N227WN

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 65,503 hrs · 39,329 cycles

R/H OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED RT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-02. OPS CHKD GOOD.

Part: PUMP — OUT OF ADJUST (ZONE 400) · airframe 65,045 hrs · 39,023 cycles

EXCESSIVE NOSE WHEEL SHIMY ON TAKE OFF ROLL DIFFICULT TIME TRACKING RUNWAY CENTERLINE ; TAKE OFF REJECTED. CREW REPORTED REJECTED T/O BETWEEN 90-100 KTS.<[01] PERFORMED INSPECTION OF NLG PER AMM 09-11-00. NO DEFECTS NOTED.;[02] PERFORMED NLG STEERING ADJUSTMENT CHECK; ALL CHECKS ARE GOOD PER AMM 32-51-00.;[03] PERFORMED INSPECTION OF RUDDER PEDAL INTERCONNECT INPUT ROD PER AMM 32-51-00. NO DEFECTS NOTED.;[04] REMOVED AND REPLACED NOSE WHEEL TIRES REF AMM 32-45-21;[05] REMOVED AND REPLACED #1 ENGINE HYD. PUMP; AND PERFORMED ALL OPS AND LEAK CHECKS; ALL CHECKS ARE GOOD PER AMM 29-11-11 ON NON-ROUTINE (TTG8Q015QTHW);[06] PERFORMED TAXI OF AIRCRAFT AND NO ABNORMAL NOSE WHEEL SHIMMY WAS NOTED PER AMM 09-20-00.

Part: TIRE — ABNORMAL (ZONE 700) · airframe 65,045 hrs · 39,023 cycles

EXCESSIVE NOSE WHEEL SHIMMY ON TAKE OFF ROLL. DIFFICULT TIME TRACKING RUNWAY CENTERLINE. TAKE OFF REJECTED. CREW REPORTED REJECTED T/O BETWEEN 90-100 KTS. PERFORMED INSPECTION OF NLG IAW AMM 09-11-00. NO DEFECTS NOTED. PERFORMED NLG STEERING ADJUSTMENT CHECK, ALL CHECKS GOOD IAW AMM 32-51-00. PERFORMED INSPECTION OF RUDDER PEDAL INTERCONNECT INPUT ROD IAW AMM 32-51-00. NO DEFECTS NOTED. REMOVED AND REPLACED NOSE WHEEL TIRES IAW AMM 32-45-21. REMOVED AND REPLACED NR 1 ENGINE HYD PUMP, AND PERFORMED ALL OPS & LEAK CHECKS, CHECKS GOOD IAW AMM 29-11-11 ON NON-ROUTINE TTG8Q015QTHW. PERFORMED TAXI OF ACFT & NO ABNORMAL NOSE WHEEL SHIMMY NOTED IAW AMM 09-20-00.

Part: HANDLE — LOOSE (ZONE 800) · airframe 65,040 hrs · 39,021 cycles

PAX CABIN FWD ENTRY DOOR UPPER ASSISTANT HANDLE LOOSE. INSTALLED CORRECTLY ASSISTAND HANDLE UPPER FWD ENTRY DOOR PAX CABIN IAW BOEING SOPM 20-50-01 REV.39.

Part: LIGHT — BROKEN (ZONE 200) · airframe 65,042 hrs · 39,022 cycles

BROKEN PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA). REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) IAW SOPM 20-50-12 REV 58 AND DWG 33500007 SHEET 2.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CRACK ON SCUFF PLATE FWD SERVICE DOOR. REPAIRED SCUFF PLATE FWD SERVICE DOOR IAW SRM 53-10-15-2R-2 REPAIR 2.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW SRM 51-40-02-0G AND DWG 141A8310 SHEET: 25 REV -.

Part: NUT PLATE — CORRODED (ZONE 600) · airframe 65,042 hrs · 39,022 cycles

CORROSION ON RAIL NUT PLATE LOCATED OFSS308 INTERNAL CAVITY LEADING EDGE AT RT WING. EVALUATED RAIL NUT PLATE AND NOT FOUND ALLOWABLE DAMAGE ON SRM IAW SRM 57-20-01-1A-1 ALLOWABLE DAMAGE. REPLACED RAIL NUT PLATE LOCATED OF SS308 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-40-02 AND MEASURES OF CORROSION ARE : L: 1.741 INCH W: 0.288 INCH.

Part: NUT PLATE — CORRODED (ZONE 600) · airframe 65,042 hrs · 39,022 cycles

CORROSION RAIL NUT PLATE LOCATED OFSS293 INTERNAL CAVITY LEADING EDGE AT RT WING. EVALUATED RAIL NUT PLATE AND NOT FOUND ALLOWABLE DAMAGE ON SRM IAW B737-700 SRM 57-20-01-1A-1 ALLOWABLE DAMAGE. REPLACED RAIL NUT PLATE LOCATED OFSS293 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-40-02 AND MEASURES OF CORROSION ARE : L: 1.741 INCH W: 0.288 INCH.

Part: ANGLE — CRACKED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CRACK ON ANGLE LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA. REPLACED ANGLE AND FASTENERS LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA IAW SRM 51-40-02-0G AND DWG 141A1311 SHEET: 1 REV: C.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 867 BTW STR 26L TO STR 27L AT AFT CARGO COMPARTMENT. FAULT RESOLVED IN OTHER FAULT SEE TTG8Q0151DJ3;[02] FAULT RESOLVED ON OTHER FAULT

Part: WEB — CORRODED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CORROSION ON WEB LOCATED BTW BS 747 TO BS 767 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. REPLACED WEB ASSY AND FASTENERS LOCATED BTW BS 747 TO BS 767 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG:146A7502 SHEET: 26 REV.

Part: WEB — CORRODED (ZONE 200) · airframe 65,042 hrs · 39,022 cycles

CORROSION ON SHIELD WEB LOCATED BTW BS 767 TO BS 794.3 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS 767 TO BS 794.3 RBL 25 WL 156.1 AT AFT CARGO COMPARTMENT I.A.W SRM 51-40-02-0G-0 AND DWG 146A0081 SHEET 31 REV: -.

Part: FITTING — CRACKED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CRACK ON FITTING LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT. REPLACED FITTING LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT. IAW SRM 51-10-02-0G-0 ITEM 9 AND DWG 149A8103 SHEET: 7 REV: A.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS 767 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. EVALUATED CORROSION ON SUPPORT ZEE LOCATED BTW BS 767 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT AND FOUND OUT OF LIMITS DUE TO DAMAGE EXCEED 10T OF ALLOWABLE DAMAGE IAW B737-700 SRM 53-00-53-1A-2 STEP4. (A.) (2)(A) FIGURE 103 DETAIL (D). NOMINAL THICKNESS IS:<BR>0.40* IAW BAC 1496-377 AND REPLACEMENT SUPPORT ZEE LOC BS 727 TO BS 847 LBL 22.

Part: WEB — CRACKED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CRACK ON WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT. REPLACED WEB ASSY AND FASTENER LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; AND DRAWING 147A7500 REV -.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CORROSION ON SUPPORT ANGLE LOCATED BS 947.5 BTW STR 25R TO STR25L AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE LOCATED BS 947.5 BTW STR 25R TO STR25L AT AFT CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 149A8117; SHEET: 6; REV-.

Part: ANGLE — CORRODED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CORROSION ON ANGLE LOCATED BS 787 BTW STR 24R TO STR 25R WL 156.5 AT AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS 787 BTW STR 24R TO STR 25R WL 156.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A1262; SHEET:95; REV:-.

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 65,042 hrs · 39,022 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 867 BTW STR 26L TO STR 27L AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE LOCATED BS 867 BTW STR 26L TO STR 27L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 DWG 149A8102 SHEET 19 REV A AND DWG 149A8102 SHEET 17 REV- AND TOOK MEASURE OF CRACK IS L: 0.3635 INCH .

Part: WEB — CORRODED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CORROSION ON WEB LOCATED BTW BS 767 TO BS 787 RBL 21 WL 156.1 AT AFT CARGO COMPARTMENT. REPLACED WEB LOCATED BTW BS 767 TO BS 787 RBL 21 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081; SHEET: 34; REV: -.

Part: STRAP — CORRODED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CORROSION ON STRAP LOCATED BS 887 BTW STR 25R TO STR 26L WL 156.1 AT AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BS 887 BTW STR 25R TO STR 26L WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG DWG 146A7500 SHEET: 85 REV: A.

Part: WEB — DAMAGED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

ELONGATED HOLE ON WEB - INTERCOSTAL LOCATED BS 492 AND S-26R AT FWD CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BS 492 AND S-26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A0080 SHET: 23 REV.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT (20 POINTS). REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-5 REPAIR 5 AND DWG: 146A7500 SHEET: 85 REV A. DWG: 146A0061 SHEET: 75 REV - ; DWG: 146A7502 SHEET: 27 REV -.

Part: WEB — CRACKED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CRACK ON WEB LOCATED BTW BS 1016 AND AFT BULKHEAD LEFT SIDE AT PAX CABIN. REPLACED WEB LOCATED BTW BS 1016 AND AFT BULKHEAD LEFT SIDE AT PAX CABIN. IAW SRM: 51-40-02-0G-0 AND DWG 148A0922 SHEET 21, REV.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CORRODED SUPPORT ANGLE LOCATED BS 500D, BETWEEN STRINGERS 26L - 26R, WL 156 IN FWD CARGO COMPARTMENT, REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, DWG 141A9481, SHEET 10, REV -, AND DWG 143A7902, SHEET 174, REV -.

Part: WEB — CORRODED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CORROSION ON SHIELD WEB LOCATED BTW BS 847 TO BS 867 RBL 21 WL 156.1 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS 847 TO BS 867 RBL 21 WL 156.1 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG 146A0081; SHEET:31;REV:-.

Part: ANGLE — CRACKED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CRACK ON ANGLE - CLIP LOCATED BS420 AND STR26L FWD CARGO COMPARTMENT. REPLACED ANGLE - CLIP LOCATED BS420 AND STR26L FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG 143A7505 SHEET: 2 REV: B.

Part: ANGLE — CRACKED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CRACK ON ANGLE - CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT. REPLACED ANGLE - CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT. IAW SRM 51-10-02-0G-0 ITEM 9 AND DWG 143A7505 SHEET: 2 REV: B.

Part: ANGLE — CRACKED (ZONE 100) · airframe 65,042 hrs · 39,022 cycles

CRACK ON ANGLE - CLIP LOCATED BS500C AND STR26R FWD CARGO COMPARTMENT. REPLACED ANGLE - CLIP AND FASTENERS LOCATED BS500C AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET:6 REV:D .

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 65,042 hrs · 39,022 cycles

CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 AND LBL 2 AT PASSENGER CABIN. REPLACED BRAKE PANEL AND FASTENERS LOCATED FLOOR STRUCTURE LOCATED STA 540 AND BTW BL O TO LBL 24.75 AT PASSENGER CABIN IAW SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 65,042 hrs · 39,022 cycles

CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 AND RBL 2 AT PASSENGER CABIN. REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 AND RBL 2 AT PASSENGER CABIN IAW B737-700 SRM51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 143A0060 SHEET: 46 REV: -.

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 65,042 hrs · 39,022 cycles

CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSANGER CABIN (1 E/A) . CRACK LENGTH APPROX 0.350 IN . PERFORMED PERMANENT REPAIR ON PRESSURE DECK WEB LOCATED BTW BS 663 TO BS 675 BTW LBL 24 TO LBL 60 IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2.

Part: LENS — BROKEN (ZONE 200) · airframe 65,042 hrs · 39,022 cycles

BROKEN EMERGENCY EXIT LENS ASSY LOWERED CEILING AT AFT GALLEY AREA (1EA). REPLACED EMERGENCY EXIT LENS ASSY LOWERED CEILING AT AFT GALLEY AREA (1EA) IAW SOPM 20-50-01;REV.39.

Part: FRAME — CRACKED (ZONE 200) · airframe 65,042 hrs · 39,022 cycles

CRACK FRAME LOCATED BS259.5 BTW STR8R TO STR9R AT PASSENGER CABIN. REPAIRED FRAME WEB AT BSTA 259.5 BTW WL 240 AND WL 280 AND RBL 20 AND RBL 50 IAW EA-25-153-02403 WIP1 AND EA-25-153-02403.

Part: DOOR — CRACKED (ZONE 800) · airframe 38,514 hrs · 64,210 cycles

RH MLG MIDDLE DOOR CRACKED AT LWR FWD POCKET CUT OUT. REMOVED RT MLG CENTER AND INNER DOORS PER AMM 32-13-11.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 62,984 hrs · 37,782 cycles

R/H OVERWING EXIT EXTERIOR EMER LIGHT INOP.<[01] 01 - REMOVED AND REPLACED LAMP ON R/H OVERWING EXIT EXTERIOR LIGHT PER [AMM 33-51-04-960-801-NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)]

Part: LENS — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 62,564 hrs · 37,538 cycles

FWD. ENTRY DOOR (L-1) EMERGENCY EXIT SIDEWALL LENS FELL OFF<[01] REMOVED & REPLACED SIDEWALL EXIT SIGN ASSAY. IAW M/M. 33-51-06 & 33-51-14

Part: LAMP — INOPERATIVE (ZN 200 FUS TOP) · airframe 62,487 hrs · 37,493 cycles

LEFT SIDE VERY AFT BY L2 DOOR OUTSIDE EMERGENCY LIGHT INOP.<[01] REPLACED AFT EMERGENCY LIGHT LAMP IAW AMM 33-51-04 OPS. CHECK GOOD.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 61,760 hrs · 37,034 cycles

-KEEL BEAM FWD PNL 192E FWD LEFT SUPPORT BRACKET CRACKED.<[01] REMOVED AND REPLACED FWD LEFT SUPPORT BRACKET AT PANEL 192E PER SRM 51-40-02

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 61,760 hrs · 37,034 cycles

-KEEL BEAM FWD PNL 192E FWD RIGHT SUPPORT BRACKET CRACKED.<[01] REMOVED AND REPLACED FWD RIGHT SUPPORT BRACKET AT PANEL 192E PER SRM 51-40-02.

Part: PLATE — BROKEN (ZONE 800) · airframe 61,760 hrs · 37,034 cycles

AFT SERVICE DOOR LOWER PAN AFT UPPER SHOCK PLATE BROKEN.<[01] R/R AFT SERVICE DOOR LOWER PAN AFT LOWER SHOCK PLATE REF AMM 51-40-02.;[02] R/R AFT SERVICE DOOR LOWER PAN AFT LOWER SHOCK PLATE REF SRM 51-40-02.;[03] CONFIRMED REPAIR WAS DONE IAW SRM.

Part: GUARD — FAULTED (EMER LITE SWITCH) · airframe 60,006 hrs · 35,971 cycles

EMERGENCY LIGHT SWITCH ON OVERHEAD PANEL COVER WILL NOT STAY IN THE CLOSED POSITION<[01] REMOVED AND REPLACED SWITCH GUARD PER SIP

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 59,361 hrs · 35,578 cycles

R/H HORIZONTAL FWD SLIDER SEAL CRACKED<[01] REMOVED AND REPLACED SEAL PER AMM 53-31-31.;[02] REMOVED AND REPLACED SEAL PER AMM 53-31-31.

Part: ISOLATOR — CRACKED (ZN 800 DOOR) · airframe 59,361 hrs · 35,578 cycles

AFT ENTRY DOOR FWD ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.

Part: STRINGER — CRACKED (ZN 500 LEFT WING) · airframe 59,356 hrs · 35,576 cycles

CRACK; L/H WING; UPPER VENT STRINGER NO. 10 ASSY; AT INSPAR RIB 6 - MX FERRY FLIGHT-TLD) [TTG8Q00NXHZV] STEP 3 REQUIRES THAT AIRCRAFT IN REFERENCE TO 23-157-03018 (N227WN - SWA - MINOR ACTION - CRACK L/H WING UPPER VENT STRINGER NO. 10 ASSY AT INSPAR RIB 6 - MX FERRY FLIGHT-TLD) [TTG8Q00NXHZV] STEP 3 REQUIRES THAT AIRCRAFT BE PLACED ON A TWO FLIGHT CYCLE MX NOTE<[01] OK TO CONTINUE AS A MX NOTE. AUTHORIZATION# 160669;[02] REPAIR COMPLETED ON LOG PAGE 2121291 AND TTG8Q00NVXEJ.

Part: VENT — CRACKED (ZN 500 LEFT WING) · airframe 59,356 hrs · 35,576 cycles

DURING FUEL TANK ENTRY/INSPECTION FOUND 3' CRACK L/H TANK AFT VENT BOX IB OF PYLON ABOVE RIB 6. WORKING MEL 28-2-05 TTG8Q00NT6WX<[01] ADDED MEASUREMENTS;[02] REMOVED BOLT TO GAIN ACCESS FOR CRACK AREA I.A.W SRM 51-40-02-0G-0;[03] OK TO TREAT AND PRIME REPAIR PARTS;[04] TREATED AND PRIMED REPAIR PARTS AND CUT EDGES IAW AMM 28-11-00 AND AMM 51-20-01;[05] VERIFIED STEP 4.;[06] BOLT REMOVED ON STEP 2 WAS INSTALLED ON FAULT TTG8Q00P0DP6 STEP 22;[07] REPAIRED LH WING STRINGER U10 CRACK AT WSTA 228.26 (RIB 6) IAW EA 23-157-03071;[08] VERIFIED STEP 7<BR>AUDIT C/W;[09] AUDIT C/W

Part: SCUFF PLATE — CRACKED (ZN 800 DOOR) · airframe 59,279 hrs · 35,528 cycles

CRACK ON SCUFF PLATE FWD CORNER FWD ENTRY DOOR 2023-530669<[01] TOOL USED DIGITAL CALIPER P/N:500-193-30;S/N:0036617; DUE DATE:19/JUL/24.;[02] TOOL USED: RADIOMETER KIT; P/N: XRP-3000; S/N: 1998072; DUE DATE: 15-OCT-23.;[03] REPAIRED THE FWD CORNER SCUFF PLATE AT FWD ENTRY DOOR IN ACCORDANCE WITH BOEING 737-700 SRM TASK 53-10-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (3) TO (6) AND (8); BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED THE FWD CORNER SCUFF PLATE AT FWD ENTRY DOOR IN ACCORDANCE WITH BOEING 737-700 SRM TASK 53-10-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (3) TO (6) AND (8); BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 59,279 hrs · 35,528 cycles

CRACK ANGLE ON INBOARD AUXILIARY SLAT TRACK SLAT1 AT LT WING 2023-530966<[01] REPLACED ANGLE ON INBOARD AUXILIARY SLAT TRACK SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM 57-43-01;[02] TASK CARD COMPLETED

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 59,279 hrs · 35,528 cycles

CRACK ANGLE ON INBOARD AUXILIARY SLAT TRACK SLAT 7 AT RT WING 2023-530943<[01] REPLACED ANGLE ON INBOARD AUXILIARY SLAT TRACK SLAT 7 AT RT WING IAW B737-700 SRM 51-40-02<BR>TOOL USED DIGITAL CALIPER<BR>PN: 500-196-30<BR>SN: A20227391<BR>DUE DATE: 11-OCT-23;[02] JOB COMPLETED.

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 59,279 hrs · 35,528 cycles

CRACK ANGLE ON INBOARD AUXILIARY SLAT TRACK SLAT 8 AT RT WING 2023-530942<[01] REPLACED ANGLE ON INBOARD AUXILIARY SLAT TRACK SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02; TOOL USED DIGITAL<BR>PN: 500-1096-30<BR>SN: A20227391<BR>DUE DATE: 11-OCT-23;[02] CORRECTED STEP 1.<BR>REPLACED ANGLE ON INBOARD AUXILIARY SLAT TRACK SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02; TOOL USED DIGITAL CALIPER<BR>PN: 500-1096-30<BR>SN: A20227391<BR>DUE DATE: 11-OCT-23;[03] JOB COMPLETED.

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 59,279 hrs · 35,528 cycles

CRACK ANGLE ON INBOARD AXILIARY SLAT TRACK SLAT 3 AT LT WING 2023-530967<[01] REPLACED ANGLE ON INBOARD AXILIARY SLAT TRACK SLAT 3 AT LT WING IAW B737-700 CMM 57-43-03 PAGE 701 THRU PAGE 703. STEP 2.C(9);[02] COMPLETE TASK CERTIFIED

Part: BRACKET — CORRODED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CORROSION ON SUPPORT BRAKETS LOCATED ON DOOR 315A ON APU COMPARTMENT (4EA) 2023-530976<[01] REPLACED SUPPORT BRAKETS LOCATED ON DOOR 315A ON APU COMPARTMENT (4EA) AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #148A6350 REV:C SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1 REPLACED SUPPORT BRAKETS LOCATED ON DOOR 315A ON APU COMPARTMENT (4EA) AND FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING #148A6350 REV:C SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 1 REPLACED SUPPORT BRAKETS LOCATED ON DOOR 315A ON APU COMPARTMENT (4EA) AND FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING #148A6350 REV:C SEE INDIVIDUAL SIGN OFF BELOW

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

BROKEN LAVATORY A COVER EMERGENCY EXIT AT FWD GALLEY AREA (1 EA) 2023-530916<[01] REPLACED LAVATORY A COVER EMERGENCY EXIT AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 2(C) ITEM 2(4);[02] REPLACED LAVATORY A COVER EMERGENCY EXIT AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 2(C) ITEM 2(4)

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 59,279 hrs · 35,528 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT LT WING 2023-530894<[01] REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE LOCATED ORSS261 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001; SHEET 32.;[02] COMPLETE TASK CERTIFIED

Part: SUPPORT BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 59,279 hrs · 35,528 cycles

CRACK TRAILING EDGE SUPPORT BRACKET LOCATED ORSS272 AT LT WING 2023-530895<[01] REPLACED TRAILING EDGE SUPPORT BRACKET LOCATED ORSS272 AT LT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. DWG: 115A2930 SHEET:7 REV: -. DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON B737-700 SRM 57-51-02-1A-1.<BR><BR>CRACK LENGTH IS: 0.727 INCHES.<BR><BR>TOOL USED ELECTRONIC CALIPER P/N: 500-196-30 S/N: A20227391 DUE DATE: 11-OCT-23;[02] COMPLETE TASK CERTIFIED

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CRACK BRACKET BODY STATION 540 LBL 6 AT AIR CONDITIONING BAY 2023-530914<[01] REPLACED BRACKET LOCATED BODY STATION 540 LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9. LENGTH OF CRACK:1.038?. TOOL USED CALIPER P/N: 500-752-20; S/N:B21037208;DUE DATE: 04-MAR-24;[02] REPLACED BRACKET LOCATED BODY STATION 540 LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9. LENGTH OF CRACK:1.038?. TOOL USED CALIPER P/N: 500-752-20; S/N:B21037208;DUE DATE: 04-MAR-24

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 59,279 hrs · 35,528 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING 2023-530896<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9. AND DRAWING # 115A2001 REV: A. SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING IAW B737-700 SRM 51-40-02 AND DRAWING # 115A2001 REV: A. SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 1. REPLACED CORRUGATE PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING IAW B737-700 SRM 51-40-02 AND DRAWING # 115A2001 REV: A. SEE INDIVIDUAL SIGN OFF BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CRACK ON ANGLE BODY STATION 663 RBL 41.10 AT LOWER FUSELAGE 2023-530908<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[03] REPLACED ANGLE AND FASTENERS LOCATED BODY STATION 663 BTW RBL 17 TO RBL 65 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND SRM 57-10-10-2R-5.SEE INDIVIDUAL SIGN OFF BELOW.;[04] TASK CARD COMPLETED <BR>REPLACED ANGLE AND FASTENERS LOCATED BODY STATION 663 BTW RBL 17 TO RBL 65 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND SRM 57-10-10-2R-5.SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: PANEL — BROKEN (ZN 600 RIGHT WIN) · airframe 59,279 hrs · 35,528 cycles

BROKEN ANGLE ACCESS PANEL 651FB TRAILING EDGE AT RT WING 2023-530820<[01] REPLACED ANGLE LOCATED ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10- 02 ITEM 9;[02] CORRECTIVE ACTION CERTIFIED

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CRACK ANGLE BTW BS 907 TO BS 927 RBL 13.8 AFT POSITION AT AFT CARGO COMPARTMENT 2023-530832<[01] REPLACED ANGLE BTW BS 907 T BS 927 AND RBL 8.10 TO RBL 20 FWD POSITION AT AFT CARGO COMPARTMENT I.A.W SRM B737-700 51-40-02.SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTIVE ACTION CERTIFIED

Part: PANEL — DELAMINATED (ZN 600 RIGHT WIN) · airframe 59,279 hrs · 35,528 cycles

DELAMINATED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR 2023-530816<[01] TOOL USED:CALIPER PN: 500-197-30 SN: B20189527; DUE DATE: 26-DEC-23.;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18185781 DUE DATE 24/JAN/24.;[03] TOOL USED SCALE P/N CR5200 S/N 8342514597 DUE DATE 21/FEB/24.;[04] TOOL USED: MULTIMETER P/N: FLUKE-289; S/N: 61180137 ; DUE DATE: 25-MAY-24;[05] REPAIRED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-05-2R-2 REPAIR 2. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] REPAIRED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-05-2R-2 REPAIR 2. SEE INDIVIDUAL SIGNOFF BELOW. COMPLETED

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

BROKEN LAVATORY A EMERGENCY EXIT LIGHT LENS AT FWD GALLEY AREA (1 EA) 2023-530837<[01] REPLACED LAVATORY A EMERGENCY EXIT LIGHT LENS AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 2(C) ITEM 2(4);[02] CORRECTED STEP 1 <BR><BR>REPLACED LAVATORY A EMERGENCY EXIT LIGHT LENS AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 2(C) ITEM (4);[03] REPLACED LAVATORY A EMERGENCY EXIT LIGHT LENS AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 2(C) ITEM (4)

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CRACK ANGLE BTW BS 907 T BS 927 AND RBL 13.8 FWD POSITION AT AFT CARGO COMPARTMENT 2023-530830<[01] REPLACED ANGLE BTW BS 907 T BS 927 AND RBL 8.10 TO RBL 20 FWD POSITION AT AFT CARGO COMPARTMENT I.A.W SRM B737-700 51-40-02.SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTIVE ACTION CERTIFIED

Part: INTERCOSTAL — CORRODED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CORROSION ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 294.5 TO BS 312 LBL 6 AT FWD GALLEY AREA 2023-530690<[01] REPLACED INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 294.5 TO BS 312 LBL 6 AT FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A5600 SHEET:1 AND 2 REV:N SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 LBL 30 AT FWD GALLEY AREA 2023-530688<[01] REPLACED INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 LBL 30 AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING#141A5400 REV:- SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CORRECTED STEP 1.<BR>REPLACED INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 LBL 30 AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING#141A5400 REV:- SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPLACED INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 LBL 30 AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING#141A5400 REV:- RII<BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 4 AT FWD GALLEY AREA 2023-530694<[01] REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 RBL 4 AT FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 32 REV -SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1 REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 RBL 4 AT FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 32 REV -SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 RBL 4 AT FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 32 REV -SEE INDIVIDUAL SIGN OFF BELOW COMPLETED RII

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 RBL 36 AT FWD GALLEY AREA 2023-530684<[01] REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 LBL 36 AT FWD GALLEY AND FASTENERS IAW B737-700 SRM 51-40-02<BR>AND DWG 141A5400 SHEET 26 REV -SEE INDIVIDUAL SIGN OFF BELOW;[02] RII COMPLETED JOB

Part: TIE CLIP — CRACKED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-530710<[01] REPLACED TIE CLIP LOCATED ON BS277 AT LEVEL STR10RAT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV.-<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED TIE CLIP LOCATED ON BS277 AT LEVEL STR10R AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV.-<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED TIE CLIP LOCATED ON BS277 AT LEVEL STR10R AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV.- <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CRACK ANGLE - CLIP LOCATED BS500A AND STR26L FWD SIDE FWD CARGO COMPARTMENT 2023-530699<[01] REPLACED ANGLE - CLIP LOCATED BS500A AND STR26L FWD SIDE FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE - CLIP LOCATED BS500A AND STR26L FWD SIDE FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV -. <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2<BR>REPLACED ANGLE - CLIP LOCATED BS500A AND STR26L FWD SIDE FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV -. <BR>SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: UNKNOWN — CORRODED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CORROSION ON EXISTING REPAIR LOCATED BS 312 LBL 8 WL 208.1 AT FWD GALLEY AREA 2023-530692<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23.;[02] TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189510; DUE DATE: 26-DEC-23.;[03] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1753759; CAL DUE DATE: 14-OCT-23;[04] PERFORMED PERMANENT REPAIR LOCATED BS 312 BTW RBL 6 TO LBL 29 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-12 REPAIR 12. THIS REPAIR IS CATEGORY A NOT FURTHER ACTION OR INSPECTION ADDITIONAL REQUIRED. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED PERMANENT REPAIR LOCATED BS 312 BTW RBL 6 TO LBL 29 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-12 REPAIR 12. THIS REPAIR IS CATEGORY A NOT FURTHER ACTION OR INSPECTION ADDITIONAL REQUIRED. SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 RBL 4 AT FWD GALLEY AREA 2023-530687<[01] REPLACED INTERCOSTAL WEB FLOOR STRUCTURE LOC BTW BS 277 TO BS 294.5 RBL 4 AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 STEP 9 AND DRAWING 141A5410 SHEET 3 REV A. ; SEE INDIVIDUAL SIGNOFFS BELOW;[02] RII COMPLETED JOB

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTWNBS 294.5 TO BS 312 RBL 36 AT FWD GALLEY AREA 2023-530685<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 294.5 TO BS 312 RBL 36 AT FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 33 REV - ;SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 294.5 TO BS 312 RBL 36 AT FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 33 REV - ;SEE INDIVIDUAL SIGN OFF BELOW ITEM RII

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CRACK ON FRAME LOCATED BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA 2023-530704<[01] REPAIRED FRAME LOCATED BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA IAW EA# M-22-153-01244 REV:2; SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPAIRED FRAME LOCATED BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA IAW EA# M-22-153-01244 REV:2; SEE INDIVIDUAL SIGNOFFS BELOW.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 15 AT FWD GALLEY AREA 2023-530697<[01] REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 RBL 15 AT FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 13 REV -SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1 REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 RBL 15 AT FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 13 REV -SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 RBL 15 AT FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 13 REV -SEE INDIVIDUAL SIGN OFF BELOW COMPLETED RII

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CORROSION ON SUPPORT ANGLE LOCATED BTW BS 312 TO BS 344 AT LEVEL STR 17L AT FWD GALLEY AREA 2023-530691<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 312 TO BS 344 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM:51-10-02 Ï¿½TEM 9 AND DWG: 141A8110 SHEET 11 REV - SEE INDIVIDUAL SING OF BELOW;[02] REPLACED SUPPORT ANGLE LOCATED BTW BS 312 TO BS 344 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM:51-10-02 Ï¿½TEM 9 AND DWG: 141A8110 SHEET 11 REV - SEE INDIVIDUAL SING OF BELOW

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CORROSION ON INNER CHORD LOCATED BTW BS 312 TO BS 344 AT LEVEL STR 17L WL 208.1 LBL 59 AT FWD GALLEY AREA 2023-530681<[01] REPLACED INNER CHORD LOCATED BTW BS 277 TO BS 360 AT LEVEL STR 17L WL 208.1 LBL 59 AT FWD GALLEY AREA IAW B737-700 SRM:51-10-02 Ï¿½TEM 9 AND DWG: 141A8110 SHEET 11 REV_ SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED INNER CHORD LOCATED BTW BS 277 TO BS 360 AT LEVEL STR 17L WL 208.1 LBL 59 AT FWD GALLEY AREA IAW B737-700 SRM:51-10-02 Ï¿½TEM 9 AND DWG: 141A8110 SHEET 11 REV_ SEE INDIVIDUAL SING OFF BELOW.<BR>RII

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CORROSION ON FLOOR BEAM LOCATED BS 986.5 RBL 35 WL 208.1 AT AFT GALLEY AREA 2023-530639<[01] TOOL USED: ULTRASONIC GAGE; P/N: 45MG; S/N: 221861811; DUE DATE: 08-NOV-23;[02] REFER TO FAULT TTG8Q00MX0TT; WHERE EA 23-153-02643 WAS ADDED AS A SUBTASK.;[03] REFER TO FAULT TTG8Q00MX0TT; WHERE EA 23-153-02643 WAS ADDED AS A SUBTASK.

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA 2023-530671<[01] REPLACED INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 AND DRAWING 141A5400 REV-; SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 AND DRAWING 141A5400 REV- RII<BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA 2023-530675<[01] REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AND FASTENERS IAW B737-700 SRM 51-40-02<BR>AND DWG 141A5400 SHEET 44 REV -SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTIVE STEP 1: REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL 46.5 AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV -SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED BY NEW WEB - INTERCOSTAL ON FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL 46.5 AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV -<BR><BR>RII<BR><BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: STRUCTURE — CORRODED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CORROSION ON INNER CHORD LOCATED BTW BS 312 TO BS 344 AT LEVEL STR 17R WL 208.1 RBL 59 AT FWD GALLEY AREA 2023-530683<[01] REPLACED INNER CHORD LOCATED BETWEEN BS259.50 TO BS360 RBL59 WL208.1 AT FWD GALLEY AREA. I.A.W SRM B737-700 51-40-02 AND DRAWING #140A9810 REV ?.SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED INNER CHORD LOCATED BETWEEN BS259.50 TO BS360 RBL59 WL208.1 AT FWD GALLEY AREA. I.A.W SRM B737-700 51-40-02 AND DRAWING #140A9810 REV ?.SEE INDIVIDUAL SIGN OFFS BELOW<BR>RII

Part: BRACKET — WORN (GIRT BAR) · airframe 59,279 hrs · 35,528 cycles

WEAR HARDWARE ON FWD ENTRY AND GALLEY GIRT BAR FLOOR BRACKETS AT FWD GALLEY AREA 2023-530621<[01] REPLACED HARDWARE ON FWD ENTRY AND GALLEY GIRT BAR FLOOR BRACKETS AT FWD GALLEY AREA IAW SOPM20-50-01;REV.38;[02] REPLACED HARDWARE ON FWD ENTRY AND GALLEY GIRT BAR FLOOR BRACKETS AT FWD GALLEY AREA IAW SOPM20-50-01;REV.38

Part: PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CRACK PLATE FLOOR PANEL 140CF FWD CUTOUT AFT CARGO COMPARTMENT 2023-530584<[01] REPLACED PLATE FLOOR PANEL 140CF FWD CUTOUT AFT CARGO COMPARTMENT AND TOOK MEASURE OF CRACK IS L: 1.852 TOOL USED CALIPER: P/N: 500-752-20 S/N: B21037208 DUE DATE: 04/MAR/24 IAW B737-700 SRM 51-10-02 STEP 9;[02] COMPLETE TASK CERTIFIED

Part: BRACKET — WORN (GIRT BAR) · airframe 59,279 hrs · 35,528 cycles

WEAR HARDWARE ON AFT ENTRY AND GALLEY GIRT BAR FLOOR BRACKETS AT AFT GALLEY AREA 2023-530586<[01] REPLACED HARDWARE ON AFT ENTRY AND GALLEY GIRT BAR FLOOR BRACKETS AT AFT GALLEY AREA I.A.W. BOEING SOPM 20-50-01 REV. 38;[02] TASK COMPLETED

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2023-530587<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W B737-700 AMM 33-51-15-400-802

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 59,279 hrs · 35,528 cycles

CRACK PLATE FLOOR PANEL 140CF AFT CUTOUT AFT CARGO COMPARTMENT 2023-530585<[01] REPLACED PLATE FLOOR PANEL 140CF FWD CUTOUT AFT CARGO COMPARTMENT AND TOOK MEASURE OF CRACK IS L: 1.465 TOOL USED CALIPER: P/N: 500-752-20 S/N: B21037208 DUE DATE: 04/MAR/24 IAW B737-700 SRM 51-10-02 STEP 9;[02] COMPLETE TASK CERTIFIED

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CORROSION ON FLOOR BEAM LOCATED BS 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2023-530610<[01] TOOL USED: ULTRASONIC GAGE; P/N: 45MG; S/N: 221861811; DUE DATE: 08-NOV-23;[02] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[04] REPAIRED FLOOR BEAM BS 986.5 LBL 43; WL 208.1 AT IAW B737-700 SRM-53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4 FIG. 205. SEE INDIVIDUAL SIGN-OFF BELOW.;[05] REPAIRED FLOOR BEAM BS 986.5 LBL 43; WL 208.1 AT IAW B737-700 SRM-53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4 FIG. 205. SEE INDIVIDUAL SIGN-OFF BELOW. RII CERTIFIED

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 59,279 hrs · 35,528 cycles

CORROSION ON FLOOR BEAM 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2023-530609<[01] TOOL USED: ULTRASONIC GAGE; P/N: 45MG; S/N: 221861811; DUE DATE: 08-NOV-23;[02] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 38DLPLUS; S/N: 120398603; CAL DUE DATE: 07-NOV-23;[03] REPAIRED ON FLOOR BEAM 986.5 BTW RBL 30.00 & RBL 50.00 AND AT WL 208.1 IAW B737-700 EA: 23-153-02643; SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED ON FLOOR BEAM 986.5 BTW RBL 30.00 & RBL 50.00 AND AT WL 208.1 IAW B737-700 EA: 23-153-02643; SEE INDIVIDUAL SIGN OFF BELOW.

Part: HOOK — OUT OF ADJUST (ZN 800 DOOR) · airframe 58,158 hrs · 34,795 cycles

FLIGHT ATTENDANT REPORTS THE J-HOOK ON THE SLIDE BUSTLE OF THR AFT ENTRY DOOR IS LOOSE<[01] ADJUSTED AFT J-HOOK ON L/H ENRTY DOOR SLIDE IAW SIP OPS CHECK GOOD.

Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 58,156 hrs · 34,794 cycles

L2 DOOR SLIDE CAME OUT OF CONTAINER<[01] REPACK L2 DOOR SLIDE PER AMM 25-66-01. A/C OK FOR SERVICE

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 57,729 hrs · 34,495 cycles

DOT A24-10 LH VAPOR BARRIER CRACKED AT STATION 663; LBL 28 JUST OUTBOARD OF WIRE FEED THROUGH.<[01] EVALUATED CRACK ON L/H 663 VAPOR BARRIER. FOUND AN 18' LONG CRACK AT LBL 25.00 TO BE REPAIRABLE. IAW B737-700 SRM 57-10-10-2R-2 PAR 1A& NOTE. CLEAN AND PREP AREA FOR REPAIR. IAW B737-700 SRM 51-70-04-2R-10 PAR 4A-C. VERIFY MATERIALS AS: BMS 8-301 (A148401); BMS 9-3 (A150508). IAW B737-700 SRM 51-70-04-2R -0 REP GEN TABLE 203. NEED OK TO BOND.;[02] VERIFIED ITEM 1<BR>OK TO BOND;[03] BONDED REPAIR. IAW B737-700 SRM 51-70-04-2R-10 PAR 4 D-G. AAR OVEN 30347 200DEG.;[04] VERIFIED STEP 3;[05] OK TO PRIME AND PAINT REPAIR AREA;[06] APPLIED FINISH TO THE REPAIR AREA IAW SRM 51-70-04-2R-0;[07] VEVERIFIED STEP 6<BR>AUDIT CW

Part: FLOOR PANEL — DAMAGED (ZN 200 FUS TOP) · airframe 57,729 hrs · 34,495 cycles

A-204 DOT #20 FLOOR PANEL 232SF; UPPER SURFACE HAS PREVIOUS REPAIRS AT 2EA LOCATIONS REPAIR LAYERS TORN.<[01] EVALED UPPER SURFACE OF FLOOR PANEL 232SF. FOUND IN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SURFACE OF FLOOR PANEL 232SF FOR WET LAY-UP IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-J);[03] VERIFIED MATERIALS FOR WET LAY-UP REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 232SF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 TABLE 201<BR><BR>FABRIC BMS 9-3 TY H3 (A162523)<BR>RESIN BMS 8-201 TY IV (A162416)<BR>POTTING COMPOUND BMS 5-28 TY 19 (A153169);[04] VERIFIED STEPS 1; 2 & 3;[05] OK GIVEN TO BOND;[06] BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 232SF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (K-O)<BR>REPAIR COMPLETE;[07] VERIFIED ITEM 6;[08] AUDIT C/W

Part: FLOOR PANEL — DAMAGED (ZN 200 FUS TOP) · airframe 57,729 hrs · 34,495 cycles

A-204 DOT #23. FLOOR PANEL 231XF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] EVALED UPPER SURFACE OF FLOOR PANEL 231XF. FOUND IN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SURFACE OF FLOOR PANEL 231XF FOR WET LAY-UP IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-J);[03] VERIFIED MATERIALS FOR WET LAY-UP REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231XF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 TABLE 201<BR><BR>FABRIC BMS 9-3 TY H3 (A162523)<BR>RESIN BMS 8-201 TY IV (A162416)<BR>POTTING COMPOUND BMS 5-28 TY 19 (A153169);[04] VERIFIED STEPS 1; 2 & 3;[05] OK GIVEN TO BOND;[06] BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231XF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (K-O)<BR>REPAIR COMPLETE;[07] VERIFIED ITEM 6;[08] AUDIT C/W

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 57,729 hrs · 34,495 cycles

A-204 DOT #21 FLOOR PANEL 232SF; LOWER SURFACE HAS DELAMINATION AROUND INSERT HOLE WITH SPLITTING FIBERS ON O/B SIDE. APPROX 60' FROM FWD SIDE<[01] EVALED LOWER SURFACE OF FLOOR PANEL 232SF. FOUND IN REPAIR LIMITS OF B737-700 SRM 53-00-50-2R-7 REPAIR 7;[02] PREPPED LOWER SURFACE OF FLOOR PANEL 232SF FOR WET LAY-UP REPAIR PLIES IAW B737-700 SRM 53-00-50-2R-7 REPAIR 7 STEPS 3 (A-E);[03] VERIFIED MATERIALS FOR WET LAY-UP REPAIR BOND TO LOWER SURFACE OF FLOOR PANEL 232SF IAW B737-700 SRM 53-00-50-2R-7 REPAIR 7 TABLE 201<BR><BR>FABRIC BMS 9-3 TY H3 (A162523)<BR>RESIN BMS 8-201 TY IV (A156917)<BR>POTTING COMPOUND BMS 5-28 TY 19 (A153169);[04] VERIFIED STEP 1; 2 & 3;[05] OK GIVEN TO BOND;[06] BONDED REPAIR PLIES TO LOWER SURFACE OF FLOOR PANEL 232SF IAW B737-700 SRM 53-00-50-2R-7 REPAIR 7 STEPS 3 (F-J)<BR>REPAIR COMPLETE;[07] JOB COMPLETE; AUDIT C/W

Part: FLOOR PANEL — DAMAGED (ZN 200 FUS TOP) · airframe 57,729 hrs · 34,495 cycles

A-204 DOT #29. FLOOR PANEL 241BF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] EVALED UPPER SURFACE OF FLOOR PANEL 241BF. FOUND IN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SURFACE OF FLOOR PANEL 241BF FOR WET LAY-UP IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-J);[03] VERIFIED MATERIALS FOR WET LAY-UP REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 241BF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 TABLE 201<BR><BR>RESIN BMS 8-201 TY IV (A159478)<BR>FABRIC BMS 9-3 TY H3 (A162523)<BR>POTTING COMPOUND BMS 5-28 (A153169);[04] VERIFIED STEPS 1; 2; & 3;[05] OK TO BOND GIVEN;[06] BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 241BF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (K-O)<BR>REPAIRS COMPLETE;[07] JOB COMPLETE; AUDIT C/W

Part: FLOOR PANEL — DAMAGED (ZN 200 FUS TOP) · airframe 57,729 hrs · 34,495 cycles

A-204 DOT #30. FLOOR PANEL 241BF; UPPER FACE SHEET PREVIOUS REPAIR HAS LAYERS OF FIBERS TORN OFF.<[01] EVALED UPPER SURFACE OF FLOOR PANEL 241BF. FOUND IN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SURFACE OF FLOOR PANEL 241BF FOR WET LAY-UP IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-J);[03] VERIFIED MATERIALS FOR WET LAY-UP REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 241BF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 TABLE 201<BR><BR>RESIN BMS 8-201 TY IV (A159478)<BR>FABRIC BMS 9-3 TY H3 (A162523)<BR>POTTING COMPOUND BMS 5-28 (A153169);[04] VERIFIED STEPS 1; 2; & 3;[05] OK TO BOND GIVEN;[06] BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 241BF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (K-O)<BR>REPAIRS COMPLETE;[07] JOB COMPLETE; AUDIT C/W

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 57,729 hrs · 34,495 cycles

A-204 DOT #24. FLOOR PANEL 231XF; CENTER ROW OF INSERTS HAS DELAMINATION AROUND INSERT LOCATION AT 9 EA LOCATIONS (MARKED IN BLACK)<[01] EVALED UPPER SURFACE OF FLOOR PANEL 231XF. FOUND WITHIN REPAIR LIMITS OF B737-700 SRM 53-00-50-2R-8;[02] PREPPED UPPER SURFACE OF FLOOR PANEL 231XF AROUND CENTER ROW INSERTS FOR RESIN INJECTION IAW B737-700 SRM 53-00-50-2R-8 STEPS 3 (A-D);[03] VERIFIED MATERIALS FOR UPPER SURFACE REPAIR OF FLOOR PANEL 231XF IAW B737-700 SRM 53-00-50-2R-8 REPAIR 8 TABLE 201<BR><BR>RESIN BMS 8-201 TY IV (A162416);[04] VERIFIED STEPS 1; 2 & 3;[05] OK GIVEN TO BOND;[06] INJECTED BMS 8-201 TY IV RESIN IN TO DELAM AREAS ON UPPER SURFACE OF FLOOR PANEL 231XF IAW B737-700 SRM 53-00-50-2R-8 STEPS 3 (E-J)<BR>REPAIR COMPLETE;[07] VERIFIED ITEM 6;[08] AUDIT C/W

Part: FLOOR PANEL — DAMAGED (ZN 200 FUS TOP) · airframe 57,729 hrs · 34,495 cycles

A-204 DOT #31. FLOOR PANEL 231YF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] EVALED UPPER SURFACE OF FLOOR PANEL 231YF. FOUND IN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SURFACE OF FLOOR PANEL 231YF FOR WET LAY-UP IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-J);[03] VERIFIED MATERIALS FOR WET LAY-UP REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231YF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 TABLE 201<BR><BR>RESIN BMS 8-201 TY IV (A159478)<BR>FABRIC BMS 9-3 TY H3 (A162523)<BR>POTTING COMPOUND BMS 5-28 (A153169);[04] VERIFIED STEPS 1; 2; & 3;[05] OK TO BOND GIVEN;[06] BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231YF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (K-O)<BR>REPAIRS COMPLETE;[07] JOB COMPLETE; AUDIT C/W

Part: FLOOR PANEL — DAMAGED (ZN 200 FUS TOP) · airframe 57,729 hrs · 34,495 cycles

A-204 DOT #26. FLOOR PANEL 241AF; UPPER FACE SHEET HAS MISSING FIBERS<[01] EVALUATED AND FOUND MISSING FIBERS ALONG FULL LENGTH OF BOARD. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. RESIN (A156918); FIBERGLASS (A150508).<BR><BR>REQUEST OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (AAR 30347 EXP 4-30-23). TAP TEST GOOD.;[04] REPAIRED FLOOR PANEL 241AF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3 & 4; JOB COMPLETE; AUDIT C/W

Part: FLOOR PANEL — DAMAGED (ZN 200 FUS TOP) · airframe 57,729 hrs · 34,495 cycles

A-204 DOT #27. FLOOR PANEL 241AF; FWD LH CORNER HAS MISSING FACE SHEET.<[01] EVALUATED AND FOUND PLY MISSING AT FWD L/H CORNER. NO DAMAGE TO CORE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP A; C; E-F.<BR><BR>APPLIED POTTING COMPOUND IAW SRM 53-00-50-2R-1 STEP 3 G-J.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. RESIN (A156918); FIBERGLASS (A150508); POTTING COMPOUND (E145043).<BR><BR>REQUEST OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (AAR 30347 EXP 4-30-23). TAP TEST GOOD.;[04] REPAIRED FLOOR PANEL 241AF FWD L/H CORNER IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3 & 4; JOB COMPLETE; AUDIT C/W

Part: NONE — LOOSE (OVERWING EXIT) · airframe 56,657 hrs · 33,797 cycles

EXIT/SALIDA SIGN NEAR FO SIDE OVERWING EXIT DOOR IS LOOSE AND WILL NOT REMAIN ATTACHED TO SIDEWALL. / [01] INSTALLED NEW EXIT COVER AT FO SIDE AFT OF OVERWING EXIT DOOR PER A.M.M. 33-51-01

Part: NONE — OUT OF POSITION (FWD SERVICE DOOR) · airframe 56,511 hrs · 33,701 cycles

FLIGHT ATTENDANT REPORTED FWD SERVICE DOOR SLIDE GIRT BAR NEEDS ADJUSTMENT. HARD TO OPERATE / [01] ADJUSTED FWD SERVICE DOOR SLIDE GIRT BAR PER AMM 25-66-01. A/C OK FOR SERVICE.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 56,227 hrs · 33,509 cycles

L2 DOOR SLIDE APPEARS LOOSE / [01] SECURED SLIDE IN CONTAINER PER M/M 25-66-01

Part: LIGHT — INOPERATIVE · airframe 55,663 hrs · 33,141 cycles

BOTH L/H AND R/H EMERGENCY EXIT WINDOW LIGHTS INOP / [01] RELAMPED BOTH L/H AND R/H EMERGENCY EXIT WINDOW LIGHTS PER AMM 33-21-00

Part: BATTERY — FAILED (CABIN) · airframe 54,353 hrs · 32,326 cycles

SUPPLEMENTAL INFORMATION: EMERGENCY LIGHT BATTERIES FAILED CAPACITY CHECK AT LOCATION M1669 AND M1675 ; / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT LOCATION M1669 AND M1675 PER AMM 33-51-06; [02] REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT LOCATION M1669 AND M1675 PER AMM 33-51-06

Part: NONE — CRACKED (VERT. STAB.) · airframe 53,921 hrs · 32,067 cycles

CRACKED REAR SPAR LT FWD DRAG BRACE FITTING INBOARD POSITION AT VERTICAL STABILIZER. REMOVED REAR SPAR DRAG BRACE FITTING IAW SRM 51-40-02, DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM AND MUST BE REPLACED AND PERFORMED VISUAL INSPECTION ON AREA AND NO FOUND DAMAGE, MEASURE OF CRACK IS 1.234 INCH. DRILLED NEW REAR SPAR LT FWD DRAG BRACE FITTING IAW SRM 51-40-05 AND SRM 51-20-01, DRAWING 148A8200, SHEET 4, REV -. INSTALLED REAR SPAR LT FWD DRAG BRACE FITTING IAW SRM 51-40-02, AND DWG 148A8200 REV -.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

DELAMINATED FLOOR PANEL 242AF AT PASSENGER CABIN ; 2021-437395 / [19] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REP 1.; [20] JOB COMPLETED RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 241BF AT PASSENGER CABIN ; 2021-437381 / ER B737-700 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3.N; TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18185781; DUE DATE: 11/DEC/21.; [21] COMPLETED STEP 20. RII[23] REPAIRED FLOOR PANEL 241BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII

Part: NONE — CORRODED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

CORROSION WEB - INTERCOSTAL LOCATED BTW BS767 TO BS794 RBL25 AND WL156 AT AFT CARGO COMPARTMENT ; 2021-437332 / [13] REPLACED WEB-INTERCOSTAL LOCATED BTW BS767 TO BS794 RBL25 AND WL156 AT AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A0081 REV ITEM RII

Part: GUSSET — CRACKED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

CRACK GUSSET LOCATED BS 500D, S19R IN FWD CARGO COMPARTMENT. REMOVED GUSSET IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND ADDITIONAL DAMAGE. CRACK LENGTH IS: 0.496 INCHES. REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMEN IAW B737-700 SRM 51-40-02; SRM 51-10-02 TEM 9 AND DRAWING 143A7902 SHEET:174 REV-.

Part: NONE — CORRODED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS 767 RBL25 AND WL156 AT AFT CARGO COMPARTMENT ; 2021-437333 / [19] REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS 767 RBL25 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG # 146A7500 REV. A. MATERIAL USED: BAC1496-377 7075-T62 PO# 2021-152049; [20] STEP 18 COMPLETED; [21] STEP 18 COMPLETED <BR>RII; [22] JOB CERTIFIED RII.

Part: NONE — CORRODED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

CORROSION LOWER SILL LOCATED BS794 TO BS847 RBL24 AND WL156 AT AFT CARGO COMPARTMENT ; 2021-437329 / [13] REPLACED LOWER SILL LOCATED BS 794 TO BS 847 RBL 24 AND WL 156 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A8340 SHEET 21 REV-; [14] RII; STEPS 12 & 13 COMPLETED. <BR>CERTIFIED RII WORK PERFORMED.

Part: NONE — CRACKED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

CRACK ANGLE SUPPORT LOCATED BS 867, S26L IN AFT CARGO. REMOVED ANGLE SUPPORT IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AREA AND NOT FOUND MORE DAMAGE. ANGLE MUST BE REPLACED DUE NOT FOUND ALLOWABLE DAMAGE LIMIT IN SRM. CRACK LENGTH IS: 0.500 INCHES. DRILLED NEW ANGLE SUPPORT IAW SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT ON OPENED HOLES IAW SRM 51-20-01. INSTALLED A NEW ANGLE SUPPORT LOCATED BS867 AND STR26L AT AFT CARGO COMPARTMENT IAW SRM 51-40- 02.; [06] REPLACED ANGLE SUPPORT LOCATED BS867 AND STR26L AT AFT CARGO COMPARTMENT IAW SRM 51-40- 02 AND SRM 51-10-02 ITEM 9. COMPLETE STEP 5 & 6. CERTIFIED WORK PERFORMED.

Part: NONE — CORRODED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

SUPPLEMENTAL INFORMATION: CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS847 LBL24 AND WL156 AT AFT CARGO COMPARTMENT ; 2021-437334 / [24] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS847 LBL24 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG # 146A7500 REV. A. MATERIAL USED: BAC1496-377 7075-T62 P.O#2021-152049; [25] STEP 23 COMPLETED <BR>RII; [26] JOB COMPLETE RII.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

CRACK STRINGER 26L LOCATED BS 540 AT FWD CARGO COMPARTMENT ; 2021-437311 / [19] INSTALLED REPAIR PARTS STRINGER SECTION (1EA); ANGLE (2EA) AND CHANNEL (1EA) LOCATED AT STR26L AND BTW BS500D + 10 TO BS540 AT FWD CARGO COMPARTMENT AND FASTENERS IAW SRM B737-700 51-40-02 AND 53-00-03-2R-1 REPAIR 1 FIG 206; [20] CERTIFIED STEP 19 RII; [21] PERFORMED PERMANENT REPAIR ON STR26L AND BTW BS500D + 10 TO BS540. AT FWD CARGO COMPARTMENT IAW B737-700 53-00-03-2R-1 REPAIR 1; FIG 206.; [22] PERFORMED PERMANENT REPAIR ON STR26L AND BTW BS500D + 10 TO BS540. AT FWD CARGO COMPARTMENT IAW B737-700 53-00-03-2R-1 REPAIR 1; FIG 206. RII

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

CRACK STRINGER 25L LOCATED BS 540 AT FWD CARGO COMPARTMENT ; 2021-437310 / [24] REPAIRED STRINGER 25L LOCATED BTW BS500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG. 206. AND DAWING # 143A3230 REV. J.; [25] CERTIFIED STEP 23.; [26] REPAIRED STRINGER 25L LOCATED BTW BS500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG. 206. AND DAWING # 143A3230,NG,NRC,2021-10-06 08:35:32,16Y,Y,MX,0,0,,CRACK STRINGER 25L LOCATED BS 540 AT FWD CARGO COMPARTMENT ; 2021-437310"

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

CRACK STRINGER 23R LOCATED BS 540 AT FWD CARGO COMPARTMENT. ] INSTALLED REPAIR TO STRINGER SECTION, ANGLE (2EA) AND CHANNEL (1EA) AND TIE CLIP AND SHEAR TIE AND FASTENERS IAW SRM 51-40-02 AND 53-00-03-2R-1, REPAIR 1, FIG 206, AND DWG 143A1225, SHEET, NG, NRC.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

CRACK SUPPORT ANGLE LOCATED BS695 AND BL0 AT PASSENGER CABIN ; 2021-437288 / [15] REPLACED SUPPORT ANGLE LOCATED BS695 AND BL0 AT PASSENGER IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 DRAWING # 273A9111 REV -. MATERIAL: P/N: 7075-T0/0.050 INCH (BAC1490-2883) PO: 2021-163767. RII <BR>TASK COMPLETED

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,921 hrs · 32,067 cycles

CORROSION SEAT TRACK LOCATED BS520 LBL45.50 WL208.1 AT PASSENGER CABIN ; 2021-437284 / [21] OK TO INSTALL REPAIR PARTS: [1] SEAT TRACK SECTION; [2] REPAIR CHANNEL ON REPAIR AREA LOCATED BTW BS500C TO BS520 AND LBL45.50; WL208.1 AND FASTENERS.; [22] STEP 21 COMPLETED. <BR>OK TO INSTALL GRANTED. RII; [23] INSTALLED REPAIR PARTS: [1] SEAT TRACK SECTION; [2] REPAIR CHANNEL ON REPAIR AREA LOCATED BTW BS500C TO BS520 AND LBL45.50; WL208.1 AND FASTENERS IAW B737-700 SRM 51-40-02 AND SRM 53-00-52-2R-4 REPAIR 4.

Part: NONE — CORRODED (VERT. STAB.) · airframe 53,921 hrs · 32,067 cycles

CORROSION REAR SPAR LT DRAG BRACE FITTING AT AFT INBD POSITION OF VERTICAL STABILIZER, REMOVED REAR SPAR LH DRAG BRACE FITTING IAW SRM 51-40-02. PERFORMED A VISUAL INSPECTION OF AREA AND NO FOUND DAMAGE. DRILLED A NEW REAR SPAR LT DRAG BRACE FITTING IAW SRM 51-40-05, AND DRAWING 148A8200, SHEET 4, REV -. INSTALLED REAR SPAR LH DRAG BRACE FITTING IAW DWG 148A8200 REV -, AND SRM 51-40-02.

Part: NONE — CORRODED (VERT. STAB.) · airframe 53,921 hrs · 32,067 cycles

CORROSION REAR SPAR LH DRAG BRACE FITTING AT FWD O/B POSITION AT VERTICAL STABILIZER ; 2021-437292 / [07] INSTALLED NEW REAR SPAR LH DRAG BRACE FITTING AT FWD O/B POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING # 148A8200 SHEET 4 REV -; [08] RII; STEP 7 COMPLETED.; [09] VERIFIED AFFECTED PART NUMBER IS 148A8220-13 IAW B737-700 DWG 148A8200 REV -; [10] REPLACED REAR SPAR LH DRAG BRACE FITTING AT FWD O/B POSITION AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 TEM 9 ; 51-40-02 AND DWG 148A8200 REV -; [11] RII; STEP 9 & 10 COMPLETED. <BR>CERTIFIED RII WORK PERFORMED.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 53,921 hrs · 32,067 cycles

CRACK LEADING EDGE RIB LOC. LE STA 161.04 AT LT HORIZONTAL STABILIZER. REMOVED L/E RIB IAW SRM 51-40-02 & PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND DAMAGE. COMPLETED DRILLED NEW L/E RIB IAW SRM 51-40-05 & APPLIED PROTECTIVE TREATMENT ON OPENED HOLES IAW SRM 51-20-01. INSTALLED NEW L/E RIB AND FASTENER IAW SRM 51-40-02 & DRAWING 186A1001 REV A.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 53,921 hrs · 32,067 cycles

CRACK LEADING EDGE RIB LOC. LE STA 105.26. AT LT HORIZONTAL STABILIZER. REMOVED LEADING EDGE RIB LOC. LE STA 105.26. AT LT HORIZONTAL STABILIZER IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND DAMAGE. STEP 1 COMPLETED DRILLED NEW CHORD RIB IAW SRM B737-700 51-40-05 AND APPLIED PROTECTIVE TREATMENT IAW SRM 51-20-01. OK TO INSTALL NEW CHORD RIB AND FASTENERS STEP 3 COMPLETE.. RII ITEM OK TO INSTALL NEW CHORD RIB AND FASTENERS GRANTED STEP 4 COMPLETE.. RII ITEM INSTALLED NEW CHORD RIB AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 186A1001 SHEET 10 REV. A REPLACED CHORD RIB AND FASTENERS IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 186A1001 SHEET 10 REV. A STEP 7 AND 8.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 53,921 hrs · 32,067 cycles

CRACK LEADING EDGE RIB LOC. LE STA 114.55 AT LT HORIZONTAL STABILIZER. REMOVED LEADING EDGE RIB LOC. LE STA 114.55 AT LT HORIZONTAL STAB IAW SRM 51-40-02 & PERFORMED VISUAL INSP ON AREA & NOT FOUND DAMAGE. DRILLED NEW LEADING EDGE RIB IAW SRM 51-40-05 & APPLIED PROTECTIVE TREATMENT ON OPENED HOLES IAW SRM 51-20-01. INSTALLED NEW LEADING EDGE RIB AND FASTENER IAW SRM 51-40-02 & DWG 186A1001 REV A. REPLACED L/E RIB IAW SRM 51-10-02 SRM 51-40-02 & DRAWING # 186A1001 REV A.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 53,243 hrs · 31,665 cycles

EMERGENCY LIGHT BATTERY PACK M1668 INOP ; / [01] R&R THE L/H CABIN EMERGENCY LIGHT BATTERY PACK M1668; OPS CK GOOD REF 33-51-06.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 52,515 hrs · 31,249 cycles

LH AFT ENTRY EXTERIOR EMERGENCY LIGHT IS OUT / RELAMPED LH AFT ENTRY EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 52,392 hrs · 31,180 cycles

194E PANEL HAS 35 FASTENER HOLES COUNTER SINKS SEVERELY WORN 6 ELONGATED. R&R'D 194E PANEL REF 5351-I-14642-NG AND AMM 53-51-21.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 52,392 hrs · 31,180 cycles

193D PANEL HAS DELAM WITH PITTING; MEASURING 4'X 1 1/2' OF AFT SIDE; MIDDLE OF PANEL / DRILLED AND COUNTER SUNK NEW 193D PANEL REF SRM 51-40-05

Part: PANEL — ELONGATED (FUSELAGE) · airframe 52,392 hrs · 31,180 cycles

193D PANEL HAS 27 FASTENER HOLES COUNTER SINKS SEVERELY WORN AND ELONGATED. / DRILLED AND COUNTER SUNK NEW 193D PANEL REF SRM 51-40-05

Part: PANEL — CHAFED (FUSELAGE) · airframe 52,392 hrs · 31,180 cycles

SEVERE WEAR/CHAFEING ON AFT SIDE OF 193D PANEL / DRILL AND COUNTER SUNK NEW 193D PANEL REF SRM 51-40-05

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 50,262 hrs · 29,905 cycles

AFT SERVICEDOOR SLIDE HOUSING DRAGS ON FLOOR DURING DOOR OPERATION / REMOVED AND REPOSITIONED SLIDE IN CONTAINER PER MT 725-61-06

Part: SIGN — DETACHED (RT CABIN) · airframe 48,853 hrs · 29,009 cycles

R/H SIDE OVER WING EXIT, EXIT SIGN FELL OFF. / SECURED EXIT SIGN IAW AMM.

Part: STUB FRAME — CRACKED (R1 DOOR) · airframe 48,770 hrs · 28,961 cycles

R1 DOOR FORWARD UPPER STUB FRAME CRACKED IN THE RADIUS. R&R STUB FRAME IAW DWG AND SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 48,770 hrs · 28,961 cycles

AFT CARGO DOOR; AFT CORNER SCUFF PLATE IS CRACKED IN 2 LOCATIONS / AFT CARGO AFT CORNER SCUFF PLATE REPAIRED ON WO# 39996-8300-0001 AND EA 1-A53-2076 REV 11.

Part: FITTING — CRACKED (R1 DOOR) · airframe 48,770 hrs · 28,961 cycles

R1 DOOR UPPER HINGE ARM FITTING OF FUSELAGE SIDE BENT AND CRACKED. R&R FITTING IAW DWG.

Part: PANEL — CORRODED (FUSELAGE) · airframe 48,770 hrs · 28,961 cycles

NOSE WHEEL WELL PANEL 113BW HAS CORROSION AROUND FASTNER HOLES ON INNER SURFACE / VERIFIED NEW NOSE WHEEL WELL PANEL PART NUMBERS 141A7900-4 IAW AIPC 32-22-11-02; RECEIVED. ATAG WN5738. EVALUATED CORROSION. NO ALLOWABLE DAMAGE LIMITS PUBLISHED. REMOVED AND REPLACED PANEL 113BW ON SHELF PANEL TO BE INSTALLED ON J PANEL-115-CLOSE

Part: BRACKET — CRACKED (L/H FUSELAGE) · airframe 48,770 hrs · 28,961 cycles

LH STA 663 VAPOR BARRIER BULKHEAD BRACKET CRACKED AT LBL 45. / REMOVED AND REPLACED LH STA 663 VAPOR BARRIER BULKHEAD BRACKET P/N 276A9183-5 IAW DWG 111A1000 REV F AND B-737 SRM 51-40-02-0G-0 STEP 7.D. ATAG_A37649

Part: SUPPORT — CRACKED (L/H VERT. STAB.) · airframe 48,770 hrs · 28,961 cycles

EXTERNAL FUSELAGE; STA 1016; 8' ABOVE LH VERTICAL STAB ATTACH LUG. LONGITUDINAL SUPPORT IS CRACKED IN RADIUS / REMOVED AND REPLACED LONGITUDINAL SUPPORT ABOVE LH VERTICAL ATTACH LUG STA 1016 IAW SRM 51-40-02-0G-0 AND BOEING DWG 176A3101 REV B

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 48,770 hrs · 28,961 cycles

FWD CARGO DOOR CUT-OUT AFT CORNER SCUFF PLATE CRACKED. / FWD CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED. REMOVED CRACKED SCUFF PLATE ON CUSTOMED CARD J753-646-62-01. SENT SCUFF PLATE TO BACK SHOP FOR WELDING. BACKSHOP REPAIRED BROKE SCUFF PLATE IAW SWA EA: 1-A53-2076 REV 11 WILL INSTALL REPAIRED SCUFF PLAT ON CUSTOMER CARD J753-646-63-01

Part: PLATE — CRACKED (LT WING) · airframe 48,770 hrs · 28,961 cycles

L/H WING LOWER SURFACE PANEL # 551GB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: PLATE — CRACKED (R/H WING) · airframe 48,770 hrs · 28,961 cycles

RH WING REAR SPAR; 9' I/B OF #6 FLAP TRACK; LOWER PANEL ATTACH PLATE IS CRACKED AT O/B FASTNER HOLE / RH WING REAR SPAR; 9' IB OF #6 FLAPTRACK LOWER PANEL ATTACH PLATE CRAKED AT OB FASTENER HOLE REMOVED CRACKED (PLATE) IAW SRM 51-40-02-0G-0 AND REPLACED WITH NEW (PLATE) IAW SRM 51-40-02-0G-0 AND IAW BOEING DWG# 115A2781 REV B ATAG QT0042

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,770 hrs · 28,961 cycles

CABIN FLOOR PANEL 241BF, AFT INBOARD CORNER, DELAMINATED DAMAGE. R&R THE FLOOR PANEL IAW SRM & DWG.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,770 hrs · 28,961 cycles

RIGHT HORIZONTAL STABILIZER RIB ASSEMBLY NR 3 STAB. STA. 111.10, 3RD STIFFENER FROM FORWARD END CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,770 hrs · 28,961 cycles

INTERNAL R/H HORIZONTAL STABILIZER, RIB ASSEMBLY NR 5 STAB. STA. 129.50, 2ND STIFFENER FROM FORWARD END CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,770 hrs · 28,961 cycles

INTERNAL L/H HORIZONTAL STABILIZER, RIB ASSEMBLY NR 6 STAB. STA. 138.70, 1ST STIFFENER FROM FORWARD END CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,770 hrs · 28,961 cycles

INTERNAL L/H HORIZONTAL STABILIZER RIB ASSEMBLY NR 5, STAB. STA. 129.50, 2ND STIFFENER FROM FORWARD END CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,770 hrs · 28,961 cycles

INTERNAL L/H HORIZONTAL STABILIZER, RIB ASSEMBLY #5, STAB. STA. 129.50, 4TH STIFFENER FROM FORWARD END CRACKED AT LOWER END. / REPAIRED STIFFENER IAW SRM.

Part: LAMP — NOT SEATED (EMERGENCY LIGHT) · airframe 48,770 hrs · 28,961 cycles

FLIGHT DECK EMERGENCY LIGHT INOP. RESEATED LIGHT LAMP IAW MM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 48,770 hrs · 28,961 cycles

L/H VAPOR BARRIER BULKHEAD CRACKED AT BS. 663. REPAIRED BULKHEAD IAW SRM.

Part: SKIN — CRACKED (RT NR 8 SLAT) · airframe 48,770 hrs · 28,961 cycles

R/H WING NR 8 LEADING EDGE SLAT NOSE SKIN CRACKED AT 2ND FASTENER FROM FORWARD ON OUTBOARD ROW OF ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 48,350 hrs · 28,673 cycles

R1 DOOR SLIDE FELL OUT OF BOX, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 48,069 hrs · 28,480 cycles

L1 DOOR EMERGENCY SLIDE LOOSE. SECURED SLIDE PER MM.

Part: NOT REPORTED — CRACKED (RT HORIZ STAB) · airframe 47,780 hrs · 28,301 cycles

RT HORIZONTAL STABILIZER CRACKED AT THE INBOARD EDGE OF STA. 184.7 AND 10" FORWARD OF THE AFT SPAR. REPAIRED STABILIZER PER EA.

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 47,780 hrs · 28,301 cycles

R/H HORIZONTAL STABILIZER HAD A 1.1" CRACK AT THE INBOARD EDGE OF STA. 184.7 AND 10" FORWARD OF THE AFT SPAR. REPAIRED STABILIZER PER EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,749 hrs · 28,283 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: CHARGER — FAILED (CABIN) · airframe 47,028 hrs · 27,831 cycles

R1 DOOR EMERGENCY LIGHTS WOULD NOT TEST. R&R BATTERY CHARGER PER AMM.

Part: LIGHT — DIM (CABIN) · airframe 46,647 hrs · 27,598 cycles

RT CABIN OVER WING HATCH BELOW EMERGENCY EXIT LIGHT VERY DIM. RE-LAMPED LIGHT PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 43,278 hrs · 25,475 cycles

EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M01673. R & R THE BATTERY PACK IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 43,278 hrs · 25,475 cycles

LEFT CABIN EMERGENCY LIGHT FOUND LOOSE AT ROW 12. SECURED THE LIGHT STRIP IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 43,278 hrs · 25,475 cycles

EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M01672. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 43,278 hrs · 25,475 cycles

EMERGENCY LIGHT BATTERY PACKS FAILED A CAPACITY CHECK AT LOCATION M01669. R & R THE BATTERY PACK IAW MM.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 43,159 hrs · 25,401 cycles

L1 DOOR SLIDE INADVERTENTLY FELL OUT OF RETAINER, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED THE SLIDE IAW MT.

Part: COVER — LOOSE (EXIT SIGN) · airframe 42,884 hrs · 25,213 cycles

RT OVERWING EXIT SIGN COVER LOOSE. R&R COVER IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 42,873 hrs · 25,207 cycles

RIGHT UPPER EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 42,845 hrs · 25,188 cycles

RT UPPER EMERGENCY EXIT LIGHT LENS COVER MISSING. R&R LENS IAW AMM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 42,437 hrs · 24,938 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. R & R THE BATTERY CHARGER IAW MM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

AFT CARGO COMPARTMENT BULKHEAD BRACKET ASSEMBLY CRACKED AT BS 727. R&R BRACKET ASSEMBLY IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

AFT CARGO Z ANGLE CORRODED BETWEEN BS 727C TO BS 747+10, LBL 22. R&R Z ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (AFT CARGO BAY) · airframe 42,011 hrs · 24,676 cycles

AFT CARGO AFT BLKD SUPPORT ANGLE CORRODED BS 947 RBL 22' .MARKED / BLENDED CORROSION FROM BS 947 RBL 22' AFT CARGO AFT BULK HEAD SUPPORT ANGLE IAW SRM 53-00-53-1A-2 ORIGINAL THICKNESS 0.080' LOSS 0.012' REMAINING 0.068' OUT OF LIMITS IAW SRM 53-00-53-1A-2 AAR TOOL NO 38290 CAL DUE 10-19-17 REMOVED AND REPLACED AFT BULK HEAD ANGLE P/N 149A8118-27 IAW SRM 51-40-02-0G-0 AND BOEING DWG 149A8118 REV B

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 42,011 hrs · 24,676 cycles

AFT CARGO T CHORD FLOOR STRAP HAS CORROSION AT BS 887 RBL 1' TO LBL 5' . MARKED. / REMOVED AND REPLACED AFT CARGO T CHORD FLOOR STRAP 'PANEL BREAK' AT STA 887 IAW SRM 51-40-02

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

AFT CARGO Z ANGLE CORRODED BETWEEN BS 767 TO BS 787, LBL 22. R&R Z ANGLE IAW SRM.

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 42,011 hrs · 24,676 cycles

AFT CARGO LOWER SILL WEB HAS CORROSION FROM BS 792 TO BS 847 RBL25' . MARKED. / REMOVED DAMAGE AT AFT CARGO LOWER SILL WEB IAW SRM 51-10-02-0G-0 10X VERIFIED ORG T .040 REM T .031 LOSS OF .009 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVED AND REPLACED LOWER SILL WEB IAW SRM 51-40-02-0G-0 AND DWG 146A8340 REV A

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

AFT CARGO Z ANGLE CORRODED BETWEEN BS 727C TO BS 767, RBL 22. REPAIRED Z ANGLE IAW SRM.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 42,011 hrs · 24,676 cycles

PASSENGER CABIN SEAT TRACK RBL 24 BETWEEN STA 500C AND 520 CORROSION IN BASE AND CROWN AS MARKED / BLENDED OUT CORROSION AND VERIFIED WITH A 10X MAGNIFYING GLASS ON SEAT TRACK STA 500C TO STA 520 RBL 24 I/A/W B737 SRM 51-10-02-0G-0 VERIFIED LIMITS ON TOP OF THE SEAT TRACK IS .028' MAX ALLOWABLE .020' FOUND TO BE OUT OF LIMITS I/A/W B737 SRM 53-00-52-1A-1 FIGURE 103. REPAIRED ON NRC # 36387/2700/0006 X629910

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 42,011 hrs · 24,676 cycles

.VERTICAL STABILIZER; RUDDER COUNTER BALANCE LEADING EDGE CORRODED. MARKED. / REPLACED VERTICAL STABILIZER; RUDDER COUNTER BALANCE I.A.W B737-700 CMM 55-40-09 A-TAG - GY1755

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

FORWARD SECTION OF T CAP FRAME CRACKED AT BS 520, LBL 6. REPAIRED T CAP IAW EA.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 42,011 hrs · 24,676 cycles

MAIN CABIN FLOOR PANEL #222CF HAS DELMANIATION. MARK ED WITH A DOT. / REPAIRED FLOOR PANEL #222CF UPPER SURFACE AREA I/A/ W (B737) SRM 53-00-50-2R-0 REV 62-10JUL2017; SRM 53- 00-50-2R-1 REV 62-10JUL2017 & NOTM 51-05-01 FABRIC ( A26386) RESIN(A27147)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

PASSENGER CABIN FORWARD WET AREA FLOOR INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

PASSENGER CABIN FORWARD WET AREA FLOOR INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 500D-520) · airframe 42,011 hrs · 24,676 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 500D TO 520, BL 0. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

R1 CREASE BEAM INNER CHORD ANGLE CORRODED BETWEEN BS 304 TO BS 323, RBL 59. R&R ANGLE IAW SRM AND DWG.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

AFT GIRT BAR FITTING MOUNT CORRODED AT BS 344 ON UPPER SURFACE. R&R MOUNT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

FORWARD WET AREA FLOOR INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, BL 0. R&R INTERCOSTAL IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

LT CREASE BEAM WEB CORRODED BETWEEN BS 887 TO BS 905. R&R WEB IAW DWG AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

PASSENGER CABIN FORWARD WET AREA FLOOR BEAM CORRODED AT BS 312, BETWEEN LBL 18 TO LBL 11. REPAIRED T CAP IAW SRM AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

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

Part: BRACKET — CRACKED (LT WING) · airframe 42,011 hrs · 24,676 cycles

LT WING TRAILING EDGE BRACKET CRACKED IN HALF ON INBOARD SIDE OF DEFLECTION CONTROL RIB JUST INBOARD OF NR 5 SPOILER. R&R BRACKET IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

FORWARD CARGO PIT LT BAFFLE AFT CLIP CRACKED BETWEEN BS 500B TO BS 500C. R&R CLIP IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

FORWARD CARGO PIT LT SIDE GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

AFT CARGO COMPARTMENT FLOORBEAM CORRODED BETWEEN BS 727A-3 TO BS 727A-10, LBL 3. REPAIRED FLOOR BEAM IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,011 hrs · 24,676 cycles

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

Part: SCUFF PLATE — CORRODED (FWD CARGO BAY) · airframe 42,011 hrs · 24,676 cycles

SUPPLEMENTAL INFORMATION: FORWARD CARGO PIT DOOR SURROUND AFT SHIELD STA 492 - 500A HAS CORROSION ON UPPER SURFACE AROUND FASTENER HOLES / REMOVED AND REPLACED FWD CARGO PIT DOOR SURROUNDING AFT SHIELD AT STA 492 TO STA 500A IAW BOEING DWG # 143A0080 REV: - AND B737-200 SRM 51-40-02-0G-0

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 42,011 hrs · 24,676 cycles

SUPPLEMENTAL INFORMATION: FORWARD CARGO PIT LEFT SIDE BULKHEAD CURVED ANGLE HAS CORROSION AROUND FASTENER HOLES / REMOVED AND REPLACED FWD CARGO PIT LEFT SIDE AFT BULKHEAD CURVED ANGLE IAW BOEING 737 SRM 51-40-02 AND DWG 143A9485 REV D ID 0008 ATAG XM1749

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 42,011 hrs · 24,676 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPARTMENT FLOOR PANEL 120BF UPPER SURFACE L/H EDGE HAS CORROSION. / EVALUATED DAMAGE; CORROSION LENGTH MORE THAN 3.0 INCHES FOUND TO BE OUT OF LIMITS I/A/W B737 SRM 53-00-53-1A-1 5 A. (1) (B). RECEIVED A NEW PANEL P/N 453A1610-4; A TUG WN 4495 I/A/W B737 SRM 53-30-53-01-1 AND BOEING DOCUMENT 453A1610 REV T.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 40,769 hrs · 23,961 cycles

LT MAIN WHEEL WELL FORWARD BULKHEAD VERTICAL CRACKED AT BS 663. REPAIRED BULKHEAD PER EA.

Part: COVER — LOOSE (EXIT SIGN) · airframe 39,138 hrs · 23,005 cycles

AFT GALLEY EMERGENCY EXIT SIGN COVER LOOSE. R&R COVER IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 37,111 hrs · 21,793 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M1674. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 37,111 hrs · 21,793 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M1668. R & R BATTERY IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,618 hrs · 20,944 cycles

EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY M1672 FAILED OPERATIONS TEST. R & R BATTERY PACK IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,618 hrs · 20,944 cycles

FLIGHT DECK LT NR 1 WINDOW FRAME CRACKED. REPAIRED FRAME IAW ACO.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,987 hrs · 20,561 cycles

RIGHT LOWER MID CABIN EMER LIGHT BATTERY PACK FAILED DEEP CYCLE CHECK. R & R BATTERY PACK IAW AMM.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 34,137 hrs · 20,090 cycles

DIVERSION, AFT LAVATORY SMOKE DETECTOR WENT OFF. NO FIRE OR SMOKE IN LAVATORY. R & R AFT LAVATORY SMOKE DETECTOR IAW MM.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 33,881 hrs · 19,940 cycles

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

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 33,881 hrs · 19,940 cycles

RIGHT MLG FWD TRUNNION SUPPORT FITTING LUG CORRODED. R & R FITTING IAW EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 33,881 hrs · 19,940 cycles

LEFT MLG FWD TRUNNION SUPPORT FITTING LOWER INBD LUG FACE CORRODED. REPAIRED FITTING IAW EA.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 33,881 hrs · 19,940 cycles

RIGHT MLG FWD TRUNNION SUPPORT FITTING UPPER OTBD LUG FACE CORRODED. REPAIRED FITTING IAW EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 30,380 hrs · 17,935 cycles

CEILING AFT ENTRY EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY PACK IAW TC.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 29,377 hrs · 17,354 cycles

FWD EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,745 hrs · 16,961 cycles

LT HORIZONTAL STABILIZER RIB CRACKED STAB STATION 120.3 RIB AT THIRD VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

FLOOR BOARD 222BF DELAMINATED ON LOWER SKIN AT THE AFT OTBD CORNER. REPAIRED FLOOR BOARD IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R & R INTERCOSTAL IAW DRAWING & SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, RBL 45. REPAIRED FLANGE IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

INTERCOSTAL CRACKED BETWEEN STATION 294 TO STATION 312, RBL 15. R & R INTERCOSTAL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

FUSELAGE SKIN CRACKED AT 540 CHORD 2ND FASTENER BELOW STRINGER 22L. REPAIRED SKIN IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, LBL 25. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, RBL 25. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, LBL 45. REPAIRED FLANGE IAW EA.

Part: FLOORBOARD — BROKEN (CABIN) · airframe 28,745 hrs · 16,961 cycles

CABIN FLOOR BOARD 221BF AFT OTBD CORNER BROKEN. R & R FLOOR BOARD IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

UPPER SURFACE WEB CORRODED BETWEEN BS 1014 TO BS 1029, LBL 3. R & R WEB IAW SRM & DRAWING.

Part: STRAP — CORRODED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

WEB STRAP CORRODED BETWEEN BS 1016 TO BS 1029, RBL 3. REPAIRED STRAP IAW SRM & DRAWING. .

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,745 hrs · 16,961 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STATION 129.5 AT THIRD VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

RT NR 3 WINDOW FRAME CRACKED ON 2ND FASTENER HOLE FROM BOTTOM OF E-F POST. REPAIRED FRAME IAW SI.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

AFT CARGO BAY UNDER SIDE OF INTERCOSTAL UPPER "J" FLANGE CORRODED BETWEEN STATION 827 TO STATION 839, RBL 18. R & R WEB IAW SRM & DRAWING.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN STATION 727D+5 TO STATION 777, LBL 21. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN STATION 727D+5 TO STATION 767, RBL 21. R & R SUPPORT IAW SRM & DRAWING.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 28,745 hrs · 16,961 cycles

MAIN WW VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 33.7 TO RBL 34.9. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

LT NR 3 WINDOW FRAME CRACKED ON 2ND FASTENER HOLE FROM BOTTOM OF E-F POST. REPAIRED FRAME IAW SI.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 28,745 hrs · 16,961 cycles

RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN STATION 895 TO STATION 945, RBL 21. R & R SUPPORT IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,745 hrs · 16,961 cycles

LT OVERHEAD BIN EMERGENCY LIGHT AT SEAT NR 6 INOPERATIVE. R & R BULB IAW AMM.

Part: PLATE — CRACKED (LT WING) · airframe 28,317 hrs · 16,699 cycles

LT WING AFT SPAR WIGGLE PLATE AFT OF NR 1 CRACKED. R & R PLATE IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 28,317 hrs · 16,699 cycles

LT WING AFT SPAR AFT OF NR 1 MOTOR LOWER BULB SEAL BRACKET CRACKED. R & R BRACKET IAW SRM & SIP.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 28,317 hrs · 16,699 cycles

RT WING UPPER TE PANEL SUPPORT FITTING CRACKED. R & R ANGLE IAW DRAWING & SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,302 hrs · 16,690 cycles

LT EMERGENCY EXIT LIGHT INOPERATIVE BETWEEN SEAT ROWS 6 TO ROW 7. R&R BATTERY PACK ASSEMBLY IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 28,084 hrs · 16,555 cycles

CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT BROKEN. R&R SIGN IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,150 hrs · 16,003 cycles

LEFT EMERGENCY LIGHT INOP AT ROW 12. R & R LIGHT IAW MM.

Part: LIGHT — MISSING (R2 DOOR) · airframe 26,378 hrs · 15,563 cycles

R2 DOOR EMERGENCY LIGHT MISSING. REPLACED R2 DOOR EMERGENCY LIGHT ASSY PER AMM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 26,028 hrs · 15,364 cycles

LEFT HORIZONTAL LOWER SKIN IS CRACKED APPROX 1.0", 8.5" FROM LEADING EDGE AND 0.25" I/B OF STAB STA 138.7. INSTALLED CATEGORY "B" REPAIR PER SRM 55-10-01-2R-11 REPAIR 11.

Part: GUSSET — CRACKED (VERTICAL STAB) · airframe 26,028 hrs · 15,364 cycles

VERTICAL STAB TO DORSAL FIN FRONT SPAR TERMINATION FITTING LOWER SPRING GUSSET IS CRACKED TO RADIUS ON BOTH FWD SIDES. REMOVED AND REPLACED SPRING GUSSET AS PER SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,028 hrs · 15,364 cycles

EXTERNAL POWER DOOR AFT VERTICAL CUTOUT HAS .200" CRACK BELOW PREVIOUS REPAIR. REPAIRED PER EA 1-A53-9269.

Part: LENS — CRACKED (CABIN) · airframe 24,943 hrs · 14,708 cycles

EEPLS LENS CRACKED BETWEEN ROW 11 TO ROW 23. REMOVED AND REPLACED LENS PER M/M.

Part: COVER — CRACKED (CABIN) · airframe 24,943 hrs · 14,708 cycles

EEPLS COVER CRACKED BETWEEN ROW 18 AND 20. REMOVED AND REPLACED COVER PER M/M.

Part: COVER — CRACKED (CABIN) · airframe 24,943 hrs · 14,708 cycles

LEFT EEPLS COVER CRACKED BETWEEN ROW 3 TO ROW 10. REMOVED AND REPLACED COVER PER M/M.

Part: COVER — BROKEN (CABIN) · airframe 24,036 hrs · 14,169 cycles

FORWARD EEPLS COVER BROKEN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 23,796 hrs · 14,030 cycles

EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER M/M.

Part: LENS — BROKEN (CABIN) · airframe 23,545 hrs · 13,880 cycles

LEFT EEPLS LENS BROKEN AT ROW 20. REMOVED AND REPLACED LENS PER MM.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 22,398 hrs · 13,235 cycles

AIR TURNBACK -- ON CLIMBOUT MASTER CAUTION AND FLIGHT CONTROL ILLUMINATED WITH FEEL DIFFERENTIAL PRESSURE ON OVERHEAD PANEL QUANTITIES NORMAL. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER IAW.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 22,033 hrs · 13,021 cycles

DURING SCHEDULED 6Y CHECK, FOUND VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 42. REPAIRED WEB IAW EA AND ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,033 hrs · 13,021 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT EEPLS INOP AT ROW 19. RELAMPED PER MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 22,033 hrs · 13,021 cycles

DURING SCHEDULED 6Y CHECK, FOUND WEB CORRODED AT BS 796 TO BS 847, RBL 23. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,033 hrs · 13,021 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT EEPLS INOP AT ROW 11. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 21,799 hrs · 12,885 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 2 TO ROW 10. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,799 hrs · 12,885 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 21,779 hrs · 12,885 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: CAP — LOOSE (CABIN) · airframe 21,627 hrs · 12,786 cycles

FWD EEPLS END CAP LOOSE. REMOVED AND REPLACED END CAP PER MM.

Part: LENS — LOOSE (CABIN) · airframe 21,295 hrs · 12,592 cycles

LT EEPLS LENS LOOSE AT ROW 1. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,824 hrs · 11,760 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP BETWEEN ROW 1 TO ROW 4. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 19,316 hrs · 11,478 cycles

DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 19,316 hrs · 11,478 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: STRUCTURE — CRACKED (HORIZ STAB) · airframe 18,156 hrs · 10,792 cycles

DURING SCHEDULED CV CHECK, FOUND RT HORIZONTAL STABILIZER CRACKED AT STA 138.7. REPAIRED STABILIZER PER SRM.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 16,951 hrs · 10,077 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER CLIPS OUT OF ADJUST. ADJUSTED CLIPS PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 16,733 hrs · 9,948 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 16,733 hrs · 9,948 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,976 hrs · 8,900 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,746 hrs · 8,131 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVERS CRACKED BETWEEN ROW 5 TO ROW 23. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 12,542 hrs · 7,395 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 12,542 hrs · 7,395 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 12,542 hrs · 7,395 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 12,403 hrs · 7,309 cycles

FWD EEPLS RED LENS MISSING. INSTALLED LENS ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 10,028 hrs · 5,809 cycles

R1 DOOR EMERGENCY EXIT LIGHTS INOP. FOUND LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM.

Part: COMPRESSOR WHEEL — CRACKED (NR 2 ENGINE) · airframe 7,550 hrs · 4,347 cycles

DURING SCHEDULED HC1 CHECK, FOUND NR 2 ENGINE BLADE PLATFORM CRACKED. REMOVED AND REPLACED PLATFORM PER MM.

Part: LIGHT — LOOSE (ROW 1 ABC) · airframe 7,422 hrs · 4,278 cycles

EEPLS LIGHT ASSY LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 7,327 hrs · 4,213 cycles

FLIGHT DECK R2 WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 7,224 hrs · 4,151 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 6,452 hrs · 3,648 cycles

EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.

Part: STRIP — CRACKED (CABIN) · airframe 4,994 hrs · 2,839 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 4,994 hrs · 2,839 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR SIDEWALL EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 3,915 hrs · 2,215 cycles

EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 3,880 hrs · 2,193 cycles

EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 3,838 hrs · 2,168 cycles

EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 3,816 hrs · 2,157 cycles

EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 2,415 hrs · 1,351 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LIGHT COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 1,232 hrs · 679 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.