ML20044B830

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Special Rept:On 930131,discovered Invalid Failure of DG Due to High Crankcase Pressure Trip.Caused by Failure of Calcon Sensor.Failed Sensor Will Be Replaced During Refueling Outage
ML20044B830
Person / Time
Site: Catawba Duke Energy icon.png
Issue date: 03/02/1993
From: Tuckman M
DUKE POWER CO.
To:
NRC OFFICE OF INFORMATION RESOURCES MANAGEMENT (IRM)
References
NUDOCS 9303100058
Download: ML20044B830 (2)


Text

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DEke freer Company

  • Catawtra Nu&ct Generatwn Department fh
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.*O Office (503)S31-3426 Dx DtJtWPOWER March 2, 1993 U.

S. Nuclear Regulatory Commission ATTN:

Document Control Desk Washington, DC 20555

Subject:

Catawba Nuclear Station, Unit 2 Docket No. 50-414 Special Report Invalid Failure of Diesel Generator 2B Pursuant to Technical Specification

4. 8.1.1. 3, and 6.9.2, find attached a Special Report concerning the Unit'2 Diesel Generator (DG 2B) invalid failure that occurred on January 31, 1993.

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Very truly yours,

, S*

W MS Tuckman KEN \\2B.DG Attachment xc:

SD Ebneter Regional Administrator, Region II WT Orders Senior Resident Inspector RE Martin, ONRR 000100 3,9y y noatooose no r

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f SPECIAL REPORT l

CATAWBA NUCLEAR STATION

'I DIESEL GENERATOR 2B INVALID FAILURE DUE TO HIGH CRANKCASE PRESSURE An invalid failure of Diesel Generator (DG) 2B occurred on January 31, 1993 at 1145 (Start #709) due to a high crankcase pressure i

trip.

This was caused by e failure of the Calcon sensor that is utilized in this application.

Unit 2 we.s in Mode 4 in 2EOC5 refueling outage at the time this failure occurred.

Operations (OPS) was in the process of running DG 2B for the Technical Specification (TS) required 24 hour2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> run.

There have been 0 valid f ailures in the last 20 valid tests and 1 valid failure in the last 100 valid tests.

DG 2B remains on a monthly operability test schedule in accordance with TS 4.8.1.1.2 Table 4.8-1.

There is no unavailability time associated with this failure.

DG 2B was manually started on January 31, 1993 for the TS required l

24 hour2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> run.

After running approximately 60 seconds, the engine tripped.

All of the Group II trip annunciators were received at the time the trip occurred.

The engine was then given an emergency i

start signal by Instrument and Electrical (IAE) personnel to allow time for a Component Engineering (CE) engineer to observe the various indications without the engine tripping. After this start, it was immediately noticed that the instrument air pressure j

required to operate the pneumatic shutdown logic system was not rising to its required 60 psi, which was indicative of an air leak somewhere in the system.

Approximately 1 minute into this run, all the Group II trip annunciators were received.

There have recently i

been problems with several crankcase pressure sensor failures on this engine, so this was immediately checked.

The crankcase pressure sensor was found to have air blowing out of its vent port during this time when it should have been blocked.

Crankcase pressure, as read on the panel mancmeter, did not indicate any adverse pressure.

After this was determine to be the cause, CE requested that the emergency start be reset so the engine would shutdown as designed.

Since there was no replacement sensor in stock, it was decided that a Temporary Station Modification (TSM) which would bypass the crankcase pressure trip would be the quickest and most reliable method to enable the 24 hour2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> run to continue.

The tubing vent line to this sensor was plugged in the engine control panel per the TSM.

OPS initiated an increased surveillance on the crankcase pressure l

manometer during the diesel run so that any crankcase pressure increase could be evaluated and the engine manually tripped as necessary.

The engine was then restarted and the 24 hour2.777778e-4 days <br />0.00667 hours <br />3.968254e-5 weeks <br />9.132e-6 months <br /> run was completed.

The failed sensor is still mounted in place on 2B DG engine.

It will be removed during the present 2EOC5 refueling outage for the implementation of a Nuclear Station Modification which will replace the pneumatic shutdown logic system with an electrical equivalent system.

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