N618AS

Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 74,636 hrs · 39,917 cycles

FA REPORTS L1 DOOR DIFFICULT TO OPEN AND CLOSE. GROUNDED - YES. ACCOMPLISHED L1 DOOR SYSTEM TEST, VISUAL INSPECTION AND OP'S CHECK REF MM 52-11-00, ALL CHECK GOOD. VERIFIED UPPER GUIDE ARM JAM AND AJUSTER NUT ARE SECURE PER TECH SERVICES REQUEST, REF AMM 52-11-00-820-801 FIG 502, DOOR OP'S CHECKS GOOD.

Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 74,615 hrs · 39,897 cycles

FA REPORTS L1 DOOR IS MORE DIFFICULT THAN USUAL TO CLOSE AND GETS STUCK. GROUNDED - YES. OPENED & CLOSED L1 DOOR MULTIPLE TIMES OPS NORMAL DOOR OPENS AND CLOSES SECURED SHUT & SECURED OPEN NO DEFECTS NOTED OK FOR SERVICE.

Part: LIGHT — UNSECURE (ZONE 200) · airframe 74,408 hrs · 39,739 cycles

EMERGENCY LIGHTING LOOSE ROW 7/8 DEF. GROUNDED - YES. RESECURED EMERGENCY LIGHTNING AS REQ.

Part: DOOR — BINDING (ZONE 800) · airframe 74,180 hrs · 39,581 cycles

FA REPORTS L1 DOOR DIFFICULT TO OPEN. GROUNDED - YES. PERFORMED L1 DOOR TEST REF AMM 52-11-00-700-804. NO DEFECTS NOTED AT THIS TIME. TORQUE ON HANDLE WITHIN LIMITS. CHECKED GUIDE ARM ADJUSTMENT MEASUREMENTS AND FOUND WITHIN LIMITS. REF AMM 52-11-00-820-801. LUBRICATED L1 DOOR. OPERATES NORMAL AT THIS TIME.

Part: GUIDE ARM — NO TEST (ZONE 800) · airframe 73,757 hrs · 39,276 cycles

FA UNABLE TO CLOSE L1 DOOR MIG-2C #40-0061016 INITIATED, 40-0061017 INITIATED. GROUNDED - YES. REF FWD ENTRY DOOR SYSTEM TEST, AMM TASK 52-11-00-700-804 E3D TORQUE TO OPEN INT HANDLE REQUIRED WAS AT HIGHER END OF ADJUSTABLE LIMITS. SEVERE SQUEAL COMING FROM UPPER GUIDE ARM REVEALED EXCESSIVE PLAY AT GUIDE ARM ROD END. REF MIG-2C #40-0061016 AND 40-0061017 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED. PERFORMED L1 DOOR ADJUSTMENTS REF AMM 52-11-00-820-801. MIG-2C #40-0061016 AND 40-0061017 ARE BOTH CLOSED.

Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 73,335 hrs · 38,975 cycles

FA REPORTS L1 DOOR DIFFICULT TO OPEN AND CLOSE. THIS IS A REPEAT WRITE UP. GROUNDED - YES. CYCLED L1 DOOR MULTIPLE TIMES USING INTERNAL HANDLE REF AMM 52-11-00-860-803, AND EXTERNAL HANDLE REF AMM 52-11-00-860-802. NO ABNORMALITIES AT THIS TIME, AIRCRAFT OK TO CONTINUE.

Part: RECEIVER — OUT OF ADJUST (ZONE 800) · airframe 73,339 hrs · 38,979 cycles

FA REPORTS L1 DOOR IS HARD TO OPEN. GROUNDED - YES. ADJUSTED UPPER AFT LATCH RECEIVER IAW AMM 52-11-00-820-018 L1 DOOR OPS CHECK GOOD.

Part: TRACK — LACK OF LUBE (ZONE 800) · airframe 73,328 hrs · 38,972 cycles

FA REPORTS L1 DOOR IS DIFFICULT TO OPEN. GROUNDED - YES. CLEANED AND LUBRICATED GUIDE PLATE TRACK OF L1. OPS CHECK NORMAL REF AMM 52-11-00.

Part: HINGE — LACK OF LUBE (ZONE 200) · airframe 73,031 hrs · 38,738 cycles

FA REPORTS L1 DOOR DIFFICULT TO OPEN. GROUNDED - YES. CLEANED AND FOUND FROZEN WATER IN GUST LOCK AND HINGE AREA, REMOVED FROZEN CONTAMINANTS, OPS CHECK GOOD REF: AMM 52-11-00.

Part: DOOR — NONE (ZONE 800) · airframe 72,837 hrs · 38,619 cycles

FA REPORTS L1 DOOR DIFFICULT TO OPEN. GROUNDED - YES. OPERATED DOOR FROM INTERIOR AND EXTERIOR, REF AMM 52-11-00 DOOR REQUIRES NORMAL AMOUNT OF FORCE TO OPEN A/C GOOD FOR SERVICE.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 71,722 hrs · 37,852 cycles

EGPR SURROUND DOUBLER IS CRACKED AT LOWER HINGE PAD FWD RIVET. GROUNDED - YES. REMOVED DAMAGE & REPAIRED SURROUND DOUBLER IAW B737-700 SRM 53-10-15-2R-4.

Part: SHEAR WEB — CORRODED (ZONE 200) · airframe 72,622 hrs · 38,461 cycles

AFT WET RH SHEAR WEB CORRODED STA 1008. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-70-51-1A-1. REMOVED AND REPLACED WEB IAW B737-700 SRM 51-40-02-0G-0 W: 2 O: .040 R: .023 L: 3 D: .017.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

CORROSION ON STR 26R STA 947.5+4. GROUNDED - YES. REPAIRED STR 26R STA 947.5+4 IAW BOEING 737-700 SRM 53-00-03-2R-1 W=1" O=.056" R=.026" L=3" D=.030".

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 72,622 hrs · 38,461 cycles

CORROSION ON STRAP STA 986 STR 20R. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-70-15-1A-1. REMOVED AND REPLACED STRAP IAW B737-700 SRM 51-40-02-0G-0 W: 1 O: .063 R: .055 L: 2 D: .008.

Part: MODULE — FAULTY (ZONE 700) · airframe 72,391 hrs · 38,301 cycles

AFTER T/O RAN THE AFTER T/O CHECKLIST AND GEAR HANDLE WENT PAST THE "OFF" DETENT ABOUT 1/2 INCH CAUSING THE NOSE GEAR AND RIGHT MAIN GEAR TO EXTEND AND CAUSE A GEAR DISAGREE. RAN GEAR DISAGREE CHECKLIST AND RESUMED NORMAL FLIGHT WITH NO FURTHER DEFECTS FIRST OFFICER FLEW THIS AIRPLANE 3X THIS WEEK AND HAS NOTICED THAT THE HANDLE OFTEN GOES PAST 'OFF DETENT". BOTH NOSE GEAR LIGHTS WERE ILLUMINATED, ONLY RED RIGHT GEAR LIGHT ILLUMINATED. GROUNDED - YES. DIVERSION - REPLACED LANDING GEAR CONT MOD + CKE'D GOOD PER AMM 32-31-11 PERFORMED F/O FMC CDU OPS TEST PER AMM 34-61-01. PERFORMED AACU OPS TEST PER AMM 32-42-00. PERFORMED ENGINE MODULE OPS TEST PER AMM 31-62-00. ALL TESTS PASSED.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 71,722 hrs · 37,852 cycles

L2 DOOR EMERGENCY LIGHTS BATTERY PACK FAILS OPS CHECK. GROUNDED - YES. REMOVED AND REPLACED AFT LH EMERGENCY LIGHT BATTERY PACK OP CK GOOD IAW B737-700 AMM 33-51-06-960-805. (S/N 312923)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 72,001 hrs · 38,038 cycles

LH BULLNOSE EMER LIGHTS INOP FROM ROW 10 TO 24. GROUNDED - YES. REMOVED AND INSTALLED SERVICEABLE EMERG LIGHTS BATTERY, OP CHECKS GOOD IAW B737-700 AMM 33-51-06-960-805.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 71,722 hrs · 37,852 cycles

EMERGENCY LIGHTS AT R1 DOOR FAILED OPS CHECK. GROUNDED - YES. REMOVED AND INSTALLED SERVICEABLE R1 DOOR BATTERY PACK, OP CHECKS GOOD IAW B737-700 AMM 33-51-06-960-805. (S/N 345808)

Part: FRAME SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

AFT PIT, FRAME SPLICE STA 787 O/B OF SHEILD PANEL IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OFF LIMITS,REMOVED AND REPLACED FRAME SPLICE ON AFT PIT STA 787 IAW B737-700 SRM 51-40-02-0G-0W=1" O=0.063" R=0.053" L=1" D=.010".

Part: WEB — CRACKED (ZONE 100) · airframe 71,722 hrs · 37,852 cycles

FWD PIT, WEB AT STA 492 TO 500 FOR RH LOWER SILL IS CRACKED AT FASTENRER HOLE. GROUNDED - YES. REMOVED AND REPLACED WEB IAW B737-700 SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

AT CABIN, FLOORBEAM STA 986 IS CORRODED. GROUNDED - YES. REMOVED & REPLACED FLOORBEAM EXISTING REPAIR TOP CAP LBL6 TO RBL 51 IAW BOEING 737-700 SRM 53-70-51-2R-4W 1 O .150 R .141 L 1 D .009.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

AFT CABIN, WALL SUPPORT LBL 45 IS CORRODED. GROUNDED - YES. REMOVED & REPLACED WALL SUPPORT IAW B737-700 SRM 51-40-02-0G-0W=1.0" O=.050 R=.042 L=1.0" D=.008.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 71,722 hrs · 37,852 cycles

FWD CABIN, FLOOR SUPPORT IS CRACKED AT STA 312 TO 328 LBL40. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL IAW B737-700 SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 71,722 hrs · 37,852 cycles

FWD CABIN, FLOOR SUPPORT CRACKED AT STA 328 TO 344 LBL 40. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL IAW B737-700 SRM 51-40-02-0G-0.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

AFT PIT, GUSSET PANEL ATTACHED TO SHIELD PANEL STA 767 RH SIDE IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OFF LIMITS, REMOVED AND REPLACED GUSSET PANEL ATTACHED TO SHIELD ON STA 767 RH SIDE IAW B737-700 SRM 51-40-02-0G-0W=1" O=0.063 R=0.050 L=1" D=0.033".

Part: WEB — CORRODED (ZONE 100) · airframe 71,722 hrs · 37,852 cycles

AFT CARGO DOOR SILL WEB HAS CORROSION IN MULTIPLE SPOTS. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SILL WEB IAW B737-700 SRM 51-40-01-0G-0W:2 O:.045 R:.035 L:10 D:.010.

Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

AFT PIT, SHEILD PANEL AFT OF DOOR IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT LIMITS, REMOVED AND REPLACE SHIELD PANEL IAW B737-700 SRM 51-40-02-0G-0W=1" O=.050" R=.042 L=3" D=.008.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 71,722 hrs · 37,852 cycles

AFT PIT, RH TRANSITION PANEL CORRODED BETWEEN STA 727 +4 -767. GROUNDED - YES. REMOVED NAD REPLACED DAMAGED SECTION OF TRANSITION PANEL IAW B737-700 SRM 53-00-53-2R-5 W:3 O:.040 R:.031 L:8 D:.009.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

FWD PIT, AFT BULKHEAD LOWER SUPPORT ANGLE IS CORROEDED BETWEEN RBL24-LBL24. GROUNDED - YES. REMOVED DAMAGE, ORIG MAT .071, MAX MAT LOSS .037, FOUND TO BE OUT OF LIMITS REMAINED & REPLACED SUPPORT ANGLE IAW B737-700 SRM 53-30-08-0A-1 & 51-40-02W=1.5" O=.071 R=.040 L=3.0" D=.031.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 71,722 hrs · 37,852 cycles

AFT PIT, RH CARGO TRACK RBL 14.5 IS CRACKED AT MOUNT STA'S 727D, 727E, 747. GROUNDED - YES. REMOVED AND REPLACED TRACK STA 727+4 TO STA 887 IAW B737-700 SRM 51-40-02-0G-0, 53-00-53-2R-3 AND ASA EA 700-53EA-27404.

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

AFT PIT, STRAP RBL 20 CORRODED BETWEEN STA 787-827. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OT LIMITS, REMOVED AND REPLACED STRAP ON AFT CARGO CO-PT IAW B737-700 SRM 51-40-02-0G-0W=1" O=.100" R=0.085" L=3" D=0.015".

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 71,722 hrs · 37,852 cycles

PER-CUSTOMER REQUEST, AT AREA ABOVE WING CENTER SECTION WING BOX SHEAR TIE AT VAPOR BARIER STA .540 RBL 12 CRACKED (MARKED). GROUNDED - YES. REMOVED AND REPLACED SHEAR TIE IAW B737-700 SRM 51-40-02-0G-0.

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

L2 DOOR SILL AREA HAS CORROSION. GROUNDED - YES. REMOVED & REPLACED MOPSILL CORD IAW B737-700 SRM 51-40-02-0G-0W=1.0" O=.080 R=.068 L=2.0" D=.012.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 71,722 hrs · 37,852 cycles

AFT PIT, LH TRANSITION PANEL CORRODED BETWEEN STA 727+4-827. GROUNDED - YES. REMOVED AND REPLACED DAMAGED SECTION OF TRANSITION PANEL IAW B737-700 SRM 53-00-53-2R-5W:2 O:.040 R:.030 L:6 D:.010.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

FWD PIT, RH TRANSITION PANEL CORRODED BETWEEN STA 500A-500D. GROUNDED - YES. REMOVED & REPLACED TRANSITONAL PANEL IAW B737-700 SRM 51-40-02-0G-0 W=1.5" O=.040 R=.032 L=3.0" D=.008.

Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

FWD PIT, RH SHIELD PANEL CORRODED BETWEEN STA 500-500+12. GROUNDED - YES. REMOVED & REPLACED SHIELD IAW B737-700 SRM 51-40-02-0G-0 W=1.0" O=.032 R=.500 L=2.0" D=.032.

Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

AFT PIT, SHEILD PANEL FWD OF DOOR IS CORRODED. GROUNDED - YES. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SHEILD PANEL ON FWD OF DOOR IAW B737-700 SRM 51-40-02-0G-0W=.500" O=0.050 R=0.040" L=2" D=0.010".

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 71,722 hrs · 37,852 cycles

FLOOR BEAM AT STA 947 AND RBL 50 AFT LAV AFT OUTBOARD LAV MOUNT AREA HAS CORROSION. GROUNDED - YES. REMOVED & REPLACED T-CAP IAW B737-700 SRM 53-70-51-2R-5W=2.0" O=.175 R=.000 L=2.0" D=.175.

Part: LIGHT — DAMAGED (CABIN) · airframe 71,921 hrs · 37,990 cycles

FA REPORTS FLOOR TRACK LIGHTING TORN FORWARD OF AFT LAV. GROUNDED - YES. REPLACED FLOOR TRACK LIGHTING FWD OF AFT LAV REF AMM 25-27-21.

Part: LIGHT — MISSING (FWD CABIN FLOOR) · airframe 71,191 hrs · 37,476 cycles

FLOOR LIGHTING STRIP MISSING R/H FWD OF LAV. GROUNDED - YES. INSTALLED PROXIMATELY 20" OF PHOTOLUMINESCENT LIGHT PER AMM 33-51-15.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,053 hrs · 35,902 cycles

FA STATES THAT L1 DOOR STICKS AND IS VERY DIFFICULT TO OPEN. DIFFICULT TO OPEN AND CLOSE. GROUNDED - YES. LUBRICTAED DOOR HINGE AND TRACKS. CYCLED L1 DOOR SEVERAL TIMES. OPS CK DUE.

Part: BATTERY PACK — INOPERATIVE (MAIN PASSENGER C) · airframe 67,496 hrs · 34,643 cycles

EMERGENCY LIGHTS AROUND LH OVERWING ESCAPE INSIDE OF AIRCRAFT ARE INOP. GROUNDED - YES. REMOVED, REPLACED, AND OPS TESTED EMERGENCY LIGHTS POWER SUPPLY MIG 68 IAW B737-NG AMM 33-51-06-960-805. NO DEFECTS NOTED.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME HAS A CRACK AT STA 827 BETWEEN STR 8 L/H & 9 L/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME HAS A CRACK AT STA 440 BETWEEN STR 8 L/H & 9 L/H AT THE I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME CRACKED AT STA 440 BETWEEN STR 8 R/H & 9R/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME AT STA 380 CRACKED BETWEEN STR 8 R/H & 9R/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME HAS A CRACK AT STA 520 BETWEEN STR 8 L/H & 9 L/H AT THE I/B HOLE FOR SUPPORT CUT OUT. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME HAS A CRACK AT STA 500C BETWEEN STR 8 L/H AND 9 L/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME CRACKED AT STA 737 BETWEEN STR 8 R/H & 9 R/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME CRACKED AT STA 787 BETWEEN STR 8 R/H & 9 R/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME CRACKED AT STA 500C BETWEEN STR 8 R/H & 9 R/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME HAS A CRACK AT STA 907 BETWEEN STR 8 L/H & 9L/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME CRACKED AT STA 520 BETWEEN STR 8 R/H & 9 R/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME HAS A CRACK AT STA 727B BETWEEN STR 8 L/H AND 9 L/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME CRACKET AT STA 727B BETWEEN STR 8 R/H & 9 R/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME HAS A CRACK AT STA 867 BETWEEN STR 8 L/H AND 9 L/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME HAS A CRACK AT STA 787 BETWEEN STR 8 L/H AND 9 L/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME CRACKET AT STA 867 BETWEEN STR 8 R/H & 9 R/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME CRACKET AT STA 480 BETWEEN STR 8 R/H & 9 R/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME HAS A CRACK AT STA 480 BETWEEN STR 8 L/H & 9 L/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1L.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME CRACKED AT STA 827 BETWEEN STR 8 R/H & 9 R/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1R.

Part: FRAME — CRACKED · airframe 67,496 hrs · 34,643 cycles

FUSELAGE FRAME HAS A CRACK AT STA 747 BETWEEN STR 8 L/H & STR 9 L/H AT I/B HOLE FOR SUPPORT BRACKET. GROUNDED - YES. REPAIRED FRAME IAW ASA AD20090102-700-25-1L.

Part: SKIN — CRACKED · airframe 67,496 hrs · 34,643 cycles

R/H HORIZONTAL LOWER SKIN IS CRACKED AT STA 101 28 INCHES FWD OF REAR SPAR. GROUNDED - YES. REPAIRED MADE TO R/H HORIZ LOWER SKIN AND STA 101, 28 IN FWD AT REAR SPAR IAW B737-700 SRM 55-10-01-2R-11.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,220 hrs · 32,729 cycles

R/H FWD EXTERIOR EMERGENCY LT INOP. GROUNDED - YES. POWER SUPPLY M1674 FOR EMERGENCY LIGHTS REMOVED AND REPLACED REF B737-700 AMM 33-51-06-960-806. INSTALLATION TEST GOOD AND R/H FWD EXTERIOR EMERG LIGHT WORKS. ONE C/B PULLED AND RESET.

Part: LAMP — INOPERATIVE (R1 DOOR EXTERIOR) · airframe 65,132 hrs · 32,646 cycles

R-1 DOOR EXTERIOR EMERGENCY LIGHT INOP. GROUNDED - YES. REPLACED R-1 DOOR EXTERIOR EMERGENCY LAMP. OPS CHECK GOOD. REF B737-700 AMM 33-51-04.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,898 hrs · 32,440 cycles

EMERGENCY LIGHT ON R1 INOP AT EXTERIOR AND L1 INTERIOR LIGHT. GROUNDED - YES. RELAMPED R1 DOOR LIGHT OPS CHECK NORMAL, ALSO INTERIOR LIGHT.

Part: WIRE — DAMAGED (AUTOTHROTTLE SYS) · airframe 64,454 hrs · 32,077 cycles

AUTOTHROTTLE FAILED TO ENGAGE PRIOR TO TAKEOFF. GROUNDED - YES. REF B737-700 WDM 22-31-51, FOUND SPLICE SP3101 PULLED ON W0051-0108-22. INSTALLED NEW SPLICE REF SWPM 20-30-12. A/T OPERATIONAL TEST PASS MM 22-31-00-700-801.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 63,457 hrs · 31,236 cycles

RIGHT HORIZONTAL STAB LOWER SKIN WAS CRACKED AT HSS 101.90. G ROUNDED - YES. REPAIRED THE SKIN IAW SRM 55-10-01-2R-11, FIG 204, REPAIR IS A CAT B.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN, AFT WET AREA, INTERCOSTAL AT STA 947.5-STA 967, RBL 50.92 CORRODED. GROUNDED - YES. EVALUATED THE INTERCOSTAL AT STA 947.5 - STA 967, RBL 50.92, WL 208.1 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1 FIG 103, DETAIL C. ORIGINAL THICKNESS 0.2050, REMAINING THICKNESS 0.125, REMOVED 0.080.

Part: TRANSITION PANEL — CORRODED (BS 887-947) · airframe 59,712 hrs · 28,038 cycles

AFT CARGO R/H TRANSITION PANEL FROM STA 887 TO STA 947 HAS CORROSION AROUND NUTPLATE HOLES THAT IS EXFOLIATED. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO R/H TRANSITION PANEL P/N 147A7501-17 FROM STA 887- TO STA 947 IAW BAC DWG 147A7501 REV. A ID: 0006, B737-700 SRM 51-40-02, BAC DWG 147A7500 REV: - ID: 0011, ID: 0012.

Part: FLOORBEAM — CORRODED (BS 887) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN, PASSENGER FLOOR BEAM STA 887, LBL 24.75, LBL 45.50, RBL 24.75, AND RBL 45.50 CORRODED ON UPPER SURFACE UNDER EACH SEAT TRACK LOCATION. GROUNDED - YES. REMOVED CORROSION ON THE UPPER SURFACE OF THE FLOOR BEAM AT STA 887 AND FOUND TO BE OUT OF LIMITS, DUE TO NO ALLOWABLE DAMAGE AT SEAT TRACK ATTACH LOCATIONS IAW B737-700 SRM 53-60-51-1A-1. ACCOMPLISHED A CATEGORY "A" REPAIR TO THE FLOOR BEAM AT STA 887, LBL 68 - RBL 68 IAW ASA EA# 700-53EA-20959 REV 00, WITH APPROVED DOCUMENT 8100-9.

Part: PRESSURE DECK — CORRODED (BS 685-695) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN UNDER FLOOR WHEEL WELL PRESSURE WEB HAS CORROSION NUMEROUS SPOTS BETWEEN BS 685 AND BS 695, RBL 60 AND RBL 74. GROUNDED - YES. REMOVED THE PRESSURE FLOOR WEB CLOSEOUT, PART #144A7720-02 AT STA 685-STA 695, RBL 60-RBL 70, WL 202 IAW B737-700 SRM 51-40-02. WEB CLOSEOUT FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-40-51, NO SRM LIMITS. BOEING GRANT A SMALL, CONTROL # 0270253420, FABRICATED, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW BOEING DRAWING 144A7720 REV C SHEET 1 AND DRAWING 144A7730 REV- SHEET 9. DOT N645 REMOVED.

Part: ATTACH ANGLE — CORRODED (BS 686) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN UNDER FLOOR WHEEL WELL PRESSURE WEB ATTACHED ANGLE HAS CORROSION @ BS 686 BETWEEN RBL 64 AND RBL 74. GROUNDED - YES. REMOVED CORRODED ATTACHED WEB ANGLE IAW B737-700 SRM 51-40-02. FABRICATED, LOCATED, DRILLED AND INSTALLED NEW WEB ATTACH ANGLE IAW BOEING DWG 144A7713 REV.B DOT REMOVED PRESSURE FLOOR ANGLE IS OUT OF LIMITS, REASON FOR REPLACEMENT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN UNDER FLOOR STRUCTURE INTERCOSTAL HAS CRACKS BETWEEN BS 311 AND BS 327 RBL 31 AS MARK. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN INTERCOSTAL, PART 141A5410-12 AT STA 312 - STA 328, RBL 31.60, WL 208.1 IAW DRAWING 141A5400 REV - SHEET 39.

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN FLOOR SUPPORT, INTERCOSTAL CRACKED BS 380 - BS 400, BL 0. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT, INTERCOSTAL/ANGLE AT BS380-BS400, BL 0 IAW B737-700 SRM 51-40-02, BAC DWG 143A5400 REV:-ID0053 DOT REMOVED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN UNDER FLOOR INTERCOSTAL CRACKED BETWEEN BS 312 AND BS 328 LBL 44. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN INTERCOSTAL, PART 141A5410-1Z AT STA 312 - STA 328, LBL 45.60, WL 208.1 IAW DRAWING 141A5400 REV - SHEET 26.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN SEAT TRACK HAS CORROSION NUMEROUS SPOTS BETWEEN BS 540 TO 663.75 LBL 45. GROUNDED - YES. REMOVED CORROSION ON THE MAIN CABIN SEAT TRACK AT STA 540 - STA 663.75, LBL 45.50 IAW SRM 51-10-02. ORIGINAL THICKNESS 0.230, REMOVED 0.030, REMAINING THICKNESS 0.200, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 AND BAC DWG 1520-2779. REMOVED SEAT TRACK AND ACCOMPLISHED A CATEGORY "A" REPAIR AT STA 540 - STA 663.75 IAW SRM 53-00-52-2R-2 AND EA 700-53EA-20991 REV 00.

Part: ATTACH ANGLE — CORRODED · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN UNDER FLOOR WHEEL WELL PRESSURE WEB ATTACHED ANGLE HAS CORROSION @ BS 693 BETWEEN RBL 64 AND RBL 74. GROUNDED - YES. REMOVED CORRODED ATTACHED WEB ANGLE IAW B737-700 SRM 51-40-02 FABRICATED, LOCATED, DRILLED AND INSTALLED NEW WEB ATTACH ANGLE IAW BOEING DWG 144A7713 REV. B DOT REMOVED. PRESSURE FLOOR ANGLE IS OUT OF LIMITS DUE TO NO SRM LIMITS, REASON FOR REPLACEMENT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN UNDER FLOOR INTERCOSTAL CRACKED BETWEEN BS 328 AND BS 344 LBL 44. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN INTERCOSTAL, PART 141A5410-16 AT STA 328-STA 344, LBL 45.60, WL 208.1 IAW DRAWING 141A5400 REV-SHEET 44 AND SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

STA 947 TRANSVERSE FLOORBEAM FLOOR CAP BETWEEN LBL 18 & RBL 18 MULTIPLE AREAS AROUND N/P HOLES ARE CORRODED. ALSO IN THE AREA OF THE AFT LAVATORY, COMMON TO THE AFT LAVATORY. GROUNDED - YES. REMOVED PREVIOUSLY INSTALLED REPAIR "T"-CAP AND REPAIR SPLICES, AND ACCOMPLISHED NEW REPAIR "T"-CAP AND REPAIR SPLICES AT STA 947.5 FLOOR-BEAM UPPER FLANGE, LBL58 IAW EA 700-53-20960.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN STA. 344 LBL-12, INTERCOSTAL IS CRACKED AT FASTENER HOLES. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02 AND DWG 141A5400 REV A SHEET 46.

Part: INTERCOSTAL — CORRODED (BS 1028-1032) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN, AFT WET AREA, AFT PRESSURE BULKHEAD LOWER INTERCOSTAL AT STA 1028-STA 1032, RBL 17-RBL 27, WL 210 UPPER SURFACE CORRODED. GROUNDED - YES. EVALUATED INTERCOSTAL ON THE AFT PRESSURE BULKHEAD AT STA 1028-STA 1032, RBL 17-RBL27, FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-80-08-1A-1 FIGURE 103, DETAIL D. REMOVED AND REPLACED INTERCOSTAL, PART# 148A2261-25 IAW B737-700 SRM 51-40-02 AND BOEING DRAWING 148A0922. REV-SHEET 11-12. DOT X076 REMOVED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN STA. 347,BL-0 , INTERCOSTAL IS CRACKED AT FWD FASTENER HOLE. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02 AND DWG 141A5400 REV-SHEET 32.

Part: INTERCOSTAL — CORRODED (BS 1016-1029) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN, AFT WET AREA, AFT PRESSURE BULKHEAD LOWER INTERCOSTAL AT STA 1016-STA 1029, RBL 27-RBL 42, WL 210 UPPER SURFACE CORRODED. GROUNDED - YES. EVALUATED INTERCOSTAL ON THE AFT PRESSURE BULKHEAD AT STA 1016-STA 1029,RBL 27-RBL 42, FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-80-08-1A-1 FIG 103, DETAIL D. REMOVED AND REPLACED INTERCOSTAL , PART # 148A2261-24 IAW B737-700 SRM 51-40-02 AND BOEING DRAWING 148A0922 REV- SHEET 11-12. DOT X075 REMOVED.

Part: INTERCOSTAL — CORRODED (BS 1028-1032) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN, AFT WET AREA, AFT PRESSURE BULKHEAD LOWER INTERCOSTAL AT STA 1028-STA 1032, LBL 17-LBL 27, WL 210 UPPER SURFACE CORRODED. GROUNDED - YES. EVALUATED INTERCOSTAL ON THE AFT PRESSURE BULKHEAD AT STA 1028-STA 1032, LBL 17-LBL 27, FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-80-1A-1 FIG 103, DETAIL D. REMOVED AND REPLACED INTERCOSTAL, PART # 148A2261-15 IAW B737-700 SRM 51-40-02 AND BOEING DRAWING 148A0922 REV-SHEET 11-12. DOT X078 REMOVED.

Part: TRANSITION PANEL — PUNCTURED (FUSELAGE) · airframe 59,712 hrs · 28,038 cycles

FWD PIT AT BS 513 AND RT TRANSITION PANEL HAS PUNCTURE. GROUNDED - YES. REPLACED WITH FABRICATED RT SHIELD/TRANSITION PNL IAW BAC DWG 143A8126 REV- AND IAW SRM 51-40-05. INSTALLED SHIELD/TRANSITION PNL IAW BAC DWG 143A8126 REV- AND IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (BS 277-294.5) · airframe 59,712 hrs · 28,038 cycles

STA. 277 BUTT LINE 0, INTERCOSTAL CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AND BRACKET AT STA 277 TO STA 294.5 BLO IAW BAC WG 141A5400 REV: - ID:0023, BAC DWG 141A5410 REV-A ID:0034 B737-700 SRM 51-40-02, SRM 51-40-05 DOT REMOVED.

Part: INTERCOSTAL — CORRODED (BS 1016-1029) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN, AFT WET AREA, AFT PRESSURE BULKHEAD LOWER INTERCOSTAL AT STA 1016-STA 1029, LBL 27-LBL 42, WL 210 UPPER SURFACE CORRODED. GROUNDED - YES. EVALUATED INTERCOSTAL ON THE AFT PRESSURE BULKHEAD AT STA 1016-STA 1029, LBL 27-LBL 42,FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-80-08-1A-1 FIG 103 DETIAL D. REMOVED AND REPLACED INTERCOSTAL, PART #65-54862-23 IAW B737-700 SRM 51-40-02 AND BOEING DRAWING 148A0922 REV-SHEET 11. DOT X079 REMOVED.

Part: INTERCOSTAL — CORRODED (BS 1032-1033) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

MAIN CABIN, AFT WET AREA, AFT PRESSURE BULKHEAD LOWER INTERCOSTAL AT STA 1032-STA 1033, LBL 8-LBL 17, WL 210 UPPER SURFACE CORRODED. GROUNDED - YES. EVALUATED INTERCOSTAL ON THE AFT PRESSURE BULKHEAD AT STA 1032-STA 1033, LBL 8-LBL 17, FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-80-08-1A-1 FIGURE 103, DETAIL D. REMOVED AND REPLACED INTERCOSTAL, PART #65-54862-18 IAW B737-700 SRM 51-40-02 AND BOEING DRAWING 148A0922 REV- SHEET 11-12. DOT X077 REMOVED.

Part: WEB — CORRODED (BS 787-847) · corrosion level 2 · airframe 59,712 hrs · 28,038 cycles

AFT PIT DOOR CUTOUT LOWER SILL WEB HAS CORROSION ALL OVER. GROUNDED - YES. REMOVED CORROSION ON AFT PIT LOWER SILL WEB IAW B737-700 SRM 51-10-02 ORIG THICKNESS, 0.045 IAW B737-700 53-60-15-0I-1. REMOVED 0.007. REMAINING THICK. 0.038. FOUND TO BE NOT WITHIN ALLOWABLE LIMITS. REMOVED CORRODED WEB IAW B737-700 SRM 51-40-02. UT GAUGE TOOLING ID: T8225P LOCATED, DRILLED, RECEIVED NEW PART LOWER SILL WEB. IAW THE FOLLOWING: BAC PL 146A8120 REV T SH 17, B737-700 SRM 51-40-05, BAC DWG 146A8123 REV C SH 6 BAC DWG 146A8120 REV E SH 3. P.N: 146A8123U6. P.O# 904518.4. INSTALLED WEB IAW B737-700 SRM 51-40-02; AND BAC DWG 146A8340 REV- SH19, AND BAC DWG 146A8340 REV A SH 9.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,750 hrs · 26,485 cycles

L1 DOOR DIFFICULT TO OPEN AND CLOSE. ACFT GROUNDED. FOUND THE UPPER AND LOWER GUIDE ARM CAM PLATES VOID OF GREASE. LUBRICATED THE CAM PLATES AND OPERATED SEVERAL TIMES. OPS CHECKED GOOD, OK FOR SERVICE. IAW AMM 12-25-11.

Part: DOOR — LACK OF LUBE (L1) · airframe 56,336 hrs · 25,514 cycles

F/A REPORTS L1 DOOR VERY HARD TO OPEN. ACFT GROUNDED. LUBED L1 DOOR IAW AMM 12-25-11-640-801. LUBED GUIDE PLATE TRACKS AND UPPER HINGE AND GUIDE ARM. OPS NORMAL.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 55,153 hrs · 24,921 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN BROKEN AT L2 DOOR. GROUNDED. REMOVED, REPLACED, AND TESTED L1190 EXIT SIGN IAW AMM 33-51-01-960-802. OPS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 55,051 hrs · 24,881 cycles

AISLE EMERGENCY LIGHT AT 8ABC INOPERATIVE. ACFT GROUNDED. FOUND LIGHT ASSY CONNECTOR DISCONNECTED. CONNECTED THE LIGHT ASSY. OPS CHECKED NORMAL, IAW SSM 33-51-13.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 55,051 hrs · 24,881 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. ACFT GROUNDED. FOUND L1188 CONNECTORS DISCONNECTED & STOWED. RECONNECTED D3666 & D3668. IAW SSM 33-51-21. OPS CHECKED NORMAL.

Part: FLOOR PANEL — CORRODED (BS 270) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

COCKPIT STEP FLOOR PANEL 141A5133-15 SEVERELY CORRODED. GROUNDED - YES. LOCATED AND DRILLED NEW FLOOR PANEL IAW B737-700 SRM 51-40-05, TOP COATED PANEL IAW B737-700 AMM 25-00-00.

Part: FLOOR SUPPORT — CORRODED (BS 270) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

COCKPIT FLOOR BS 270 BL 0 ANGLE CORRODED. ACFT GROUNDED. REPAIRED BS 270 THE FLOOR SUPPORT IAW 700-53EA-18037 REV 00, AND REO-G20417 REV A.

Part: CHANNEL — CORRODED (BS 727D) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

AFT CARGO RT TRANSITION PANEL CHANNEL IS CORRODED AT BS 727D. ACFT GROUNDED. REMOVED CORROSION, FOUND BEYOND ALLOWABLE SRM LIMITS, IAW SRM 53-00-53. INSTALLED REPAIR IAW DWG 146A7500 REV C AND SRM 53-00-53. .

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

COCKPIT FLOOR STA 270 BL0 FLOOR SUPPORT IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED SUPPORT CHANNEL IAW DWG 141A5210 REV- AND SRM 51-40-02.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

SUPPORT FITTING CORRODED BS 947-967 RBL 25 45. GROUNDED - YES. LOCATED AND DRILLED NEW SUPPORT IAW DWG 147A5660. SUPPORT WILL BE INST ON CARD G754113 N/R 26613.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

SUPPORT FITTING CORRODED BS 947-967 LBL 45. GROUNDED - YES. LOCATED AND DRILLED NEW SUPPORT FITTING IAW DWG 147A5660. FITTING TO BE INST ON CARD G754113 N/R 26613.

Part: FLOOR SUPPORT — CRACKED (BS 986-1006) · airframe 54,835 hrs · 24,781 cycles

FLOOR SUPPORT CRACKED BS 986 - 1006 LBL 30. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 AND SRM 53-70-51 & DWG 147A5700 REV-.

Part: WEB — CORRODED (BS 947-992) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

RIGHT CREASE BEAM WEB CORRODED BS 947 - 992. ACFT GROUNDED. REMOVED CORRODED WEB IAW SRM 51-10-2, FABRICATED NEW WEB IAW DWG 147A8510-51 REV E AND INSTALLED WEB IAW DWG 147A8501 REV-.

Part: WEB — CORRODED (BS 922-1006) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

CREASE BEAM WEB AT RT BS 992-1006 CORRODED. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-70-15-1A-1 FIG 103. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02, DWG 147A8510 REV A, SRM 51-20-01.

Part: FRAME — CORRODED (BS 559) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

FRAME AT LEFT SIDE WALL CORRODED . BS 559, STRINGERS 16 - 17L. ACFT GROUNDED. ACCOMPLISHED REPAIR IAW REO-G20407 REV A AND EA 700-53EA-18015 REV 00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

SEAT TRACK CORRODED AT SEVERAL SPOTS. BS 540 - BS 706, RBL 45.57. GROUNDED - YES. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-40-52-1A-1, ORIGINAL MATERIAL THICKNESS IS 0.146 IN, REMAINING THICKNESS IS 0.080 IN, REMOVED 0.066 IN. REMOVED SEAT TRACK SECTION FABRICATED NEW SEAT TRACK SECTIONS AND REPAIR SPLICE AND INSTALLED SEAT TRACK SECTIONS AND SPLICE IAW SRM 53-00-52-2R-2 AND DWG 144A5300 REV E.

Part: SUPPORT ANGLE — CORRODED (BS 992) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

SUPPORT ANGLE AT BS 992 RBL 31-45 CORRODED. ACFT GROUNDED. REPLACED THE SUPPORT ANGLE IAW DWG 147A5700 REV- .

Part: DOOR FRAME — CORRODED (BS 303) · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN L1 DOOR FRAME INBD FLANGE, CORRODED BS 303.9, STRINGERS 9 - 10L. ACFT GROUNDED. REMOVED CORROSION IAW 700-53EA-17989 REV 00, REO-G20402 REV A.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN AFT WET AREA DOOR SILL UPPER SURFACE HAS CORROSION BETWEEN BS 951 AND BS 992 LBL 47. GROUNDED - YES. REMOVED CORRODED WEB IAW SRM 51-40-02, FABRICATED NEW WEB [-50] IAW DWG 147A8510 REV B. LOCATED, DRILLED AND DEBURRED NEW WEB IAW DWG 147A8501 REV A, INSTALLED NEW WEB IAW DWG 147A8501 REV A.

Part: FRAME — CORRODED (BS 695) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN LT STUB FRAME BS 693.75 HAS CORROSION. ACFT GROUNDED. REPAIRED THE FRAME BETWEEN STRINGERS 16 -17L IAW 700-53EA-18018 REV 00, AND REO-G20401 REV A.

Part: WEB — CORRODED (BS 987-993) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN FLOOR WEB HAS CORROSION BETWEEN BS 987 AND 993. RBL 31 AND 45. ACFT GROUNDED. REMOVED AND REPLACED THE WEB IAW DWG 147A5700 REV-.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN FLOOR SUPPORT CRACKED AT BS 333, LBL 46. GROUNDED, YES. REMOVED AND REPLACED FLOOR SUPPORT AT BS 333 LBL 46 IAW SRM 51-40-02 AND DWG 141A3400.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN FLOOR SUPPORT HAS CORROSION AT BS 950 BETWEEN LBL 35 AND LBL 49. GROUNDED - YES. REMOVED CORR, LOSS OF 50% OF MAT. FOUND OUT OF LIMITS IAW SRM 53-70-51. LOCATED AND DRILLED NEW SUPPORT IAW DWG 147A5676. SUPPORT WILL BE INST ON CARD G754113 N/R 26613.

Part: FLOOR SUPPORT — CRACKED (BS 318) · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN FLOOR SUPPORT CRACKED AT BS 318 RBL 30. ACFT GROUNDED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5400.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN FLOOR SUPPORT HAS CORROSION AT BS 950 AND RBL 29. GROUNDED - YES. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW DWG 147A5650. SUPPORT WILL BE INST ON CARD G754113 N/R 26613.

Part: FLOORBEAM — CORRODED (BS 967) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN FLOORBEAM TEE HAS CORROSION BS 967 BETWEEN LBL 10 AND RBL 04. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-70-51. REPAIRED IAW SRM 53-00-51-2R-1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN FLOOR SUPPORT CRACKED AT BS 319, LBL 46. GROUNDED, YES. REMOVED AND REPLACED FLOOR SUPPORT AT BS 319, LBL 46 IAW SRM 51-40-02 AND DWG 141A5400.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN FLOOR SUPPORT HAS CORROSION AT BS 957,LBL 51. GROUNDED - YES. REMOVED CORR. LOSS OF 50% MAT. FOUND OUT OF LIMITS IAW SRM 53-70-51. LOCATED AND DRILLED NEW SUPPORT IAW DWG 147A5560. SUPPORT WILL BE INST ON CARD G754113 N/R 26613.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN L2 DOOR CUTOUT LOWER AREA SILL SUPPORT HAS CORROSION BETWEEN BS 947 AND BS 987 LBL 47. GROUNDED - YES. FOUND CORROSION TO BE BEYOND THE SRM LIMITS REPAIRS. FOUND OUT OF LIMITS IAW SRM 53-70-15 AND 57-10-02, REMOVED Z ANGLE SUPPORT AND ADJACENT ANGLES IAW SRM 57-40-02, RECEIVED NEW ANGLE SUPPORT, POSITIONED DRILLED AND DEBURRED NEW CHORD / SILL SUPPORT , INSTALLED CHORD AND SILL SUPPORT IAW DWG 147A8501 REV 0 AND DWG 147A0060 REV 0 CIC AREA UNDER CHORD IAW AMM 51-21-91, ORIGINAL MAT. WAS 0.080 MAT LOSS 100% ON LOWER CHORD AT STA BS947 AND BS987 LBL 47.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

AFT MAIN CABIN R-2 DOOR SILL SUPPORT HAS CORROSION BETWEEN BS 947.05 AND BS 995 , RBL 60. GROUNDED - YES. EVALUATED DAMAGE CORROSION FOUND OUT OF LIMITS, ORIGINAL MATERIAL THICKNESS IS .080, REMOVED .026, REMAINING IS .054 IAW SRM 53-70-15 REMOVED AND REPLACED NEW CHORD PO 879784.3 IAW SRM 51-40-02 AND DWG 147A8501, REV-, 147A0000 REV - AND 147A060 REV-.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN FLOORBEAM HAS CORROSION AT BS 947.05 AND RBL 51. GROUNDED - YES. REMOVED CORROSION FROM FLOORBEAM IAW SRM 51-10-02. CORROSION REMOVAL BEYOND LIMITS IAW SRM 53-70-51-1A-1, ORIGINAL THICKNESS 0.180 WITH 0.149 REMAINING , 0.031. REMOVED FLOORBEAM UPPER CHORD AND FABRICATED NEW CHORD, REPAIR SPLICES, REPAIR STRAPS , AND REPAIR SHIMS IAW SRM 53-70-51-2R-5. ALODINED AND PRIMED IAW SRM 51-20-01. INSTALLED NEW UPPER CHORD AND REPAIR PARTS IAW SRM 53-70-51-2R-5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN FLOORBEAM T-CAP HAS CORROSION AT BS 987, BETWEEN RBL 12 AND RBL 45. GROUNDED - YES. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-70-51-1A-1, ORIGINAL MATERIAL THICKNESS IS .150 IN. REMAINING IS .136 IN, REMOVED .014 IN REMOVED, EXISTING TEE CAP SECTIONS AND SPLICE IAW SRM 51-40-02, FABRICATED AND INSTALLED NEW T-CAP REPAIR SECTIONS AND SPLICE IAW SRM 53-70-51-2A-4.

Part: STRAP — CORRODED (BS 1018-1030) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

MAIN CABIN WEB STRAP ANGLE HAS CORROSION AT BS 1018 , LBL 27. ACFT GROUNDED. CORROSION BEYOND REPAIRABLE LIMITS, REMOVED AND REPLACED MAIN CABIN WEB STRAP ANGLE AT BS 1018 LBL 27 IAW DWG 147A5714 REV A, 147A5700 REV-, AND SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (BS 727-727E) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

AFT CARGO LEFT TRANSITION PANEL. BS 727 TO 727E+10 HAS CORROSION. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION PANEL IAW SRM 51-40-02 AND SPLICED IN NEW TRANSITION PANEL IAW SRM 53-00-53-2R-5 AND DWG 146A7500 REV C AND 146A7502 REV A.

Part: TRANSITION PANEL — CORRODED (BS 727E-847) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

AFT CARGO BAY LT TRANSITION PANEL. BS 727E+10 TO 847 HAS CORROSION. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, REMOVED DAMAGE IAW SRM 51-40-02, FABRICATED A NEW TRANSITION PANEL IAW SRM 53-00-53 AND DWG 146A7500 REV C, ALODINED PARTS IAW SRM 57-20-01, PRIMED IAW SOPM 20-41-02, INSTALLED NUT PLATES AND TRANSITION PANEL IAW SRM 51-40-02 AND SRM 53-00-53.

Part: BULKHEAD — CRACKED (BS 663) · airframe 54,835 hrs · 24,781 cycles

BS 663 UPPER PRESSURE BULKHEAD CRACKED RBL 42.5. ACFT GROUNDED. REPAIRED THE BULKHEAD IAW SRM 57-10-10-2R-3.

Part: DOUBLER — CRACKED (BS 219-235) · airframe 54,835 hrs · 24,781 cycles

ELECTRICAL GROUND POWER 304 RECEPTACLE SURROUND DOUBLER FWD LOWER END CRACKED. ACFT GROUNDED. REPAIRED IAW EA 700-53EA-17997 AND REO-G20385 REV B.

Part: FLOOR PANEL — GOUGED (FWD CARGO) · airframe 54,835 hrs · 24,781 cycles

FWD CARGO FLOOR PANEL 120CF GOUGED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW DWG 453A1610-31 REV C.

Part: FLOOR PANEL — GOUGED (FWD CARGO) · airframe 54,835 hrs · 24,781 cycles

FWD CARGO FLOOR PANEL 120BF GOUGED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW DWG 453A1610-43 REV B.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · corrosion level 2 · airframe 54,835 hrs · 24,781 cycles

FWD CARGO FLOOR PANEL 120AF CORRODED AND GOUGED. ACFT GROUNDED. FOUND BEYOND SRM LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW DWG 453A1610-13.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 54,835 hrs · 24,781 cycles

AFT CARGO FLOOR PANEL 140CF DENTED AND SCRATCHED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610. ALODINED IAW SRM 51-20-01. AND PRIMED IAW SOPM 20-41-02.

Part: FLOOR PANEL — DENTED (BS 887-947) · airframe 54,835 hrs · 24,781 cycles

AFT CARGO FLOOR PANEL 140DF DENTED AND SCRATCHED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW 53-00-53, FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610-19 REV B. ALODINED IAW SRM 57-20-01, PRIMED IAW SOPM 20-41-02.

Part: FLOOR PANEL — DENTED (BS 727-727D) · airframe 54,835 hrs · 24,781 cycles

AFT CARGO FLOOR PANEL 140AF DENTED AND SCRATCHED ALL ARROUND. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610-33, ALODINED IAW SRM 57-21-01, PRIMED IAW SOPM 20-41-02.

Part: FLOOR PANEL — DENTED (AFT CARGO) · airframe 54,835 hrs · 24,781 cycles

AFT CARGO FLOOR PANEL 140BF DENTED AND SCRATCHED. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW DWG 453A2610-31, ALODINED IAW SRM 57-20-01, PRIMED IAW SOPM 20-41-02.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 54,813 hrs · 24,770 cycles

EMERGENCY EXIT SIGN ADJACENT TO LEFT OVERWING EXIT HAS MULTIPLE LAMPS INOPERATIVE AND A BROKEN LENS. ACFT GROUNDED. REPLACED THE LAMPS, AND LENS, TESTED IAW AMM 33-51-01-960-801 - OPS NORMAL.

Part: TRACK — OUT OF ADJUST (RT OVR WING DOOR) · airframe 54,769 hrs · 24,750 cycles

OVERWING EMERGENCY EXIT AT SEAT 16F MAKES LOUD LEAKING NOISE IN FLIGHT. PRESSURIZATION OPERATES NORMAL ALL PHASES OF FLIGHT. FAULT CODES D223616F AND D224216F. ACFT GROUNDED. PRESSURIZED ACFT TO 2 PSI, FOUND RT OVERWING EXIT EXTERIOR HANDLE TO BE LEAKING. ATTEMPTED TO OPEN EXIT DOOR & FOUND EXTREMELY HARD TO OPEN WITHOUT EXCESSIVE OF FORCE. REMOVED LINER & FOUND AFT LOWER STOP TRACK OUT OF ADJUSTMENT. ADJUSTED THE STOP TRACK IAW AMM 52-22-00. DOOR NOW OPERATES NORMAL. REINSTALLED LINER IAW AMM 52-22-51. PRESSURIZED ACFT, NO LEAKS NOTED.

Part: WEB — CORRODED (BS 1018-1030) · corrosion level 2 · airframe 54,665 hrs · 24,698 cycles

MAIN CABIN FLOOR WEB HAS CORROSION AT BS 1018, LBL 33. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, CORRODDED 20% OUT OF LIMITS IAW SRM 53-70-51, REMOVED AND REPLACED NEW WEB IAW DWG 147A5700, REV B.

Part: STRINGER — DAMAGED (BS 500-500A) · airframe 53,739 hrs · 24,248 cycles

WHILE INSPECTING FWD ATG ANTENNA SUPPORT STRUCTURE, FOUND 2EA DOUBLE FLUSH RIVETS INSTALLED IN STR 27R BS 500+5 HAT SECTION ADJACENT TO PLUG RIVETS FROM PREVIOUS ANTENNA STRUCTURE REF GOGO DWG P19110-23906, FLAGNOTE 12. ACFT GROUNDED. REMOVED DAMAGE IN STR 27R, BS 500+5 HAT SECTION, REPAIRED DAMAGE IAW SRM 53-00-03, ALL WORK ACCOMPLISHED IAW ER 16-02948, REV IR DATE 28 MAY 2016, AS WELL AS EA 700-53EA-17192, REV 00 DATE 28, MAY 2016.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 53,244 hrs · 24,014 cycles

LAMPS INOPERATIVE RT OVERWING EMERGENCY EXIT SIGN, OVERWING CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN, L1 DOOR OVERHEAD EMERGENCY EXIT SIGN, R1 DOOR OVERHEAD EMERGENCY EXIT SIGN, L2 DOOR OVERHEAD EMERGENCY EXIT SIGN. REF LOG PAGES 11495051, 11495052, 11495053, 11495054, 11495055. ACFT GROUNDED. RELAMPED ALL. OPS CHECK NORMAL.

Part: LATCH — FAILED (L1 DOOR SLIDE) · airframe 53,148 hrs · 23,970 cycles

REPORTED BY F/A: L-1 DOOR SLIDE LATCH ASSY BROKEN. ACFT GROUNDED. R & R LATCH ASSY REF AMM 25-66-01-400-803, 25-66-01-00-801, 25-66-01-00-802, 25-66-01-400-801.

Part: FUEL CELL — CORRODED (BS 539) · corrosion level 2 · airframe 53,113 hrs · 23,951 cycles

AFTER REMOVAL OF RT DRAG LINK ASSY. FOUND CENTER FUEL TANK SKIN CORRODED. ACFT GROUNDED. BLENDED CORRODED RT CENTER FUEL TANK SKIN, OUT OF LIMITS, IAW SRM 5710-01-1A-2, ACCOMPLISHED EA 700-57EA-16677, W-1.500, O-.304, R-.268, L-1.600, D-0.036.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 52,554 hrs · 23,693 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ON NR 1 GALLEY ADJACENT TO R-1 DOOR HAS MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. REF WDM 33-51-21-2, FOUND LIGHT ASSY L1186 BROKEN. REMOVED, REPLACED, AND TESTED L1186 EMERGENCY LIGHT EXIT LOCATOR SIGN IAW AMM 33-51-01-960-802. OPS NORMAL.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 51,917 hrs · 23,405 cycles

UPPER HINGE FWD UPPER SKIN CUTOUT DEFORMED AND APPEARS GOUGED ON L1 DOOR. ACFT GROUNDED. REMOVED AND REPLACED THE SKIN PANEL IAW SRM 51-40-02, DWG S 141A8180, 141A3110, 141A3112, SRM 51-20-01 AND AMM 51-21-99.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · corrosion level 2 · airframe 49,402 hrs · 22,220 cycles

AFT CARGO BAY RT OTBD FLOOR SUPPORT CORRODED FROM BS 787-827, RBL 13.8. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. R & R THE FLOOR SUPPORT IAW SRM 51-40-05, 51-40-02 AND DWG 146A7500.

Part: WINDOW FRAME — CRACKED (RT WINDOW) · airframe 49,402 hrs · 22,220 cycles

RT WINDOW POST BETWEEN R1 AND R2 WINDOWS CRACKED IN UPPER FOWARD RADIUS. ACFT GROUNDED. ACCOMPLISHED HFEC INSPECTION OF R1 OTBD WINDOW POST IAW MM PART 6 51-00-00, PROC 23, FOUND TO BE CRACKED. REPAIR OF R1 WINDOW POST TO BE ACCOMPLISHED ON SB737-53-1336-NG-2, OPS:7397.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 48,836 hrs · 21,958 cycles

EMERGENCY LIGHTS INOPERATIVE SEATS 10 & 17 LT SIDE AND BOTH OVERWING ESCAPE GROUND. GROUNDED. R & R REPLACED THE LAMPS AND POWER SUPPLY. OPS GOOD, IAW AMM 33-51-00.

Part: OVEN — OVERHEATED (AFT GALLEY) · airframe 47,173 hrs · 21,181 cycles

AFT GALLEY OVEN NR 2 OVERHEATED EVEN THOUGH IT HAD BEEN TURNED OFF FOR ABOUT 45 MINUTES. IT WAS GLOWING RED INSIDE IN THE SIDE PANELS. VERY LITTLE SMOKE WAS PRESENT WHEN THE OVEN DOOR WAS OPENED BUT THERE WAS INTENSE HEAT. THE FOOD IN THE OVEN TRAY WAS NOT GETTING BURNED. HALON EXTINGUSHER WAS DISCHARGED INTO THE OVEN. OVEN DOOR WAS THEN CLOSED AND REMAINED CLOSED. ALL AFT GALLEY CIRCUIT BREAKER WERE PULLED AS SOON AS THE OVERHEAT WAS DETECTED AND BEFORE THE HALON WAS DISCHARGED. OVEN AND TFS SURROUNDING BINS WERE REPORTED TO REMAIN VERY HOT. ACFT GROUNDED. DIVERSION TIME: 28 MINUTES. INSTALLED NEW OVEN IAW REF 25-30-01MM AFT GALLEY DOUBLE OVEN CKS NORMAL. OPS CKD NORMAL FOR .5 HR.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 47,078 hrs · 21,135 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ON NR 4 GALLEY ADJACENT TO R-2 DOOR HAS BROKEN LENS. ACFT GROUNDED. R & R LENS AND TESTED SIGN IAW MM 33-51-01-960-801-OPS NORMAL.

Part: SKIN — SCRATCHED (CARGO DOOR) · airframe 43,713 hrs · 19,592 cycles

FWD CARGO DOOR SKIN HAS A SCRATCH APPROX TWO INCHES LONG. STRIPPED AFFECTED AREA IAW CMM 51-21-11. CUT OUT DAMAGED AREA IAW SRM 52-00-01, REPAIR 3. EXTENDED CUT OUT TO DOOR SKIN EDGE. ACCOMPLISHED HFEC INSPECTION AROUND DAMAGE CUTOUT IAW NDT MANUAL PART 6 51-00-00 PROCEDURE 23 IAW SRM 52-00-01, R-3. NO CRACKS OR OTHER DAMAGE FOUND. FABRICATED DOUBLER AND FILLER. DRILLED DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER IAW SRM 52-00-01 R2 4. (L.(1)(2)(3) 31628 AND INSTALLED NEW FLAPPER DRAIN IAW SRM 51-40-02.

Part: FRAME — DAMAGED (BS 747) · airframe 43,239 hrs · 19,369 cycles

AFTER REMOVING THE RT TRANSITION PANEL, FOUND FRAME AT BS 747 DAMAGED. REPAIRED FRAME IAW EA 700-53EA-09571.

Part: CHANNEL — PUNCTURED (BS 747) · airframe 49,239 hrs · 19,369 cycles

AFT CARGO COMPARTMENT, RT FORWARD TRANSITION PANEL CHANNEL PUNCTURED, BS 747, RBL 20. REPAIRED IAW SRM 53-00-53, FIG 2.

Part: WEB — CORRODED (BS 807-847) · airframe 43,239 hrs · 19,369 cycles

AFT CARGO LOWER DOOR SILL WEB CORRODED UNDER NUT PLATES. R & R WEB IAW SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (BS 934-947) · airframe 43,239 hrs · 19,369 cycles

AFT CARGO BAY TRACK CORRODED BS 934-947, RBL 13.5. R & R CARGO TRACK IAW SRM 53-00-53 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 43,239 hrs · 19,369 cycles

AFT CARGO BAY FLOOR SUPPORT, BS 772, RBL 3 HAS CORROSION OVER THE JOGGLE AREA. REPAIRED IAW EA 700 53EA 09548.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 43,239 hrs · 19,369 cycles

AFT CARGO BAY FLOOR SUPPORT BS 772, RBL 8.1 HAS CORRODED OVER JOGGLE AREA. REPAIRED IAW EA 700 53, EA 09548.

Part: CARGO TRACK — GOUGED (BS 767-820) · airframe 43,239 hrs · 19,369 cycles

AFT CARGO BAY LEFT CARGO TRACK GOUGED, WORN BS 790, LBL17. ACFT GROUNDED. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R 3.

Part: SKIN — CHAFED (NR 4 SLAT) · airframe 43,239 hrs · 19,369 cycles

LEFT WING L/E NR 4 SLAT LOWER SURFACE INBD T/E CHAFED. REPAIRED LT WING L/E NR 4 SLAT LOWER SURFACE INBD T/E CHAFE IAW SRM 57-42-01 2R 6, REPAIR 6.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

CRACK IN MAIN CABIN FRAME AT BS 360 STR 8L. REPAIRED FRAME PER EA 700 53EA 04482.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,009 hrs · 16,462 cycles

M1675 EMERGENCY LIGHT BATTERY PACK STA 322 WL 291 LBL 7 FAILS DEEP CYCLE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW B737 700 MM 33 51 06 960 805.

Part: RIB — CRACKED (HORIZ STAB) · airframe 37,009 hrs · 16,462 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STA 92.7 IS CRACKED IN FOUR PLACES. REPAIRED CRACKED RIB IAW B737 700 SRM 55 10 09 USING DOUBLERS IN ALL FOUR PLACES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

CRACKED MAIN CABIN FRAME BS 400 JUST BELOW STR 8L. REPAIRED MAIN CABIN FRAME IAW ATS ER 10 05657.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

CRACKED MAIN CABIN FRAME BS 400 JUST BELOW STR 8R. REPAIRED MAIN CABIN FRAME IAW ATS ER 10 05657.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

CRACK IN FUSELAGE COMMON TO BIN RAIL ATTACH BRACKET AT BS 727D. REPAIRED FRAME IAW ATS ER 10 05657.

Part: FRAME — CRACKED (BS 727D) · airframe 37,009 hrs · 16,462 cycles

CRACK ON FRAME AT STR 8 ATTACH BRACKET BS 727D. REPAIRED CRACK ON FRAME IAW ATS ER 10 05657.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

CRACKED INTERCOSTAL BS 312 TO BS 328 RBL 32. REMOVED AND REPLACED THE INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

CRACKED INTERCOSTAL BS 328 344 LBL 45. REMOVED AND REPLACED CRACKED INTERCOSTAL IAW B737 700 SRM 51 40 02.

Part: FRAME — CRACKED (BS 727D S8-9L) · airframe 37,009 hrs · 16,462 cycles

CRACK IN FUSELAGE FRAME COMMON TO BIN RAIL ATTACH BRACKET AT BS 727D BETWEEN STR 8L AND 9L. REPAIRED FRAME PER EA 700-53EA-04482.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,009 hrs · 16,462 cycles

M1673 BATTERY PACK STA 952 WL 290 LBL 13 FAILS DEEP CYCLE. REMOVED AND REPLACED BATTERY PACK IAW B737 700 MM 33 51 06 960 805.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,009 hrs · 16,462 cycles

M1672 EMERGENCY LIGHT BATTERY PACK STA 952 WL 290 RBL 14 FAILS DEEP CYCLE. REMOVED AND REPLACED BATTERY PACK IAW B737 700 MM 33 51 06 960 805.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

CRACKED INTERCOSTAL BS 277 294 RBL 1. REMOVED AND REPLACED INTERCOSTAL IAW B737 700 SRM 53 10 51.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

AFT CARGO AFT BULKHEAD SUPPORT BRACKET IS CRACKED BEYOND LIMITS. REPLACED AFT CARGO AFT BULKHEAD SUPPORT BRACKET PER B737 700 SRM 51 40 02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

CABIN FLOOR PANEL SUPPORT CRACKED.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

FWD BELLY DOOR SURROUND FWD UPPER HINGE SUPPORT FITTING IS CRACKED. REMOVED FITTING & INSTALLED SERVICEABLE FITTING IAW SRM 51-40-05, 51-40-02, DRAWING 141A8358 & 141A8350.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

CABIN FLOOR SUPPORT CRACKED BEYOND LIMITS.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,962 cycles

CABIN FLOOR PANEL SUPPORT CRACKED. REMOVED AND FABRICATED NEW AND INSTALLED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,962 cycles

CABIN FLOOR SUPPORT CRACKED BEYOND LIMITS. REMOVED AND FABRICATED NEW AND INSTALLED.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 37,009 hrs · 16,462 cycles

MAIN E-BAY DOOR CUTOUT FRAME WEB DENTED AND CRACKED BS 335.5 LBL 6. REMOVED CRACKED WEB FABRICATED AND INSTALLED FRAME WEB PER B737 700 SRM 51 40 02 AND BOEING DWG 141A8512.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 32,592 hrs · 14,359 cycles

RT WHEEL WELL FWD INBOARD VAPOR BARRIER CRACKED. REPLACED VAPOR BARRIER.

Part: STOP FITTING — CHAFED (ENTRY DOOR) · airframe 32,592 hrs · 14,359 cycles

FWD ENTRY DOOR AFT BOTTOM STOP PIN FITTING HAS CHAFING DAMAGE. REPLACED FWD ENTRY DOOR AFT BOTTOM STOP PIN FITTING.

Part: STOP FITTING — GOUGED (SERVICE DOOR) · airframe 32,592 hrs · 14,359 cycles

AFT SERVICE DOOR FWD UPPER STOP PIN FITTING IS GOUGED. REPLACED AFT SERVICE DOOR FWD UPPER STOP PIN FITTING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 32,592 hrs · 14,359 cycles

CRACKED VAPOR BARRIER STIFFENER BS 663 RBL 7 RBL 31 WL 160. REPLACED STIFFENER BS 663 RBL 7 RBL 31 WL 160.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 32,592 hrs · 14,359 cycles

CAPTAINS AFT O/B SEAT TRACK CHAFED AT AFT RADIUS. REMOVED AND REPLACED CAPTAINS AFT O/B SEAT TRACK.

Part: SEAT TRACK — CHAFED (COCKPIT) · airframe 32,592 hrs · 14,359 cycles

FIRST OFFICERS AFT O/B SEAT TRACK CHAFED AT AFT RADIUS. REMOVED AND REPLACED FIRST OFFICERS AFT O/B SEAT TRACK.

Part: SUPPORT ANGLE — CORRODED (APU INLET) · corrosion level 2 · airframe 32,592 hrs · 14,359 cycles

BS 1088 RBL 23 30 WL 240 APU INLET CUTOUT SUPPORT ANGLE IS CORRODED. REPLACED SUPPORT ANGLE AT BS 1088 RBL 23 TO RBL 30 WL 240.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,592 hrs · 14,359 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORROSION OUT OF LIMITS BS 727-827 LT. REMOVED AND REPLACED LT FLOOR TO SIDEWALL PLATE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,592 hrs · 14,359 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORROSION OUT OF LIMITS, BS 767-787 RT 25R WL 156 PER SRM 53-00-53. REMOVED AND REPLACED SHIELD.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,592 hrs · 14,359 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORROSION OUT OF LIMITS BS 727D-767 RT. REMOVED AND INSTALLED FABRICATED SUPPORT PLATE PER SRM 53-60-53.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,241 hrs · 14,173 cycles

EMERGENCY LIGHT EXIT SIGN AT R1 DOOR EXIT IDENTIFIER AT L1 DOOR AND EXIT SIGN IN FORWARD CABIN CEILING DID NOT COME ON FOR EMERGENCY LIGHTS OPERATIONAL CHECK. REF SSM 33 51 12. REMOVED, REPLACED AND TESTED M1675 EMERGENCY EXIT LIGHT BATTERY AND POWER SUPPLY PER MM 33 51 06 960 806, OPS NORMAL.

Part: GUIDE ARM — WORN (L1 DOOR) · airframe 31,456 hrs · 13,786 cycles

F/A REPORTS AT 1435Z THAT MAIN CABIN DOOR OPEN LOCK WILL NOT RELEASE. CLEANED AND LUBED GUST LOCK LEVER OPS CHECK GOOD HOWEVER IT IS REPORTED INTERMITTENT. FOUND MECHANISM BINDING DUE TO WORN BUSHINGS AND GENERAL DETERIORATION. REMOVED FWD GUIDE ARM ASSY AND INSTALLED NEW GUIDE ARM ASSY PER MM 52 11 21 000 802 AND MM 52 11 21 400 802. DOOR OPERATES SMOOTHLY AND NEW GUST LOCKS AND RELEASES NORMALLY. OKAY FOR CONTINUED SERVICE.

Part: PIN — MIGRATED (L1 DOOR) · airframe 31,371 hrs · 13,745 cycles

L1 DOOR GUST LOCK DIFFICULT TO OPERATE. FOUND PIN (205 IPC REF 52 11 21 01 FIG C) MIGRATED. REPOSITIONED PIN GUST LOCK, OPS CHECK NORMAL.

Part: LATCH — DIRTY (L1 DOOR) · airframe 31,287 hrs · 13,704 cycles

L1 DOOR HOLD OPEN LATCH WILL NOT UNLOCK. CLEANED AND LUBED L1 DOOR HOLD OPEN LATCH, OPS CHECK GOOD.

Part: GUIDE ARM — LOOSE (R1 DOOR) · airframe 30,765 hrs · 13,435 cycles

FWD SERVICE DOOR LIGHT REMAINED ILLUMINATED AFTER DOOR CLOSED, FOUND JAMNUT LOOSE ON GUIDE ARM AND TIGHTENED REF 52 41 21. NOTED UPPER HINGE LOWER CAMPLATE LOOSE IN FUSELAGE. TIGHTENED UPPER HINGE LOWER CAMPLATE REPLACED DOOR SNUBBER AND ADJUSTED THE GUIDE ARM PER MM'S 52 41 21 52 41 51 AND 52 41 00. OPS CHECK GOOD.

Part: DOOR — OBSTRUCTED (SERVICE DOOR) · airframe 29,108 hrs · 12,622 cycles

FWD SERVICE DOOR IS NOT CLOSING PROPERLY. INSPECTED FRAME FOR OBSTRUCTIONS SUSPECT SAFETY STRAP INTERFERENCE. DOOR OP CHECKS NORMALLY.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,815 hrs · 12,084 cycles

SKIN DENTED AFT OF L2 DOOR 12FT AFT OF EMERGENCY LIGHT. REPAIRED SKIN IAW B737 700 SRM 53-00-01 FIG 201.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CARGO PIT RIGHT TIE DOWN TRACK CORROSION FOUND FROM STA 767 TO 857. CORRODED SECTION FROM SEA 747+12 887 REPLACED WITH NEW PART IAW B737 700 SRM 53-00-53 FIG 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 22. REPLACED UPPER CAP IAW ERD 7360.

Part: STRIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

CORROSION ON CAP STRIP BETWEEN BS 847 AND BS 947 RT SIDE AFT CARGO. REPLACED CAP STRIP IAW ERD 7347 & B DRWG 453A2611.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 17. REPLACED UPPER CAP IAW ERD 7360.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CARGO CORROSION ON FLOOR SUPPORT TEE. REPLACED WITH NEW PART IAW B737 700 SRM 53-00-53.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 32. REPLACED UPPER CAP IAW ERD 7360.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 28. REPLACED UPPER CAP IAW ERD 7360.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CARGO PIT CORROSION ON FLOOR SUPPORT TEE. REPLACED WITH NEW PART IAW B737 700 SRM 53-00-53.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CARGO PIT FLOOR SUPPORT TEE CORRODED BS 887 RBL 20. REPLACED WITH NEW PART.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,815 hrs · 12,084 cycles

AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 4. REPLACED UPPER CAP IAW ERD 7360.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT LBL 24. REPLACED UPPER CAP IAW ERD 7360 & EA5310 02739.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT LBL 18. REPLACED UPPER CAP IAW CASCADE ERD 7360.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CABIN BS 986.5 FLOORBEAM UPPER CAP CORRODED AT RBL 10. REPLACE UPPER CAP IAW ERD 7360.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

CORROSION AROUND EDGES OF FLOOR PANEL NR 1 BETWEEN BS 727+4 AND BS 727D AFT CARGO PIT. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53-60-53 FIG 2 & 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CARGO PIT FLOOR SUPPORT ZEE AT LBL 21 BETWEEN BS 727 & BS 847 CORRODED. ZEE CHANNEL REPLACED.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CARGO PIT RT SIDEWALL ZEE CHANNEL BADLY CORRODED FROM STD 727+4 TO 767. AFT CARGO PIT RT SIDE PLATE ZEE CHANNEL AT BS 727+4 TO BS 767 WAS REPAIRED IAW B737 700 SRM 53 00 53.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 27,815 hrs · 12,084 cycles

AFT CARGO PIT FLOOR PANEL NR 3 WITH TEMPORARY REPAIRS AND MISSING EDGE. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53-60-53 FIG 2 & 51-40-05.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CARGO PIT LT ZEE CHANNEL FROM BS 727+4 BS 847 LBL 21 CORRODED. ZEE CHANNEL REPLACED 727+4 TO BS 847 LBL 21.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CARGO PIT CORROSION AROUND EDGES ON FLOOR PANEL NR 2 BETWEEN BS 727D AND BS 787. REPLACED WITH MADE REPAIR PARTS IAW B737 700 SRM 53-60-53 FIG 2 & 51-40-05.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CARGO PIT CORROSION AROUND EDGES ON FLOOR PANEL NR 4 BETWEEN BS 887 AND BS 947.5. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53-70-53 FIG 2 & 51-40-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,815 hrs · 12,084 cycles

CABIN FLOORBEAM AT BS 217 RBL 30 INTERCOSTAL CRACKED. REPLACED WITH NEW PART.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,815 hrs · 12,084 cycles

AFT CARGO PIT FLOOR SUPPORT WEB BETWEEN B767 & 787 RBL 20 CORRODED. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53-60-15, 51-30-01 & 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,815 hrs · 12,084 cycles

FWD CARGO RBL 22 INTERCOSTAL BS 5004 500B UPPER FLANGE CRACKED. REPAIR IAW B737 700 SRM 51-70-11 FOR 201.

Part: GROUND WIRE — DAMAGED (CABIN) · airframe 24,249 hrs · 10,349 cycles

AFT LEFT BULL NOSE EMERGENCY EXT IDENTIFIERS ARE NOT ILLUMINATING. WHEN OPS CHECKED FOUND GROUND MISSING ON WIRE W3142 040116. REPOSITIONED WIRE TO OPERATIONAL GROUNDING SPOT. OPS CHECKED GOOD.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 22,576 hrs · 9,722 cycles

FOUND INTERCOSTAL CRACKED AT BS 328. REPAIRED IAW 51 40 02.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 22,576 hrs · 9,722 cycles

FOUND INTERCOSTAL CRACKED AT BS 321. REPAIRED IAW SRM 51 40 02.

Part: DOUBLER — CRACKED (BS 225-237) · airframe 22,576 hrs · 9,722 cycles

FOUND EXTERNAL POWER RECEPTICAL CUTOUT INTERNAL DOUBLE CRACKED. REPAIRED IAW SRM 51 40 02.

Part: WEB — CRACKED (FUSELAGE)

PAE - FOUND DURING MAINTNANCE CHECK, 8 INCH CRACK IN WEB AT BS 663, LB 13 AND WL 140. REPAIR IAW SRM 57-10-10. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE FOUND FWD ROW EMERGENCY TRACK LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK.

Part: DOOR — PUNCTURED (APU BAY)

OAK - DURING MAINTENANCE CHECK, FOUND APU COMPARTMENT DOOR DAMAGED ON OUTER SKIN. REPAIRED IAW SRM. (M)

Part: CAM — LACK OF LUBE (PAX DOOR)

SEA - PRIOR TO FLT 499, L1 FORWARD ENTRY DOOR REPORTED DIFFICULT TO OPEN. LUBRICATED CAM PLATE. DOOR OPERATES NORMALLY. (M)