N7744A

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 58,802 hrs · 31,331 cycles

PASSENGER CABIN EMERGENCY FLOOR LIGHTING GLOW STRIP NOT SECURE INBOARD OF FORWARD RIGHT WINDSCREEN. SECURED EMERGENCY FLOOR LIGHTING GLOW STRIP INBOAR OF FORWARD RIGHT WINDSCREEN PER AMM SIP.

Part: FUSE — LEAKING (ZONE 700) · airframe 58,638 hrs · 31,232 cycles

AFTER GEAR RETRACTION LOSS OF HYD SYST. A; HYD A ENG1 AND ELEC2 LOW PRESSURE LIGHTS; FLT CTRL A LOW PRESSURE LIGHTS AND FEEL DIFF PRESS LIGHTS ALL ILLUMINATED AND HYDR A QRT WAS ZERO<[01] FOUND MAIN GEAR RETRACT PRESSURE FUSE LEAKING. R/R MAIN GEAR RETRACT FUSE PER AMM 32-32-21. UP TO SUBTASK E FOR INSTALLATION.

Part: TIRE — BLOWN (ZONE 700) · airframe 58,420 hrs · 31,109 cycles

#2 MAIN TIRE BLOWN ON TAKEOFF FROM MCO. R&R #2 MLG WHEEL AND TIRE ASSY IAW AMM 32-45-11.

Part: SKIN — BULGED (ZONE 500 FLAP) · airframe 58,420 hrs · 31,109 cycles

LH INBD TRAILING EDGE AFT FLAP UPPER FLAP SKIN AREA HAS BULGE 2.5IN FROM TRAILING EDGE AND 7IN FROM INBD EDGE<[01] REF TTG8Q013J5AB FOR REMOVAL AND INSTALLATION OF L/H INBOARD AFT FLAP REF AMM 27-51-12;[02] PERFORMED RII OF LH INBOARD AFT FLAP INSTALLATION ON TTG8Q013J5AB PER AMM 27-51-12

Part: SLIDE — OUT OF LIMITS (ZONE 800) · airframe 57,664 hrs · 30,671 cycles

FA REPORTS AFT SERVICE SLIDE PRESSURE IN RED<[01] R+R AFT SERVICE SLIDE PER MT 725-61-06

Part: SEAL — CRACKED (ZONE 300) · airframe 57,526 hrs · 30,589 cycles

R/H HORIZONTAL STABILIZER FORWARD UPPER SLIDER CRACKED/TORN<[01] REMOVED AND REPLACED SEAL PER AMM 53-31-31.;[02] C/W INSPECTION OF REMOVED AND REPLACED SEAL PER AMM 53-31-31.

Part: SEAL — CRACKED (ZONE 300) · airframe 57,526 hrs · 30,589 cycles

L/H HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL CRACKED/TORN<[01] REMOVED AND REPLACED SEAL PER AMM 53-31-31.;[02] C/W INSPECTION OF REMOVED AND REPLACED SEAL PER AMM 53-31-31.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

AFT GALLEY ENTRY DOOR LOWER EMERGENCY EXIT LOCATOR SIGN HAS INOP BULBS<[01] RELAMPED AFT GALLEY ENTRY DOOR LOWER EMERGENCY EXIT LOCATOR AND PERFORMED A SATISFACTORY OPERATIONAL TEST WITH NO DEFECTS FOUND; IAW AMM 33-51-01-960-801 STEPS 2(C)(1)(A)4)(C)(2)(A)1)(B)1.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1668 INOP. REMOVED EMERGENCY LIGHT BATTERY PACK M1668 AND INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED INSTALLATION TEST PER AMM 33-51-06-960-805; LIGHTS STILL INOP. REMOVED EMERGENCY LIGHT BATTERY CHARGER M1668 AND INSTALLED SERVICEABLE CHARGER AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-806; ALL LIGHTS NOW FUNCTIONAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

FWD EMERGENCY CEILING COVE LIGHT INOP. REMOVED; REPLACED AND PERFORMED GOOD OPS CHECK OF THE FWD EMERGENCY CEILING COVE LIGHT IAW AMM 33-51-03-960-801.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITHS STEPS

Part: WIRE — BROKEN (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

EMERGENCY EXIT LIGHT JUST FWD OF R/H OVERWING EXIT HAS A BROKEN WIRE; W4142. RETERMINATED PLUG SIDE OF D3666 PER WDM 33-51-21 AND SWPM 20-30-12; AND PERFORMED GOOD FUNCTIONAL TEST OF EMERGENCY EXIT LIGHT JUST FWD OF R/H OVERWING EXIT PER AMM 33-51-00-710-801.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

CRACKED STR CLIP AT PAX CABIN BS727C S-7L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727C S-7L IAW SRM 51-40-02-0G-0 AND DWG# 146A1103.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: BEAM — CRACKED (ZONE 800) · airframe 56,818 hrs · 30,178 cycles

CRACK FOUND ON FSD NO.4 (141A6536-14) BEAM AT MOST I/B FASTENER LOCATION; L: 0.5' MARKED<[01] UPDATED PARTS REMOVAL;[02] REMOVAL AND REPLACEMENT OF FORWARD SERVICE DOOR WAS ACCOMPLISHED ON CC#TTG8Q00XFLNQ.;[03] VERIFIED CORRECTIVE ACTION ITEM 2.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

CRACKED STR CLIP AT PAX CABIN BS727B S-5L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727B S-5L IAW SRM 51-40-02-0G-0 AND DWG# 146A1102.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

CRACKED STR CLIP AT PAX CABIN BS727D S-6L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727D S-6L IAW SRM 51-40-02-0G-0 AND DWG# 146A1111.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

CRACKED STR CLIP AT PAX CABIN BS727D S-7L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727D S-7L IAW SRM 51-40-02-0G-0 AND DWG# 146A1111.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON PAX CABIN SEAT TRACK CROWN AND WELL AT BS 360+9 TO BS360+18 LBL25 WL208.<[01] REMOVED AND REPLACED SEATTRACK AT BS 360+9 TO BS360+18 LBL25 WL208 IAW B737-7 SRM 51-40-02-0G-0 AND DWG 143A5300; ID: 55; REV:;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: STUB FRAME — CRACKED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CRACK FOUND ON STUB FRAME BS291.5 + 8.5; .2' ABOVE SEAL DEPRESSOR AND .8' IN LENGTH. REMOVED AND REPLACED STUB FRAME FSD UPPER FWD AREA PER SRM 51-40-02 AND DWG 141A8370 REV D.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON AFT CARGO COMPARTMENT AFT BULKHEAD SUPPORT AT STA 947.5; LBL3 AND RBL 15; WL 158.<[01] REJECTED; FOUND CORROSION ON AFT CARGO COMPARTMENT AFT BULKHEAD SUPPORT AT STA 947.5; LBL3 AND RBL 15; WL 158.;[02] REMOVED AND REPLACED ON AFT CARGO COMPARTMENT BULKHEAD SUPPORT AT BS947 FROM RBL 20 TO LBL 8.1 IAW SRM 51-40-02 AND DWG 149A8117 ID: 0006 REV:-;[03] REJECT STEP 4 ITEM 4 AFT CARGO COMPARTMENT BULKHEAD SUPPORT AT BS947 WL158 HAS 5 FASTENER HOLES WITH OVER SIZE COUNTERSINKS. (MARKED);[04] REJECTION WAS VERIFIED ON STEP 4;[05] VERIFIED RII CORRECTIVE ACTION ITEM 2; CARD COMPLETE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 807+2; LBL 24; WL 158.<[01] AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT WITH CORROSION OUT OF LIMITS REMOVED AND REMPLACED IAW SRM 53-00-53-1A-2<BR>AND DWG 146A7500 REV A;[02] REMOVED AND REPLACED ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 847 LBL 24 WL 158 SRM 51-40-02<BR>AND DWG 146A7500 REV: A;[03] VERIFIED RII CORRECTIVE ACTION ITEM 2; CARD COMPLETE.

Part: SHIELD — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT FWD SHIELD FROM STA 767 TO 787; RBL 26; WL 158.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT DOOR CUTOUT FWD SHIELD FROM STA 767 TO STA 787 RBL 26 WL 158<BR>IAW SRM 51-40-02-0G AND DWG # 146A0081 REV:-;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.;[03] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED

Part: SUPPORT — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT FROM STA 727A TO 767; RBL 24; WL 158.<[01] REMOVED AND REPLACED ON AFT CARGO COMPARTMENT FLOOR TO SIDEWAL SUPPORT FROM BS727 TO BS767 RBL24 WL158 IAW SRM 51-40-02 AND DWG 146A7500 ID:0085 REV: A;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON AFT CARGO COMPARTMENT BULKHEAD SUPPORT AT STA 947; RBL 22; WL 159.<[01] REJECTED; FOUND CORROSION ON AFT CARGO COMPARTMENT BULKHEAD SUPPORT AT STA 947; RBL 22; WL 159.;[02] REMOVED AND REPLACED ON AFT CARGO COMPARTMENT BULKHEAD SUPPORT AT BS947 FROM STR 25R TO STR 21R IAW SRM 51-40-02 AND DWG 149A8117 ID: 0006 REV:-;[03] CORRECTIVE ACTION COMPLETED.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241UF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 146A5810 ID:0054.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 231ZF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID:0160.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF ALL OF THE DAMAGE; PANEL 242CF WAS REPLACED WITH A NEWLY FABRICATED PANEL. WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A NOTE; PARAGRAPH 4.A.(2); TABLE 204 AND PARAGRAPH 5. (1); ALSO IAW DRAWING 144A5810 SHEET 125.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

CRACKED INTERCOSTAL AT FWD WET AREA BS317 RBL31 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA<BR>BS 317 RBL 31 WL 208 IAW SRM 51-40-05 AND DWG# 141A5400 REV:C;[02] CORRECTIVE ACTION COMPLETED.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

AFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ACF UPPER SKIN HAD AREAS OF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED RII ITEMS COMPLETE;[03] TASK COMPLETE

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID:0127.

Part: FLOOR PANEL — BUCKLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

AFT FLOOR PANEL 242XF IS BUCKLED IN MIDDLE OF PANEL. DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242XF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).

Part: STRAP — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON STRAP AT MID CABIN BS707 LBL61 WL203. MARKED<[01] 'REFER TO FAULT TTG8Q00XAD3G WHERE EA 24-153-03359 WAS ADDED AS A SUBTASK'.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE. FLOOR PANEL 221EF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON FLOOR SUPPORT AT FWD WET AREA BS303 LBL11 WL208. MARKED<[01] REMOVED AND INSTALLED NEW INTERCOSTALL SUPPORT BETWEEN BS 294 TO BS 312 LBL 11 PER SRM 51-40-02 AND DWG 141A5600 REV B;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.;[03] VERIFIED ITEM 1 AND TASK CARD COMPLETED.

Part: FLOOR PANEL — BUCKLED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

AFT FLOOR PANEL 242SF O/B AFT CORNER IS BUCKLED. AFT FLOOR PANEL 242SF O/B AFT CORNER WITH BUCKLED WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BDWG D1040M003-301; BDWG 147A5810 ID:0058.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 56,818 hrs · 30,178 cycles

PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221CF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF ALL OF THE DAMAGE; PANEL 241BF WAS REPLACED WITH A NEWLY FABRICATED PANEL ALL OF THE WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 1. PARAGRAPH 4.A.(2); TABLE 204 AND PARAGRAPH 5. 1, AND DRAWING 144A5810 SHEET 189.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

CRACKED INTERCOSTAL AT FWD WET AREA BS349 BL0 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN BS 344 TO BS 360 BL 0 WL 208 PER SRM 51-40-02 AND DWG 141A5400 REV -;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: STRAP — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON STRAP AT MID CABIN BS713 RBL61 TO RBL67 WL203. MARKED<[01] 'REFER TO FAULT TTG8Q00XAD3G WHERE EA 24-153-03359 WAS ADDED AS A SUBTASK'.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 222A UPPER SKIN HAS AREAS OF PULLED STRANDS. PANEL 222A UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.

Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 56,818 hrs · 30,178 cycles

PANEL 222DF HAS A DAMAGED GIRT BAR INSERT.<[01] PANEL 222DF DAMAGED INSERTS REMOVED & REPLACED IAW SRM 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED PER [SRM 53-00-50-2R-0-A00938.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF ALL OF THE DAMAGE, PANEL 241EF WAS REPLACED WITH A NEWLY FABRICATED PANEL WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A NOTE; PARAGRAPH 4.A.(2); TABLE 204 AND PARAGRAPH 5. (1); ALSO IAW DRAWING 144A5810 SHEET 129.

Part: STRAP — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON STRAP AT MID CABIN BS713 LBL61 WL203. REMOVED CORROSION; REWORKED; AND TREATED STRAP AT MID CABIN BS713 LBL61 WL203 IAW EA 24-153-03359.

Part: STRAP — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON STRAP AT MID CABIN BS707 RBL61 WL203. MARKED<[01] 'REFER TO FAULT TTG8Q00XAD3G WHERE EA 24-153-03359 WAS ADDED AS A SUBTASK'.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 231MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231MF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221FF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE. PANEL 242AF WAS REPLACED WITH A NEWLY FABRICATED PANEL. ALL OF THE WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A NOTE; PARAGRAPH 4.A.(2); TABLE 204 AND PARAGRAPH 5. (1); ALSO IAW DRAWING 144A5810 SHEET 189.

Part: WEB — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION AT AFT CABIN ON 1016 WEB LBL9 TO LBL15; AND BS1027 LBL7 WL208. MARKED<[01] STEPS 1-2 COMPLETE. REWORKED CORRODED STRUCTURE AND TREATED AT AFT CABIN ON 1016 WEB LBL9 TO LBL15; AND BS1027 LBL7 WL208 IAW EA 24-153-03337.

Part: WEB — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON WEB AT AFT CABIN BS1016+14 BL0 WL208. REFER TO FAULT TTG8Q00X9Q7X WHERE EA 24-153-03337 WAS ADDED AS A SUBTASK.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON FLOOR BEAM AT AFT CABIN BS986 RBL43 WL208.<[01] REMOVED AND REPLACED REPAIR PARTS PER SRM 51-40-02 AS SHOW IN SWA EA#1-753-34154 REV IR;[02] VERIFIED CORRECTIVE ACTION COMPLETE.

Part: STRAP — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON TENSION STRAP AT AFT CABIN BS1016 LBL17 WL208.<[01] REMOVED AND REPLACED AFT CABIN TENSION STRAP BS-1016; LBL17; WL208 IAW SRM 51-40-02-0G-0 AND DWG#147A5600 REV-C;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: STRAP — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON TENSION STRAP AT AFT CABIN BS1016 LBL3 WL208. REMOVED AND REPLACED AFT CABIN TENSION STRAP BS-1016; LBL3; WL208 IAW SRM 51-40-02-0G-0 AND DWG#147A5600 REV-C.

Part: STRAP — CORRODED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CORROSION ON TENSION STRAP AT AFT CABIN BS1016 RBL3 WL208.<[01] REMOVED AND REPLACED AFT CABIN TENSION STRAP BS-1016; RBL3; WL208 IAW SRM 51-40-02-0G-0 AND DWG#147A5600 REV-A;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

CRACKED INTERCOSTAL IN CABIN FLOOR STRUCTURE AT BS380+9 WL208 RBL2.<[01] REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE<BR>BS380-BS400 RBL2 WL208; IAW SRM 51-40-02 & DWG 143A5400;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: BEAM — CRACKED (ZONE 600) · airframe 56,818 hrs · 30,178 cycles

RT WING TRAILING EDGE PANEL BEAM CRACKED AT ORSS 280.<[01] REMOVED AND REPLACED RT WING TRAILING EDGE PANEL BEAM ASSY IAW SRM 51-40-02 AND DWG 115A3712 REV: A<BR> SCREW GUN ID PER2216 CAL DUE 11/2025;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1.;[03] JOB COMPLETE.

Part: ANGLE — CRACKED (ZONE 100) · airframe 56,818 hrs · 30,178 cycles

CRACKED INTERCOSTAL IN CABIN FLOOR STRUCTURE AT BS380+3 AND BS380+13 WL208 RBL11. REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE<BR>BS380-BS400 RBL11 WL208; IAW SRM 51-40-02 & DWG 143A5400.

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 56,818 hrs · 30,178 cycles

CRACKED INTERCOSTAL IN CABIN FLOOR STRUCTURE AT BS380+12 LBL15 WL208. REMOVED AND REPLACED INTERCOSTALL ANGLE ON FLOOR STRUCTURE BETWEEN BS 380 TO BS 400 LBL 15 WL 208 PER SRM 51-40-02 AND DWG 143A5400 REV-.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 56,818 hrs · 30,178 cycles

CRACKED INTERCOSTAL IN CABIN FLOOR STRUCTURE AT BS277+14 RBL2 WL208<[01] REMOVED AND REPLACED INTERCOSTAL IN CABIN FLOOR STRUCTURE AT BS 277+14 RBL 2 WL 208 IAW SRM 51-40-02 AND DWG# 1415400 REV:C;[02] VERIFIED CORRECTION ACTION ITEM 1; ALL STEPS; MEASUREMENT FIELD COMPLETE; CARD COMPLETE.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 56,032 hrs · 29,673 cycles

LH CABIN EMERGENCY EXIT LIGHTS BY EMERGENCY DOOR INOP<[01] RE-LAMPED LH CABIN EMERGENCY EXIT LIGHTS BY EMERGENCY DOOR REF AMM 33-51-01. OPS CHECK GOOD.

Part: LENS — BROKEN (ZONE 200) · airframe 56,032 hrs · 29,673 cycles

LH EMERGENCY EXIT LENS ASSY BY EMERGENCY DOOR BROKEN<[01] R&R LH EMERGENCY EXIT LENS ASSY BY EMERGENCY DOOR REF AMM 33-51-01. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 55,824 hrs · 29,547 cycles

AFT ENTRY DOOR EMERGENCY LIGHT INOP.<[01] RELAMPED AFT ENTRY DOOR EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.

Part: LENS — INCORRECT (EMERGENCY LIGHT) · airframe 55,636 hrs · 29,441 cycles

INCORRECT EXIT SIGN AFT ENTRY DOOR<[01] REPLACED EXIT SIGN LENS AT AFT ENTRY DOOR REF AMM 33-51-01.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,555 hrs · 29,395 cycles

R/H OVERWING EXIT AFT EMERGENCY LIGHT INOP<[01] R&R CABIN OVERWING EXIT SIGN EMERGENCY LIGHT BULB PER AMM 33-51-01;[02] 02 - INSPECTED PER [AMM 33-51-01-960-801-NG (EXIT SIGN - LAMP REPLACEMENT - PERMANENT)]

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,555 hrs · 29,395 cycles

L/H OVERWING EXIT FWD EMERGENCY LIGHT INOP<[01] R&R CABIN OVERWING EXIT SIGN EMERGENCY LIGHT BULB PER AMM 33-51-01;[02] 02 - INSPECTED PER [AMM 33-51-01-960-801-NG (EXIT SIGN - LAMP REPLACEMENT - PERMANENT)]

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 54,811 hrs · 28,956 cycles

CABIN AREA EMERGENCY LIGHT OUT AT 20 ABC<[01] RELAMPED AREA EMERGENCY LIGHT AT 20- ABC IAW AMM 33-51-03. OPS CHECK OK.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 54,491 hrs · 28,776 cycles

L1 SLIDE FELL OUT<[01] REINSTALLED L1 DOOR SLIDE PER M.T 725-61-06.

Part: MOTOR — FAILED (ZN 300 STABILIZE) · airframe 53,872 hrs · 28,398 cycles

STAB TRIM FAIL LT AND STAB OUT OF TRIM LIGHT ILLUMINATED. RETURNED TO BASE (DEN) MESSAGES 22-11181 22-11173 22-11167<[01] REMOVED AND REPLACED STAB TRIM MOTOR PER AMM 27-41-71. STAB TRIM TEST GOOD.

Part: SLIDE — LOOSE (ZN 800 DOOR) · airframe 52,639 hrs · 27,629 cycles

AFT ENTRY EMERGENCY ESCAPE SLIDE LOOSE<[01] SECURED SLIDE REF. MM 25-66-01

Part: CUSHION — OUT OF ADJUST (SEAT BACK) · airframe 52,386 hrs · 27,479 cycles

SEATBACK @ 11D RECLINES. SHOULD NOT. ITS AN EXIT ROW SEAT<[01] REPLACED HYDROLOCK PER S.I.P.

Part: HANDLE — LOOSE (ZN 200 FUS TOP) · airframe 51,809 hrs · 27,132 cycles

INTERIOR HANDLE ON THE AFT ENTRY DOORIS LOOSE<[01] RESESCURED AFT ENTRY DOOR HANDLE PER SIP. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (ZN 800 DOOR) · airframe 51,418 hrs · 26,891 cycles

L1 DOOR EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED L1 SLIDE EMERGENCY LIGHT PER AMM 33-51-04.

Part: SUPPORT ANGLE — CORRODED (BS 663) · airframe 51,253 hrs · 26,798 cycles

CORROSION VAPOR VARRIER AIR CONDITIONING PACK EXHAUST LOWER SUPPORT ANGLE BTW LBL 15 TO LBL 25 AT MAIN WHEEL WELL COMPARTME 2022-691952<[01] TOOLS USED: POWER PACK P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 26-JAN-23; MULTIMETER P/N: FLUKE 87-5; S/N: 17930029; DUE DATE: 13-DEC-23; THERMOMETER P/N: FLUKE 566; S/N: 46660121WS; DUE DATE: 13-APR-23.;[02] REPLACED LOWER SUPPORT ANGLE BTW LBL 15 TO LBL 25 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND B737-700 SRM 51-40-02 AND DWG 149A7216 REV A MATERIAL USED BAC1505-101645? PO 2021 140343 SEE INDIVIDUAL SIGNS OFF BELOW;[03] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,253 hrs · 26,798 cycles

INOP EMERGENCY EXIT LIGHT BATTERY PACK BTW 727C TO 727D LOWER LT SIDE AT PASSENGER CABIN 2022-691935<[01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK BTW 727C TO 727D LOWER LT SIDE AT PASSENGER CABIN IAW BOEING 737-700 AMM 33-51-06-960-805 TEST IS OK;[02] CERTIFIED WORK PERFORMED.

Part: FLOOR PANEL — BROKEN (FWD CABIN) · airframe 51,253 hrs · 26,798 cycles

BROKEN FLOOR PANEL 221BF AT FWD GALLEY AREA (1 EA) 2022-691934<[01] REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM-53-21-00-400-801 3.A THRU 3.F (14);[02] CORRECTED STEP 1. REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM-53-21-00-400-801 3.A THRU 3.F (14) TOOL USED TORQUE P/N: QD1R50A S/N: 0721112702 DUE DATE: SEP-13-2023;[03] REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM-53-21-00-400-801 3.A THRU 3.F (14) TOOL USED TORQUE P/N: QD1R50A S/N: 0721112702 DUE DATE: SEP-13-2023<BR><BR>RII ACCOMPLISHED

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 51,253 hrs · 26,798 cycles

DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING FROM STA 663 TO STA 887 LT SIDE AT PASSENGER CABIN (3 EA) 2022-691923<[01] FAULT RESOLVED ON OTHER FAULT JOB INSTRUCTION 733-080-00-01 TTG8Q003PXMJ;[02] FAULT RESOLVED ON OTHER FAULT JOB INSTRUCTION 733-080-00-01 TTG8Q003PXMJ

Part: ANGLE — ELONGATED (ZN 100 FUS LOWER) · airframe 51,251 hrs · 26,797 cycles

(CUSTOMER REQUEST) ELONGATED HOLE ON CENTER TANK ANGLE LOC BS663 AND BTW LBL 5 TO LBL 65 MAIN WHEEL WELL COMPARTMENT 2022-691910<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[02] STEP 1 CORRECTED. TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23.;[03] REPLACED REPAIR ANGLE LOC. BTW LBL 5 TO LBL 65 AND BS 663 MAIN WHEEL WELL COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 111A1000 SHEET: 224 REV: A SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPLACED REPAIR ANGLE LOC. BTW LBL 5 TO LBL 65 AND BS 663 MAIN WHEEL WELL COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 111A1000 SHEET: 224 REV: A SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII Ï¿½TEM

Part: STIFFENER — DAMAGED (BS 663 BULKHEAD) · airframe 51,253 hrs · 26,798 cycles

(CUSTOMER REQUEST) ELONGATED HOLE 2E/A ON LOWER STIFFENER LOC. BS 663 L/H AND LBL 25 MAIN WHEEL WELL COMPARTMENT 2022-691907<[01] REPLACED LOWER STIFFENER LOC. BS 663 L/H AND LBL 25 MAIN WHEEL WELL COMPARTMENT I.A.W B737-700 SRM 51-10-02 AND DWG 149A7210 SHEET:3 REV:- AND DWG 111A1000 SHEET 140 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: BULKHEAD WEB — DAMAGED (BS 663) · airframe 51,251 hrs · 26,797 cycles

(CUSTOMER REQUEST) ELONGATED HOLE ON WEB LOC. BS 663 LH AND BTW LBL 55 TO LBL 65 AT MAIN WHEEL WELL COMPARTMENT 2022-691905<[01] REPLACED WEB LOC. BS 663 LH AND BTW LBL 55 TO LBL 65 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWG 111A1001 REV:A. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED WEB LOC. BS 663 LH AND BTW LBL 55 TO LBL 65 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWG 111A1001 REV:A. SEE INDIVIDUAL SIGNOFFS BELOW. RII Ï¿½TEM

Part: STIFFENER — ELONGATED (ZN 100 FUS LOWER) · airframe 51,253 hrs · 26,798 cycles

(CUSTOMER REQUEST) ELONGATED HOLE 2 E/A ON STIFFENER LOC. BS663 L/H AT LBL 15 MAIN WHEEL WELL COMPARTMENT 2022-691906<[01] TOOL USED PN: NORTEC 600D; SN:220272712; DUE DATE: 17-DEC-23.;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X11290U021704; DUE DATE: 01 FEB 23;[03] TOOL USED THICKNESS GAGE : P/N 45MG; S/N: 130060401; DUE DATE: 26-JAN-23;[04] PERFORMED REPAIR ON STIFFENER LOC. BS663 L/H AT LBL 15 MAIN WHEEL WELL COMPARTMENT IAW EA# 23-157-00036. SEE INDIVIDUAL SIGNS OFF BELOW;[05] CORRECTIVE ACTION CERTIFIED

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 51,253 hrs · 26,798 cycles

CORROSION FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2022-691872<[01] TOOL USED: ULTRASONIC GAGE: P/N: 45MG; S/N: 221861811; DUE DATE: 08-NOV-23;[02] EVALUATED REWORK AREA LOCATED ON FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 5A(B)(1) FIGURE 102.. NO FURTHER ACTION OR INSPECTION REQUIRED;SEE INDIVIDUAL SIGNOFF BELOW.;[03] CORRECTED STEP 2 <BR>EVALUATED REWORK AREA LOCATED ON FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT AND FOUND OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 5A(1)(B)(1) FIGURE 102.. NO FURTHER ACTION OR INSPECTION REQUIRED;SEE INDIVIDUAL SIGNOFF BELOW.;[04] EDITED STEP 3 (CORRECTED CORRECTIVE ACTION)<BR>REPLACED FLOOR PANEL ACCESS PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 ; P/N USED : 453A2610-32; PO#2021-233448; SEE INDIVIDUAL SIGN OFFS BELOW.;[05] REPLACED FLOOR PANEL ACCESS PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 ; P/N USED : 453A2610-32; PO#2021-233448; SEE INDIVIDUAL SIGN OFFS BELOW.

Part: FLOOR SUPPORT — CORRODED (BS 312-344) · airframe 51,253 hrs · 26,798 cycles

CORROSION FLOOR STRUCTURE LH INNER CHORD LOCATED BTW BS312 TO BS344 AT LEVEL OF STR17L AT FWD GALLEY AREA 2022-691833<[01] THIS CARD WAS RESOLVED IN THE WORK CARD TTG8Q00GNDMX;[02] FAULT RESOLVED ON OTHER FAULT.

Part: SUPPORT CHANNEL — CORRODED (BS 767-794) · airframe 51,253 hrs · 26,798 cycles

CORROSION CHANNEL SUPPORT LOCATED BETWEEN BS 767 TO BS 794 STRINGER 25R AND WL 156 AFT CARGO COMPARTMENT. ] REPLACED CHANNEL SUPPORT LOCATED BETWEEN BS 767 TO BS 794 STRINGER 25R AND WL 156 AFT CARGO COMPARTMENT AND FASTENERS IAW SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 146A0081 REV - SHEET 31.

Part: SUPPORT ANGLE — CORRODED (BS 727B-767 S25R) · airframe 51,253 hrs · 26,798 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727B TO BS 767 STRINGER 25R AND WL 156 AFT CARGO COMPARTMENT 2022-691858<[01] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEEN BS 727 TO BS 767 STRINGER 25R AND WL 156 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG: 146A7500 SHEET: 61 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEEN BS 727 TO BS 767 STRINGER 25R AND WL 156 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG: 146A7500 SHEET: 61 REV:- SEE INDIVIDUAL SIGN OFF BELOW RII

Part: SUPPORT ANGLE — CRACKED (AFT PAX DOOR) · airframe 51,253 hrs · 26,798 cycles

CRACK ACCCESS PANEL 834DZ ENTRY DOOR SUPPORT ANGLE AT AFT GALLEY AREA. REPLACED SUPPORT ANGLE ON ACCESS PANEL 834DZ ENTRY DOOR AT AFT GALLEY AREA IAW SRM 51-40-02 AND 51-10-02.

Part: WEB — CRACKED (BS 294-303) · airframe 51,253 hrs · 26,798 cycles

CRACK WEB PASSENGER CABIN LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL OF STR 16L AT FWD GALLEY AREA 2022-691830<[01] REPLACED WEB PASSENGER CABIN LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL OF STR 16L AT FWD GALLEY AREA IAW B737-700 51-40-02 AND DWG 141A8180 REV C.;[02] CORRECTED STEP 1.<BR>REPLACED WEB PASSENGER CABIN LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL OF STR 16L AT FWD GALLEY AREA IAW B737-700 51-40-02 AND DWG 141A8180 REV C. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTIVE ACTION 2 COMPLETE AND CERTIFIED RII <BR><BR>REPLACED WEB PASSENGER CABIN LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL OF STR 16L AT FWD GALLEY AREA IAW B737-700 51-40-02 AND DWG 141A8180 REV C. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CORRODED (BS 727D S23-25L) · airframe 51,253 hrs · 26,798 cycles

CORROSION ANGLE - SUPPORT LOCATED BS 727D BETWEEN STRINGER 23L TO STRINGER 25L AND WL158 AFT CARGO COMPARTMENT REPLACED ANGLE-SUPPORT LOCATED ON BS727D BETWEEN STRINGER 19L TO STRINGER 25L AND WL158 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 ;SRM 51-40-02 AND DWG 146A1220 SHEET 52 REV- ;DWG 146A9403 SHEET 36 REV- . REPLACED ANGLE-SUPPORT LOCATED ON BS727D BETWEEN STRINGER 19L TO STRINGER 25L AND WL158 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 ;SRM 51-40-02 AND DWG 146A1220 SHEET 52 REV- ;DWG 146A9403 SHEET 36 REV-.

Part: FLOORBEAM — CORRODED (BS 986 LBL42) · airframe 51,253 hrs · 26,798 cycles

CORROSION ON FLOOR BEAM LOCATED BS986 LBL42 AND WL208 AT AFT GALLEY AREA 2022-691865<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 130066701; CAL DUE DATE: 08-APR-23;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101U102020 DUE DATE: 30 AUG 23;[03] REPAIRED ACCOMPLISHED AS PER SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 3 AND EA 22-153-03765 LOC ON FLOOR BEAM LOCATED BS986 LBL42 AND WL208 AT AFT GALLEY AREA SEE INDIVIDUAL SIGN OFF BELOW.;[04] CERTIFIED WORK PERFORMED RII<BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: INTERCOSTAL — CORRODED (BS 847-867) · airframe 51,253 hrs · 26,798 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 847 TO BS 867 S25L & S26L WL 152. REPLACED NEW WEB - INTERCOSTAL LOCATED BETWEEN BS 847 TO BS 867 STRINGER 25L AND STRINGER 26L WL 152 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 SRM 51-40-02 AND DWG 149A8102 SHEET 17 REV-.;[02] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS 847 TO BS 867 STRINGER 25L AND STRINGER 26L WL 152 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 SRM 51-40-02 AND DWG 149A8102 SHEET 17 REV-.;[03] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS 847 TO BS 867 STRINGER 25L AND STRINGER 26L WL 152 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 SRM 51-40-02 AND DWG 149A8102 SHEET 17 REV-. RII

Part: STRUCTURE — CRACKED (BS 303) · airframe 51,253 hrs · 26,798 cycles

CRACK FLOOR STRUCTURE LOCATED ON LH INNER CHORD AT LEVEL OF STR 17L BS 303.9 AT FWD GALLEY AREA 2022-691828<[01] REPLACED INNER CHORD AND ANGLES (2EA) LOCATED AT LEVEL OF STR 17L BTW BS 360 AND BS 259.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 140A9810 REV -;[02] REPLACED INNER CHORD AND ANGLES (2EA) LOCATED AT LEVEL OF STR 17L BTW BS 360 AND BS 259.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 140A9810 REV -VERIFIED AS RII

Part: INTERCOSTAL — CORRODED (BS 847-867) · airframe 51,253 hrs · 26,798 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 847 TO BS 867 STRINGER 25L AND STRINGER 26L WL 151 AFT CARGO COMPARTMENT 2022-691871<[01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS 847 TO BS 867 STRINGER 25L AND STRINGER 26L WL 151 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG 146A7500 SHEET 86 REV A<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTIVE ACTION 1 COMPLETE AND CERTIFIED RII <BR><BR>REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS 847 TO BS 867 STRINGER 25L AND STRINGER 26L WL 151 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG 146A7500 SHEET 86 REV A <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT ANGLE — CORRODED (BS 787 S23-25L) · airframe 51,253 hrs · 26,798 cycles

CORROSION ANGLE SUPPORT LOCATED BS 787 BETWEEN STRINGER 23L TO STRINGER 25L AND WL 158 AT AFT CARGO COMPARTMENT 2022-691869<[01] REPLACED ANGLE SUPPORT LOCATED BS 787 BETWEEN STRINGER 23L TO STRINGER 25L AND WL 158 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 146A1262 REV:-. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED ANGLE SUPPORT LOCATED BS 787 BETWEEN STRINGER 23L TO STRINGER 25L AND WL 158 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 146A1262 REV:-. RII;SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (ZONE 200) · airframe 51,253 hrs · 26,798 cycles

CRACK FLOOR STRUCTURE ANGLE LOCATED AT BS295.5 RBL53.5;WL208.1 AT LEVEL OF STR17R AT FWD GALLEY AREA 2022-691834<[01] THIS CARD WAS RESOLVED IN THE WORK CARD TTG8Q00GNKZ;[02] STEP CORRECTED 1<BR>THIS CARD WAS RESOLVED IN THE WORK CARD TTG8Q00GNKZ3;[03] FAULT RESOLVED ON OTHER FAULT.

Part: SUPPORT ANGLE — CRACKED (ZN 900 LAV/GALLE) · airframe 51,253 hrs · 26,798 cycles

CRACK ACCESS PANEL 844DZ SERVICE DOOR AT AFT GALLEY AND LAV (2 EA) 2022-691845<[01] REPLACED SUPORT ANGLES LOCATED ON PANEL ACCES PANEL 844DZ SERVICE DOOR AT AFT GALLEY AND LAV (2 EA) IAW SRM B737-700 51-40-02 AND 51-10-02; SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPORT ANGLES LOCATED ON PANEL ACCES PANEL 844DZ SERVICE DOOR AT AFT GALLEY AND LAV (2 EA) IAW SRM B737-700 51-40-02 AND 51-10-02; SEE INDIVIDUAL SIGN OFF BELOW<BR>VERIFIED AS RII

Part: CARGO TRACK — CRACKED (BS 727D-767) · airframe 51,253 hrs · 26,798 cycles

CRACK TRACK RBBL 13.84 LOCATED BETWEEN BS 727D TO BS 767 AND STRINGER 26R AFT CARGO COMPARTMENT. REPAIRED TRACK RBBL 13.84 LOCATED BETWEEN BS727C TO BS787 AND STRINGER 26R AT AFT CARGO COMPARTMENT IAW EA 23-153-00247 AND EA 23-153-00247-WIP1.

Part: STUB FRAME — CRACKED (FWD DOOR FRAME) · airframe 51,253 hrs · 26,798 cycles

CRACK SERVICE DOOR FWD ; LOWER STUFF FRAME LOCATED AT BS 294.5 BTW STR 14R TO STR 17R AT FWD GALLEY AREA . PERFORMED REPAIR SERVICE DOOR FWD ; LOWER STUFF FRAME LOCATED AT BS 294.5 BTW STR 14R TO STR 17R AT FWD GALLEY AREA IAW B737 SRM 53-10-15-2R-7 REPAIR 7.

Part: BRACKET — CRACKED (BS 947 S26L) · airframe 51,253 hrs · 26,798 cycles

CRACK BRACKET LOCATED AT BS 947 AND STRINGER 26L AT AFT CARGO COMPARTMENT. REPLACED BRACKET LOCATED AT BS 947 AND STRINGER 26L AT AFT CARGO COMPARTMENT IAW SRM: 51-10-02; AND DWG: 149A8103 REV. A.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 51,253 hrs · 26,798 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 AT LBL 45 PASSENGER CABIN AT FWD GALLEY AREA 2022-691829<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 AT LBL 45 PASSENGER CABIN AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 AT LBL 45 PASSENGER CABIN AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -. <BR>SEE INDIVIDUAL SIGNS-OFF BELOW.<BR>RII

Part: SUPPORT ANGLE — CORRODED (BS 727A-827 S25L) · airframe 51,253 hrs · 26,798 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727A AND BS 827 STRINGER 25L AND WL 156 AFT CARGO COMPARTMENT 2022-691856<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 847 STRINGER 25L AND WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 ;SRM 53-00-53-2R-6 REPAIR 6 AND DWG 146A7500 SHEET 85 REV A ;SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 847 STRINGER 25L AND WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 ;SRM 53-00-53-2R-6 REPAIR 6 AND DWG 146A7500 SHEET 85 REV A ;SEE INDIVIDUAL SIGN-OFF BELOW.

Part: FLOOR PANEL — DAMAGED (FWD GALLEY) · airframe 51,253 hrs · 26,798 cycles

PERFORATION ON FLOOR PANEL 221AF AT FWD GALLEY AREA 2022-691840<[01] TOOL USED CALIPER: 500-196-30 S/N: A21033526 DUE DATE: 15-NOV-23.;[02] HOT BONDER PN: HCS9200B-AV; SN: 18185781 DUE DATE: 16/JAN/23.;[03] TOOL USED= SCALE P/N: 91847; S/N: AE-409316; DUE DATE: 06-JUN-23.;[04] TOOL USED: HOT BONDER P/N HCS9200B-AV S/N 18185781 DUE DATE 16-JAN-23;[05] TOOL USED: SCALE P/N:SPX621 S/N:8340225441 DUE DATE:20-JUL-23.;[06] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18196021; DUE DATE: 16-JAN-23;[07] REPAIRED FLOOR PANEL 221AF AT FWD GALLEY AREA IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW;[08] REPAIRED FLOOR PANEL 221AF AT FWD GALLEY AREA IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW <BR>RII ITEM

Part: SUPPORT CHANNEL — CORRODED (BS 847-867) · airframe 51,253 hrs · 26,798 cycles

CORROSION CHANNEL SUPPORT LOCATED BETWEEN BS 847 TO BS 867 STR 25R AND WL 156 AFT CARGO COMPARTMENT 2022-691862<[01] REPLACED CHANNEL SUPPORT LOCATED BETWEEN BS 847 TO BS 867 STR 25R AND WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 146A0081 SHEET 31 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: CONTACTOR — DEBONDED (BS 847-867) · airframe 51,253 hrs · 26,798 cycles

DEBONDED INTERNAL STRUCTURE CONTACTOR LOCATED BETWEEN BS 847 AND BS 867 AND BETWEEN STRINGER 24L AND STRINGER 25L AT AFT CARGO COMPARTMENT 2022-691825<[01] BONDED INTERNAL STRUCTURE CONTACTOR LOCATED BETWEEN BS 847 AND BS 867 AND BETWEEN STRINGER 24L AND STRINGER 25L AT AFT CARGO COMPARTMENT IAWB737-00 AMM 30-71-04?400-801 STEP 3.F (3).;[02] BONDED INTERNAL STRUCTURE CONTACTOR LOCATED BETWEEN BS 847 AND BS 867 AND BETWEEN STRINGER 24L AND STRINGER 25L AT AFT CARGO COMPARTMENT IAWB737-00 AMM 30-71-04?400-801 STEP 3.F (3).

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,253 hrs · 26,798 cycles

INOP EMERGENCY EXIT LIGHT BATTERY PACK RT SIDE AT PASSENGER CABIN (1 EA) 2022-691817<[01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK RT SIDE AT PASSENGER CABIN (1 EA) IAW BOEING 737-700 AMM 33-51-06-960-805 TEST IS OK;[02] CORRECTED STEP 1 <BR>REPLACED EMERGENCY EXIT LIGHT BATTERY PACK POSITION D RT SIDE AT PASSENGER CABIN (1 EA) IAW BOEING 737-700 AMM 33-51-06-960-805 TEST IS OK;[03] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK POSITION D RT SIDE AT PASSENGER CABIN (1 EA) IAW BOEING 737-700 AMM 33-51-06-960-805 TEST IS OK

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,253 hrs · 26,798 cycles

INOP EMERGENCY EXIT LIGHT BATTERY PACK LT SIDE AT PASSENGER CABIN (1 EA) 2022-691818<[01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK LT SIDE AT PASSENGER CABIN (1 EA) IAW BOEING 737-700 AMM 33-51-06-960-805 TEST IS OK;[02] CORRECTED STEP 1<BR>REPLACED EMERGENCY EXIT LIGHT BATTERY PACK POSITION B LT SIDE AT PASSENGER CABIN (1 EA) IAW BOEING 737-700 AMM 33-51-06-960-805 TEST IS OK;[03] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK POSITION B LT SIDE AT PASSENGER CABIN (1 EA) IAW BOEING 737-700 AMM 33-51-06-960-805 TEST IS OK

Part: SUPPORT CHANNEL — CORRODED (BS 500A-500D) · airframe 51,253 hrs · 26,798 cycles

CORROSION CHANNEL SUPPORT ZEE BTW BS 500A TO BS 500D AT LEVEL STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT 2022-691699<[01] REPLACED CHANNEL SUPPORT ZEE BTW BS 500A TO BS 500D AT LEVEL STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 PARAGRAPH 9 AND DRAWING 143A7500 SHEET 58 REV-<BR>SEE INDIVIDUAL SIGNS OFF BELOW.;[02] REPLACED CHANNEL SUPPORT ZEE BTW BS 500A TO BS 500D AT LEVEL STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 PARAGRAPH 9 AND DRAWING 143A7500 SHEET 58 REV- <BR>SEE INDIVIDUAL SIGNS OFF BELOW... RII ITEM

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 51,253 hrs · 26,798 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2022-691685<[01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A21303968; DUE DATE 06-MAY-23;[02] REPAIRED THE AFT CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1-REPAIR 1 PARAGRAPH 4.B. AND BAC 5975. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPAIRED THE AFT CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1-REPAIR 1 PARAGRAPH 4.B. AND BAC 5975.

Part: SUPPORT CHANNEL — CORRODED (BS 500-500D) · airframe 51,253 hrs · 26,798 cycles

CORROSION CHANNEL SUPPORT ZEE BTW BS 500 TO BS 500D AT LEVEL STR 26L AND WL 154.5 AT FWD CARGO COMPARTMENT 2022-691703<[01] REPLACED SUPPORT ZEE BTW BS 500 TO BS 500D AT LEVEL STR 26L AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7500 SHEET 58; REV <BR>SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED SUPPORT ZEE BTW BS 400 TO BS 500D AT LEVEL STR 26L AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7500 SHEET 58; REV SEE INDIVIDUAL SIGNOFF BELOW.;[03] CORRECTED STEP 1;2 <BR>REPLACED SUPPORT ZEE BTW BS 400 TO BS 500D AT LEVEL STR 26L AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 143A7500 SHEET 58; REV <BR>SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPLACED SUPPORT ZEE BTW BS 400 TO BS 500D AT LEVEL STR 26L AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 143A7500 SHEET 58; REV <BR>RII <BR>SEE INDIVIDUAL SIGNOFF BELOW.

Part: ANGLE — CRACKED (BS 400 S26L) · airframe 51,253 hrs · 26,798 cycles

CRACK ANGLE - CLIP ON BS 400 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2022-691708<[01] REPLACED ANGLE - CLIP LOCATED ON BS 400 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 PARAGRAPH 9 AND DWG 143A7505 SHEET 81 REV- .SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] REPLACED ANGLE - CLIP LOCATED ON BS 400 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 PARAGRAPH 9 AND DWG 143A7505 SHEET 81 REV- .SEE INDIVIDUAL SIGN-OFFS BELOW.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 51,253 hrs · 26,798 cycles

CORROSION BILGE AREA SHEAR PLATE BTW BS 500 TO BS 500A AT LEVEL STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT 2022-691698<[01] REPLACED SHEAR PLATE AND FASTENERS LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A0080 SHEET 11 REV -<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED SHEAR PLATE (SHIELD) AND FASTENERS LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A0080 SHEET 11 REV - <BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED SHEAR PLATE (SHIELD) AND FASTENERS LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A0080 SHEET 11 REV - <BR>SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 51,253 hrs · 26,798 cycles

CORROSION BILGE AREA SHEAR PLATE BTW BS 420 TO BS 440 AT STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT 2022-691696<[01] REPLACED SHEAR PLATE AND FASTENERS LOCATED BTW BS 420 TO BS 440 AT STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG <BR>143A0080 REV - <BR>SEE INDIVIDUAL SIGN-OFFS BELOW;[02] CORRECTED STEP 1<BR><BR>REPLACED SHEAR PLATE (SHIELD) AND FASTENERS LOCATED BTW BS 420 TO BS 440 AT STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG <BR>143A0080 REV - <BR>SEE INDIVIDUAL SIGN-OFFS BELOW;[03] CORRECTED STEP 1. 2<BR><BR>REPLACED SHEAR PLATE (SHIELD) AND FASTENERS LOCATED BTW BS 420 TO BS 440 AT STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A0080 REV - <BR>SEE INDIVIDUAL SIGN-OFFS BELOW;[04] REPLACED SHEAR PLATE (SHIELD) AND FASTENERS LOCATED BTW BS 420 TO BS 440 AT STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A0080 REV - <BR>SEE INDIVIDUAL SIGN-OFFS BELOW<BR>RII

Part: STRINGER — CRACKED (BS 540 S23L) · airframe 51,253 hrs · 26,798 cycles

CRACK STRINGER 23L ON BS 540 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 23L;BTW BS 500D TO BS 540 I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG 206. REPAIR 1 PARAGRAPH 4; TABLE 201; 202;AND SRM 51-40-02-0G-0.

Part: WEB — CRACKED (NR 2 FAN COWL) · airframe 51,253 hrs · 26,798 cycles

CRACK WEB OUTBOARD FAN COWL INTERNAL AREA ON ENGINE 2 2022-691652<[01] REPLACED NEW WEB OUTBOARD FAN COWL INTERNAL AREA ON ENGINE 2 IAW B737-700 SRM 51-40-02 AND CMM 314-2200;[02] REPLACED NEW WEB OUTBOARD FAN COWL INTERNAL AREA ON ENGINE 2 IAW B737-700 SRM 51-40-02 AND CMM 314-2200 SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED NEW WEB OUTBOARD FAN COWL INTERNAL AREA ON ENGINE 2 IAW B737-700 SRM 51-40-02 AND CMM 314-2200 SEE INDIVIDUAL SIGN-OFF BELOW

Part: RIB — CRACKED (VERTICAL STAB) · airframe 51,253 hrs · 26,798 cycles

CRACK ON RIB 8 LOC DORSAL FIN 321A AT VERTICAL STABILIZER 2022-691651<[01] REPLACED RIB 8 LOC DORSAL FIN 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 DWG #174A1008 SHEET 2 REV. C SEE INDIVIDUAL SING OF BELOW TOOL USED CALIPER P/N: 700-113-10 S/N: 0033152 DUE DATE: 08-OCT-23;[02] REPLACED RIB 8 LOC DORSAL FIN 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 DWG #174A1008 SHEET 2 REV. C SEE INDIVIDUAL SING OF BELOW TOOL USED CALIPER P/N: 700-113-10 S/N: 0033152 DUE DATE: 08-OCT-23

Part: SUPPORT ANGLE — CRACKED (NR 1 FAN COWL) · airframe 51,253 hrs · 26,798 cycles

CRACK INBOARD FAN COWL SUPPORT ANGLE AFT LOWER POSITION ON ENGINE 1 2022-691670<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 22-FEB-23.;[02] PERFORMED REPAIR LOCATED INBOARD FAN COWL SUPPORT ANGLE AFT LOWER POSITION ON ENGINE 1 IAW EA EA 23-171-00074 AND B737-700 SRM 737-700 SRM 54-20-02-1A-1.. SEE INDIVIDUAL SIGNOFFS BELOW;[03] CORRECTED STEP 2 <BR>PERFORMED REPAIR LOCATED INBOARD FAN COWL SUPPORT ANGLE AFT LOWER POSITION ON ENGINE 1 IAW EA 23-171-00074 AND B737-700 SRM 54-20-02-1A-1.. SEE INDIVIDUAL SIGNOFFS BELOW;[04] PERFORMED REPAIR LOCATED INBOARD FAN COWL SUPPORT ANGLE AFT LOWER POSITION ON ENGINE 1 IAW EA 23-171-00074 AND B737-700 SRM 54-20-02-1A-1.. SEE INDIVIDUAL SIGNOFFS BELOW

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 51,253 hrs · 26,798 cycles

CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 1.0 INCH. APPROX. 2022-691682<[01] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE: 22-APR-23 WAS USED.;[02] REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 1.0 INCH. APPROX IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 MATERIAL USED ALUMINUM SHEET 2024T3-080 P.O: 2021 138258 SEE INDIVIDUAL SIGNS OFF BELOW;[03] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: ACCESS PANEL — CRACKED (BODY FAIRING) · airframe 51,253 hrs · 26,798 cycles

CRACK ACCESS PANEL 195BL BODY FAIRING AT HOLE FUSELAGE EXTERIOR 2022-691599<[01] TOOL USED: SCALE PN: 91847 SN: AE-409318 DUE DATE: 06/JUN/23.;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 24/SEP/23;[03] TOOL USED HOT BONDER P/N:HCS9200B S/N:15102320 DUE DATE 16 JAN 23;[04] TOOL USED: MULTIMETER P/N: FLUKE 1587 FC. S/N: 57580015 DUE DATE: 15-DEC-23.;[05] REPAIRED ACCESS PANEL 195BL BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-05-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] TASK COMPLETED.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 51,253 hrs · 26,798 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER 2022-691535<[01] TOOL USED PN NORTEC 600D; SN 200048001; DUE DATE 30-MAR-23;[02] PERFORMED REPAIR CATEGORY A ON INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4 . SEE INDIVIDUAL SIGNOFFS BELOW;[03] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 51,253 hrs · 26,798 cycles

CRACK ACCESS PANEL 561BB TRAILING EDGE AROUND HOLES LT WING 2022-691624<[01] TOOL USED CALIPER P/N 500-196-30 S/N A21033526 DUE DATE 15 NOV 23;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 24/SEP/23.;[03] TOOL USED: SCALE P/N: SPX621 S/N: 8340225441 DUE DATE:20-JUL-23.;[04] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18185733 DUE DATE 16/JAN/23.;[05] TOOL USED SCALE P/N 91847 S/N AE-409316 DUE DATE 06/JUN/23;[06] TOOL USED HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE 16/JAN/23.;[07] TOOL USED: MULTIMETER PN: FLUKE 1587 ; SN: 99180027 ; DUE DATE:15-DEC-23;[08] REPAIRED ACCESS PANEL 561BB TRAILING EDGE LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 51,253 hrs · 26,798 cycles

CRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2022-691592<[01] REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV- .

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 51,253 hrs · 26,798 cycles

CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2022-691590<[01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 DWG 143A7902 SHEET 209 REV-.

Part: ACCESS PANEL — CRACKED (HORIZONTAL STAB) · airframe 51,253 hrs · 26,798 cycles

CRACK SEAL - PLATE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2022-691555<[01] REPLACED SEAL - PLATE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.;[02] REPLACED SEAL - PLATE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.

Part: ACCESS PANEL — CRACKED (BODY FAIRING) · airframe 51,253 hrs · 26,798 cycles

CRACK ACCESS PANEL 195CL BODY FAIRING AT FUSELAGE EXTERIOR 2022-691589. REPAIRED ACCESS PANEL 195CL BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 51,253 hrs · 26,798 cycles

CRACK LEADING EDGE RIB IN LE STA 95.96 AT RT HORIZONTAL STABILIZER 2022-691465<[01] RENPLACED LEADING EDGE RIB IN LE STA 95.96 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 Ï¿½TEM 9 AND DWG 186A1001 SHEET 1 REV. B. SEE<BR>INDIVIDUAL SIGNOFFS BELOW.;[02] CORRECTED STEP 1<BR>REPLACED LEADING EDGE RIB IN LE STA 95.96 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 186A1001 SHEET 1 REV. B. SEE<BR>INDIVIDUAL SIGNOFFS BELOW.;[03] CORRECTED STEP 1 <BR>REPLACED LEADING EDGE RIB IN LE STA 95.96 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 186A1001 SHEET 1 REV. B. RII;SEE <BR>INDIVIDUAL SIGNOFFS BELOW.

Part: CREASE BEAM — CORRODED (BS 639 RBL 59) · airframe 51,253 hrs · 26,798 cycles

CORROSION CREASE BEAM ANGLE LOCATED AT BS 639 RBL59 S-17R WL208.1. EVALUATED REWORKED AREA & FOUND WITHIN LIMITS IAW SRM 53-40-13-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 4A(2)(A) FIGURE 103 DETAIL F LOCATED AT BS 639 RBL59 S-17R WL208.1. MEASURES AFTER REWORK ARE L= 1.270 INCHES W=1.083 INCHES. PERFORMED VISUAL INSPECTION ON AREA & NO FOUND EVIDENCE MORE DAMAGE; ULTRASONIC THICKNESS MEASURE PERFORMED ON REWORKED AREA IAW NDT PART 4; 51-00-00 PROCEDURE 3. THE MINIMUM REMAINING THICKNESS IS 0.046 IN. & THE INITIAL THICKNESS IS 0.051 IN. EVALUATED REWORKED AREA & FOUND WITHIN LIMITS IAW SRM 53-40-13-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 4A(2)(A) FIGURE 103 DETAIL F. LOCATED AT BS 639 RBL59 S-17R WL208.1, MEASURES AFTER REWORK ARE L= 1.270 INCHES W=1.083 INCHES. PERFORMED VISUAL INSPECTION ON AREA & NO FOUND EVIDENCE MORE DAMAGE; ULTRASONIC THICKNESS MEASURE PERFORMED ON REWORKED AREA IAW NDT PART 4; 51-00-00 PROCEDURE 3. THE MINIMUM REMAINING THICKNESS IS 0.046 IN. AND THE INITIAL THICKNESS IS 0.051 IN.

Part: FLOORBEAM — CRACKED (BS 695 BL0) · airframe 51,253 hrs · 26,798 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED AT BS 695 BL0 WL 208.1 CENTER SECTION 2022-691466<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED AT BS 695 BL0 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DWG 273A9110 SHEET 6 REV A ;SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] TASK CARD COMPLETED <BR>REPLACED ANGLE FLOOR STRUCTURE LOCATED AT BS 695 BL0 WL 208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DWG 273A9110 SHEET 6 REV A ;SEE INDIVIDUAL SIGN-OFFS BELOW.<BR>RII

Part: FLOORBEAM — CRACKED (BS 540 BL0-LBL25) · airframe 51,253 hrs · 26,798 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.75 WL 208.1 CENTER SECTION 2022-691469<[01] REPLACED STIFFENER LOC FLOOR STRUCTURE AT BS 540 BETWEEN BL0 AND LBL 24.75 WL 208.1 CENTER SECTION PASSENGER CABIN IAW B737-700 SRM 51-10-02; ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNS-OFF BELOW.

Part: ACCESS PANEL — CRACKED (HORIZONTAL STAB) · airframe 51,253 hrs · 26,798 cycles

CRACK SEAL - PLATE ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2022-691472<[01] REPLACED SEAL - PLATE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02;[02] REPLACED SEAL - PLATE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02

Part: CREASE BEAM — CORRODED (BS 616) · airframe 51,253 hrs · 26,798 cycles

CORROSION CREASE BEAM LOCATED AT BS 616 PLUS 5 INCH RBL59 S-17R WL 208.1. REPAIRED CREASE BEAM LOC BTW BSTA616 TO BSTA639 RBL59 AND STR17R ON WL208.1 AT CENTER SECTION I.A.W. EA 23-153-00136; EA 23-153-00136-WIP1 AND EA 23-153-00136-WIP2. REPAIRED CREASE BEAM LOC BTW BSTA616 TO BSTA639 RBL59 AND STR17R ON WL208.1 AT CENTER SECTION I.A.W. EA 23-153-00136; EA 23-153-00136-WIP1 AND EA 23-153-00136-WIP2.

Part: FLOORBEAM — CRACKED (BS 540 BL0-RBL25) · airframe 51,253 hrs · 26,798 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 TO RBL24.75 WL 208.1 CENTER SECTION 2022-691471<[01] REPLACED STIFFENER LOC.FLOOR STRUCTURE AT BS 540 BETWEEN BL0 TO RBL24.75 WL 208.1 CENTER SECTION PASSENGER CABIN IAW B737-700 SRM 51-10-02; ITEM 9 AND SRM 51-40-02 .SEE INDIVIDUAL SIGNOFFS BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 51,253 hrs · 26,798 cycles

CRACK LEADING EDGE RIB IN LE STA 95.96 AT LT HORIZONTAL STABILIZER 2022-691463<[01] REPLACED LEADING EDGE RIB IN LE STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 Ï¿½TEM 9 AND DWG 186A1001 REV. B. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED LEADING EDGE RIB IN LE STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 Ï¿½TEM 9 AND DWG 186A1001 REV. B. RII;SEE INDIVIDUAL SIGNOFFS BELOW.

Part: CREASE BEAM — CORRODED (BS 578 RBL59) · airframe 51,253 hrs · 26,798 cycles

CORRODED CREASE BEAM LOCATED AT BS 578 RBL 59 S-17R WL208. EVALUATED REWORKED AREA & FOUND WITHIN LIMITS IAW SRM 53-40-13-1A-1 4A(2)(A) ALLOWABLE DAMAGE 1 MEASURES AFTER REWORK ARE L= 2.330 INCHES W=1.300 INCHES. PERFORMED VISUAL INSPECTION ON AREA & NO FOUND EVIDENCE MORE DAMAGE. ULTRASONIC THICKNESS MEASURE PERFORMED ON REWORKED AREA IAW NDT PART 4; 51-00-00 PROCEDURE 3. THE MINIMUM REMAINING THICKNESS IS 0.147 IN. & THE INITIAL THICKNESS IS 0.160 IN. EVALUATED REWORKED AREA & FOUND WITHIN LIMITS IAW SRM 53-40-13-1A-1 4A(2)(A) ALLOWABLE DAMAGE 1 MEASURES AFTER REWORK ARE L= 2.330 INCHES W=1.300 INCHES. PERFORMED VISUAL INSPECTION ON AREA & NO FOUND EVIDENCE MORE DAMAGE. ULTRASONIC THICKNESS MEASURE PERFORMED ON REWORKED AREA IAW NDT PART 4; 51-00-00 PROCEDURE 3. THE MINIMUM REMAINING THICKNESS IS 0.147 IN. AND THE INITIAL THICKNESS IS 0.160 IN.

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 51,253 hrs · 26,798 cycles

(CUSTOMER REQUEST) CRACK ON VAPOR BARRIER BSTA663 L/H SIDE AT MAIN WHEEL WELL COMPARTMENT 2022-691457<[01] TOOL USED: CALIPER P/N: 500-464; S/N: B17030933; DUE DATE: 17-OCT-23;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N: 18196127 DUE DATE: 16 JAN 23.;[03] TOOL USED SCALE P/N: CL5000 S/N: AE-409559 DUE DATE: 06 JUN 23;[04] TOOL USED SCALE P/N: 91847 S/N: AE-409321 DUE DATE: 06 JUN 23;[05] REPAIRED VAPOR BARRIER BSTA663 L/H SIDE AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] REPAIRED VAPOR BARRIER BSTA663 L/H SIDE AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW. RII

Part: WEB — CORRODED (BS 616-639 S16R) · airframe 51,253 hrs · 26,798 cycles

CORROSION WEB CUT OUT EMERGENCY DOOR LOWER AREA LOCATED BS616 TO BS 639 S-16R AND WL 228.1. REWORKED AREA LOC CUT OUT EMERGENCY DOOR LOWER AREA LOCATED BS616 TO BS 639 AT LEVEL S-16R AND WL 228.1 AT PASSENGER CABIN; EVALUATED & FOUND WITHIN LIMITS IAW SRM 53-40-15-1A-1 ALLOWABLE DAMAGE 1 AND APPLIED PROTECTIVE TREATMENT ON REWORK AREA SRM 51-20-01. REWORKED AREA LOC CUT OUT EMERGENCY DOOR LOWER AREA LOCATED BS616 TO BS 639 AT LEVEL S-16R AND WL 228.1 AT PASSENGER CABIN; EVALUATED AND FOUND WITHIN LIMITS IAW SRM 53-40-15-1A-1 ALLOWABLE DAMAGE 1 AND APPLIED PROTECTIVE TREATMENT ON REWORK AREA SRM 51-20-01.

Part: LINER — DETERIORATED (PAX DOOR) · airframe 51,253 hrs · 26,798 cycles

DETERIORATED LINNING ENTRY DOOR ASSISTANT HANDLE AND NUT (2EA) AT FWD GALLEY AREA 2022-691383<[01] REPLACED LINNING ENTRY DOOR ASSISTANT HANDLE AND NUT (2EA) AT FWD GALLEY AREA IAW AMM 52-11-31-400-802 STEP 3.G (2);[02] CORRECTED STEP 1. REPLACED LINNING ENTRY DOOR ASSISTANT HANDLE AND NUT (2EA) AT FWD GALLEY AREA IAW B737-700 AMM 52-11-31-400-802 STEP 3.G (2);[03] CERTIFIED WORK PERFORMED.

Part: POWER SUPPLY — INOPERATIVE (MID CABIN) · airframe 50,706 hrs · 26,460 cycles

EMER LTS ON 6ABC; 9ABC; 12ABC; 8FED; MID CABIN EMERGENCY EXIT SIGN AND LH OVER WING EMER LT INOP / [01] REPLACED POWER SUPPLIES M1668 AND M2335 PER AMM 33-51-05. OPS CHK GOOD.

Part: POWER SUPPLY — INOPERATIVE (L/H OVERWING EXI) · airframe 50,706 hrs · 26,460 cycles

EMER LTS ON 6ABC; 9ABC; 12ABC; 8FED; MID CABIN EMERGENCY EXIT SIGN AND LH OVER WING EMER LT INOP / [01] REPLACED POWER SUPPLIES M1668 AND M2335 PER AMM 33-51-05. OPS CHK GOOD.

Part: BATTERY PACK — INOPERATIVE (AFT FUSELAGE) · airframe 50,472 hrs · 26,316 cycles

TOTAL OF 4 MID CABIN AND EXTERNAL EMERGENCY LIGHTS INOP. TWO AISLE LIGHTS FROM ROWS 14-17ABC. AND BOTH L/H AND R/H EXTERNAL AFT FUSELAGE LAMPS NEAR WING BODY STATION 727. / [01] TROUBLESHOT SYSTEM DOWN TO MID CABIN BATTERY PACK (M1670) AT BODY STATION 727C. REPLACED PER AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY — FAILED (CABIN) · airframe 50,164 hrs · 26,130 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1669; M167; M1673; M1675 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1669 M167 M1673 M1675 / [01] CHANGED EMERGENCY LIGHT BATTERIES AT LOCATIONS M1673;M1672;M1675 AND M1669 PER AMM 33-5106. OPS CHECK GOOD

Part: COVER — MISSING (R/H CABIN) · airframe 48,650 hrs · 25,270 cycles

RH EMERGENCY EXIT ROW SIGN COVER IS MISSING ; / [01] INSTALLED NEW EXIT ROW SIGN COVER IAW AMM 33-51-01.

Part: NONE — CRACKED (FUSELAGE) · airframe 48,540 hrs · 25,212 cycles

193 D PANEL LEFT HAND T CLIP CRACKED / [01] INSTALLED T- CLIP THAT WAS FABRICATED PER EA 22-153-00243 PER SRM 51-40-02

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,158 hrs · 24,434 cycles

LH EMERGENCY EXIT BULLNOSE LIGHT @ ROW 13 ABC INOP ; / [01] RELAMPED EMERGENCY EXIT AISLE LIGHT REF AMM 33-51-03

Part: SIGN — DETACHED (CABIN) · airframe 45,981 hrs · 23,821 cycles

AFT EXIT SIGN (AFT GALLY) DETATCHED FROM CIELING / RESECURED AFT GALLY EMERGENCY EXIT SIGN IAW AMM 33-51-01

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,752 hrs · 23,691 cycles

RH AFT EMER LT INOP / RELAMPED RH AFT EMER LT PER AMM 33-51-01

Part: DOME NUT — BROKEN (FWD CARGO) · airframe 45,446 hrs · 23,506 cycles

FORWARD CARGO LOWER AFT THRESHOLD CORNER PLATE DOME NUT BROKEN. / REPLACED DOME NUT PER SRM 51-40-02.

Part: ANGLE — CORRODED (BS 500-500A) · airframe 45,446 hrs · 23,506 cycles

FWD CARGO COMPARTMENT RT FLOOR TO SIDEWALL TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500 TO 500A TO STA / REPLACED TRANSITION ANGLE PER SRM 51-40-02.PART NUMBER 146A8125-53.

Part: SKIN — CORRODED (NR 1 INLET) · airframe 45,446 hrs · 23,506 cycles

#1 ENGINE INLET COWL O/B BARREL SKIN HAS A LARGE AREA OF SURFACE CORROSION AT AFT EDGE BETWEEN THE 2 O'CLOCK AND 3 O'CLOCK POSITION / WP:E36645-LYNCH; MARK - 12/03/2020 12:51 COMPLETE: R&R INLET COWL PER AMM 71-11-01 TAG NO: 738795 PN ON: 314-2100-2 SN ON: 314-2100-2 PN OFF: SN OFF: 4284001

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 45,446 hrs · 23,506 cycles

COCK PIT FLOOR HAS DENTS AT STATION 254 LBL 2 AND UNDER OBSERVER SEAT. REPAIRED COCKPIT FLOOR WEB, PER EA 1-A53-33179.

Part: SEAT TRACK — WORN (CABIN) · airframe 45,446 hrs · 23,506 cycles

NR 1 LBL 45.50 SEAT TRACK HAS LIGHT WEAR ON UPPER TRACK CROWN SURFACE STA 520. REMOVED AND REPLACED SEAT TRACK SECTION, PER EA-20-153-02399.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 45,446 hrs · 23,506 cycles

AFT LOWER CORNER SCUFF PLATE IS CRACKED. / REMOVED AND REPLACED LOWER AFT CORNER SCUFF PLATE IAW AMM 53-11-02.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 45,446 hrs · 23,506 cycles

CABIN FLOOR PANEL 241AF HAS FIBER DAMAGE / REMOVED AND REPLACED PER AMM.53-21-00

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 45,446 hrs · 23,506 cycles

CABIN FLOOR PANEL 241BF HAS FIBER DAMAGE / REMOVED AND REPLACED PER AMM. 53-21-00

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 45,446 hrs · 23,506 cycles

AFT CARGO FLOOR PANEL 140AF HAS NUMEROUS AREAS OF DAMAGE. / REMOVED REPLACED FLOOR PANEL PER AMM 25-52-01.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 45,446 hrs · 23,506 cycles

AFT CARGO FLOOR PANEL 140BF HAS NUMEROUS AREAS OF DAMAGE. / REMOVED REPLACED FLOOR PANEL PER AMM 25-52-01.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 45,446 hrs · 23,506 cycles

AFT CARGO FLOOR PANEL 140CF HAS NUMEROUS AREAS OF DAMAGE. / REMOVED REPLACED FLOOR PANEL PER AMM 25-52-01.

Part: BULLNOSE — DAMAGED (AFT CARGO) · airframe 45,446 hrs · 23,506 cycles

THE AFT CARGO ENTRY THRESHOLD BULLNOSE HAS AREAS OF DAMAGE. / INSTALLED NEW BULLNOSE PER A/M/M 53-11-02 AND LEAK CHECK PER M/M 05-51-91. LEAK CHECK GOOD.

Part: SKIN — DELAMINATED (NOT REPORTED) · airframe 45,299 hrs · 23,415 cycles

PANEL 193B INNER SKIN IS CUT AND DELAMINATED (.5'X1.5') MARKED / R&R 193B PANEL PER SRM 51-40-02

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,450 hrs · 22,899 cycles

EMERGENCY EXIT LIGHTS 2 EACH NEAR L2 DOOR INOP / R&R BATTERY PACK IN AFT GALLEY L/H CEILING PER MM 33-51-06. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,160 hrs · 22,129 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOP/ RELAMPED LIGHT PER AMM.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 41,771 hrs · 21,268 cycles

RUDDER COUNTER BALANCE WEIGHT IS CORRODED / REMOVED AND REPLACED RUDDER COUNTER BALANCE WEIGHT PER CMM 55-40-09

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,413 hrs · 21,053 cycles

R/H FORWARD SLIDE EXTERIOR LIGHT OUT. RELAMPED LIGHT PER AMM.

Part: LENS — MISSING (CABIN) · airframe 40,375 hrs · 20,467 cycles

R2 DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW. R&R LENS COVER IAW SIP.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 40,356 hrs · 20,456 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED PER EA# 1-A53-2076 REV11 AFT CARGO BAY FWD CORNER SCUFF PLATE

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

LT VAPOR BARRIER CRACKED AT BS 663 AT INBOARD SIDE ABOVE THE EXHAUST CUTOUT. REPAIRED BARRIER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 40,356 hrs · 20,456 cycles

RT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STA 120.30 ON LOWER END OF 4TH VERTICAL STIFFENER FROM THE FRONT. REPAIRED RIB PER SRM.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 40,356 hrs · 20,456 cycles

VAPOR BARRIER WEB CRACKED AT BS 663, LBL 26. REPAIRED WEB IAW SRM.

Part: STRIP — BROKEN (FWD CARGO COMPT) · airframe 40,356 hrs · 20,456 cycles

FCB DOOR SURROUND PANEL FWD AND AFT CAP STRIP ARE BROKEN FWD AND AFT PUCK HAS INCORRECT FASTENERS INSP86 12FEB19 / INSTALLED NEW FCB DOOR SURROUND PANEL FWD & AFT CAP STRIP'S AND INSTALLED PROPER FASTENERS INTO PUCKS FWD & AFT OF FCB DOOR 56334U 12FEB19 LEAD138 12FEB19 WORK ACCOMPLISHED IAW AMM 25-52-06-400-801 LEAD138 12FEB19

Part: SKIN — DENTED (FWD FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

REF LOG PAGE 0019359. LARGE FUSELAGE EXTERNAL SKIN DENT CENTERED AT STA 196.5 + 6'; 3'ABOVE STRINGER 24L REQUIRES INSPECTION AND EVALUATION / AN EXTERNAL REPAIR WAS INSTALLED IAW ATS ER 19-01456 REV IR AND EA 1-753-34172 REV IR

Part: SKIN — DENTED (FWD FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

REF LOG PAGE 0112219. LARGE FUSELAGE EXTERNAL SKIN DENT CENTERED AT STA 185; 10'ABOVE STRINGER 24L REQUIRES INSPECTION AND EVALUATION / AN EXTERNAL REPAIR WAS INSTALLED IAW ATS ER 19-01456 REV IR AND EA 1-753-34172 REV IR

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

FLOOR PANEL 241ACF LOWER SKIN DELAMINATED. REPAIRED FLOOR PANEL IAW SRM & DWG. (BETWEEN BS. 887 TO BS. 1016)

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 40,356 hrs · 20,456 cycles

***CORROSION*** ALONG EDGES OF ACB FLOOR PANEL 140DF / FABRICATED NEW ACB FLOOR PANEL 140DF FROM .071 2024T3; LOT# 1373736-1 PER AMM 25-52-01-201-801 DUE TO NO ALLOWABLE DAMAGE LIMITS GIVEN IN SRM FOR THIS PART

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 40,356 hrs · 20,456 cycles

***CORROSION*** ALONG EDGES OF ACB FLOOR PANEL 140CF / FABRICATED NEW ACB FLOOR PANEL 140CF FROM .071 2024T3; LOT# 1373736-1 PER AMM 25-52-01-201-801 AND DWG A53A2610 DUE TO NO ALLOWABLE DAMAGE LIMITS GIVEN IN SRM FOR THIS PART

Part: STRAP — CORRODED (AFT PRESS BULKHE) · airframe 40,356 hrs · 20,456 cycles

***CORROSION*** ON TENSION STRAP BS1016 RBL3 WL208.1. MARKED / CORROSION ON TENSION STRAP @ BS 1016 RBL 3 WL 208.1 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTERAL ITEMS THAT DO NOT HAVE LIMITS ARE CALLED REPAIRABLE BY REPLACEMENT. IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED TENSION STRAP PN # 147A5620-3 FROM BS 1006 - 1021 RBL 3 IAW SRM 51-40-02 AND IAW DWG # 147A5600

Part: STRAP — CORRODED (AFT PRESS BULKHE) · airframe 40,356 hrs · 20,456 cycles

***CORROSION*** ON TENSION STRAP BS1016 LBL27 WL208.1. MARKED / CORROSION ON TENSION STRAP @ BS 1016 LBL 27 WL 208.1 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEMS THAT DO NOT HAVE ENTRIES CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED TENSION STRAP PN # 147A5714-3 FROM BS 1006 - 1021 LBL 27 IAW SRM 51-40-02 AND IAW DWG # 147A5600

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

FLOOR SUPPORT CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. R&R SUPPORT IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

R1 DOOR MOP SILL CORRODED BETWEEN BS 294 TO BS 328, RBL 68. R&R MOP SILL IAW SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

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

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 40,356 hrs · 20,456 cycles

RT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STA 120.30, ON THE LOWER END OF THE 3RD VERTICAL STIFFENER FROM THE FRONT. R&R RIB PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED AT BS 827+19, RBL 21. R&R WEB IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

SEAT TRACK CORRODED BETWEEN BS 540 TO BS 727B, LBL 24.5. R&R SEAT TRACK IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 727 TO BS 787, RBL 21. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

AFT CARGO BAY AFT BULKHEAD TO FLOOR PANEL SUPPORT ANGLE CORRODED AT BS 947, BETWEEN RBL 18 TO LBL 9. R&R ANGLE PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

FLOORBEAM AROUND FASTENER HOLE CORRODED AT BS 986, RBL 43. REPAIRED FLOORBEAM IAW ATS ER AND EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 727A TO BS 847, LBL 21. R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

AFT CARGO BAY SIDE WALL SUPPORT CORRODED AT BS 727D, RBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL12. R&R INTERCOSTAL IAW SRM & DWG.

Part: SCUFF PLATE — CORRODED (R1 DOOR) · airframe 40,356 hrs · 20,456 cycles

***CORROSION*** ON FORWARD SERVICE DOOR SCUFF PLATE INBOARD SUPPORT AT B.S.294-328; RBL62; WL209 / REMOVED AND REPLACED FSD SCUFF PLATE I/B SUPPORT BS 294-328 DUE TO NO ALLOWABLE DAMAGE LIMITS FOUND IN THE SRM AND THIS PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND DWG# 141A8310

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 40,356 hrs · 20,456 cycles

RT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STA 120.30, LOWER END OF THE 2ND VERTICAL STIFFENER FROM THE FRONT. R&R RIB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

FLOORBEAM AROUND FASTENER HOLE CORRODED AT BS 986, LBL 43. REPAIRED FLOORBEAM IAW ER AND EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

AFT CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 794, RBL 21. R&R SHIELD IAW SRM & DWG.

Part: STRAP — CORRODED (AFT PRESS BULKHE) · airframe 40,356 hrs · 20,456 cycles

***CORROSION*** ON TENSION STRAP BS1016 LBL17 WL208.1. MARKED / CORROSION ON TENSION STRAP @ BS 1016; LBL 17 WL 208.1 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEMS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED TENSION STRAP PN # 147A5714-5 SOPM BS 1006 - 1021 LBL 17 IAW SRM 51-40-02 AND IAW DWG # 147A5600

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

R2 DOOR MOP SILL CORRODED BETWEEN BS 967 TO BS 987, RBL 49. R&R MOPSILL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

L1 DOOR CENTER SCUFF PLATE INBOARD SUPPORT UPPER SURFACE CORRODED BETWEEN BS 312 TO BS 344, LBL 53. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

AFT CARGO BAY AFT SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 21. R&R SHIELD IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL1. R&R INTERCOSTAL IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

FORWARD CARGO DOORWAY LOWER THRESHOLD SUB WEB CORRODED BETWEEN BS 440 TO BS 480, RBL 24. R&R SUB WEB IAW DWG AND SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

FORWARD CARGO DOOR AFT CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE PER EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

FORWARD CARGO DOOR FORWARD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE PER EA.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 40,356 hrs · 20,456 cycles

RT WING ATTACH ANGLE COMMON TO DEFLECTION CONTROL RIB AND TRANSVERSE WEB CRACKED. R&R CLIP IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

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

Part: RETAINER — CRACKED (LT WING) · airframe 40,356 hrs · 20,456 cycles

LT WING BULB SEAL RETAINER ABOVE #1 PYLON AFT TIP IS CRACKED / REMOVED AND REPLACED LT WING BULB SEAL RETAINER ABOVE #1 PYLON AFT TIP IAW SRM 51-40-02-0G-0 AND IPC 57-50-00-25 52234U 24JAN19

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

FORWARD CARGO BAY INTERCOSTAL CLIP CRACKED AT BS 400, LBL 24. R&R CLIP IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 40,356 hrs · 20,456 cycles

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

Part: BULKHEAD — PEELING (RT MLG WW) · airframe 40,356 hrs · 20,456 cycles

LOWER COMPOSITE BULKHEAD HAD PREVIOUS REPAIR PEELING OFF AT BS 663, RBL 40. REPAIRED BULKHEAD IAW SRM.

Part: BULKHEAD — PEELING (LT MLG WW) · airframe 40,356 hrs · 20,456 cycles

LOWER COMPOSITE BULKHEAD HAD PREVIOUS REPAIR PEELING OFF AT BS 663, LBL 40. REPAIRED BULKHEAD IAW SRM PER SRM.

Part: CABLE — DISCONNECTED (SPOILER SYS) · airframe 40,244 hrs · 20,387 cycles

AIR TURNBACK, GEAR WOULD NOT RETRACT (HANDLE WOULD NOT GO PAST OFF) AFTER TAKEOFF. QRH SAY THIS INDICATES A FAILURE OF AIR/GRD SAFETY SENSOR OR FAILURE OF THE GRD. SPOILER INTERLOCK VALVE TO CLOSE. REINSTALLED GROUND SPOILER INTERLOCK VALVE CABLE IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,641 hrs · 18,837 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 35,780 hrs · 17,738 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED SLIDE PER SIP.

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 35,404 hrs · 17,540 cycles

TOILET SERVICE DOOR HAS CORRODED HINGES. / REMOVED AND REPLACED TOILER SERVICE DOOR ASSY PER AMM 52-49-09.

Part: SIGN — MISSING (CABIN) · airframe 35,318 hrs · 17,483 cycles

R2 DOOR EMERGENCY EXIT LENS COVER MISSING. R&R SIGN ASSEMBLY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 35,060 hrs · 17,324 cycles

RT FLOOR LIGHT LOOSE AT ROW 11. SECURED LIGHT STRIP PER SIP.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 33,896 hrs · 16,669 cycles

RT PHOTO ILLUMINESCENT STRIP LOOSE BETWEEN ROW 8 TO ROW 9. SECURED STRIP IAW AMM.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 33,791 hrs · 16,606 cycles

LEFT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING CORRODED. REPAIRED THE FITTING IAW EA.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 33,791 hrs · 16,606 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 33,680 hrs · 16,530 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF POSITION. REPOSITIONED SLIDE PER AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 33,680 hrs · 16,530 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 44. REPAIRED WEB IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,680 hrs · 16,530 cycles

STRINGER CRACKED BETWEEN BS 312 TO BS 328, STR 28R. R&R STRINGER IAW DWG AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,680 hrs · 16,530 cycles

STRINGER CLIP CRACKED AT BS 312, STR 28R. R&R CLIP IAW SRM.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 33,083 hrs · 16,162 cycles

R2 DOOR EXIT LIGHT COVER CAME OFF. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: LATCH — DIRTY (R1 DOOR GIRT BAR) · airframe 32,521 hrs · 15,842 cycles

R1 DOOR EMERGENCY SLIDE GIRT BAR LATCHES ARE DIRTY. CLEANED THE LATCH IAW AMM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 31,806 hrs · 15,460 cycles

FORWARD EXIT SIGN COVER LOOSE. SECURED COVER IAW SIP.

Part: BATTERY — FAILED (CABIN) · airframe 31,355 hrs · 15,200 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT M1672. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 31,355 hrs · 15,200 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT M1675. R & R BATTERY IAW AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 31,355 hrs · 15,200 cycles

FORWARD CARGO COMPARTMENT, FLOORBOARD SUPPORT CRACKED AT BS 540, BL 0. R & R SUPPORT IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,923 hrs · 14,419 cycles

RIGHT OVERHEAD EMER LIGHT INOPERATIVE AT ROW 6. RELAMPED LIGHT IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 28,774 hrs · 13,764 cycles

R2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: LIGHT — BROKEN (CABIN) · airframe 28,570 hrs · 13,654 cycles

L2 DOOR EMER EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 28,216 hrs · 13,453 cycles

L1 DOOR EMER LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 27,789 hrs · 13,215 cycles

L2 DOOR EMER EVAC SLIDE EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,372 hrs · 12,967 cycles

L1 DOOR EMER EXIT LIGHT AT AFT FACE OF FWD LAVATORY BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,372 hrs · 12,967 cycles

LEFT OVERWING LOWER EMER EXIT LIGHT BULB INOPERATIVE. R & R LIGHT IAW AMM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 27,372 hrs · 12,967 cycles

FLOOR PANEL 241ABF LOWER SKIN CRACKED AT DRAIN TROUGH RECESS. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 27,372 hrs · 12,967 cycles

SHEAR TIE CORRODED BETWEEN BS 1016 TO 1024, LBL 2. R & R SHEAR TIE IAW DWG & SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 27,372 hrs · 12,967 cycles

AFT CARGO BAY SUPPORT THRESHOLD WEB CORRODED. R & R WEB IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,618 hrs · 12,522 cycles

FORWARD EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,614 hrs · 12,520 cycles

FORWARD LOWER FLASH LIGHT INOPERATIVE. REPOSITIONED FLASHLIGHT IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,271 hrs · 11,731 cycles

AFT GALLEY EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW SIP.

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 23,473 hrs · 10,722 cycles

DIVERSION AT CRUISE ALTITUDE FELT VIBRATION, LOOKED AT OVERHEAD PANEL & SAW THE ENG 1 "A" SIDE HYD LIGHT ILLUMINATED. R & R NR 1 HYD PUMP IAW MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 22,946 hrs · 10,409 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,248 hrs · 9,998 cycles

AFT INBD EMERGENCY FLASHLIGHT INOPERATIVE. R&R BATTERY IAW MM.

Part: RETAINER — CRACKED (RT WING) · airframe 21,916 hrs · 9,848 cycles

RT WING TE CURVED SEAL RETAINER ANGLE CRACKED JUST ABOVE NR 2 PYLON TIP. R&R RETAINER IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 21,916 hrs · 9,848 cycles

LT HORIZONTAL STABILIZER RIB 120.30 CRACKED AT NR 3 VERTICAL STIFFENER LOWER END. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 21,916 hrs · 9,848 cycles

LT HORIZONTAL STABILIZER RIB 92.70 CRACKED AT NR 2 VERTICAL STIFFENER LOWER END. REPAIRED RIB IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 21,916 hrs · 9,848 cycles

FWD CARGO FLOOR PANEL 120CF CORRODED. R&R PANEL IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 21,916 hrs · 9,848 cycles

LT WING UPPER TE PANEL SUPPORT ANGLE CRACKED AT ORSS 273. R&R ANGLE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 21,916 hrs · 9,848 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R SUPPORT IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,916 hrs · 9,848 cycles

LOWER BULKHEAD CRACKED AT BS 663, RBL 31. REPAIRED BULKHEAD IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,916 hrs · 9,848 cycles

LOWER BULKHEAD CRACKED AT BS 663, LBL 32. REPAIRED BULKHEAD IAW SRM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 21,916 hrs · 9,848 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER FWD GIRT BAR RETAINER CLIP LOOSE. R&R RETAINER CLIP IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 21,916 hrs · 9,848 cycles

AFT CARGO FLOOR PANEL 140AF CORRODED ALONG EDGES AT SEVERAL AREAS. R&R PANEL IAW SRM & DRAWING.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 21,916 hrs · 9,848 cycles

AFT CARGO FLOOR PANEL 140DF CORRODED ALONG EDGES AT SEVERAL AREAS. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 21,916 hrs · 9,848 cycles

AFT CARGO FLOOR PANEL 140CF CORRODED ALONG EDGES AT SEVERAL AREAS. R&R PANEL IAW SRM & DRAWING.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 21,916 hrs · 9,848 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767. R&R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 21,916 hrs · 9,848 cycles

FLOOR SUPPORT CRACKED AT BS 540, LBL 2. R&R SUPPORT IAW SRM & DRAWING.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 21,916 hrs · 9,848 cycles

AFT CARGO FLOOR PANEL 140BF CORRODED ALONG EDGES AT SEVERAL AREAS. R&R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 21,916 hrs · 9,848 cycles

FWD CARGO FLOOR PANEL 120AF CORRODED ALONG EDGES IN SEVERAL AREAS. R&R PANEL IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 21,916 hrs · 9,848 cycles

LT WING TE CURVED SEAL RETAINER ANGLE CRACKED ABOVE NR 1 PYLON TIP. R&R ANGLE IAW SRM.