ML20126C039
| ML20126C039 | |
| Person / Time | |
|---|---|
| Site: | Calvert Cliffs  |
| Issue date: | 03/18/1980 |
| From: | Lundvall A BALTIMORE GAS & ELECTRIC CO. |
| To: | Eisenhut D Office of Nuclear Reactor Regulation |
| References | |
| NUDOCS 8003250303 | |
| Download: ML20126C039 (49) | |
Text
BALTIMORE GAS AND ELECTRIC COMPANY P. o. B ox 14 7 5 D ALTI M O R C. M ARYL AN D 212O3 AnTHuH E. LunDvALL.dR.
l< arch 18,1980 vice rus.orm S U P pl.Y Office of iTuclear Peactor Fenulation U. S. Nuclear Her,ulatory Conniasion Wanhinrton, D. C.
20555 Attn:
Mr. D. G. Einenhut Actine, Director Division of Operating Beactorc Cubject:
Calvert Cliffs Nuclear Power Plant Unit No. 2, Docket I!o. 50-318 Westinrhoune lov Prassure ' Turbine Disc Innnectien
Reference:
TIRC letter dated 2/25/80 fro:a D. C.
Eisenhut to A. E. Lundvall, Jr., name nub.icct.
Gentlemen:
The referenced letter inforned us of 0.n increaned nrchtbility of crack fornation in the Jov pressure turbine diner of Wertinrhouse-surmlied turbinen.
Ve vere reauested to nunnly, nu cunnt to 10 U R c0.Sh (f), juntification for continued oteration of Cr_17ert Clif fr Unit Ja.
9, nending a full ultrasonic innrection of the LP rotor dices, incivii nc certain plant-nnecific information and reneric information.
In nahrecuent discuccions with NRC Staff, we were informed that our generic inforation l
cubnittal nay be deferred until March 2h,1980 and the rensining infor-nation until March 19, 1980.
Attnehnent 1 to thin letter providen the juctification for continued oneration of Calvert Cliffc Unit No. 2. contains our responses to the Site Specific General mwntionn found in Encionare 2 to it aferenced letter. The format for the recponcea in the cree as that for the quentienn.
The reimonse to Duestion I.D contains Westinrhocoe-
]
Pronrietary infornation. !.ccordinnly, the prourietary portion of that
~
response is presented separately in Attachment 3.
Attnelune r.t h (20 copics )
is the non-pronrietary version of Attachment 3.
Our reononsec to the Generic Ducatiens fcund in Enclosure 2 to the referenced letter vill be urovided by March 2h, 1o80 an discucced above.
At that tine ve vill also forward a cirned nfridavit executed by Pertinc-house Flectric Cornoration in cunnort of the followJ ne, requent for pronrictary treatment.
soosuo303
Mr. D. G. Eicenhut l' arch 18,1030 Pursuant to the nrovinionc ofalo CFR Part 2.790 it in recueated that the information contained in Attachment 3 to thin letter be treated as proprietary infort.ation and~be withheld from nublic disclocure.
BALTIMORE GAS AfiD ELECTRIC COMPAITY i,
3y. [
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,Jr
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A. E. Lundvall, Jr.
/
Vice President - Supply
/
STATE OF MARYLAfID:
TO WIT:
CITY OF BALTIMORE:
A. E. Lundvall, Jr. being duly avorn states that he is Vice President of the Baltimore Gac and Electric Company, a cornoration of the State of Maryland, that he executed the forecoinn Response for the nurnoces therein set forth, that the statements made in said Pennonce are true and correct to the best of hin knowledce, information and belief: and that he was authorized to execute the Response on behalf of naid cornoration.
WITI!ESS My Hand and Notarial Scal:
I
//
My Commission Expires:
/
! l Attachments (h)
]
cc:
J. A. Biddinon, Esquire G. P. Trovbridge, Esquire Ib. E. L. Conner, Jr. - MFC
m Pare 1 of 8' ATTACHMDIT 1 e
The analysis of turbine-renerated missiles during a destructive overspeed incident is detailed in Section 1h.8 of the FSAR, a copy of.which j
is' included in this At'tachment. Several assumptions; vere made concerning-missile characteristics. After careful consideration of the recent infor-nation from the turbine manufacturer concerning cracking, we have determined that the adecuacy of protection of vital areas from such missiles has not been comuromised'in any way. A summary of our determination follows.
I.
Missile Enercy 1.
From the Westinghouse " Report Covering the Effects of a Turbine Accelerating to Destructive Overspeed" it is shown that if the turbine were to accelerate to 189% of its norma 1' operating speed, destruction of disc #2 vill occur and not allow further acceleration.
2.
The assumption is then made that all discs burst at this 189%
of rated speed.
3.
Dise number 6 is postulated to have the highest exit energy of any missile which vill penetrate the turbine casing under the conditions assumed.
h.
The energies of the missile during this incident under the assumed conditions are:
6 a.
Prior to innact with easing: 17 0 x 10 ft-lb.
6 b.
Following penetration of the casing:
o.O x 10 ft-lb.
II.
Penetration of the Missile Into the Protective Barrier 1.
Lov Trajectory Missiles In the results outlined in table Ib.8.2 of the FSAR two cases are calculated and their effects shovn.
Se first, Case I, utilizes the postulated exit energy from the turbine and the second, Case II, uses the postulated energy of the fragment before its impact with the turbine casing and assumes no energy loss during the penetration of the easing.
It is clearly shown that even with these extremely conservative assumptions, the barrier is not penetrated.
2.
High Trajectory Missiles The same assumptions are made as in 1 above and the results are
.shown in table Ib.8.2 to indicate penetration of the barrier under
'the least conservative conditions.-
i Pace 2 of 8 Conclusions Using the.most conservative assumntions it is apparent that. the -
turbine fracments vill not 'venetrate the protective barrier durine the 189% oversneed failure. The current concern involves damage incurred during a 120% overspeed condition with attendant fragment ejection. The energy of these fragments vill clearly be significantly below that calculated for the 189% overspeedf condition and thus will be incapable of penetrating the protective barrier and vill' present no hazard to the protected vital areas.
j For the above reasons, postulated failure of a low pressure turbine disc as a result of disc or keyvay cracking does not reduce overall nuclear safety in'the plant and, thus, does not result in any increased
- risk to the public health and safety. Consequently, ve have concluded that continued unrestricted operation of Calvert Cliffs Unit No. 2 is justified until such time as a. ultrasonic insoection of the discs is performed.
i I
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I I
ATTACEMENT 1 Page 3 of 8 14.8 TURBINE-CENCRATOR OVERSPEED INCIDENT 14.8.1 CENERAL The purpose of this scetion is to evaluate the potential damage which would result from a structural failure or malfunction of the redundant control system resulting in missile like piecen 1 caving the turbino casing. The manufacturers of both units have conservatively designed the turbine-genera-tors to climinnte any stress concentration points which could give rise to crack propagation. Manufacturing and inspection techniques for turbine rotor and disc forgings make the possibility of an undetected flaw extremely remote. Nevertheless, both turbine-generator manufacturers have conducted tests to determine the ef fects of a turbine control system failure resulting in a turbine runaway. The consequences of thit occurrence and the protection afforded vital plant compartments and equipment areas are analyzed in this section.
14.8.2 TURBINE STEAM FLOW The turbines for Units No. I and 2 arc essentially the same. They are 1800 rpm, tuo stage reheat, tandem compound, six flow exhaust machines with a last row blade of 38 and 40 inches, respectively. The turbines are designed for 815 psia saturated steam inlet pressure and 2.0 inches Hg absolute exhaust pressure.
There are six stages of feedwater heaters.
Dry saturated steam from the two steam generators enters the high pressure turbine through four sets of stop-throttle and control valves. The steam expands in the high pressure turbine and then flows to the moisture separator reheat units.
After the moisture saparator reheat unit, the steam flows through either combined intermediate valves (Unit 1) or reheat stop and intercept valves (Unit 2), to the low pressure turbine where the steam expands and then exhausts to the condenser.
A bypass system is provided in order to allow excess steam generator energy to be bypassed into the condenser whenever the turbine cannot accept all of the generated steam, e.g., during startup or a sudden change in load.
Positive closing nonreturn valves are provided in all extraction lines, except those located in the condenser neck, to limit flow of stored energy (which could cause the turbine to,overspeed) f rom the heaters to the turbine on a turbine trip.
These valves are actuated by the Electro-Hydraulic Control Trip System.
14.8.3 TURBINE-GENERATOR GOVERNING DEVICES Both units have an Electro-Hydraulic Control System.
The Unit 1 turbine-generator (1) uses only electro-hydraulic control (EHC) fluid for all turbine tripping functions.
The Unit 2 turbine-generator uses the high pressu 2 bearing lubrication oil for its overspeed trip valve and EHC fluid for all other valves. Both units are equipped with the following steam valves:
1.
Stop-throttle valves 2.
Control valves 3.
Combined intermediate valves for Unit 1:
Reheat stop and intercept valves for Unit 2 14.8-1
l'..
.I Pagg h of 8 6
,a e
i
(". "
s The speed governor will start to close the control, combined intermediate
,(Unit No. 1) or reheat stop and intercept valves ( Un i t No. 2) at 101 percent of rated speed. At l'O percent of rated speed the mechanical overspeed trip will operate and close all s ecam valves. The backup overspeed trip system
.will actuate the master trip solenoid valve at 112 percent of rated speed.
Two independent speed signals _ are used permitting speed control with either one of the signals incapacitated.
14.8.4 METHOD OF ANALYSIS 10 14.8.4.1 General Despite the unlikelihood of a turbine runaway to destructive overspeed, the following conditions have been analyced to arrive at a conservative estimate of the missile penetration ability and to evaluate the potential damage which would result.
14.8.4.2 Unit No. 1 Analysis The General Electric Company, manufacturer of the Calvert Cliffs tinit I turbine-generator, determined their most severe turbine missile by assuming the instantaneous loss of load from a full load operating condition (2,3),
In addition, it was postu1.ated that the normal speed governing system and independent overspeed governing system fail to close the emergency stop valves. The turbine can then accelerate to from 150 to 170 percent of rated speed before severe generator damage due to thrown windings and probable retaining ring failure will decelerate the turbine. The last stage low pressure turbine wheel is postulated to fail when the turbine reaches 169 percent of rated speed, resulting in three 120 degree disc fragments. These fragments were determined to be the most dangerous of those which could be formed. High pressure turbine rotors are not expected to f ail at destructive overspeed, but even if failure did occur, the fragments should be retained by the heavy section, bolted high pressure shells.
Generator field and retaining ring parts are expected to be retained by the generator housing, which, by its construction, is an ideal energy absorber.
14.8.4.3 Unit No. 2 Analysis The Westinghouse Electric Corporation, manufacturer of the Celvez: Cliffs Unit 2 Turbine-Generator, determined their most serious turbine missile by assuming both the stop-throttle and control valves fail to closp {o11owing the opening of the main generator circuit breaker at full load Proven control system reliability and equipment redundancy makes such a turbine runaway highly improbable.
The criterion used is that the dise will fail when the average tangential stress equals the maximum specified yield strength of the disc material.
Dise No. 2 on the low pressure element is the most highly stressed dise with a calculated failure speed of 189 percent of rated speed.
Upon failure the dise fragments. will damage the turbine to the extent that additional over-speed will not be possible. For the purpose of the analysis which was performed, all other discs were assumed to fail at 189 percent of rated speed.
14.8-2 Rev. 5/31/7:2
e a
Pass 5 of 8 Due to the very large margin between the high pressure spindle bursting speed of 270 percent of rated speed and the maximum speed that the unit may
- run, i.e., 189 pe,rcent, the probability of spindle failure is practically zero. Therefore, no missiles from the high pressure section will develop during turbine runaway.
Generator field and retaining ring parts are ex-pected to be retained by the generator housing, which, by its construction, is an ideal energy absorber.
Calculations by Westinghouse considered fractures of discs into 90,120, and 180 degree segments. It was determined that the 90 degree segment posed the most severe missile threat.
14.8.4.4 Missile Characteristics The worst missile characteristics (3,4) which will penetrate the turbine casings for both Unita No I and 2 are presented in Table 14.8-1.
TABLE 14.8-1 TURBINE MISSILI CHARACTERISTICS Unit 1 Unit 2 Length of bucket (in.)
38 40 Arc (degrees) 120 90 Weight (1b) 5944 2431 666.8 671 Initial Translation Velocity (f t/sec) 6 Initial Translation Kinetic Energy (10 f t-lb) 41 17.0 Exit Velocity (6ft/see) 480 488 20.5 9
Exit Energy (10 ft-lb) 2 Minimum Impact Area (ft )
3.66 2.2 2
Maximum Impact Area (ft )
8.4 3.3 14.8.4.5 Penetration Ability of a Turbine Missile Penetration Formulas As indicated by Amirikian ( }, the Petry formula is most suitable for determining missile penetration into an infinite slab:
Di= kap logio (1 +
V2
)
215,000 Where:
Di = penetration depth into an infinitely thick slab (ft),
A = sectional pressure = missile weight / representative p
2 sectional area (1bs/ft ),
V = striking velocity (ft/sec),
K = experimentally obtained material coefficient for 3
penetration (ft /lb).
14.8-3 N
l,
~
Page 6 of 8 The following formula, which is reinted to the one above, can be used to determino missile penetration into a finite slab:
1 + c~'.(T/0)-2 Dr = Di Where:
Dg = penceration depth into an infinitely thick slab (f t)
Dg = penetration depth into a finite slab (ft)
T=
sinb thickness (ft)
For the case where Di = T/2, the above formula can be stated as follows :
D = KA log 10 (1 +
Y
)
s e
p 215,000 Where:
D can be interproced as a conservative estimate of the penetrationdepEh. The exponential relationship is not valid for 0 4 T/2.
1 In this study, missile penetration depths were calculated on the basis of D'
c As indicated by Zwicky( ), the effect of air drag on missile velocity can be determined by using the following formula:
V2=
i 1 + BV Where:
V = striking velocity (f t/sec),
Vi = initial velocity (ft/sec),
g = acceleration of gravity (ft/sec2), and B = sACd/2W (ft),
3 Where:
s = air density (1bs/ft )
2 A = representative sectional area (ft )
Cd = drag coefficient (dimentionless), and W = missile weight (1bs).
The translational velocity on impact was estimated for the low trajectory missile (LM) and the high trajectory missile (Hm).
In the case of the L2, air drag was neglected while full credit was taken for air drag in computing the 's triking velocity of the Hm.
3 The air density, s, was taken as 0.0809 lbs/f t, which is the air density at STP.
The drag coefficient, Cd, was taken as 1.0, which is a representative valve for an irregularly shaped object.-
14.8-4 v.
__ ~
e.
)
~
Page 7 of 8 Af ter' penetrating tho' casing, the missile can be expected to.be deformed.
y Thus the body will: be acredynamically unstable and tumble erratically as it pass es through the air.
Because of this expected crratic motion, the L sectional. arca was - computed as the average of - the maximum a'nd minimum areas (in a plane perpendicular to the shaf t axis).
Theuc areas are given in Tabic 14.8-l.
In this study, the value of_ K Cor the auxiliary building miss'ile barrier i
3 at clovation 698-0" was chosen to bc 0.00476 ft/jbcorrespondingto3000 psi compressive strength (5) and a value of.0.0023 f t /lb (5000 psi compressive strength).was 'used for the containment structure and missile barrier pro-tecting the cpent fuel pool (5) 14.8.4.6 Results A 2'-6" thick concrete missile barrier located at elevation 69'-0" protects the control room, switch. gear room, and waste processing area f rom a high trajectory missile (see Figures 1-8,1-12,. and 1-16). A 2'-0" thick con-crete misslic barrier positioned at elevstion 118'-0" protects the spent fuci pool from a high trajectory missile, j
Protection against a low trajectory missile -is provided by a 3'-0" thick concrete wall located between' the turbine building and the auxiliary building (see Figure 1-16).
)
The missile penetration depths for the above barriers are given in Table 14.8-2 for two cases; case I, in which half of the initial kinetic energy of the potential missile was assumed to be available for penetration, and Case II (conservative) wherein it was assumed that no loss of kinetic energy occurred upon penetration of the turbine casing. The containment structure, its dome and cylinder, provide adequate protection against turbine missiles.
(See Section 5.1.3.2.h.)
TAB 12 14.8-2 TURBINE MISSILE PENETRATION DEPTHS Depth of Penetration (inches) j t?nf t No. 1 thf t N s.
?
Protection f rom H.T.M.
Case I Case II Case I Case II
- ontrol Room, Switchgear Room & Waste Processing Area 17.00 23.0 7.60 10.88 Spent Puel Pool 10.44 15.48 7.48 10.88 Protection from L.T.M.
Wall-between' Auxiliary and.
Turbine : Building.
20.46 32.47
.19 44 29.16 i
'14.8-5
- t;
~~'
i-l Paga 8 of 8 14.
8.5 CONCLUSION
. Based on the above results it is concluded that the Calvert'Clif fs Nuclear TE
- j Plant'tInits No. I and 2 arc adequately protected against turbinc missiles.
O[
i
'14.
8.6 REFERENCES
(1)
General Electric Co., Description of Control Mechanism for Calvert Clif fs Station, January 1969 (2)
General Elcetric Report, Failure of Rotating Elements of Steam Turbinen and Gencrntors, March 29, 1968.
-(3).
Zwicky, E. E., An Analysis of Turbine Missiles Resulting from Last-Stage Whcol Failure, General Electric, Schenectady, New York, TR675L211; October 3,1967.
(4).
Westinghouse Report Covering the Effects of a Turbine Accelerating to Des truc tive Overspeed.
(5)
Amirikian, il., Design of Protective Struc tures, Bureau of Yards and Docks, Department of the Navy, Washington, D. C., NavDocks P-51, Augus t 1950.
14.8-6 4
ATTACEMENT 2 Pace 1 of 3 ANSWERS TO OUESTIONS RELATED TO CALVERT CLIFFS U-2 TURBINE DISCS SITE SPECIFIC GENERAL I.
A'. Subject unit is a tandem-compound sextuple flow, 1800 rpm steam turbine-generator rated nominally at 878 Mw. utilizing i
40 inch last row blades.
The LP element is designated as a
)
Building Block 80.
)
l B.
Each LP turbine has 23,253 hours0.00293 days <br />0.0703 hours <br />4.183201e-4 weeks <br />9.62665e-5 months <br /> of parallel operation as of March 4, 1980.
Projected hours of additional parallel operation un'il 1-1-81. planned inspection equals 6110 hours0.0707 days <br />1.697 hours <br />0.0101 weeks <br />0.00232 months <br />.
t 1
Total time of operation until inspection equals 29,363 hours0.0042 days <br />0.101 hours <br />6.001984e-4 weeks <br />1.381215e-4 months <br />, l
C.
This unit has-been subjected to three (3) intentional over-speed trip tests and no un-intentional over-speeds.
D.
See Attachment 3 Notes for items 1 to 11.
l 1.
Type of material is Ni-Cr-Mo-V alloy steel similar to ASTM
]
A-471.
2.
Tensile properties data of tests *.aken from the disc hub are given in Section B.
Data obtained from rim material are presented in Section C.
3.
Toughness properties are also presented in Sections B and C.
As described above, Section B contains hub properties and Section C contains rin properties. Upper shelf energy is not presented when it is the same as the room temperature energy.
4.
The keyway temperature is presented in Section G.
This is the calculated temperature two inches from the exhaust face of the disc at the bore during full load operation with all moisture separator reheaters functioning (where applicable).
5.
The maximum expected keyway, crack size has been calculated and is included in Section G.
This is done by multiplying the crack growth rate by the time the unit was in operation
)
prior to the disc bore / keyway inspection. For units not yet inspected, the time used should be the expected operating time when the unit will be inspected.
6.
The critical crack size at 1800 rpm and at design overspeed is presented in Section F.
7.
This is the ratio of Item 5 to Item 6.
It has been calculated and included in Section G.
E
Pace 2 of 3 8.
The crack growth rate is given in Section G.
These crack growth rates are the maximum expected rates based upon known cracks to date.
Westinghouse has changed the basis for determining these rates to utilize the NRC gray book operating hours.
It is believed this agrees with the way the NRC staff determines crack growth rates. The crack growth rate of the number six disc and number one disc of BB 80 turbines is assumed to be zero since these discs operate dry under normal conditions.
9.
The bore tangential stress at 1800 rpm and at design overspeed are presented in Section E.
The values presented include the stresses due to shrink fit and centrifugal force loads only.
Additional analyses to include thermal stresses and pressure stresses are being made, but are not presently available.
10.
The fracture toughness, K f each dice is calculated from IC, the Charpy v-notch and tensile data.
The values, presented in Sections B and C;are calculated at the upper shelf temperature or room temperature, whichever gives the lower result.
11.
The minimum yield strength specified for each disc is presented in Section B.
II.
As of this writing none of the three (3) LP rotors have recieved either disc bore or disc keyway irspections (other than during manufacturing).
III. The following parameters and values represent the nominal water chemistry of Calvert Cliffs U-2 and are considered representative of the LP turbine environment.
PARAMETER NOMINAL VALUE 1.
Sodium (Ma )
1 ppb 2.
pH (-log (H 0*))
8.5-9.0 3
3.
Cation Conductivity
(.10.15)/Mmhos/cm 4.
Specific Conductivity (2.0-2.5)j4mhos/cm 5.
Silica 10 ppb 6.
Chloride 10 ppb Significant changes in secondary water chemistry are subject to control as described be ow in " Table of Operational Steam Generator Chemistry".
Deviations in normal values are promptly examined /
evaluated so that necessary corrective action can be taken to preclude significant disturbances to the LP turbine chemical en vironment.
TABLE OF OPERATIONAL STEAM GENERATOR CHEMISTRY ANALYSIS NORMAL ABNORMAL PROCEDURES / METHOD SPECIFICATION (2)
LIMITS (3)
FREQUENCY (1) 1.
Specific Conductivity /901 4
15 1/24 hrs.
@mhos/cm. max) t I
Pare 3 of 3 ANALYSIS NORMAL ABNORMAL PROCEDURES / METHOD SPECIFICATION (2)
LIMITS (3)
FREQUENCY (1)
'2.
pH @ 25 C/902 E.2 - 9.2 7.5 - 8.2(4) 1/24 hrs.
9.2 - 9.5 3.
Sodium /908 (ppm, max) 0.1 7/W 4.
Suspended Solids /911 (ppm, max) 1.0 10.0 2/W 5.
SiO /916 (ppm, max) 1.0 10 1/W 2
6.
C1/906 (ppm, max) 0.1 7/W N.S = Not Specified (1)
Frequency noted is minimum.
These may be adjusted upward if conditions i
warrant.
If normal specs are exceeded, the out of spec parameter (s) must be analyzed at least daily.
If abnormal limits are exceeded, the out-of-spec parameter (s) must be analyzed at least once per shift.
If blowdown is secured, a grab sample must be drawn and analyzed for spec.
cond. and pH at least 1/24 hcurs.
(2)
Normal specifications are those which should be maintained during proper operation of secondary systems.
4 (3)
Abnormal limits indicate a fault condition exists and plant shutdown should be commenced if abnormal limits are exceeded for four (4) hours.
(4)
The unit should be immediately shut down when pH exceeds 10.5.
"UK Experience of Stress Corosion Cracking in Steam Turbine Discs";
J.
M. Hodge; IL Mooford, I Mech E 1979.
This paper concludes there appears to be no presently known correlation between disc cracking
)
and secondary water chemistry.
IV.
It is our intention to inspect all three (3) LP rotors during the planned re-fueling outage commencing on or about January 1, 1981.
Plans are currently being drawn which include both keyway and disc bore inspections as per Westinghouse recommendation.
Inspection is subject to availability of qualified inspection teams of Westinghouse personnel.
V.
Not Applicable.
VI.
Please refer to Attachment 1.
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inspection time.
"'j Ratio of calculated crack to
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critical crack size.
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4.
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Data for this disc w!!! be supplied by Westinghouse at a later date.
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(FI.L S. 13.5. KICIgsg,sg,gggg,33,
i.
gFT.LB.3 st o
- 11. U.S. NIC IE51*5C#itI4.ll I
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F. Casta DATA f
i E. BCet STeE55
- 1. A-Ca-OP (1800 RPMB tlh.)
58EED ton =3 SieI55
~
!!4.5
- 2. A-CR-05 (OVEESPEEDS l.
1800 (8518
- 2. 2160 (123%l ta515 S. SEnvict Ca's All Bracketed Data Subject to 1: ini:ailf e.Mihi9 hat
'o" "
1
@ eroariet n
- 6 c -
c F
- b,c.e, 3.
Calculated keyway crack size till i
' =
inspection time.
Ratio of calculated crack to 4.
critical crack size.
L
.i W
t
e s
J 3
,..: u 6.
)
y o
..E ' 4 s
-i s;:
m
',i.*
\\
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e t.___J a.
E'-
~
~
n O as e
a.
t.,.
a
-.s -, n-- w.e e
.,y g *u.
Qe v.*o.,,l.",,.,4
".n '
- )
w
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-.o 5 =-
- . - - a.....u-w ai
.. ed. --- - =
a e.
1u ro e
e e JJa&*1,1,
- n r,
it tN esJ
>3W8bg ees sa
=
~
o 3
c a,.,
e.u a
e.
u a
u-a
\\
,e,, 4;J J~e
~ *
'i. J W
gg aw,,
e.t. w j
e I
u g
hd
- a. o.
r.
I uu N
- \\,
O, O
d
.4 u
dd
'a I
e-l s.
e.
- [1 o
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43 d
ed &
e M b.J b
wg
- e an e* g est F
4 e8 D
34 e
w q Q '*"
G8 e D
e ed we Q1 W
e e es ens ee, as t.a
==*
e G N'
' wt,
_i e
me g
b > h tese to e'
W en
- +8 9
.4 9 e tJ y
c
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- e-iam e e.
W W
e i
a e..n,
.u w w ve-ws us o.,
W es as omm as F
o ed e*w w o w ew s wa. www w
a s a ww ee a
>wn e-oss & M
==em www w a a
_A u
os
- .a ne o o e we se s.st s e e r es,* e e m
e we we en e e 4==& ene-o m > > in e
e u
ev e r s e e.s e s e e wa= = c e. D wtP a e D D 3 r1 n.#
e e
M g
a e-rw*t e c eda = e.e e eeeeee en tA n
=o=.'
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a.
L_)
in 3 =*
e a
e l
M M
end O
m
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40 **
- 4
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w.
r aM W o
w.
3 **
U, 84 k ed O see X
meQ ws#0e vt as en b
t Mk u,
M MM n,
.4 w ~
.i %
y ye WW 5
WW
- .te w
m he U
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4/9 4
- 8 9
N M
7 ft 9..
W 3e en n n
.e f.,, [ 8,o.
r gas e e.1 se e-e4 em s
ou u M
ee
. b
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U ygU ee p 4A P
sk C1 e
F F1 setent +
w *e
@W N
Oe-na.A Q
L.J e
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U m.e e0 c.
w e,
e e
aa nas er w u a we e o
.r o..
a 40a
- g ** *b a a
- = ins fl w
wp 4
ew a
s7 **
9 ** #
90 m.6 4#
me Q u
e= a a en ed U "*
U end W
-e te s
(14.s m
O
.d w e=
g td>
E ft O
, eed S vertvl led S
ee e
e ea **
Q ee
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M3 # 3& OMtad 3
3) me N we
== N e8 J 'D 3%e.J asoon Q
a 8
e e
eeeeee 60 w
O e me twPt s trid- -
Q
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e 14- 0 F 3L i i 10 s : 000CICC 90 3 e
~
2 LP YuBSINE 015C 14F04*ATIOA
- 43 pes'.E5 te Pl C. pattegat g,
ggggggg'p40PEeflE5 tut,8.'
7 A. U%If 13E%i!FIta!!3%
g, tapg g3
. an5Ill
- 1. SUILCING is:Ca tu!N. v.s.
5 tall -
. Y.5.
tuill
- IDvad; ng6'P
- 5. v.5. tests i
. u.r.5. t=513
- 2. L%11 Cai. wear CLIFF 5 2
- 2. SUPPLIER:
i 3.
CUSTCwEn:
osLil*C3E EEE
. o.r.5. en5I:
- 3. EL0kGattom
- .t**
- 5. ELCAGATIo%
{
i 4.
a.a.
10EG.F8 luP&CTtFT. S*y sc8
- 5. Fail
- 5. LOCattog
- 6. e.a.
2
- 6. a.1.
7.
IE5T %C.
T%1525
- 8. R.1.
1= PACT 4FT.L9.3
- 3. U.S. InPACI IEMp*
- 6. DISCS
- 7. FaTI s0Es.F s
- IDEG.Fl
- 9. U.S. I=ePSCI TEMP.
- s. U.S. In%1 j.
40EG.F8
- 10. U.S. IMPACT E46.
Efl.LS.3
- 9. U.S. KIC(ESI.gggi g 3n.4 3
- 11. U.S. KIC-IK51*SQti414.38 s
8.
na Ce b'I..i ) -
- h.. ]. -
(
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D. C6 tea 15f or Mb C
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58
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%I
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. DATA (a5 )
{
-)*
J F. CRACE a
E. BORE 5f EE55 (1800 RPnl IIM.)
a SPEEC 4DP's 5f4E55
- 1. A-CR-OP (IN.5 L
- 2. a-CR-05 toyERSPEE05 4
(4518 1
I.
1503
- 2. 2163 tt20tt in518
~
1 i
G.
SEatICE ;ava All Bracketed Data subject to F
- 2. Esti-a1EL *an C4/DT (Ih/HR) h Proprietary Codes, b,c.e, DE*. TEMP. " Etat TEmo. HUB 40EG.Fl 1.
L.
Calculated keyway crack size till 3.
inpsectiors time.
Ratio of calculated crack to 4.
critical crack size.
m.
.u.
4
')
~
4
.10 s : D000100 90 3
~
fu 81NE DISC Iwrce=sT10h e
- sa 48 LP
- c. Pattelst PR W.'
- 3. =81ERIst PROPEnt1E5 tuult
- a. u%It ICE %f!FICartas 1
g,gg,,
?2
- 5. APPL I E R :
n.GW80L M
.9 g,'
y.5. tuSIl l
- 1. sult31V. ?LCC8
,,g, I"13,
- 2. U.T.5 110h Cagvizi CLIFF 5 s2
- 3. v.5.
88513
- 3. ELossGa
- 2. s%1T
- 3. CusTG=[o:
6stf1=3ag stE
- e. U.T.5.
48514 e,e.a.
2
- 5. ElokGatION*
- 5. F a t t 40Eg.7, TIFT.LS*I
~' '
- e. Lse 6Cv j.8.}*g#fECT1E"P*
6.
U.S.
- 5. LOCa11Gg 3
{*, (AjI,- {0, Idyg,tg,3'~
,a
- 4. DISCS
. t 0E G.F 7.
TEST ACs f %3 526 e* U.S. IMPACI E g
- I
- 9. U.S. Impact itMP.
- * ' I
- 10. u.5. IMPACT EhG.
q
- g. U.S. RIC6tLI450#ILI"*II i
d.
- 11. u.5. RICLE51*50Rit14.ll
,:T.
y,,
-t
[:
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gg D. CHEMISIST t
i
.($..)." '.[ u j E'" )
L' d
+
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t j
t.5 ]
[s.,-
u F. CasCE D&TA 9
I-1 A-CR-OP (1800 RPMI II"*,g L
E. BORE STeE55 tlh*
SPEEC t.
STRES5
- 2. &-Ca 05 tosERSPEEDI i-9 88513 1
I. IMO
- 2. 2163 tl2.Al tuS13 a
G. 5E041LE :sfa All Bracketed Data Subject to 1
03E4. TEwP. =[ Tat TE**. Hua (DEG.Fl hProprietaryCodes,b,c.e.
(IN/Het
- 2. E5tiratE 3 ra u Cs/DT
{}bc.e.
Calculated keyway crack size till 3.
inspection time.
Ratio of calculated crack to s
4.
critical crack size.
r-S 1
6
6 IL OF 36 o
10 s OCs01:390 3 LP fu St%E 015C IhTORwatIOb I R I I -
o 94 0Pd - I I E S C. m&TEatal peopERTIES twuB8 13 3, watEggAL
- 8. UNIT ICE %1!FICaflas 3 11PE tasill
- 1. 6ulL3t%; tLCE=
E; 1914. v.5.
HEP 8(%5 TALL
- 1. T.S.
Em51 M10 VAL CsLbECT CLIFF 5 s2
- 3. v.5. (n516 J. U.T.S.
taill
- 2. SUPPLIER:
2.
Alf
.acTI= sat sgg U.T.S.
4m5:3
- 3. ELO% Gat 10m
- 3. CusT0=Ec 2
- 5. ELokGaf!04
- 5. Fait e.
- e. R.a.
(DEG.F3 6.
e.A.
IMPatitF1.LS.I e.
Los OCv
- 6. sISCs TA1527
- s. R.T.
IPPACTIFF.L9 9
- 6. R.T.
- 5. LOCATION
- 7. raTT (DE6.Ft
^~
~
- 7. U.S.
3*PsCT TEMP.
EDEG.F8 7.
TEST %3.
9.
U.S. I" PACT TE*P.
S. U.S. IPPACT EkG.
(CEE.Fs
-ifI.L8.1
'l
- 10. u.5. IPPACT [AG.
f* r-tFt.Lt.3
- 9. U.S. KICt a 51'5E*I II* I I L,
- 31. u.5. aICta5I*SGRTt1%.it J
[
]
E.
1 E
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[
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3 M0 C#
L SI
- 0. CHE*Isfat MA
' ?'
0
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CU AL Sat
(
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( 58 h,
4 A5
%I FJ CRACat Data
- 1. A-CR-OP 41800 RPnp (IN.)
E. 800E 51GE55 5'EED t# Pet STRE55 (IN.)
- 2. 3-CR-05 (CVERSPEEDI tusts 1.
1803 t otill
- 2. 2160 (12Jts All Bracketed Data Subject to G. SEGriC[ QATA 1
@ Proprietary codes, b,c.e.
- 3. opER. TEMP. PC I A L IEPP. 908 40EG.F3
{*
- b Cees l
IIN/HQ)
- 2. r 51]Pa1E 3 Pas Da /DT Calculated keyway crack size till I
3.
inspection time.
Ratio of calculated crack to e.
4.
critical crack size.
L r
i 9
n O P-3L i
10 s : 30901C3903 La Tuo814E CISC IkF04*atich C.
- A TEGIst '80'E ~ d '
- 8. UNIT IDENTIFICsIIO%
- 3. -stE21st peoPEeTIES t*u*
Ti
~
- 1. BUILCl*.3 ?.Cte e l.
- 1. Trot t*5183 t=Is. v.5.
i
- 2. CNIT 08Ldie r ;t g*F5 s2
- 2. SLPPLIER:
mfGWaCE mEP %$ TALL
- 1. v.5. ta518
- 3. CuST0=Es malt 1=C3E Ett
- 3. v.5, ga s g t.
- 2. U.T.S.
ta5!,
8 LPs 2
g.
u.t.5.
tm513 i
- 3. E.LC45aT104
.5. LCCa.1104 5.. E Loksaf10%
- 5. F41T 4 30s
.a.
c15C 5
...a g
gg,tg,3
- 7. FaTI IDEG.rg 7 1[5 T %C.
141524
- 6. R.I.
I
- 4. e.T. 1*PatttFI.L3.5 I* U*S*
I y gg,p,
- 9. U.S. ImPECT TE*P.
gggg,p 3 -
1"%I]"j*
~.
S. U.S.
- 10. u.5. 1=
G.
- 11. u.5. aIC
- 9. U.S. EIC y.
(Fi.LB.3 ta5195 Crit 14 55 1.
7 E
g D. CHEMI51RY
}
[ ]-
]
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bA c J c"3 c" J c" A c'5 -
c '" 'l - - CD 5*EEc saa-51sE55 F. CasCa Catt
~ -
E. 30eE $1stis
- 3. A-CR-OP (1800 RPnl (14.5 1.
1803 tests
- 2. a-Ce-05 101E45 PEE 01 (It.8
- 2. 2160 412;t 3 ta511 a
- 3. SE2stCE Cara' All Bracketed Data Subject to
- l. 3ota. TE=P. *EitL TE*P. HUB (CE3.F 3 SProprietarycodes,b,c.e
- 2. E5fl*4tE3 =at ;ap;t glhta#8
{ ] b,c.e Calculated keyway crack size till LJ 3.
inspection time.
4.
Ratio of calculated crack to critical crack size.
el m
4
WOF36 i.
10 e :.30801Co*C1 e
LP Tb8814E D15C INF04maTIC4 I
POOPEa *M a C. *sIE31a(
- 5. *aTEstat poGPE4f1E5 tug 53 ft A. UsIT ISENI;rItaT 3%-
1.
TTPE Nk StaLLp
- 1. eu!LCl%' 8.0C.
Ljtaf'
- 1. v.5. ta$tt
= val
- 2. U.t.5.
ta518 2.
cs6eEst CL grF5 s2
- 3. v.5. taste
- 3. ELohGaf10%
- 2. LSIT
- 3. CUSTL"E*:
stLf;=0*E GEE
- n. u.i.5.
ta$tt 2
- 5. ELO9GatIO%
4.
A.a.
- 5. FATI t0ES.F8 S.g
- L**
- 6. D15Ce
- 7. Faff 80EG.F3
- 4. R.I. 1*PACitF
- 5. LO:afgC%
6.
e.a.
- 7. IEST SC.
TA1525
- 3. 9.T. 1*pacitF1.L3.5
- 7. g.5 1*P
,, =
t
~-
.. u.5. i P;g'*Jt
~'
- 9. U.S. 1* PACT TE*P.
- 12. U.S.1.!!!?-RG.
- 9. U.S. AIC eftIW.83 I
~~
(FT.LS.1 IESI
- 11. U.S. RICtKSI+50RTt14.tl 6-E' 3 c "' ]
c ".J E' ]
c" J E '* J 1]
t D. CHE=ister c" 3 c "a c" J c" a c "2 c '"3 c' 3
~ '
F. CRACK DATA l-9 t
- 1. A-CR-0P (1830 aPut (14.1 E. 934E 5 FEE 55 J
- 2. A-CE-05 801EG5PEEDn (1h.8 5 DEED 447*5 STRE55 (m113 1.
1523
- 2. 21m? 112 M s imS13 G. 5Ent!;E cat *
~
All Bracketed Data Subject to wua scEs.rg
{
+
- 1. ;*Io. TEgo.
- Etat TE*P.
9ProprietaryCodes,b,c.e tig/weg
- 2. E5 f;* A TE3 = A a Es /DT Calculated keyway crack size till
{- } b,c.e 3
inspection time.
Ratio of calculated crack to
- i 4.
critical crack size.
w r
L 2
~.
14 0 F 3/.
ID C : 008010070=
LP Top 31%E 015C IkF04 PATI 3h ~
- RC8E3'IO
'"I*I C. =stEelst t %3 8 kAL80CpteTIE5 E.
I O!!
- s i:!. p n.Fs 2
- 2. I.:. % d.ai-7cd MU'd51.u.
15 It t
2.,
- i.. 5. t.sii.
- 2. o.r.5 1 51 i:
- E 3.
5.
t 51,.
..<,,Crn.
. u.v.5. 4 5:.
- 3. EtogGaf!C4
- 5. EtokGattog
- 5. Lot.,.;s jE %
I* [!i (DES.Fl 5'.
5 i (3tG.F 8 ImPACitFT.L9.1
- 6. O!5Ce
- 6. B.T.
TEM *.
7.'TE51 %C.
f%15te
- 8. 8.1. I*PACF8F1.LB.3
- 7. U.S. IPPACT
. t0EG.F3
- 9. U.S. 1= PACT TEPP.
_v (GEG.9s
~
- s. U.S. 14PACI ThS*
IFT.LI*I
- 10. U.S. 1=PACI Eks.
I tFt.tg.3
- s. U.S. mICtast esca t(Ins., y
- 11. u.5. mICtm51*5 Cattle.33 O'
D. CHE*ISTRY
-7
(
]
{
(
F. Casta Data E. ecoE SioE55 58EE3 487"5 STRESS
- 1. a-C4-CP t1600 2FMI tlk.1 II%.3 1.
ISOC ta513
- 2. A-Ca-c5 tovERSPEE03
- 2. 216; 8123t3 t=515 G. SE4 1CE Cava All Bracketed Data Subject to
- W
- D****
~
~ b,c.e r
- 3. 0*IG.
TE**.
- Etat TE=p. hub (DEG.Ft
- 2. E 511-s t E J *a s La t3 T (1%phet 3.
Calculated keyway crack size till irtspection time.
4.
Ratio of calculated crack to critical crack size.
==
=
e e
- -------. ------. -e-- -
l l
l l
l Jo o P %
10 a : D0001C0904
.e LP T6stI4E. 015C 14F0esat t0A. ~
4 C. =atEttat PicPEsttE5 88I"#
- g. *stEGint *DCPE3flE5 t*J38
- 1. cu1Lt1%5 3.0ce s;
!. fYDE C J tasti TE
- s. UN!! ICE %f1FItaTIs%
1
- =i%. v.s.
- i;faLE MEPPE&iTAta_
- 1. v.s. Easts l
- 2. b%It
- . vest CL;rF5 s2 2 5sP PL IE R
ta5Il
- 3. Cus1C*E8:
esti1*Crt GCE J. v.5. tasta
- 2. U.T.S.
4 LPs 2
w.
U.1.5.
tail)
- 3. ELO% GAT 13e 4
- 5. LCCatics CE %
- 5. ELC%EaTIch 4
e.a.
- 5. Fa1I (CEG.F I f
6.
DIsta
- 6. e.a.
i
- 6. a.T. 1=PacitFig8.g 4
- 7. FATT EDEG.Fi
- t. 2.1. 1*PACitFT.LS.I.
{
- 1. U.S. 1*PICI IE 7.
I E 5,I %3.
'%1519
- 5. u.s. luPaCl TEM.
g EDE6.F3
- 10. t* $. IMPaCf E%G.
~
8* U*I* I"Pht
[
4 4 0EG.F i i
L
's.
i 8
(Ft.L3.3 l
9.u.s. alka 51*5Cattih.88 g_.
. _f
- 11. u.5. mittR$1oiCGTilt.ll I
f
~
CJ f'3 l'3 L.3 '
C3 03
- 0. CMEatster f
E )
[_
)
O
]
E. 900E STEE55 F. CeaCa Data
.5 PEED t***3 i': m
- 1. A-CR-OP 1140C RPM) (14.8
- 2. a-CR-Ci (OWER5 PEE 05
.I (14.3
't.
19CO inst I
]
t
- 2. 21oS 117;tt
(=519 L
t s'
G. SEh !CE :sta
- 1. CDEC. TEMP. "EtaL TE*P. HO6 (CEG.F3 all Bracketed Data Subject to
- 2. E5tI*stE3 was as/31 II%INSB
@ Proprietary codes, b e.e l
- - b,c.e 3.
Calculated keyway crack size till inspectiort time.
4.
Ratio of calculated crack to critical crack size.
4 W
- e e
h
__________________._____,___.________________________________.__.________._______________.________._______.________..________.___._-_..___-____.__s
4
. 2. i o f M.
-ID e.* D3401:090=
4 LP fu#5thE DISC IhFOReaf104 C. *ATERIAL FC"E*'*-
- g..stEstat pnC#EeTIES toaat
~
g3
- a. u%II IDEst tF t ta tin
- g. TYPE
~ Ed5III
- l. sutL31.a
.CCd t=l%. v.5.
vaD nEPPiMf ah
- 2. U.t.5." SIS
- 3. v.5. t
=
2 5.*PLIre-14511
- 2. o%If pstyg:t CL;'F5 s2 3.
v.5.
ta511.
ssig=;oE :EE
- m. U.T.S.
tasis
- 3. ELogss110%
- 3. Cust:*Ea:
e l
2
- LP8
- 5. Eto%Gatics
- m. p.a.
~l 4CES.Fl
- 5. LocaTIO%
CE 4
- 5. Falt I*PACitFI.(6.5
- 6. 0150s 2
6.
8.s.
- 7. FATT (DE G.F 3
- 6. E.T.
TEM
- 2. 4.T. t=PatitFT.LS.8
- 7. g.5. 1* Pati I* IESI %G.
Mii2 40EG.Fl
~
- 9. u.5. 1*PRCf'TE*P.
- s. U.S. I'PajiEh6.
(OEG.rg (F,..LB. 3
~;
- 13. U.S.
Iwpati E=E.'
~
m tF1.LB.3
- 9. U.S. a!Cla51e50SitIN.II -
II. 3.5. mIC l
ta5I*5:RitI4.ll i
r dJ CJ c"a (j
C"3 T""]
l
~,
D. CHEMI5127 c" 3 cb c" 3 c"j c'b c'3 63
~
c i
Data F. C#aCK-E. BO#E SisE55 t.
- 1. A-CR-OP 4180C RPMI (IM.9 t
5DEEC 80**1 StaE55 814.1
- 2. A-te-05 (OVERSPEE01 I.
1803 ta519 2 2160 8120tl smSII G. SEctICE rara All Bracketed Data Subject to
- 1. 3*ED.
TEgp. wEisL TE=P. huS tLEG.F1 hroprietaryCodes,b,c.e
.i
- 2. ESTImatEJ was St/31 41%/.449 s,c.e f
3.
Calculated keyway crack size till L
inspection time.
4 Ratio of calculated crack to crit.
ical crack size.
~
e e*
o=
e m
1.
a
r 2-2. o f 3(,
i t
10 s t 00s01C090=
j LP Tu0nINE DISC INF04=&TIOk 4
P80PE8I M C. wattelst
- 3. =af E41 st. Pn0 peat 1Es teu3s 13 i
c--
- a. UNIT ICE %TIFItaTI;\\
- 1. TvPE testst
- ,gg, "IUvan SEPP W AL 4
- 1. Y.5*
ea518 83 t=1%. v.s.
n
- 1. EUILLI%5 c60U
- 2. 5.p PL IE R :
- 2. U.f.5.
- 2. a%IT La.vi:1 OL ;' F 5 s 2
- 3. v.5.
tusil
- 3. ELONGATI i
a
- 4. U. f.5.
tu$'t n tt1=L3E CEE 4.
- 8. jfy,FT.LE.8
'3. CU5fC=E4:
2
- 5. EL0hG A T ICar
- 5. Faft acit 4
LDs GE %
- 6. s.a.
0* #*I*
g,,pggy ggyP.
- 5. L 3Cai tC%
EDEG.Fl 7* U+5'
$0EG.F3
- 7. FaTT
=
- 4. 4.t. I=PACitFI.L4 5
- 6. 315Cs 7%11!!
1
- 7. IEST %0.
u.5..I= PACT TEMP.
~
- 3. U.S.
IMP Q'
~~j~
9.
6.
- 10. U.S. ImIFI.Lt.1
.$.u.5.aIj,5g=50ettIh.88 -
- 11. u.5. aICan5I*50ettlk.nl
'-l
^
- e. y s
]
]
-]
]
D. CHEMI5tav c" :
dL n c" a cn c'" a cM ' ~ ' -
L
" ~
l'. CR&ta DATA 11800 RPnl (It.1 s
(Is.1
- 1. A-CR-0P E. BOCE STRESS steE55
- 2. A-CR-05 10nERSPEE08 s
==s o
5'EEC 7
easil j
- 1. leCG tsill 2 216C 512315 G. SEsst:E rata All Bracketed Data subject to -
- 1. OPE 4 TE@. *ElaL TEPP. hua (SEG.Fl gp g,
%,, g, LI%/ ne l
{}b,c.e
- 2. E5f!PaTE3 s.am LafDT Calculated keyway crack size till 3.
inspection time.
Ratio of calculated crack to crit-
- t..
ical crack size.
S i
4
23 oF 3C 3
10 e : 00totC050=
e e
198S14[ DISC 1hFORusTIQ4 28
- ' I LP C. wa1Entat
- 2. mate #.Ist raCPERTIES t*Mt gg I
~
- 1. eu1LLI*.yrgrtCat;&%
u%ff'13E 3, g, g ua d h k Ist&L A.
- sst a;
- 2. U.T.5."5EI y, b'.N* gf gf * ' e 1* Y.5*
8 2
8d5Il
- 2. u%ti Cs vtar (t;rr$.2
- 1. 1 5.
ta5il
- 3. FLO4Ga11C4 CJ5fC*Es:
ga,,fg.gog,tg
- e. u.t.5.(gasgs
- e. R.a. t0E3.F8 I
- 5. ELONGA Ich O*3
- L'8
- Eh
- 5. Falt 1"F8CIIEI
- 6. a.a.
- 6. R.T.
1= Pact T
- 5. LCCattsg 5
y rATT 10E G.F 3
- 6. GISCs I. U.5*
- 7. IE5T 40.
T%1522
- 5. 9.T. 1*PACI(Ft.t3.9 is. u.5. iJf!? IL.
..u.5.i4Hi'IA;-
~'
- 9. u.5. (* PACT TE*P.
AFT.LS.
~~
EFI.LE.8
- 9. 43.5. EIC d 4188.3 3 (E5
- 11. u.5. AIC(K51*SQ41 tilt.ll a
w m.
u -
)
)
O. CHEMISIST L
CU AL b
b b]
b) b.]
set 8
%I A
F. Ct&Ct DATA tlk.I g
E. 30eE Sf4E55 a-CG-CP (1800 RPRI (Ih.D
_J 52EED s 7* n SteE55 c
3.
- 2. A-CR-05 tovEe5PEEDI l
m 4
- 2. 2160 412318 14513 g
I ta513 l.
19C3 j.
All Brac M ed h ta W ect to
- 3. SL*vlCE ;s?s l'
7 Oroprietarycodes,b.c.e
- 1. CDE*. TEMP. *EttL TE*P. hu3 (CEG.Fs r - b,c.e
- 2. Esti-aTEa -a s ca tui II%#wes
{-
Calculated keyway crack size till 3.
inspection time.
Ratio of calculated crack to 4.
critical crack size.
W s
i m
MO
-36 10 e : 30801CC90s 0
i, e
Toetl%E DISC IMF0epAf!0s.
P23PEsf1ES 181"8 LP C. matEalat
- 2. =ATEalAL pa0PEtt1E5 s.s ss Ts f-
]
u
- a. u%I7 IDE %T Ir g(s t;-*.
- 1. TvPE a451st EG
- 1. Eu tL0!*.3 f. Cs t=ts. r.5.
piEPP W5ISLL-
- 1. v.5. tustl as ya g en5IS
- 2..%I7' ta64Est ;LtrF5 e2
- 2. 56*PLIEG;
- 2. u.T.S.
3.
T.S.
EN5IS e
- 3. ELos58TIQh
- 3. Cu$f0*Es:
catt1*C2E stE
- e. U.t.5.
(n5tg a
2
- 5. Ete%6aTIon
- e. e.a.
igEG.Fl
- L U..at!C%
Gf%
t>PsCTtFig5.g
- 5. L
- 6. e.a.
- 5. Fall 4
6.
8.5.
- 6..15C*
- 7. FATI IDES.F3 I*
If 5I NC.
I%1523
- 8. 8I.T. !=PACitFT L3.8
- 1. L*-5.
g=PsCT I
t0EG.F 3 TE P..
IPPACT ENG.
- 9. U.S.
1* PACT ID. U.S. IPPACT E45,
- 9. U.S. aICtESIe5Ga t t!*8. 3 3
~j tCEG.F8 t.
I J. U.S.
III*LO*I
~'
tFT.La.)
t
- 11. U.S. mICtuite50RTt1%.lt
~
E']
L"]
C" J E' J c ]
t" 3 T'. 3 1 ~
D. CHEMIster Ca C3 (8 'D C3 c ~J C3 C5S-CU su '
at 41 a5
~
- r. Ctats Data
[* EDGE Si8I55
- 1. A-CR-OP (1800 RPMI (14.8 SPEEL gan=3 StaE55 i14.1-
- 2. s-CR-05 (OWERSPEEDS T
east t.
1900 smSIB
- 2. 2163 t173ta t
- 5. 5Eo* ICE Cata All Bracketed Data Subject to
]
hroprietaryCodes,b,c.e
- 1. CDE*. IE 98
=Etag IE=P. wug sgEG.F3 p,b,c.e
- 2. EST!*afEJ *ss as3r (I%spes Calculated keyway crack size till
- 3. ' inspection time.
~
Ratio of calculated crack to 4.
critical crack size.
6 W
+
X b P 3c.
10 e : DC.01C09C5 5 i fu 41%E 015C !=F04-ATICE 2
~
'"I*I e
LP o' -
C. pafERIst 9
- 9. 481EC,IAL PROPEGilCS (Hw13,ta518I l
is F-4-
L' li 10E% f ;F I:s t g;%
g,g, g.
- 1. $u1LCI*,; 3.,C;.
8=
IGuaLf eEpars5 TALL 1 T.S. 185I'taSit g
t*I%. v.5.
r
- 2. U.t.5.
2 SuP PL IE R :
2.. A.lf,
CatvEst CLgrF5 82
- 3. v.5. taitt
- 3. ELO4G&f10%
a e CuST;wEo:
.s,tge;3E SEE 4
u.t.5.
satif s 4.
9.8.
t0EG.F8 3
- 5. ELChGal104
- 5. FATI IwPatitFI.LO.g
- L'"sIIO%
GOW LOC
- 6. a.s.
- 7. Fait IDEC.Fs
--6.
R.T.
G150' D.
1%3536
- 8. 9.T. 1*P AC T1F t..Lt.)
- 7. U.S.
3 6.
DEG.F4 IE18 %
.. U.S.
- giJ t-F.
- 9. U.S. IMPACT IE*P.
1-,IDE G.F 3gg.
- 9. u.5. aIC("5I,$,,9, g,,,3 3 L
iO. U.S.
L
.. i
~ _
- 11. U.S. mIC(M51*5341414.tl
~
pr 8
n0 p
[b #
ce sg D. CHEP15Tev nh
- ]
I-
-~
CU AL 58s
( 55 ]
%I F. (GSCS DATA i
1 4-CS-OP (1800 RPM) (IM.I E. BCol 574E 55 ST:~ is Lih.I 5PEEC 887*
- 2. a-Ca-05 tout 45 PEED) t.518 f
1.
1900 is518 L
- 2. 2163 11Mt B All Bracketed Data Subject to G. $E8v!CE : sis hProprietaryCodes,b,c.e
- 1. C*E2 TEMP. -EtaL TE=P. Hug (CES.F3
- ]
b,c..
(Issues
- 2. E511*stE3 -en cs/31
~~
Calculated keyway crack size till 3.
inspection time.
Ratio of calculated crack to ggisp
- 4. critical crack size.
6 N
.I l
I i
l l
l 1
- - - - ~
m
r 3 oF 3G e
10 e : D00CIC905 I
J Tu 3INE DISC I4F0a=aTIos o
LP c
" t a r a ' ** :'""" ' ' * " '
'i."!Elit?'i'!!'""-
'-;:'jup'acar="c5t~si] t.5n.
~
[
4:
i-i~. v.5.
,pgi,-E.:
':: t:!.PHP 2 i: u;&is;;,
.<:.u E m'aur
,..5.
,,51,
.5:>
- 2. o.T.S.
u
.T.S.
..Si,
- 3. ELO%6aTIO4 2
- 5. ELo%5aT104 II: 0E S.F l
,- L
$0*
5 1*P8CitFI*LO*I
~
I.fi!i80EG.Fl 6.
R.T.
7.
TE57 \\C.
7%1537 B. R.T.
1*P 8 C i t F T*.L3'. 9
- 7. U.S. IwPaCT TEMP.
6
- 9. U.S.
IMPACT TE=P.
aDE6.F3 tCEG.Fg
- s. U.S. IMPACT f*E*
(
(FI*L#*3 be-
-I
- 13. u.5. I= Pact EhG.
IFI.Lt.1 J.'j
- 9. U.S. mICt a 5 I
- F,'
- p
.* g g
- 11. U.S. alt
- -a.
tm518504Tt14.tl E'
]
[. J
[ "- ]
['-J
[" 1 E' J E '
.]
- 0. CHEMISTR,
~
5 J
E ~ 58 J E
'l
[ AL J.
E l.
. E l Cu 54
%I 5
- r. costa Data 9
E. B0GE STEE55 a-CR-OP tt800 RPal (IN.8 L-
-- l (14.3 SDEEC 8C8*t 5'EE55 l
- 2. a-ca-05 t0ste5 PEE 08 I.
1.
19~0 tm5tl J
- 2. 216 412:1e im515 All Bracketed Data Subject to G. Sta.!:E ata 9
@ProprietaryCodes,b,c.e I. ODE 8 IE*P. PEist TE*P. Hua 40EG.F3 b,c.e
- 2. E 511-a f E 3 -s e Ost3T (1% shen L-Calculated keyway crack size till 3.
inspection time.
Ratio of calculated crack to 4.
critical Grock size.
e 9
4 T
o e
w-*
M Of 3C 10 e : 3080100905 g i L# fu'61%E DISC IhF00patt3%
t e 1H ea;PEarti.
C. paler 1st L
1 ""
7 watteint pe0PERTIES tauBB ft s.
7
- a. Usti gGE,yt:rg;st!;%
- 1. TYoE 85Ill
- 1. cu1L;1 4 e.CL*
'O
(*I%.
T.S.
EPol"45 FALL]
I. T.5.
44513
- pat 5.
f.5.
Im519
- 2. U.T.S.
tm514 Casetzt tt;t r $ m2
- 2. 1. ppt 1ER:
{
%II 3
4 U.I.S.
(55tg
- 3. ELO4G8?I34 CUSIC*Eo:
sattl*CSE OEE 1
- 5. ELC%t;alLQ4
- s. e.a.
5.
0Eaft;%
- 6. a.a.
+
- 5. FsTI LUE3*rt
- h. LPs
- CJ 1
F. FATT IDE G.F t
- 6. R.T. 1*PACitFI S.g
- 7. U.S.
[* PACT TE
- 6. OtSte
- 1. IEST %0.
t%tS!c
- 8. 9.T. 1*PacitFT.L).1 I
83I0*II
- 9. u.5. I* Pact TE*P.
- 8. U*S. 1*PaCf Eh6 60EG.F 8 III*lI*I IC. U.S. I=PaCI E%$.
l
,,p,yg (Fi.LS.4
- 1. U.S. aICLES,,
- 11. U.S. mIC(E51eSQRit1% ll
]
-]
. ]
]
h
]
t D. CHE*IStaf j
5 Cg
(
)
(~)
( 53 ')
(~ 54 )
(
SL*
NI AS F. CeaCa Onts i.
l f
E. BOSE Sf4Ess (Ih.)
- 1. 4-CA-OP tl80C aFMI 58EEC 487'l 5T4E55 (Ihl L
y a-CA-05 tavta5 PEE 05 2.
1.
1BGC td5ft
- 2. 21c0 412314 (m518 All Bracketed Data Subject to 3* 5EEbICE :aYa
@ProprietaryCodes,bc.e 3*E2 1E1P. "!!
TE*P. nut (CES.F8 b.c.e i
E 511*s tEJ =a s a'L 1.
/DT II%/H88 2.
Calculated keyway crack size till 3.
inspection time.
Ratio of calculated crack to 4.
critical crack site.
6 i
9 e
4
de 2 Er O F 3 (.
5 10 s : DE801C0905
,i Tu 81mE DISC 14F0e=afloh e
L*
83'I" 8 C. =aTEttal scopI4flE5
- 9. wa!E4Iat #40PERTIES tubts rg F
S
- s. 9 11 I;tsygr:ge:ICN g, g,pg e451st 1
- 1. tutLCI% i s* Ce 4:
t=l%. v.5.
2.
JN;l
.a.diat CLirF5 e'
- f. 5,pPtgte-8;satt,gpa % 5 fall'
- 3. v.5. t*5Il a4518
- 3. CustC*E8:
i:a6'1=C=E ;EE
- 3. v.5.
tustn..
- 2. U.t.5.
I
- o. u.t.5.
im513
- 3. ELO%G4II3'
- e. a.a.
- L'8
- 5. ELc4Ga T10%
- 5. Fatt 50E3.F8
- 5. scCattes
- 08 1=PACitFT. 5.,
- 6. o.a.
- 6. k.T.
6.
LI5Cs
- 7. raTT E DE s.F s
- 7. TEST %;.
T%15?i
- 8. 9.T. 14P8C IFinL3 3
- 7. U.S. Impact TEM IDE6.F8
- 9. U.S. 1* PAC TE=P.
GCEG.F 3
- s. U.S. I' Pati EhG.
~ -
tF1.LB.
- 10. U.S.
IMPaC1 EhG,.
- 9. u.5. aIC
-c-(Ft.LS.
("5I
- 11. U.S. mICtutle50ettIt.ll 6'
[
J
[ "' ]
[ s]
["
]
E :]
["* - ]
L'
]
D. CHE=I5fav
[
]
[ as ]
fa -]
[ su 1
[ AL l L
1
[5 '3 Cu 41 F. C4ata cafa E. 903E 57:E55
- 3. a-CR-CP (153G EPPI (1%.I 5'EE3 t**=3 star 55
)
814.5 g
I.
1800 taill
- 2. a-CR-05 tovCR5 PEE 05
- 2. 21c; 812319 tu518 L
G.
5E*6fCf C a t 's All Bracketed Data Subject to hProprietaryCodes,b,c.e
- 1. CDE*.
TE*p. =5 tat TE**. cu6 80EG.F3 i } b,c.e
- 2. E511=st!; =an ;asti (IApne i
Calculated keyway crack size till
~',
3.
inspection time.
4.
Ratio of calculated crack to critical crack size.
r i
24 o f 26 10 e : OC801C39C5 i ;
L# Tw#3I%E DISC 1%FC4=af1C%
- a..s:t. !CC%IIF1 -
- 3. ware 9 tat co0PE4 TIE 5 t at,i s C. =alEelat =s0PEaflE5 4*I"8 1.
? IL C I* G f.* * *
~
1.
frof r
7 TE t=tA. v.5.
L J t < 51 2.
.%;T
... 38 Ct;rri a2
- 2. g,pptgre
=lighg rpplst 3.
- .5 f C =E **
i..'
'il "Ei 3.
v.5.
4
.:s 4
U.t.5.
42513
- 1. v.5.
ta513 5.
.~CatIC%
3"*
- 5. Etc%GAfich
- 2. u.T.S. tESIB 4.
5Ce
-.J e.
- .A.
1 6.
o.4
- 3. [Lo=GaTID=
- 7. fEST %C.
- 7. raTT EDEG.FB
- 5. FATI 10EG.Fl
- 3. c.T.
l=psCitFT.LS.I
- 6. R.T. !=PACTtFt.LE.1 9.
U.S. I"PACI TE*P.
- 7. U.S. I" PACT TE"P*
(DEG.F
- 10. U.S. InP ACI EsG.
t DE G.F I
- 3. U.S. IPPACI Ekb.
EF1.LS.)
- 11. p.5. mIC 8FI.LO*'
.,?
- 9. u.s. mIC, (K S I
- 5 L R T.f l.4. I I D. C-E=ISTRT
(
]
h
).
{
]
{
-]
{
]
{
_.]
{
'_ ^ )
%I A5 E
l E
l
[ 58 ]
E_]
E l-
[ Cu ], - L
-]
54 AL 5
E. SC;E STDE55 52EEG ges.
- i35 F. CasC= DATA 1.
19C0
=. 8
~
2.
- 160 412'.18
- 't
- 2. a-CR-05.t oven 5 PEED s 114. 8
- 3. a.Co-OP tla3C 2P=I (IN.)
- 3. SE:a:CE Cafa All Pracketed Data Subject to 1.
- 2E9 T E * *. *I '.. * - =2 auS (CEG.Fs P'.k'C'*
- 7 d***
2.
ESTI= ATE 3 =sa - -
- s ; *s/.0 3 3.
Calculated keyway crack size till inspection time.
4.
Ratio of calculated crack to critical crack size.
l 1
l
4 30 0F 34 b
i 10 s = ocoolC0305 LP Tup 3thi DISC 1%FCamaT1cg se!M Pe08Es.1E5 C. msTEntat g,28tE4 tat 8400ESTIE5 twaan
]
!a
- 8. U%lf {
- E *. T !F l( A T;;*.
1.
o 9
Tr E 1:451st
- 1. ru1L;1\\0 5,00 89ts. v.5.
cg e tE ** EP G l %5 f aLL =
- 1. v.5.
4*518 Ct1FF5 s2
- 2. 5. ppt 3Ea:
445I8
- 2. u.T.S.
- If LA,di.st 3.
v.5.
ta5is' a
- 2. y*d 5T c-E c :
- 3. E.Lc45a T 104 Es fl :st EE e. u. T.S. esil
!. s
?
.a.
5.. E.te.ssa f log
- . L*'aTICA
.. oist.
- 7. FaTT IDEE.Fl
- 5. FsTT egQjFlat.5 4
SCd
- 5. LCC
- 6. S.I.
I
,p*
S. D.T. IPPACTtFT,LS.)
- f. U.S. I
4 7.
TEST %0.
% 12*1
- 9. U.S.
IMPACT TEMP.
I
- s. U.S. IntP
- 10. U.S. 1" 5.
8
~(
(Ft.Lt.l
- 9. U.S. KICIK51$50a f t1*.8 8 11 13.5. KICtK51*50eiE14.I3 w
{
}
{
}
{
~]
']
(
)
(
]
{_
O. CoeEMISTsv
+
~
E ]
[ ]
["
]
[ '" 3 E ]
[ '" J E ' 9.] -
~
.j F. CaaC4 ORTa
~-
i E. EC4E ST:ESS (18CO RPMI EIN.8 5'EE3 (88*3 5T3155 a-CR-OP
, ~
- 1. a-CR-05 (CVERSPEEDn (14.1 L
1.
ISOC an513 2.
- 2. 2160 412;ta ta513 i
3..SE*vl;E Otis All Bracketed Data subject to i
{
hProprietaryCodes,b,c.e l
7 1.
03E*.
TE98
- ETaL TE*P. nu& 10EG.F 8
- 2. EST1= ATE 3 was ;a/DT t I s s e.4 8 f - b,c.e
(
Calculated keyway crack size till L
2nspection time.
Ratio of calculated crack to 4.
critical crack size.
m
==i
v 7.
3 f 0 F.34 10 5 0040103906 1
4 Tu tt%E Otst INFot*ATIOk PR3 pes.li v
.3 4 o
91 LP C. watEstat
=arEatst PeopE4f1Es twoBI 15 o.
A. t%!! ;3E%11FICatI3%
- 3. t,ag ta51st a
y, 5,,ts. v.5.
PLIE4:
13 sat EP P M5 f 4Lt. '9
- 1. v.5. t*5I8
- 1. Bu!LLIM 3.CC.
t=
8 dill
- 3. v.5. 6851s
- 2. U.t.5
- a.viar Ct; rig.2 4.
u.f.5.
t a s!.
- 3. EL0%3aT10%
- 2. cNIT Ea.tI=;3E CLE
- 3. CusfG=E3:
- 5. EL34Gst10%
- 5. Fati.80E3.Flt=psCTtF1 t.
8.a.
y.3 -
4 Los 3E 4
- 5. LCCatt;%
6
- .a.
1
- r. FAFI tCE3.Fl
.6. W.I.
TE TE 57 %
T.ti!;
J.
4.7. 1*PACitF1.Lt.8
- 1. U.S. I=PsCT I5C' C..
IDI 6 *E I 6.
7.
' 8I!*lgh6.
- 9. U.S.
I* PACT TE=P.
I= PACT
( DE G'.F l*
- 8. U.S.
L_.
- 10. U.S. I" PACT EA3.?
- g. u.5. SIC sitta.lt (FT.LB.)
'j.
I"5
- 11. d.5. dICtm 51*50eil14. l l-
- f.. J F.
E
[:
]
F., ]
[Si ]
[,,
]
[ c.. ]
O. CME *1 STET s.-
C.
b
-]
L - ']
]
(~.t ]
]
I-:-
5 u
a5 F. CRACE OSTA
- 1. E-Co-CP (1800 BPal IIA.8 E. E00E 574E55 5*EEC 488-9 51cE55 514.5 g
ta519
- 2. a.Ce-05 towCR5 PEE 05
=
1.
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