N7733B

Part: SUPPORT — CRACKED (ZONE 600) · airframe 60,714 hrs · 31,519 cycles

WHILE PERFORMING WALK-AROUND, FOUND TWO CRACKS REVEALING HONEY COMB STRUCTURE ON FLAP SUPPORT NR 7, FORWARD ASSY ACCESS PANEL 643AB. PERFORMED INSPECTION IAW EA PROVIDED IN TTG8Q019994P. IAW EA 25-157-03350.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 60,650 hrs · 31,478 cycles

LEFT AFT MOST EMERGENCY LIGHT, AFT OF L2 DOOR, INOPERATIVE. RELAMPED IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (ZONE 600 FLAP) · airframe 60,650 hrs · 31,478 cycles

FOUND RT WING TRAILING EDGE OTBD MAIN FLAP LOWER TRAILING EDGE COVE SKIN CREASED OVER FASTENER. IAW SRM 57-53-01-0I-3, TABLE 2, ITEM 5 FOR CLARIFICATION. RT WING TRAILING EDGE OTBD MAIN FLAP LOWER TRAILING EDGE COVE SKIN DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01-1A-3. FAULT RESOLVED ON ANOTHER FAULT REF EA 25-157-03256 AND TTG8Q0192NGU. ENGINEERING PROVIDED EA 25-157-03256 FOR RT OTBD MAIN FLAP LOWER TRAILING EDGE COVE SKIN CREASED OVER FASTENER.

Part: HOOK — LOOSE (GIRT BAR) · airframe 59,932 hrs · 31,035 cycles

LEFT GIRT BAR HOOK ON SLIDE BUSSLE ON FORWARD RIGHT DOOR IS LOOSE. REPAIRED FWD RT DOOR FWD GIRT BAR CLIP IAW M-23-125-01839.

Part: SIGN — LOOSE (ZONE 200) · airframe 59,688 hrs · 30,896 cycles

EMERGENCY EXIT SIGN IN AFT GALLEY NEEDS SECURED. PERFORMED EA M-24-133-00396, SECURED EMERGENCY EXIT SIGN IAW TSR 2025006998, OK TO CONTINUE.

Part: ATTACH FITTING — CRACKED (ZONE 100) · airframe 59,653 hrs · 30,870 cycles

FWD CARGO A/C MIX BAY INTERCOSTAL ATTACH FITTING CRACKED AT FWD FACE OF FLOOR BEAM AT STATION 520 CENTER. SEE PIC.<[01] LOCATED AND DRILLED NEW ?L? ANGLE AT STA 520 FLOOR BEAM USING PN: 143A5410U9 PRE FORMED MATERIAL PER SRM 51-40-05;[02] INSTALLED NEW ?L? ANGLE PER SRM 51-40-02;[03] ADDED FAILURE TYPE; CORRECTED FAILURE TYPE FROM NO TO YES.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 58,422 hrs · 30,169 cycles

CAPTAINS EMER EXIT SIDEWALL LIGHT INOP<[01] PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECK GOOS. PLACARDS REMOVED.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 58,116 hrs · 29,998 cycles

LEFT O/W EXIT SIGN LIGHT INOP<[01] OK TO CONTINUE PER. MEL 33-2-03. SP1B AUTHORIZATION #235312. ALL EMERGENCY LIGHTS AND SIGN ILLIUNNATE ON LH OVERWING DOOR. FOUND SIDEWALL LIGHT UNDERNEATH EXIT SIGN TO BE INOP.; [02] REMOVED AND REPLACED L/H O/W EXIT SIGN LIGHT LAMP IAW AMM 33-51-01.

Part: DRAIN — LEAKING (FUEL PUMP) · airframe 57,197 hrs · 29,459 cycles

FUEL DRIP ON #2 ENG RAN ENGINE; PER MX FOR 5 MIN & ENGINE CONTINUED TO DRIP<[01] RAN ENGINE FOR 5 MINUTES & FOUND THE MAIN FUEL PUMP DRAIN LEAKING 7 DROPS PER MINUTE & FOUND TO BE WITHIN THRESHOLD LIMITS WITH NO MX ACTION NECESSARY PER AMM 71-71-00. A/C OK FOR SERVICE.

Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 57,040 hrs · 29,368 cycles

FORWARD ENTRY DOOR EMERGENCY SLIDE COVER HAS A PART STICKING OUT ON THE BOTTOM OF THE COVER<[01] RESTORED BATTERY TEST LEAD BACK INTO ITS POUCH ON FWD ENTRY DOOR SLIDE REF AMM 25-66-01.

Part: BATTERY — NO TEST (FWD MEGAPHONE) · airframe 56,121 hrs · 28,811 cycles

FWD GALLEY MEGAPHONE WILL NOT TEST. R & R FWD GALLEY MEGAPHONE BATTERIES AS PER AMM 25-64-00. OPS TEST GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,097 hrs · 28,794 cycles

INOP LOWERED CEILING PANEL BATTERY PACK LT SIDE AT AFT GALLEY AREA (1EA) 2024-293979<[01] REPLACED LOWERED CEILING PANEL BATTERY PACK LT SIDE AT AFT GALLEY AREA (1EA) AND PERFORMED OPERATIONAL TEST IAW B737-700 AMM-33-51-06-960-805 SEE INDIVIDUAL SIGN OF BELOW;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: GIRT BAR — DETERIORATED (ZONE 200) · airframe 56,097 hrs · 28,794 cycles

DETERIORATED ENTRY DOOR GIRT BAR FITTING PLATE (2EA) AND SHIM (2EA) AT FWD GALLEY AREA 2024-293600 DETERIORATED ENTRY DOOR GIRT BAR FITTING PLATE (1EA) AND SHIM (2EA) AT FWD GALLEY AREA<[01] REPLACED ENTRY DOOR GIRT BAR FITTING PLATE (1EA) AND SHIM (2EA) AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801.;[02] REPLACED ENTRY DOOR GIRT BAR FITTING PLATE (1EA) AND SHIM (2EA) AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801.

Part: FLOORBEAM — CRACKED (BS 540 BL0-25) · airframe 56,097 hrs · 28,794 cycles

(CUSTOMER REQUEST) PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75 2024-293943<[01] REPLACED NEW SUPPORT BREAK INSTALLED NEW SUPPORT BREAK LOCATED ON PASSENGER CABIN; FLOOR STRUCTURE AT STA 540; BL 0 TO RBL 24.75 IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 46 REV - <BR>SEE INDIVIDUAL SING OFF BELOW.;[02] CORRECTED STEP 1: REPLACED NEW SUPPORT BREAK INSTALLED NEW SUPPORT BREAK LOCATED ON PASSENGER CABIN; FLOOR STRUCTURE AT STA 540; BL 0 TO RBL 24.75 IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 46 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED NEW SUPPORT BREAK INSTALLED NEW SUPPORT BREAK LOCATED ON PASSENGER CABIN; FLOOR STRUCTURE AT STA 540; BL 0 TO RBL 24.75 IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 46 REV -SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (RT WING) · airframe 56,097 hrs · 28,794 cycles

CRACK BRACKET ANGLE LOCATED ACCESS PANEL 651FB AT RT WING 2024-293939<[01] REPLACED BRACKET LOCATED ON ACCESS PANEL 651FB AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9.;[02] CORRECTED STEP 1: <BR>REPLACED BRACKET LOCATED ON ACCESS PANEL 651FB AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N: A21043202 DUE DATE: 13NOV24;[03] REPLACED BRACKET LOCATED ON ACCESS PANEL 651FB AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N: A21043202 DUE DATE: 13NOV24

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 56,097 hrs · 28,794 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS266 AT RT WING 2024-293935<[01] REPLACED ANGLE LOCATED TRAILING EDGE LOCATED ORSS266 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2930 SHEET 8 REV -.;[02] REPLACED ANGLE LOCATED TRAILING EDGE LOCATED ORSS266 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2930 SHEET 8 REV -.

Part: BRACKET — CRACKED (BS 540-559) · airframe 56,097 hrs · 28,794 cycles

CRACK SUPPORT BRACKET LOCATED ON PNEUMATIC DUCT BTW BS540 TO BS559 RH SIDE AT AIR CONDITIONING BAY 2024-293901<[01] REPLACED SUPPORT BRACKET LOCATED ON PNEUMATIC DUCT BTW BS540 TO BS559 RH SIDE AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] REPLACED SUPPORT BRACKET LOCATED ON PNEUMATIC DUCT BTW BS540 TO BS559 RH SIDE AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02

Part: INTERCOSTAL — CORRODED (BS 767-794 S25R) · airframe 56,097 hrs · 28,794 cycles

CORROSION WEB - INTERCOSTAL LOCATED BTW BS767 TO BS794.3 STR25R AND WL156 AFT CARGO COMPARTMENT 2024-293831<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS767 TO BS794.3 STR25R AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG DWG 146A0081; SHEET 31; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED WEB - INTERCOSTAL LOCATED BTW BS767 TO BS794.3 STR25R AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A0081; SHEET 31; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED STEP 2 COMPLETED<BR>RII

Part: ANGLE — CORRODED (BS 767-787 S25R) · airframe 56,097 hrs · 28,794 cycles

CORROSION ANGLE LOCATED BTW BS767 TO BS787 STR25R AND WL156 AFT CARGO COMPARTMENT 2024-293835<[01] REPLACED ANGLE LOCATED BTW BS767 TO BS787 STR25R AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG DWG 146A8123; SHEET 16; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED ANGLE LOCATED BTW BS767 TO BS787 STR25R AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A8123; SHEET 16; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] CERTIFIED STEP 2 COMPLETED<BR>RII

Part: ANGLE — CRACKED (BS 400 S26L) · airframe 56,097 hrs · 28,794 cycles

CRACK ANGLE - CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT 2024-293828<[01] REPLACED ANGLE - CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #143A7505 SHEET 81 REV.- TOOK MEASURE OF CRACK IS: 1.520? TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A23329421 DUE DATE: 22-FEB-25;[02] REPLACED ANGLE - CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #143A7505 SHEET 81 REV.- TOOK MEASURE OF CRACK IS: 1.520? TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A23329421 DUE DATE: 22-FEB-25

Part: SUPPORT — CORRODED (BS 727-807 S25L) · airframe 56,097 hrs · 28,794 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS807 STR25L AND WL156 AFT CARGO COMPARTMENT 2024-293833<[01] TOOL USED IN STEP 4: UT EQUIPMENT; P/N: 45MG; S/N: 130064101 DUE DATE: 13-DEC-25;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS807 STR25L AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:146A7500; SHEET:85; REV:A<BR>SEE INDIVIDUAL SIGNOFF BELOW;[03] CORRECTED STEP 2<BR>REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS847 STR25L AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:146A7500; SHEET:85; REV:A<BR>SEE INDIVIDUAL SIGNOFF BELOW;[04] JOB COMPLETED AND CERTIFIED RII

Part: ANGLE — CRACKED (BS 500C S26L) · airframe 56,097 hrs · 28,794 cycles

CRACK ANGLE - CLIP LOCATED BS500C AND STR26L FWD CARGO COMPARTMENT 2024-293829<[01] REPLACED ANGLE - CLIP LOCATED BS500C AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #143A7505 SHEET 81 REV.- TOOK MEASURE OF CRACK IS: 1.210? TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A23329421 DUE DATE: 22-FEB-25;[02] REPLACED ANGLE - CLIP LOCATED BS500C AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #143A7505 SHEET 81 REV.- TOOK MEASURE OF CRACK IS: 1.210? TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A23329421 DUE DATE: 22-FEB-25

Part: SUPPORT — CORRODED (BS 727-767 S25R) · airframe 56,097 hrs · 28,794 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS767 STR25R AND WL156 AFT CARGO COMPARTMENT 2024-293834<[01] TOOL USED IN STEP 4: UT EQUIPMENT; P/N: 45MG; S/N: 130064101 DUE DATE: 13-DEC-25;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 STR25R AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:146A7500; SHEET:85; REV:A;[03] CORRECTED STEP 2<BR>REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 STR25R AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:146A7500; SHEET:85; REV:A<BR>SEE INDIVIDUAL SIGNOFF BELOW;[04] COMPLETED TASK CERTIFIED

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 56,097 hrs · 28,794 cycles

CRACK ON SUPPORT ANGLE LOCATED FWD BELLY FAIRING BS500D AND STR19L AT LT WING 2024-293817<[01] REPLACED SUPPORT ANGLE LOCATED FWD BELLY FAIRING BS500D AND STR19L AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 116A3010 SHEET 1 REV H<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED SUPPORT ANGLE LOCATED FWD BELLY FAIRING BS500D AND STR19L AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 116A3010 SHEET 1 REV H<BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 56,097 hrs · 28,794 cycles

BROKEN LAVATORY A LENS OF EMERGENCY LIGHT AT FWD GALLEY AREA 2024-293798<[01] REPLACED LAVATORY A LENS OF EMERGENCY LIGHT AT FWD GALLEY AREA IAW B737-700 AMM-33-51-01-960-802 TEST IS OK;[02] REPLACED LAVATORY A LENS OF EMERGENCY LIGHT AT FWD GALLEY AREA IAW B737-700 AMM-33-51-01-960-802 TEST IS OK. JOB COMPLETED.

Part: FUEL PANEL — CORRODED (RT WING) · airframe 56,097 hrs · 28,794 cycles

CORROSION LEADING EDGE FUEL QUANTITY INDICATOR CASE AT RT WING 2024-293815<[01] REPLACED REFUEL PANEL (P15) TEST OK IAW B737-700 AMM 28-21-00-400-801<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED REFUEL PANEL (P15) TEST OK IAW B737-700 AMM 28-21-00-401<BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: FLOORBEAM — CORRODED (BS 312- LBL15) · airframe 56,097 hrs · 28,794 cycles

CORROSION FLOORBEAM LOCATED BS 312 AND LBL 15 WL208.1 AT FWD GALLEY AREA. REPAIRED FLOOR BEAM LOCATED ON BS 312 AND WL208.1 AT FWD GALLEY AREA I.A.W. B737-700 SRM 53-10-51-2R-17 REPAIR 17 WITH SHIMMING DEVIATIONS DOCUMENTED IN EA 24-153-01280.

Part: STRINGER CLIP — CRACKED (BS 277 S10R) · airframe 56,097 hrs · 28,794 cycles

CRACK TIE CLIP LOCATED BS 277 AND S-10R AT PASSENGER CABIN. REPLACED TIE CLIP LOCATED BS 277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG 141A1110 SHEET 18 REV-. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED TIE CLIP LOCATED BS 277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG 141A1110 SHEET 18 REV-.

Part: FLOOR SUPPORT — CRACKED (BS 312-328 LBL46) · airframe 56,097 hrs · 28,794 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 312 TO BS 328 AND LBL 46 FWD GALLEY AND LAV 2024-293721<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 312 TO BS 328 AND LBL 46 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400; SHEET 26; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: FLOOR SUPPORT — CRACKED (BS 270-277) · airframe 56,097 hrs · 28,794 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS270 TO BS 277 AND BL 0 FWD GALLEY AND LAV 2024-293722<[01] REPLACED INTERCOSTAL AND FASTENERS ON FLOOR STRUCTURE LOCATED BS270 TO BS 277 AND BL 0 FWD GALLEY AND LAV. I.A.W. B737-700 SRM 51-10-02 Ï¿½TEM 9; B737-700 SRM 51-40-02 AND DRAWING #141A5210; SHEET 18; REV-.;[02] REPLACED INTERCOSTAL AND FASTENERS ON FLOOR STRUCTURE LOCATED BS270 TO BS 277 AND BL 0 FWD GALLEY AND LAV. I.A.W. B737-700 SRM 51-10-02 Ï¿½TEM 9; B737-700 SRM 51-40-02 AND DRAWING #141A5210; SHEET 18; REV-.

Part: FLOORBEAM — CORRODED (BS 987 RBL 43) · airframe 56,097 hrs · 28,794 cycles

CORROSION FLOORBEAM LOCATED BS 986.5; RBL 43; WL 208.1 AT AFT GALLEY AREA. REPAIRED FLOORBEAM LOCATED BS 986.5; RBL 43; WL 208.1 AT AFT GALLEY IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4.

Part: SUPPORT BRACKET — CORRODED (GIRT BAR) · airframe 56,097 hrs · 28,794 cycles

CORROSION SUPPORT BRACKET GIRT BAR LOCATED BS312 AND 344 AND LBL 53 WL208.1 AT FWD GALLEY AREA (2 EA) 2024-293727<[01] REPLACED SUPPORT BRACKET GIRT BAR LOCATED BS312 AND 344 AND LBL 53 WL208.1 AT FWD GALLEY AREA (2 EA) IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] REPLACED SUPPORT BRACKET GIRT BAR LOCATED BS312 AND 344 AND LBL 53 WL208.1 AT FWD GALLEY AREA (2 EA) IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. JOB COMPLETED.

Part: STRAP — CORRODED (BS 1006-1016) · airframe 56,097 hrs · 28,794 cycles

CORROSION FLOOR STRUCTURE STRAP LOCATED BETWEEN BS 1006 AND BS 1016; RBL 6; WL 208.1 AT AFT GALLEY AREA 2024-293752<[01] REPLACED FLOOR STRUCTURE STRAP LOCATED BETWEEN BS 1006 AND BS 1016; RBL 6; WL 208.1 AT AFT GALLEY AREA IAW SRM 51-10-02 ITEM 9 AND DWG #156A5600 SHEET 49 REV. A SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: FLOORBEAM — CRACKED (BS 295 RBL 52) · airframe 56,097 hrs · 28,794 cycles

CRACK FLOOR BEAM LOCATED BS294.5 AND RBL 52 AT FWD GALLEY AREA 2024-293720<[01] TOOL USED: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 200053402; DUE DATE: 24-AUG-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:142811019; DUE DATE: 23-JAN-25.;[03] STEP 9; TOOL USED: RADIOMETER / PHOTOMETER KIT; P/N: XRP-3000; S/N: 1859843; DUE DATE: 24/JUL/24.;[04] REPAIRED FLOOR BEAM LOCATED BS294.5 AND RBL 24 TO RBL 60 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02;SRM 53-10-51-2R-16 REPAIR 16 FIGURE 202 SHEET 3<BR>SEE INDIVIDUAL SIGNOFF BELOW;[05] CORRECTED STEP 4<BR>REPAIRED FLOOR BEAM LOCATED BS294.5 AND RBL 13 TO RBL 60 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02;SRM 53-10-51-2R-16 REPAIR 16 FIGURE 202 SHEET 3<BR>SEE INDIVIDUAL SIGNOFF BELOW;[06] CORRECTED STEP 5<BR>CORRECTED STEP 4<BR>REPAIRED FLOOR BEAM LOCATED BS294.5 AND RBL 13 TO RBL 60 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02;SRM 53-10-51-2R-16 REPAIR 16 FIGURE 202 SHEET 7<BR>SEE INDIVIDUAL SIGNOFF BELOW;[07] CORRECTED STEP 4<BR>REPAIRED FLOOR BEAM LOCATED BS294.5 AND RBL 13 TO RBL 60 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02;SRM 53-10-51-2R-16 REPAIR 16 FIGURE 202 SHEET 7<BR>SEE INDIVIDUAL SIGNOFF BELOW AS RII

Part: FLOORBEAM — CORRODED (BS 987 LBL 43) · airframe 56,097 hrs · 28,794 cycles

CORROSION FLOORBEAM LOCATED BS 986.5; LBL 43; WL 208.1 AT AFT GALLEY AREA. REPAIRED FLOOR STRUCTURE BEAM LOCATED BS 986.5; LBL 43; WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6.

Part: STUB FRAME — CRACKED (BS 295) · airframe 56,097 hrs · 28,794 cycles

CRACK ON STUB FRAME LOCATED BS 294.5 RBL 54 AT FWD GALLEY AREA 2024-293724<[01] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[02] EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 60007161486 AND DUE DATE: 28-JUL-24.;[03] PERFORMED REPAIR STUB FRAME LOCATED BS 294.5 RBL 54 AT FWD GALLEY AREA 53-10-15-2R-7 REPAIR 7. SEE INDIVIDUAL SIGNOFF BELOW;[04] PERFORMED REPAIR STUB FRAME LOCATED BS 294.5 RBL 54 AT FWD GALLEY AREA 53-10-15-2R-7 REPAIR 7. SEE INDIVIDUAL SIGNOFF BELOW<BR>RII CERTIFIED

Part: STIFFENER — CORRODED (BS 312-328 LBL12) · airframe 56,097 hrs · 28,794 cycles

CORROSION ON STIFFENER LOCATED BS312 TO BS 328 AND LBL 12 WL 208.1 AT FWD GALLEY AREA 2024-293719 NAME PART IS: PANEL BREAK IAW B737-700 SRM 53-10-51-0L-2.<[01] REPLACED PANEL BREAK LOCATED BS312 TO BS 328 AND LBL 12 WL 208.1 AT FWD GALLEY AREA IAW B737-700 #DWG: 141A5400 SHEET: 27 REV:- AND SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9.<BR>SEE INDIVIDUAL SIGNS OFF BELOW;[02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW.

Part: WEB — CRACKED (BS 295-304) · airframe 56,097 hrs · 28,794 cycles

CRACK WEB LOCATED BS 294.5 TO BS303.9 AND S-16L AT FWD GALLEY AREA. REPAIRED WEB LOCATED BS 294.5 TO BS303.9 AND S-16L AT FWD GALLEY AREA IAW EA 24-153-01209 REV. 1.

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 56,097 hrs · 28,794 cycles

CORROSION ON UPPER WEB FWD CARGO DOOR CUTOUT AT FWD CARGO COMPARTMENT] REPLACED REPAIR UPPER WEB FWD CARGO DOOR CUTOUT AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING : 143A8112 SHEET: 10 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP: REPLACED REPAIR UPPER WEB FWD CARGO DOOR CUTOUT AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING : 143A8112 SHEET: 10 REV:- PERFORMED TEST ON FLOODLIGHT IAW B737-700 AMM 33-36-00-960-803 PARAGRAPH 6.F.(10) TEST IS OK .SEE INDIVIDUAL SIGN OFF BELOW;[04] REPLACED REPAIR UPPER WEB FWD CARGO DOOR CUTOUT AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING : 143A8112 SHEET: 10 REV:- PERFORMED TEST ON FLOODLIGHT IAW B737-700 AMM 33-36-00-960-803 PARAGRAPH 6.F.(10) TEST IS OK .SEE INDIVIDUAL SIGN OFF BELOW. JOB COMPLETED.

Part: FLOORBEAM — BROKEN (BS 695 BL 0) · airframe 56,097 hrs · 28,794 cycles

BROKEN FLOORBEAM ANGLE LOCATED BS 695; BL0 CENTER WING BOX AT PASSENGER CABIN 2024-293673<[01] REPLACED SUPPORT ANGLE LOCATED BS 695; BL0 CENTER WING BOX AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET: 6; REV: A <BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] CERTIFIED STEP 1 COMPLETED

Part: FITTING — DETERIORATED (GIRT BAR) · airframe 56,097 hrs · 28,794 cycles

DETERIORATED GIRT BAR FITTING HARDWARE ON AFT SERVICE DOOR AT AFT GALLEY AREA (8 EA) 2024-293587<[01] REPLACED GIRT BAR FITTING HARDWARE ON AFT SERVICE DOOR AT AFT GALLEY AREA (8 EA) I.A.W B737-700 AMM 25-66-02-400-801;[02] JOB COMPLETED

Part: FITTING — DETERIORATED (GIRT BAR) · airframe 56,097 hrs · 28,794 cycles

DETERIORATED GIRT BAR FITTING HARDWARE ON AFT ENTRY DOOR AT AFT GALLEY AREA (8 EA) 2024-293584<[01] REPLACED GIRT BAR FITTING HARDWARE ON AFT ENTRY DOOR AT AFT GALLEY AREA (8 EA) I.W.A B737-700 AMM 25-66-02-400-801;[02] CORRECTED ACTION 1 <BR>REPLACED GIRT BAR FITTING HARDWARE ON AFT ENTRY DOOR AT AFT GALLEY AREA (8 EA) I.A.W B737-700 AMM 25-66-02-400-801;[03] REPLACED GIRT BAR FITTING HARDWARE ON AFT ENTRY DOOR AT AFT GALLEY AREA (8 EA) I.A.W B737-700 AMM 25-66-02-400-801

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 56,097 hrs · 28,794 cycles

CRACK VAPOR BARRIER LOCATED BS 663 AND LBL 35 AT WING CENTER SECTION 2024-293579<[01] TOOLS USED CALIPER P/N 500-197-30<BR>SIN B20189521 DUE DATE 26-JAN-25;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18196119; DUE DATE: 23-MAY-24.;[03] TOOL USED: SCALE P/N: CR5200; S/N: 8342514561; DUE DATE: 22-FEB-25.;[04] TOOL USED: SCALE P/N: CR5200; S/N: 8342514551; DUE DATE: 17-FEB-25.;[05] TOOL USED ON STEP 12 ULTRASONIC FLAW DETECTOR P/N: EPOCH 600 S/N 130547106 DUE DATE: 25-AUG-24;[06] REPAIRED VAPOR BARRIER LOCATED BS 663 AND LBL 35 AT WING CENTER SECTION IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. REFER TO INDIVIDUAL SING OFF BELOW.;[07] REPAIRED VAPOR BARRIER LOCATED BS 663 AND LBL 35 AT WING CENTER SECTION IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. REFER TO INDIVIDUAL SING OFF BELOW RII;[08] REPAIRED VAPOR BARRIER LOCATED BS 663 AND LBL 35 AT WING CENTER SECTION IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10 RII COMPLETED

Part: PLATE — DETERIORATED (GIRT BAR) · airframe 56,097 hrs · 28,794 cycles

DETERIORATED GIRT BAR FITTING PLATE AND SHIM ON AFT ENTRY DOOR AT AFT GALLEY AREA (8 EA) 2024-293582 DETERIORATED GIRT BAR FITTING PLATE AND SHIM ON AFT ENTRY DOOR AT AFT GALLEY AREA (4 EA)<[01] REPLACED GIRT BAR FITTING PLATE AND SHIM ON AFT ENTRY DOOR AT AFT GALLEY AREA (8 EA) I.A.W B737-700 AMM 25-66-02-400-801;[02] CORRECTED ACTION 1 REPLACED GIRT BAR FITTING PLATE AND SHIM ON AFT ENTRY DOOR AT AFT GALLEY AREA (4 EA) I.A.W B737-700 AMM 25-66-02-400-801;[03] REPLACED GIRT BAR FITTING PLATE AND SHIM ON AFT ENTRY DOOR AT AFT GALLEY AREA (4 EA) I.A.W B737-700 AMM 25-66-02-400-801

Part: PLATE — DETERIORATED (GIRT BAR) · airframe 56,097 hrs · 28,794 cycles

DETERIORATED GIRT BAR FITTING PLATE AND SHIM ON AFT SERVICE DOOR AT AFT GALLEY AREA (4 EA) 2024-293585<[01] REPLACED GIRT BAR FITTING PLATE AND SHIM ON AFT SERVICE DOOR AT AFT GALLEY AREA (4 EA) I.W.A B737-700 AMM 25-66-02-400-801;[02] CORRECTED ACTION 1<BR>REPLACED GIRT BAR FITTING PLATE AND SHIM ON AFT SERVICE DOOR AT AFT GALLEY AREA (4 EA) I.A.W B737-700 AMM 25-66-02-400-801;[03] REPLACED GIRT BAR FITTING PLATE AND SHIM ON AFT SERVICE DOOR AT AFT GALLEY AREA (4 EA) I.A.W B737-700 AMM 25-66-02-400-801

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 56,097 hrs · 28,794 cycles

CRACK ON LEADING EDGE RIB LOC. LE STA 105.26 AT LT HORIZONTAL STABILIZER 2024-293611<[01] REPLACED RIB LOC. ON LEADING EDGE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 ; SHEET 10 ; REV A. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED RIB LOC. ON LEADING EDGE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 ; SHEET 10 ; REV A. SEE INDIVIDUAL SIGNS-OFF BELOW.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 56,097 hrs · 28,794 cycles

CRACK ON LEADING EDGE RIB LOC. LE STA 105.26 AT LT HORIZONTAL STABILIZER<[01] TOOL USED DIGITAL CALIPER P/N: 500-752-20 S/N: B21037197 DUE DATE: 03/OCT/24;[02] FAULT RESOLVED ON FAULT TTG8Q00SZC8F.;[03] FAULT RESOLVED ON OTHER FAULT TTG8Q00SZC8F.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 56,097 hrs · 28,794 cycles

CRACK ON LEADING EDGE RIB LOC. LE STA 95.96 AT LT HORIZONTAL STABILIZER 2024-293609<[01] TOOL USED DIGITAL CALIPER P/N: 500-752-20 S/N: B21037197 DUE DATE: 03/OCT/24;[02] REPLACED RIB LOC. ON LEADING EDGE STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 ; SHEET 10 ; REV A. SEE INDIVIDUAL SIGNS-OFF BELOW.;[03] REPLACED RIB LOC. ON LEADING EDGE STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 ; SHEET 10 ; REV A. SEE INDIVIDUAL SIGNS-OFF BELOW.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,097 hrs · 28,794 cycles

INOP EMERGENCY LIGHT BATTERY PACK IN STA 603 LT SIDE AT PASSENGER CABIN 2024-293488<[01] REPLACED EMERGENCY LIGHT BATTERY PACK IN STA 603 LT SIDE AT PASSENGER CABIN AND PERFORMED OPERATIONAL TEST I.A.W B737-700 AMM-33-51-06-960-805 SEE INDIVIDUAL SIGN OF BELOW;[02] CORRECTED ACTION 1<BR>REPLACED EMERGENCY LIGHT BATTERY PACK IN STA 603 LT SIDE AT PASSENGER CABIN AND PERFORMED OPERATIONAL TEST I.A.W B737-700 AMM-33-51-06-960-805 ?TEST IS OK? SEE INDIVIDUAL SIGN OF BELOW;[03] REPLACED EMERGENCY LIGHT BATTERY PACK IN STA 603 LT SIDE AT PASSENGER CABIN AND PERFORMED OPERATIONAL TEST I.A.W B737-700 AMM-33-51-06-960-805 ?TEST IS OK? SEE INDIVIDUAL SIGN OF BELOW. JOB COMPLETED.

Part: INTERCOSTAL — CRACKED (BS 847-867) · airframe 56,097 hrs · 28,794 cycles

CRACK WEB - INTERCOSTAL LOCATED BS847 TO BS 867 UPPER POSITION AFT CARGO COMPARTMENT 2024-293519<[01] REPLACED WEB - INTERCOSTAL LOCATED BS847 TO BS 867 UPPER POSITION AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.;[02] TASK COMPLETED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,097 hrs · 28,794 cycles

INOP EMERGENCY LIGHT BATTERY PACK IN STA 727C LT SIDE AT PASSENGER CABIN 2024-293493<[01] REPLACED EMERGENCY LIGHT BATTERY PACK IN STA 727C LT SIDE AT PASSENGER CABIN AND PERFORMED OPERATIONAL TEST IAW B737-700 AMM-33-51-06-960-805.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,097 hrs · 28,794 cycles

INOP EMERGENCY LIGHT BATTERY PACK IN STA 603 RT SIDE AT PASSENGER CABIN. REPLACED EMERGENCY LIGHT BATTERY PACK IN STA 603 RT SIDE AT PASSENGER CABIN AND PERFORMED OPERATIONAL TEST IAW AMM-33-51-06-960-805.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,873 hrs · 28,660 cycles

L/H OVERWING EXIT DOOR EMERGENCY EXIT LIGHT LENS FELL OFF<[01] R&R LENS PER AMM 33-51-01

Part: SLIDE — WRONG PART (FWD SERVICE DOOR) · airframe 55,682 hrs · 28,562 cycles

REFERENCE :725-61-06-FS (REP - EMERGENCY ESCAPE SLIDE FWD SERVICE DOOR) [TTG8Q00E1PPL]; PART REQUIREMENT FOR FWD SVC DOOR SLIDE IS INCORRECT SERIAL #BNG50940 AND SHOULD REFLECT SER#BNG33233<[01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE IAW AMM 25-66-01 AND MT 725-61-06-FS.<BR>SEE MX TTG8Q00E1PPL.

Part: TRANSMITTER — INCORRECT (ZN 100 FUS LOWER) · airframe 55,052 hrs · 28,193 cycles

TRAILING EDGE FLAPS DISAGREE ON APPROACH. TRAILING EDGE FLAPS INDICATE 13 DEGREES WITH FLAP HANDLE AT 30 DEGREES.<[01] R&R'D L/H FLAP POSITION X-MITTER PER AMM 27-58-01. OPS CHK NORMAL

Part: CONTROL PANEL — DAMAGED (FIRE WARNING) · airframe 54,941 hrs · 28,134 cycles

ABORTED T/O @ 90 KTS ABORTED T/O @ 90 KTS DUE TO ALL FIRE INDICATIONS . ALL OTHER NDICATIONS NORMAL<[01] REMOVED AND REPLACED ENG & APU FIRE CONTROL PANEL (FOUND PUSHED PIN) IAW AMM 26-00-01; PERFORMED HIGH ENERGY STOP INSPECTION IAW AMM 05-51-07; NO DEFECTS NOTED AT THIS TIME

Part: COWLING — CRACKED (ZN 400 NACELLE/P) · airframe 54,191 hrs · 27,700 cycles

#1 ENGINE INBD FAN COWL HAS A 3 INCH CRACK 2.5 INCHES FWD OF TRAILING EDGE AND 4 INCHES UP FROM LOWER EDGE<[01] REMOVED AND REPLACED #1 ENGINE INBD FAN COWL. REF:AMM 71-11-02

Part: HANDLE — LOOSE (ZN 200 FUS TOP) · airframe 54,191 hrs · 27,700 cycles

FWD SERVICE DOOR LINER ASSIST HANDLE IS LOOSE<[01] RESECURED FWD SERVICE DOOR LINER ASSIST HANDLE IN REF AMM 20-50-11

Part: HANDLE — LOOSE (ZN 200 FUS TOP) · airframe 54,191 hrs · 27,700 cycles

FWD ENTRY FWD BULKHEAD ASSIST HANDLE IS LOOSE<[01] RESECURED FWD ENTRY FWD BULKHEAD ASSIST HANDLE IN REF AMM 20-50-11

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 54,191 hrs · 27,700 cycles

FWD ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] READJUSTED FWD ENTRY DOOR SLIDE GIRT BAR IN REF AMM 25-66-01

Part: BATTERY PACK — INOPERATIVE (ZN 100 FUS LOWER) · airframe 52,487 hrs · 26,685 cycles

EMERGENCY EXIT ROW SIGN ON THE CA SIDE APPEARS INOP.<[01] REPLACED CAPT'S EMER. EXIT ROW BATTERY PACK PER AMM 33-51-06; CHECK GOOD.

Part: GUARD — LOOSE (EMERGENCY LIGHT) · airframe 51,459 hrs · 26,091 cycles

COCKPIT EMERGENCY EXIT LIGHT GUARD LOOSE / [01] REPLACED COCKPIT EMERGENCY LIGHT SWITCH GUARD PER M/M S.I.P.

Part: LIGHT — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 51,216 hrs · 25,952 cycles

SIDEWALL LIGHT AT EMERGENCY EXIT 12DEF INOP. / [01] RELAMPED SIDEWALL LIGHT AT EMERGENCY EXIT 12DEF IAW AMM 33-21-00.

Part: LIGHT — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 51,216 hrs · 25,952 cycles

SIDEWALL LIGHT AT EMERGENCY EXIT 11BC INOP. / [01] RELAMPED SIDEWALL LIGHT AT EMERGENCY EXIT 11BC IAW AMM 33-21-00.

Part: LIGHT — INOPERATIVE · airframe 50,055 hrs · 25,216 cycles

FORWARD ENTRY PROXIMITY AND RIGHT OVERWING PROXIMITY LIGHTS HAVE 3 INOPERATIVE LAMPS. / [01] REPLACED FORWARD ENTRY PROXIMITY CENTER AND RIGHT OVERWING PROXIMITY TOP AND NEXT TO BOTTOM LAMPS AND PERFORMED TEST OF NEW LAMPS PER AMM 33-51-01-960-801; NO DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION #1

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 50,055 hrs · 25,216 cycles

FORWARD ENTRY PROXIMITY AND RIGHT OVERWING PROXIMITY LIGHTS HAVE 3 INOPERATIVE LAMPS. / [01] REPLACED FORWARD ENTRY PROXIMITY CENTER AND RIGHT OVERWING PROXIMITY TOP AND NEXT TO BOTTOM LAMPS AND PERFORMED TEST OF NEW LAMPS PER AMM 33-51-01-960-801; NO DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION #1

Part: BATTERY PACK — INOPERATIVE · airframe 50,055 hrs · 25,216 cycles

LIGHTS ASSOCIATED WITH M1670 EMERGENCY EXIT LIGHT BATTERY PACK INOP / [01] PARTIAL UPDATE TO STEP 1.;[02] REMOVED AND REPLACED BATTERY PACK M1670 AND PERFORMED INSTALLATION TEST PER AMM 33-51-06 CHECKED GOOD;[03] COMPLETED STEP 1.<BR>VERIFIED CORRECTIVE ACTION 2.<BR>CHECK GOOD;[04] OK TO CLOSE CARPET RISER AT BATTERY PACK M1670;[05] CERTIFY

Part: BATTERY PACK — INOPERATIVE · airframe 50,055 hrs · 25,216 cycles

LIGHTS ASSOCIATED WITH M2335 EMERGENCY EXIT LIGHT BATTERY PACK INOP / [01] PARTIAL UPDATE TO STEP 1.;[02] REMOVED AND REPLACED M2335 BATTERY PACK AND PERFORMED INSTALLATION TEST PER AMM 33-51-06 CHECKED GOOD;[03] COMPLETED STEP 1.<BR>VERIFIED CORRECTIVE ACTION 2.<BR>CHECK GOOD;[04] OK TO CLOSE CARPET RISER LOCATED AT M2335;[05] CERTIFY

Part: BATTERY PACK — INOPERATIVE · airframe 50,055 hrs · 25,216 cycles

LIGHTS ASSOCIATED WITH M1669 EMERGENCY EXIT LIGHT BATTERY PACK INOP / [01] PARTIAL UPDATE TO STEP 1.;[02] REMOVED AND REPLACED M1669 BATTERY PACK AND PERFORMED INSTALLATION TEST PER AMM 33-51-06 CHECKED GOOD;[03] COMPLETED STEP 1.<BR>VERIFIED CORRECTIVE ACTION 2.<BR>CHECK GOOD;[04] OK TO CLOSE CARPET RISER AT BATTEY PACK M1669;[05] CERTIFY

Part: SKIN — CRACKED (LH HOR STAB) · airframe 50,055 hrs · 25,216 cycles

L/H HORIZONTAL STAB LWR STAB SKIN CRACKED AT STAB STA 193.90; MARKED (TTG8Q00CCGGU / [01] CORRECTION TO FAULT TTG8Q00CCGGU FOR CATEGORY B REPAIR

Part: PANEL — DELAMINATED · airframe 50,055 hrs · 25,216 cycles

PANEL 193AR HAS DELAMINATIONS ON THE OUTER SURFACE (2EA) UPON INSPECTION OF PANEL FOUND 1EA ADDITIONAL DELAMINATION ON OUTER SURFACE 5' FROM FWD EDGE; 21.5' FROM I/B EDGE. ORIGINAL DAMAGE NOTED; AND DAMAGE FOUND; IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4A(6).REPAIRS TO BE ACCOMPLISHED IAW SRM 51-70-05-2R-2 PER SRM 53-40-70-2R-1 PAR 4B(1).REMOVED 1' DIAMETER OF DAMAGE TO OUTER SURFACE FACE SHEET AND PARTIAL CORE DEPTH AT 3EA AREAS ON OUTER SURFACE; FABRICATED AND INSTALLED REPAIR PLIES AT 3EA REPAIR AREAS USING FIBERGLASS BMS 8-79; CLASS 3; STYLE 120; LOT# 1488453-1 AND FILM ADHESIVE BMS 5-129; TYPE 2; GRADE 5; LOT# 1491228-1.VACUUM BAGGED REPAIRS; WORK ACCOMPLISHED IAW SRM 51-70-05-2R-2 PAR 4.D + F-I AND SRM 51-70-05-2R-11 PAR 4.B-D.

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

FWD CARGO BAY GUSSET CRACKED BS 500D STR 19 R/H / [01] NOT FOUND ALLOWABLE DAMAGE LIMITS ON FOR FWD CARGO BAY GUSSET CRACKED BS 500D STR 19 R/H ; MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED FWD CARGO BAY GUSSET CRACKED BS 500D STR 19 R/H IAW SRM 51-40-02;[03] RECEIVED; LOCATED AND DRILLED NEW FWD CARGO BAY GUSSET AT BS 500D STR 19 R/H. P/N 143A9481-5 LOT #1481232-7 IAW SRM 51-40-05 AND DWG 143A7902 REV:;[04] OK TO INSTALL;[05] VERIFIED ITEM 3 CORRECTIVE ACTIONS. OK TO INSTALL.;[06] INSTALLED NEW FWD CARGO BAY GUSSET AT BS 500D STR 19 R/H. P/N 143A9481-5 IAW SRM 51-40-02 AND DWG 143A7902 REV:;[07] VERIFIED ITEM 6 CORRECTIVE ACTIONS.;[08] VERIFIED MEASUREMENTS.

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

FWD CARGO BAY GUSSET CRACKED BS 500D STR 19 L/H / [01] NOT FOUND ALLOWABLE DAMAGE LIMITS ON FOR FWD CARGO BAY GUSSET CRACKED BS 500D STR 19 L/H ; MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED FWD CARGO BAY GUSSET CRACKED BS 500D STR 19 L/H IAW SRM 51-40-02;[03] RECEIVED; LOCATED AND DRILLED NEW FWD CARGO BAY GUSSET AT BS 500D STR 19 L/H. P/N 143A9481-6 LOT #1480476-3 IAW SRM 51-40-05 AND DWG 143A 7902 REV:;[04] OK TO INSTALL;[05] VERIFIED ITEM 3 CORRECTIVE ACTIONS. OK TO INSTALL.;[06] INSTALLED NEW FWD CARGO BAY GUSSET AT BS 500D STR 19 L/H. P/N 143A9481-6 IAW SRM 51-40-02 AND DWG 143A7902 REV:;[07] VERIFIED ITEM 6 CORRECTIVE ACTIONS.;[08] VERIFIED MEASUREMENTS.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

AFT CARGO BAY AFT CORRNER SCUFF PLATE CRACKED / [01] UPDATED MEASUREMENTS;[02] WELDED CRACKED RADIUS OF AFT CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4)<BR>WELDING MACHINE CAL INFO. E105083; DUE DATE 12/22;[03] VERIFIED CORRECTIVE ACTION 2.;[04] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2561-1;2;3 CAL DUE: 08/22;[05] SANDED REPAIR AREA PER SRM 53-60-15-2R-1 PARA 4.B.(5);[06] VERIFIED CORRECTIVE ACTION 5.;[07] APPLIED CHEMICAL CONVERSION COATING; PRIMER AND PARTING AGENT. IAW SRM 51-20-01; AMM 53-11-02-420-801. INSTALLED AFT CORNER SCUFF PLATE IAW AMM 53-11-02-420-801

Part: SIDEWALL SUPPORT — CORRODED (FWD CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

CORROSION FCB L/H FLOOR TO SIDEWALL SUPPORT FROM STA 400+2 TO STA 500B+13; LBL 25; WL 156. AFTER THE REWORK PIECE SIDEWALL SUPPORT IS OUT OF LIMITS IAW SRM 53-00-53-1A-2 IT HAS TO BE REPLACED IAW SRM 51-10-02; BLENDED AREAS AFT OF BS 480+6 MEASUSURE:480+11; 1.7'L X 0.9'W. REMAINING 0.038'.FABRICATED; LOCATED AND DRILLED REPAIR SPLICE LOCATED AT BS 480+8 LBL25; WL156; IAW SRM 53-00-53-2R-5; SRM 51-40-05-0G-0. LOCATED AND DRILLED NEW L/H FLOOR TO SIDEWALL AT BS 396 TO BS 480+8; LBL 25; WL 156 IAW SRM 51-40-05-0G-0 AND DWG 143A7500.APPLIED CHEMICAL CONVERSION COATING AND PRIMER AT ALL REWORKED AREAS FROM BS480+11 TO BS500D+13 IAW SRM 53-00-53-1A-2 STEP 2E INSTALLED SPLICE REPAIR LOCATED AT BS 480+8 LBL25; WL156; IAW SRM 53-00-53-2R-5; INSTALLED BONDED NUT PLATES IAW BOEING DWG 143A7501 REV:A;

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767 - BS787 RBL22. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION 1.;[03] RECEIVED NEW ACB FWD SHIELD<BR>ITEM# : 146A8127U12ATSMRO<BR>PO# : 863268/1;[04] LOCATED; DRILLED; AND COUNTERSANK NEW ACB FWD SHIELD IAW SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 146A8127 ID:0008 REV:-;[05] UPDATED MEASUREMENTS;[06] VERIFIED CORRECTIVE ACTIONS 4 AND 5.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS767 - BS727B RBL21. REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS767-BS727B RBL 21 WL 156. BS 767; L=2.' X W=1.'X DEPTH =.010' ;ORIGINAL THICKNESS .040' REMAINING THIKCNESS 0.030' FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A-2. BS 727B; L=3.' X W = 2.' X DEPTH= 0.010';ORIGINAL THICKNESS 0.040' REMAINING THICKNESS 0.030' FOUN TO BE OUT LIMITS IAW SRM 53-00-53-1A-2. FABRICATED;LOCATED AND DRILLED NEW FLOOR TO SIDEWAL SUPPORT AT AFT CARGO BAY BS 727 TO BS 767 RBL 21 WL 156 MATERIAL USED P/N BAC 1496-377#7075T62.IAW SRM 51-40-05 AND DWG 146A7502 REV: APPLIED CHEMICAL CONVERSION COATING ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727 TO BS 767 RBL 21 WL 156 IAW SRM 51-20-01 AND AMM 51-21-72-370-804. APPLIED PRIMER ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727 TO BS 767 RBL 21 WL 156 IAW AMM 51-21-72-370-804.

Part: STRINGER — CRACKED · airframe 50,055 hrs · 25,216 cycles

STR 23L/H CRACKED AT BS 520+16' / EVALUATED CRACK AT STRINGER 23L; STA 536. L= 1.5' X D= .036'.FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMIS PER SRM 53-00-03-1A-1.REMOVED DAMAGE BY TRIMMING OUT STRINGER 23L SECTION BETWEEN STA 500D +10' AND STA 536. PER SRM 51-10-02-0G-0. NEW STRINGER SECTION HFAB53-STS-011 AND HAT SECTION HFAB53-HS-011 IAW SRM 53-00-03-2R-1 REPAIR 1; MATERIAL USED 7075T0 .036' LOT#1470354; HEAT TREATED TO T6 AND PENETRAND INSPECTED IAW EA:22-153-01410; SRM 53-00-03-2R-1 REAPAIR 1. BAC5602 AND DWG 143A3221-(37).AND HAT SECTION HFAB53-HS-011; MATERIAL USED: 7075T0 0.040' LOT#1391218-1; HEAT TREATED TO T6 IAW EA:22-153-01410; SRM 53-00-03-2R-1 REAPAIR 1. BAC5602;THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 22-153-01410

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

CRACKED BULKHEAD SUPPORT ANGLE AT AFT CARGO BAY BS866 LBL10. MARKED. / [01] NO SRM ALLOWABLE DAMAGE NOTED; PART REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARA 9.;[02] REMOVED AND REPLACED BULKHEAD SUPPORT BRACKET(ANGLE) PN 149A8109-114 AT BS 866 LBL 10 PER SRM 51-40-05-0G-0; 51-40-02-0G-0 AND DWG 149A8102 REV: - SHT 17.;[03] VERIFIED CORRECTIVE ACTION #1; 2

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS807 - BS836 RBL26. MARKED. / [01] REMOVED CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS 807 TO BS 836; RBL 26 ; WORK AREA ; BS 807 ; L 1.5'X W 1.0'X D 0.025'; BS 812 ; L 1.0'X W 1.0'X D 0.012; BS 827 ; L 1.5'X W 1.0'X D 0.015' ; FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1; USED DEPTH GAGE ; ID: ATS2677; S/N: UNKNOWN; DUE: 11/2022;[02] SRM 53-60-15-1A-1 IS APPLICABLE TO THIS;[03] RECEIVED A NEW WEB FROM STORES PN 146A8123U25 FROM STORES REF PO 863713.<BR>LOCATED AND DRILLED NEW WEB IAW SRM 51-40-05-0G-0 AND DWG 146A8120 REV:-;[04] NEW WEB TO BE INSTALLED ON CUSTOMER CARD TTG8Q0049N7S.

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

CORROSION ON FCB R/H FLOOR TO SIDEWALL SUPPORT FROM STA 500A+2 TO STA 500C+17; RBL 25; WL 156.REMOVED CORROSION FROM FCB R/H FLOOR TO SIDEWALL SUPPORT AT BS500A+6 MEASURED 1.4'L X 0.9'W AND 0.0075'DEEP, FROM FCB R/H FLOOR TO SIDEWALL SUPPORT AT BS500A+10 MEASURED 1.7'L X 1'W AND 0.0095'DEEP, FROM FCB R/H FLOOR TO SIDEWALL SUPPORT AT BS500A+14' MEASURED 1.4'L X 0.9'W AND 0.0065' , FROM FCB R/H FLOOR TO SIDEWALL SUPPORT AT BS500C+15 MEASURED 1.1'L X 0.7'W AND 0.005'DEEP,FROM FCB R/H FLOOR TO SIDEWALL SUPPORT AT BS500A+6 MEASURED 1.4'L X 0.9'W AND 0.0075'DEEP, FROM FCB R/H FLOOR TO SIDEWALL SUPPORT AT BS500A+10 MEASURED 1.7'L X 1'W AND 0.0095'DEEP FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. FABRICATED LOCATED AND DRILLED ON FCB R/H FLOOR TO SIDEWALL SUPPORT BS 500A TO BS 500D;RBL 25 WL 156 P/N BAC1496-444#7075T62 IAW SRM 51-40-05 AND DWG 143A7500 REV

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS918 RBL12. MARKED. / [01] REMOVED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS 918; RBL 12 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS 918; RBL 12 IAW SRM 51-40-05 AND BOEING DWG 147A7221. OK TO INSTALL;[03] VERIFIED ITEM 2 CORRECTIVE ACTIONS.;[04] INSTALLED NEW SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS 918; RBL 12 IAW SRM 51-40-02 AND BOEING DWG 147A7221;[05] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 4.;[06] TASK CARD COMPLETE;[07] VERIFIED MEASUREMENT TABLE AND TASK COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (AFT CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS787 - BS727A LBL21. REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS787-BS727A LBL 21 WL 156. BS 787; L=2.' X W=1.'X DEPTH =.010' ;ORIGINAL THICKNESS 0.040'REMAINING THIKCNESS 0.030' FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A-2. BS 727A; L=3.' X W = 2.' X DEPTH= 0.010';ORIGINAL THICKNESS 0.040' REMAINING THICKNESS 0.030' FOUN TO BE OUT LIMITS IAW SRM 53-00-53-1A-2.FABRICATED;LOCATED AND DRILLED NEW FLOOR TO SIDEWAL SUPPORT AND SPLICE; AT AFT CARGO BAY BS 727 TO BS 847; SPLICE BS 727E TO 747 LBL 21 WL 156 MATERIAL USED P/N BAC 1496-377#7075T62 ;IAW SRM 51-40-05 AND DWG 146A7502 REV; APPLY CHEMICAL CONVERSION COATING AND PRIMER.APPLIED CHEMICAL CONVERSION COATING AND PRIMER SIDEWALL SUPPORT AT AFT CARGO BAY BS 727 TO BS 847 AND SPLICE BS 727E TO BS 747 LBL 21 WL 156 IAW SRM 51-20-01 AND AMM 51-21-72-370-804.INSTALLED SPLICE BTW BS 727E TO BS 747 LBL 21 WL 156 IAW SRM 51-40-02 AND SRM 53-00-53-2R-6 REPAIR 6

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

CORROSION ON FCB DOOR CUTOUT FWD SHIELD FROM STA 420+16 TO STA 420+18; RBL 23 TO RBL 25; WL 156. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION 1.;[03] RECEIVED NEW FCB DOOR CUTOUT FWD SHIELD <BR>ITEM# : 143A8126U21ATSMRO<BR>PO# : 855387/1;[04] LOCATED; AND DRILLED NEW FCB DOOR CUTOUT FWD SHIELD IAW SRM 51-40-05-0G-0 AND DWG 143A8127 ID:0011 REV:A;[05] UPDATED MEASUREMENTS;[06] VERIFIED CORRECTIVE ACTIONS 4 AND 5..

Part: STRINGER — CRACKED · airframe 50,055 hrs · 25,216 cycles

STR 26L/H CRACKED AT BS 520+16'. ALLOWABLE DAMAGE 1 IS APPLICABLE FOR THIS EVALUATION.EVALUATED CRACK AT STRINGER 26L; STA 520+16. L= 0.75' X D= .036'. STRINGER CRACK FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-03-1A-1.REMOVED DAMAGE BY TRIMMING OUT STRINGER 26L SECTION BETWEEN STA 500D +10' AND STA 520+16 IAW SRM 51-10-02-0G-0.HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. LOCATED AND DRILLED NEW STRINGER SECTION 26 L/H BTW B/S 500D+10' TO B/S 540' HAT SECTION LOCATED STR 26L/H BTW B/S 500D TO B/S 520 LOT #1491203-1 IAW SRM 53-00-03-2R-1 REPAIR 1 AND DWG 143A3230 REV:A APPLIED CHEMICAL CONVERSION AND PRIMER ON REPAIR PARTS IAW SRM 53-00-03-2R-1 REPAIR 1 STEP 4(I-J) INSTALLED NEW STRINGER SECTION 26 L/H BTW B/S 500D+10' TO B/S 540' AND HAT SECTION BTW B/S 500D TO B/S 520 IAW SRM 53-00-03-2R-1 REPAIR 1 AND DWG 143A3230 REV:A AND DWG 143A0060 REV:A

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

CORROSION ON FCB DOOR CUTOUT AFT SHIELD FROM STA 480+5 TO STA 480+18; RBL 25; WL 156. / [01] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM FOR FCB DOOR AFT SHIELD; PART TO BE REPAIRED BY REPLACMENT PER SRM 51-10-02-0G-0;[02] VERIFIED APPLICABILITY OF SRM 51-10-02-0G-0;[03] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM FOR FCB DOOR AFT SHIELD; PART TO BE REPAIRED BY REPLACMENT PER SRM 51-10-02-0G-0VERIFIED APPLICABILITY OF SRM 51-10-02-0G-0;[04] INSPECTED & VERIFIED CORRECTIVE ACTION ITEMS 1-3.;[05] RECEIVED NEW FCB DOOR CUTOUT AFT SHIELD<BR>ITEM# : 143A8126U31ATSMRO<BR>PO# : 860330/1;[06] LOCATED; AND DRILLED NEW FCB DOOR CUTOUT AFT SHIELD IAW SRM 51-40-05-0G-0 AND DWG 143A8126 ID:0010 REV:A;

Part: SKIN — CRACKED (LH HOR STAB) · airframe 50,055 hrs · 25,216 cycles

LH HORIZONTAL STAB; LWR STAB SKIN CRACKED AT STAB STA 193.90; CUTOUT LOWER HORIZONTAL SKIN OF L/H HORIZONTAL STAB PER SRM 55-10-01-2R-11 STEP 4 (B) 2. AND DRILLED OUT EXISTING FASTENERS IN REPAIR AREA PER STEP 4 (F) 1. FABRICATED REPAIR DOUBLER PER SRM 55-10-01-2R-11 STEP4 G; DOUBLER FABRICATED FROM LOT #1468128-1 2024-T3; FILLER FABRICATED FROM LOT #1468136-12024-T3. FILLER FABRICATION;APPLIED CHEMICAL CONVERSION AND PRIMER PER SRM 55-10-01-2R-11 STEP 4 (M) AND (N);INSTALLED REPAIR DOUBLER IAW SRM 55-10-01-2R-11 REPAIR 11.TOTAL SURFACE AREA FOR REPAIR DOUBLER IS 78.375 SQUARE INCHES IAW SRM 55-10-01-2R-11 REPAIR 11 STEP 1 H APPLIED SEALANT AROUND EDGES OF DOUBLER IAW SRM 55-10-01-2R-11 REPAIR 11 STEP 4Q;

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 50,055 hrs · 25,216 cycles

AFT CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / WELDED CRACK ON FLANGE OF AFT CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4) WELDING MACHINE CALIBRATION ID: E10583; DUE DATE 12/2022;[02] VERIFIED CORRECTIVE ACTION 1.;[03] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2561-1;2;3 CAL DUE: 08/22;[04] SANDED WELD REPAIR AREA PER SRM 53-30-15-2R-1 PARA 4.B.(5);[05] VERIFIED CORRECTIVE ACTION 4.;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO BARE METAL AREAS IAW SRM 53-60-15-2R-1 STEPS 4.B.(6-7). INSTALLED ACB FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1 STEPS 4.B.(8-13).

Part: VAPOR BARRIER — CRACKED · airframe 50,055 hrs · 25,216 cycles

L/H VAPOR BARRIER DOUBLER (111A1511-27) LBL 6-31; BS 663 HAS A CRACK. (MARKED) / [01] FABRICATED DOUBLER FROM 2024-0 #0.040 LOT 1313418-1 IAW DWG 11A1511-27 REV.-A AND DWG 111A1000 REV:A;[02] VERIFIED CORRECTIVE ACTION 1.;[03] RECIVED DOUBLER ON CUSTOMER RO NO 867641-SWA. REQ. OK TO TREAT AND PRIME;[04] VERIFIED CORRECTIVE ACTION 3.<BR>OK TO TREAT AND PRIME;[05] APPLIED CHEMICAL CONVERSION AND PRIME AT DOUBLER IAW SRM 51-20-01-0G-0 AND SOPM 20-43-03;[06] DOUBLER GOING TO BE INSTALL ON CARDTTG8Q00C9UEE;[07] VERIFIED CORRECTIVE ACTION 5 AND 6.

Part: SUPPORT — CRACKED · airframe 50,055 hrs · 25,216 cycles

FLOOR SUPPORT CRACKED AT STA 540+1; WL 208; LBL1. / [01] REMOVED AND REPLACED FLOOR SUPPORT AT STA 540+1 WL 208 LBL 1 IAW SRM 51-40-02 AND BOEING DWG 143A0060;[02] EDITED FOR PROPER SIGN OFF REQUIREMENT.;[03] VERIFIED;[04] PICKED UP HOLES COMMON TO FLOOR PANEL INSTALLATION IAW SRM 51-40-05;[05] VERIFIED;[06] VERIFIED CORRECTIVE ACTIONS #1; #4.

Part: SUPPORT — CRACKED · airframe 50,055 hrs · 25,216 cycles

FLOOR SUPPORT CRACKED AT STA 540+1; WL 208; RBL1. / [01] COMPLETED STEP 1;<BR>REMOVED AND REPLACED CRACKED FLOOR SUPPORT AT BS 540+1 WL20 AND MATCHED DRILLED FLOOR BOARD HOLES IAW BOEING DWG 143A0060 AND SRM 51-40-02 AND SRM 51-40-05.;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION 1.;[04] COMPLETED TASK CARD;[05] COMPLETED TASK CARD SCREW GUN INFO: ID-ATS2271; S/N-1703316; DUE-04/2023;[06] CERITFY EDIT;[07] VERIFIED COMPLETE.

Part: FRAME — CRACKED (FWD ENTRY DOOR) · airframe 50,055 hrs · 25,216 cycles

CRACK IN RADIUS OF FRAME AT B.S. 312 JUST ABOVE FORWARD ENTRY DOOR CUT OUT. / [01] TRIMMED OUT DAMAGE AT STA 312 FRAME LBL32 WL282 IAW SRM 51-10-02-0G-0;[02] SRM 53-10-15-1A-1 IS APPLICABLE FOR ALLOWABLE DAMAGE.;[03] TRIMMED .250 FROM EDGE OF FRAME. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1.;[04] REQUEST NDI VERIFY TRIM OUT IS CRACK FREE IAW SRM 51-10-02-0G-0 PENDING ENGINEERING.;[05] VERIFIED CORRECTIVE ACTION 1-3;[06] HFEC INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS1465 CAL DUE: 08/22;[07] COMPLETE;[08] COMPLETE

Part: BULKHEAD — CRACKED · airframe 50,055 hrs · 25,216 cycles

CRACKED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL32 WL156. IDENTIFIED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL32 WL156 IAW SRM 57-10-10-0I-2 FIGURE 2; SHEET 1; TABLE 2; ITEM 4.DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR 4D(1).REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-04-2R-10 PER SRM 57-10-10-2R-2 PAR 1C. STOP DRILLED CRACK; REMOVED DAMAGE FROM BOTH FWD AND AFT FACE SHEETS; CLEANED IAW SRM 51-70-04-2R-10 PAR 4A-C. VALIDATED REPAIR PER SRM 51-70-04-2R-10; FABRICATED REPAIR PLIES OUT OF BMS 9-3 ST 1581 LOT#1393735-8 IAW SRM 51-70-04-2R-10 PAR 4D. INSTALLED REPAIR PLIES USING BMS 8-301 CL1 GR1 LOT#JH1GAA7833; VACUUM BAGGED; UNBAGGED AND LIGHTLY SANDED REPAIR PLIES IAW SRM 51-70-04-2R-10 PARA 4F;HREFINISHED REPAIR AREAS IAW SRM 51-70-04-2R-10 PARA 4.H;

Part: BULKHEAD — CRACKED · airframe 50,055 hrs · 25,216 cycles

CRACKED LOWER R/H COMPOSITE BULKHEAD AT BS663 RBL34 WL158.DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR 4D(1).REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-04-2R-10 PER SRM 57-10-10-2R-2 PAR 1C.STARTED DAMAGE REMOVAL ON BOTH FWD AND AFT FACE SHEETS IAW SRM 51-70-04-2R-10 PAR 4A-B. COMPLETED DAMAGE REMOVAL ON FWD AND AFT FACESHEETS AND CLEANED REPAIR AREAS IAW SRM 51-70-04-2R-10 PARA 4B-C FABRICATED REPAIR PLIES OUT OF BMS 9-3 ST 1581 LOT#1393735-8 IAW SRM 51-70-04-2R-10 PAR 4D.; INSTALLED REPAIR PLIES USING BMS 8-301 CL1 GR1 LOT#JH1GAA7833; VACUUM BAGGED; UNBAGGED AND TRIMMED EXCESS MATERIAL IAW SRM 51-70-04-2R-10 PARA 4.F;H.

Part: LIGHT — INOPERATIVE · airframe 49,896 hrs · 25,111 cycles

EMERGENCY LIGHTS POWER SUPPLY M1673 WILL NOT POWER LIGHTS OR TAKE A CHARGE. / [01] REMOVED & REPLACED EMERGENCY LIGHTS POWER SUPPLY M1673 PER AMM 33-51-06.

Part: LIGHT — INOPERATIVE · airframe 49,896 hrs · 25,111 cycles

LH OVERWING EMERGENCY EXIT SIGN HAS TWO BULBS INOP. / [01] RELAMPED LH OVERWING EMERGENCY EXIT SIGN PER AMM 33-51-01.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 46,850 hrs · 23,341 cycles

FWD SERVICE DOOR EMER LIGHT LENS; LOWER; MISSING DIRECTIONAL ARROW / REMOVED AND REPLACED FWD SERVICE DOOR EMERGENCY LIGHT LENS REF MM 33-51-01. OPS CHECKED GOOD

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,966 hrs · 22,838 cycles

EMERGENCY LIGHTS ABOVE L1 DOOR, EXTERIOR R1 DOOR, AND ABOVE SEAT ROW 6 DEF INOPERABLE. REMOVED AND REPLACED FWD GALLEY RT OVERHEAD EMERGENCY LIGHT BATTERY, REF AMM 33-51-06. OPERATIONS CHECKED GOOD.

Part: HOOK — DISLODGED (L1 DOOR GIRT BAR) · airframe 45,887 hrs · 22,794 cycles

FWD ENTRY DOOR GIRT BAR STORAGE CLIP ON THE LEFT SIDE IS VERY LOOSE AND THE GIRT BAR IS EASILY DISLODGED. SECURED BRACKET/CLIP, PER AMM 25-66-00. AIRCRAFT OKAY FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,788 hrs · 22,735 cycles

RT FWD EMERGENCY LIGHT INOPERABLE. RELAMPED RT FWD EMERGENCY LIGHT. OPS GOOD, REF AMM 33-51-04.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 45,657 hrs · 22,658 cycles

EXIT LIGHT SWITCH GUARD/COVER HAS BROKEN SPRING. ABOVE AFT FLIGHT ATTENDANT SEAT. R & R EXIT LIGHT SWITCH GUARD/COVER, REF. AMM 33-51-01.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 45,453 hrs · 22,543 cycles

EMERGENCY LIGHT LENS UNSECURE AT THE LEFT OVERWING EXIT. SECURED THE LEFT OVERWING EMERGENCY LIGHT LENS IAW SIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,238 hrs · 22,401 cycles

EMERGENCY EXIT LIGHTS L1187 ON FWD LAV & L1191 ON AFT GALLEY HAVE BULBS OUT. REPLACED THE LAMPS AND PERFORMED A GOOD FUNCTIONAL TEST IAW AMM 33-51-01-960-801, STEP 2C.(1)(A)1);4)(C);(2) AND (4).

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,238 hrs · 22,401 cycles

ALL EMERGENCY LIGHTS POWERED BY M1675 DID NOT ULLUMINATE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY (M1675) IAW AMM 33-51-06-960-805, REPLACED THE LAMP AT THE ESCAPE SLIDE LIGHT. PERFORMED A GOOD TEST.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,238 hrs · 22,401 cycles

AFT EMERGENCY LIGHT AT LEFT OVERWING EXIT WINDOW IS INOPERATIVE. REPLACED THE LAMPS AND PERFORMED A GOOD FUNCTIONAL TEST IAW AMM 33-51-01-960-801.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 45,238 hrs · 22,401 cycles

LEFT HORIZONTAL STABILIZER INSPAR RIB AT HSS 120.30; 4TH VERTICAL STIFFENER WAS CRACKED. REPAIRED STIFFENER IAW SRM 55-10-09-2R-4, PARA 4, & FIG 202.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 45,238 hrs · 22,401 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB, AT HSS 120.30, 2ND VERTICAL STIFFENER WAS CRACKED. REPAIRED STIFFENER IAW SRM 55-10-09-2R-4

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 45,238 hrs · 22,401 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB AT HSS 120.30, 4TH VERTICAL STIFFENER WAS CRACKED. REPAIRED THE STIFFNER IAW SRM 55-10-09-2R-4.

Part: SEAT TRACK — CORRODED (BS 500D) · airframe 45,238 hrs · 22,401 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT BS 500D, LBL 45, WL 208.1. REMOVED CORROSION, BLENDED 0.035'D X 2' X 1'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED AND REPLACED THE SEAT TRACK SECTION FROM BS480 - 520 IAW SRM 51-40-02, AND DWG 143A5300.

Part: BOOT — DAMAGED (RADOME) · airframe 45,238 hrs · 22,401 cycles

NOSE RADOME BOOT IS DAMAGED / REMOVED DAMAGED RADOME BOOT IAW AMM 53-52-00-000-802 PAR 4C(1-2). 6042U 22JUN20. 10537C 06/22/20 INSTALLED NEW RADOME BOOT IAW AMM 53-52-00-400-802 PAR 5E(1-14) 13742C 06-26-20

Part: SKATE ANGLE — CHAFED (BS 1106-1110) · airframe 45,238 hrs · 22,401 cycles

CHAFING ON RIGHT HAND SKATE ANGLE AT B.S. 1106-1110; W.L. 306.5; R.B.L. 14. / REMOVED AND REPLACED SKATE ANGLE R/H SIDE BS1016 TO BS1132 W.L.306.5 RBL14 IAW SRM 51-40-02 AND DWG 148A8300 57049U 25JUNE2020

Part: SKATE ANGLE — CHAFED (BS 1106-1110) · airframe 45,238 hrs · 22,401 cycles

CHAFING ON LEFT HAND SKATE ANGLE AT B.S. 1106-1110; W.L. 306.5; L.B.L. 14. / REMOVED DAMAGED LEFT HAND SKATE ANGLE AT BS 1106-1110; WL 306.5; LBL 14. IAW SRM 51-40-02. FABRICATED AND INSTALLED A NEW SKATE ANGLE IAW SRM 51-40-02; 51-40-08; 51-40-05 AND DWG 148A8300 SH2; REV A

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 45,238 hrs · 22,401 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION IN MULTIPLE AREAS BS 727-849 LBL 24 WL 148 / REPLACED AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT B.S 727-849 LBL24 W.L 148 IAW DWG 146A7500 AND SRM 51-40-02-0G-0 CORROSION OUT OF LIMITS.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 45,238 hrs · 22,401 cycles

CHAFING ON RIGHT HAND SKATE ANGLE AT B.S. 1007-1016; W.L. 306.5; R.B.L. 14. / REMOVED AND REPLACED SKATE ANGLE AT BS1007 TO BS1016 WL306.5 RBL14 IAW SRM 51-40-02 AND DWG 147A0030 REV. A 57049U 25JUNE2020

Part: SKATE ANGLE — CHAFED (BS 1007-1016) · airframe 45,238 hrs · 22,401 cycles

CHAFING ON LEFT HAND SKATE ANGLE AT B.S. 1007-1016; W.L. 306.5; L.B.L. 14. / REMOVED DAMAGED LEFT HAND SKATE ANGLE AT BS 1007-1016; WL 306.5; LBL 14 IAW SRM 51-40-02. FABRICATED AND INSTALLED A NEW SKATE ANGLE IAW SRM 51-40-02; 51-40-05; 51-40-08 AND DWG 147A0030 SH 14; REV A

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 45,238 hrs · 22,401 cycles

BS 663 LWR COMPOSITE VAPOR BARRIER CRACKED RBL 36 WL 150. REPAIRED IAW SRM 51-70-04-2R-10.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 45,238 hrs · 22,401 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED / REPAIRED AFT CARGO BAY; AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1 AND BAC5975. SCUFF PLATE IS INSTALLED ON CUSTOMER CARD 753-721-10-01

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 44,884 hrs · 22,198 cycles

WE REBALANCED THE FUEL TO WITHIN 300-400 LBS. WE WERE ON DECENT & BALANCING WAS SLOW. AFTER CLOSING THE CROSSFEED VALVE AGAIN & CONFIGURED FOR LANDING; THE RIGHT TANK FUEL LOAD BEGAN INCREASING. RIGHT SIDE WENT FROM 4100 LBS TO 4780 FROM 1000' AGL TO THE GATE THE LEFT TANK DECREASED ABOUT 100-300 LBS. IN THE SAME TIME FROM CONTINUED FROM PAGE 1199100 / TRANSFERED TO NRC # D423185

Part: STRAP — LOOSE (L1 DOOR) · airframe 43,292 hrs · 21,237 cycles

FORWARD ENTRY DOOR SAFETY STRAP COULD NOT BE SECURED. INSTALLED SAFETY STRAP SNAP PER SIP.

Part: PAD — WORN (L1 DOOR SLIDE) · airframe 43,283 hrs · 21,229 cycles

FORWARD ENTRY DOOR EMERGENCY SLIDE GIRT PAD WORN. R&R SLIDE PER AMM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 43,283 hrs · 21,229 cycles

FORWARD RT EGRESS LIGHTING STRIP DELAMINATED. R&R LIGHT STRIP PER AMM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 42,691 hrs · 20,846 cycles

FORWARD GALLEY EMERGENCY #1 FLASHING NOT BLINKING. R&R BATTERY PER SIP.

Part: BLADE — CRACKED (NR 2 ENGINE) · airframe 41,692 hrs · 20,240 cycles

#2 ENGINE, #1 BLADE SHOWS VTI CRACK INDICATION OF 376 FSH WITHIN GATED AREA @ 7.0 ON THE HORIZONTAL BASELINE. REMOVED & REPLACED #1 FAN BLADE ON #2 ENGINE PER TASK CARD 772-21-20 AMM 72-21-02 POS/1

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,105 hrs · 19,906 cycles

RT OVERWING EMERGENCY EXIT DOWN LIGHT AFT BULB INOP. RELAMPED BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,105 hrs · 19,906 cycles

AFT GALLEY DOOR EMERGENCY DOWN LIGHT BULB INOP. RELAMPED AFT GALLEY DOOR EMERGENCY DOWN LIGHT IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 39,548 hrs · 18,939 cycles

G1 LOWER EMERGENCY LIGHT ASSEMBLY DAMAGED. R&R LIGHT IAW AMM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 39,548 hrs · 18,939 cycles

R1 DOOR NR 5 BEAM UPPER BEAM CRACKED. R&R BEAM IAW CCO AND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 39,548 hrs · 18,939 cycles

R1 DOOR NR 4 BEAM LOWER BEAM CRACKED. R&R NR 4 BEAM IAW CCO AND DWG.

Part: PANEL — CRACKED (RT WING) · airframe 39,548 hrs · 18,939 cycles

RH WING LEADING EDGE LOWER CAVITY PANEL 621YB HAS A CRACK O/B FWD CORNER. / REPAIRED RH WING L/E PANEL 621YB IAW SRM 51-70-04-2R-6 REV 65; SRM 51-70-04-2R-0; AND SRM 51-70-14-2R-3 REV 65. RESTORED FINISH TO PANEL IAW AMM 51-21-77-300-801 REV. 65

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 39,548 hrs · 18,939 cycles

LH HORIZONTAL STABILIZER REAR SPAR STIFFENER IS CRACKED AT STAB STA 120.30 / FABRICATED L/H HORIZONTAL STAB REAR SPAR RIB STA 120.3 AFT STIFFENER IAW AAR EA 180427 IR AND SWA EA 1-755-4177 REV IR REMOVED AND INSTALLED ON NRC X800778 SA-M 326 E275917 ITEM 4

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 39,548 hrs · 18,939 cycles

LT WHEEL WELL VERTICAL BULKHEAD ATTACH ANGLE CRACKED AT BS 663, LBL 35. REPAIRED ANGLE IAW EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

E&E BAY CHORD CORRODED BETWEEN BS 360 TO BS 312, STR 23L. R&R CHORD IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,548 hrs · 18,939 cycles

PASSENGER CABIN FLOOR PANEL 242HF AFT EDGE DELAMINATED SEVERAL AREAS / REPAIRED DELAMINATION ALONG AFT EDGE OF CABIN FLOOR PANEL 242HF I.A.W B737 SRM 53-00-50-2R-9

Part: SUPPORT — PULLED (CABIN) · airframe 39,548 hrs · 18,939 cycles

PASSENGER CABIN FLOOR SUPPART SPLICE AT STA 540 LBL 0- LBL 24 HAS PULLED THROUGH THE FASTENERS / REMOVED AND REPLACED FLOOR SUPPORT AR STA 540 LBL0-LBL24 IAW BOEING DWG# 143A0060 REV- FRAME 2 AND SRM 51-40-02-0G-0 STEP 9

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 39,548 hrs · 18,939 cycles

AFT CARGO PIT FLOOR PANEL 140DF HAS CORROSION ON UPPER SURFACE AFT AND LEFT EDGES / FABRICATED AFT CARGO PIT FLOOR PANEL 140DF IAW BOEING DWG 453A 2600 REV: A AND B737 SRM 51-40-05-0G-0

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 39,548 hrs · 18,939 cycles

AFT CARGO PIT DOOR SURROUND FORWARD SHIELD STA 767-794 RBL 22 HAS CORROSION UPPER AND LOWER SURFACE / REMOVED AND RPLACED AFT CARGO DOOR SURROUND FORWARD SHEILD STA 767-794 FBL IAW BOEING DWG 146A0081 REV A AND B737 SRM 51-40-02-0G-0

Part: CARGO TRACK — CORRODED (CARGO TRACK) · airframe 39,548 hrs · 18,939 cycles

AFT CARGO PIT FLOOR TRACK CORRODED BETWEEN BS 787 TO BS 827+14, RBL 13.8. REPAIRED FLOOR TRACK IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

FORWARD WET AREA STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 35. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, LBL 2. R&R INTERCOSTAL IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

AFT CARGO PIT LT Z ANGLE CORRODED BETWEEN BS 727+4 TO BS 727E+13, LBL 21. REPAIRED Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

AFT CARGO PIT RT Z ANGLE CORRODED BETWEEN BS 727+4 TO BS 767, RBL 21. R&R "Z" ANGLE IAW SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO THRESH) · airframe 39,548 hrs · 18,939 cycles

AFT CARGO PIT DOORWAY LOWER SILL NUTPLATE STRAP UNDER UPPER FLANGE OF VERTICAL WEB HAS CORROSION STA 827+16 RBL 19 / REMOVED AND REPLACED NUTPLATE STRAP P/N 146A31528-19 AT STA 827 +16 RBL19 IN AFT PIT IAW BOEING DRAWING 146A8340 REV C AND SRM 51-40-02-0G-0 STEP 7

Part: WEB — CORRODED (CABIN) · airframe 39,548 hrs · 18,939 cycles

AFT WET AREA FLOOR STRUCTURE; AFT WEB AT STA 1016 TO BULKHEAD; LBL 9-15; AREA HAVE CORROSION. / BLENDED CORROSION ON AFT L/H LAV PAN 100% MATERIAL LOSS. FOUND OUT OF LIMITS IAW SDM53-70-51-1A-1. FABRICATED NEW WEB ON B/S W/O 38046-2400-0001. REPLACED WB; P/N 147A5620-19; AND INSTALLED IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 147A5600 REV A

Part: SHIELD — CORRODED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

AFT CARGO PIT DOOR SURROUND AFT SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 22. R&R SHIELD IAW DWG & SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

FUSELAGE SKIN BELOW AFT CARGO DOOR SCUFF PLATE CORRODED BETWEEN BS 797 TO BS 839. REPAIRED SKIN IAW SRM AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: TRACK — CORRODED (AFT CARGO COMPT) · airframe 39,548 hrs · 18,939 cycles

AFT CARGO PIT FLOOR TRACK LBL 17.1 HAS CORROSION INSIDE OF TIEDOWN STA 787-791 / REMOVED CORROSION AND MEASURED MATERIAL LOSS TO BE .004 WITH A MAX LOSS ALLOWED TO BE .040. MATEIRIAL LOSS FOUND TO BE 'OUT OF LIMITS' IAW SRM 53-00-53-1A-2 STEP 4(B)2 AND FIGURE 103 DETAIL D-D. REMOVED AND REPLACED FLOOR SUPPORT TRACK AT STA 727 - 847 LBL 17 IAW BOEING DWG # 146A7500 REV: A AND SRM 51-40-02-0G-0. APPLIED CIC TO NEW TRACK IAW AMM 51-21-91-620-802 STEP 3(C) WN7849

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

L1 DOOR FORWARD WET AREA CREASE BEAM CORRODED AT BS 328. R&R CHORD IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 39,548 hrs · 18,939 cycles

RT MAIN WHEEL WELL SPAR VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,548 hrs · 18,939 cycles

FWD WET AREA FLOORBOARD 221AF HAS PEELING COMPOSITES. / EVALUATED; PREPPED; CLEANED AND REPAIRED DAMAGE TO UPPER SURFACE FIBERS ON FLOORBOARD 221AF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A; C; E & F; K1; L1; M1) REV 65.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 39,548 hrs · 18,939 cycles

PASSENGER CABIN FLOOR PANEL 232CF HAVE TOP SURFACE FIBERGLASS PULLED UP. / REPAIRED PASSENGER CABIN FLOOR PANEL 232CF OF LOOSE FIBERS ON TOP SURFACE WITH NO DAMAGE TO COMPOSITE SUBSTRATE IAW B737 SRM 53-00-50-2R-0 REV 65 AND B737 SRM 53-00-50-2R-1 REV 65 A11393;A75111

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 39,548 hrs · 18,939 cycles

PASSENGER CABIN FLOORBOARD 231CF HAS EDGE DAMAGE ON FWD EDGE AND O/B EDGE AS MARKED. / EVALUATED; PREPPED; CLEANED AND REPAIRED DAMAGE TO UPPER FACESHEET AND CORE AT FWD & O/B EDGE OF FLOORBOARD 231CF IAW B737 SRM 53-00-50-2R-4; PAR 3 (A-K1; L1; M1) & (N) REV 65.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,548 hrs · 18,939 cycles

FWD WET AREA FLOORBOARD 221DF HAS PEELING COMPOSITES AS MARKED. / REPAIRED FWD WET AREA FLOORBOARD 221DF OF PEELING FIBERS ON FACE SHEET WITH NO DAMAGE TO COMPOSITE SUBSTRATE IAW B737 SRM 53-00-50-2R-0 REV 65 AND B737 SRM 53-00-50-2R-1 REV 65. A62661; A11393

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 39,548 hrs · 18,939 cycles

AFT CARGO PIT DOORWAY LOWER SILL WEB STA 794-847 RBL26 UPPER SURFACE HAS CORROSION / REMOVED CORROSSION ON AFT CARGO DOOR LOWER SILL UPPER SUFACE IAW B737-700 51-10-OG-0 PARA 51 MATERIAL LOSS AND LIMITS VERIFIED AS MAX 10T OF ORIG 'T'.050 ' LOSS .008 REM '042' MATERIAL LOSS WAS DEEMED OUT OF LIMITS IAW B737-7-- SRM 53-60-15-1A-1 FIG103. REMOVED AND REPLACED LOWER SILL IAW B737-700 SRM 57-40-0G-0 PARA 4 AND 5 APPLIED CK TO SILL IAW B737-700AMM 51-2191-620 802 TOOL36644 DUE 09/26/18

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 39,548 hrs · 18,939 cycles

RT HORIZONTAL STABILIZER LEADING EDGE STA 123.85 AND 27" AFT RIB CRACKED AT STIFFENER. REPAIRED STIFFENER IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,548 hrs · 18,939 cycles

FWD WET AREA FLOORBOARD 221BF HAS PEELING COMPOSITES AS MARKED. / REPAIRED PEELING COMPOSITE AS MARKED ON FWD WET AREA FLOOR BOARD 221BF I.A.W B737 SRM 53-00-50-2R-1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,548 hrs · 18,939 cycles

FWD WET AREA FLOORBOARD 221EF HAS PEELING COMPOSITES. / REPAIRED FWD WET AREA FLOORBOARD 221EF OVER ALMOST ENTIRE UPPER SHEET IAW B737 SRM 53-00-50-2R-1 REV 65; CURED IN OVEN FOR 1 HR.L IN AT 12:30-OUT AT 1:30 A30990 A80195

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,548 hrs · 18,939 cycles

FWD WET AREA FLOORBOARD 221CF HAS PEELING COMPOSITES. / REPAIRED FWD WET AREA FLOORBOARD 221CF UPPER SURFACE IAW B737 SRM 53-00-50-2R-0 REV 65 AND SRM 53-00-50-2R-1 REV 65

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 39,548 hrs · 18,939 cycles

FWD WET AREA FLOORBOARD 221BF HAS PEELING COMPOSITES. / REPAIRED DAMAGE ON PANEL 221BF. BONDED REPAIR PLY AND CURED. TAP TEST GOOD. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0

Part: BRACKET — CRACKED (LEFT WING) · airframe 39,548 hrs · 18,939 cycles

L/H WING TRAILING EDGE AT MAIN LANDING GEAR SUPPORT BEAM BRACKET THAT ATTACHES TO PANEL 551FB IS BROKEN / REMOVED & REPLACED L/H WING TRAILING EDGE SUPPORT BEAM BRACKET ATTACHED TO PANEL 551FB IAW B757-700 SRM 51-40-02-0-0G1 DWG 115 A2710 REV - SHEET 007 ATAG-A97139

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 39,548 hrs · 18,939 cycles

LT HORIZONTAL STABILIZER INSPAR RIB STAB STA 120.30 CRACKED AT 3RD VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 39,548 hrs · 18,939 cycles

RIGHT WING; UPPER FIXED TRAILING EDGE; BETWEEN #7 AND #8 SPOILER; MIDDLE BULB SEAL RETAINER BRACKET IS CRACKED. / REMOVED AND REPLACED SEAL RETAINER IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG # 115A293U REV-

Part: ANGLE — CORRODED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

FORWARD CARGO COMPARTMENT BETWEEN RT Z ANGLE CORRODED BETWEEN BS 500 TO BS 500D. R&R "Z" ANGLE IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 39,548 hrs · 18,939 cycles

LT WING TRAILING EDGE INBOARD OF DEFLECTION CONTROL RIB SEAL SUPPORT BRACKET CRACKED. R&R BRACKET IAW SRM.

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 39,548 hrs · 18,939 cycles

FWD CARGO COMPARTMENT BETWEEN STA 440 AND 492 UNDER CARGO DOOR CENTER TRESHOLD PLATE; TRESHOLD WEB IS CORRODED SEVERAL AREAS TOP SURFACE / REMOVED AND REPLACED THRESHOLD WEB IAW B737 SRM 51-40-02 PARA 5 AND BOEING DWG# 143A8330 REV 8 SHEET 0042

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 39,548 hrs · 18,939 cycles

LT HORIZONTAL STABILIZER INSPAR RIB STAB STA 120.30 CRACKED AT 2ND VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: SHIELD — CORRODED (FWD CARGO RH) · airframe 39,548 hrs · 18,939 cycles

FWD CARGO COMPARTMENT BETWEEN STA 492 AND 500A AND BETWEEN STR 25R AND 26R FLOOR SHIELD IS CORRODED IN SEVERAL AREAS TOP SURFACE / EVALUATED CORROSION ON SHIELD FOUND TO BE 100% OUT OF LIMITS IAW SRM 53-30-15-1A-1 FIG 103 VERIFIED NEW SHIELD P/N 143A8126431 IAW BOEING DWG 143A0080 REV- INSTALLED NEW SHIELD FWD PIT STA 492-500A BETWEEN STR 25R AND 26R IAW BOEING DWG 143A0080 REV- ATAG #TI0086

Part: GUSSET — CRACKED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW DWG & SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW DWG AND SRM.

Part: STRIP — CORRODED (FWD CARGO RH) · airframe 39,548 hrs · 18,939 cycles

FWD CARGO PIT R/H/S AFT CAP STRIP IS CORRODED IN SEVERAL AREAS BOTTOM SIDE AS MARKED / REPLACED CORRODED FWD CARGO R/H/S CAP STRIP; PN-453A1611-12 IAW BOEING DWG 453A1611; ID:8; REV:D. A TAG # WN8944.

Part: STRIP — CORRODED (FWD CARGO LH) · airframe 39,548 hrs · 18,939 cycles

FWD CARGO PIT L/H/S MID CAP STRIP TOP SIDE; BOTH FWD AND AFT CORNERS ARE CORRODED / REPLACED FWD CARGO L/H/S MID CAP STRIP PN 453A1611-11 IAW BOEING DWG 453A1611; ID:7. REV:B A TAG # YV0021

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 39,548 hrs · 18,939 cycles

FWD CARGO FLOOR PNL 120 AF TOP AND BOTTOM SIDES IN SEVERAL AREAS AS MARKED IS CORRODED / REPLACED PART ON SHELF IAW BOEING DWG #453A 1600 REVA SHEET 0088 ATAG # WN770

Part: STRIP — CORRODED (FWD CARGO LH) · airframe 39,548 hrs · 18,939 cycles

FWD CARGO PIT #2 CAPSTRIP L/H/S SEVERAL AREAS OF CORROSION ON BOTTOM SIDE AS MARKED / REPLACED FWD CARGO PIT #2 CAP STRIP; L/H/S. PN 453A1611-10 IAW BOEING DWG 453A1611; ID:6; REV:D. A TAG # WN2820.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 39,548 hrs · 18,939 cycles

AFT CARGO COMPARTMENT DOOR LOWER FORWARD CORNER THRESHOLD PLATE CRACKED ON TOP AFT EDGE. REPAIRED SCUFF PLATE IAW EA.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 39,311 hrs · 18,799 cycles

RUDDER BALANCE WEIGHT SHOWS SIGNS OF CORROSION WITH MISSING MATERIAL ON TOP SIDE IN TWO LOCATIONS. / REPLACED RUDDER BALANCE WEIGHT PER CMM 55-40-09.

Part: LENS — LOOSE (CABIN) · airframe 37,885 hrs · 17,985 cycles

L2 DOOR EMERGENCY SIGN LENS LOOSE. R&R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,173 hrs · 16,923 cycles

LT EXTERIOR ESCAPE HATCH EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,887 hrs · 16,147 cycles

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

Part: SIGN — DEFECTIVE (CABIN) · airframe 33,999 hrs · 15,635 cycles

R1 DOOR LOWER BULKHEAD EXIT SIGN MISSING RED ARROW. R&R SIGN PER AMM.

Part: SIGN — DEFECTIVE (CABIN) · airframe 33,999 hrs · 15,635 cycles

L1 DOOR LOWER BULKHEAD EXIT SIGN MISSING RED ARROW. R&R SIGN PER AMM.

Part: SEAT TRACK — CORRODED (BS 787) · airframe 33,293 hrs · 15,238 cycles

NR 3 SEAT TRACK FLANGE CORRODED AT BS 787. REPAIRED THE SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 810) · airframe 33,293 hrs · 15,238 cycles

NR 4 SEAT TRACK CORRODED ON FLANGE AND INSIDE OF TRACK AT BS 810. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 727A) · airframe 33,293 hrs · 15,238 cycles

NR 4 SEAT TRACK FLANGE CORRODED AT BS 727A+10. REPAIRED THE SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 757) · airframe 33,293 hrs · 15,238 cycles

NR 4 SEAT TRACK CORRODED ON FLANGE AND INSIDE OF TRACK AT BS 757. R & R THE SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 787) · airframe 33,293 hrs · 15,238 cycles

NR 4 SEAT TRACK CORRODED ON FLANGE AND INSIDE OF TRACK AT BS 787. R & R THE SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 727E) · airframe 33,293 hrs · 15,238 cycles

NR 4 SEAT TRACK FLANGE CORRODED AT BS 727E+2. REPAIRED THE SEAT TRACK IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,293 hrs · 15,238 cycles

INTERCOSTAL CRACKED AT BS 540, RBL 0, SEAT TRACK NR 3. R & R INTERCOSTAL IAW SRM.

Part: HOOK — CORRODED (EMERGENCY EXIT) · airframe 33,293 hrs · 15,238 cycles

RIGHT EMERGENCY EXIT ESCAPE HATCH STRAP HOOK CORRODED. REPAIRED HOOK PER MT.

Part: HOOK — CORRODED (EMERGENCY EXIT) · airframe 33,293 hrs · 15,238 cycles

LEFT EMERGENCY EXIT ESCAPE HATCH STRAP HOOK CORRODED. REPAIRED HOOK PER MT.

Part: INTERCOSTAL — DELAMINATED (BS 312-328) · airframe 32,945 hrs · 15,052 cycles

INTERCOSTAL DELAMINATED BETWEEN BS 312 - 328. R & R THE INTERCOSTAL PER SRM.

Part: FITTING — CORRODED (LT MLG) · airframe 32,583 hrs · 14,872 cycles

LEFT MLG FWD TRUNNION BEARING FITTING LUG FACE CORRODED. R & R FITTING IAW EA.

Part: SUPPORT FITTING — CORRODED (RT WING) · airframe 32,583 hrs · 14,872 cycles

RIGHT WING UPPER INBD BORE FACE OF TRUNNION SUPPORT FITTING CORRODED. R & R FITTING IAW EA.

Part: LENS — UNSECURE (CABIN) · airframe 31,862 hrs · 14,465 cycles

FORWARD SERVICE EMER EXIT LIGHT LENS FELL OFF. R & R LIGHT ASSEMBLY IAW AMM.

Part: MODULE — FAULTY (COCKPIT) · airframe 29,574 hrs · 13,148 cycles

DIVERSION, OVERHEAT DETECTION FAULT LIGHT ILLUMINATED INTERMITTENTLY WITH OVERHEAT DETECTION SWITCH IN B POSITION. LOOP DEFERRED AS INOPERATIVE. R & R ENG FIRE DETECTOR MODULE IAW MM.

Part: SENSOR — FAULTY (TE FLAP) · airframe 28,587 hrs · 12,616 cycles

DECLARED EMER, FLAPS DID NOT DEPLOY NORMALLY OR USING ALTERNATE FLAP SWITCH. R & R NR 7 FLAP SKEW SENSOR IAW MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 26,708 hrs · 11,613 cycles

L2 DOOR EMER EVAC SLIDE GIRT BAR FABRIC LOOSE. SECURED SLIDE IAW AMM.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 26,708 hrs · 11,613 cycles

AFT CARGO DOOR INNER SKIN CORRODED. REPAIRED SKIN IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 26,708 hrs · 11,613 cycles

FORWARD CARGO BAY FLOOR PANEL 120CF CORRODED. R & R PANEL IAW DWG.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

AFT CARGO COMPARTMENT FRAME SPLICE CORRODED AT BS 787 BETWEEN RBL 20 TO 30. REPAIRED SPLICE IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

FORWARD SEAT TRACK HOLES COMMON TO SPLICE STRAP CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW ER & EA.

Part: LENS — CRACKED (CABIN) · airframe 26,708 hrs · 11,613 cycles

R1 DOOR EMER LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 26,708 hrs · 11,613 cycles

AFT CARGO BAY CARGO TIE DOWN TRACK CORRODED AT BS 794 RBL 14. R & R TRACK IAW SRM.

Part: FASTENER — MISSING (L1 DOOR) · airframe 26,708 hrs · 11,613 cycles

L1 DOOR SLIDE COVER AFT GIRT BAR RETAINER FASTENER MISSING. INSTALLED FASTENER IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 26,708 hrs · 11,613 cycles

AFT CGO BAY FLOOR PANEL 140DF CORRODED ON UPPER SURFACE ALONG THE EDGES OF PANEL. R & R PANEL IAW DWG & SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 26,708 hrs · 11,613 cycles

AFT CABIN FLOOR PANEL 241YF DELAMINATED ON UPPER SURFACE. REPAIRED FLOOR PANEL IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 727B TO 847 LBL 20. REPAIRED SUPPORT IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

FORWARD SEAT TRACK HOLES COMMON TO SPLICE STRAP CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW ER & EA.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 26,708 hrs · 11,613 cycles

FORWARD CARGO BAY FLOOR PANEL 120AF CORRODED. REPAIRED PANEL IAW DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

FORWARD SEAT TRACK, HOLES COMMON TO SPLICE STRAP CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW ER & EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 867 TO 947 RBL 20. R & R ANGLE IAW SRM.

Part: WEB — CRACKED (RT WING) · airframe 26,708 hrs · 11,613 cycles

RIGHT WING TRANSVERSE WEB CRACKED. R & R WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986 LBL 43. REPAIRED CHORD IAW EA.

Part: FITTING — CRACKED (VERTICAL STAB) · airframe 26,708 hrs · 11,613 cycles

CROSSBEAM CUT OUT AT FWD LUG FITTING ON RT SIDE CRACKED. R & R FITTING IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

BULKHEAD UPPER BARRIER CRACKED AT BS 663 RBL 32. REPAIRED BULKHEAD IAW SRM.

Part: WEB — CRACKED (LT WING) · airframe 26,708 hrs · 11,613 cycles

LEFT WING TRANSVERSE WEB CRACKED. R & R WEB IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

RIGHT NR 3 WINDOW FRAME E - F POST 2ND FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED POST IAW EO.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

FRAME SPLICE CORRODED AT BS 767 BETWEEN RBL 20 TO 30. REPAIRED SPLICE IAW ER & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 26,708 hrs · 11,613 cycles

RIGHT HORIZONTAL STABILIZER RIB AT 166.3 THIRD VERTICAL STIFFENER FROM LE CRACKED NEAR LOWER END. REPAIRED RIB IAW ER & EA.

Part: POST — CRACKED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

LEFT NR 3 WINDOW FRAME E - F POST 2ND FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED POST EO.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

AFT CARGO COMPARTMENT FLOOR SPLICE STRAP CORRODED AT BS 887, BETWEEN RBL 20 TO LBL 20. R & R SPLICE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

FORWARD SEAT TRACK HOLES COMMON TO SPLICE STRAP CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW ER & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 26,708 hrs · 11,613 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL CLOSE OUT WEB CORRODED BETWEEN BS 767 TO 794 RBL 20. R & R WEB IAW DWG & SRM.