N736SA

Part: SLIDE — OUT OF ADJUST (ZN 900 LAV/GALLE) · airframe 79,132 hrs · 46,991 cycles

FWD SVC DOOR SLIDE POTRUDING FROM COVER / [01] REPACKED FWD SVC ESCAPE SLIDE IAW AMM 25-66-01;[02] REPOSITIONED LOWER FLAP ON FWD SVC ESCAPE SLIDE IAW AMM 25-66-01.

Part: SLIDE — OUT OF ADJUST (FWD SERVICE DOOR) · airframe 78,887 hrs · 46,830 cycles

FLIGHT ATTENDENT REPORTS FWD SEERVICE DOOR ESCAPE SLIDE AUGE DIFFICULT TO READ THRU VIEWING WINDOW / [01] ADJUSTED FWD SERVIVE DOOR SLIDE AS REQUIRED PER AMM 25-66-01

Part: SLIDE — INTERFERENCE (AFT ENTRY DOOR) · airframe 78,661 hrs · 46,672 cycles

AFT ENTRY SLIDE HAS EXTRA FOLD AND INTERFERES WITH DOOR OPENING. / [01] REPACKED SLIDE PER MT#725-61-06.

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 77,882 hrs · 46,151 cycles

RIGHT OVER WING EMERGENCY EXIT LIGHT INOP / [01] OPS CHECKED RIGHT OVER WING EMERGENCY EXIT LIGHT PER AMM 33-51-00; NO FAULTS NOTED

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 77,175 hrs · 45,701 cycles

GIRT BAR CLIP LOOSE ON FORWARD ENTRY DOOR / [01] ADJUSTED GIRT BAR CLIP PER STANDARD INDUSTRY PRACTICES; OPS CK GOOD.

Part: LIGHT — INOPERATIVE · airframe 76,507 hrs · 45,276 cycles

LEFT OVERWING CABIN SIDEWALL EXIT LIGHT OUT ; / [01] OK TO CONTINUE PER MEL 33-2-03. SP1 SP1B; [02] R&R?D LEFT OVER WING EXIT SIDEWALL LIGHT BALLAST REF AMM 33-21-00. OPS CHECK GOOD.

Part: STRUCTURE — DEBONDED (FUSELAGE) · airframe 76,298 hrs · 45,152 cycles

THREE FILLERS HAVE DISBONDED FROM 194E SUPPORT STRUCTURE. / [01] FABRICATED PER SOPM 20-50-20

Part: PANEL — NONE (FUSELAGE) · airframe 76,298 hrs · 45,152 cycles

PANEL 193D PANEL FRETTING WEAR ; 193D AFT EDGE SHOW FRETTING WEAR ALONG FLL WIDTH OF PANEL. / [01] REMOVED AND REPLACED 193D PANEL REF 53-51-21

Part: SLIDE — OUT OF POSITION (R1 DOOR)

FED SERVICE DOOR ESCAPE SLIDE REQUIRES REPOSITIONING. ; / [01] REPOSITIONED EWD SERVICE DOOR SLIDE PER MT 725-61-06.

Part: SIGN — LOOSE (CABIN)

FWD 1R DOOR EXIT SIGN LOOSE ; / [01] RESECURED FWD 1R DOOR EXIT SIGN PER AMM 33-51-01

Part: INTERCOSTAL — CORRODED (BS 494-500A) · airframe 74,899 hrs · 44,315 cycles

CORROSION WEB - INTERCOSTAL BTW BS 494 TO BS 500A AT LEVEL STR 25R AND RBL 23 AT FWD CARGO COMPARTMENT ; 2021-257941 / [01] REPLACED WEB INTERCOSTAL (SHIELD) LOCATED BTW BS 494 TO BS 500A AT LEVEL STR 25R AND RBL 23 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 AND DRAWING 143A0080. REV -; [02] REPLACED WEB INTERCOSTAL (SHIELD) LOCATED BTW BS 494 TO BS 500A AT LEVEL STR 25R AND RBL 23 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 AND DRAWING 143A0080. REV - RII

Part: STUB FRAME — CRACKED (FWD GALLEY) · airframe 74,899 hrs · 44,315 cycles

CRACK ON STUB FRAME LOCATED AT BS 294.5 AT LEVEL STR 9R; FWD GALLEY DOOR AREA. ; 2021-257904 / [01] REPLACED STUB FRAME AND FASTENERS ;LOC AT BS 294.5 AT LEVEL STR 9R FWD GALLEY DOOR AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8370 REV C .; [02] REPLACED STUB FRAME AND FASTENERS ;LOC AT BS 294.5 AT LEVEL STR 9R FWD GALLEY DOOR AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8370 REV C . RII ITEM; [03] COMPLETED TASK RII ITEM

Part: ANGLE — CRACKED (BS 693) · airframe 74,899 hrs · 44,315 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 693 AT LEVEL RBL 24.5 CENTER SECTION ; 2021- 257907 / [01] REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 693 AT LEVEL OF RBL 2R.5 CENTER SECTION IAW SRM B737-700 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DWG # 273A9112 REV - MATERIAL USED BAC1490-2782 7075-0 HEAT TREATED TO T73 IAW BAC5602; [02] TASK COMPLETED VERIFIED AS RII <BR><BR>REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 693 AT LEVEL OF RBL 2R.5 CENTER SECTION IAW SRM B737-700 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DWG # 273A9112 REV - .

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 74,899 hrs · 44,315 cycles

CRACK OUTBOARD TRAILING EDGE SUPPORT ANGLE LOCATED OBSS 274 AT LT WING (1 EA) ; 2021-257845 / [01] REPLACED OUTBOARD TRAILING EDGE SUPPORT ANGLE LOCATED OBSS 274 AT LT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02; [02] REPLACED OUTBOARD TRAILING EDGE SUPPORT ANGLE LOCATED OBSS 274 AT LT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02

Part: LIGHT — BROKEN (AFT GALLEY) · airframe 74,899 hrs · 44,315 cycles

BROKEN LAVATORY B EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA ; 2021-257786 / [01] REPLACED LAVATORY B EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801; [02] REPLACED LAVATORY B EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801. OPERATIONAL TEST IS OK.; [03] TASK COMPLETED.<BR><BR>REPLACED LAVATORY B EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA AND PERFORMED OPERATIONAL TEST IS OK.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,899 hrs · 44,315 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER. REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4; [04] REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4; [05] REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4<BR>RII

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 74,899 hrs · 44,315 cycles

ELONGATED HOLE FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT ; 2021-257765 / [01] FABRICATED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 453A2610 REV E .MATERIAL USED : 2024T3/0.080 PO# 2021-147804 .; [02] FABRICATED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 453A2610 REV E .MATERIAL USED : 2024T3/0.080 PO# 2021-147804 .

Part: BEAR STRAP — CRACKED (BS 295) · airframe 74,899 hrs · 44,315 cycles

CRACK INDICATION FOUND AROUND FASTENER LOCATED ON BEAR STRAP AT STA 295 AND 4 INCHES BELOW OF S-8R. L=0.200 INCHES APPROX ; 2021-247728 / [01] TOOL USED PN NORTEC600D SN 60009161631 DUE DATE DEC-01-21; [02] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22.; [03] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22.; [04] NDT MANUAL 51-00-00 TO STEP 7; [05] INSPECTION WAS DONE; [06] TOOL USED : PRECISION BALANCE MICELLANEOUS P/N : PPC-200W S/N : 090199 DUE DATE : 27- JAN - 22; [07] SUMMARY EA 21-153-01659 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q0059ZS8.; [08] PERFORMED REPAIR ON BEAR STRAP LOCATED BETWEEN BS 277 AND BS 320 AND BETWEEN STRG 6R AND STRG 11R IAW EA 21-153-01659 SUMMARY AND EA 21-153-01659-WIP 1; [09] PERFORMED REPAIR ON BEAR STRAP LOCATED BETWEEN BS 277 AND BS 320 AND BETWEEN STRG 6R AND STRG 11R IAW EA 21-153-01659 SUMMARY AND EA 21-153-01659-WIP 1; [10] PERFORMED REPAIR ON BEAR STRAP LOCATED BETWEEN BS 277 AND BS 320 AND BETWEEN STRG 6R AND STRG 11R IAW EA 21-153-01659 SUMMARY AND EA 21-153-01659-WIP 1

Part: STRINGER — CRACKED (BS 540 S23L) · airframe 74,899 hrs · 44,315 cycles

CRACK STRINGER 23L LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-257660 / [01]. REPAIRED STRINGER 23L LOCATED BS 540 FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1; [04] REPAIRED STRINGER 23L LOCATED BS 540 FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1; [05] REPAIRED STRINGER 23L LOCATED BS 540 FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1. COMPLETE RII INSPECTION.

Part: STRINGER — CRACKED (BS 540 S24L) · airframe 74,899 hrs · 44,315 cycles

CRACK STRINGER 24L LOCATED BS540 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STR 24L LOCATED BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T0/0.045 PO 2021 134008 1 AND 7075- T0/0.050 PO 2021 139514 1; [06] PERFORMED PERMANENT REPAIR ON STR 24L LOCATED BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED 7075-T0/0.045 PO 2021 134008 1 AND 7075- T0/0.050 PO 2021 139514 1.. RII ITEM

Part: STRINGER — CORRODED (BS 540 S26L) · airframe 74,899 hrs · 44,315 cycles

CORROSION STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT. REPAIRED STRINGER 26L LOCATED BS 540 AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1; [07] REPAIRED STRINGER 26L LOCATED BS 540 AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1; [08] REPAIRED STRINGER 26L LOCATED BS 540 AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1<BR>RII

Part: STRINGER — CRACKED (BS 540) · airframe 74,899 hrs · 44,315 cycles

CRACK STRINGER 25R LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-257673 / [01] TOOL USED DIGITAL CALIPER P/N:700-113-10 S/N:0013356 DUE DATE 02-APR-21; [02] TOOL USED PN: 45MG; SN: 130060401; DUE DATE: 22 APR 22.; [03] TOOL USED P/N: NORTEC 500D; S/N: N500X11290U021704; DUE DATE: 08-OCT-21; [04] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [05] UPDATED TOOL INFORMATION (DUE DATE) OF #1 CORRECTIVE ACTION: CALIPER P/N:700-113-10 S/N:0013356 DUE DATE 02-APR-22; [06] REPAIRED STRINGER 25L LOCATED BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; [07] REPAIRED STRINGER 25L LOCATED BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. COMPLETE RII INSPECTIONS

Part: SPAR WEB — CORRODED (RT WING) · airframe 74,899 hrs · 44,315 cycles

CORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APROX. AND WBL 94.24 AT RT WING ; 2021-257643 / [01] TOOL USED: CALIPER P/N 700-113-10 S/N 0031753 CAL DUE DATE: 30 SEP 21.; [02] TOOL USED P/N NORTEC500D S/N N500X11290U021704 DUE DATE : 08-OCT-21.; [03] TOOL USED P/N NORTEC500D S/N N500X112900U021704 DUE DATE : 08-OCT-21.; [04] TOOL USED DIGITAL CALIPER; P/N: 700-113-10; S/N: 0010815; DUE DATE: 06/MAY/22; [05] TOOL USED P/N 45 MG S/N 130064101 DUE DATE 11/MAR/22; [06] SUMMARY EA 21-157-01723 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q0059XDE.; [07] REPAIRED FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APROX. AND WBL 94.24 AT RT WING IAW EA 21-157-01723; [08] REPAIRED FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APROX. AND WBL 94.24 AT RT WING IAW EA 21-157-01723

Part: BULKHEAD WEB — CRACKED (BS 663 RBL11) · airframe 74,899 hrs · 44,315 cycles

CRACK ON VAPOR BARRIER LOC ON BS 663 RBL 11. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10 REPAIR 10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,544 hrs · 44,105 cycles

L/H OVERWING EMERGENCY EXIT LT INOP. / RE-LAMPED L/H OVER WING EMERGENCY EXIT LT IAW AMM 33-51-04.

Part: SIGN — LOOSE (CABIN) · airframe 74,364 hrs · 44,003 cycles

CABIN OVERWING EXIT CEILING SIGN IS LOOSE / R&R'D CABIN OVERWING EXIT CEILING SIGN ASSEMBLY PER MM 33-51-01

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 73,664 hrs · 43,583 cycles

COVER MISSING ON OVERHEAD BIN EMERGENCY AISLE LIGHT, SEAT 14C. OK TO CONTINUE, PER MEL 33-15-02 SP1 TKG NR 60549. REPLACED MISSING EMERGENCY LIGHT LENS AT OVERHEAD BIN 14ABC, PER SIP CLR 60645.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 73,664 hrs · 43,583 cycles

14ABC EMERGENCY AISLE LIGHT OVERHEAD BIN LENS MISSING. OK TO CONTINUE, PER MEL 25-10-01 SP1B TRG NR 60550. REPLACED MISSING LENS AT OVERHEAD BIN 14ABC, PER SIP CLR NR 60644.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,059 hrs · 43,199 cycles

3 EACH EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST / REMOVED AND REPLACED 3 EACH EMERGENCY LIGHTING BATTERY PACKS AT LOCATIONS M1672; M1674; AND M1675 PER AMM 33-51-06 AND ENG DWG 33500005.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,605 hrs · 42,921 cycles

OVERWING EXIT LIGHT RH IS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 71,232 hrs · 42,084 cycles

DIVERT/DECLARED EMERGENCY----------------------------------------------------------ENGINE DRIVEN PUMP HYDRAULIC A LOW PRESSURE LIGHT ILLUMINATED AND SYSTEM A QUANTITY FELL TO 16%. / R&R #1 ENGINE PUMP PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,907 hrs · 41,216 cycles

R1 DOOR EMERGENCY EXIT LIGHT ABOVE INOP. R&R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,907 hrs · 41,216 cycles

R1 DOOR EMERGENCY EXIT LIGHT ABOVE INOP. R&R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 69,907 hrs · 41,216 cycles

RIGHT HAND OVER WING LOWER FWD EMERGENCY EXIT LIGHT HAS ONE BULB OUT. RELAMPED PER AMM.

Part: LIGHT — INOPERATIVE (ENTRY DOOR) · airframe 69,907 hrs · 41,216 cycles

EMERGENCY EXIT LIGHT INOP. RELAMPED PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 69,907 hrs · 41,216 cycles

EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 69,907 hrs · 41,216 cycles

RT OVERWING ESCAPE HATCH LIGHT ASSY DOES NOT ILLUMINATE. RELAMPED AND PERFORMED GOOD OPERATIONAL TEST PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 69,907 hrs · 41,216 cycles

EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PACK PER MM.

Part: LENS — DAMAGED (CABIN) · airframe 69,907 hrs · 41,216 cycles

EXIT LIGHT ON AFT WALL OF LAV A DAMAGED. R&R EXIT LIGHT IAW AMM.

Part: SPOILER — DEBONDED (SPOILER) · airframe 69,907 hrs · 41,216 cycles

#10 SPOILER IS DISBONDED ON THE UPPER SURFACE. AREA MARKED IN RED / REPAIRED DISBONDED AREA ON #10 SPOILER UPPER SURFACE PER SRM 51-70-10-2R-2 AND SRM 51-70-10-2R-0.

Part: FLAP — DEBONDED (LH OUTBD AFT FLA) · airframe 69,907 hrs · 41,216 cycles

LT WING O/B AFT FLAP I/B LWR T/E IS DISBANDED. / LT WING O/B AFT FLAP I/B LWR T/E DISBONDED WILL BE REPLACED ON CUST CARD #T947279.

Part: CONNECTOR — WORN (CABIN) · airframe 69,907 hrs · 41,216 cycles

EMERGENCY LIGHT CONNECTOR PIN REQUIRES REPLACEMENT. RETERMINATED CONNECTOR W4142 PER WDM.

Part: STRAP — CORRODED (CABIN) · airframe 69,907 hrs · 41,216 cycles

LT OVER WING EXIT HATCH ESCAPE STRAP CORRODED ON MOUNTING END. R&R ESCAPE STRAP IAW AMM.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 69,907 hrs · 41,216 cycles

FLOOR SUPPORT CRACKED BETWEEN BS. 344 TO BS. 360, LBL 11. R & R FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,907 hrs · 41,216 cycles

FLOORBEAM UPPER CHORD CORRODED. REPAIRED FLOORBEAM IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 69,907 hrs · 41,216 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 294 TO 312, RBL 17. R & R FLOOR SUPPORT IAW SRM AND DWG.

Part: CHANNEL — CRACKED (BS 270-360) · airframe 69,907 hrs · 41,216 cycles

FORWARD ENTRY MOPSILL CRACKED BETWEEN BS. 270 TO BS. 360, LBL 60. REMOVED MOPSILL IAW SRM & DWG.

Part: STOP — CORRODED (RT OW EXIT) · airframe 69,907 hrs · 41,216 cycles

***CORROSION*** ON RH OVERWING EXIT LOWER SILL LINING STOP ASSY BS 627; WL 221. / REMOVED AND REPLACED R/H OVERWING EXIT LOWER SILL LINING STOP ASSY AT B.S627; WL221 IAW SRM 51-40-02-0G-0 AND DWG 411A2800.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 69,907 hrs · 41,216 cycles

BULKHEAD STIFFENER CORRODED AT BS. 1088, RBL 27. REPAIRED STIFFENER PER EA.

Part: FAIRING — ELONGATED (LWR FUSELAGE) · airframe 69,907 hrs · 41,216 cycles

PANEL 191D HAS 2 ELONGATED FASTENER HOLES AT DOOR HINGE ATTACH POINT / REPAIRED 2 ELONGATED FASTENER HOLES AT DOOR HINGE ATTACH POINT ON PANEL 191D PER SRM 51-70-05-2R-9 59654U 6-17-19.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,907 hrs · 41,216 cycles

3RD RIB FROM INBOARD END OF R/H HORIZONTAL STABILIZER REMOVABLE LEADING EDGE (LES 95.96) WAS CRACKED. / R&R 3RD RIB IAW SRM AND DWG.

Part: RIB — CRACKED (RH HOR STAB) · airframe 69,907 hrs · 41,216 cycles

R/H HORIZONTAL STA101.90 RIB IS CRACKED AT 1ST STIFFENER FROM LEADING EDGE.MARKED / PERFORMED HFEC INSPECTION ON R/H HORIZONTAL STAB RIB AT STA 101.90; NO CRACKS NOTED ON 1ST VERT STIFFENER IAW 737 NDTM PT 6. 51-00-00 PROC 23.

Part: STIFFENER — CRACKED (RH HOR STAB) · airframe 69,907 hrs · 41,216 cycles

R/H HORIZONTAL STA120.30 RIB IS CRACKED AT 3RD STIFFENER FROM LEADING EDGE.MARKED / REPAIRED RT HORIZ STAB RIB 3RD STIFFENER FROM LE AT STAB STA 120.30 IAW SRM 55-10-09-2R-4

Part: STIFFENER — CRACKED (LH HOR STAB) · airframe 69,907 hrs · 41,216 cycles

L/H HORIZONTAL STA129.50 RIB IS CRACKED AT 3RD STIFFENER FROM LEADING EDGE.MARKED / REPAIRED L/H HORIZONTAL STAB RIB @ STA 129.5 PER SRM 55-10-09-2R-5 56304R 27JUN19

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 69,907 hrs · 41,216 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS. 480 TO BS. 520, LBL 45. / R&R SEAT TRACK PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,907 hrs · 41,216 cycles

INTERCOSTAL CORRODED. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,907 hrs · 41,216 cycles

SEAT TRACK CROWN CORRODED. R&R SEAT TRACK IAW SRM, DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,907 hrs · 41,216 cycles

SEAT TRACK CROWN CORRODED. R&R SEAT TRACK IAW SRM, DWG.

Part: SUPPORT — CORRODED (BS 727D-787) · airframe 69,907 hrs · 41,216 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 727D TO BS. 787, LBL 23. / REPAIRED SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (BS 303) · airframe 69,907 hrs · 41,216 cycles

R1 DOOR SCUFF PLATE INBOARD SUPPORT CORRODED AT BS. 303, RBL 62. / R&R SUPPORT PER SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 69,907 hrs · 41,216 cycles

FORWARD CARGO BAY BULKHEAD GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET PER SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 550-727B) · airframe 69,907 hrs · 41,216 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS. 550 TO BS. 727B, LBL 25. / R&R SEAT TRACK PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,907 hrs · 41,216 cycles

SCUFF PLATE SUPPORT CORRODED. R&R SUPPORT IAW SRM, DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,907 hrs · 41,216 cycles

SEAT TRACK CROWN CORRODED. R&R SEAT TRACK PER SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,907 hrs · 41,216 cycles

CREASE BEAM WEB CORRODED AT BS. 862, LBL 66. R&R WEB PER SRM, EA, & DWG.

Part: CHANNEL — CORRODED (AFT SERVICE DOOR) · airframe 69,907 hrs · 41,216 cycles

***CORROSION*** ON AFT SERVICE DOOR MOP SILL AT B.S. 960-986; R.B.L. 50; W.L. 208.1. / REMOVED CORROSION ON ASD MOPSILL BS 960-986; RBL50 WL208; REMOVED .017' 1' X 1' FROM .080' OUT OF LIMITS PER SRM 51-10-02-0G-0; SRM 53-70-15-1A-1; REMOVED AND INSTALLED NEW ASD MOPSILL PER DWG 147A0000; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND SRM 51-40-08-0G-0.

Part: ATTACH BRACKET — CRACKED (MAIN CABIN) · airframe 69,907 hrs · 41,216 cycles

CRACK AT BIN RAIL ATTACH BRACKET FASTENER AT B.S. 36 0 AT STRINGER 8R.R. / ACCOMPLISHED REPAIR ON FRAME STA 360 CRACKED AT STRINGER 8R IAW EA #1-A53-12114 REV 4 59192U 18JUN19

Part: GUSSET — CRACKED (BS 500D) · airframe 69,907 hrs · 41,216 cycles

FORWARD CARGO BAY BULKHEAD GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET PER SRM AND DWG.

Part: DOOR FRAME — CRACKED (BS 312) · airframe 69,907 hrs · 41,216 cycles

L1 DOOR FRAME CUTOUT CRACKED AT BS. 312, IN THE RADIUS. REPAIRED FRAME IAW EA AND ER.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 69,907 hrs · 41,216 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS727D TO BS767 RBL23 WL156 / EVALUATED CORROSION ON FLOOR TO WALL SUPPORT PLATE; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED; FABRICATED ITEM #BAC1496-327 #7075-T62 LOT# 139572-1; LOCATED; DRILLED; DEBURRED ALL HOLES; APPLIED CHEMICAL CONVERSION COATING; PRIMED; AND INSTALLED R/H FLOOR TO WALL SUPPORT BS727-767 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-20-01-0G-0; AMM 51-21-72-370-804; AND DWG 146A7502. 57151U 17JUN19

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,907 hrs · 41,216 cycles

SCUFF PLATE SUPPORT CORRODED. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,907 hrs · 41,216 cycles

SCUFF PLATE SUPPORT CORRODED. R&R SUPPORT IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 69,907 hrs · 41,216 cycles

AFT CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / AFT CARGO BAY; FWD CORNER SCUFF PLATE REPAIRED PER EA 1-A53-2076; REV 11.

Part: ANGLE — CRACKED (RT WHEEL WELL) · airframe 69,907 hrs · 41,216 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L 12; W.L. 162. / B.S 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE AT RBL 12 WL 162 WAS REPAIRED PER ATS ER 19-03533 REV IR AND SWA EA# 1-757-16337 REV IR

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 69,907 hrs · 41,216 cycles

L2 DOOR EMERGENCY LIGHT LENS DISCOLORED. R&R LENS IAW AMM.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 69,907 hrs · 41,216 cycles

THE FORWARD SERVICE DOOR LWR -14 BEAM IS CRACKED IN THE RADIUS / THE FORWARD SERVICE DOOR LWR -14 BEAM WAS REPLACED ON CUSTOMER R.O. NO. 0520055-EWR AND JOB # 524226.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 69,907 hrs · 41,216 cycles

L2 DOOR EXIT LIGHT LENS DISCOLORED. / R&R LENS IAW AMM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 69,907 hrs · 41,216 cycles

FORWARD ENTRY CENTER LOWERED CEILING PANEL EXIT LENS DISCOLORED. R&R LENS IAW AMM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 69,907 hrs · 41,216 cycles

R2 DOOR EMERGENCY LIGHT LENS DISCOLORED. R&R LENS IAW AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 69,907 hrs · 41,216 cycles

FWD CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / FWD CARGO BAY; FWD CORNER SCUFF PLATE REPAIRED PER EA 1-A53-2076. REV 11

Part: LENS — FADED (EMERGENCY LIGHT) · airframe 69,907 hrs · 41,216 cycles

L1 DOOR OVERHEAD EMERGENCY LENS DISCOLORED. R & R LENS IAW AMM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 69,907 hrs · 41,216 cycles

R1 DOOR OVERHEAD EMERGENCY LENS DISCOLORED. R & R LENS IAW AMM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 69,907 hrs · 41,216 cycles

R2 DOOR EXIT LIGHT LENS DISCOLORED. R&R LENS IAW AMM.

Part: LENS — BROKEN (SERVICE DOOR) · airframe 69,907 hrs · 41,216 cycles

SLIDE VIEWING WINDOW DAMAGED. R&R SLIDE VIEWING WINDOW IAW AMM.

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 69,907 hrs · 41,216 cycles

FLOOR CREASED. REPAIRED IAW EA.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 69,675 hrs · 41,084 cycles

COCKPIT FLOOR CREASED ALONG FLOORBEAM BETWEEN BS. 254.5 TO BS. 259.5, LBL 15.33. REPAIRED FLOORBEAM IAW EA.

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 69,675 hrs · 41,084 cycles

COCKPIT FLOOR CREASED. REPAIRED COCKPIT FLOOR PER EA.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 69,675 hrs · 41,084 cycles

COCKPIT FLOOR CREASED ALONG FLOORBEAM BETWEEN BS. 254.5 TO BS. 259.5, LBL 4.33. REPAIRED FLOORBEAM IAW EA.

Part: WINDOW FRAME — GOUGED (CABIN) · airframe 69,675 hrs · 41,084 cycles

WINDOW FRAME GOUGED. R&R CABIN WINDOW FRAME PER SRM AND DWG.

Part: COVER — MISSING (CABIN) · airframe 68,197 hrs · 40,135 cycles

LT EMERGENCY EXIT BULLNOSE LENS COVER MISSING AT ROW 12. INSTALLED COVER PER SIP.

Part: BATTERY — FAILED (CABIN) · airframe 67,632 hrs · 39,761 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01675. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 67,632 hrs · 39,761 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01672. R&R BATTERY PER MM.

Part: RADOME — DELAMINATED (FWD FUSELAGE) · airframe 67,632 hrs · 39,761 cycles

NOSE RADOME LEFT UPPER SIDE APPROX. 11 O'CLOCK AFT LOOKING FWD HAS DELAMINATED SPOT APPROX. 6'X2' DELAM STARTS 3' FWD OF AFT END. IN DELAMINATED AREA AREA THERE IS COUPLE SPOTS APPROX. .5'X.5' MISSING SEVERAL PLIES 4'; 5.75'; 6.75'; 11.5' FWD OF THE AFT EDGE. / REMOVED AND REPLACED PER AMM 53-52-00 TAG NO: UNK PN ON: 1061002-70 SN ON: 171700 PN OFF: SN OFF: 867272

Part: SUPPORT — CRACKED (LOWER EXT FUSELA) · airframe 67,632 hrs · 39,761 cycles

KEEL BEAM PNL 192E FWD LEFT SUPPORT CRACKED. / REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02

Part: BATTERY — FAILED (CABIN) · airframe 67,632 hrs · 39,761 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01670. R&R BATTERY PER MM.

Part: COVER — MISSING (CABIN) · airframe 67,436 hrs · 39,645 cycles

LT SIDE OVERWING EMERGENCY EXIT LIGHT COVER MISSING. R&R COVER PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 66,554 hrs · 39,075 cycles

CEILING EMERGENCY EXIT LIGHT INOP AT ROW 11. R&R CHARGER ASSEMBLY PER AMM.

Part: LIGHT — UNSECURE (ROW 11ABC) · airframe 66,214 hrs · 38,862 cycles

EMERGENCY LIGHT LOOSE AT ROW 11ABC. SECURED THE LIGHT ASSY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 65,419 hrs · 38,360 cycles

BATTERY PACKS FAILED TEST AT LOCATION M0168. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 65,419 hrs · 38,360 cycles

BATTERY PACKS FAILED TEST AT LOCATION M0166. R&R BATTERY PACK PER AMM.

Part: FITTING — CORRODED (RT MLG) · airframe 64,766 hrs · 37,935 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LUG FACE CORRODED. REPAIRED THE FITTING IAW EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 64,756 hrs · 37,930 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FITTING CORRODED. REPAIRED THE FITTING IAW EA.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 64,507 hrs · 37,770 cycles

DECLARED EMERGENCY, AT FL 320 LT PACK TRIP FOLLOWED BY RAPID DECOMPRESSION. R&R NR 2 ENGINE HIGH STAGE REGULATOR PER AMM.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 64,507 hrs · 37,770 cycles

DECLARED EMERGENCY, AT FL 320 LT PACK TRIP FOLLOWED BY RAPID DECOMPRESSION. R&R NR 1 ENGINE HIGH STAGE REGULATOR PER AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

FRAME WEB CORRODED AT BS 1006, BETWEEN STR 27R TO STR 26L. REPAIRED WEB PER SRM AND DWG.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

FRAME FAIL SAFE CHORD CORRODED AT BS 1006, STR 27L. REPAIRED FAIL SAFE PER SRM AND DWG.

Part: STRINGER CLIP — CORRODED (BS 1006) · airframe 63,434 hrs · 37,107 cycles

STRINGER CLIP 27L CORRODED AT BS 1006. R & R THE STRINGER CLIP IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

STRINGER CORRODED AT BS 1016, STR 27L. REPAIRED STRINGER IAW SRM.

Part: FITTING — CORRODED (BS 1016) · airframe 63,434 hrs · 37,107 cycles

FITTING CORRODED AT BS 1016, STRINGER 26L. R & R THE FITTING IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

FLOORBEAM FRAME SPLICE CORRODED AT BS 1016, FRAME BETWEEN STR 26L TO STR 27R. R&R FRAME SPLICE IAW DWG & SRM.

Part: STRINGER — CRACKED (LT WING) · airframe 63,434 hrs · 37,107 cycles

LT WING INBOARD FIXED LEADING EDGE STRINGER CRACKED AT WSTA 204.25. R&R STRINGER IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

LAV B FLOOR SUPPORT CORRODED AT BS 1014, LBL 40. R&R SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

FLOORBEAM HORIZONTAL FLANGE CORRODED AT BS 1016, LBL TERMINATING END. REPAIRED FLOORBEAM IAW ER & EA.

Part: TEE FITTING — CRACKED (BS 680) · airframe 63,434 hrs · 37,107 cycles

TEE FITTING CRACKED AT BS 680, RBL 25. R & R THE TEE FITTING IAW SRM & DWG.

Part: ANGLE — ELONGATED (CABIN) · airframe 63,434 hrs · 37,107 cycles

OUTBOARD SUPPORT ANGLE FOR INTERCOSTAL AT RBL 8; BS 986 HAS AN ELONGATED FASTENER HOLE. / REPAIRED OUTBOARD SUPPORT ANGLE FOR INTERCOSTAL AT RBL 8; B.S. 986 IAW ER 17-02794 REV IR & EA 1-753-31347 IR

Part: WEB — CORRODED (BS 980-993) · airframe 63,434 hrs · 37,107 cycles

R2 DOOR LOWER SILL MAIN THRESHOLD WEB CORRODED BETWEEN BS 980 TO 993, WL 208. R & R THE WEB IAW SRM.

Part: ANGLE — CORRODED (BS 967-986) · airframe 63,434 hrs · 37,107 cycles

R2 DOOR MOPSILL SUPPORT ANGLE CORRODED BETWEEN BS 967 TO 986. R & R THE ANGLE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 947) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY FLOOR SUPPORT CRACKED AT BS 947, RBL 20. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: SKIN — DELAMINATED (R/H WING) · airframe 63,434 hrs · 37,107 cycles

#7 SPOILER PANEL LOWER SKIN DENT 47.8' FROM I/B EDGE AND 10' FROM AFT EDGE IS OUT OF LIMITS AND DELAMINATED / REPAIRED DENT ON #7 SPOILER PANEL LOWER SKIN 47.8' FROM I/B EDGE AND 10' FROM AFT EDGE PER SRM 51-70-10-2R-3 AND SRM 51-70-10-2R-0.

Part: BAFFLE — DAMAGED (BS 500A-500B) · airframe 63,434 hrs · 37,107 cycles

FORWARD CARGO BAY BAFFLE DAMAGED BETWEEN BS 500A TO 500B, LBL 20. REPAIRED THE BAFFLE IAW EA.

Part: INTERCOSTAL — ELONGATED (FWD CARGO RH) · airframe 63,434 hrs · 37,107 cycles

FWD CARGO BAY INTERCOSTAL HAS MULTIPLE ELONGATED HOLES BS 420-440 RBL 22 / REMOVED DAMAGED INTERCOSTAL AND REPLACED WITH A NEW INTERCOSTAL AT FWD CARGO BAY BS 420 TO BS 440; RBL 22 IAW DWG. #143A8121 AND DWG. #143A8122 AND SRM 51-40-02-0G-0; PARG. 4.B AND 7.D. 88964U 01JUN17

Part: FLOORBEAM — CORRODED (BS 328) · airframe 63,434 hrs · 37,107 cycles

FLOORBEAM CORRODED AT BS 328, RBL 50. REPAIRED THE FLOORBEAM IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,434 hrs · 37,107 cycles

FWD ENTRY FLOORPANEL 221GF FWD LEFT CORNER DAMAGED. / REPAIRED DAMAGE ON FWD ENTRY FLOOR PANEL 221GF IAW SRM 53-00-50-2R-2 AND SRM 53-00-50-2R-6. 56749U 29MAY17

Part: CARGO TRACK — CORRODED (BS 727-867) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY CARGO TRACK CORRODED BETWEEN BS 727 TO 867, LBL 17. REPAIRED CARGO TRACK IAW SRM.

Part: BEAM — CORRODED · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** ON B.S. 986 FLOOR BEAM UPPER SURFACE LBL 30-45. / BLENDED CORROSION ON BS 986 FLOORBEAM UPPER SURFACE LBL 30-45 15' X 2.0' X .030' ORIGINAL THICKNESS .150' FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1 TOP CHORD TO BE REPAIRED ON CUSTOMER CARD #T662612

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 63,434 hrs · 37,107 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294.5, BL 0. R & R THE FLOOR SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** AFT CARGO BAY FLOOR SUPPORT BS800-815 RBL19. / ALL WORK IS ACCOMPLISHED ON CUSTOMER CARD T662690

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

FORWARD CARGO RT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 430 TO BS 440, RBL 20. R&R PLATE IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (BS 790-847) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY SUB THRESHOLD CORRODED BETWEEN BS 790 TO 847, RBL 25. R & R THE THRESHOLD IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, BETWEEN RBL 20 TO LBL 20. R&R ANGLE IAW SRM & DWG.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

L1 DOOR GIRT BAR AFT SUPPORT FITTING CORRODED AT BS 312. R&R FITTING IAW SRM.

Part: SUPPORT PLATE — CORRODED (FWD CARGO BAY) · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** FWD CARGO FLOOR TO SIDEWALL SUPPORT PLATE; LH BS 500A TO BS 500D; LBL 20 / EVALUATED DAMAGE AND WAS FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2. 4(A). SUPPORT WILL BE REMOVED AND REPLACED ON CARD # T662663 (FUSE 5125) 86750U 26MAY17.

Part: CARGO TRACK — CORRODED (BS 727-887) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY SEAT TRACK CORRODED BETWEEN BS 727 TO 887, RBL 13.8. R & R THE CARGO TRACK IAW SRM.

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** FWD CARGO DOORWAY SUB-THRESHOLD WEB; BS 440 - BS 495; SEVERAL AREAS / REMOVED AND REPLACED FWD CARGO DOORWAY SUB-THRESHOLD WEB; BS 440 - BS 495 IAW SRM 51-40-02 83802U 27MAY17

Part: SIDEWALL SUPPORT — CORRODED (BS 500A-500D) · airframe 63,434 hrs · 37,107 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500A TO 500D, RBL 20. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** AFT CARGO BAY FLOOR PNL 140CF HAS CORROSION AROUND EDGES / EVALUATED CORROSION ON AFT CARGO BAY FLOOR PANEL 140CF FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. FABRICATED REPLACEMENT FLOOR PANEL 140CF IAW BOEING DWG 453A2610; SRM 53-60-53; AMM 51-21-41 AND AMM 51-21-72

Part: STRAP — CORRODED (BS 767) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY FLOORBEAM STRAP CORRODED AT BS 767, LBL 12. REPAIRED THE STRAP IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

R1 DOOR FORWARD LOWER STUB BEAM CRACKED AT BS 295, WL 209. REPAIRED STUB BEAM IAW ER AND EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 790, RBL 20. R&R SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 34. R&R INTERCOSTAL PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 63,434 hrs · 37,107 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 328 TO 344, LBL 46. R & R THE FLOOR SUPPORT IAW SRM.

Part: STRAP — CORRODED (BS 767) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY FLOORBEAM STRAP CORRODED AT BS 767, RBL 8. REPAIRED THE STRAP IAW EA.

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** AFT CARGO BAY FLOOR T SPLICE AT BS 767 HAS CORROSION / REMOVED AND REPLACED ACB FLOOR 'T' SPLICE AT F/S 767 PER AMM 25-52-10-400-801. 87667U 19/JUNE/17; AND FIG 406. 87267U 19/JUNE/17

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,434 hrs · 37,107 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, LBL 46. R & R THE FLOOR SUPPORT IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 847-867) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 TO 867, RBL 20. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: STRAP — CORRODED (BS 767) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY FLOORBEAM STRAP CORRODED AT BS 767, LBL 8. REPAIRED THE STRAP IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 63,434 hrs · 37,107 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-767) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO 767, RBL 20. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

L1 DOOR GIRT BAR FORWARD SUPPORT FITTING CORRODED AT BS 312. R&R FITTING IAW SRM.

Part: BRACKET — CRACKED (BS 663) · airframe 63,434 hrs · 37,107 cycles

VERTICAL BRACKET CRACKED AT BS 663, RBL 14.5. R & R THE BRACKET IAW SRM.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** AFT CARGO BAY FLOOR STRAP 887. / EVALUATED ACB FLOOR STRAP TO BE OUT OF LIMITS & IS REPAIRBLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.(C) LOCATED; DRILLED; & COUNTERSUNK NEW PART IAW SRM 51-40-05-0G-0 & SRM 51-40-08-0G-0 56052U 12JUN17

Part: SERVICE DOOR — CORRODED (FWD SERVICE DOOR) · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** ON FORWARD SERVICE DOOR MOP SILL AT B.S. 294-328. / REMOVED CORRODED FWD. SVC. DOOR MOP SILL AND INSTALLED NEW MOP SILL PER SRM 51-40-05-0G-0 FIG. 3 & FIG 4. AND SRM 51-40-02-0G-0 PAR. 4 AND PAR. 7. CORROSION WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-15-1A-2 FIG. 103. D. 8528C 30MAY17

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** AFT CARGO BAY CROSS STRAP BS727E+4. / REMOVED AND REPLACED ACB FLOOR CROSS 'T' STRIP AT F/S 727E+4 PER AMM 25-52-10-400-801 87667U 19/JUN/17 AND FIG 406. 87667U 19/JUNE/17

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

FLOORBEAM UPPER SURFACE CORRODED AT BS 986, BETWEEN RBL 30 TO RBL 45. REPAIRED FLOORBEAM IAW ER AND EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY AFT SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO BAY - AFT SCUFF PLATE PER EA# 1-A53-2076 REV. 11

Part: STRAP — CORRODED (AFT CARGO THRESH) · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** LOWER SIL I/B STRAP BS812 RBL19. / REMOVED LOWER SIL I/B STRAP AT BS 769 TO BS 857 RBL 19 AND INSTALLED NEW LOWER SIL I/B STRAP PN 146A8128U1 PO #628488 IAW SRM 51-40-02 57049U 02JUN17 DWG. 146A8120

Part: SIDEWALL SUPPORT — CORRODED (BS 420-500A) · airframe 63,434 hrs · 37,107 cycles

LEFT FORWARD CARGO FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 420 TO 500A. R & R SIDEWALL SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS867-947 RBL20. / REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS 867-947; RBL 20; EVALUATED CORROSION: L = 2.50'; W = 1.00'; D = 0.006'; FOUND OUT OF LIMITS I.A.W. SRM 53-60-53-1A-0; VIEW D; A-A; INSTALLED NEW FLOOR TO SIDEWALL SUPPORT. AT BS 867-947; RBL 20. I.A.W. SRM. 51-40-02-0G-0 88919U 26MAY17.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 20. R&R SUPPORT PER SRM.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 495 TO BS 500A RBL 20. R&R PLATE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (BS 500D) · airframe 63,434 hrs · 37,107 cycles

FORWARD CARGO FLOOR TO AFT BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 15 TO RBL 15. R & R THE SUPPORT ANGLE IAW SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 63,434 hrs · 37,107 cycles

FWD CARGO DOORWAY AFT CORNER SCUFF PLATE CRACKED / ACCOMPLISHED FWD CARGO DOORWAY AFT CORNER CRACKED SCUFF PLATE PER EA 1-A53-2076R11(T662585) REPAIRED. INSTALLED SCUFF PLATE-FWR CARGO DOORWAY (AFT CORNER) PER AMM 53-11-02-420-801

Part: PLATE — CRACKED (LEFT WING) · airframe 63,434 hrs · 37,107 cycles

L/W T/E LOWER REAR SPAR CORRIGATED PLATE AT ORSS 261 IS CRACKED. / REMOVED AND REPLACED L/W T/E LOWER REAR SPAR CORRIGATED PLATE AT ORSS 261 IAW SRM 51-40-05-0G-0 AND SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (R/H WING) · airframe 63,434 hrs · 37,107 cycles

RT WING FIXED LEADING EDGE SKIN HAS DENT WITH CRACK AT FASTENER @ APROX WBL 71.4 AND 2.5' IB OF LIGHT COMPARTMENT / RT WING FIXED L/E DENT ON L/E SKIN WILL BE INVESTIGATED ON CUST. CARD #T947380.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 63,434 hrs · 37,107 cycles

FORWARD LT WINDSCREEN FLASHLIGHT CRADLE CRACKED. R & R THE CRADLE IAW SOPM.

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 63,434 hrs · 37,107 cycles

***CORROSION*** NOTED ON LAV SERVICE DOOR (145AL) INTERIOR SURFACE 'MARKED'. / REMOVED AND REPLACED LAV SERVICE DOOR (145AL) IAW SRM 51-10-02-0G-0 SRM 51-40-02-0G-0; AMM 52-49-07-400-80 EXTERIOR FINISH TO BE APPLIED ON CUST CARD #T662839

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 63,434 hrs · 37,107 cycles

AFT CARGO COMPARTMENT DOOR CUTOUT CENTER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,204 hrs · 36,966 cycles

RT OVERWING EXIT LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: COVER — UNSECURE (CABIN) · airframe 63,192 hrs · 36,961 cycles

RT FORWARD GALLEY EMERGENCY LIGHT COVER FELL OFF. R&R LIGHT ASSEMBLY IAW MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 63,180 hrs · 36,954 cycles

RIGHT AFT GALLEY DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LENS IAW AMM.

Part: ACTUATOR — INOPERATIVE (FUEL SYSTEM) · airframe 61,874 hrs · 36,156 cycles

ON DESCENT/APPROACH NOTED FUEL IMBALANCE, ATTEMPTED CROSSFEED BUT SWITCH INOP. / R&R ENGINE FUEL CROSSFEED VALVE ACTUATOR PER AMM.

Part: RIB — CRACKED (LT WING) · airframe 61,577 hrs · 35,977 cycles

LEFT WING FIXED UPPER TRAILING EDGE PANEL CENTER SUPPORT RIB CRACKED. R & R THE RIB IAW AMM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 61,577 hrs · 35,977 cycles

R1 DOOR FRAME NR 4 AND 5 CRACKED AT FORWARD END OF DOOR MECHANISM BOX ATTACHMENT BOLTS. R & R DOOR IAW AMM.

Part: PIN — CORRODED (LT MLG TRUNNION) · airframe 61,380 hrs · 35,855 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING PIN CORRODED. / R&R PIN PER DWG.

Part: LENS — LOOSE (CABIN) · airframe 58,789 hrs · 34,335 cycles

LOWER FWD SERVICE DOOR EMER LIGHT EXIT LENS LOOSE. SECURED LENS IAW EA.

Part: LIGHT — LOOSE (CABIN) · airframe 57,648 hrs · 33,688 cycles

EMERGENCY EXIT PATH LIGHTING STRIP LOOSE BETWEEN ROW 8 - 9. SECURED STRIP IAW SIP.

Part: SHIELD — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

LOWER BULKHEAD FIBERGLASS DUST SHIELD CRACKED AT BS 540, LBL 12. REPAIRED FIBERGLASS IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,623 hrs · 33,673 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 11. R & R LAMP IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME WEB CRACKED AT BS 259, WL 256 RT SIDE. REPAIRED WEB IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

LEFT FRAME WEB CRACKED AT BS 259, WL 256. REPAIRED WEB IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME WEB CRACKED AT BS 251, WL 228 LT SIDE. REPAIRED WEB IAW ER & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,623 hrs · 33,673 cycles

RIGHT HORIZONTAL STABILIZER STATION 92.70, VERTICAL RIB STIFFENERS CRACKED AT LOWER END. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,623 hrs · 33,673 cycles

RIGHT HORIZONTAL STABILIZER STATION 157.10 AFT INBD HOLE ON RIB CRACKED. REPAIRED RIB IAW EA & ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 727B, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,623 hrs · 33,673 cycles

EXTERNAL POWER PANEL CUT OUT CRACKED AT LOWER EDGE. REPAIRED CUT OUT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,623 hrs · 33,673 cycles

LEFT WING NR 3 LE SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,623 hrs · 33,673 cycles

RIGHT WING NR 7 LE SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,623 hrs · 33,673 cycles

LEFT WING NR 1 LE SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 57,388 hrs · 33,532 cycles

RIGHT WW FLOOR PRESS DECK CRACKED AT BS 663-75, RBL 37.5. REPAIRED DECK IAW EA.

Part: FLAP — CRACKED (LT WING) · airframe 53,073 hrs · 31,000 cycles

LEFT WING NR 1 LE KREUGER FLAP CRACKED AT THE INBD END. R & R FLAP IAW MM.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 52,034 hrs · 30,400 cycles

RT WINDSHIELD ARCED. R & R RT WINDSHIELD ASSEMBLY IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 50,880 hrs · 29,737 cycles

AFT GALLEY EMERGENCY LIGHT LENS BROKEN. R&R LENS IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 50,880 hrs · 29,737 cycles

L1 DOOR EMERGENCY LIGHT LENS BROKEN. R&R LENS IAW MM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 50,880 hrs · 29,737 cycles

OPC LAPTOP CHARGING CRADLE MOUNT PLATE CRACKED AT TOP SIDE. R&R PLATE IAW SRM.

Part: REPAIR — LOOSE (LT MLG WW) · airframe 50,880 hrs · 29,737 cycles

LT WW FWD BULKHEAD LOWER VAPOR BARRIER PREVIOUS PATCH LOOSE AT STATION 663, BAY 2L. REPAIRED PATCH IAW SRM.

Part: REPAIR — LOOSE (LT MLG WW) · airframe 50,880 hrs · 29,737 cycles

LT WW FWD BULKHEAD LOWER VAPOR BARRIER PREVIOUS PATCH LOOSE AT STATION 663, BAY 1L. REPAIRED PATCH IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,880 hrs · 29,737 cycles

HORIZONTAL STIFFENER ON FRONT SIDE OF 663 BULKHEAD LOWER VAPOR BARRIER PANEL RT SIDE CRACKED. R&R STIFFENER IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,880 hrs · 29,737 cycles

AFT EE COMPARTMENT INTERCOSTAL CRACKED BETWEEN STATION 340 TO STATION 360, RBL 1. R&R INTERCOSTAL IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 50,880 hrs · 29,737 cycles

LT WW FWD BULKHEAD VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN LBL 31.83 & LBL 40. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 50,880 hrs · 29,737 cycles

LT WW FWD BULKHEAD VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN LBL 24.92 & LBL 31.83. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 50,880 hrs · 29,737 cycles

LT WW FWD BULKHEAD VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN LBL 40 & LBL 45.64. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,880 hrs · 29,737 cycles

RT WW FWD BULKHEAD VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 31.83 TO RBL 40. REPAIRED WEB IAW SRM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 50,880 hrs · 29,737 cycles

LT NR 3 WINDOW POST FASTENER NR 3 FROM THE BOTTOM CRACKED. REPAIRED POST IAW SWA EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,880 hrs · 29,737 cycles

RT NR 3 WINDOW POST CRACKED AT NR 2 HOLE FROM THE BOTTOM. REPAIRED POST IAW EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 50,880 hrs · 29,737 cycles

LT NR 3 WINDOW POST FASTENER NR 2 FROM THE BOTTOM CRACKED. REPAIRED POST IAW SWA EA.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 50,880 hrs · 29,737 cycles

LT WW FWD BULKHEAD LOWER RT WEB PATCH LOOSE AT BS 663. REPAIRED BULKHEAD IAW SRM.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 50,880 hrs · 29,737 cycles

RT WW FWD BULKHEAD LOWER RT WEB PATCH LOOSE AT BS 663. REPAIRED BULKHEAD IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,880 hrs · 29,737 cycles

RT NR 3 WINDOW POST CRACKED AT NR 3 HOLE FROM THE BOTTOM. REPAIRED POST IAW EA.

Part: HOOK — LOOSE (GIRT BAR) · airframe 50,880 hrs · 29,737 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. REPAIRED HOOK IAW MM.

Part: MOUNT BRACKET — BROKEN (L1 DOOR) · airframe 47,956 hrs · 27,955 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOWAGE HOOK MOUNTNG BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER AMM AND MT.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 45,106 hrs · 26,275 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 45,001 hrs · 26,207 cycles

LT EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 44,122 hrs · 25,703 cycles

DURING SCHEDULED HC CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 44,122 hrs · 25,703 cycles

DURING SCHEDULED HC CHECK, LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT BS 720, LBL 30. RELAMPED IAW MM.

Part: FUSE — BLOWN (CABIN) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT BS 603, RBL 67. REMOVED AND REPLACED FUSE IAW MM.

Part: FUSE — BLOWN (CABIN) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED FUSE IAW MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, EMERGENCY EXIT LIGHT BATTERY PACK INOP AT BS 322, RBL 7. REMOVED AND REPLACED BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT BS 379, LBL 26. RELAMPED IAW MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 709 TO BS 720. REMOVED AND REPLACED WEB PER SRM.

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT FLIGHT COMPARTMENT FWD I/B SEAT TRACK CRACKED. REMOVED AND REPLACED SEAT TRACK IAW MM.

Part: SIGN — CRACKED (CABIN) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT SIGN HOUSING CRACKED. REMOVED AND REPLACED SIGN PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND EMERGENCY EXIT SIGN NEAR L1 DOOR BROKEN. REMOVED AND REPLACED SIGN IAW MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOOR WEB CRACKED BETWEEN BS 328 TO BS 344, LBL 43. REPAIRED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOOR WEB CRACKED BETWEEN BS 312 TO BS 328, LBL 43. REPAIRED WEB IAW SRM AND DWG.

Part: ANGLE — CORRODED (GIRT BAR) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKETS AFT MOUNTING ANGLE CORRODED. REMOVED AND REPLACED ANGLE IAW SRM.

Part: ANGLE — CORRODED (GIRT BAR) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKETS FWD MOUNTING ANGLE CORRODED. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 22. REPAIRED BEAM IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,009 hrs · 25,632 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 42,547 hrs · 24,785 cycles

DIVERSION - AT FL 400 FLIGHT ATTENDANT REPORTED SMELL OF SMOKE AT MID CABIN. SMOKE SMELLED ELECTRICAL IN NATURE. REMOVED AND REPLACED GASPER FAN PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 39,604 hrs · 23,105 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 37,610 hrs · 21,905 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 131.10. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 37,610 hrs · 21,905 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 131.10. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 37,179 hrs · 21,640 cycles

L1 DOOR SIDEWALL EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 37,131 hrs · 21,611 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 4 L/E SLAT I/B END LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,499 hrs · 20,645 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION LUG FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,499 hrs · 20,645 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION LUG FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: STRIP — WORN (CABIN) · airframe 35,305 hrs · 20,519 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP WORN AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 33,895 hrs · 19,656 cycles

L2 DOOR EMERGENCY EVAC SLIDEOUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: ENGINE — STALLED (LEFT) · airframe 32,830 hrs · 19,015 cycles

NR 1 ENG COMPRESSOR STALLED. REMOVED AND REPLACED NR 1 ENG PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,970 hrs · 19,096 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 32,147 hrs · 18,587 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 32,113 hrs · 18,567 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,488 hrs · 17,591 cycles

DURING SCHEDULED HC2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROW 11 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 30,488 hrs · 17,591 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,488 hrs · 17,591 cycles

DURING SCHEDULED HC2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROW 9 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,080 hrs · 17,348 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 11 TO RBL 10. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,078 hrs · 17,357 cycles

DURING SCHEDULED 8Y CHECK, FOUND L2 DOOR LOWER STUB FRAME CRACKED AT BS 296. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 29,608 hrs · 17,062 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 28,044 hrs · 16,185 cycles

DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 28,044 hrs · 16,185 cycles

DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 28,044 hrs · 16,185 cycles

DURING SCHEDULED HC1 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 28,044 hrs · 16,185 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 23,091 hrs · 13,358 cycles

L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,017 hrs · 13,324 cycles

FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,088 hrs · 12,213 cycles

DURING SCHEDULED RON CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,242 hrs · 11,162 cycles

DURING SPV, FOUND AFT FUSELAGE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM.

Part: PIN — DAMAGED (CONNECTOR) · airframe 19,242 hrs · 11,162 cycles

DURING SPV, FOUND FWD CENTER CEILING EMERGENCY EXIT LIGHT INOP. RESEATED PIN 13 ON CONNECTOR D10750 PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 18,155 hrs · 10,557 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN AT BS 500A + 5, BOTTOM CENTERLINE, CORRODED. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 16,019 hrs · 9,347 cycles

DURING SCHEDULED RON, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 15,630 hrs · 9,124 cycles

L2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 14,629 hrs · 8,567 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 14,629 hrs · 8,567 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 1, 2, 3, 7, 17, 20, 22 AND 23. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: TAB — CRACKED (LT AILERON) · airframe 14,629 hrs · 8,567 cycles

DURING SCHEDULED C2 CHECK, FOUND LT AILERON TAB CRACKED ON OUTBD L/E. REMOVED AND REPLACED LT AILERON TAB PER MM.

Part: SKIN — CRACKED (L/E FLAP) · airframe 14,264 hrs · 8,378 cycles

NR 4 L/E FLAP SKIN CRACKED AT WEB STIFFENER. REMOVED AND REPLACED NR 4 L/E FLAP PER MM.

Part: COVER — CRACKED (CABIN) · airframe 12,307 hrs · 7,301 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 10, NR 11, NR 12, NR 13 AND NR 15. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: CAP — MISSING (CABIN) · airframe 12,307 hrs · 7,301 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING AT FWD CABIN. INSTALLED END CAP PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 11,335 hrs · 6,749 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 10,002 hrs · 5,994 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: GIRT BAR — OUT OF POSITION (ENTRY DOOR) · airframe 7,338 hrs · 4,473 cycles

FWD ENTRY DOOR EVAC SLIDE GIRT BAR WOULD NOT ALIGN WITH BRACKETS. REPOSITIONED GIRT BAR PER MM.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 6,965 hrs · 4,270 cycles

DURING SCHEDULED SERVICE CHECK,(SI 11038-55) FOUND RH ELEVATOR TAB OTBD CONTROL ROD BUSHING WORN. R&R BUSHING PER MM.

Part: STOP PIN — OUT OF ADJUST (CARGO DOOR)

AIR TURNBACK - AFT CARGO DOOR LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. REPOSITIONED DOOR BUNGE CORD AND ADJUSTED AFT CARGO DOOR STOP PINS PER MM.