N559WN

Part: SLIDE — UNPACKED (ZN 800 DOOR) · airframe 57,246 hrs · 39,107 cycles

FORWARD RIGHTHAND SERVICE DOOR SLIDE POPPED OUT OF HOUSING.<[01] REMOVED SLIDE FROM RH SERVICE DOOR FWD AND REINSTALLED SLIDE IN HOUSING COVER; AND INSTALLED SLIDE ASSAY TO RH SERVICE FWD DOOR. OPTS CHECK GOOD OF DOOR REF AMM 25-66-01.

Part: SLIDE — OUT OF POSITION (ZN 200 FUS TOP) · airframe 56,516 hrs · 38,667 cycles

GIRT BAR ON PASSENGER DOOR IS DIFICULT TO ARM/DISARM<[01] REPOSITIONED AND REATTACHED Z-FOLD REF MT 725-61-06

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 56,287 hrs · 38,531 cycles

FORWARD ENTRY DOOR GIRT BAR LOOSE AND WILL NOT STAY IN FITTING<[01] FOUND RIVET ON SLIDE BRACKET SHEARED OFF. REMOVED AND REPLACED RIVET IAW AMM 51-40-02.

Part: SLIDE — LOW PRESSURE (ZN 200 FUS TOP) · airframe 56,161 hrs · 38,458 cycles

FWD MAIN CABIN DOOR ESCAPE SLIDE PRESSURE INDICATOR NOT IN THE GREEN RANGE<[01] REMOVED AND REPLACED FORWARD ENTRY DOOR ESCAPE SLIDE PER MT 725-61-06-FE.

Part: BRACKET — BROKEN (ZONE 100) · airframe 54,788 hrs · 37,645 cycles

PANEL 192 E L/H FWD HANGER BRACKET BROKE OFF . REMOVED AND REPLACED L/H FWD HANGER BRACKET FOR PANEL 192E IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (SERVICE DOOR) · airframe 54,430 hrs · 37,423 cycles

RH SUPPORT BRACKET CRACKED ON PANEL 844DZ; AFT RH GALLEY SERVICE DOOR. REMOVED AND REPLACED AFT SUPPORT BRACKET AND FASTENERS ON PANEL 844DZ IAW SRM 51-40-02.

Part: SLIDE — OUT OF POSITION (AFT SERVICE DOOR) · airframe 54,090 hrs · 37,194 cycles

AFT SERVICE DOOR SLIDE SKIRT HANGOUT TO MUCH / [01] SECURED SKIRT TO HOUSING PER SIP

Part: COVER — LOOSE (CABIN) · airframe 54,065 hrs · 37,180 cycles

EMERGENCY EXIT LIGHT COVER BY FORWARD FA JUMP SEAT CAME OFF / [01] REINSTALLED EMERGENCY EXIT LIGHT COVER LOCATED AT FWD L/H DOOR AREA PER AMM 33-51-00 OP CHECK OK

Part: PANEL — OVERHEATED (COCKPIT) · airframe 53,980 hrs · 37,116 cycles

COCKPIT VOICE RECORDER MICROPHONE OVERHEATED & MELTED. PULLED CVR CIRCUIT BREAKER ON PANEL P-18-2. NO SMELL NOTED / [01] R&R CVR MICROPHONE MONITOR PANEL AS PER AMM 23-71-12. OPS CHECK GOOD. PERFORMED CONDITIONAL INSP PER AMM 05-51-56; NO SMOKE OR FUMES NOTED IN CONTROL CABIN.

Part: SUPPORT — CRACKED (FWD CARGO) · airframe 53,973 hrs · 37,112 cycles

CRACK CLAMP SUPPORT ON VERTICAL ANGLE LOC STA 500C LBL 25 AT FWD CARGO COMPARTMENT 2022-447795 / [01] REPLACED CLAMP SUPPORT ON VERTICAL ANGLE LOC STA 500C LBL 25 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 STEP 9;[02] TASK COMPLETED

Part: WEB — CRACKED (FWD CARGO) · airframe 53,973 hrs · 37,112 cycles

CRACK WEB LOC BTW BS 400 TO 420 AND STR 25R AT FWD CARGO COMPARTMENT 2022-447782 / [01] REPLACED NEW WEB LOC. BTW BS 400 TO 420 AND STR 25R AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; DWG 143A7505 SHEET 2 REV B.;[02] CORRECTED STEP 1: REPLACED WEB LOC. BTW BS 400 TO 420 AND STR 25R AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; DWG 143A7505 SHEET 2 REV B; SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 1: REPLACED WEB LOC. BTW BS 400 TO 420 AND STR 25R AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; DWG 143A7505 SHEET 2 REV B; SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT — BROKEN (FUSELAGE) · airframe 53,973 hrs · 37,112 cycles

BROKEN MODULATION PANEL RAM AIR INLET LINK SUPPORT LOWER POSITION ON RH SIDE AT AIR CONDITIONING BAY 2022-447729 / [01] REPLACED MODULATION PANEL RAM AIR INLET LINK SUPPORT LOWER POSITION ON RH SIDE AT AIR CONDITIONING BAY IAW B737-700 SRM:51-40-02;[02] REPLACED MODULATION PANEL RAM AIR INLET LINK SUPPORT LOWER POSITION ON RH SIDE AT AIR CONDITIONING BAY IAW B737-700 SRM:51-40-02. VERIFIED

Part: SUPPORT ANGLE — CRACKED (AFT CARGO) · airframe 53,973 hrs · 37,112 cycles

CRACK SUPPORT ANGLE LOCATE BTW BS 907 TO BS 927 AND STR 26R AFT CARGO COMPARTMENT 2022-447726 / [01] REPLACED SUPPORT ANGLE LOCATE BTW BS 907 TO BS 927 AND STR 26R AFT CARGO COMPARTMENTIAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DWG 147A7221 SHEET 17 REV D. SEE INDIVIDUAL SIGNSOFF BELOW.;[02] REPLACED SUPPORT ANGLE LOCATE BTW BS 907 TO BS 927 AND STR 26R AFT CARGO COMPARTMENTIAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DWG 147A7221 SHEET 17 REV D. SEE INDIVIDUAL SIGNSOFF BELOW.<BR><BR>RII ACCOMPLISHED

Part: SUPPORT ANGLE — CRACKED (AFT CARGO) · airframe 53,973 hrs · 37,112 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS 867 AND STR 25L AFT CARGO COMPARTMENT 2022-447727 / [01] REPLACED ANGLE-SUPPORT LOCATED ON BS 867 AND STR 25L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9. SRM 51-40-02 AND DWG #149A8102 SHEET 15 REV A.;[02] CORRECTED STEP 1 REPLACED ANGLE-SUPPORT LOCATED ON BS 867 AND STR 25L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9. SRM 51-40-02 AND DWG #149A8102 SHEET 15 REV A. SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 1 REPLACED ANGLE-SUPPORT LOCATED ON BS 867 AND STR 25L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9. SRM 51-40-02 AND DWG #149A8102 SHEET 15 REV A. SEE INDIVIDUAL SIGN OFF BELOW

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,973 hrs · 37,112 cycles

CRACK STRINGER 23L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2022-447706 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN:60009161631; DUE DATE: 03-DEC-22;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23;[03] REPAIRED STRINGER 23L LOC. BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A. NOT FURTHER ACTION OR REINSPECTION REQUIERED. SEE INDIVIDUAL SING OFF BELOW.;[04] REPAIRED STRINGER 23L LOC. BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A. NOT FURTHER ACTION OR REINSPECTION REQUIERED. SEE INDIVIDUAL SING OFF BELOW.<BR>CERTIFIED AS RII

Part: PANEL — BROKEN (R1 DOOR) · airframe 53,973 hrs · 37,112 cycles

BROKEN SERVICE DOOR COVER EXIT HEADER PANEL AT FWD GALLEY AREA (1 EA) 2022-447692 / [01] REPLACED SERVICE DOOR COVER EXIT HEADER PANEL AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 2 C (1)(A) AND (3);[02] CORRECTED STEP 1<BR>REPLACED SERVICE DOOR COVER EXIT HEADER PANEL AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 2 C (1)(A) AND (4).;[03] REPLACED SERVICE DOOR COVER EXIT HEADER PANEL AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 2 C (1)(A) AND (4). COMPLETED

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,973 hrs · 37,112 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2022-447648 / [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] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM:9 AND DWG:273A9110 SHEET:3 REV:- SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM:9 AND DWG:273A9110 SHEET:3 REV:-; RII. SEE INDIVIDUAL SIGN OFF BELOW.

Part: NONE — CRACKED (FUSELAGE) · airframe 53,973 hrs · 37,112 cycles

CRACK INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED BS 540 BTW LBL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN 2022-447650 / [01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BS 540 BTW LBL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND 51-40-02 DWG 143A0060 PARTS USED: 143A5240 -35;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BS 540 BTW LBL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND 51-40-02 DWG 143A0060 PARTS USED: 143A5240 -35 RII

Part: NONE — CRACKED (FUSELAGE) · airframe 53,973 hrs · 37,112 cycles

CRACK INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED BS 540 BTW RBL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN 2022-447651 / [01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BS 540 BTW RBL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND 51-40-02 DWG 143A0060 PARTS USED: 143A5240 -36;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BS 540 BTW RBL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND 51-40-02 DWG 143A0060 PARTS USED: 143A5240 -36 RII

Part: SUPPORT ANGLE — CRACKED (R/H HORIZ. STAB.) · airframe 53,973 hrs · 37,112 cycles

CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.750 INCH 2022-447673 / [01] TOOL USED EDDY CURRENT PN/ NORTEC 600D; SN/ 210138003; DUE DATE/ 22-FEB-23.;[02] REPAIRED RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN BTW STAB STA 184.70 AND STAB STA 203.10 I.A.W B737-700 SRM 55-10-01-2R-11 REPAIR 11 FIGURE 204 SHEET 2 DETAIL:B AND SRM 51-40-02.THIS REPAIR IS CATEGORY B. SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPAIRED RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN BTW STAB STA 184.70 AND STAB STA 203.10 I.A.W B737-700 SRM 55-10-01-2R-11 REPAIR 11 FIGURE 204 SHEET 2 DETAIL:B AND SRM 51-40-02.THIS REPAIR IS CATEGORY B. SEE INDIVIDUAL SIGNOFF BELOW. RII

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 53,973 hrs · 37,112 cycles

CRACK FWD CORNER SCUFF PLATE FWD CARGO COMPARTMENT 2022-447626 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 29/SEP/22.;[02] REPAIRED FWD CORNER SCUFF PLATE FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFF BELOW.;[03] STEP 2 VERIFIED AND CORRECTIVE ACTION COMPLETED : REPAIRED FWD CORNER SCUFF PLATE FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFF BELOW.

Part: ANGLE — CRACKED (L/H WING) · airframe 53,973 hrs · 37,112 cycles

CRACK TRAILING EDGE SUPPORT ANGLE LOCATED DEFLECTION CONTROL RIB AREA; ORSS 261 PLUS 10 INCHES; LT WING 2022-447296 / [01] REPLACED SUPPORT ANGLE LOCATED DEFLECTION CONTROL RIB AREA; ORSS 261 PLUS 10 INCHES; LT WING. IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 STEP 9. TOOL USED: CALIPER P/N 700-113-10; S/N: 0023203 DUE DATE: 01/FEB/23.;[02] CERTIFIED WORK PERFORMED.

Part: SUPPORT ANGLE — CRACKED (R/H WING) · airframe 53,973 hrs · 37,112 cycles

CRACK TRAILING EDGE SUPPORT ANGLE LOCATED ON DEFLECTION CONTROL RIB AREA; ORSS 261 PLUS 9INCHES AT RT WING 2022-447277 / [01] INSTALLED NEW SUPPORT ANGLE LOC. ON DEFLECTION CONTROL RIB AREA ORSS 261 PLUS 9INCHES AT RT WING; IAW B737-700 SRM 51-10-02 ITEM 9;[02] TASK COMPLETED

Part: NONE — WORN (R/H WING) · airframe 53,973 hrs · 37,112 cycles

WEAR ON FLAP TRACK 6 LOWER TRACK FLANGE ROLLER CONTAC INBOARD AT RT WING 2022-447262 / [01] REPAIRED FLAP TRACK 6 LOWER TRACK FLANGE ROLLER CONTAC INBOARD AT RT WING IAW B737-700 SRM 57-53-02-2R-10 REPAIR 10 PARAGRAPH 4;PERFORMED FLUORESCENT PENETRANT INSPECTION AND NOT CRACK INDICATION ; THIS REPAIR IS CATEGORY A WITH DEEPEST POINT OF 0.009?; NO FURTHER ACTION OR REINSPECTION REQUIRED; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPAIRED FLAP TRACK 6 LOWER TRACK FLANGE ROLLER CONTAC INBOARD AT RT WING IAW B737-700 SRM 57-53-02-2R-10 REPAIR 10 PARAGRAPH 4;PERFORMED FLUORESCENT PENETRANT INSPECTION AND NOT CRACK INDICATION ; THIS REPAIR IS CATEGORY A WITH DEEPEST POINT OF 0.009?; NO FURTHER ACTION OR REINSPECTION REQUIRED; SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 53,973 hrs · 37,112 cycles

CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB BTW RBL 39 TO RBL 50 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROXIMATELY: 0.312 INCH. 2022-447263 / [01] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 200048001 AND DUE DATE: 30-MAR-23.;[02] TOOL USED EDDY CURRENT P/N: NORTEC 500D; S/N: N500X12101V022237; DUE DATE: 06-OCT-22.;[03] REPAIRED HORIZONTAL PRESSURE DECK WEB BTW RBL 39 TO RBL 50 STA 663 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND B737-700 SRM 53-40-51-2R-2 REPAIR 2 SEE INDIVIDUAL SING OFFS BELOW.;[04] REPAIRED HORIZONTAL PRESSURE DECK WEB BTW RBL 39 TO RBL 50 STA 663 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND B737-700 SRM 53-40-51-2R-2 REPAIR 2 SEE INDIVIDUAL SING OFFS BELOW.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 53,973 hrs · 37,112 cycles

CRACK AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2022-447202 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 29/SEP/22.;[02] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.;[03] JOB COMPLETED

Part: ANGLE — CRACKED (L/H WING) · airframe 53,973 hrs · 37,112 cycles

CRACK TRAILING EDGE SUPPORT ANGLE LOCATED ORSS 261 PLUS 8INCHES; AT DEFLECTION CONTROL RIB AREA AT LT WING 2022-447294 / [01] REPLACED SUPPORT ANGLE LOC ORSS 261 PLUS 8INCHES; AT DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02 P/N: 115A2992-9; PO: 2022 142158 AND SRM 51-10-02 STEP 9. TOOL USED: CALIPER P/N: 700-113-10; S/N: 0023203 DUE DATE: 01/FEB/23;[02] CORRECTION STEP 1: REPLACED SUPPORT ANGLE LOC ORSS 261 PLUS 8INCHES; AT DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02 P/N: 115A2982-9; PO: 2022 142158 AND SRM 51-10-02 STEP 9. TOOL USED: CALIPER P/N: 700-113-10; S/N: 0023203 DUE DATE: 01/FEB/23;[03] CERTIFIED STEP 2 COMPLETE <BR>IAW B737-700 SRM 51-40-02

Part: NONE — BROKEN (CABIN) · airframe 53,973 hrs · 37,112 cycles

BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8 EA) 2022-447218 / [01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8 EA) IAW SOPM 20-50-12;[02] TASK CARD COMPLTED

Part: BRACKET — CRACKED (L/H WING) · airframe 53,973 hrs · 37,112 cycles

CRACK TRAILILNG EDGE BRACKET LOCATED ORSS 261 PLUS 19 INCHES; DEFLECTION CONTROL RIB AND SUPPORT BEAM AREA AT LT WING 2022-447298 / [01] REPLACED NEW BRACKET AND FASTENERS LOC. ORSS 261 PLUS 19?; DEFLECTION CONTROL RIB AND SUPPORT BEAM AREA AT LT WING B737-700 SRM 51-40-02 AND SRM 51-10-02 STEP 9 TOOL USED: CALIPER P/N 700-113-10; S/N: 0023203 DUE DATE: 01/FEB/23.;[02] TASK COMPLETED

Part: FLAP TRACK — WORN (L/H WING) · airframe 53,973 hrs · 37,112 cycles

WEAR ON FLAP TRACK 3 UPPER AND LOWER TRACK FLANGE ROLLER CONTAC INBOARD AT LT WING 2022-447246 / [01] REPAIRED FLAP TRACK 3 UPPER AND LOWER TRACK FLANGE ROLLER CONTAC INBOARD AT LT WING IAW B737-700 SRM 57-53-02-2R-10 REPAIR 10 PARAGRAPH 4;PERFORMED FLUORESCENT PENETRANT INSPECTION; THIS REPAIR IS CATEGORY A; NO FURTHER ACTION OR REINSPECTION REQUIRED; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTED STEP 1:<BR>REPAIRED FLAP TRACK 3 UPPER AND LOWER TRACK FLANGE ROLLER CONTAC INBOARD AT LT WING IAW B737-700 SRM 57-53-02-2R-10 REPAIR 10 PARAGRAPH 4;PERFORMED FLUORESCENT PENETRANT INSPECTION AND NOT CRACK INDICATION ; THIS REPAIR IS CATEGORY A WITH DEEPEST POINT OF 0.008?; NO FURTHER ACTION OR REINSPECTION REQUIRED; SEE INDIVIDUAL SIGN OFFS BELOW.;[03] CORRECTED STEP 1: <BR>REPAIRED FLAP TRACK 3 UPPER AND LOWER TRACK FLANGE ROLLER CONTAC INBOARD AT LT WING IAW B737-700 SRM 57-53-02-2R-10 REPAIR 10 PARAGRAPH 4;PERFORMED FLUORESCENT PENETRANT INSPECTION AND NOT CRACK INDICATION ; THIS REPAIR IS CATEGORY A WITH DEEPEST POINT OF 0.008?; NO FURTHER ACTION OR REINSPECTION REQUIRED; SEE INDIVIDUAL SIGN OFFS BELOW.

Part: NONE — CRACKED (FUSELAGE) · airframe 53,973 hrs · 37,112 cycles

CRACK EXTERNAL GROUND ELECTRICAL POWER LOC FWD LOWER CUTOUT AT LOWER FUSELAGE 2022-447082 / [01] TOOL USED CALIPER P/N: 500-197-30; S/N: A21143439; DUE DATE: 11-OCT-22.;[02] ET TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 07-JUL-23;[03] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 210138003 AND DUE DATE: 22-FEB-23.;[04] REPAIRED EXTERNAL GROUND ELECTRICAL POWER LOC FWD LOWER CUTOUT AT LOWER FUSELAGE IAW EA NÏ¿½22-153-02677-WIP1 REV1. THIS REPAIR IS CLASSIFIED AS MINOR AND DEFINED AS CATEGORY A. SEE INDIVIDUAL SIGN OFF BELOW;[05] REPAIRED EXTERNAL GROUND ELECTRICAL POWER LOC FWD LOWER CUTOUT AT LOWER FUSELAGE IAW EA NÏ¿½22-153-02677-WIP1 REV1. THIS REPAIR IS CLASSIFIED AS MINOR AND DEFINED AS CATEGORY A. SEE INDIVIDUAL SIGN OFF BELOW. COMPLETED RII

Part: SLIDE — OUT OF TOLERANCE (L1 DOOR) · airframe 53,539 hrs · 36,846 cycles

FWD ENTRY DOOR SLIDE OVER-PRESSURIZED / [01] REMOVED AND REPLACED SLIDE PER MT 725-61-06

Part: GIRT BAR — OUT OF POSITION (FWD ENTRY DOOR) · airframe 53,482 hrs · 36,808 cycles

FWD ENTRY DOOR; EVAC SLIDE NEEDS TO BE REPOSITIONED; AS REPORTED BY CREW. / [01] REPOSITIONED GIRT BAR ONLY AND PERFORMED INSTALLATION TEST PER A.M.M. 25-66-02-210-002.

Part: PUMP — LEAKING (NR 2 EDP) · airframe 49,706 hrs · 34,625 cycles

ENG 2 B HYD PUMP LOW PRESSURE LIGHT ON. B HYDRAULIC QTY READS ZERO. B HYDRAULIC PRESSURE READS 3000. NO OTHER LIGHTS ON. UPON FLAP LEVER TO 5, B SYSTEM WENT TO 0 AND FLUCTUATED UP TO 1000 PSI. FLAPS STOPPED MOVING AT LESS THAN ONE. FOLLOWED LOSS OF B HYDRAULIC SYSTEM CHECKLIST. FLAPS EXTENDED TO 15 USING ALTERNATE SYSTEM. / TROUBLESHOOT #2 ENG B HYD PUMP FOUND EDP LEAKING FROM PRESSURE LINE FITTING AND SYSTEM B EDP CASE DRAIN FILTER ELEMENT HAD DEBRIS SO 1 R/R #2 EDP PER AMM 29-11-11 OPS/LEAK CK GOOD ALSO PERFORMED HYD SYSTEM A OR B FLUSHING PER AMM 29-11-00 ON SYSTEM B OPS/LEAK CK GOOD RAR # 92167 P/N OFF/ON 849589 S/N OFF MX597199 S/N ON MX718526

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,806 hrs · 34,131 cycles

CRACK INSPAR RIB ON STIFFENER LOCATED STA 120.30 FRONT SPAR AT LT HORIZONTAL STABILIZER. REPLACED STIFFENER LOCATED STA 120.30 FRONT SPAR AT LT HORIZONTAL STABILIZER, IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DRAWING 182A5304 REV C.

Part: STRINGER — CRACKED (BS 540) · airframe 48,806 hrs · 34,131 cycles

CRACK STRINGER 26R BS540 FWD CARGO COMPARTMENT. PERFORMED REPAIR STRINGER 26R BS540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. THIS REPAIR IS A CATEGORY A, NO FURTHER ACTION OR INSPECTION REQUIRED.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 48,806 hrs · 34,131 cycles

CRACK LAVATORY A LENS EMERGENCY LIGHT AT FWD GALLEY AREA. REPLACED LAVATORY A LENS EMERGENCY LIGHT AT FWD GALLEY AREA, IAW B737-700 AMM 33-51-01-960-801 STEP 2B ITEM (4).

Part: SHEAR TIE — CRACKED (BS 277) · airframe 48,806 hrs · 34,131 cycles

CRACK TIE CLIP LOCATED BS277 AT STR 10R AT PASSENGER CABIN. REPLACED TIE CLIP LOC BS 277 AT STR 10R AT PASSENGER CABIN, IAW B737-700 SRM 51-10-02 AND DWG 141A1110 REV.

Part: STRINGER — CRACKED (BS 540) · airframe 48,806 hrs · 34,131 cycles

CRACK STRINGER 25R BS540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 25R BS540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. THIS REPAIR IS CATEGORY A, FURTHER INSPECTION IS NOT REQUIRED.

Part: STRINGER — CRACKED (BS 540) · airframe 48,806 hrs · 34,131 cycles

CRACK BS 540 STRINGER 26L AT FWD CARGO COMPARTMENT. REPAIRED STRINGER 26L BS500D AND BS540 AT FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. THIS REPAIR IS CATEGORY A, FURTHER INSPECTION IS NOT REQUIRED.

Part: WEB — CRACKED (BS 294-303) · airframe 48,806 hrs · 34,131 cycles

CRACK WEB LOCATED BETWEEN BS 294.5 TO BS 303.9 STRINGER 16L AT FWD GALLEY AREA. REPLACED WEB LOC BETWEEN BS 294.5 TO BS 303.9 STRINGER 16L AT FWD GALLEY AREA, IAW B737-700 SRM 51-10-02-0G-0 AND B737-700 SRM 51-40-02-0G-0 AND DWG 141A8180 SHEET 27 REV C.

Part: SUPPORT ANGLE — CORRODED (BS 727B-767) · airframe 48,806 hrs · 34,131 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS727B TO BS767; RBL19 AND WL154.5 AFT CARGO COMPARTMENT / REPLACED SUPPORT ZEE LOCATED BETWEEN BS727B TO BS767 RBL 19 AND WL 154.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DRAWING #146A7500 REV

Part: SUPPORT — CORRODED (BS 727B-807) · airframe 48,806 hrs · 34,131 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727B TO BS 807 LBL 19 AND WL 154 .5 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOC BETWEEN BS 727B TO 847 LBL 19 AND WL 154.5 AFT CARGO COMPARTMENT, IAW B737-700 SRM 51-10-02 PAR 9 DWG 146A7500 REV 0 AND REPAIRED IAW B737- 700 SRM 53-00-53-2R-6 REP 6 (SPLICE REPAIR).

Part: FRAME — CRACKED (BS 294) · airframe 48,806 hrs · 34,131 cycles

CRACK FRAME STUB BS 294.5 AT LEVEL STR 17R AT PASSENGER CABIN. REPLACED FRAME STUB BS 294.5 BETWEEN STR 15R TO STR 17R AT PASSENGER CABIN, IAW SRM B737- 700 51-10-02 AND 51-40-02 DWG NR 141A8371 REV A 141A8430 REV A AND 141A8370 REV C.

Part: STRAP — CORRODED (BS 767-787) · airframe 48,806 hrs · 34,131 cycles

CORROSION STRAP LOCATED BETWEEN BS767 TO BS787; RBL19 TO LBL19 AND WL154.5 AFT CARGO COMPARTMENT (1 EA) / REPLACED STRAP LOCATED BETWEEN BS 767 TO BS 787 RBL 19 TO LBL 19 AND WL 154.5 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 146A7500 REV.- SHEET 61

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 48,806 hrs · 34,131 cycles

DENTS ON INBOARD MAIN FLAP UPPER SURFACE, DENTED AREA NR 1 IS LOC AT 3' FROM OUTBOARD EDGE AND 3.25' FROM T/E, AND DENTED AREA NR 2 IS LOC AT 17' FROM OUTBOARD EDGE AND 9.25' FROM T/E AT LT WING (REFER TO DEFECT T328194). REPAIRED INBOARD MAIN FLAP UPPER SURFACE, AS PER B737-700 SRM 57-53-01-2R-7 REPAIR 7. TOOL USED DENT GAUGE PN PG KIT PREMIUM SN 012029 DUE DATE 20 APR 21; HOT BONDER PN HCS8800 SN 01112550 DUE DATE 24DEC20; HOT BONDER PN HCS9200B SN 18185781 DUE DATE 25OCT20; POSITECTOR PN N52 SN 138341 DUE DATE 27MAY21; PN GEIT1480179 SN G0PLS15100158 DUE DATE 020-JUN-21.

Part: NUT PLATE — BROKEN (RADOME) · airframe 48,806 hrs · 34,131 cycles

BROKEN EXTERNAL RADOME NUT PLATE LOC. BTW BS 727B TO BS 727C AND STR 1 TO STR 2L AT UPPER FUSELAGE (1 EA) / REPLACED NUT PLATE LOC ON EXTERNAL RADOME BTW BS 727B TO BS 727C AND STR 1 TO STR 2L AT UPPER FUSELAGE(1EA)B737-700 SRM 51-10-02 ITEM 9 51-40-02 AND DWG DG234-7025 -00 REV.F

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 48,806 hrs · 34,131 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT / REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975

Part: PLATE — WORN (L2 DOOR GIRT BAR) · airframe 48,806 hrs · 34,131 cycles

WEAR ON GIRT BAR FITTING ADAPTER PLATE AND HARWARD AFT SERVICE AND AFT ENTRY DOOR (4EA) AT AFT GALLEY AREA (4 EA). REPLACED ON GIRT BAR FITTING ADAPTER PLATE AND HARWARD AFT SERVICE AND AFT ENTRY DOOR (4EA) AT AFT GALLEY AREA (4EA), IAW SRM 51-40-03-06-0 AND INSTALLATION WILL BE DOCUMENTED ON WORK INSTRUCTION NR 725-025-00-02T.

Part: PLATE — WORN (R2 DOOR GIRT BAR) · airframe 48,806 hrs · 34,131 cycles

WEAR ON GIRT BAR FITTING ADAPTER PLATE AND HARWARD AFT SERVICE AND AFT ENTRY DOOR (4EA) AT AFT GALLEY AREA (4 EA). REPLACED ON GIRT BAR FITTING ADAPTER PLATE AND HARWARD AFT SERVICE AND AFT ENTRY DOOR (4EA) AT AFT GALLEY AREA (4EA), IAW SRM 51-40-03-06-0 AND INSTALLATION WILL BE DOCUMENTED ON WORK INSTRUCTION NR 725-025-00-02T.

Part: SUPPORT ANGLE — CRACKED (BS 500C) · airframe 48,806 hrs · 34,131 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS500C FWD AND AFT FACE AND STR26R FWD CARGO COMPARTMENT / REPLACED ANGLES-SUPPORTS LOCATED BETWEEN BS500C FWD AND AFT FACE AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 REV

Part: SUPPORT ANGLE — CRACKED (BS 500A) · airframe 48,806 hrs · 34,131 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS500A FWD FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE-SUPPORT AND FASTENERS LOCATED BETWEEN BS500A FWD FACE AND STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG N.143A7505 SHEET 37 REV

Part: SUPPORT ANGLE — CRACKED (BS 500B S26L) · airframe 48,806 hrs · 34,131 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS500B FWD FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT LOC. BTW BS500 B FWD FACE AND STR 26L FWD CARGO COMPART. I.A.W SRM B737-700 51-40-02 AND DWG #143A7505 REV. B AND 51-10-02 ITEM 9

Part: SUPPORT ANGLE — CRACKED (BS 500C S26L) · airframe 48,806 hrs · 34,131 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS500C FWD AND AFT FACE AND STR26L FWD CARGO COMPARTMENT (2EA) / REPLACED ANGLE-SUPPORT LOC. BTW BS500C FWD CARGO COMPARTMENT AND STR 26L (2EA) IAW SRM B737-700 51-40-02 AND DWG #143A7505 REV B AND 51-10-02 ITEM 9

Part: GUSSET — CRACKED (BS 500D S21L) · airframe 48,806 hrs · 34,131 cycles

CRACK GUSSET LOCATED BETWEEN BS500D AND STR21L FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED BETWEEN BS500D AND SRR21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 174 REV

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 48,806 hrs · 34,131 cycles

CRACK GUSSET LOCATED BETWEEN BS500D AND STR19L FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED BETWEEN BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 174 REV

Part: SUPPORT ANGLE — CRACKED (BS 400 S26L) · airframe 48,806 hrs · 34,131 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS400 AFT FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE-SUPPORT LOCATED BETWEEN BS400 AFT FACE AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 DWG 143A7505 SHEET 2 REV B

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 48,806 hrs · 34,131 cycles

CRACK GUSSET LOCATED BETWEEN BS500D AND STR19R FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED BETWEEN BS500D AND STR14R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; AND DWG 143A7902 SHEET 174; REV

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,806 hrs · 34,131 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR LT HORIZONTAL STAB, IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG 202.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,806 hrs · 34,131 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. REPAIRED INSPAR RIB LOC STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER, IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. THIS REPAIR IS CATEGORY A, REINSPECTION IS NOT REQUIRED.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,806 hrs · 34,131 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FRONT SPAR LT HORIZONTAL STAB, IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG 202.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,806 hrs · 34,131 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. REPAIRED INSPAR RIB LOC STAB STA 120.30 AT RT HORIZONTAL STABILIZER, IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. THIS REPAIR IS CATEGORY A. RE INSPECTION IS NOT REQUIRED.

Part: TAB — PEELING (R/H HORIZ. STAB) · airframe 48,806 hrs · 34,131 cycles

PEELED PAINT ON ELEVATOR TAB AT RT HORIZONTAL STABILIZER. REPAINTED ELEVATOR TAB AT RT HORIZONTAL STABILIZER, IAW B737-700 AMM 51-21-73-370-803. PERFORMED WEIGHT AND BALANCE ON ELEVATOR TAB RT, IAW SRM 51-61-06-06-0.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,806 hrs · 34,131 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. REPAIRED INSPAR RIB LOC STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER, IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. THIS REPAIR IS CATEGORY A, REINSPECTION IS NOT REQUIRED.

Part: TAB — PEELING (HORIZ. STAB) · airframe 48,806 hrs · 34,131 cycles

PEELED PAINT ON ELEVATOR TAB AT LT HORIZONTAL STABILIZER. REPAINTED ELEVATOR TAB AT LT HORIZONTAL STABILIZER, IAW B737-700 AMM 51-21-73-370-803. PERFORMED WEIGHT AND BALANCE CHECK ON ELEVATOR TAB LT, IAW B737-700 SRM 51-61-06-06-0.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,806 hrs · 34,131 cycles

CRACK INSPAR RIB LOCATED STAB STA 92.70 AT 40 INCH FROM FRONT SPAR LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 92.70 AT 40 INCH FROM FRONT SPAR LT HORIZONTAL STAB, IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG 202.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,806 hrs · 34,131 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR LT HORIZONTAL STAB, IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG 202.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 48,806 hrs · 34,131 cycles

CRACK PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT AT PASSENGER CABIN, 5EA. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT AT PASSENGER CABIN 5 EA, IAW MT CARD 753-400-00-01Y.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 48,806 hrs · 34,131 cycles

CRACK PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT AT PASSENGER CABIN, 5 EA. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTNG LT AT PASSENGER CABIN 5 EA, IAW MT CARD 753-400- 00-01Y.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,543 hrs · 33,974 cycles

NR 2 LEFT EMERGENCY CABIN INTERIOR LIGHT WAS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-03.

Part: TRUNNION — OUT OF TOLERANCE (LT MLG) · airframe 48,509 hrs · 33,954 cycles

L/H MLG FWD TRUNNION FITTING ;UPPER O/B LUG BORE DIAMETER IS BEYOND NOMINAL DIMENSIONS 1.5602-1.5610 / ACCOMPLISHED E.A 1-A57-3246 ON UPPER OUTBD TRUNNION FITTING LUG. REF D&M ENTERPRISES W.O.#SSR1227

Part: TRUNNION — OUT OF TOLERANCE (LT MLG) · airframe 48,509 hrs · 33,954 cycles

:L/H MLG FWD TRUNNION FITTING ;LOWER I/B LUG BORE DIAMETER IS BEYOND NOMINAL DIMENSIONS 1.5602-1.5610 / ACCOMPLISHED E.A 1-A57-3246 ON LOWER INBD TRUNNION FITTING LUG. REF D&M ENTERPRISES W.O.#SSR1227

Part: TRUNNION — OUT OF TOLERANCE (LT MLG) · airframe 48,509 hrs · 33,954 cycles

:L/H MLG FWD TRUNNION FITTING ;LOWER O/B LUG BORE DIAMETER IS BEYOND NOMINAL DIMENSIONS 1.5602-1.5610 / ACCOMPLISHED E.A 1-A57-3246 ON LOWER OUTBD TRUNNION FITTING LUG. REF D&M ENTERPRISES W.O.#SSR1227

Part: TRUNNION — OUT OF TOLERANCE (LT MLG) · airframe 48,509 hrs · 33,954 cycles

:L/H MLG FWD TRUNNION FITTING ;UPPER I/B LUG BORE DIAMETER IS BEYOND NOMINAL DIMENSIONS 1.5602-1.5610 / ACCOMPLISHED E.A 1-A57-3246 ON UPPER INBD TRUNNION FITTING LUG. REF D&M ENTERPRISES W.O.#SSR1227

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,509 hrs · 33,954 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01669. R&R EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,392 hrs · 33,882 cycles

FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOP. BATTERY PACK ON M1675 INOP REMOVED & REPLACED BATTERY PACK REF AMM 33-51-06. OPS CHECK GOOD.

Part: CHARGER — FAULTY (CABIN) · airframe 47,658 hrs · 33,436 cycles

EMERGENCY LIGHTS POWERED BY M1674 (FORWARD RT BATTERY) ONLY CAME ON FOR A SECOND. R&R CHARGER ASSEMBLY IAW AMM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 47,658 hrs · 33,436 cycles

EMERGENCY LIGHTS POWERED BY M1674 (FORWARD RT BATTERY) ONLY COME ON FOR A SECOND. R&R BATTERY PACK IAW AMM.

Part: SUPPORT ANGLE — CRACKED (L/H WING) · airframe 47,008 hrs · 33,058 cycles

LEFT WING ANGLED WEB SUPPORT COMMON TO WING DEFLECTION RIB CRACKED / REMOVED AND REPLACED WEB SUPPORT ANGLE PER SRM 51-40-02 AND SRM 51-10-02

Part: FAN — FAILED (RECIRCULATION) · airframe 44,918 hrs · 31,795 cycles

STRONG ELECTRICAL BURNING ODOR NOTED ON CUMBOUT. RECIRC FAN OFF, PACKS HIGH SMELL DISAPPEARED. / RECIRC FAN INOP. R&R RECIRC FAN PER AMM.

Part: PIN — RUSTED (RT MLG TRUNNION) · airframe 44,683 hrs · 31,656 cycles

RT MLG FWD TRUNION FITTING PIN RUSTED. R&R PIN PER MM.

Part: PIN — RUSTED (LT MLG TRUNNION) · airframe 44,683 hrs · 31,656 cycles

LT MLG FWD TRUNION FITTING PIN RUSTED. R&R PIN PER MM.

Part: RETAINER — CORRODED (LT WHEEL WELL) · airframe 43,668 hrs · 31,046 cycles

***CORROSION*** LH MLG WHEEL WELL; AFT; OUTBOARD UPPER BLADE SEAL; RETAINER CORRODED ON LOWER SURFACE AT 2ND FASTENER FROM INBOARD END. MARKED. / REMOVED AND REPLACED RETAINER ITEM 7530584 PER SRM 51-40-02 88324U 10NOV18

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,668 hrs · 31,046 cycles

LT EMERGENCY LIGHTS INOP. REPAIRED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,668 hrs · 31,046 cycles

RT EMERGENCY LIGHTS INOP. REPAIRED LIGHT PER AMM.

Part: FAIRING — DAMAGED · airframe 43,668 hrs · 31,046 cycles

SUPPLEMENTAL INFORMATION: FAIRING 193AL I/B EDGE IS CHAFED AND MULTIPLE OVERSIZED HOLES. (MARKED) / FAIRING 193AL I/B EDGE WITH CHAFING AND MULTIPLE; OVERSIZED HOLES AS MARKED WAS REPAIRED PER SWA EA# 1-753-33559 REV IR DATED 07NOV2018 AND ATS ER# 18-05109 REV IR DATED 07-NOV-2018.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO DOOR SUB THRESHOLD WEB CORRODED. R&R WEB IAW DWG & SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AIR INTAKE AFT STIFFENER CORRODED AT ZONE 316, BS 1125. R&R STIFFENER IAW DWG AND SRM.

Part: CYLINDER — CORRODED (NLG WW) · airframe 43,668 hrs · 31,046 cycles

NOSE LANDING GEAR CORRODED OUTER CYLINDER AND STEERING COLLAR. R&R GEAR PER CCO.

Part: PLATE — CRACKED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

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

Part: PLATE — CRACKED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

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

Part: SCUFF PLATE — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

FORWARD CARGO BAY AFT OF DOOR SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE PER EA.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 43,668 hrs · 31,046 cycles

***CORROSION*** ON ACB PANEL 140CF ALONG OUTBOARD EDGES / FABRICATED NEW ACB FLOOR PANEL 140CF FROM .071 2024T3; LOT# 1358971-1 PER AMM 25-52-01-201-801 AND DWG 453A2610. NO ESTABLISHED LIMITS FOR CORROSION GIVEN IN SRM FOR THIS PART; DAMAGE IS OUT OF LIMITS. 2462C 10/29/18

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 43,668 hrs · 31,046 cycles

***CORROSION*** ON ACB R/H SIDEWALL CAP STRIPS FWD OF DOOR / CORROSION ON ACB R/H SIDEWALL CAP STRIP FWD OF DOOR FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. REMOVED AND REPLACED ACB R/H SIDEWALL CAP STRIPS FWD OF DOOR. IAW SRM 51-10-02-0G-0 PAR 9.C. REPAIRABLE BY REPLACEMENT

Part: RETAINER — CRACKED (LT WING) · airframe 43,668 hrs · 31,046 cycles

CANOE FAIRING 542BB O/B SIDE FWD SEAL RETAINER IS CRACKED / REPLACED CRACKED OB FWD SEAL RETAINER ON CANOE FAIRING 542BB IAW SRM 51-10-02-0G-0 PARA 9A; REMOVAL & INSTALLATION WAS ACCOMPLISHED ON CARD # T844735

Part: SPLICE — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY T-SPLICE CORRODED AT BS 767+4. R&R T-SPLICE IAW SRM AND DWG.

Part: BRACKET — CORRODED (MAIN CABIN) · airframe 43,668 hrs · 31,046 cycles

***CORROSION*** CORROSION AROUND DISCONNECT BRACKET AP0600A GROUND STUD BS 270-277 2' INBD OF STR 2L / CORROSION FOUND ON DISCONNECT BRACKETS WAS OUT OF LIMITS THEREFORE BRACKET WAS REMOVED AND REPLACED PER SRM. 51-40-02. AND DG #287A4106 86760U 24OCT18

Part: STRIP — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY LT SIDEWALL CAP STRIPS CORRODED FORWARD OF DOOR. R&R CAP STRIPS IAW SRM AND DWG.

Part: BRACKET — CORRODED (MAIN CABIN) · airframe 43,668 hrs · 31,046 cycles

***CORROSION*** AREAS OF CORROSION ON DISCONNECT BRACKET AP1800A BS 270-277 3' OTBD OF STR 1R / CORROSION FOUND ON DISCONNECT BRACKET WAS OUT OF LIMITS THEIRFORE BRACKET WAS REMOVED AND REPLACED PER SRM - 51-40-02 AND DG # 287A4106 86700U 24OCT18.

Part: SCUFF PLATE — BROKEN (AFT CARGO BAY) · airframe 43,668 hrs · 31,046 cycles

ACB AFT OF DOOR SCUFF PLATE BROKEN. / RECEIVED LOCATED AND DRILLED NEW ACB DOOR AFT SCUFF PLATE IAW DWG 146A8341; SRM 51-40-05; AND SRM 51-40-08 INSTALLED ACB AFT SCUFF PLATE IAW AMM 53-11-02-420-801

Part: SPLICE — CORRODED (AFT CARGO BAY) · airframe 43,668 hrs · 31,046 cycles

***CORROSION*** ON ACB T-SPLICE STA 727D+4' / REMOVED ACB T-SPLICE STA 727D+4 IAW AMM # 25-52-10-000-801. 57609U 16OCT18. LEAD113 16OCT18 RECEIVED AND INSTALLED ACB T SPLICE STA 727D+4 IAW AMM 25-52-10-400-801. 57609U 30OCT18 AND BOEING DRAWING #146A9401. 57609U 30OCT18.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY ON FLOOR SUPPORT CORRODED AT BS 927+16, RBL 14.5. R&R SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY ON INTERCOSTAL CORRODED AT BS 867+3, BETWEEN STR 26L TO STR 27L. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY FLOOR T-STRAP SUPPORT CORRODED AT BS 887. R&R SPLICE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY T-STRAP SUPPORT TIE CORRODED AT BS 887, LBL 10. R&R SUPPORT TIE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO BS 947. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

FLOOR TO BULKHEAD SUPPORT CORRODED AT BS 847+1, LBL 17. R&R SUPPORT IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY ON AFT BULKHEAD TO FLOOR SUPPORT CORRODED AT BS 947, LBL 4. R&R SUPPORT IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY BETWEEN STRINGER TO FRAME CLIP CORRODED AT BS 727D, STR 26L. R&R CLIP IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY BILGE INTERCOSTAL CORRODED AT BS 767+3, RBL 6.5. R&R INTERCOSTAL IAW DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

LT BULKHEAD TO SIDEWALL SUPPORT CORRODED AT BS 727, BETWEEN WL 198 TO WL 152. R&R SUPPORT IAW DWG & SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY ON KEELBEAM CORRODED AT BS 787+5.5, LBL 5. REPAIRED KEELBEAM IAW ER AND EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS 727D, STR 26R. R&R CLIP IAW DWG & SRM.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 43,668 hrs · 31,046 cycles

***CORROSION***ON ACB SHIELD STA 767 TO 787+6 RBL 23 FWD OF DOOR (MARKED ) / REMOVED AND REPLACED ACB SHIELD STA 767 TO 787+6 RBL 23 FWD OF DOOR IAW DWG 146A0081 AND SRM 51-40-02-0G-0 83802U 20OCT18

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY THRESHOLD SUPPORT CORRODED AT BS 787+7, RBL 18.5. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 787+13, LBL 22. R&R SUPPORT IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

INTERCOSTAL CRACKED AT BS 284, BL 0. R&R INTERCOSTAL PER DWG AND SRM.

Part: SUPPORT ANGLE — CORRODED (MAIN CABIN) · airframe 43,668 hrs · 31,046 cycles

***CORROSION*** IN MULTIPLE AREAS ON FWD ENTRY DOOR SUB THRESHOLD ANGLE SUPPORT STA 312 TO 344 LBL 58 / REMOVED CORROSION ON SUPPORT ANGLE IN A 23.0' LONG X 1' WIDE X 0.012' DEEP; ANGLE FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED FED ANGLE SUPPORT STA 312-344 LBL 58 IAW SRM 53-10-15-01-1; SRM 53-10-15-1A-1; SRM 51-40-05-0G-0; AND SRM 51-40-02-0G-0 84632U 15OCT18

Part: FITTING — CRACKED (FWD ENTRY DOOR () · airframe 43,668 hrs · 31,046 cycles

***CORROSION*** ON FWD ENTRY AFT HARD-POINT STA 344 LBL 54 WL 208 / REMOVED FWD ENTRY AFT HARD-POINT STA 344 LBL 54 WL 208 IAW SOPM 20-50-01. STRUCTURAL ITEM HAS NO APPLICABLE REPAIR PROCEDURES IN SRM. HARD-POINT IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9 83802U 11OCT18 LEAD 122 11OCT18 INSP 24 13OCT18 REPLACED FWD ENTRY AFT HARD-POINT BS 344 LBL 54 WL 208 PER REF B737 AMM 20-50-11-910-801 AND IPC 53-42-00-29. 92962U 13-OCT-18 LEAD 138 13OCT18

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R INTERCOSTAL PER DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

R1 DOOR SUB THRESHOLD ANGLE SUPPORT CORRODED BETWEEN BS 294 TO BS 328, RBL 57. R&R SUPPORT IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

FORWARD ENTRY FORWARD HARD-POINT CORRODED AT BS 312, LBL 52. R&R HARD-POINT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

FRAME CRACKED AT BS 727B, STR 1L. R&R FRAME IAW SRM.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 43,668 hrs · 31,046 cycles

FORWARD CARGO BAY FLOOR TIE DOWN CORRODED AT BS 500B, LBL 17. R&R TIE DOWN IAW MT.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500B TO BS 500, LBL 25. R&R SUPPORT IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (FWD SERVICE DOOR) · airframe 43,668 hrs · 31,046 cycles

FORWARD SERVICE DOOR SCUFF PLATE IS CRACKED / REMOVED THE SCUFF PLATE IAW AMM 53-11-01-000-801 88929U 30OCT18 89263C 30OCT18 OK TO INSTALL SCUFF PLATE AT FWD SERVICE DOOR 89763C 30OCT18 INSP12 30OCT18 INSTALLED FORWARD SERVICE DOOR SCUFF PLATE IAW AMM 53-11-01-420-801 88929U 30OCT18 REPAIRED FSD SCUFF PLATE PER EA 1-A53-2076 REV 11

Part: SHIELD — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 480+10 TO BS 500A. R&R SHIELD PER SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

FORWARD CARGO BAY SUB THRESHOLD CORRODED BETWEEN BS 440 TO BS 480+12. R&R THRESHOLD IAW DWG & SRM.

Part: COVER — BROKEN (CABIN) · airframe 43,668 hrs · 31,046 cycles

AFT ATTENDANTS PANEL EMERGENCY LIGHT SWITCH COVER BROKEN. R&R COVER PER SIP.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

FORWARD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT CORRODED AT BS 500D. R&R SUPPORT IAW SRM AND DWG.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 43,668 hrs · 31,046 cycles

FORWARD CARGO BAY FLOOR TIE DOWN CORRODED AT BS 500, LBL 17. R&R TIE DOWN PER SRM & DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 43,668 hrs · 31,046 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 34. REPAIRED WEB PER SRM.

Part: STRIP — CRACKED (LT WING) · airframe 43,668 hrs · 31,046 cycles

LT WING WIGGLE STRIP CRACKED AT ORSS 261. R&R WIGGLE STRIP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FAIRING) · airframe 43,668 hrs · 31,046 cycles

LT WING LEADING EDGE WING-TO-BODY FAIRING SUPPORT ANGLE CRACKED AT BS 500D, STR 19L. R&R ANGLE PER DWG AND SRM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 43,668 hrs · 31,046 cycles

R1 DOOR NR 4 (LOWER) BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE. REPAIRED DOOR PER AMM.

Part: SEAL — CRACKED (RT WING) · airframe 43,668 hrs · 31,046 cycles

RT WING TRANSITION WEB SEAL RETAINER CRACKED / REMOVED AND REPLACED RT WING TRANSITION WEB SEAL RETAINER IAW. AIPC 57-50-00-25. SRM 51-40-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

REAR SPAR BULKHEAD VAPOR BARRIER WEB VERTICAL STIFFENER CRACKED AT BS 663, LBL 28. R&R WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,668 hrs · 31,046 cycles

REAR SPAR BULKHEAD VAPOR BARRIER WEB CRACKED AT BS 663, LBL 38. REPAIRED WEB IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 43,668 hrs · 31,046 cycles

RT WING WIGGLE PLATE CRACKED AT ORSS 261. R&R WIGGLE PLATE IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,668 hrs · 31,046 cycles

RT WING NR 7 ACTUATOR LEADING EDGE SLAT SKIN CRACKED AROUND AFT FASTENER HOLE. REPAIRED SLAT SKIN IAW SRM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 43,668 hrs · 31,046 cycles

LT OVERWING EMERGENCY UPPER LIGHT LENS OUT OF POSITION. R&R LENS PER IPC AND SOPM.

Part: LENS — LOOSE (CABIN) · airframe 43,668 hrs · 31,046 cycles

LT EMERGENCY BIN LIGHT LENS LOOSE AT ROW 4. SECURED LENS PER AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,668 hrs · 31,046 cycles

RT WING NR 8 ACTUATOR LEADING EDGE SLAT SKIN CRACKED. REPAIRED SLAT SKIN IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 43,221 hrs · 30,778 cycles

RT AFT CABIN EMERGENCY EXIT LIGHT BATTERY FAILED TEST. R&R BATTERY PER MM.

Part: NONE — CRACKED (LT WING) · airframe 43,214 hrs · 30,774 cycles

SUPPLEMENTAL INFORMATION: AFT SPAR VERTICAL SEAL RETAINER IS CRACKED ABOVE #1 ENGINE AFT FAIRING / REMOVED AND REPLACED PER SRM 51-40-02.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 42,995 hrs · 30,625 cycles

DIVERSION< REPORTED BURNT RUBBER SMELL IN AFT GALLEY. R&R NR 1 AFT GALLEY COFFEEMAKER PER AMM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 42,995 hrs · 30,625 cycles

DIVERSION, REPORTED BURNT RUBBER SMELL IN AFT GALLEY. R&R NR 2 AFT GALLEY COFFEEMAKER PER AMM.

Part: CHARGER — FAULTY (CABIN) · airframe 42,804 hrs · 30,500 cycles

RT AFT CABIN EMERGENCY LIGHTS CHARGER CIRCUIT BREAKER FOUND OPEN. R&R BATTERY CHARGER IAW AMM.

Part: SLIDE — FAILED INSP (R1 DOOR) · airframe 42,204 hrs · 30,121 cycles

R1 DOOR SLIDE FAILED INSPECTION. R & R THE SLIDE ASSY IAW MM.

Part: SLIDE — FAILED INSP (L1 DOOR) · airframe 42,204 hrs · 30,121 cycles

L1 DOOR SLIDE FAILED AN INSPECTION. R & R THE SLIDE ASSY IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 41,876 hrs · 29,930 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: BRACKET — DETACHED (LT WING TE FLAP) · airframe 41,563 hrs · 29,747 cycles

LEFT WING INBOARD AFT FLAP ACTUATING MECHANISM, DETACHED FROM THE FLAPTRACK BRACKET. R & R THE BRACKET IAW AMM & EA.

Part: STRIP — DELAMINATED (CABIN) · airframe 41,414 hrs · 29,658 cycles

RT FLOOR MOUNTED EGRESS STRIPS DELAMINATED. R&R STRIPS PER DWG.

Part: ANGLE — CRACKED (WHEEL WELL LH) · airframe 41,414 hrs · 29,658 cycles

L/H FWD UPPER FIXED T/E PANEL HAS CRACKED ANGEL I/B FWD CORNER IN MLG W/W. / R/R ANGLE IAW SRM 51-40-02.

Part: COVER — CRACKED (EMERGENCY EXIT) · airframe 41,414 hrs · 29,658 cycles

LT EMERGENCY EXIT HATCH RELEASE COVER CRACKED. R&R COVER PER AMM.

Part: STRIP — DELAMINATED (CABIN) · airframe 41,414 hrs · 29,658 cycles

FORWARD ENTRY AREA FLOOR MOUNTED EGRESS STRIPS DELAMINATED. R&R STRIPS PER DWG.

Part: STRIP — DELAMINATED (CABIN) · airframe 41,414 hrs · 29,658 cycles

LT FLOOR MOUNTED EGRESS STRIPS DELAMINATED. R&R STRIPS PER DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,409 hrs · 29,033 cycles

RT EMERGENCY EXIT DOOR LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: RETAINER — LOOSE (R2 DOOR) · airframe 40,154 hrs · 28,867 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT RETAINING BAR LOOSE. SECURED RETAINER PER SIP AND AMM.

Part: SLIDE — BROKEN (R2 DOOR) · airframe 39,185 hrs · 28,284 cycles

R2 DOOR SLIDE OUT, DOOR HINGE BROKEN. R & R THE SLIDE IAW CMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,242 hrs · 27,758 cycles

LEFT AFT WING EMERGENCY SLIDE LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,242 hrs · 27,758 cycles

RIGHT AFT WING EMERGENCY SLIDE LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,242 hrs · 27,758 cycles

L2 DOOR SLIDE LIGHT INOPERATIVE. REPLACED THE BULB IAW AMM.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 38,106 hrs · 27,687 cycles

RT OVERWING ESCAPE GROUND EMERGENCY EXIT LIGHTS INOP. REPAIRED LIGHTS PER SIP.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 38,106 hrs · 27,687 cycles

LT OVERWING ESCAPE GROUND EMERGENCY EXIT LIGHTS INOP. REPAIRED LIGHTS PER SIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,049 hrs · 27,654 cycles

RT OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,660 hrs · 27,433 cycles

EMERGENCY LIGHT M1670 INOPERATIVE. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 37,092 hrs · 27,128 cycles

EXTERIOR LT EMERGENCY LIGHTS AFT OF THE WING INOP AT ROW 17. R&R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 37,092 hrs · 27,128 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 36,828 hrs · 26,976 cycles

RIGHT EXIT SIGN LIGHT INOPERATIVE AT ROW 12. RELAMPED SIGN IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,287 hrs · 26,668 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 36,034 hrs · 26,525 cycles

R1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: SUPPORT — CRACKED (TE FLAP) · airframe 34,893 hrs · 25,911 cycles

LEFT WING INBD AFT FLAP AREA, INBD UPPER FIXED PANEL, LOWER SEAL SUPPORT CRACKED. REPAIRED SUPPORT IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 32,281 hrs · 24,417 cycles

AFT RT EMER LIGHT LENS LOOSE. R & R LENS IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 31,640 hrs · 24,047 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW MT.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 32,241 hrs · 24,393 cycles

AIR TURN BACK, MODE CONTROL PANEL ALTITUDE LOCKED SHOWING 50000' FEET. R & R MODE CONTROL PANEL IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 30,538 hrs · 23,413 cycles

EMERGENCY LIGHTS BATTERY CHARGER M1675 INOPERATIVE. R & R CHARGER IAW AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 30,538 hrs · 23,413 cycles

AFT LT EMER AISLE LIGHT INOPERATIVE. INSTALLED WIRE IAW MM.

Part: SHROUD — BROKEN (R2 DOOR) · airframe 30,538 hrs · 23,413 cycles

R2 DOOR ESCAPE SLIDE SHROUD BROKEN. R & R SLIDE IAW MT.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 30,538 hrs · 23,413 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED STATION 105 AT MID SPAR. REPAIRED SKIN IAW CCO.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

FORWARD CARGO BAY LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D BETWEEN RBL 24 TO LBL 24. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

FLOOR TO SIDE WALL SUPPORT ANGLE CORRODED BETWEEN BS 500A TO 500D RBL 24. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 30,538 hrs · 23,413 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED STATION 101.90 AFT OF FRONT SPAR. REPAIRED SKIN IAW CCO.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 30,538 hrs · 23,413 cycles

LEFT HORIZONTAL STAB THIRD VERTICAL STIFFENER RIB CRACKED AT STATION 92.70. REPAIRED STIFFENER IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 30,537 hrs · 23,413 cycles

RIGHT WING REAR SPAR TO TE BEAM ATTACH ANGLE CRACKED AT RSS 76. R & R ANGLE IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 30,537 hrs · 23,413 cycles

RIGHT WING LOWER TE WAFFLE PLATE CRACKED JUST OTBD OF PANEL 661DB. R & R WIGGLE PLATE ASSEMBLY IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 30,537 hrs · 23,413 cycles

RIGHT WING UPPER AFT TE SUPPORT ANGLE CRACKED ABOVE NR 2 PYLON AFT TIP AT TRANSVERS E WEB ATTACH POINT. R & R ANGLE IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 30,538 hrs · 23,413 cycles

LEFT HORIZONTAL STAB SECOND VERTICAL STIFFENER RIB CRACKED AT STATION 92.70. REPAIRED STIFFENER IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 30,537 hrs · 23,413 cycles

RIGHT WING LOWER TE WAFFLE PLATE CRACKED JUST INBD OF NR 2 PYLON. R & R WAFFLE PLATE IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 30,537 hrs · 23,413 cycles

RIGHT WING RSS 500 TE RIB CRACKED ON INBD UPPER LEG. R & R RIB IAW SRM & DWG.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 30,538 hrs · 23,413 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED STATION 147.90 AFT OF FRONT SPAR. REPAIRED SKIN IAW CCO.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 30,538 hrs · 23,413 cycles

LEFT WING COVE SEAL SUPPORT ANGLE CRACKED ABOVE NR 1 PYLON AFT TIP. R & R ANGLE IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 30,537 hrs · 23,413 cycles

LEFT WING LOWER TE WAFFLE PLATE CRACKED JUST INBD OF NR 1 PYLON. R & R WAFFLE PLATE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 30,537 hrs · 23,413 cycles

LEFT WING UPPER TE PANEL AFT SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT ABOVE NR 1 PYLON AFT TIP. R & R ANGLE IAW SRM.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 30,527 hrs · 23,413 cycles

L1 DOOR EMER EVAC SLIDE COVER AFT GIRT BAR RETAINER CLIP LOOSE. R & R CLIP IAW SRM.

Part: SLIDE — DISCONNECTED (L1 DOOR) · airframe 300,537 hrs · 23,413 cycles

L1 DOOR ESCAPE SLIDE DISCONNECTED TO COVER. CONNECTED SLIDE TO BACKING PAN IAW MT.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 30,537 hrs · 23,413 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

SEAT TRACK AFT FLANGE CRACKED AT BS 727B, LBL 45.5 AT THE TWO INBD HOLES. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

SEAT TRACK AFT FLANGE CRACKED AT BS 727B, RBL 24.75 AT TWO INBD HOLES. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

SEAT TRACK AFT FLANGE CRACKED AT BS 727B, RBL 45.5 AT THE AFT OTBD HOLE. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75, AT THE AFT OTBD HOLE. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

SEAT TRACK AFT FLANGE CRACKED AT BS 727B, LBL 24.75 AT THE AFT OTBD HOLE. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

SEAT TRACK AFT FLANGE CRACKED AT BS 727B, RBL 45.5 AT THE AFT INBD HOLE. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

SEAT TRACK AFT FLANGE CRACKED AT BS 727B, LBL 45.5 AT THE TWO OTBD HOLES. REPAIRED SEAT TRACK IAW ER & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

AFT CARGO BAY ON LOWER SURFACE OF FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO 887 RBL 16. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

AFT CARGO BAY SIDEWALL TO FLOOR SUPPORT CORRODED BETWEEN BS 727+4.5 TO 767 RBL 21. R & R SUPPORT IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

AFT CARGO INTERCOSTAL FLOOR SUPPORT CORRODED BETWEEN STATION 848 TO 867 RBL 13 TO 18. REPAIRED FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 727A TO 727E+ 12.5, LBL 21. R & R SUPPORT IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

FRAME CRACKED AT BS 440 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

FRAME CRACKED AT BS 440 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

FRAME CRACKED AT BS 480 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

FRAME CRACKED AT BS 400 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

INTERCOSTAL CRACKED BETWEEN BS 294 TO 312 RBL 16. REPAIRED INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

INTERCOSTAL CRACKED BETWEEN BS 294 TO 312 LBL 27. REPAIRED INTERCOSTAL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

FRAME CRACKED AT BS 480 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,538 hrs · 23,413 cycles

FRAME CRACKED AT BS 360 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 30,537 hrs · 23,413 cycles

LEFT WING NR 2 SLAT LE LOWER SKIN CRACKED AT ACTUATOR ATTACH FITTING AT AFT INBD FASTENER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 30,537 hrs · 23,413 cycles

LEFT WING NR 1 SLAT LE LOWER SKIN CRACKED AT ACTUATOR ATTACH FITTING AT AFT INBD & OTBD FASTENERS. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

RIGHT NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED FRAME CRACKED IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 30,537 hrs · 23,413 cycles

LEFT NR 3 WINDOW FRAME CRACKED AT EF POST, SECOND HOLE FROM BOTTOM. REPAIRED POST IAW ACO.