48)


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ATTACHMENT - *

- SHEET __I _0F._7_

4EL&ri cac No.

c-cu-io o.03 o q-q;g i

. _. -,I L E A: sT %o c

E

?

a d

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  • o a a 8

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..... x x x e E,z e

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ATTACHMENT A

SHEET

  • 0F 9 4

f PAGE NO.

1 CALC.N0.

C-C5 5 -lo b 0 3-C43 ID: Toledo Edison I

8 T A A D - III Revision 20.0b Proprietary Program of Research Engineers, Inc.

Date=

APR 20, 1995 d

Time =

9:51:29 USER ID: Toledo Edison 1.

STAAD SPACE 2.

UNIT INCH KIPS 3.

JOINT COORDINATES 4.

1 0.

O.

O.

5.

2 0.

22.

O.

6.

3 0.

36.5 0.

7.

4 0.

54.

D.

8.

5 O.

62.5 0.

9.

6 0.

76.5 0.

10. 7 0.

98.

O.

11. 8 -20.

22.

O.

12. 9 -20.

54.

O.

13. 10 20. 36.5 0.
14. 11 20. 62.5 O.
15. 12 20. 76.5 0.
16. MEMBER INCIDENCES
17. 112
18. 22 3
19. 3 3 4
20. 4 4 5
21. 5 5 6
22. 667
23. 78 2
24. 89 4
25. 9 3 10
26. 10 5 11
27. 11 6 12
28. MEMBER PROPERTIES
29. 1 TO 6 PRIS AX 1.95 IX.1 IY 1.107 YD 4.875 IZ 4.062 ZD 1.625
30. 7 TO 11 PRIS AX 1.11 IX.1 IY.478 YD 3.25 IZ.93 ZD 1.625
31. SUPPORTS
32. 1 FIXED BUT MY MZ
33. 7 FIXED BUT FY MY MZ
34. CONSTANTS
35. E 29000. ALL
36. DEN.000283 ALL
37. LOAD 1
38. SELF X

.96

39. SELF Y -1.
40. JOINT LOAD
41. 8 TO 10 FX 216

.-.~. -.. _ -. -

_=

i 1

STAAD SPACE ATTACHMENT- ^

SHEET 3 Of 9

-- PAGE NO.

2 i

ID: Toledo Edison

[

42. 8 TO 10'FY

.225 L

l CALC.N0.

c -c 5 5-too.0 2-o t2 f

43. 11 FX

.325 j

44, 11 FY

.338

45. 12 FX

.432 4

~ ~ ~ ~

l

46. 12 FY

.45

47. LOAD 2
48. SELF X.96
49. SELF Y -1.0
50. JOINT LOAD i
51. 8 TO 10 FX.216 1

l

52. 8 TO 10 FY

.225

{

1

53. 11 FX.325 i

s

54. 11 FY

.338

55. 12 FX.432 j
56. 12 FY

.45 l

57. PERFORM ANALYSIS e

i PROBLEM STATISTICS l

a' NUMBER OF JOINTS / MEMBER + ELEMENTS / SUPPORTS =

12/

11/

2 i

ORIGINAL / FINAL BAND-WIDTM =

7/

3 I

TOTAL PRIMARY LOAD CASES

=

2, TOTAL DEGREES OF FREEDOM =

65 i

SIZE OF STIFFNESS MATRIX =

1560 DOUBLE PREC. WORDS REQRD/ AVAIL. DISK SPACE =

12.04/

156.5 MB, EKMEM = 12.90 MB

)

++ PROCESSING ELEMENT STIFFNESS MATRIX.

9:51:32 l

2

++ PROCESSING GLOBAL STIFFNESS MATRIX.

9:51:32 j

++ PROCESSING TRIANGULAR FACTORIZATION.

9:51:32

[

i 00$ WARNING - IMPROPER LOAD WILL CAUSE INSTABILITY AT JOINT 12 i

4 j

DIRECTION = MY PROBABLE CAUSE MODELING. PROBLEM 0.455E-12

++ CALCULATING JOINT DISPLACEMENTS.

9:51:32 l

f

++ CALCULATING MEMBER FORCES.

9:51:32 l

j 1

l

58. PRINT MEMBER FORCES i

1 I

k i

I

(

J d

4 t

0 J

f

STAAD SPACE

.IIACHMENT A

SHEET H OF T

-- PAGE NO.

3 l

C. NO.

C-CSI-f oo 0 3 -o G MEMBER'END FORCES STRUCTURE TYPE.= SPno" ALL UNITS ARE -- KIPS INCH i

MEMB LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 1

1 1

1.55

-0.77 0.00 0.00 0.00 0.00 2

-1.54 0.76 0.00 0.00 0.00

-16.78 2

1 1.55 0.54 0.00 0.00 0.00 0.00 2

-1.54

-0.53 0.00 0.00 0.00 11.70 a

2 1

2 1.31

-0.54 0.00 0.00 0.00 21.35 3

-1.30 0.53 0.00, C.00 0.00

-29.05 2

2 1.31 0.30 0.00 0.00 0.00

-7.14 l

3

-1.30

-0.30 0.00 0.00 0.00 11.49 3

1 3

1.07

-0.31 0.00 0.00 0.00 24.49 4

-1.06 0.30 0.00 0.00 0.00

-29.75 2

3 1.07 0.07 0.00 0.00 0.00

-16.05 4

-1.06

-0.06 0.00 0.00 0.00 17.27 4

1 4

0.82

-0.07 0.00 0.00 0.00 34.31 5

-0.82 0.07 0.00 0.00 0.00

-34.92 l

2 4

0.82

-0.16 0.00 0.00 0.00

-12.71 5

-0.82 0.16 0.00 0.00 0.00 11.35 5

1 5

0.48 0.26 0.00 0.00 0.00 28.10 6

-0.47

-0.27 0.00 0.00 0.00

-24.38 2

5 0.48

-0.49 0.00 0.00 0.00

-18.18 6

-0.47 0.50 0.00 0.00 0.00 11.23 6

1 6

0.01 0.71 0.00 0.00 0.00 15.32 7

0.00

-0.72 0.00 0.00 0.00 0.00 2

6 0.01

-0.94 0.00 0.00 0.00

-20.29 7

0.00 0.95 0.00 0.00 0.00 0.00 7

1 8

-0.22

-0.23 0.00 0.00 0.00 0.00 2

0.22 0.23 0.00-0.00 0.00

-4.56 2

8 0.22

-0.22 0.00 0.00 0.00 0.00 2

-0.22 0.23 0.00 0.00 0.00

-4.56 8

1 9

-0.22

-0.22 0.00 0.00 0.00 0.00 4

0.22 0.23 0.00 0.00 0.00

-4.56 2

9 0.22

-0.23 0.00 0.00 0.00 0.00 4

-0.22 0.23 0.00 0.00 0.00

-4.56 9

1 3

0.22 0.23 0.00 0.00 0.00 4.56 10

-0.22

-0.22 0.00 0.00 0.00 0.00 2

3

-0.22 0.23 0.00 0.00 0.00 4.56 10 0.22

-0.22 0.00 0.00 0.00 0.00

..e, l

1 A

SHEET C OL9-'

'll: a ACHMENT STAAD SPACE

-- PAGE NO.

4

(.i '.C. N0.

c-us-tod,o3-o o _ _

ID: Toledo Edison 4

MEMBER END FORCES STRUCTURE TYPE - 6? ACE i

ALL UNITS ARE -- KIPS INCH MEMD LOAD JT AXIAL SHEAR-Y SHEAR-Z TOPSION MOM-Y MOM-Z 10 1

5 0.33 0.34 0.00 0.00 0.00 6.82 11

-0.33

-0.34 0.00 0.00 0.00 0.00 2

5

-0.33 0.34 0.00 0.00 0.00 6.82 11 0.32

-0.34 0.00 0.00 0.00 0.00 11 1

6 0.44 0.46 0.00 0.00 0.00 9.06 12

-0.43

-0.45 0.00 0.00 0.00 0.00 2

6

-0.44 0.46 0.00 0.00 0.00 9.06 12 0.43

-0.45 0.00 0.00 0.00 0.00

    • 0***********

END OF LATEST ANALYSIS RESULT **************

59. PRINT SUPPORT REACTIONS 1

I I

i l

l

I

~ !ACHMENT A

SHEET 0 0F 9 i

STAAD SPACE

-- PAGE NO.

5 C. NO.

c-CSS- 00 0-ot3 ID: Toledo 'dison E

i SUPPORT REACTIONS -UNIT KIPS INCH 61huvivaE lire - APACE JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z l'

1 0.77 1.55 0.00 O.00 0.00 0.00 2

-0.54 1.55 0.00 0.00 0.00 0.00 7

1 0.72 0.00 0.00 0.00 0.00 0.00 2

-0.95 0.00 0.00 0.00 0.00 0.00 l

                            • END OF LATEST ANALYSIS RESULT **************

]

60. PRINT MEMBER STRESSES

)

4 i

1 i

f STAAD SPACE

-- PAGE NO.

6 ATTACHMENT - A SHEET 7 0F A ID: T led Edison

~

MEMBER STRESSES ALL UNITS ARE KIPS /SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 1

1

.0 0.8 C 0.0 0.0 0.8 0.4 0.0 1.00 0.8 C 0.0 10.1 10.9 0.4 00 2

.0 0.8 C 0.0 0.0 0.8 0.3 0.0

' :L. 0 0 0.8 C 0.0 7.0 7.8 0.3 0.0 j

j 2

1

.0 0.7 C

0. Ct 12.8 13.5 0.3 0.0 1.00 0.7 C 0.0 17.4 18.1 0.3 0.0 2

.0 0.7 C 0.0 4.3 5.0 0.2 0.0 1.00 0.7 C 0.0 6.9 7.6 0.2 0.0 l

3 1

.0 0.5 C 0.0 14.7 15.2 0.2 0.0 l

1.00 0.5 C 0.0 17.9 18.4 0.2 0.0 2

.0 0.5 C 0.0 9.6 10.2 0.0 0.0 1.00 0.5 C 0.0 10.4 10.9 0.0 0.0 4

1

.0 0.4 C 0.0 20.6 21.0 0.0 0.0 l

1.00 0.4 C 0.0 21.0 21.4 0.0 0.0 2

.0 0.4 C 0.0 7.6 8.0 0.1 0.0 1.00 0.4 C 0.0 6.8 7.2 0.1 0.0 f

5 1

.0 0.2 C 0.0 16.9 17.1 0.1 0.0 1.00 0.2 C 0.0 14.6 14.9 0.1 0.0 2

.0 0.2 C 0.0 10.9 11.2 0.3 0.0 1.00 0.2 C 0.0 6.7 7.0 0.3 0.0 6

1

.0 0.0 C 0.0 9.2 9.2 0.4 0.0 1.00 0.0 C 0.0 0.0 0.0 0.4 0.0 2

.0 0.0 C 0.0 12.2 12.2 0.5 0.0 1.00 0.0 C 0.0 0.0 0.0 0.5 0.0 7

1

.0 0.2 T 0.0 0' 0 0.2 0.2 0.0 1.00 0.2 T 0.0 8.0 8.2 0.2 0.0 2

.0 0.2 C 0.0 0.0 0.2 0.2 0.0 1.00 0.2 C 0.0 8.0 8.2 0.2 0.0 i

8 1

.0 0.2 T 0.0 0.0 0.2 0.2 0.0 1.00 0.2 T 0.0 8.0 8.2 0.2 0.0 2

.0 0.2 C 0.0 0.0 0.2 0.2 0.0 1.00 0.2 C 0.0 8.0

8. 2.

0.2 0.0 1

9 1

.0 0.2 C 0.0 8.0 8.2 0.2 0.0 1.00 0.2 C 0.0 0.0 0.2 0.2 0.0 2

.0 0.2 T 0.0 8.0 8.2 0.2 0.0 1.00 0.2 T 0.0 0.0 0.2 0.2 0.0 l

10 1

.0 0.3 C 0.0 11.9 12.2 0.3 0.0 1.00 0.3 C 0.0 0.0 0.3 0.3 0.0 2

.0 0.3 T 0.0 11.9 12.2 0.3 0.0 1.00 0.3 T 0.0 0.0 0.3 0.3 0.0 l

. _. _ _ _. ~ -. _ _ _ _... _. _.. _ _... _ _ _ _.. _ _ _ _ _..

1

~'

STAAD SPACE

-- PAGE NO.

7 ATTACHMENT-A SHEET 2 O' q ID: Toledo Edison i

CI L C. No.

C-C 5.5 -00.0 3_--09 MEMBER STRESSES f

4 j

ALL UNITS ARE KIPS /SQ INCH

' ~ ~ ~ ~

j MEMB-LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAP-Z

^

l 11 1

.0 0.4 C 0.0 15.8 16.2 0.4 0.0 i

i 1.00 0.4 C 0.0 0.0 0.4 0.4 0.0 l

2

.0 0.4 T 0.0 15.8 16.2 0.4 0.0 I

1.00 0.4 T 0.0 0.0 0.4 0.4 0.0 J

9 l

l

  1. 00***********

END OF LATEST ANALYSIS RESULT **************

61. PRINT JOINT DISPLACEMENTS i

j i

4 k

e j

i 1

s a

1 l

4 1

l.

i-4 a

s k

i i

i 1

W ACHMENT-A SHEET _3_ b. 9 STAAD SPACE

-- PAGE NO.

8

,i Cl LC. N0.

C -C CHoo 03 -o 13. -

ID: Toledo Edison j

I JOINT DISPLACEMENT (INCH RAurans; ornvu2vns 1YPE = SPACE JOINT LOAD X-TRANS Y-TRANS Z-TRANS

.X-ROTAN Y-ROTAN Z-ROTAN 1

1 0.00000 0.00000 0.00000 0.00000 0.00000 0.00779 2

0.00000 0.00000 0.00000 0.00000 0.00000

-0.00420 2

1

-0.15983

-0.00060 0.00000 0.00000 0.00000 0.00622 2

0.08443

-0.00060 0.00000 0.00000 0.00000

-0.00311 3

1

-0.22865

-0.00093 0.00000 0.00000 0.00000 0.00312 2

0.12182

-0.00093 0.00000 0.00000 0.00000

-0.00196

~

4 1

-0.24904

-0.00126 0.00000 0.00000 0.00000

-0.00092 2

0.13471

-0.00126 0.00000 0.00000 0.00000 0.00052 5

1

-0.23067

-0.00139 0.00000 0.00000 0.00000

-0.00341 2

0.12655

-0.00139 0.00000 0.00000 0.00000 0.00139 6

1

-0.16054

-0.00150 0.00000 0.00000 0.00000

-0.00653 2

0.09395

-0.00150 0.00000 0.00000 0.00000 0.00313 7

1 0.00000

-0.00150 0.00000 0.00000 0.00000

-0.00793 2

0.00000

-0.00150 0.00000 0.00000 0.00000 0.00499 8

1

-0.15997

-0.14744 0.00000 0.00000 0.00000 0.00790 2

0.08457 0.03907 0.00000 0.00000 0.00000

-0.00142 9

1

-0.24917

-0.00544 0.00000 0.00000 0.00000 0.00077 2

0.13484

-0.03408 0.00000 0.00000 0.00000 0.00220 10 1

-0.22878 0.03889 0.00000 0.00000 0.00000 0.00143 2

0.12195

-0.06261 0.00000 0.00000 0.00000

-0.00364 11 1

-0.23088

-0.10330 0.00000 0.00000 0.00000

-0.00594 2

0.12676

-0.00733 0.00000 0.00000 0.00000

-0.00114 12 1

-0.16081

-0.17689 0.00000 0.00000 0.00000

-0.00989 2

0.09423 0.01644 0.00000 0.00000 0.00000

-0.00022 000***********

END OF LATEST ANALYSIS RESULT **************

62. FINISH
                              • END OF STAAD-III ***************
        • DATE: APR 20,1995 TIME =

9:51:35 ****

For questions on STAAD-III, contact:

Research Engineers, Inc at Ph: (714) 974-2500 Fax:

(714) 921-2543

. -. ~. _... _ _ _ _ _. ~.. -. _

(tm) 7.4 L IT-53 @.11 b

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Raceway ID Status Serv Layout Length Card Last Rev BLFA12 PSC Lvl Drawing No.

Eng Act Rev 11/22/88 L C 7. ' 6 b'

O' Rwy Code: T3 C 7 L E356 45 50 12:01 L4 P-l3

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'3M Rwy type: Tray SU-Sys:

SG: B SC:

Fac:

Revision:

g_4

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[

FCR/ MOD t DCN No Iso Dwg :

g g

xP-u Inct cab Pct filt Avail Space Overfill Wt/ unit

'M Design: 150 33.30 28.843 0.00 L11 - $

$ IM "

Const : 150 33.29 28.843 0.00 g_g g

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y Z. 7,4

{

l. L Q - 4 0

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i Included Cables BLCOA502A(1-L1T)C BLC0A503A(1-L1T)C BLC0A504A(1-L1T)C LYP-I k '" ~

BLCC*505A(1-L17)C BLCOA506A(1-L1T)C BLC0A507A(1-L1T)C g4 - 1 g,13

'? O

  • N BLC0A508A(1-LIT)C BLCOA509A(1-L1T)C BLC0A510A(1-LIT)C BLCOA511A(1-L1T)C BLCOA512A(1-L1T)C BLC0A513A(1-L1T)C D. 9 [ hi.

t BLC0A514A(1-LIT)C BLCCA515A(1-LIT)C BLC0A516A(1-L1T)C C % 24" T M Y W O C. E gA BLCCt.517A(1-LIT)C BLCOA318A(1-LIT)C BLC0A522A(1-L17)C BLC0A523A(1-L1T)C BLC0A324A(1-LIT)C BLC0A525A(1-L1T)C q g, 3 4 44jt f gf g g L,4 7,g y BLCOA526A(1-L17)C RLCOA527A(1-LIT)C BLCOA535B(1-LIT)C BLC0A550A(1-LIT)C BLC0A603A(1-L1T)C BLC0A604A(1-L1T)C l

55 % Dr#,

BLCC*.605A(1-L1T)C BLCOA613A(1-L1T)C BLC0A619A(1-L17)C BLC0A624A(1-L1T)C BLC0A627A(1-L17)C BLC0A628A(1-LIT)C BLCOA637A(1-LIT)C BLCOA638A(1-L17)C BLC0A639A(1-L1T)C f

BLC0A640A(1-L1T)C BLCOB504A(1-TJ2)C BLCOB505A(1-TJ2)C Q

BLCOB506A(1-TJ2)C BLCOB507A(1-TJ2)C BLCOB508A(1 TJ2)C A

y l

b 1

BLCOB510A(1-TJ2)C BLCOBS11A(1-TJ2)C BLCOB512A(1-TJ2)C

  • E 2

CLCOB513A(1 TJ2)C BLCOB514A(1-TJ2)C BLCOB533A(1-TJ2)C P E BLCC0535A(1-TJ3)C BLCOB542C(1-TJ1)C BLCOB542D(1-TJ1)C I

BLCOB542E(1 TJ1)C BLCOB542F(1-TJ1)C BLCOB543D(1-TJ1)C q

g BLCOB546A(1-TJ1)C BLCOE538A(1-L4P)C BLCCF520A(1-L4P)C BLC0J503A(1 i1P)C BLC0J505A(1-L4P)C BLC0J508A(1-L1P)C.

U g

BLC0Y101A(1-LC2)C BLC0Y102A(1-LC2)C BLC0Y103A(1-LC2)C Y

l BLC0Y104A(1-LC2)C BLC0Y124A(1-LC4)C BLC0Y126A(1-LC4)C BLC0Y142A(1-LC2)C BLC0Y143A(1-LC2)C BLC0Y144A(1-LC2)C y

f BLC0Y145A(1 LC2)C BLCV1 B(1 L1T)C BLCV1 C(1-L1P)C O

.c

{

y f

BLCV2 B(1 L17)C BLCV2 C(1-L1P)C BLCV3 B(1-L1T)C BLCV3 C(1-L1P)C BLCV4 B(1-L1T)C BLCV4 C(1-L1P)C h

9 h(

W BLDESTf.01(1-L58)C BLMY4532C(1-L1P)C BLICS183D(1-L1P)C BLICS183M(1-L1P)C BLISV1 B(1-L17)C BLISV2 B(1-LIT)C 61

-a

'1 BLISV3 B(1-L1T)C BLISV4 B(1-LIT)C BLIV1 B(1 LIT)C og EtlVI D(1-L1P)C BLIV2 8(1 L1t)C BLIV2 D(1-L1P)C l

l

Bllv3 8(1 L17)C SLIV4 B(1-L1T)C SLL3401A(1-L58)C 8LL34018(1-L58)C BLME510 A(1-LXP)C BLME512 A(1-L4P)C BLME513 A(1-LXP)C BLME514 A(1 L4P)C BLME518 A(1-L&P)C BLME521 A(1-L&P)C SLME522 A(1-L1P)C BLME523 A(1-L1P)C i

' 8LME525 A(1 L1P)C 8LME548 A(1-L1P)C BLME548 C(1-L1P)C BLME548 D(1-L1P)C BLME550 A(1-L&P)C BLME551 A(1-L4P)C BLME569 A(1-L4P)C BLME576 A(1-LXP)C SLME640 A(1-L1T)C BLME641 A(1-L1P)C BLN41121(1-L21)C' BLNN1122(1-L21)C 8LN41123(1-L21)C 8LN4113E(1-L20)C BLNul13G(1-L20)C SLNN113N(1-L20)C 8LN41141(1-L20)C BLNN1143(1-L20)C BLN11144(1-L20)C 8LNN1145(1-L20)C BLNN1146(1-L20)C 8LN41194F(1-L1P)C 8LSPARE21(1-L1P)C BLSPARE25(1-L1P)C BLSPAREA1(1-L10)C BLSPAREA2(1-L10)C BLSPAREA3(1-L10)C SLSP"REf.4(1-L10)C BLSPAREE4(1-LTP)C BLSPAREG5(1-L58)C SLT02 C(1-L4P)C BLT09 A(1-L1P)C BLT09 B(1-L4P)C 8LT09 C(1-L1P)C SLT09 D(1-L1P)C BLT09 E(1-L1P)C BLT09 F(1-L1P)C BLT09 G(1 L1P)C BLT09 1(1-L1P)C.

BLT09 J(1-L1P)C BLT10 A(1-L1P)C BLT10 B(1-L1T)C BLT10 C(1-L1P)C BLT10 J(1-LIT)C BLT11 A(1-L1T)C t

BLT11 8(1 L1P)C 8LY11 C(1-L1P)C CLNF5878(1-L4P)C Recency Links..: 27079A 47180A 47181A BLP77A BLWD11 T-BLPA11/8LPA21 T BLPA13/BLWD11 Wrap / Zone /Lgth.: N/422A/0

    • END OF REPORT -- NORMAL TERMINATION **

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Cable ACSPARC0100 cannot be routed through Recewey ACPG52'

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~~

GA*(e) DETECTED DURING ROUTING CJ CABLE ACSPARE0100 BETWEEN:

"FROM" equipment (MA01) and first recewey (ACPG52*)

Lett Racewey (ACPG52*) and "To" e gipment (C57618)

Included cables for Racewey ACPG52*

CABLE ID DWG NO ACSPIRE010D E488 (t-MD ' IT@.34%r

=- 5.to"/rz Included cables for Raceway ACPG52*

[f - Ec 1) ? IO @.IL

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3. 2 O r

END LIST 2.53 (I'CIO) 15

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RACEWAY INOUIRY REPORT o-cos) :

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Davis-Besse Nucteer Power Station (1-C.2 O) ".

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Receway ID Status Serv Layout Length Card Lost Rev 1

ACPG51 PSC Lvl Drawing No.

Eng Act Rev 11/22/88 h - C2.2.] ;

I h,2.2.

O, 7 2.

l Rwy Code: T3 C 7 C E356 15 14 12:01 b

/*

W C ! ' (2O)

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~~

Rwy type: Trey SU-Sys:

SG: A SC:

Fac:

Revision:

L

,g h

FCR/ MOD :

DCN No :

Iso Dwg :

Inct cab Pet filt Avell Space Overfill Wt/ unit u

(,a g _ Lj p ')

( @,d

, ll Design: 95 31.88 30.375 6.70 Q

r const : 95 31.88 30.375 6.70 Ci-L4e) :

2 G,zo

=.sc included Cables Act::AM A(1-C10)C '

AC1PAM A(1-C10)C '

AC1PNAM A(1-C10)C'

~~

I) -

Ik

' If

~~

ACAACC2 C(1-C12)C '

ACAACC2 M(1*C10)C -

ACAC2031A(1-C01)C -

22. 9 $'[l:p ACAC2032A(1-Cf"C '

ACAC205 B(1'-C12)C -

ACAC205 C(1-C01)C -

ACAC206 B(1-C.)C '

ACAC206 C(1-C13)C '

ACAC208 8(1-C01)C -

ACAC208 C(1-C13)C '

ACAC211 G(1-C12)C '

ACAC211 M(1-C01)C -

g g

y,g dg ACAC211 J(1-C01)C -

ACC02172A(1-L4P)C /

ACC02176B(1-LSTjC '

ACC0Z188a(1-L4P)C '

ACD1AM A(1-C01)C ACD1AM 8(1-C01)C -

og t

j,34-g ACD1NVM A(1-C10)C '

ACD1PVM A(1-C10)C -

ACD1VM A(1-C10)C '

Q ACDAP22A(1-807)C /

ACMA01 M;1-C13)C -

Acta 03 M(1-C13)C '

sb-5 h.

ACHA0501C(1-C11)C /

ACHA05010(1-C11)C '

ACMA0501E(1-C10)C '

+

N ACHA10028(1 C10)Ce ACMAAC A(1-C12)C '

ACMAAC B(1-C01)C '

ACMAAE2 G(1 C01)C /

ACMAAE2 M(1-C12)C '

ACMAAE2 L(1-C01)C /

53 l

ACMAAE3 G(1-C01)C /

ACMAAE3 M(1-C12)C '

ACMAAE3 L(1 C01)C' ACMAAE4 D(1-C12)C /

ACMAAE4 F(1-C01)C '

ACHAAE4 L(1-C01)C e y

ACMx01A J(1-C10)C/

ACM).01A M(1 C10)C '

ACMx02A G(1-C13)C /

i 5

ACMX11A D(1-C10)C e ACMX110 E(1-C10)C -

ACL1526 A(1-C20)C '

ACPSRC22C(1-C23)C /

ACPSRC22G(1-C23)C '

ACPSRC23C(1-C23)C '

ACSPARE43(1-C10)C e ACSPARE45(1-C10)C '

ACSPARE4' Sit-807)C '

ACSPARE64(1 807)C '

ACSPARE6A(1-C23)C '

ACSPARE8A(1 L1P)C '

ACSPACEAM(1-C13)C '

ACT01v(1 CS3)C ACVSP7A1G(1-C11)C /

ACVSP7ASE(1-C11)C -

ACVSP781G(1 C11)C '

ACVSP7BSE(1-C22)C '

ACY1vM A(1-C10)C /

ACY3VM A(1-C10)C /

ACY45115A(1-825)C '

ACTAR12 A(1-807)C '

ACTARVM A(1-C10)C -

ACTAU14 B(1-C10)C '

ACYAU14 C(1-C10)C -

ACYAU28 A(1 807)C -

ACYAU32 A(1-807)C -

ACYAU43 A(1-807)C -

ACTAU45 A(1-807)C e ACYAU47 A(1-807)C '

ACYAU40 A(1 807)C -

ACYAuvM A(1-C10)C '

CCAN3J014(1-ANN)C -

CCAN3M015(1-ANN)C -

CCAN3M016(1-ANN)C -

CCAN3VL11(1-AM)C -

CCAN3VL12(1-ANN)C '

CCA43VL13(1-ANN)C e CCAN4XX19(1-ANN)C-CCCNSF022(1-ANN)C '

CCAM5F023(1-ANN)C' CCAMSF024(1-ANN)C-CCAN5cP25(1-ANN)C '

CCAN50P26(1-ANN)C' CCAN5T017(1-ANN)C '

CCT5T018(1-ANN)Ce CCAN60E27(1-ANN)C -

RCtetoy liras..: ACPG50 TRAY ACPG50 TRAY ACPG52 Wrap / Zone /Lgth.: N/422A/0 O* END OF REPORT -- NORMAL TERMINATION **

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Cable ACSPARE010D cemet be routed through Receway ACPG52' because the Recewey la Sep Group incompatiblo

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,j 04-16-95 Setreute(tm) 7.4 RACEWAY INQUIRY REPOR7 I

d i

S @,% glPT Davis-Besse Nuclear Power Station 5.\\o lpr O - M cS)

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R2cewey ID Status Serv Layout Length Card Last Rev

()_6(f g Q,@ gg =

f. CPG 52 P$C Lvt Drawing No.

Eng Act Rev 04/16/95 b-DLh f @ 4b C.b Rwy Codes T3 C 7 C E356 43 43 23:01 Rwy Type: Tray SU-Sys: SG: A SC: Fac: Revision: FCR/ MOD : DCN No : Iso Dwg : y j 2,(c4 P $ Inct cab Pct fitt. Avall Space Overfilt Wt/tmit ({ -Clo] 7,qQ,}{ Z I D: sign: 95 31.74 30.526 6.38 b ~b I h Yh M const : 95 31.74 30.526 6.38 2*00 Q-Cid 7 @ *90 P Included Cables I Act:AM A(1-C10)C ' AC1PAM A(1-C10)C - AC1PNAM A(1-C10)C - h-C \\ b ) ] ,49 p ACAACC2 C(1 C12)C / ACAACC2 M(1-C10)C ' ACAC2031A(1-C01)C - ( I'C2-0) {@ Ot ,Og l v. c ACAC2032A(1-C01)C - ACAC205 s(1-C12)C ' ACAC205 C(1-C01)C - ACAC206 8(1 C01)C - ACAC206 C(1-C13)C ' ACAC208 B(1-C01)C - {\\-C2 Q C,Q ? g ACAC208 C(1 C13)C - ACAC211 G(1-C12)C - ACAC211 HC1-C01)C - O T ACAC211 J(1-C01)C - ACA41106A(1-LP1)C / ACC0Z172A(1-L4P)C ' bbD) 4 h '2 b ACC0Z176B(1 LS1)C. '" ACC0Z188A(1-L4P)C ' ACD1AM A(1-C01)C - - '4 ACD1AM 8(1-C01)C - ACD1NVM A(1-C10)C r ACD1PVM A(1-C10)C - (l-C3h } o ACD1VM A(1 C10)C - ACDAP22A(1-807)C e ACHA01 M(1-C13)C - ACHA03 M(1 C13)C ' ACHA0501C(1-C11)C ' ACHA0501D(1 C11)C ' I_ g *gg _ *gg'

I%

4 { } _ Q p) y Q 36 ACHA0501E(1-C10)C ' ACHA1002B(1-C10)C / ACHAAC A(1-C12)C ' ACHAAC B(1-C01)C / ACHAAE2 G(1-C01)C ' ACHAAE2 H(1-C12)C - ((-(_fI) { ,gl 0 ACHAAE2 L(1-C01)Cf ACHAAE3 G(1-C01)C - ACHAAE3 M(1-C12)Cf ACHAAE3 L(1-C01)C ' ACHAAE4 D(1 C12)C ' ACHAAE4 F(1-C01)C ' i (l-Ol) l Q.Ik ACHAAE4 L(1 C01)C/ ACHX01A JC1-C10)C r ACMX01A M(1-C10)C - e -~ ~~~~~ ACHXO2A G(1-C13)C - ACMX02A Jt1 C10)C / ACMXO2A M(1-C10)C ' ~ i ACMX11A A(1-C13)C / ACMX11A D(1-C10)C ' ACMX11A E(1-C10)C e g* ACL1526 A(1-C20)C ' ACPSRC22C(1-C23)C ' ACPSRC22G(1-C23)C - ACPSIC23C(1 C23)C ' ACSPARE43(1-C10)C ' % % SPARE 45(1 ]-C10) f Q b.5 { g" g ACSPAIE49(1-B07)C ' ACSPARE6A(1 C23)C / ACSPARESA(1-L1P)C ACVSPTA1G(1-C11)C - ACVSP7ASE(1-C11)C ' ACVSP7B1G(1-C11)C - g [l tt[ ACS7ARE9U(1 C10)C - ACSPAREAM(1-C13)C " ACT01V(1-CS3)C ACVSP7BSE(1 C22)C ' ACT1VM A(1-C10)C / ACY3VM A(1-C10)C ' 30.(g9gb y& y i,CY45115A(1-825)C ' ACYARVM A(1-C10)C ' ACTAU14 B(1-C10)C - ACYAU14 C(1 C10)C - ACYAU28 A(1-807)C ' ACYAU32 A(1-807)C - ACTAU43 A(1 807)C ' ACYAU45 A(1-807)C ' ACYAU47 A(1 807)C ' O ACYAU49 A(1-837)C / ACYAUvM A(1-C10)C / CCAN3J014(1-ANN)C / 9 CCA23M015(1-ANN)C ' CCAN3M016(1-ANN)C / CCAN3VL11(1 ANN)C ' -D -mm= --w- --P s a-- + -n a t-s--.m T-w-m m m m

m.m .m._ m_. ... _......... _.. ~.. _-- m ...m_.... -...u.... b CCAN5F022(1 ANN)C e CCAN5F023(1 ANN)C - CCAWSF024(1-ANN)C e CCAN5cP25(1-A44)C - CCAN50P26(1-ANN)C - CCAN57017(1-ANN)C - g CCAN60E27(1-ANN)C - CCANST018(1-ANN)C f i Recewey Lir*s..: 5712A1 57742A 579941 CCP21C CCP22A T-ACPG31/ACPG32 i TRAY ACPG51 Notes..........t RRRR 1 i G END OF REPORT ** NORMAL TERMINATION ** s k I t P i t O k M r H O O 2 Z P Krn 2 H i p' i O w D1 I48 i d o t h en Q Z g rrt I o Q O P on } N I 7 Ra! P u eg: O9 _D I l

_mm.m 3(_,fbbN T. t P -> 2 1 ,23 g,gg . vs Satrouts(tm) 7.4 gp , [] '. W RACEWAY IN0UIRY REPORT C (1 N l3 5,70 49 4go C__13 ar lo 8 Davis Besse Nuclear Power Station c <S~l 5 13, _ _ ~ c_ ; q. e i

c. 2.H 2.

38 '7 C 3 Raceway 10 Status Serv Layout length Card Last Rev r- ~ 9 $ v BCPC16 PSC Lyl Drawing No. Eng Act Rev 11/22/88 2 I Rwy code: T3 C 7 C E356 20 22 12:01 L { D'> 'D O K is*f 6 Rwy Type: Tray SU-Sys: SG: 8 SC: Fac: Revision: I m .Z4 { FCR/ MOD : DCN No : Iso Dwg : gg g lg ,ld q inct cab Pct fill Avail Space Overfill Wt/ unit ,h% h 6Q] q f -lb g Design: 155 49.34 11.499 0.64 }7 const : 147 47.80 13.176 0.48 g

c. z.o -> ?_o

.ui 3 LXP94 a a.Y y p a_,. inclueea Caeles _..s... :. = 7 .. -....... u, ;

,.,,. m.,,.

ggg } ,G ,t2 s, q m 1 7 =a.,,.._,- t o u

===== -v n -.--= a e :- 3'c v> J;g====mme;9:f_ L 7 32_a e = . :b==.:: -u " C 6 O l1 33' u = 0 e -~

-u-

=1: M apr.ad cgfg[ ,go } -~ g, =: a &a 7 k=j-3 -,4r me- =- = aua uur = m=e =- a = =ncjac- { gg 9 l , li 2~ i ef nicc-c=::

== 33 a=4="j** (_ O l-71 3 3' l q xuo =e f x _=. g= o-m y rem

==j c-ma e 7:= g;2,c-- j r gy .scw3,v $q a= C . =pcG7 ,ce r og, vs.n - u,3 =r u see m m q-v r~c

==q= e -v a7,e

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==L.\\ -u;a .===1. \\e n. J= L.,a.l..,= c Q;,e (_, 2. '? - '> l i i ur ._.,m - - (:,.1,,.,,s.- = 2, . m,lu_., g q9 g5-@q: L ,.~ a 3..,.. 7 -e m % rs nose-

== ew =.55 0 -,,. -- - ~ ^ 7;^ .m,ut u u-cs6 .i wir G b SNMM b* d' ^ e

a,u x -

- g g. gp g5 3= p y,,,39' ' u - 6. 16 - -8&g m..TR ~ ' " ~ "7 '? iciAn a -00 6 iciiwata-ucu.ru-

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m. _ .-..m_ .._m__ -,..m _ _ _... _ _ ~ __.... _m JG44-G309e-BetENemt4-9Mtt> ^^ ;;;- - : J. ^. - * - CM,. ,r ....,n,. __,,,,,._,,,u_,,. w. 7-40sesM48 eft-999te- .;..si-ci esmr unti-u W,; - M C

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'._*_'_#= ^^tye W g ggg3.gsejt . - *=aattrit eers,-, T _ - _ - _, _.. _,... /.opu. .,.,, 4. _.,.,.i, _, o 3.,_--, ..,. ~_ 1_w__ d_ io__tt.nr =.*.a**=.\\=>* d_e .. 7, _ 7_ __ m - iansat _3raanTt 6cuiu___ .-w r _/ ACSa.,__i _ fi mm q is.f m i 6 v,w p7.s. my,w u, u viv wp/( 3 -L w)G - m.a , m. = - - -. -- ;. _ r. s.e< s_ w - accenen,._=.,. -.,, y,a s a. - - oJ(i-LTP7e-GA -vii-i"^,6 "'" ^" " '_4"!C war .,{.v M.? R.. A s-u W iir """"[" J^' t ' ' * * -_ -6C. a,}71;,",_r;70 meetnv.tarskeit1w f _ _1, ' _,=,,, are ,M, ,f,,,,,_(,,,C m.2.__... 1__ m, m.. I..~. I ../,,.d_.,..__.._,__ n o,. __. sur (1-cur 7 ir ~s. o-00'f i ^ ^Zic - "C? r'." T t-C'??C-N'?' B P682A(1- )E .I 6,uay mui d==- ' 207:0-Siinii-C2 qG l ^^ C^2?" "? ' ?"_ o.v395ntap .is nN'^' * - C? ?,h - 80 " ' ' C2 ' "- iser mc n(1-TXP7e* g 6f1-tvol u LC.,-G iGi g 7^6 .._ AE m i v.riu reen "."C"' * ' i e w-i CCSR."C 'O '?"10-Racewry Links..: 57142A BCPC15 BCPC17 BCTG20 BCWB11 Wrap / Zone /Lgth.: N/422A/0

    • END OF REPORT -- NORMAL TERMINATION **

f r b i r-C"l1 h i Cr p 2 1 ,O E rr-g I b I IO 06 u 't t. O O. r i O rn FT) .[ t W -a 3 c r-l t I 4

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R ( T 0 L P E C A L P r s s e 3 S s s s s 1 P 0 A D A T N !4 A S e s a 1 A : E L T T I S T 7 1 M 1 4. no 1 s i J d e 0c A 0 0 0 T E e A C 5 0 0 l D A 4 7 O 4 1 4 9 o P 1 1 t E S R Y U = T

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ATIACHMENT-o SHEET 2-O d t

PAGE NO. 1 '"4 C. NO. L-c 5 r-too.o3. oq ID: toledo edison t i S T A A D - III Revision 19.0a j' RESEARCH ENGINEERS, Inc. Proprietary Program of Data = APR 21, 1995 2 Time = 11: 7:40 4 USER ID: toledo edison

                                      • +******************************

] 3 1 j 1. STE%D SPACE 2. UNIT INCH KIPS 3. JOINT COORDINATES I 4. 1 0. O. O. 5. 2 0. 12. O. 6. 3 0. 28. O. 7. 4 0. 44. O. 8. 5 O. 60. O. i

9..6 0.

76. O. j

10. 7 0.

98. O.

11. 8 46.

O. O.

12. 9 46. 12.

O. 4-

13. 10 46. 28.

O. l i '

14. 11 46. 44.

D. l ~~

15. 12 46. 60.

O.

16. 13 46. 76.

O. i

17. 14 46. 98.

O. i

18. MEMBER INCIDENCES
19. 112 i

'20. 22 3 i.

21. 3 3 4 l
22. 4 4 5
23. 55 6
24. 6 67
25. 78 9 4

l

26. 8 9 10

{

27. 9 10 11

[

28. 10 11 12
29. 11 12 13 i
30. 12 13 14 l

31.-13 2 9

32. 14 3 10 l
33. 15 4 11
34. 16 5 12 4
35. 17 6 13
36. MEMBER PROPERTIES t<
37. 1 TO 12 PRI.9 AX 1.95 IX.1 IY 1.107 YD 4.875 IZ 4.602 ZD 1.625
38. 13 TO 17 PRIS AX 1.11 IX

.1 IY.478 YD 3.25 IZ 93 ZD 1.625 j

39. SUPPORTS i
40. 178 14 PINNED
41. CONSTANTS j

-42. E 29000. ALL i 1 l f f 3

l ( OTAAD SPACE ATIACHMENT SHEET 3 bi 9 -- PAGE NO. 2 ID: toledo edison [ 2 C -OS 'oo 63 -oG

43. DEN.000283 ALL CALC.N0.

44.-LOAD 1

45. SELF X.96 l
46..SELF Y -1.

( 4

47. MEMBER LOAD
48. 13 TO 17 CON GY

.45 23. I i '

49. 13 TO 17 CON GX.43 23.
50. PERFORM ANALYSIS PROBLEM STATISTICS NUMBER OF JOINTS / MEMBER + ELEMENTS / SUPPORTS =

14/ 17/ 4 l ORIGINAL / FINAL BAND-WIDTH = 7/ 4 TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 72 OIEE OF STIFFNESS MATRIX = 2944 DOUBLE PREC. WORDS REQUIRED DISK SPACE = 12.06 MB, TOTAL EXMEM = 6.75 MB ++ PROCESSING ELEMENT STIFFNESS MATRIX. 11 7:43 l ++ PROCESSING GLOBAL STIFFNESS MATRIX. 11: 7:43 ++ PROCESSING TRIANGULAR FACTORIZATION. 11: 7:43 ++ CALCULATING JOINT DISPLACEMENTS. 11: 7:44 ++ CALCULATING MEMBER FORCES. 11: 7:44 f

51. PRINT MEMBER FORCES i

t l i f

7 ' ulACHMENT C SHEET _3.. b i STAAD CPACE -- PAGE NO. 3 t' N O. c-c. ss-ro o.o 3 - 33 ID: toledo edison '~ MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- KIPS INCH HEMD LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 1 1 1 0.35 0.58 0.00 0.00 0.00 0.00 2 -0.35 -0.58 0.00 0.00 0.00 6.96 2 1 2 0.39 0.29 0.00 0.00 0.00 -3.22 3 -0.38 -0.28 0.00 0.00 0.00 7.78 3 1 3 0.32 0.06 0.00 0.00 0.00 -6.35 4 -0.32 -0.05 0.00 0.00 0.00 7.28 4 1 4 0.13 -0.17 0.00 0.00 0.00 -8.72 5 -0.13 0.18 0.00 0.00 0.00 5.95 5 1 5 -0.19 -0.42 0.00 0.00 0.00 -10.48 6 0.20 0.43 0.00 0.00 0.00 3.72 6 1 6 -0.65 -0.51 0.00 0.00 0.00 -11.30 7 0.66 0.52 0.00 0.00 0.00 0.00 7 1 8 0.98 0.79 0.00 0.00 0.00 0.00 9 -0.97 -0.78 0.00 0.00 0.00 9.40 8 1 9 0.47 0.62 0.00 0.00 0.00 -0.45 10 -0.46 -0.61 0.00 0.00 0.00 10.36 9 1 10 0.05 0.39 0.00 0.00 0.00 -3.71 11 -0.04 -0.38 0.00 0.00 0.00 9.88 10 1 11 -0.24 0.16 0.00 0.00 0.00 -6.09 12 0.25 -0.15 0.00 0.00 0.00 8.59 11 1 12 -0.40 -0.05 0.00 0.00 0.00 -7.90 13 0.41 0.06 0.00 0.00 0.00 7.02 12 1 13 -0.42 -0.42 0.00 0.00 0.00 -9.42 14 0.44 0.43 0.00 0.00 0.00 0.00 13 1 2 -0.29 -0.04 0.00 0.00 0.00 -3.74 9 -0.16 0.51 0.00 0.00 0.00 -8.95 14 1 3 -0.22 0.06 0.00 0.00 0.00 -1.43 10 -0.22 0.41 0.00 0.00 0.00 -6.65 15 1 4 -0.22 0.18 0.00 0.00 0.00 1.44 11 -0.22 0.28 0.00 0.00 0.00 -3.78 16 1 5 -0.24 0.32 0.00 0.00 0.00 4.53 12 -0.20 0.15 0.00 0.00 0.00 -0.69

SHEET ' 0F.S_ - ATTACHMENT c-5 STAAD SPACE -- PAGE NO. 4 "!1 C. NO. _C - CS S -lo o 03 -0 9 - ID: tol'd 'di8 " MEMBER END FORCES STRUCTURE TYPE = SPACE ALL UNITS ARE -- KIPS INCH MEMD LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 17 1 6 -0.08 0.45 0.00 0.00 0.00 7.58 13 -0.36 0.02 0.00 0.00 0.00 2.40 600*********** END OF LATEST ANALYSIS RESULT **************

52. PRINT SUPPORT REACTIONS 4

e i

1 m 4 ' ATTACHMENT - c-SHEET _L Of :i STAAD SPACE -- PAGE NO. 5 ' c NO. c-C SS-too. o3-o #3 ID: toledo edison i SUPPORT REACTIONS -UNIT KIPS INCH STRUCTURE TYPE = SPACE i JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z 1 1 -0.58 0.35 0.00 0.00 0.00 0.00 7 1 -0.52 0.66 0.00 0.00 0.00 0.00 8 1 -0.79 0.98 0.00 0.00 0.00 0.00 14 1 -0.43 0.44 0.00 0.00 0.00 0.00 1 END OF LATEST ANALYSIS RESULT **************

53. PRINT MEMBER STRESSES

STAAD SPACs -- PAGE NO. 6 MMCHMUE C-SHfH 7 0F f ID: toledo eaison CALC.NO. c-c 5 I-too os -oss MEMBER STRESSES ALL UNITS ARE KIPS /SQ INCH M'JMB LD SECT-AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z 1 1 .0 0.2 C 0.0 0.0 0.2 0.3 0.0 1.00 0.2 C 0.0 3.7 3.9 0.3 0.0 2 1 .0 0.2 C 0.0 1.7 1.9 0.1 0.0 l 1.00 0.2 C 0.0 4.1 4.3 0.1 0.0 3 1 .0 0.2 C 0.0 3.4 3.5 0.0 0.0 1.00 0.2 C 0.0 3.9 4.0 0.0 0.0 i 4 1 .0 0.1 C 0.0 4.6 4.7 0.1 0.0 1.00 0.1 C 0.0 3.2 3.2 0.1 0.0 5 1 .0 0.1 T 0.0 5.6 5.7 0.2 0.0 f 1.00 0.1 T 0.0 2.0 2.1 0.2 0.0 6 1 .0 0.3 T 0.0 6.0 6.3 0.3 0.0 1.00 0.3 T 0.0 0.0 0.3 0.3 0.0 } 7 1 .0 0.5 C 0.0 0.0 0.5 0.4 0.0 1.00 0.5 C 0.0 5.0 5.5 0.4 0.0 i l 8 1 .0 0.2 C 0.0 0.2 0.5 0.3 0.0 1 1.00 0.2 C 0.0 5.5 5.7 0.3 0.0 9 1 .0 0.0 C 0.0 2.0 2.0 0.2 0.0-l 1.00 0.0 C 0.0 5.2 5.3 0.2 0.0 l 10 1 .0 0.1 T 0.0 3.2 3.4 0.1 0.0 l 1.00 0.1 T 0.0 4.6 4.7 0.1 0.0 l 11-1 .0 0.2 T 0.0 4.2 4.4 0.0 0.0 l 1.00 0.2 T 0.0 3.7 3.9 0.0 0.0 12 1 .0 0.2 T 0.0 5.0 5.2 0.2 0.0 l 1.00 0.2 T 0.0 0.0 0.2 0.2 0.0 13 1 .0 0.3 T 0.0 6.5 6.8 0.0 0.0 j 1.00 0.1 T 0.0 15.6 15.8 0.5 0.0 i 14 1 .0 0.2 T 0.0 2.5 2.7 0.1 0.0 1.00 0.2 T 0.0 11.6 11.8 0.4 0.0 l f 15 1 .0 0.2 T 0.0 2.5 2.7 0.2 0.0 l 1.00 0.2 T 0.0 6.6 6.8 0.3 0.0 i 16 1 .0 0.2 T 0.9 7.9 8.1 0.3 0.0 1.00 0.2 T 0.0 l'2 1.4 0.1 0.0 17 1 .0 0.1 T 0.0 13.2 13.3 0.4 0.0 l 1.00 0.3 T 0.0 4.2 4.5 0.0 0.0 l h l l

. _. _. _ _ _ _ _. _ _ _ _ _ _ _ = - - CTAAD SPACE ATTACHMENT f. SHEET f 0F T ID ed edison .o 3 -oG MEMBER STRESSES ALL UNITS ARE KIPS /SQ INCH MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z o+e*********** END OF LATEST ANALYSIS RESULT ************** I

54. PRINT JOINT DISPLACEMENTS I

J l 3 2 i 4 i l

ADACHMENT c-SHEET 9 OfA STAAD SPACE E 0* c-tsS-to.o 3-i3 -- PAGE NO. 8 {ID: toledo edison 1 JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE 4 JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN 1 1 0.00000 0.00000 0.00000 '0.00000 0.00000 -0.00215 2 1 0.02458 -0.00007 0.00000 0.00000 0.00000 -0.00184 3 1 0.04945 -0.00018 0.00000 0.00000 0.00000 -0.00118 4 1 0.06190 -0.00027 0.00000 0.00000 0.00000 -0.00036 5 1 0.06017 -0.00031 0.00000 0.00000 0.00000 0.00052 6 1 0.04393 -0.00025 0.00000 0.00000 0.00000 0.00137 7 1 0.00000 0.00000 0.00000 0.00000 0.00000 0.00231 8 1 0.00000 0.00000 0.00000 0.00000 0.00000 -0.00220 9 1 0.02467 -0.00021 0.00000 0.00000 0.00000 -0.00177 2 10 1 0.04945 -0.00034 0.00000 0.00000 0.00000 -0.00112 11 1 0.06191 -0.00035 0.00000 0.00000 0.00000 -0.00031 12 1 0.06020 -0.00028 0.00000 0.00000 0.00000 0.00057 13 1 0.04373 -0.00017 0.00000 0.00000 0.00000 0.00147 14 1 0.00000 0.00000 0.00000 0.00000 0.00000 0.00225 660*********** END OF LATEST ANALYSIS RESULT ************** 1 2 l

55. FINISH
                              • END OF STAAD-III ***************

1

        • DATE= APR 21,1995 TIME = 11: 7:46 ****

i For questions on STAAD-III/ISDS, contact: RESEARCH ENGINEERS, Inc at Ph: (714) 974-2500 Fax: (714) 974-4771 1 4 E \\ I

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1 a.flACHMENT o SHEEL._2. 7 l Ci10. N0. C-CE-ioo o 3 -o \\3-PAGE NO. 1 ID: Toledo Edison l

                              • (Af********************A***********

S T A A D - III Revision 20.0b Proprietary Program of Research Engineers, Inc. Date= APR 20, 1995 Time = 7:27:25 l USER ID: Toledo Edison I i 1. STAAD SPACE 2. UNIT INCH KIPS 3. JOINT COORDINATES 4. 1 0. O. O. 5. 2 0. 22.5 O. 6. 3 0. 38.5 O. 7. 4 0. 79. O. 8. 5 0. 98. O. 9. 6 71. O. O.

10. 7 71. 22.5 0.
11. 8 71. 38.5 0.
12. 9 71. 79.

O.

13. 10 71. 98.

O.

14. MEMBER INCIDENCES
15. I 12
16. 2 2 3 i
17. 3 3 4
18. 4 4 5
19. 567
20. 678
21. 7 8 9 I
22. 8 9 10
23. 9 2 7
24. 10 38
25. 11 4 9
26. MEMBER PROPERTIES
27. 1 TO 8 PRIS AX 1.95 IX.1 IY 1.107 YD 4.875 IZ 4.602 ZD 1.625
28. 9 TO 11 PRIS AX 1.11 IX

.1 IY.478 YD 3.25 IZ.93 ZD 1.625

29. SUPPORTS
30. 1 5 6 10 PINNED
31. CONSTANTS
32. E 29000. ALL
33. DEN.000283 ALL
34. LOAD 1
35. SELF X.96
36. SELF Y -1.
37. HEMBER LOAD
38. 9 10 11 CON GY

.15 20.

39. 9 10 11 CON GX.144 20.
40. 10 11 CON GY

.275 50.

41. 10 11 CON GX.264 50.

l

ATTACHMENT D SHEET __3_ U 7 STAAD'DPACE -- PAGE NO. 2 ID: Toledo Edison

42. PERFORM ANALYSIS

" ' !f.. N O. M S S - Wo.o s - o! 3 l t PROBLEM STATISTICS i l NUMBER OF JOINTS / MEMBER + ELEMENTS / SUPPORTS = 10/ 11/ 4 ORIGINAL / FINAL BAND-WIDTH = 5/ 4 TOTAL PRIMARY LOAD CASES = 1, TOTAL DEGREES OF FREEDOM = 48 SIZE OF STIFFNESS MATRIX = 1152 DOUBLE PREC. WORDS REQRD/ AVAIL. DISK SPACE = 12.04/ 373.5 MB, EXMEM = 12.90 MB ++ PROCESSING ELEMENT STIFFNESS MATRIX. 7:27:30 ++ PROCESSING. GLOBAL STIFFNESS MATRIX. 7:27:30 ++ PROCESSING TRIANGULAR FACTORIZATION. 7:27:30 l ++ CALCULATING JOINT DISPLACEMENTS. 7:27:31 l ++ CALCULATING MEMBER FORCES. 7:27:32 i

43. PRINT MEMBER FORCES l

I 4 1

1 c i I nACHMENT D-SHEET _1 bi. 7 A CTAAD SPACE f -- PAGE NO. 3 r/!C.N0. c-tss-I 3 - c7J3 ID: Toledo Edison i MEMBER END FORCES STRUCTURE' TYPE f SPACE ~~~'~~ ALL UNITS ARE -- KIPS INCH MEMB LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z 1 1 1 0.23 0.26 0.00 0.00 0.00 0.00 2 -0.22 -0.24 0.00 0.00 0.00 5.64 i 2 1 2 0.15 0.01 0.00 0.00 0.00 -5.00 j 3 -0.14 0.00 0.00 0.00 0.00 5.14 j l 3 1 3 -0.03 -0.12 0.00 0.00 0.00 -7.18 4 0.05 0.14 0.00 0.00 0.00 1.87 4 1 4 -0.31 -0.37 0.00 0.00 0.00 -7.11 5 0.32 0.38 0.00 0.00 0.00 0.00 1 5 1 6 0.31 0.29 0.00 0.00 0.00 0.00 7 -0.30 -0.27 0.00' O.00 0.00 6.30 6 1 7 0.20 0.34 0.00 0.00 0.00 -3.26 8 -0.19 -0.33 0.00 0.00 0.00 8.64 7 1 8 -0.09 0.03 0.00 0.00 0.00 -4.29 9 0.11 -0.01 0.00 0.00 0.00 4.95 0 1 9 -0.30 -0.20 0.00 0.00 0.00 -3.82 10 0.31 0.21 0.00 0.00 0.00 0.00 9 1 2 -0.23 0.07 0.00 0.00 0.00 -0.64 7 0.07 0.11 0.00 0.00 0.00 -3.04 10 1 3 -0.12 0.17 0.00 0.00 0.00 2.03 8 -0.30 0.28 0.00 0.00 0.00 -4.35 11 1 4 -0.23 0.26 0.00 0.00 0.00 5.23 9 -0.20 0.19 0.00 0.00 0.00 -1.13 000*********** END OF LATEST ANALYSIS RESULT **************

44. PRINT SUPPORT REACTIONS

I D SHEET _E 't 7 l ATIACHMENT STAAD SPACE -- PAGE NO. 4 r p;), c -t S 5 - t 00,03 - O o ID: Toledo Edison SUPPORT REACTIONE -UNIT KIPS INCH STRUCTURE TYPE = SPACE JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM Z 1 1 -0.26 0.23 0.00 0.00 0.00 0.00 5 1 -0.38 0.32 0.00 0.00 0.00 0.00 6 1 -0.29 0.31 0.00 0.00 0.00 0.00 10 1 -0.21 0.31 0.00 0.00 0.00 0.00 i

                            • END OF LATEST ANALYSIS RESULT
          • r********
45. PRINT MEMBER STRESSES I

4 I

l ATTACHMENT D SHEET Co 0F__7_. l: STAAD SPACE -- PAGE NO. 5 ID: Toledo Edison 1 . " C. NO. L-CSS-'00.07-00 MEMBER STRESSES ALL UNITS ARE KIPS /SQ INCH ! MEMB LD SECT AXIAL BEND-Y BEND-Z COMBINED SHEAR-Y SHEAR-Z i 1 1 .0 0.1 C 0.0 0.0 0.1 0.1 0.0 4 1.00 0.1 C 0.0 3.0 3.1 0.1 0.0 2 1 .0 0.1 C O.0 2.7 2.7 0.0 0.0 1 1.00 0.1 C 0.0 2'7 2.8 'O.0 0.0 ] 3 1 .0 0.0 T 0.0 3.8 3.8 0.1 0.0 l 1.00 0.0 T 0.0 1.0 1.0 0.1 0.0 I 4 1 .0 0.2 T 0.0 3.8 3.9 0.2 0.0 a 1.00 0.2 T 0.0 0.0 0.2 0.2 0.0 } 5 1 .0 0.2 C 0.0 0.0 0.2 0.1 0.0 4 1.00 0.2 C 0.0 3.3 3.5 0.1 0.0 6 1 .0 0.1 C 0.0 1.7 1.8 0.2 0.0 1.00 0.1 C O.0 4.6 4.7 0.2 0.0 j i 7 1 .0 0.0 T 0.0 2.3 2.3 0.0 0.0 l 1.00 0.1 T 0.0 2.6 2.7 0.0 0.0 1 8 1 .0 0.2 T 0.0 2.0 2.2 0.1 0.0 l 1.00 0.2 T 0.0 0.0 0.2 0.1 0.0 l 9 1 .0 0.2 T 0.0 1.1 1.3 0.1 0.0 1.00 0.1 T 0.0 5.3 5.4 0.1 0.0 10 1 .0 0.1 T 0.0 3.6 3.7 0.2 0.0 i 1.00 0.3 T 0.0 7.6 7.9 0.3 0.0 11 1 .0 0.2 T 0.0 9.1 9.4 0.2 0.0 1.00 0.2 T 0.0 2.0 2.2 0.2 0.0 l i i

                            • END OF LATEST ANALYSIS RESULT **************
46. PRINT JOINT DISPLACEMENTS i

_ ~.. STAAD SPACE ATTACHMENT D SHEET._.10' 7 __ p3gg 3g, ID: Toledo Edison oc go, __.c d u -too.03-013 l JOINT DISPLACEMENT (INCH RADIANS) . STRUCTURE TYPE = SPACE d JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN 1 1 0.00000 0.00000 0.00000 0.00000 0.00000 -0.00151 2 l' O.03026- -0.00009 0.00000 0.00000 0.00000 -0.00103 3 1 0.04183 -0.00013 0.00000 0.00000 0.00000 -0.00042 l 4 1 0.02502 -0.00010 0.00000 0.00000 0.00000 0.00098 5 1 0.00000 0.00000 0.00000 0.00000 0.00000 0.00149 t 6 1 0.00000 0.00000 0.00000 0.00000 0.00000 -0.00154 7 1 0.03052 -0.00012 0.00000 0.00000 0.00000 -0.00100 8 1 0.04168 -0.00018 0.00000 0.00000 0.00000 -0.00029 9 1 0.02510 -0.00010 0.00000 0.00000 0.00000 0.00114 10 1 0.00000 0.00000 0.00000 0.00000 0.00000 0.00141

                            • END OF LATEST ANALYSIS RESULT **************

a +

47. FINISH
                              • END OF STAAD-III ***************
        • DATE= APR 20,1995 TIME:

7:27:37 **** 4 For questions on STAAD-III, contact: j Research Engineers, Inc at t Ph: (714) 974-2500 Fax: (714) 921-2543 I \\ -}}