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AS TO DATE : January 31, 2013ENGINE MODEL : CFM56-3C-1 TOTAL ENGINE TIME : 53176.71SERIAL NUMBER : 721644 TOTAL ENGINE CYCLES : 40229

SB REFERENCE ISSUENUMBER EFFECT. DATE HOURS CYCLES

1 86-08-05 R1 SB 72-205 R5 7-Jul-86 CFM56-3/3BINSPECTION OF RDS OIL DISTRIBUTOR P/N:335-305-800-0-1 AND SPIROLOCK P/N:649-363-137-0

N/A

SB Torque check increases from 50 inch-lbs to 100 inch- lbs is required prior to inspection for the pupose of this AD

N/A to TGB Installed : PN 335-300-011-0. Ref. GE Shop Visit Report dated on October 18, 2010.

2 89-13-51 737-71-1203 29-Jan-97FAN DISK PN:335-04-511-0 & FAN BLADES PNs: 9527M99P08P09& 1285M39P01 REMOVAL.(OPERATED AT RESTRICTED CFM56-3C-1 THRUST)

S SUPERSEDED SUPERSEDED BY AD 96-25-11

3 89-17-04 28-Jan-98

INSPECT FORWARD SUMP MCD AND REMOVED THE AFFECTED NO.3 BEARING PN:9732M10P12 SNs FAFDxxxx or FAFExxxx) PN: 9732M10P18, or 1376M76P12 FROM SERVICE

S SUPERSEDED SUPERSEDED BY AD 89-23-06 R1

2 89-23-06 R1 SB 72-530 R3 28-Jan-98 CFM56-2,3,3B, 3C & -5

NO.3 BEARING MCD INSPECTION MCD INSPECTION PROGRAM REPLACEMENT OF NO.3 OR INSPECTION OF MCD ACC. TO P/N AND S/N

N/A

Inspect MCD within the next 50 hrs TIS after the EOD of this AD. E-inspect at interval not to exceed 50 hrs TIS since last inspection or remove the NO.3 bearing PN: 9732M10P18 & PN: 1362M76P02 from service at the next shop visit or before 31 Jan 1998 whichever come first.

No.3 Bearing Installed : PN 9340M90P06 SN FAFP5695. Ref. GE Shop Visit Report dated on October 18, 2010.

3 90-20-13 72-494 R2 14-Oct-90 CFM56-3B, -3C

TO PREVENT FAN BLADE FAILURE, IFSD, AND SEVERE ENGINE DAMAGE BY INCORPORATING THE FAN BLADE DAMPERS PN: 335-105-305-0, AXIAL STOPS PN: 335-105-201-0, AND BOLTS PN: J815P056A, TO THE FAN MODULE ASSEMBLY.

N/A

Modify the fan module by installing the fan blade dampers, axial stops and bolts within 60 days from the EOD of this AD. (EOD: 14 Oct 1990)

Fan blade P/N 1590M21P01, 1663M24P01, 1663M24P02 & 1663M24P04 installed not affected. Ref. GE Shop Visit Report dated on October 18, 2010.

4 91-02-10 SB 72-450 11-Feb-91 CFM56-3, 3B, 3C

INSTALLATION OF NEW SPLITTER FAIRING, STAGE 1 VANE ASSY, & NEW CENTERING SHROUD T

If a later revision of the Service Bulletin is used for complying with this FAA-AD recorded

Previously Complied, perform in accordance with SB 72-450. Ref. GE Shop Visit Report dated on October 18, 2010.

5 91-02-10 72-462 R1 11-Feb-91 CFM56-3, 3B, 3C

INSTALL THE 12 DOOR VARIABLE BYPASS VALVE (VBV) CONFIGURATION T

If a later revision of the Service Bulletin is used for complying with this FAA-AD recorded

Previously Complied, perform in accordance with SB 72-462. Ref. GE Shop Visit Report dated on October 18, 2010.

6 96-18-16 SB 72-695 9-Dec-96CFM56-2, 2A,

2B, 3, 3B, 3C & 5

TO PREVENT LCF FAILURE OF LPT ROTOR (LPTR) STUB SHAFT AND CONICAL SUPPORT, WHICH COULD RESULT IN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

N/A

For CFM56-3,-3B,-3C, reidentify the LPTR stub shaft, PN: 301-330-618-0/619-0/623-0/624-0, with S/N listed in Table 2 of SB72-695. To be carried out at next piece-part exposure after the EOD of this AD but not to exceed a total thrust rating life cycles of 20,000 (Cat.A)/11.400 (Cat.B)/7,900 (Cat.C). (EOD: 29 Jan 1997)

Both of Conical Support Installed :PN 305-056-116-0 Stub Shaft Installed : PN 301-330-626-0. Ref. GE Shop Visit Report dated on October 18, 2010.

REMARKSMETHOD OF COMPLIANCESTATUS INTERVALLAST ACCOMPLISHED

AIRWOTHINESS DIRECTIVE COMPLIANCE STATUSENGINE

FAA AD NO.NO DESCRIPTIONAPPLICABILITY NEXT DUE REMAIN

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7 96-25-11 72-543 R8 29-Jan-97 CFM56 3B2, 3C1

TO PREVENT FAN BLADE FAILURE BY REMOVING AFFECTED FAN DISK & BLADE SET OPERATED AT UNRESTRICTED CFM56-3C-1 THRUST LEVELS.

N/A N/A N/A N/A

To replace affected Fan Disk P/N 335-014-511-0 & Fan Blades P/N 9527M99P08/09/11 or 1285M3P01 and/or listing of affected CFM56-3B2 Engines which have operated at unrestricted CFM56-3C-1 Thrust Levels include operation at either more than CFM56-3B2 max. Takeoff thrust above 5000-ft pressure altitude or more than CFM56-3B2 max. Continuous or max Climb thrust above 10000 ft pressure altitude.

Fan disk P/N installed 335-014-511-0, fan blade installed not affected by this AD. Ref. GE Shop Visit Report dated on October 18, 2010.

8 97-08-01 CFMI-TP SM.8 23-Jun-97 CFM56-3, -3B, 3C

TO PREVENT A LACF FAILURE OF THE FAN DISK, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE

T

Remove the Fan Disk operated under the Cat C Thurst rating life before the max life limit of 20100 cycles or re-calculate the disk cycle life if -3C engine operated under all Cats A, B & C thrust ratings to Cat C Fan Disk life limit of 20100 cycles per Chapter 05 of ESM CFMI-TP-SM.5

Life limit 20100 cycles at cat C as per published in Chapter 05 of CFM56-3 Engine Shop Manual. Ref. GE Shop Visit Report dated on October 18, 2010.

9 T97-25-51 3-Jun-98 CFM56-3, -3B, 3C

TO PREVENT IFSD DUE TO AN AGB STARTER GEARSHAFT OR TGB INPUT BEVEL GEAR FAILURE S SUPERSEDED SUPERSEDED BY AD 98-10-11

10 98-07-02 SB 72-856 30-Mar-98 CFM56-2,3,3B, 3C

TO PREVENT RUBS BETWEEN THE E OUTER CONE OF THE NO.3 BEARING AFT. STA. AIR SEAL AND STAGE 1-2 HPC SPOOL, WHICH COULD RESULT IN A POTENTIAL UNCONTAINED ENGINE FAILURE.

N/A

Install no.3 Bearing Aft. A/O Seal retention bushings per SB72-855 and/or remove the Stage 1-2 HPC spool PN: 1589M66P02 with a list of affected S/Ns at the next shop visit that 1st confirmed the rub event or whichever come first.

HPCR Stage 1-2 Spool Installed SN GWN00PVP is not affected by this AD. No. 3 Bearing Rear Air/Oil Seal Installed per SB 72-920 P/N 1663M91G04 S/N CTDCLJUV. Ref. GE Shop Visit Report dated on October 18, 2010.

11 98-10-11

SB 72-A861 SB 72-865 SB 72-867 SB 72-863

3-Jun-98 CFM56-3, 3B,3C,5,5B,5C

TO PREVENT IFSD DUE TO AGB STARTER GEARSHIFT, TGB INPUT BEVEL GEAR, TGB OUTPUT BEVEL GEAR, AGB GEARSHAFT CLUSTER SPUR ASSY OR AGB INTERMEDIATE GEAR ASSY FAILURE.

N/A

Check the MCD prior to further flight and/or replace the affected parts/assemblies to serviceable parts per related SB72-

ESN 721644 not affected. Ref. GE Shop Visit Report dated on October 18, 2010.

12 98-12-32 SB 72-843 20-Jul-98 CFM56-2, 2A, 2B, 3, 3B, 3C

TO PREVENT THE POTENTIAL FOR AN UNCONTAINED FAILURE OF THE HPT ROTOR DISK, WHICH COULD RESULT IN AN IFSD, ATO OR DAMAGE TO AIRCRAFT.

N/A ECI for cracks/gouges in HPTR Disk.

HPT Disk Installed : SN GWN083TP not affected by this AD. Ref. GE Shop Visit Report dated on October 18, 2010.

13 98-19-10 SB 72-877 28-Sep-98 CFM56-3, 3B, 3C

TO PREVENT AGB STARTER GEARSHAFT FAILURE, WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A

Replace suspected gearshaft within 350 hrs TIS after the EOD of this AD (EOD: 28 Sept 1998)

AGB SN WB1579 installed is not affected by this AD. Ref. GE Shop Visit Report dated on October 18, 2010.

14 99-08-16 72-541 13-May-99 CFM56-3, 3B, 3C

TO PREVENT CRITICAL LIFE LIMITED ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN UNCONTAINED

S SUPERSEDED Superseded by AD 2000-12-01

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15 2000-05-22 SB 72-922 2-May-00CFM56 -2, 2A,2B, 3, 3B, 3C TO DETECT CRACKS IN THE BOLT HOLES OD HPT FRONT

ROTATING AIR SEALS PN: 1282M72P03 N/A

Perform one time ECI to the listed HPT rotating air seals SNs per SB72-922 and based upon engine model and thrust ratings. (EOD: 2 May 2000)

HPT Front Air Seal Installed : PN 1282M72P05 is not affected by this AD. Ref. GE Shop Visit Report dated on October 18, 2010.

16 2000-12-01 NONE 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

TO PREVENT CRITICAL LIFE LIMITED ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE

S SUPERSEDED Superseded by AD 2002-13-03

17 2000-15-01 SB 73-126 R1/ SB 73-A129 2-Oct-00

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5A, 5B, 5C

TO PREVENT FUEL LEAKAGE FROM BETWEEN THE FUEL PUMP FILTER COVER AND GEAR HOUSING WHICH COULD RESULT IN AN ENGINE FIRE AND DAMAGE TO THE AIRPLANE

T

Perform initial/repetitive visual inspection of the fuel pump filter cover helicoil inserts and bolts for damage per SB72-126.; Terminating Action must be done at next engine or fuel pump shop visit whichever occur first but not later than 5 yrs from the EOD of this AD by incorporating a D-bolt filter cover attachment per SB73-A129 or SB 73-125. (EOD: 2 Oct 2000)

SB 73-A129 previously embodied. Ref. GE Shop Visit Report dated on October 18, 2010.

18 2001-04-06 SB 72-854R5 04-Apr-0130-Mar-05

CFM56 -3, 3B,3C

TO PREVENT FAN DISK FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINES FAILURE AND DAMAGE TO THE AIRPLANE.

T 18-Oct-10 51658 38950

Perform one time fan disk dovetail wear measurement per SB72-854R2. If required, perform a local ultrasonic inspection. (EOD: 4 April 2001). CAUTION: After the effective date of this AD, the following lubricants are no longer approved for use on the CFM56-3 series engine : Sandstorm 27A, ZIP D5460, Surf-Kote A1625, Tiolube 70, and Tiolube 75/75.

Carried out at GE Shop Visit. Ref. GE Shop Visit Report dated on October 18, 2010.

19 2001-11-05 CN 2002-390-IMP (B) 11-Jun-01

CFM56 -2, 2B,3, 5B, 5C & 7B TO PREVENT NO.4 BEARING FAILURES, WHICH COULD

CAUSE AN ENGINE FAILURE. N/A

Remove the suspected no.4 bearing PN: 305-355-717-0 that has SN listed in Table 1 of this AD not later than 1 Jul 2001. CAUTION: After the effective date of this AD , do not install any engine that has a No.4 bearing with serial number listed in the Table 1 of this Ad.

No.4 Baering Installed : PN 335-352-303-0 is not affected by this AD. Ref. GE Shop Visit Report dated on October 18, 2010.

20 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

FAN DISK (ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10

DUE AT NEXT PIECE PART

OPPORTUNITY

FPI, Disk Bore and Dovetail Eddy Current Inspection (ECI). Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

Complied previously at GE Shop Visit. Ref. GE Shop Visit Report dated on October 18, 2010.

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21 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

FAN SHAFT(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY

Magnetic Particle Inspection (MPI). Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.


22 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPT DISK(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.


23 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPT FRONT ROTATING AIRSEAL(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY



24 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPC STAGE 1-2 SPOOL(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY



25 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPC STAGE 3 DISK(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY



26 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPC STAGE 4-9 SPOOL(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY



27 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPC FRONT SHAFT(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY

FPI, Disk Bore and Dovetail Eddy Current Inspection (ECI). Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.


28 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPC REAR (CDP) AIRSEAL(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY

FPI, Seal Bore ECI and Bolt holes ECI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.


29 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

LPT STAGE 1 DISK(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY



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30 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B


R 18-Oct-10


OPPORTUNITY



31 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B


R 18-Oct-10


OPPORTUNITY



32 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B


R 18-Oct-10


OPPORTUNITY



33 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

LPT ROTOR SUPPORT(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY



34 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

LPT SHAFTALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY



35 2002-13-03 CN 2002-390-IMP (B) 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

LPT STUB SHAFTALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 18-Oct-10


OPPORTUNITY



36 2004-10-1373-A129 73-087

73-0120 R524-Jun-04

CFM56 -2-C, -3Series & -5

Series.

TO PREVENT MAIN FUEL PUMP BEARING FAILURES RESULTING IN FUEL NOZZLE CLOGGING, LOW PRESSURE TURBINE (LPT) CASE BURN-THROUGH, AND DAMAGE TO THE AIRPLANE.

N/A

Remove the affected MFP for incorporating of SB73-120R5 at next engine shop visit, or main fule pump repair shop, whichever is earlier but not later than 1 Jan 2007.

N/A to fuel pump installed. Ref. GE Shop Visit Report dated on October 18, 2010.

37 2006-26-01 73-141 1-Mar-07

CFM56 -2-C, -3Series, -5Series, -7B

Series.

TO PREVENT THE LOSS OF ENGINE THRUST THAT COULD RESULT IN LOSS OF CONTROL DURING TAKEOFF OR LANDING BY REPLACING THE DEFECTIVE/AFFECTED FUEL FILTER ELEMENTS

N/A

Remove the affected fuel filter, Western Filters PN: WF337881 or WF337017 and PTI Technologies PN: 7595983-101 or 7588133 and replace with filter that has PN not listed in this AD, but not later yahn 03 Jan 2007.

N/A To fuel filter PN installed.Ref. GE Shop Visit Report dated on October 18, 2010.

38 2009-11-02 23-Jun-09CFM56 -2, -3,-5A,-5B,-5C,-

7B .

TO PREVENT CRACKING OF THE HPC 4-9 SPOOL WHICH COULD RESULT IN POSSIBLE UNCONTAINED FAILURE OF THE SPOOL AND DAMAGE TO THE AIRPLANE

N/A

Remove HPC 4-9 spools from service that have a P/N and S/N listed in Table 1of this AD before accumulating 8,900 cycles-since -repair at PTLLC or within 1,100 cycles from the effective date of this AD.

N/A to HPC 4-9 spoll PN 1588M89G03 and S/N GWN03N6E installed. Ref. GE Shop Visit Report dated on October 18, 2010.

eng2 (721644) 072112-072912_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 08/13/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 08/13/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 071912 * . G . F X 2 . -999.99 110 42 0 072112 * . G . F X 2 . -999.99 100 40 0 072112 * . G . F X 2 . -999.99 95 40 0 072212 * . G . F X 2 . -999.99 90 46 0 072212 * . G . F X 2 . -999.99 100 40 0 072212 * . G . F X 2 . -999.99 105 40 0 072212 * . G . F X 2 . -999.99 120 38 0 072312 * . G . F X 2 . -999.99 100 42 0 072312 * . G . F X 2 . -999.99 105 43 0 072312 * . G . F X 2 . -999.99 105 43 0 072312 * . G . F X 2 . -999.99 120 42 1 072412 * . G . F X 2 . -999.99 97 46 1 072412 * . G . F X 2 . -999.99 110 42 0 072412 * . G . F X 2 . -999.99 120 43 0 072412 * . G . F X 2 . -999.99 100 39 0 072512 * . G . F X 2 . -999.99 110 42 0 072512 * . G . F X 2 . -999.99 105 43 0 072512 * . G . F X 2 . -999.99 107 47 0 072612 * . G . F X 2 . -999.99 105 43 0 072612 * . G . F X 2 . -999.99 110 40 0 072612 * . G . F X 2 . -999.99 105 40 0 072612 * . G . F X 2 . -999.99 105 42 0 072712 * . G . F X 2 . -999.99 110 42 0 072712 * . G . F X 2 . -999.99 100 42 0 072712 * . G . F X 2 . -999.99 105 42 0 072712 * . G . F X 2 . -999.99 110 42 0 072712 * . G . F X 2 . -999.99 105 40 0 072712 * . G . F X 2 . -999.99 105 42 0 072712 * . G . F X 2 . -999.99 105 44 0 072712 * . G . F X 2 . -999.99 100 40 0 072812 * . G . F X 2 . -999.99 100 40 0 072812 * . G . F X 2 . -999.99 110 40 0 072812 * . G . F X 2 . -999.99 101 42 0 072812 * . G . F X 2 . -999.99 105 40 0 072912 * . G . F X 2 . -999.99 110 45 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 072712 * . G . F X 2 . -999.99 0 072712 * . G . F X 2 . -999.99 0 072712 * . G . F X 2 . -999.99 0 072712 * . G . F X 2 . -999.99 0 072712 * . G . F X 2 . -999.99 0 072812 * . G . F X 2 . -999.99 0 072812 * . G . F X 2 . -999.99 0 072812 * . G . F X 2 . -999.99 0 072812 * . G . F X 2 . -999.99 0 072912 * . G . F X 2 . -999.99 0

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eng2 073012-080712_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 08/13/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 08/13/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 073012 * . G . F X 2 . -999.99 100 42 0 073012 * . G . F X 2 . -999.99 100 43 0 073012 * . G . F X 2 . -999.99 105 42 0 073012 * . G . F X 2 . -999.99 100 42 0 073012 * . G . F X 2 . -999.99 105 42 0 073112 * . G . F X 2 . -999.99 110 40 0 073112 * . G . F X 2 . -999.99 110 40 1 080112 * . G . F X 2 . -999.99 100 43 0 080112 * . G . F X 2 . -999.99 100 40 0 080112 * . G . F X 2 . -999.99 100 43 0 080112 * . G . F X 2 . -999.99 100 42 0 080112 * . G . F X 2 . -999.99 115 42 0 080112 * . G . F X 2 . -999.99 100 47 0 080112 * . G . F X 2 . -999.99 105 40 0 080212 * . G . F X 2 . -999.99 95 40 0 080212 * . G . F X 2 . -999.99 110 42 0 080212 * . G . F X 2 . -999.99 120 42 0 080212 * . G . F X 2 . -999.99 103 41 0 080312 * . G . F X 2 . -999.99 100 40 0 080312 * . G . F X 2 . -999.99 99 46 0 080312 * . G . F X 2 . -999.99 110 46 0 080412 * . G . F X 2 . -999.99 105 40 0 080412 * . G . F X 2 . -999.99 105 40 1 080512 * . G . F X 2 . -999.99 100 42 0 080512 * . G . F X 2 . -999.99 105 40 0 080612 * . G . F X 2 . -999.99 110 42 0 080612 * . G . F X 2 . -999.99 110 42 0 080612 * . G . F X 2 . -999.99 100 42 0 080612 * . G . F X 2 . -999.99 110 40 0 080712 * . G . F X 2 . -999.99 105 42 0 080712 * . G . F X 2 . -999.99 110 40 0 080712 * . G . F X 2 . -999.99 100 42 0 080712 * . G . F X 2 . -999.99 100 45 0 080712 * . G . F X 2 . -999.99 110 42 0 080712 * . G . F X 2 . -999.99 105 43 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 080612 * . G . F X 2 . -999.99 0 080612 * . G F . X 2 . -999.99 0 080612 * . G . F X 2 . -999.99 0 080612 * . G . F X 2 . -999.99 0 080712 * . G . F X 2 . -999.99 0 080712 * . G . F X 2 . -999.99 0 080712 * . G . F X 2 . -999.99 0 080712 * . G . F X 2 . -999.99 0 080712 * . G . F X 2 . -999.99 0 080712 * . G . F X 2 . -999.99 0

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eng2 080812-081412_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 08/15/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 08/15/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 080812 * . G . F X 2 . -999.99 105 43 0 080812 * . G . F X 2 . -999.99 104 46 0 080912 * . G . F X 2 . -999.99 100 42 0 080912 * . G . F X 2 . -999.99 105 43 0 080912 * . G . F X 2 . -999.99 105 46 1 080912 * . G . F X 2 . -999.99 110 42 0 080912 * . G . F X 2 . -999.99 110 42 1 080912 * . G . F X 2 . -999.99 105 42 0 081012 * . G . F X 2 . -999.99 110 39 0 081012 * . G . F X 2 . -999.99 105 47 0 081012 * . G . F X 2 . -999.99 103 43 0 081012 * . G . F X 2 . -999.99 103 42 0 081012 * . G . F X 2 . -999.99 101 42 0 081012 * . G . F X 2 . -999.99 102 42 0 081012 * . G . F X 2 . -999.99 100 46 0 081112 * . G . F X 2 . -999.99 100 45 0 081112 * . G . F X 2 . -999.99 110 46 0 081112 * . G . F X 2 . -999.99 100 43 0 081112 * . G . F X 2 . -999.99 110 42 0 081212 * . G . F X 2 . -999.99 105 42 0 081212 * . G . F X 2 . -999.99 100 44 0 081212 * . G . F X 2 . -999.99 100 43 0 081212 * . G . F X 2 . -999.99 105 40 0 081212 * . G . F X 2 . -999.99 105 48 0 081312 * . G . F X 2 . -999.99 110 40 0 081312 * . G . F X 2 . -999.99 110 40 0 081312 * . G . F X 2 . -999.99 110 42 0 081312 * . G . F X 2 . -999.99 120 45 0 081312 * . G . F X 2 . -999.99 105 38 0 081412 * . G . F X 2 . -999.99 105 44 0 081412 * . G . F X 2 . -999.99 115 46 0 081412 * . G . F X 2 . -999.99 105 45 0 081412 * . G . F X 2 . -999.99 120 46 1 081412 * . G . F X 2 . -999.99 110 42 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 081312 * . G . F X 2 . -999.99 0 081312 * . G . F X 2 . -999.99 0 081312 * . G .F X 2 . -999.99 0 081312 * . G F X 2 . -999.99 0 081312 * . G . F X 2 . -999.99 0 081412 * . G . F X 2 . -999.99 0 081412 * . G . F X 2 . -999.99 0 081412 * . G . F X 2 . -999.99 0 081412 * . G . F X 2 . -999.99 1 081412 * . G . F X 2 . -999.99 0

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eng2 081512-082212_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 08/23/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 08/23/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 081512 * . G . F X 2 . -999.99 100 41 0 081512 * . G . F X 2 . -999.99 120 42 0 081612 * . G . F X 2 . -999.99 110 38 0 081612 * . G . F X 2 . -999.99 110 40 0 081612 * . G . F X 2 . -999.99 110 42 0 081612 * . G . F X 2 . -999.99 108 48 1 081612 * . G . F X 2 . -999.99 105 48 0 081712 * . G . F X 2 . -999.99 110 40 0 081712 * . G . F X 2 . -999.99 102 39 0 081712 * . G . F X 2 . -999.99 110 40 0 081812 * . G . F X 2 . -999.99 105 40 0 081812 * . G . F X 2 . -999.99 102 44 0 081912 * . G . F X 2 . -999.99 100 48 0 081912 * . G . F X 2 . -999.99 100 40 0 081912 * . G . F X 2 . -999.99 110 44 0 081912 * . G . F X 2 . -999.99 105 41 0 081912 * . G . F X 2 . -999.99 110 40 1 082012 * . G . F X 2 . -999.99 103 42 0 082012 * . G . F X 2 . -999.99 110 40 0 082012 * . G . F X 2 . -999.99 102 50 1 082012 * . G . F X 2 . -999.99 102 40 0 082012 * . G . F X 2 . -999.99 105 40 0 082112 * . G . F X 2 . -999.99 108 38 1 082112 * . G . F X 2 . -999.99 120 47 0 082112 * . G . F X 2 . -999.99 100 43 0 082112 * . G . F X 2 . -999.99 110 42 0 082212 * . G . F X 2 . -999.99 100 40 0 082212 * . G . F X 2 . -999.99 100 42 0 082212 * . G . F X 2 . -999.99 110 44 0 082212 * . G . F X 2 . -999.99 90 40 0 082212 * . G . F X 2 . -999.99 105 44 1 082212 * . G . F X 2 . -999.99 105 45 0 082212 * . G . F X 2 . -999.99 105 45 0 082212 * . G . F X 2 . -999.99 110 41 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 082112 * . G . +F X 2 . -999.99 0 082112 * . G F. X 2 . -999.99 0 082212 * . G .F X 2 . -999.99 0 082212 * . G . F X 2 . -999.99 0 082212 * . G . F X 2 . -999.99 0 082212 * . G . F X 2 . -999.99 0 082212 * . G . F X 2 . -999.99 1 082212 * . G . F X 2 . -999.99 0 082212 * . G -F . X 2 . -999.99 0 082212 * . G . F X 2 . -999.99 0

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eng2 082312-083112_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 09/11/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 09/11/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 082312 * . G . F X 2 . -999.99 100 43 0 082312 * . G . F X 2 . -999.99 110 40 0 082412 * . G . F X 2 . -999.99 98 39 0 082412 * . G . F X 2 . -999.99 110 48 1 082412 * . G . F X 2 . -999.99 110 46 0 082512 * . G . F X 2 . -999.99 115 48 0 082512 * . G . F X 2 . -999.99 120 43 0 082512 * . G . F X 2 . -999.99 110 42 0 082512 * . G . F X 2 . -999.99 105 42 1 082512 * . G . F X 2 . -999.99 105 43 0 082512 * . G . F X 2 . -999.99 110 47 0 082612 * . G . F X 2 . -999.99 110 42 0 082612 * . G . F X 2 . -999.99 110 42 0 082712 * . G . F X 2 . -999.99 102 42 0 082712 * . G . F X 2 . -999.99 110 39 0 082712 * . G . F X 2 . -999.99 105 42 0 082812 * . G . F X 2 . -999.99 120 41 0 082812 * . G . F X 2 . -999.99 110 42 0 082812 * . G . F X 2 . -999.99 115 42 0 082912 * . G . F X 2 . -999.99 110 40 0 082912 * . G . F X 2 . -999.99 110 42 0 082912 * . G . F X 2 . -999.99 110 42 0 082912 * . G . F X 2 . -999.99 110 42 0 082912 * . G . F X 2 . -999.99 110 45 0 082912 * . G . F X 2 . -999.99 105 42 0 082912 * . G . F X 2 . -999.99 110 47 2 083012 * . G . F X 2 . -999.99 110 42 0 083012 * . G . F X 2 . -999.99 102 42 0 083012 * . G . F X 2 . -999.99 100 42 0 083112 * . G . F X 2 . -999.99 110 40 0 083112 * . G . F X 2 . -999.99 100 40 0 083112 * . G . F X 2 . -999.99 110 40 0 083112 * . G .F X 2 . -999.99 110 41 0 083112 * . G . F X 2 . -999.99 102 42 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 082912 * . G F . X 2 . -999.99 0 082912 * . G . +F X 2 . -999.99 2 083012 * . G . F X 2 . -999.99 0 083012 * . G . F X 2 . -999.99 0 083012 * . G F. X 2 . -999.99 0 083112 * . G . F X 2 . -999.99 0 083112 * . G . F X 2 . -999.99 0 083112 * . G F X 2 . -999.99 0 083112 * . G F X 2 . -999.99 0 083112 * . G . F X 2 . -999.99 0

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eng2 090112-090712_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 09/11/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 09/11/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 090112 * . G .F X 2 . -999.99 100 42 0 090112 * . G .F X 2 . -999.99 105 44 0 090112 * . G .F X 2 . -999.99 102 47 0 090212 * . G .F X 2 . -999.99 101 42 0 090212 * . G .F X 2 . -999.99 102 42 0 090212 * . G .F X 2 . -999.99 101 41 0 090212 * . G .F X 2 . -999.99 110 42 0 090212 * . G .F X 2 . -999.99 110 45 1 090212 * . G .F X 2 . -999.99 120 46 0 090312 * . G .F X 2 . -999.99 105 46 0 090312 * . G .F X 2 . -999.99 110 42 0 090312 * . G .F X 2 . -999.99 110 42 0 090312 * . G .F X 2 . -999.99 105 39 0 090312 * . G .F X 2 . -999.99 105 43 0 090312 * . G .F X 2 . -999.99 105 42 1 090412 * . G .F X 2 . -999.99 102 42 1 090412 * . G . F X 2 . -999.99 102 39 0 090412 * . G .F X 2 . -999.99 120 46 2 090412 * . G .F X 2 . -999.99 102 42 1 090412 * . G .F X 2 . -999.99 120 42 1 090412 * . G .F X 2 . -999.99 120 47 0 090512 * . G . F X 2 . -999.99 110 42 1 090512 * . G .F X 2 . -999.99 105 44 0 090512 * . G .F X 2 . -999.99 120 42 1 090512 * . G F X 2 . -999.99 115 42 1 090512 * . G F X 2 . -999.99 110 39 0 090612 * . G F X 2 . -999.99 110 42 0 090612 * . G F X 2 . -999.99 110 42 0 090612 * . G F X 2 . -999.99 105 42 0 090612 * . G F X 2 . -999.99 105 42 0 090712 * . G F X 2 . -999.99 110 40 0 090712 * . G F X 2 . -999.99 100 40 0 090712 * . G .F X 2 . -999.99 120 42 1 090712 * . G F X 2 . -999.99 110 46 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 090512 * . G F . X 2 . -999.99 1 090512 * . G . F X 2 . -999.99 0 090612 * . G F. X 2 . -999.99 0 090612 * . G . F X 2 . -999.99 0 090612 * . G . F X 2 . -999.99 0 090612 * . G F X 2 . -999.99 0 090712 * . G . F X 2 . -999.99 0 090712 * . G . F X 2 . -999.99 0 090712 * . G . F X 2 -999.99 1 090812 * . G F X 2 . -999.99 0

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eng2 090812-091612_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 09/19/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 09/19/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 090112C * . G .F X 2 . -999.99 -5 -5 0 090712 * . G .F X 2 . -999.99 120 42 1 090812 * . G .F X 2 . -999.99 100 44 1 090812 * . G .F X 2 . -999.99 110 47 1 090812 * . G .F X 2 . -999.99 110 46 0 090912 * . G .F X 2 . -999.99 110 45 1 090912 * . G .F X 2 . -999.99 105 40 0 090912 * . G . F X 2 . -999.99 115 38 0 090912 * . G . F X 2 . -999.99 110 40 0 090912 * . G . F X 2 . -999.99 110 42 0 091012 * . G . F X 2 . -999.99 110 42 0 091012 * . G .F X 2 . -999.99 100 42 0 091112 * . G . F X 2 . -999.99 110 42 1 091112 * . G . F X 2 . -999.99 100 40 2 091112 * . G . F X 2 . -999.99 105 45 0 091212 * . G . F X 2 . -999.99 120 42 0 091212 * . G . F X 2 . -999.99 108 42 0 091312 * . G . F X 2 . -999.99 105 42 0 091312 * . G . F X 2 . -999.99 110 42 0 091312 * . G . F X 2 . -999.99 120 47 0 091312 * . G . F X 2 . -999.99 108 39 0 091312 * . G . F X 2 . -999.99 110 42 0 091412 * . G . F X 2 . -999.99 100 40 0 091412 * . G . F X 2 . -999.99 100 43 0 091412 * . G . F X 2 . -999.99 105 39 0 091412 * . G . F X 2 . -999.99 100 42 0 091512 * . G . F X 2 . -999.99 105 45 0 091512 * . G . F X 2 . -999.99 110 42 0 091512 * . G . F X 2 . -999.99 110 38 0 091512 * . G . F X 2 . -999.99 110 40 0 091512 * . G . F X 2 . -999.99 110 42 0 091612 * . G . F X 2 . -999.99 110 38 0 091612 * . G . F X 2 . -999.99 110 42 0 091612 * . G . F X 2 . -999.99 110 45 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 091412 * . G -F . X 2 . -999.99 0 091412 * . G . F X 2 . -999.99 0 091512 * . G . F X 2 . -999.99 0 091512 * . G F. X 2 . -999.99 0 091512 * . G . F X 2 . -999.99 0 091512 * . G . F X 2 . -999.99 0 091512 * . G .F X 2 . -999.99 0 091612 * . G . F X 2 . -999.99 0 091612 * . G . F X 2 . -999.99 0 091612 * . G .F X 2 . -999.99 0

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eng2 091712-092512_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 09/27/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 09/27/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 090112C * . G .F X 2 . -999.99 -5 -5 0 091812 * . G . F X 2 . -999.99 105 44 0 091812 * . G . F X 2 . -999.99 120 42 0 091812 * . G . F X 2 . -999.99 120 42 0 091812 * . G . F X 2 . -999.99 105 38 0 091812 * . G . F X 2 . -999.99 100 43 0 091912 * . G . F X 2 . -999.99 110 42 0 091912 * . G . F X 2 . -999.99 110 40 0 092012 * . G . F X 2 . -999.99 100 40 1 092012 * . G . F X 2 . -999.99 100 40 1 092012 * . G . F X 2 . -999.99 110 42 0 092012 * . G . F X 2 . -999.99 105 42 0 092112 * . G . F X 2 . -999.99 107 47 1 092112 * . G . F X 2 . -999.99 105 45 0 092112 * . G . F X 2 . -999.99 103 47 0 092212 * . G . F X 2 . -999.99 103 39 1 092212 * . G . F X 2 . -999.99 100 42 0 092212 * . G . F X 2 . -999.99 105 42 0 092212 * . G . F X 2 . -999.99 100 40 1 092212 * . G . F X 2 . -999.99 110 39 1 092312 * . G . F X 2 . -999.99 110 42 1 092312 * . G . F X 2 . -999.99 110 40 0 092312 * . G . F X 2 . -999.99 110 42 0 092312 * . G . F X 2 . -999.99 110 41 0 092312 * . G . F X 2 . -999.99 110 42 0 092412 * . G . F X 2 . -999.99 105 47 0 092412 * . G . F X 2 . -999.99 110 40 0 092412 * . G . F X 2 . -999.99 120 42 0 092412 * . G . F X 2 . -999.99 120 45 1 092512 * . G . F X 2 . -999.99 120 42 1 092512 * . G . F X 2 . -999.99 115 41 1 092512 * . G . F X 2 . -999.99 115 43 0 092512 * . G . F X 2 . -999.99 105 40 1 092512 * . G . F X 2 . -999.99 115 42 1 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 092312 * . G . F X 2 . -999.99 0 092412 * . G F . X 2 . -999.99 0 092412 * . G . F X 2 . -999.99 0 092412 * . G F X 2 . -999.99 0 092412 * . G F X 2 . -999.99 1 092512 * . G F . X 2 . -999.99 1 092512 * . G F. X 2 . -999.99 1 092512 * . G . F X 2. -999.99 0 092512 * . G . F X 2 . -999.99 1 092512 * G. .F X 2 . -999.99 1

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eng2 092612-100312_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 10/08/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 10/08/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 090112C * . G .F X 2 . -999.99 -5 -5 0 092512 * . G . F X 2 . -999.99 115 42 1 092612 * . G . F X 2 . -999.99 115 42 0 092612 * . G . F X 2 . -999.99 105 39 2 092712 * . G . F X 2 . -999.99 100 45 0 092712 * . G . F X 2 . -999.99 107 44 0 092712 * . G . F X 2 . -999.99 100 40 0 092712 * . G . F X 2 . -999.99 105 44 0 092812 * . G . F X 2 . -999.99 100 42 0 092812 * . G . F X 2 . -999.99 110 48 1 092812 * . G . F X 2 . -999.99 120 48 0 092812 * . G . F X 2 . -999.99 120 42 0 092812 * . G . F X 2 . -999.99 120 42 1 092812 * . G . F X 2 . -999.99 110 40 0 092912 * . G . F X 2 . -999.99 105 47 2 092912 * . G . F X 2 . -999.99 120 42 0 092912 * . G . F X 2 . -999.99 100 42 1 092912 * . G . F X 2 . -999.99 100 42 1 092912 * . G . F X 2 . -999.99 115 42 0 093012 * . G . F X 2 . -999.99 110 42 1 093012 * . G . F X 2 . -999.99 110 42 1 093012 * . G . F X 2 . -999.99 110 40 0 100112 * . G . F X 2 . -999.99 102 45 0 100112 * . G . F X 2 . -999.99 102 46 0 100112 * . G . F X 2 . -999.99 102 46 1 100112 * . G . F X 2 . -999.99 120 42 1 100112 * . G . F X 2 . -999.99 100 45 1 100112 * . G . F X 2 . -999.99 110 45 0 100112 * . G . F X 2 . -999.99 105 47 1 100212 * . G . F X 2 . -999.99 100 40 0 100212 * . G . F X 2 . -999.99 110 46 0 100312 * . G . F X 2 . -999.99 110 32 3 100312 * . G . F X 2 . -999.99 105 45 0 100312 * . G . F X 2 . -999.99 110 42 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 100112 * . G .F X 2 . -999.99 1 100112 * . G F. X 2 . -999.99 1 100112 * . G . F X 2 . -999.99 1 100112 * . G . F X 2 . -999.99 0 100112 * . G F . X 2 . -999.99 1 100212 * . G . F X 2 . -999.99 0 100212 * . G . F X 2 . -999.99 0 100312 * . G . F X . 2 -999.99 3 100312 * . G . F X 2 . -999.99 0 100312 * . G . F X 2 . -999.99 0

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eng2 101412-102212_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 10/24/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 10/24/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 090112C * . G .F X 2 . -999.99 -5 -5 0 101412 * . G . F X 2 . -999.99 122 42 0 101412 * . G . F X 2 . -999.99 120 40 0 101512 * . G . F X 2 . -999.99 100 48 1 101512 * . G . F X 2 . -999.99 105 43 0 101512 * . G . F X 2 . -999.99 105 40 0 101512 * . G . F X 2 . -999.99 105 43 1 101612 * . G . F X 2 . -999.99 100 40 1 101612 * . G . F X 2 . -999.99 105 42 0 101712 * . G . F X 2 . -999.99 100 40 0 101712 * . G . F X 2 . -999.99 100 42 0 101812 * . G . F X 2 . -999.99 120 39 0 101812 * . G . F X 2 . -999.99 120 42 0 101812 * . G . F X 2 . -999.99 110 40 0 101812 * . G . F X 2 . -999.99 110 38 0 101912 * . G . F X 2 . -999.99 100 40 0 101912 * . G . F X 2 . -999.99 100 40 0 101912 * . G . F X 2 . -999.99 100 42 0 101912 * . G . F X 2 . -999.99 100 42 0 101912 * . G . F X 2 . -999.99 100 42 0 101912 * . G . F X 2 . -999.99 100 40 0 102012 * . G . F X 2 . -999.99 102 45 0 102012 * . G . F X 2 . -999.99 102 42 0 102112 * . G . F X 2 . -999.99 100 40 0 102112 * . G . F X 2 . -999.99 120 42 0 102112 * . G . F X 2 . -999.99 120 39 0 102112 * . G . F X 2 . -999.99 100 45 0 102212 * . G . F X 2 . -999.99 100 42 0 102212 * . G . F X 2 . -999.99 105 40 0 102212 * . G . F X 2 . -999.99 110 42 0 102212 * . G . F X 2 . -999.99 110 42 0 102212 * . G . F X 2 . -999.99 100 44 0 102212 * . G . F X 2 . -999.99 105 42 1 102212 * . G . F X 2 . -999.99 105 42 1 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 102112 * . G F . X 2 . -999.99 0 102112 * . G . F X 2 . -999.99 0 102112 * . G . F X 2 . -999.99 0 102212 * . G .F X 2 . -999.99 0 102212 * . G F X 2 . -999.99 0 102212 * . G . F X 2 . -999.99 0 102212 * . G F. X 2 . -999.99 0 102212 * . G . F X 2 . -999.99 0 102212 * . G .F X 2 . -999.99 1 102212 * . G .F X 2 . -999.99 1

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eng2 102312-103112_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 11/02/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 11/02/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 090112C * . G .F X 2 . -999.99 -5 -5 0 100112C * . G . F X 2 . -999.99 -5 -5 0 102212 * . G . F X 2 . -999.99 100 42 0 102212 * . G . F X 2 . -999.99 105 40 0 102212 * . G . F X 2 . -999.99 110 42 0 102212 * . G . F X 2 . -999.99 110 42 0 102212 * . G . F X 2 . -999.99 100 44 0 102212 * . G . F X 2 . -999.99 105 42 1 102212 * . G . F X 2 . -999.99 105 42 1 102312 * . G . F X 2 . -999.99 110 41 0 102312 * . G . F X 2 . -999.99 105 40 0 102312 * . G . F X 2 . -999.99 120 42 1 102312 * . G . F X 2 . -999.99 105 42 1 102412 * . G . F X 2 . -999.99 105 38 0 102412 * . G . F X 2 . -999.99 105 40 0 102512 * . G . F X 2 . -999.99 110 46 0 102512 * . G . F X 2 . -999.99 100 44 0 102512 * . G . F X 2 . -999.99 120 42 0 102512 * . G . F X 2 . -999.99 110 42 0 102512 * . G . F X 2 . -999.99 105 42 0 102612 * . G . F X 2 . -999.99 105 42 0 102612 * . G . F X 2 . -999.99 102 41 0 102712 * . G . F X 2 . -999.99 110 48 1 102712 * . G . F X 2 . -999.99 110 48 1 102812 * . G . F X 2 . -999.99 110 40 0 102812 * . G . F X 2 . -999.99 110 40 0 102912 * . G . F X 2 . -999.99 100 40 0 102912 * . G . F X 2 . -999.99 100 40 0 102912 * . G . F X 2 . -999.99 110 40 0 102912 * . G . F X 2 . -999.99 100 44 0 103012 * . G . F X 2 . -999.99 110 45 0 103012 * . G . F X 2 . -999.99 105 40 0 103012 * . G . F X 2 . -999.99 110 45 0 103012 * . G . F X 2 . -999.99 100 40 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 102812 * . G F X 2 . -999.99 0 102812 * . G . F X 2 . -999.99 0 102912 * . G . F X 2 . -999.99 0 102912 * . G . F X 2 . -999.99 0 102912 * . G F. X 2 . -999.99 0 102912 * . G F X 2 . -999.99 0 103012 * . G . F X 2 . -999.99 0 103012 * . G . F X 2 . -999.99 0 103012 * G F . X 2 . -999.99 0 103012 * . G . F X 2 . -999.99 0

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eng2 110112-111012_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 11/13/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 11/13/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -20..-10....0...EGT..20...30...40 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 090112C * . G .F X 2 . -999.99 -5 -5 0 100112C * . G . F X 2 . -999.99 -5 -5 0 110112 * . G . F X 2 . -999.99 110 42 0 110112 * . G . F X 2 . -999.99 110 42 0 110112 * . G . F X 2 . -999.99 110 43 0 110212 * . G . F X 2 . -999.99 110 35 2 110212 * . G . F X 2 . -999.99 101 46 0 110212 * . G . F X 2 . -999.99 105 42 1 110312 * . G . F X 2 . -999.99 105 38 0 110312 * . G . F X 2 . -999.99 110 42 0 110312 * . G . F X 2 . -999.99 100 43 0 110412 * . G . F X 2 . -999.99 98 44 0 110412 * . G . F X 2 . -999.99 110 43 0 110412 * . G . F X 2 . -999.99 105 41 0 110412 * . G . F X 2 . -999.99 105 38 0 110512 * . G . F X 2 . -999.99 100 47 1 110512 * . G . F X 2 . -999.99 102 47 0 110612 * . G . F X 2 . -999.99 100 39 0 110612 * . G . F X 2 . -999.99 110 39 0 110612 * . G . F X 2 . -999.99 105 47 0 110712 * . G . F X 2 . -999.99 110 43 0 110712 * . G .F X 2 . -999.99 110 40 0 110712 * . G .F X 2 . -999.99 110 39 0 110712 * . G .F X 2 . -999.99 110 39 0 110812 * . G .F X 2 . -999.99 105 42 0 110812 * . G .F X 2 . -999.99 110 42 0 110812 * . G .F X 2 . -999.99 105 39 0 110912 * . G .F X 2 . -999.99 102 44 0 110912 * . G .F X 2 . -999.99 105 46 0 110912 * . G .F X 2 . -999.99 105 46 0 110912 * . G .F X 2 . -999.99 110 42 0 111012 * . G F X 2 . -999.99 110 42 0 111012 * . G F X 2 . -999.99 104 48 1 111012 * . G F X 2 . -999.99 104 42 0 RAW DATA -20..-10....0...EGT..20...30...40 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 110812 * . G . +F X 2 . -999.99 0 110812 * . G .F X 2 . -999.99 0 110812 * . G F. X 2 . -999.99 0 110912 * . G . F X 2 . -999.99 0 110912 * . G F . X 2 . -999.99 0 110912 * . G .F X 2 . -999.99 0 110912 * . G F . X 2 . -999.99 0 111012 * . G F. X 2 . -999.99 0 111012 * . G F . X 2 . -999.99 1 111012 * . G . F X 2 . -999.99 0

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eng2 111112-112412_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 11/27/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 11/27/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -20..-10....0...EGT..20...30...40 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G .F X 2 . -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 090112C * . G .F X 2 . -999.99 -5 -5 0 100112C * . G . F X 2 . -999.99 -5 -5 0 110112C * . G . F X 2 . -999.99 -5 -5 0 111012 * . G F X 2 . -999.99 104 48 1 111012 * . G F X 2 . -999.99 104 42 0 111112 * . G F X 2 . -999.99 130 42 0 111112 * . G F X 2 . -999.99 110 42 0 111212 * . G F X 2 . -999.99 98 43 0 111212 * . G F X 2 . -999.99 103 40 0 111212 * . G F X 2 . -999.99 102 43 0 111212 * . G F X 2 . -999.99 110 42 0 111212 * . G F X 2 . -999.99 110 42 0 111312 * . G F X 2 . -999.99 110 40 0 111312 * . G F X 2 . -999.99 100 44 0 111412 * . G F X 2 . -999.99 110 42 0 111412 * . G F X 2 . -999.99 105 42 0 111412 * . G F X 2 . -999.99 110 42 0 111412 * . G F X 2 . -999.99 105 42 0 111412 * . G F X 2 . -999.99 105 39 0 111512 * . G F X 2 . -999.99 101 42 0 111512 * . G F X 2 . -999.99 105 42 0 112012 * . G F X 2 . -999.99 102 43 0 112112 * . G F X 2 . -999.99 110 42 0 112112 * . G F X 2 . -999.99 110 45 0 112212 * . G F. X 2 . -999.99 110 42 0 112212 * . G F. X 2 . -999.99 105 42 0 112312 * . G F. X 2 . -999.99 110 40 0 112312 * . G F. X 2 . -999.99 110 40 0 112312 * . G F. X 2 . -999.99 110 42 0 112312 * . G F X 2 . -999.99 103 45 0 112412 * . G F X 2 . -999.99 100 40 0 112412 * . G F X 2 . -999.99 105 39 1 112412 * . G F X 2 . -999.99 105 42 0 112412 * . G F X 2 . -999.99 100 40 0 RAW DATA -20..-10....0...EGT..20...30...40 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 112212 * . G F. X 2 . -999.99 0 112212 * . G . F X 2 . -999.99 0 112312 * . G F . 2X . -999.99 0 112312 * . G F. X 2 . -999.99 0 112312 * . G F . X 2 . -999.99 0 112312 * . G .F X 2 . -999.99 0 112412 * G F. X 2 . -999.99 0 112412 * . G . F X 2 . -999.99 1 112412 * . G . F X 2. -999.99 0 112412 * . G F. X 2 . -999.99 0

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eng2 112512-120412_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 12/05/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 12/05/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -42..-40..-38...F/F.-34..-32..-30 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G +F X 2 . -999.99 -5 -5 0 080112C * . G +F X 2 . -999.99 -5 -5 0 090112C * . G +F X 2 . -999.99 -5 -5 0 100112C * . G +F X 2 . -999.99 -5 -5 0 110112C * . G +F X 2 . -999.99 -5 -5 0 112612 * . G +F X 2 . -999.99 105 40 0 112612 * . G +F X 2 . -999.99 110 42 0 112612 * . G +F X 2 . -999.99 110 42 0 112612 * . G +F X 2 . -999.99 100 43 1 112712 * . G +F X 2 . -999.99 105 46 1 112712 * . G +F X 2 . -999.99 100 42 0 112812 * . G +F X 2 . -999.99 102 40 0 112812 * . G +F X 2 . -999.99 100 41 0 112812 * . G +F X 2 . -999.99 100 45 0 112812 * . G +F X 2 . -999.99 100 42 0 112812 * . G +F X 2 . -999.99 110 45 0 112812 * . G +F X 2 . -999.99 95 42 0 112912 * . G +F X 2 . -999.99 105 40 0 113012 * . G +F X 2 . -999.99 103 42 0 113012 * . G +F X 2 . -999.99 110 48 3 113012 * . G +F X 2 . -999.99 110 45 1 113012 * . G +F X 2 . -999.99 100 43 1 113012 * . G +F X 2 . -999.99 110 46 1 120212 * . G +F X 2 . -999.99 120 42 0 120212 * . G +F X 2 . -999.99 105 40 0 120312 * . G +F X 2 . -999.99 100 42 0 120312 * . G +F X 2 . -999.99 110 42 0 120312 * . G +F X 2 . -999.99 100 44 0 120312 * . G F. X 2 . -999.99 110 42 0 120312 * . G F . X 2 . -999.99 105 42 0 120312 * . G F . X 2 . -999.99 110 40 0 120412 * . G F . X 2 . -999.99 95 42 0 120412 * . G F . X 2 . -999.99 110 42 0 120412 * . G F . X 2 . -999.99 100 42 0 120412 * . G F . X 2 . -999.99 110 42 0 120412 * . G -F . X 2 . -999.99 100 48 1 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -42..-40..-38...F/F.-34..-32..-30 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 120312 * . G -F . X 2 . -999.99 0 120312 * . G -F . X 2 . -999.99 0 120312 * . G -F . X 2 . -999.99 0 120312 * . G-F . X 2 . -999.99 0 120312 * . G -F . X 2 . -999.99 0 120412 * . -* . X 2 . -999.99 0 120412 * . G -F . X 2 . -999.99 0 120412 * . G -F . X 2 . -999.99 0 120412 * . G -F . X 2 . -999.99 0 120412 * . G -F . X 2 . -999.99 1

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eng2 120512-121112_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 12/12/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 12/12/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -16..-14..-12...F/F..-8...-6...-4 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512C * . G +F X 2 . -999.99 -5 -5 0 080112C * . G +F X 2 . -999.99 -5 -5 0 090112C * . G +F X 2 . -999.99 -5 -5 0 100112C * . G +F X 2 . -999.99 -5 -5 0 110112C * . G +F X 2 . -999.99 -5 -5 0 120512 * . G -F . X 2 . -999.99 100 40 3 120612 * . G -F . X 2 . -999.99 100 42 1 120612 * . G -F . X 2 . -999.99 120 47 2 120612 * . G -F . X 2 . -999.99 105 42 2 120612 * . G F . X 2 . -999.99 102 44 2 120612 * . G F . X 2 . -999.99 101 44 2 120612 * . G F . X 2 . -999.99 100 40 3 120712 * . G F . X 2 . -999.99 110 42 2 120712 * . G F . X 2 . -999.99 110 42 2 120712 * . G F . X 2 . -999.99 118 48 1 120712 * . G F . X 2 . -999.99 118 38 3 120812 * . G F . X 2 . -999.99 105 40 1 120812 * . G F . X 2 . -999.99 105 45 2 120812 * . G F . X 2 . -999.99 105 40 2 120812 * . G F . X 2 . -999.99 105 42 3 120812 * . G F . X 2 . -999.99 105 42 2 120812 * . G F . X 2 . -999.99 110 40 2 120912 * . G F . X 2 . -999.99 110 42 1 120912 * . G F . X 2 . -999.99 110 42 0 120912 * . G -F . X 2 . -999.99 110 42 0 121012 * . G -F . X 2 . -999.99 110 40 1 121012 * . G F . X 2 . -999.99 110 42 1 121012 * . G F . X 2 . -999.99 110 39 1 121012 * . G F . X 2 . -999.99 110 43 2 121012 * . G F . X 2 . -999.99 105 40 1 121112 * . G F . X 2 . -999.99 105 47 2 121112 * . G F . X 2 . -999.99 110 40 1 121112 * . G F . X 2 . -999.99 110 42 1 121112 * . G F . X 2 . -999.99 100 42 1 121112 * . G F . X 2 . -999.99 100 46 2 121112 * . G F . X 2 . -999.99 105 42 2 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -16..-14..-12...F/F..-8...-6...-4 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 121012 * . G +F X 2 . -999.99 1 121012 * . G +F X 2 . -999.99 1 121012 * . G +F X 2 . -999.99 2 121012 * . G +F X 2 . -999.99 1 121112 * . G +F X 2 . -999.99 2 121112 * . G +F X 2 . -999.99 1 121112 * . G +F X 2 . -999.99 1 121112 * . G +F X 2 . -999.99 1 121112 * . G +F X 2 . -999.99 2 121112 * . G +F X 2 . -999.99 2

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eng2 121212-122212_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 12/24/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 12/24/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 090112C * . G .F X 2 . -999.99 -5 -5 0 100112C * . G . F X 2 . -999.99 -5 -5 0 110112C * . G . F X 2 . -999.99 -5 -5 0 120212C * . G -F . X 2 . -999.99 -5 -5 0 121312 * . G F . X 2 . -999.99 105 45 1 121412 * . G F . X 2 . -999.99 105 42 0 121412 * . G F . X 2 . -999.99 105 45 1 121512 * . G F . X 2 . -999.99 105 45 1 121512 * . G F . X 2 . -999.99 110 42 1 121512 * . G F . X 2 . -999.99 110 48 0 121512 * . G F . X 2 . -999.99 105 42 0 121612 * . G F . X 2 . -999.99 110 40 0 121612 * . G F . X 2 . -999.99 120 42 0 121612 * . G F . X 2 . -999.99 120 42 0 121612 * . G . F X 2 . -999.99 120 39 1 121712 * . G . F X 2 . -999.99 120 39 0 121712 * . G . F X 2 . -999.99 110 42 0 121812 * . G . F X 2 . -999.99 105 46 0 121812 * . G . F X 2 . -999.99 105 45 0 121812 * . G . F X 2 . -999.99 100 43 0 121912 * . G . F X 2 . -999.99 110 44 0 121912 * . G . F X 2 . -999.99 100 40 0 122012 * . G . F X 2 . -999.99 102 48 0 122012 * . G . F X 2 . -999.99 140 49 0 122012 * . G . F X 2 . -999.99 105 43 0 122012 * . G . F X 2 . -999.99 110 42 0 122112 * . G .F X 2 . -999.99 110 48 0 122112 * . G .F X 2 . -999.99 100 46 0 122112 * . G .F X 2 . -999.99 105 40 0 122112 * . G .F X 2 . -999.99 105 43 0 122112 * . G .F X 2 . -999.99 120 48 0 122212 * . G .F X 2 . -999.99 100 40 0 122212 * . G .F X 2 . -999.99 105 42 0 122212 * . G .F X 2 . -999.99 105 42 0 122212 * . G F X 2 . -999.99 105 45 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 122012 * . G . F X 2 . -999.99 0 122112 * . G F. X 2 . -999.99 0 122112 * . G F. X 2 . -999.99 0 122112 * . G . F X 2 . -999.99 0 122112 * . G .F X 2 . -999.99 0 122112 * . G F. X 2 . -999.99 0 122212 * . G . +F X 2 . -999.99 0 122212 * . G F. X 2 . -999.99 0 122212 * . G F. X 2 . -999.99 0 122212 * . G F. X 2 . -999.99 0

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eng2 122312-123112_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 01/02/2013 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 01/02/2013 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -2....X...-1....X...N2....X....1....X....2 SMOOTH 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 080112C * . G . F X2 . -999.99 -5 -5 0 090112C * . G .F * . -999.99 -5 -5 0 100112C * . G . F X 2 . -999.99 -5 -5 0 110112C * . G . F X2 . -999.99 -5 -5 0 120212C * . G -F . X 2 . -999.99 -5 -5 0 122412 * . G .F X 2 . -999.99 105 39 0 122412 * . G .F X 2 . -999.99 105 40 1 122412 * . G .F X 2 . -999.99 105 39 0 122412 * . G .F X 2 . -999.99 110 45 1 122512 * . G .F X 2 . -999.99 105 45 0 122512 * . G .F X 2 . -999.99 110 42 0 122612 * . G .F X 2 . -999.99 105 41 1 122612 * . G .F X 2 . -999.99 110 45 2 122712 * . G F X 2 . -999.99 110 43 0 122712 * . G F. X 2 . -999.99 100 41 0 122712 * . G F. X 2 . -999.99 120 42 0 122712 * . G F. X 2 . -999.99 110 40 0 122712 * . G F. X 2 . -999.99 110 42 0 122812 * . G F. X 2 . -999.99 105 42 0 122812 * . G F . X 2 . -999.99 102 45 0 122812 * . G F . X 2 . -999.99 102 44 0 122812 * . G F . X 2 . -999.99 102 46 1 122812 * . G F . X 2 . -999.99 120 46 1 122812 * . G F . X 2 . -999.99 105 42 1 122812 * . G F . X 2 . -999.99 110 40 1 122912 * . G F . X 2 . -999.99 120 42 0 122912 * . G F . X 2 . -999.99 115 45 1 122912 * . G F . X 2 . -999.99 105 42 1 122912 * . G F . X 2 . -999.99 110 47 1 122912 * . G F . X 2 . -999.99 105 47 1 123012 * . G F . X 2 . -999.99 105 45 1 123112 * . G F . X 2 . -999.99 103 45 1 123112 * . G F . X 2 . -999.99 110 48 0 123112 * . G F . X 2 . -999.99 110 44 2 123112 * . G F . X 2 . -999.99 105 45 1 123112 * . G F . X 2 . -999.99 105 43 1 RAW DATA -10....0...10...EGT..30...40...50 -2....X...-1....X...N2....X....1....X....2 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 122912 * . G F . X 2 . -999.99 1 122912 * . G F . X 2 . -999.99 1 122912 * . G F . X 2 . -999.99 1 122912 * . G F X2 . -999.99 1 123012 * . G F . X 2 . -999.99 1 123112 * . +G F . X 2 . -999.99 1 123112 * G F . X 2 -999.99 0 123112 * . G . F X 2 . -999.99 2 123112 * . G -F . X 2 . -999.99 1 123112 * . -F G . X . 2 -999.99 1

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eng2 010113-011013_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 01/11/2013 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 01/11/2013 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 080112C * . G . F X 2 . -999.99 -5 -5 0 090112C * . G .F X 2 . -999.99 -5 -5 0 100112C * . G . F X 2 . -999.99 -5 -5 0 110112C * . G . F X 2 . -999.99 -5 -5 0 120212C * . G -F . X 2 . -999.99 -5 -5 0 010113 * . G F . X 2 . -999.99 110 38 3 010113 * . G F . X 2 . -999.99 120 48 1 010113 * . G F . X 2 . -999.99 101 40 2 010113 * . G F . X 2 . -999.99 110 42 0 010213 * . G F . X 2 . -999.99 105 40 2 010213 * . G F . X 2 . -999.99 110 46 2 010213 * . G F . X 2 . -999.99 110 46 2 010213 * . G F . X 2 . -999.99 100 46 1 010213 * . G F . X 2 . -999.99 110 42 1 010313 * . G F . X 2 . -999.99 105 42 2 010313 * . G F . X 2 . -999.99 103 45 0 010313 * . G F . X 2 . -999.99 103 46 1 010413 * . G F . X 2 . -999.99 120 41 0 010413 * . G F . X 2 . -999.99 110 46 1 010513 * . G F . X 2 . -999.99 100 40 2 010513 * . G F . X 2 . -999.99 102 40 1 010513 * . G F . X 2 . -999.99 100 43 4 010613 * . G F . X 2 . -999.99 110 49 3 010613 * . G F . X 2 . -999.99 105 45 2 010613 * . G F . X 2 . -999.99 105 45 2 010713 * . G F . X 2 . -999.99 110 42 2 010713 * . G F . X 2 . -999.99 110 47 1 010813 * . G F . X 2 . -999.99 105 43 2 010913 * . G F . X 2 . -999.99 110 40 2 010913 * . G F . X 2 . -999.99 105 40 1 010913 * . G F . X 2 . -999.99 110 42 1 010913 * . G F . X 2 . -999.99 105 45 1 011013 * . G F . X 2 . -999.99 110 46 1 011013 * . G F . X 2 . -999.99 110 45 1 011013 * . G F . X 2 . -999.99 105 40 1 011013 * . G F . X 2 . -999.99 105 39 1 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 010713 * . G F . X 2 . -999.99 1 010813 * . G F . X 2 . -999.99 2 010913 * . G F . X 2 . -999.99 2 010913 * . G .F X 2 . -999.99 1 010913 * . G F . X 2 . -999.99 1 010913 * . G F X 2 . -999.99 1 011013 * . G F . X 2 . -999.99 1 011013 * . G .F X 2 . -999.99 1 011013 * . G . F X 2 . -999.99 1 011013 * . G F X 2 . -999.99 1

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eng2 011113-011813_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 01/21/2013 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 01/21/2013 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 090112C * . G .F X 2 . -999.99 -5 -5 0 100112C * . G . F X 2 . -999.99 -5 -5 0 110112C * . G . F X 2 . -999.99 -5 -5 0 120212C * . G -F . X 2 . -999.99 -5 -5 0 010113C * . G -F . X 2 . -999.99 -5 -5 0 011113 * . G F. X 2 . -999.99 100 43 2 011113 * . G F. X 2 . -999.99 110 40 0 011113 * . G F. X 2 . -999.99 110 41 0 011213 * . G F . X 2 . -999.99 110 39 0 011213 * . G F . X 2 . -999.99 103 45 0 011213 * . G F . X 2 . -999.99 107 47 0 011213 * . G F . X 2 . -999.99 100 40 1 011313 * . G F . X 2 . -999.99 110 39 1 011313 * . G F . X 2 . -999.99 105 43 0 011413 * . G F . X 2 . -999.99 100 46 1 011413 * . G F . X 2 . -999.99 100 42 1 011413 * . G F . X 2 . -999.99 110 44 0 011413 * . G F. X 2 . -999.99 105 41 1 011513 * . G F. X 2 . -999.99 105 45 0 011513 * . G F. X 2 . -999.99 110 42 0 011513 * . G F. X 2 . -999.99 102 44 0 011513 * . G F. X 2 . -999.99 110 44 0 011513 * . G F. X 2 . -999.99 105 39 0 011613 * . G F. X 2 . -999.99 110 40 0 011613 * . G F. X 2 . -999.99 120 42 0 011613 * . G F. X 2 . -999.99 110 42 0 011613 * . G F. X 2 . -999.99 105 45 0 011613 * . G F. X 2 . -999.99 105 42 0 011613 * . G F. X 2 . -999.99 110 39 0 011713 * . G F. X 2 . -999.99 100 40 0 011713 * . G F. X 2 . -999.99 110 39 1 011713 * . G F. X 2 . -999.99 105 40 0 011813 * . G F X 2 . -999.99 105 45 1 011813 * . G F X 2 . -999.99 98 41 0 011813 * . G F X 2 . -999.99 110 40 0 011813 * . G F X 2 . -999.99 105 41 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 011613 * . G F . X 2 . -999.99 0 011613 * . G F . X 2 . -999.99 0 011613 * . G .F X 2 . -999.99 0 011713 * . G . F X 2 . -999.99 0 011713 * . G F X 2 . -999.99 1 011713 * . G . F X 2 . -999.99 0 011813 * . G .F X 2 . -999.99 1 011813 * . +G . F 2 X . -999.99 0 011813 * . G F . X 2 . -999.99 0 011813 * . G . F X 2 . -999.99 0

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eng2 011913-012713_PK-YVL_2.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 01/29/2013 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 01/29/2013 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YVL -2 B737-300 CFM56-3C-1 721644 120630 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 070512A V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 070512B V=-999.0 R=-999.0 12.1 0.55 N2=-1.11 VSV=-999.00 -999.99 -5 -5 0 090112C * . G .F X 2 . -999.99 -5 -5 0 100112C * . G . F X 2 . -999.99 -5 -5 0 110112C * . G . F X 2 . -999.99 -5 -5 0 120212C * . G -F . X 2 . -999.99 -5 -5 0 010113C * . G -F . X 2 . -999.99 -5 -5 0 011913 * . G .F X 2 . -999.99 105 42 0 011913 * . G .F X 2 . -999.99 105 40 0 012013 * . G .F X 2 . -999.99 110 46 0 012013 * . G .F X 2 . -999.99 110 49 1 012113 * . G .F X 2 . -999.99 110 42 0 012113 * . G .F X 2 . -999.99 100 40 1 012113 * . G .F X 2 . -999.99 110 42 1 012113 * . G .F X 2 . -999.99 110 42 0 012113 * . G .F X 2 . -999.99 110 45 3 012213 * . G .F X 2 . -999.99 102 41 1 012213 * . G .F X 2 . -999.99 100 40 1 012213 * . G F X 2 . -999.99 105 43 0 012213 * . G F. X 2 . -999.99 120 42 1 012313 * . G F. X 2 . -999.99 100 42 1 012313 * . G F. X 2 . -999.99 100 40 0 012313 * . G F. X 2 . -999.99 120 45 0 012313 * . G F. X 2 . -999.99 120 42 1 012313 * . G F. X 2 . -999.99 120 42 0 012413 * . G F. X 2 . -999.99 100 45 1 012413 * . G F. X 2 . -999.99 105 39 1 012413 * . G F. X 2 . -999.99 105 47 0 012413 * . G F. X 2 . -999.99 105 39 1 012513 * . G F. X 2 . -999.99 105 47 1 012513 * . G F. X 2 . -999.99 103 45 0 012513 * . G F . X 2 . -999.99 110 46 1 012613 * . G F. X 2 . -999.99 110 42 2 012613 * . G F. X 2 . -999.99 110 40 1 012613 * . G F. X 2 . -999.99 110 42 0 012613 * . G F. X 2 . -999.99 100 44 1 012713 * . G F. X 2 . -999.99 100 42 2 012713 * . G F X 2 . -999.99 110 46 3 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 012413 * . G F. X 2. -999.99 1 012513 * . G .F X 2 . -999.99 1 012513 * . G F . X 2 . -999.99 0 012513 * . G F . X 2 . -999.99 1 012613 * . G . F X 2 . -999.99 2 012613 * . G . F X 2 . -999.99 1 012613 * . G F . X . 2 -999.99 0 012613 * . G F . X 2 . -999.99 1 012713 * . G . F X 2 . -999.99 2 012713 * . G . F X 2 . -999.99 3

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