N7814B

Part: FLAP — LOCKED (ZN 600 RIGHT WIN) · airframe 61,809 hrs · 32,941 cycles

AFTER LANDING FLAPS WOULD NOT RETRACT. SPLIT FLAP. RT #2 FLAP 28 LFT #1 FLAP 26<[01] R & R #5 TEE ANGLE GEARBOX REF. AMM 27-51-55 OPS CHECK GOOD

Part: LIGHT — FAULTY (ZN 200 FUS TOP) · airframe 60,416 hrs · 32,112 cycles

EMERGENCY EXIT LIGHTS WILL NOT SHUTOFF AT POWER SHUTDOWN.<[01] TURNED OFF EMERGENCY EXIT LIGHTS PER AMM 33-51-00

Part: BATTERY — DISCONNECTED (ZN 200 FUS TOP) · airframe 60,395 hrs · 32,101 cycles

BOTH FWD FLASHLIGHTS INOP<[01] FOUND BOTH BATTERIES DISCONNECTED. CONNECTED BATTERIES PER AMM 25-64-00. OPS CHECK NORMAL.

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 60,385 hrs · 32,095 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 2ND VERTICAL STIFFENER IS CRACKED.<[01] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[02] HFEC REQUEST ON THE CUT OUT EDGES; WEB AND EXISTING FASTENERS HOLES WITHIN THE REPAIR AREA TO ENSURE NO CRACKS EXIST.;[03] VERIFIED CORRECTIVE ACTION 1;[04] NDT HFEC INSPECTED CUT OUT EDGES AND WEB AREAS IAW 737 NDTM PART 6 51-00-00 PROC 23. <BR>NO CRACKS NOTED. <BR>EQUIP USED: NORTEC 600 ATS1465 DUE 09/23;[05] NDT HFEC INSPECTED OPEN HOLE IAW 737 NDTM PART 6 51-00-00 PROC 16. CRACKS NOTED IN 2 EA HOLES DIRECTLY BELOW CUT-OUT; MARKED.<BR>EQUIP USED: NORTEC 600 ATS1465 DUE 09/23 MINIMITE ID: ATS1411 DUE 07/23;[06] STEP 1 COMPLETE.;[07] VERIFIED STEP 1.;[08] PERFORMED GVI OF ALL AREAS WITHIN THE REPAIR AREA AND NO DEFECT NOTED IAW SRM 55-10-09-2R-5;[09] FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 7075 T76511 LOT# 1449876-1 (2) ANGLE FROM BAC 1490-2793 7075 T62 CLAD LOT# 1491233-1 (3) FILLER FROM 7075 T6 0.050' CLAD LOT# 1505777-1 (4) SHIM FROM 7075 T6 0.020' CLAD LOT# 1381332-1; APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-5 OK TO PRIME.;

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 60,385 hrs · 32,095 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 2ND VERTICAL STIFFENER IS CRACKED.<[01] REPAIR WILL BE ACCOMPLISHED ON CARD TTG8Q00M3HGQ.;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 60,385 hrs · 32,095 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 3RD VERTICAL STIFFENER IS CRACKED.<[01] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;;[13] FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 7075 T76511 LOT# 1449876-1 (2) ANGLE FROM BAC 1490-2793 7075 T62 CLAD LOT# 1491233-1 (3) FILLER FROM 7075 T6 0.050' CLAD LOT# 1505777-1 (4) SHIM FROM 7075 T6 0.020' CLAD LOT# 1381332-1; APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-5 OK TO PRIME.

Part: COVER — LOOSE (ZN 800 DOOR) · airframe 59,860 hrs · 31,768 cycles

CREW REPORTD AFT SERVICE DOOR SLIDE LOOSE TOUCHING DOOR EDGE<[01] PROPERLY INSTALLED AFT SERVICE DOOR SLIDE COVER IAW AMM 25-66-01

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 58,202 hrs · 30,763 cycles

EMERGENCY LIGHTS ON CABIN AND LH OVER WING EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OP CHECK GOOD.

Part: LIGHT — INOPERATIVE (R/H CABIN) · airframe 57,843 hrs · 30,534 cycles

ROW 18 RIGHT SIDE EMER LIGHT INOP / [01] RELAMPED PER AMM 33-51-03 OPS CK GOOD

Part: NONE — INOPERATIVE · airframe 56,782 hrs · 29,892 cycles

EMERGENCY LIGHTS AFT AND BELOW WING INOPERATIVE. / [01] REMOVED AND REPLACED POWER SUPPLY BATTERY PACK AT LOCATION M1670. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (FWD LH) · airframe 56,680 hrs · 29,843 cycles

FOUND SEVERAL EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED FWD LH EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-06

Part: GIRT BAR — LOOSE (L2 DOOR) · airframe 56,111 hrs · 29,540 cycles

REAR ENTRY DOOR GIRT BAR DOES NOT ALIGN SECURELY IN BRACKET ; / [01] REMOVED FLOOR-MOUNTED ESCAPE SLIDE GIRT BAR<BR>BRACKET PER AMM 25-66-02; [02] FOUND 1 BOLT IN ADAPTOR PLATE TO SHORT. REPLACED BOLT AND INSTALLED ADAPTOR PLATE PER AMM 25-66-02. OPS CK GOOD

Part: RETAINER — CRACKED (RT FLP FRG SEAL) · airframe 56,074 hrs · 29,521 cycles

R/H WING #6 FLAP FAIRING OUT BOARD SEAL RETAINER CRACKED. REMOVED AND REPLACED R/H WING #6 FLAP FAIRING OUTBOARD SEAL RETAINER PER AMM 27-51-18. REMOVED AND REPLACED R/H WING #6 FLAP FAIRING OUTBOARD SEAL RETAINER PER AMM 27-51-18.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 56,070 hrs · 29,520 cycles

R2 AND L2 DOORS ESCAPE SLIDE SKIRT RUB ACUFF PLATE WHEN CLOSING ; / [01] REPOSITIONED GIRT 'Z' FOLD ON L2 AND R2 DOOR SLIDES AS PER B737 AMM 25-66-01-400-804; [02] VERIFIED STEP 1

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,070 hrs · 29,520 cycles

SUPPLEMENTAL INFORMATION: R2 AND L2 DOORS ESCAPE SLIDE SKIRT RUB ACUFF PLATE WHEN CLOSING ; / [01] REPOSITIONED GIRT 'Z' FOLD ON L2 AND R2 DOOR SLIDES AS PER B737 AMM 25-66-01-400-804; [02] VERIFIED STEP 1

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 56,070 hrs · 29,520 cycles

FLIGHT DECK ENTRY EMERGENCY LIGHT INOP. ; / [01] REPLACED LAMP ON FLIGHT DECK EMERGENCY ENTRY LIGHT; PERFORMED TEST; TEST PASS. REF. TO B 737 AMM 33-51-01-960-801.; [02] VERIFIED STEP 1

Part: DRAIN — CRACKED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

CUSTOMER REQUEST: BS 1016 CENTER FUSELAGE DRAIN CRACKED ; / [01] REMOVED DAMAGE DRAIN AT STA 1016 ( CENTER DRAIN ) PER B737 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW DRAIN PER B737 SRM 51-40-05-0G-0; [03] VERIFIED STEPS 1 AND 2; [04] OK TO INSTALL DRAIN; [05] INSTALLED NEW FUS. DRAIN FITTING AT STA. 1016 CENTER LOWER AREA; AS PER B737-7 SRM 51-40-02-0G-0.; [06] VERIFIED STEP 5

Part: SEAL PLATE — DELAMINATED (L/H VERT. STAB.) · airframe 56,070 hrs · 29,520 cycles

LEFT VERTICAL STAB TRAILING EDGE SEAL PANEL 324ABL IS DELAMINATED AND HAS SECTIONS OF THE SEAL MISSING ; / [01] RECEIVED NEW SEAL PANEL P/N 175A1601-86; [02] OK TO INSTALL PANEL.; [03] INSTALLED NEW PANEL P/N 175A1601-86 REF B 737 SRM 51-40-02. WORK WAS ACCOMPLISHED BY TECHNICIAN REINIER PRADO EMPL # 32404; [04] FINAL INSPECTION; EDGE SEAL PANEL REPLACED.

Part: NONE — CRACKED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

FWD. CARGO COMPT. INTERCOSTAL/BAFFLE HAS CRACKED FWD. CLIP AT BS 400; LBL 21;(143A7502-5) ; / [01] REMOVED CLIP AT FWD CARGO COMPT. INTERCOSTAL/ BAFFLE IAW B737-700 SRM 51-40-02-0G-0; [02] LOCATED HOLES AT NEW CLIP. IAW B737-700 SRM 51-40-05-0G-0; [03] VERIFIED STEP 1 & 2; [04] OK TO INSTALL NEW CLIP AT FWD CARGO COMPT. INTERCOASTAL/ BAFFLE BS 400 LBL 21; [05] INSTALLED NEW CLIP AT FWD CARGO COMPT. INTERCOSTAL BAFFLE. IAW B 737-700 SRM 51-40-02-0G-0; [06] VERIFIED STEP 5

Part: PANEL — CRACKED (R/H VERT. STAB.) · airframe 56,070 hrs · 29,520 cycles

RT SIDE HORIZONTAL FUSELAGE BLADE GUIDE FOR PANEL 343AT CRACKED. ; / [01] REMOVED RT SIDE HORIZONTAL FUSELAGE BLADE GUIDE FOR PANEL 343AT IAW B737 SRM 51-40-02; [02] VERIFIED STEP #1; [03] OK TO INSTALL NEW REPLACEMENT; [04] INSTALLED RT SIDE HORIZONTAL FUSELAGE BLADE GUIDE FOR PANEL 343AT REF B 737-700 51-40-02. WORK WAS ACCOMPLISHED BY TECHNICIAN REINIER PRADO EMPL # 32404; [05] VERIFIED STEP 4

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

FOUND INTERCOSTAL/BAFFLE CRACKED AT FWD. CARGO COMPT. BETWEEN BS 400 & 420;LBL 21. ; / [01] REMOVED INTERCOSTAL/BAFFLE AT FWD CARGO COMPT. STA 400 AND 420;LBL 21 IAW B737-700 SRM 51-40-02-0G-0; [02] LOCTED AND DRILLED NEW INTERCOSTAL/BAFFLE; AT FWD CARGO COMPT SAT 400 AND 420 LBL 21. IAW B737-700 51-40-05; [03] OK TO INSTALL INTERCOASTAL/BAFFLE AT FWD CARGO COMPT. BETWEEN BS 400 & 420; LBL 21; [04] INSTALLED INTERCOSTAL/BAFFLE AT FWD CARGO COMPT. BETWEEN BS 400 AND BS 420 LBL 21. IAW B737-700 SRM 51-40-02-0G-0; [05] VERIFIED STEP 4

Part: PANEL — CRACKED (L/H VERT. STAB.) · airframe 56,070 hrs · 29,520 cycles

LT SIDE HORIZONTAL FUSELAGE BLADE GUIDE FOR PANEL 333AT CRACKED. ; / [01] REMOVED LT SIDE HORIZONTAL FUSELAGE BLAD GUIDE FOR PANEL 333AT IAW B737 SRM 51-40-02; [02] VERIFIED STEP M#1; [03] OK TO INSTALL NEW REPLACEMENT.; [04] INSTALLED LT SIDE HORIZONTAL FUSELAGE NEW BLADE GUIDE FOR PANEL 333 AT IAW B737 SRM 51-40-02; [05] VERIFIED STEP 4

Part: DOOR — CORRODED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

FOUND CORROSION & WORN AT L-1 DOOR CUTOUT FWD. FRAME LOWER HINGE BOX UPPER FITTING HOLE. PARTIAL REMOVED HINGE BOX AT L-1 DOOR CUTOUT FWD. FRAME LOWER. IAW SRM 51-40-02. INSTALLED EWIS PROTECTION AT L-1 DOOR CUTOUT FWD. LOWER HINGE BOX AREA DURING MAINT. IAW AMM 20-60-07-913-801. REMOVED INTERCOSTAL STR 13L AT L-1 DOOR CUTOUT FWD IAW SRM 51-40-02-0G-0; REMOVED INTERCOSTAL STR 13N-L AT L-1 DOOR CUTOUT FWD. AT L-1 DOOR CUTOUT FWD. LOCATED AND DRILLED NEW HOLES ON FWD FRAME LOWER HINGE BOX AT L-1 DOOR CUTOUT IAW SRM 51-40-05-0G-0; LOCATED AND DRILL ALL REMAINING NEW HOLE ON FWD FRAME LOWER HINGE BOX AT L-1 DOOR CUTOUT IAW SRM 51-40-05-0G-0 AND DWG 141A8180.

Part: RIB — CRACKED (LT WING TE FLAP) · airframe 56,070 hrs · 29,520 cycles

L/W I/B FLAP L/E SECOND RIB IS CRACKED.(FROM I/B). ; / [01] REMOVED DAMAGED RIB AT L/W I/B FLAP L/E AREA UNDER PANEL #553AT; AS PER B737-7; SRM 51-40-02-0G-0.; [02] FPI ACCOMPLISHED AT IN-PROGRESS FABRICATION OF RIB AFTER ALL MACHINING IAW BOEING DRAWING # PL113A2218 SHEET 6 BAC 5423/BSS 7039. NO CRACKS NOTED.; [03] LOCATED AND DRILLED NEW RIB AT L/W I/B FLAP L/E REF B737-700 SRM 51-40-05-0G-0; [04] REMOVED PANEL # 553BB FOR ACCESS IAW B737 SRM 51-40-02; [05] VERIFIED STEP #3; [06] OK TO TREAT AND PRIME.; [07] VERIFIED STEPS 1 AND 4; [08] APPLIED TREAT AND PRIMED TO THE L/W I/B FLAP L/E SECOND RIB REF.B-737-700 AMM 51-00-58-201 AND B-737-700-AMM 51-21-72-370-804; [09] VERIFIED STEP 8; [10] OK TO INSTALL RIB; [11] INSTALLED NEW RIB 113A2218-1; AT L/W I/B FLAP L/E SECOND POSITION(FROM I/B); AS PER BOEING DWG. 113A2218. & B737-7 SRM 51-40-02-0G-0.; [12] PANEL#553BB ;OPENED ON STEP #4; WILL BE CLOSED ON CARD:CLOSE PANEL 553BB; BARCODE:TTG8Q0097EZT.; [13] VERIFIED STEP 12; [14] VERIFIED STEP 11; [15] RECEIVED NEW RIB P/N:113A2218-1; PO#:1746218; CONTROL TAG:400950. AS PER DWG 113A2218.

Part: BRACKET — CRACKED (VERT. STAB.) · airframe 56,070 hrs · 29,520 cycles

DORSAL FIN FWD ATTACHMENT BRACKET IS CRACKED ; / [01] REMOVED FWD ATTACHMENT BRACKET(WEB) FROM DOSAL FIN REF B737-700 SRM 51-40-02-0G-0; [02] INSTALLED BRACKET AT FWD DORSAL FIN IAW B737 SRM 51-40-02; [03] PART TRANSACTION ONLY; [04] VERIFIED INSTALLATION OF NEW BRACKET IN STEP 2

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

FWD CARGO COMPT STA 500D STR 18 R/H GUSSET CRACKED ; / [01] REMOVED R/H GUSSET AT FWD CARGO COMPT STA 500D STR 18 IAW B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED HOLES AT NEW GUSSET AT FWD CARGO COMPT SAT 500D STR 18 R/H. IAW B737-700 SRM 51-40-05-0G-0; [03] VERIFIED STEP:1 AND 2. <BR>OK TO INSTALL RH GUSSET.; [04] PARTIAL INSTALLED R/H GUSSET AT FWD CARGO COMPT. STA 500D STR 18 IAW B 737-700 SRM 51-40-02-0G-0; [05] INSTALLED NEW GUSSET AT FWD. CARGO COMPT. FR. BS. 540D; STRG. 18R. AS PER B717-7 SRM 51-40-02-0G-0; & DWG. 143A9481.; [06] VERIFIED STEPS 4 AND 5; [07] VERIFIED STEPS 4 AND 5

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 277 AND STA 294.5 RBL 12' CRACKED ; MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 277 AND STA 294.5 BL 0 CRACKED / [01] REMOVED DAMAGED INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 277 AND STA 294.5 RBL 12'; AS PER B737-7; SRM 51-40-02-0G-0.; [02] VERIFIED STEP 1 OK TO INSTALL INTERCOSTAL; [03] INSTALLED INTERCOSTAL AT MAIN CABIN FWD WET AREA STA 277 AND STA 294.5 RBL 12. IAW B 737-700 SRM 51-40-02-0G-0; [04] CORRECTION FOR STEP3 AND DWG # 141A5410; [05] VERIFIED STEPS 3 AND 4

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 30' CRACKED ; / [01] REMOVED INTERCOSTAL AT MAIN CABIN FWD WET AREA STA 312 AND 328 RBL. 30 IAW B 737-700 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1; [03] OK TO INSTALL INTERCOSTAL; [04] INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA. 312 & 328; RBL 30; AS PER B-737-7 SRM 51-40-02-0G-0 & DWG. 141A5400.; [05] VERIFIED STEP 4. TASK C/W; [06] VERIFIED STEP 4. TASK C/W

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 328 AND STA 344 LBL 34' CRACKED ; MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 328 AND STA 344 LBL 46' CRACKED / [01] REMOVED AT MAIN CABIN WET AREA INTERCOSTAL BETWEEN STA 328 344LBL 46' IAW B737-7 SRM 51-40-02-0G-0.; [02] VERIFIED STEP 1 OK TO INSTALL INTERCOSTAL; [03] INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA. 328 & 344; LBL 46 AS PER B737-7 SRM 51-40-02-0G-0 & DWG 141A5400.; [04] VERIFIED STEP 3

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN BS 312 AND 328 LBL 34' CRACKED. REMOVED INTERCOSTAL AT MAIN CABIN FWD WET AREA STS 312 AND 328 LBL 44 IAW SRM 51-40-02-0G-0; [02] REMOVE MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 312 AND STA 328 LBL; [03] VERIFIED STEPS 1 AND 2; [04] OK TO INSTALL NEW INTERCOSTAL; [05] INSTALLED AT MAIN CABIN FWD WEB AREA INTERCOSTAL BETWEEN STA 312 AND STA 328 LBL IN REF B0ING 737-700 SRM 51-40-02-OG-0; [06] CORRECTION ON STEP #2:COMPLETED REMOVAL OF INTERCOSTAL BETWEEN STA. 312 & STA. 328; LBL 34'; AS PER B737-7 SRM 51-40-02-0G-0.; [07] CORRECTION OF REF. ON STEP #5:AS PER B737-7 SRM 51-40-02-0G-0.; [08] VERIFIED STEPS 5-7. TASK C/W; [09] VERIFIED STEPS 5-7. TASK C/W

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

CORROSION FWD CARGO L-26 STRINGER TO FRAME AT BS 540. REMOVED CORROSION S26L, BS 540 FOUND OUT LIMITS IAW B737-700 SRM 51-10-02, ORIG. MAT.: 0.045'; MAT. REMOVED:0.035'; REMAINING MAT. : 0.015'; FOUND OUT OF LIMITS IAW SRM 53-00-03-1A-1, TABLE 101. CUT-OUT STRINGER DAMAGED SECTION 24' 7/8 FROM AFT END IAW SRM 53-00-03-2R-1, FIG 206. PERFORMED HFEC INSP. ON THE REPAIR AREA IAW NDT PART 6; 51-00-00; PROCEDURE 23. NO CRACKS NOTED. REPAIR OF S26L WAS ACCOMPLISHED ON EA:21-153-03789-WIP1.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

FW CARGO R-26 STRINGER TO FRAME BS 540. CLEANED AREA AT FWD CARGO R-26 STRINGER TO FRAME BS 540. FOUND WITH CRACK. IAW SRM 53-00-03-1A-1. REMOVED CORROSION AT STR. 26R; BS 540, ORIGINAL MAT.: 0.040'; MAT. REMOVED 0.035'; REMAINING MAT 0.005', FOUND OUT OF LIMITS IAW SRM 51-10-02-0G-0; & 53-00-03-1A-1, TABLE 101. REMOVED FAIRING ANGLE SUPPORT TO GET ACCESS AT FWD CARGO R-26 STG STA 540 REPAIR AS PER SRM 51-40-02-OG-O. REMOVED FASTENERS COMMON TO REPAIR AT STRG. 26R BETWEEN BS 540 & 500D IAW SRM 51-40-02-0G-0. ACCOMPLISHED REPAIR AT S-26R; BS. 540; AS PER EA:21-153-03792-WIP1.

Part: FLOOR PANEL — FRAYED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

MAIN CABIN FLOOR PNL 241 AF FRAYED FIBER GLASS ON TOP SURFACE ; / [01] REMOVED CABIN FLOOR PANEL 241AF IN REF B737-700 AMM- 53-21-00-000-801; [02] VERIFIED STEP 1. OK TO INSTALL PNL 241AF; [03] INSTALLED CABIN FLOOR PANEL 241AF IN REF B737-700 AMM-53-21-00-400-801; [04] NEW FLOOR PANEL WAS INSTALLED; [05] CERTIFIED WORK CAPTURE EDITED NEW PANEL INSTALLED; [06] VERIFIED STEPS 3 AND 4

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

AFT CARGO RT BS 727D S25 SIDEWALL SUPPORT CRACKED. REMOVED RT SIDEWALL SUPPORT ANGLE IAW SRM 51-40-02-0G-0. FABRICATED SIDEWALL SUPPORT BRACKET IAW DR 146A9403, LOCATED AND DRILLED HOLES IN SIDEWALL SUPPORT BRACKET IAW SRM 51-40-05. TREATED AND PRIMED NEW SIDEWALL SUPPORT BRACKET IAW AMM 51-21-41 AND AMM 51-21-72. APPLIED TWO COAT OF PRIMER TO SUPPORT BRACKET REF SRM51-20-01. INSTALLED RT SIDE WALL SUPPORT BRACKET AT AFT CARGOBS 727D, S25 IAW SRM 51-40-02-0G-0. FABRICATION OF CHANNEL WAS ACCOMPLISHED IAW DWG 146A9403 WHILE CUT AND TRIMMING WAS ACCOMPLISHED PER DWG 790408 AND ESR 1069.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

CORROSION FWD CARGO R-27 STRINGER TO FRAME AT BS 540. REMOVED FASTENERS TO GAIN ACCESS AT FWD CARGO R-27 STRINGER TO FRAME AT BS 540 IAW B737-700 SRM 51-40-02-0G-0. CLEANED AREA AT FWD CARGO R-27 STRINGER TO FRAME AT BS 540 FOUND CRACKED IAW SRM 53-00-03-1A-1. REMOVED CORROSION ORIG. MAT. 0.032'; MAT. REMOVED: 0.020' REMAINING MAT. 0.012'. FOUND OUT OF LIMITS IAW SRM 51-10-02-0G-0 & 53-00-03-1A-1 TABLE 101. REMOVED FASTENERS COMMON TO REPAIR AT STRINGER-SKIN ATTACH FLANGE OF S-27R BETWEEN BS 540 & 500D IAW SRM 51-40-02-0G-0. CUT-OUT STRINGER DAMAGED SECCION 24' 7/8 FROM AFT END. ACCOMPLISHED ON EA:21-153-03794-WIP1.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

AFT CARGO COMP L/H BETWEEN STA 747 AND STA 847 ZEE CHANNEL UPPER SURFACE SEVERAL AREA WITH CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G-0-A00248. PERFORMED UT THICKNESS INSP. ON REWORKED AREA IAW NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS .029'. ORIGINAL MATERIAL 0.040;MATERIAL LOSS 0.011 MATERIAL REMAINING 0.029, OUT OF LIMITS IAW SRM BCG D634A201. FABRICATED NEW ZEE CHANNEL FROM BS 747 TO 847 IAW SRM 53-60-53-01-2 AND DWG 146A7500. MEASUREMENTS INPUT ONLY; [09] STEP 7/8 VERIFIED; OK TO TREAT/PRIME; [10] TREATED AND PRIMED ZEE CHANNEL REF SRM 51-20-01-0G-0 AND AMM 51-21-72-370.

Part: BATTERY — INOPERATIVE (FWD CABIN) · airframe 56,070 hrs · 29,520 cycles

L1 WINDSCREEN BOTH FLASHLIGHT BATTERIES INOP ; / [01] REMOVED AND REPLACED L1 WINDSCREEN BOTH FLASHLIGHT BATTERIES AS PER BOEING AMM 25-64-00-900-806; [02] VERIFIED STEP 1

Part: BATTERY — INOPERATIVE (FWD CABIN) · airframe 56,070 hrs · 29,520 cycles

L2 MEGAPHONE BATTERIES INOP ; / [01] REMOVED AND REPLACED L2 MEGAPHONE BATTERIES AS PER BOEING AMM 25-64-00-900-804.; [02] VERIFIED STEP 1

Part: FLOOR PANEL — FRAYED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

MAIN CABIN; FLOOR PNL 242 AF HAS FRAYED FIBERS GLASS ON TOP SURFACE ; / [01] RECEIVED SERVICEABLE FLOOR PANEL 242AF. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q0097DKZ; [02] VERIFIED STEP 1

Part: PANEL — CORRODED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

L/W FUEL PANEL 534BB INNER SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G-0. FOUND WITHIN LIMITS IAW SRM 57-20-01-2R-1, FIG 203, DETAIL B-B. TREATED REWORKED AREA OF PANEL IAW SRM 51-10-02-0G-0.

Part: FLOOR PANEL — FRAYED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

MAIN CABIN FLOOR PANEL 241AAF UPPER SURFACE FRAYING ; / [01] PARTIALLY FABRICATED PASSENGERS CABIN FLOOR PANEL 241AAF REF B-737-700 SRM-53-0050-1A-1 PENDING INSERTS INSTALLATION; [02] VERIFIED FABRICATED PASSENGERS CABIN FLOOR PANEL 241AAF REF B-737-700 SRM-53-0050-1A-1 PENDING INSERTS INSTALLATION; [03] FINALIZED FABRICATION OF PASSENGER CABIN FLOOR PANEL 241AAF REF B 737-700 SRM 53-00-50-1A-1. WORK WAS ACCOMPLISHED BY TECHNICIAN RAFAEL MERLANO EMP # 15961. PANEL WILL BE CLOSED ON TASK CARD TTG8Q0097D7E; [04] VERIFIED COMPLETED.

Part: FLOOR PANEL — FRAYED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

MAIN CABIN FLOOR PANEL 241ACF UPPER SURFACE FRAYING ; / [01] PARTIALLY FABRICATED PASSENGER CABIN FLOOR PANEL 241ACF REF B-737-700 SRM-53-00-50-1A-1 PENDING INSERTS INSTALLATION.; [02] VERIFIED FABRICATED PASSENGERS CABIN FLOOR PANEL 241ACF REF B-737-700 SRM-53-0050-1A-1 PENDING INSERTS INSTALLATION; [03] FINISHED FABRICATION PASSENGER CABIN FLOOR 241ACF IAW B737 SRM 53-00-50; [04] FLOOR PANEL 241ACF WILL BE CLOSED ON TASK CARD TTG8Q0097D7A; [05] VERIFIED COMPLETE.

Part: FLOOR PANEL — FRAYED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

MAIN CABIN FLOOR PANEL 241XF UPPER SURFACE FRAYING ; / [01] PARTIALLY FABRICATED PASSENGER FLOOR PANEL 241XF REF B-737-700 SRM-53-00-50-1A-1 PENDING INSERTS INSTALLATION.; [02] VERIFIED FABRICATED PASSENGERS CABIN FLOOR PANEL 241XF REF B-737-700 SRM-53-0050-1A-1 PENDING INSERTS INSTALLATION; [03] FINALIZED FABRICATION OF PASSENGER CABIN FLOOR PANEL 241XF REF B 737-700 SRM 53-00-50-1A-1. WORK WAS ACCOMPLISHED BY TECHNICIAN RAFAEL MERLANO EMP # 15961. PANEL WILL BE CLOSED ON TASK CARD TTG8Q0097D6K; [04] VERIFIED STEP 3

Part: FLOOR PANEL — FRAYED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

MAIN CABIN FLOOR PANEL 241ADF UPPER SURFACE FRAYING ; / [01] PARTIALLY FABRICATED PASSENGERS CABIN FLOOR PANEL 241ADF REF B-737-700 SRM-53-00-50-1A-1 PENDING INSTALLATION; [02] CORRECTION TO STEP 1: PARTIALLY FABRICATED PASSENGER CABIN FLOOR PANEL 241ADF REF B-737-700 SRM-53-00-50-1A-1 PENDING INSERTS INSTALLATION.; [03] VERIFIED FABRICATED PASSENGERS CABIN FLOOR PANEL 241ADF REF B-737-700 SRM-53-0050-1A-1 PENDING INSERTS INSTALLATION; [04] FINALIZED FABRICATION OF PASSENGER CABIN FLOOR PANEL 241ADF REF B 737-700 SRM 53-00-50-1A-1. WORK WAS ACCOMPLISHED BY TECHNICIAN RAFAEL MERLANO EMP # 15961. PANEL WILL BE CLOSED ON TASK CARD TTG8Q0097D78; [05] VERIFIED STEP 4.

Part: ANGLE — BROKEN (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

PANEL 423BL HAS SHIM BROKEN INSIDE PANEL DOOR. ; / [01] RREMOVED ANGLE (SHIM) AT PANEL 423BL REF B 737-700 SRM 51-40-02; [02] THE ANGLE SHIM P/N: 314-2215-3; WAS REPLACED ON N/R 4000/0009; W/O: 2018123; BARCODE: TTG8Q009M4UD.; [03] VERIFIED STEPS 1 AND 2

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 56,070 hrs · 29,520 cycles

EXTERNAL POWER RECEPTACLE DOOR LOWER CUT OUT SKIN DOUBLER IS CRACKED. PROTECTED EWIS AREA AT EXTERNAL POWER RECEPTACLE DOOR. IAW AMM 20-60-07-913-801. REMOVED DOOR PANEL 114 AR FOR GAIN ACCESS. IAW SRM 51-40-02-0G-0. REMOVED THE INITIAL RUBBING BLOCK; THE LAMINATED SHIM AND TRIMMED OUT THE DAMAGE AREA AT EXTERNAL POWER RECEPTACLE DOOR LWR CUTOUT SKIN. IAW SRM 53-10-15-2R-4 FIG. 204 DETAIL C. PERFORMED HFEC AT CUT OUT IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS. FABRICATED DOUBLER FOR REPAIR PART. FABRICATED FILLER FOR REPAIR PART IAW SRM 53-10-15-2R-4 FIG. 204 DETAIL C. TREATED AND PRIME DOUBLER AND FILLER IAW SRM 51-20-01.

Part: SKIN — CRACKED (R/H WING) · airframe 56,070 hrs · 29,520 cycles

RT WING LOWER SURFACE L/E; #6 SLAT NOSE SKIN AT ACTUATOR RIBS. CRACK AROUND FASTENER SKIN. CRACK CONFIRMED IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK FOUND AT 2ND FWD O/B FASTENER. CRACK LENGTH :0.157. REMOVED INBD CENTER, OTBD COVE SKIN & PARTIAL FLEX SKIN SECTION IAW SRM 51-40-02-0G-0; REMOVED FASTENER FROM REPAIR AREA, CUTOUT DAMAGE AREA IAW SRM 57-42-01-2R-8 FIG 202; PERFORMED HFEC AT CUT OUT IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS. PERFORMED HFEC HOLE PROBE INSPECTION ON ALL REMOVED FASTENER LOCATIONS WITHIN REPAIR AREA IAW NDTM PART 6; 51-00-00; PROCEDURE 16. NO CRACKS. FABRICATED DOUBLER AND FILLER IAW SRM 57-42-01-2R-8.

Part: BATTERY — FAILED (CABIN) · airframe 55,888 hrs · 29,411 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1668, M1669 AND M1675 IN CABIN. R&R EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS M1668, M1669 AND M1675 PER AMM 33-51-06.

Part: LENS — BROKEN (CABIN) · airframe 55,354 hrs · 29,079 cycles

LOWER L1 DOOR EMERGENCY LIGHT LENS ASSEMBLY BROKEN AND NOT SECURE. / R&R L1 EMERGENCY LIGHT ASSEMBLY PER AMM.

Part: VALVE — FAULTY (NR 2 ENGINE) · airframe 54,066 hrs · 28,264 cycles

AIR TURNBACK, DURING PASSING 10' BLEED TRIP OFF NR 2 ENG. WOULD NOT RESET. R & R THE NR 2 ENGINE HIGH STAGE VALVE PER AMM.

Part: GROUND WIRE — BROKEN (CABIN) · airframe 53,796 hrs · 28,089 cycles

EMERGENCY LIGHTS ARE ACTIVIATING WHEN SWITCH IS IN THE OFF POSITION. REPAIRED BROKEN GROUND PIN AT GROUND BLOCK GD11098-DE IAW WDM AND SWPM.

Part: ANGLE — CRACKED (AFT FUSELAGE) · airframe 53,796 hrs · 28,089 cycles

EXTERNAL FUSELAGE; STA 1016+3; LBL 11; 7' ABOVE FUSELAGE SKIN; LATTERAL ANGLE IS CRACKED IN RADIUS (COMMON TO FWD VERTICAL STAB A-FRAME FITTING) / REPMOVED AND REPLACED LATTERAL ANGLE P/N L776A3101-26 A TAG A84524 IAW BOEING DWG 3 176A3001 REV A.

Part: CONNECTOR — LOOSE (CABIN) · airframe 53,796 hrs · 28,089 cycles

FWD GALLEY EMERGENCY EXIT SIGN LOOSE AT CONNECTOR D3658. R&R CONNECTOR D3658 PER AMM.

Part: NONE — CRACKED (CABIN) · airframe 53,796 hrs · 28,089 cycles

PANEL BREAK AT STA 540 BETWEEN BL 0 AND LBL 25 CRACKED FWD SIDE AT LBL 3. / REMOVED & REPLACED PANEL BREAK SUPPORT AT STA 540; BLO TO LBL 25 IAW BOEING DWG #143A0060 REV. B ATAG # GE1605

Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 53,796 hrs · 28,089 cycles

MAIN LANDING GEAR FORWARD PRESSURE BULKHEAD TO FUEL TANK ATTACH ANGLE CRACKED AT BS. 663, RBL 34, INBOARD SIDE OF DRAIN HOLE TO ATTACH FASTENER HOLE. / REPAIRED ANGLE IAW EA.

Part: RETAINER — CRACKED (LT WHEEL WELL) · airframe 53,796 hrs · 28,089 cycles

DURING INSTALLATION OF THE L/H 663 VAPOR BARRIER BULKHEAD REPAIR FOUND CRACKED SEAL RETAINER. / REMOVED SEAL RETAINER FROM VAPOR BARRIER STA 663 L/H IBL15-LBL25 IAW SRM N737NG 51-40-02-0G-02; VERIFIED PN 111A1512V1 IAW B737 DRW 111A1000 REV:F. INSTALLED A NEW SEAL RETAINER & SEAL IAW SRM B737NG 51-40-02-0G-02

Part: WEB — CRACKED (BS 986-1016) · airframe 53,796 hrs · 28,089 cycles

FLOOR SUB WEB FOUND CRACKED BETWEEN BS. 986 TO BS. 1016, LBL 53. R&R SUB WEB IAW DWG & SRM.

Part: DOUBLER — CORRODED (AFT CARGO BAY) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO BULKHEAD STA 947. RIGHT SIDE ANGLE DOUBLER 149A8118-15 IS CORRODED. / REMOVED AFT CARGO BULKHEAD STA 947; RIGHT ANGLE DOUBLER RBL20 FOUND TO BE OUT OF LIMITS. ORG 'T' .063 LOSS .011' REM. .052' IAW DWG 144A8118 REV 13 B737-700 AND SRM 53-00-53-1A-2 RECEIVED NEW R/H CURVE CHORD ASSY WITH R/H ANGLE DOUBLER INSTALLED FROM MFG. ISNTALLED ON W/O X961699 P/N 149A8118-15

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 53,796 hrs · 28,089 cycles

G-1 GALLEY, EXIT LIGHT LENS COVER CRACKED. R&R COVER IAW AMM.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 53,796 hrs · 28,089 cycles

CABIN FLOOR BOARD 231JF LOWER SURFACE INBOARD EDGE HAD LAYER CRACKED BETWEEN BS. 480 TO BS. 520. / REPAIRED FLOOR PANEL 231JF IAW SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA FLOORBOARD 222AF HAD UPPER LAYERS DAMAGED, BETWEEN BS. 270 TO BS. 420. REPAIRED FLOORBOARD 222AF IAW SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA FLOOR BOARD 221CF DAMAGED UPPER LAYER FIBERS, BETWEEN BS. 270 TO BS. 420. / REPAIRED FLOOR BOARD 221CF IAW SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA FLOORBOARD 222DF HAD DAMAGED UPPER LAYER FIBERS, BETWEEN BS. 270 TO BS. 420. REPAIRED FLOORBOARD 222DF IAW SRM.

Part: FLOORBOARD — DAMAGED (FWD WET AREA) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA FLOORBOARD 221EF HAD DAMAGED UPPER LAYER FIBERS, BETWEEN BS. 270 TO BS. 420. REPAIRED FLOORBOARD 221EF IAW SRM.

Part: ATTACH BRACKET — CRACKED (AFT SERVICE DOOR) · airframe 53,796 hrs · 28,089 cycles

AFT SERVICE DOOR (R2) PANEL 844DZ FORWARD ATTACH BRACKET IS CRACKED. / REMOVED; VERIFIED; LOCATED; DRILLED AND INSTALLED NEW ATTACHED BRACKET AFT SERVICE DOOR R.2 PANEL #844DZ I/A/W AIPC 52.41.31.10 PGS 14;21 SRM 51.40.02 P/N 411A2129-547 ATAG# A72848

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

CABIN FLOOR BOARD 232SF UPPER SURFACE OUTBOARD EDGE LAYER IS CRACKED WITH CRUSHED CORE 33' FROM AFT EDGE / REPAIRED CABIN FLOOR BOARD 232SF OF UPPER SURFACE EDGE DAMAGE WITH CRUSHED CORE 33' FROM AFT EDGE (P.S MARKED) IAW B737-700 SRM 53-00-50-2R-10 REV 67 AND B737-700 SRM 53-00-50-50-2R-0 REV 67 REPAIR GENERAL A02940

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

FWD WET AREA FLOOR BOARD 222BF HAS 2EA PUNCTERS AT INSERTS. MARKED. / REPAIRED 2EA PUNCTURES @ INSERTS ON FWD WET AREA FLOORBOARD 222BF IAW B737 SRM 53-00-50-2R-2 REV 67

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

CABIN FLOOR BOARD 231JF LOWER SURFACE INBOARD EDGE HAS LAYER CRACKED WITH CRUSHED CORE 22.5' FROM FWD EDGE / REPAIRED CRACKED LAYER W/ CRUSHED CORE 22.5' FROM FWD EDGE I/B OF LOWER SURFACE CABIN FLOOR BOARD 231JF IAW B737 SRM 53-00-50-2R-8 REV 67

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

CABIN FLOOR BOARD 231JF LOWER SURFACE INBOARD EDGE HAS LAYER CRACKED WITH CRUSHED CORE 15' FROM AFT EDGE / REPAIRED CRACKED LAYER W/ CRUSHED CORE 15' FROM AFT EDGE OF LOWER SURFACE I/B OF BABIN FLOOR PANEL 231JF IAW B737 SRM 53-00-50-2R-8 REV 67

Part: FLOORBOARD — DAMAGED (FWD WET AREA) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA FLOOR BOARD 221GF HAD DAMAGED UPPER LAYER FIBERS, BETWEEN BS. 270 TO BS. 420. REPAIRED FLOOR BOARD 221GF IAW SRM.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 53,796 hrs · 28,089 cycles

CABIN FLOORBOARD 242DF LOWER SURFACE FORWARD INBOARD CORNER LAYER CRACKED BETWEEN BS. 537.45 TO BS. 727B WITH CRUSHED CORE. / REPAIRED FLOORBOARD 242DF IAW SRM.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA FLOOR BOARD 222AF HAD CORNER DELAMINATED. / REPAIRED FLOOR BOARD 222AF IAW SRM.

Part: FLOORBOARD — DAMAGED (FWD WET AREA) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA FLOOR BOARD 222BF HAD UPPER LAYER DAMAGED FIBERS, BETWEEN BS. 270 TO BS. 420. / REPAIRED FLOOR BOARD 222BF IAW SRM.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

CABIN FLOOR BOARD 231JF LOWER SURFACE INBOARD EDGE HAS LAYER CRACKED WITH CRUSHED CORE 18' FROM AFT EDGE / REPAIRED CRACKED LAYER WITH CRUSHED CORE 18' FROM THE AFT EDGE 11B ON LOWER SURFACE OF CABIN FLOOR BOARD 231JF IAW B737 SRM 53-00-50-2R-8 REV 67

Part: FLOOR PANEL — DELAMINATED (AFT WET AREA) · airframe 53,796 hrs · 28,089 cycles

AFT WET AREA FLOOR PANEL 242VF TOP SURFACE OF PANEL DELAMINATED, BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR BOARD 242VF IAW SRM.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 53,796 hrs · 28,089 cycles

AFT WET AREA FLOOR PANEL 241AEF, TOP SURFACE OF PANEL DELAMINATED, BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR PANEL 241AEF IAW SRM.

Part: FLOORBOARD — DAMAGED (BS 270-420) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA FLOOR BOARD 221BF UPPER LAYER DAMAGED WITH EDGE DAMAGE, BETWEEN BS. 270 TO BS. 420. REPAIRED FLOOR BOARD 221BF IAW SRM.

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

CABIN FLOOR BOARD 242BF UPPER SURFACE IS PUNCTURED ON OUTBOARD EDGE 19' FROM FWD EDGE WITH DAMAGED INSERT / REPAIRED CABIN FLOORBOARD 242BF UPPER SURFACE DAMAGE O/B EDGE 19' FROM FWD EDGE I.A.W. B737-700 SRM'S 53-00-50-2R-0 REV. 67 AND 53-00-50-2R-9 REV. 67 TAP TEST GOOD. (A42411) (A19477) (A09236) (A40400) (A66416)

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO COMPARTMENT DOOR CUT-OUT AFT CORNER THRESHOLD CRACKED. / AFT CARGO DOOR AFT CORNER THRESHOLD REPAIRED ON BACKSHOP WORK ORDER 39556-1600-0002 IAW EA 1-A53-2076 REV 11.

Part: GIRT BAR — CORRODED (FWD ENTRY DOOR () · airframe 53,796 hrs · 28,089 cycles

FWD WET AREA L1 GIRT BAR Z CORRODED AT BS 312 LBL 55. / REMOVED AND REPLACED FWD WER AREA L1 GRIT BAR Z AT BS 312 LBL 55 IAW B737 SRM 51-40-02-0G-0 STEP 9 P/N 141A5220-2

Part: CREASE BEAM — CRACKED (BS 303) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA CREASE BEAM CRACKED AT BS. 303.9, LBL 52. / R&R CREASE BEAM IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

FWD WET AREA INTERCOSTAL CRACKED AT BS 344 - 8' LBL 42. / REMOVED AND REPLACED INTERCOSTAL FWD WET AREA AT BS344-8 LBL 42 IAW BOEING DWG 141A5400 REV:- AND B737 SRM 51-40-05-0G-0; 51-40-02-0G-0

Part: GIRT BAR — CORRODED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

FWD WET AREA GIRT BAR Z CORRODED AT BS 344 LBL 57. / REMOVED AND REPLACED FWD WET AREA GIRT BAR Z AT BS344 LBL 57 IAW B737 SRM 51-40-02-0G-0 STEP 9 P/N 141A5220-4

Part: CREASE BEAM — CORRODED (BS 312) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA R1 DOOR INNER L ANGLE AT CREASE BEAM NUT PLATE AREAS CORRODED BETWEEN BS. 312-10 TO BS. 312+15, RBL 60. / R&R L ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

FWD WET AREA FLOOR BEAM AREAS AS CORROSION AT BS 328 RBL 45 TO RBL 53. / REMOVED CORROSION FROM BS 328 FLOOR BEAM RBL 45 TO RBL 53 ORIGINAL T .125' REMAINING T .110' LOSS OF .015' FOUND TO BE OUT OF LIMITS IAW SRM 53-30-51-1A-1 REPAIRED IAW EA 1-A53-8530 REV- P/N 141A5504-26 A90733 TOOL 36647 CAL 10JUN19/ 47745 CAL 6/20/019

Part: WEB — CORRODED (BS 986) · airframe 53,796 hrs · 28,089 cycles

PASSENGER CABIN AFT WET AREA FLOOR WEB CORRODED AT BS 986, RBL 53. R&R WEB IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

FWD WET AREA INTERCOSTAL CRACKED AT BS 312 + 8' LBL 42. / REMOVED; LOCATED; DRILLED; VERIFIED AND INSTALLED FWD WET AREA INTERCOSTAL STA. 312 + 8' LBL 42 I/A/W B737-700 BOEING DWG # 141A5400 SRM 51.40.02. P./N # 141A5410012 A TAG # A21333.

Part: SPLICE — CORRODED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

PASSENGER CABIN AFT WET AREA FLOOR BEAM STA 986 RBL 55-LBL 55; UPPER FLANGE IS CORRODED ON TOP AND BOTTOM SIDES. / ACCOMPLISHED STA 986.5 FLOOR BEAM UPPER HORIZONTAL TEE CAP SPLICE REPAIR I.A.W. E.A. 1-A53-7848 REV - P/N 147A5506-8

Part: CREASE BEAM — CORRODED (BS 947-993) · airframe 53,796 hrs · 28,089 cycles

CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 947 TO BS. 993, RBL 55. R&R CREASE BEAM INNER CHORD IAW DWG AND SRM.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA INTERCOSTAL CRACKED BETWEEN BS. 277 TO BS. 294.5- 9, BL 0. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 53,796 hrs · 28,089 cycles

FWD WET AREA INTERCOSTAL CRACKED AT BS 344 + 8' LBL12. / REMOVED AND REPLACED FWD WET AREA INTERCOSTAL STA 344-360 LBL 12 IAW BOEING DWG 141A5400 REV: A. AND B737 SRM 51-40-02-0G-0 AND B737 SRM 51-40-02-0G-0. APPLIED CIC IAW B737 AMM 51-21-91-620-802

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 53,796 hrs · 28,089 cycles

FORWARD CABIN STRINGER CLIP CRACKED AT BS. 277, STR. 10R. / R&R STRINGER CLIP IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 344) · airframe 53,796 hrs · 28,089 cycles

FORWARD WET AREA INTERCOSTAL CRACKED AT BS. 344+5, BL 0. / R&R INTERCOSTAL IAW SRM & DWG.

Part: NONE — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT AFT BULKHEAD STA 947 LOWER CHORD LBL10-RBL20 HAS CORROSION / REMOVED CORROSION AT AFT CARGO PIT AFT BULKHEAD STA 947 LOWER CHORD RBL20-LBL10. ORIG T .100 REMOVED .025' REM .075' FOUND TO BE OUT OF LIMITS. RECEIVED NEW LOWR CHORD MPN 149A8118-29; INSTALLED ALL TASKS DONE IAW B737-700 SRM'S 51-10-02-0G-0; 53-00-53-1A-2; 5370-53-01-2; 51-40-02-0G-0 AND BOEING 737-NG DWG 149A8117 REV: C P/N 149A8118-29 ATAG WN6880

Part: BEAM — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT FLOOR BEAM STA 727D+6 RBL8 HAS CORROSION AROUND FASTENER HOLES / REMOVED AND REPLACED AFT CARGO FLOOR SUPPORT RAIL AT RBL 88 FROM STA 731 TO 887 ON NRC X961684 P/N 146A7503-6

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT DOOR SURROUND STRUCTURE FORWARD SHIELD STA 767-794 RBL22 UPPER AND LOWER SURFACE HAS CORROSION / REMOVED CORROSUION IAW B737 NG SRM 51-10-02-0G-0 STEP 15 ON AFT CARGO PIT DOOR SURROUND FWD SHIELD; CORROSION ON SHIELD FOUND T OBE OUT OF LIMITS 100%. LOCATED & DRILLED AND INSTALLED NEW SHIELD MPN 3 146A8127012 A TAG NO WN0264 I/A/W SRM 53-60-15-1A1 DETAIL D; BOEING 737NG DWG NO 146A0081 REV A. P/N 146A8127-9.

Part: CARGO TRACK — CORRODED (BS 827) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT FLOOR TRACK CORRODED AT BS. 827+15, RBL 13.8 UPPER SURFACE AROUND TIE DOWN. / R&R FLOOR TRACK IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 53,796 hrs · 28,089 cycles

LT Z-ANGLE CORRODED. R&R Z ANGLE IAW SRM AND AMM.

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT FLOOR TRACK CORRODED BETWEEN BS. 727D+6 TO BS. 727D+8, RBL 13.8 AROUND FASTENER HOLES. / REPAIRED FLOOR TRACK IAW SRM.

Part: STRAP — CORRODED (CARGO DOOR FRAME) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT DOOR SURROUND STRUCTURE LOWER SILL UPPER STRAP CORRODED BETWEEN BS. 787 TO BS. 847, RBL 18 UPPER SURFACE. / R&R STRAP IAW DWG & SRM.

Part: STRINGER CLIP — CORRODED (BS 807) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT STRINGER CLIP CORRODED AT BS. 807, STR. 26R. / R&R STRINGER CLIP IAW SRM AND DWG.

Part: SEAL RING — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT STA 727 BULKHEAD LOWER SEAL RING FOR APU BLEED AIR TUBE HAS CORROSION ON EDGES LBL1-RBL2 / REMOVED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO DAMAGE ALLOWED IN THAT LOCATION IAW B737-700 SRM 53-40-08-1A-3 FIG 102. REMOVED LOCATED; DRILLED AND INSTALLED SEAL RING IAW BOEING DWG # 144A2600 REV C. APPLIED CAP SEAL FASTENERS COMMON TO THE SEAL RING IAW B737-700 AMM 51-31-00-390-801. APPLIED CIC IAW B737-700 AMM 51-21-91-620-802 P/N 144A2621-1

Part: TRACK — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT FLOOR TRACK STA 927+15 LBL3 HAS CORROSION ON UPPER SURFACE AROUND TIE DOWN / REMOVED & REPLACED AFT CARGO PIT FLOOR TIE DOWN TRACK SUPPORT BLENDED CORROSION FOUND TO BE OUT OF LIMITS ORIGINAL THICKNESS .070' REMAINING .058 LOSS OF .012 IAW B737 SRM 51-40-02-0G-0 ATAG# GE1551 P/N 1470A2501-13

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT FLOOR TEE SUPPORT STA 794 RBL14.5-19 UPPER FLANGE HAS INTERGRANULAR CORROSION / REMOVED AND REPLACED DAMAGED TEE ANGLE FLOOR SUPPORT AT STR 794 RBL 14.5 PN 146A9401-42 A-TAG # A70819; I/A/W SRM 51-40-02-0G-0 PAR 7 AND AIPC 53-42-11-30 P/N 146A9401-42.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT R/H Z-ANGLE STA 727+8 TO 767 RBL21 HAS CORROSION AROUND FASTENER HOLES UPPER AND LOWER SURFACE / REMOVED CORROSION ON R/H Z ANGLE FROM STA 727 TO STA 767; ORIGINAL .040' LOSS OF .010' REMAINING .030' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. FABRICATED NEW Z ANGLE PER AFT PIT FROM STA 727 TO STA 767 ON R/H SIDE IAW BOEING DRAWING 146A7500 REV B. ACCOMPLISHED CONFORMITY INSPECTION AND VERIFIED Z ANGLE; P/N 146A7502-6; CONFORMS TO THE SPECIFICATIONS FOUND IN DRAWING 146A7500 REV B. INSTALLED Z ANGLE IAW DRAWING 146A7500 REV B AND SRM 51-40-02-0G-0 STEPS 4 AND 7. TREATED; PRIMED AND APPLIED CIC IAW AMM 51-21-41-370-803; AMM 51-21-72-370-804 AND AMM 51-21-91-620-802 P/N 146A

Part: BAFFLE — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT RIGHT SIDE BAFFLE STA 867-887 RBL 23 HAS CORROSION AROUND NUTPLATES / BLENDED OUT AREA @ AFT CARGO COMPARTMENT STA 867-887 RBL 23 BAFFLE IAW B737.700 SRM 51.10.02.0G-0. MAT.:0.032' MAT. LOSS .0007' REMAINING MAT:0.025'. FOUND TO BE OUT OF LIMITS IAW IAW B737.700 SRM 53.00.53.10.2. REMOVED & REPLACED BAFFLE PN: 146A7502-56 IAW B737.700 SRM 51.40-02.0G-0 & BOEING DRWG # 146A7500 REV. B. P/N 146A7502-6

Part: NONE — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT AFT BULKHEAD STA 947 RIGHT CURVED CHORD RBL25-RBL20 HAS CORROSION / REMOVED CORROSION AFT CARGO PIT AFT BULKHEAD STA 947 RIGHT CURVED CHORD RBL25-RBL20. ORIG 'T' .100; REMOVED .013 REM .087 FOUND TO BE OUT OF LIMITS. RECEIVED NEW R CURVED CHORD PF.S. 947. RIGHT SIDE ANGLE DOUBLER AND CHORD ASSY MPM0149 A8118-28; INSTALLED ALL TASKS DONE IAW SRM'S 51-10-02-0G-0; 53-00-53-1A-2; 51-40-02-0G-0; B737-700 AND DWG 148A8117 REV:C P/N 149A8118-28 ATAG WN1784

Part: CARGO TRACK — CORRODED (BS 767-887) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT FLOOR TRACK CORRODED BETWEEN BS. 767+4 TO BS. 887, RBL13.8, AROUND FASTENER HOLES. / REPAIRED FLOOR TRACK IAW SRM & DWG.

Part: WEB — CORRODED (BS 794-847) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT DOOR SURROUND STRUCTURE LOWER SILL WEB CORRODED BETWEEN BS. 794 TO BS. 847, RBL 27 UPPER SURFACE. / R&R WEB IAW DWG & SRM.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT FLOOR PANEL SPLICE STRAP STA 887 HAS CORROSION AROUND FASTENER HOLES / REMOVED AND REPLACED AFT CARGO FLOOR PANEL SPLICE STRAP AT STA 887 IAW SRM 51-40-02 AND SRM 51-40-04. P/N 146A9401-21 A71154

Part: ANGLE — CORRODED (FUSELAGE) · airframe 53,796 hrs · 28,089 cycles

RIGHT Z-ANGLE GOUGED. R&R Z-ANGLE IAW SRM AND DWG.

Part: BEAM — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT FLOOR BEAM STA 727+6 RBL3 HAS CORROSION AROUND FASTENER HOLE UPPER AND LOWER SURFACE / AFT CARGO FLOOR BEAM STA 727 TO STA 887 RBL 3 REPLACED ON NR X961685 146A7503-2

Part: WEB — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT BILGE VERTICAL WEB STA 727+8 LBL3-RBL3 HAS CORROSION FORWARD FACE AROUND FASTENERS AT UPPER AND LOWER ENDS / REMOVED AND REPLACED BILGE VERTICAL WEB STA 727+8 IN AFT CARGO BAR I/A/W DWG 146A0061 REV A AND SRM 51-40-02-0G-0 PAR 4+7. FABRICATED ON WO 39556-1600-0003. ORIG 'T' .032' 100% MAT LOSS. FOUND OUT OF LIMITS I/A/W SRM 53-00-53-1A-2 FIG 103 DETAIL D. RESTORED CIC I/AW AMM 51-21-91-620-802. P/N 146A3426-7

Part: RETAINER — CRACKED (RIGHT WING) · airframe 53,796 hrs · 28,089 cycles

RIGHT WING ACCESS PANEL 651GB; AFT SEAL RETAINER IS CRACKED AT O/B END. / REMOVED AND REPLACED R/H WING AFT SEAL RETAINER AT ACCESS PANEL 651GB. IAW B737-700 DWG 115A2752 REV: D; AIPC 27-51-00-15; SRM 51-40-02-0G-0

Part: BEAM — CORRODED (AFT CARGO COMPT) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT FLOOR BEAM STA 727+4 LBL13 HAS EVIDENCE OF CORROSION EMITTING FROM MATING SURFACE / REMOVED DAMAGE IAW SRM 51-10-02; VERIFIED LIMITS ORG 'T' .090' LOSS .050' REMAINING .040' OUT OF LIMITS IAW SRM 53-00-53-1A-2 DETAIL C; REMOVED FASTENERS FOR ACCESS AND REMOVED FLOOR SUPPORT IAW SRM 51-40-02-0G-0; VERIFIED MATERIAL P/N AND 10136-2007 7075 T6 IAW DWG 144A2616 REV. C PRIMED PART IAW SRM 51-20-01-0G-0 INSTALLED NEW PART IAW SRM 51-40-02-0G-0 APPLIED CIC AREA REWORK IAW SRM 51-20-01-0G-0 P/N 144A2616-7

Part: FLOOR SUPPORT — CORRODED (BS 727+8-14) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO PIT FLOOR BEAM CORRODED BETWEEN BS. 727+8 TO BS. 727+14, LBL 3, AROUND FASTENER HOLES UPPER AND LOWER SURFACE. / R&R FLOOR BEAM IAW SRM & DWG.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,796 hrs · 28,089 cycles

FRAME FLANGE DENTED. REPAIRED IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 53,796 hrs · 28,089 cycles

L/H WING TRAILING EDGE MIDSPAR BULKHEAD AFT CURVED SEAL RETAINER ANGLE CRACKED / R&R ANGLE IAW SRM & DWG.

Part: PLATE — CRACKED (R/H WING) · airframe 53,796 hrs · 28,089 cycles

RIGHT WING T/E BELOW #8 SPOILER ACTUATOR; WIGGLE PLATE IS CRACKED. / REMOVED AND REPLACED R/H WING T/E BELOW #8 SPOILER ACTUATOR WAFFLE PLATE IAW SRM 51-40-02-0G-0 AND BOEING DWG 115A3700 SHT 6 REV: B.

Part: PLATE — CRACKED (RT WING) · airframe 53,796 hrs · 28,089 cycles

R/H WING TRAILING EDGE JUST INBOARD OF PYLON SAIL TAIL, WIGGLE PLATE CRACKED. / R&R WIGGLE PLATE IAW SRM & DWG.

Part: PLATE — CRACKED (RT WING) · airframe 53,796 hrs · 28,089 cycles

R/H WING TRAILING EDGE BELOW INBOARD END OF #8 SPOILER, WIGGLE PLATE CRACKED. / R&R WIGGLE PLATE IAW SRM.

Part: SUPPORT — CORRODED (FWD CARGO LH) · airframe 53,796 hrs · 28,089 cycles

FWD PIT STA 500D AFT BULKHEAD FLOOR SUPPORT HAS CORROSION ON TOP SURFACE LH SIDE 2EA SPOTS / REMOVED AND REPLACED FLOOR SUPPORT AT STA 500D P/N 143A9485-35 SI # 7530142 A-TAG #WN0120 I/A/W SRM 51-40-02-0G-0. ORIG 'T' .080' .016' LOSS .064' REM FOUND OUT OF LIMITS SRM 53-00-53-1A-2 FIG 103 DETAIL D. P/N 143A9485-35

Part: BRACKET — CRACKED (RT WING) · airframe 53,796 hrs · 28,089 cycles

R/H WING TRAILING EDGE FIXED TRAILING EDGE SUPPORT BRACKET CRACKED AT FLAP DEFLECTION CONTROL RIB. / REMOVED BRACKET IAW DWG AND SRM.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,796 hrs · 28,089 cycles

FWD CARGO PIT FRAME INNER FLANGE DENTED AT BS. 500, LBL 28. REPAIRED CHORD FRAME PER EA.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 53,796 hrs · 28,089 cycles

RIGHT WING T/E ABOVE PYLON SAIL TAIL; UPPER SEAL SUPPORT BRACKET IS CRACKED. / REMOVED AND REPLACED UPPER SEAL SUPPORT BRACKET ON RIGHT WING T/E ABOVE PYLON SEAIL TAIL IAW BOEING DWG DWG 115A2930 REV - AND B737 SRM 51-40-02-0G 'A' TAG 2766 P/N 115A2982-10.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 53,796 hrs · 28,089 cycles

AFT CARGO DOOR CUT-OUT FWD CORNER THRESHOLD CRACKED. / AFT CARGO DOOR FWD CORNER THRESHOLD REPAIR ON BACKSHOP WORK ORDER # 39566-1600-0001 IAW EA 1-A53-2076.

Part: ANGLE — ELONGATED (FWD CARGO LH) · airframe 53,796 hrs · 28,089 cycles

FORWARD CARGO PIT LEFT SIDE Z-ANGLE STA 400-500+9' HAS ELONGATED HOLES / REMOVED AND REPLACED LH ZEE ANGLE BS 396-5001J ON NRC X961413

Part: RIB — CRACKED (RT WING) · airframe 53,796 hrs · 28,089 cycles

R/H WING TRAILING EDGE, LOWER PANEL SUPPORT CRACKED OUTBOARD OF FLAP DEFLECTION CONTROL RIB. / R&R RIB IAW DWG AND SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 53,796 hrs · 28,089 cycles

FWD CARGO COMPARTMENT FORWARD CORNER SCUFF PLATE CRACKED. / RECEIVED FWD CORNER SCUFF PLATE FROM BACK SHOP. VERIFIED ACCOMPLISHED WELD REPAIR IAW EA 1-A53-2076 REV 11. INSTALLATION ACCOMPLISHED ON WO # 39553-1400-0007

Part: STRAP — CORRODED (FUSELAGE) · airframe 53,796 hrs · 28,089 cycles

FORWARD CARGO PIT DOOR SURROUND FRAME INNER FAIL SAFE STRAP CORRODED AROUND FASTENER HOLE AT BS. 493, RBL 28. R&R STRAP IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 53,796 hrs · 28,089 cycles

VERTICAL PRESSURE DECK WEB CRACKED AT BS. 663, LBL 42. REPAIRED DECK IAW SRM.

Part: BRACKET — BROKEN (LEFT WING) · airframe 53,796 hrs · 28,089 cycles

LEFT WING TRAILING EDGE OUTBOARD SUPPORT BEAM FOR PANEL 551DB FORWARD ATTACH BRACKET IS BROKEN OFF / REMOVED AND REPLACED SUPPORT BARCKET; P/N 115A5552-1; ON L/H WING T/E SUPPORT BEAM FOR PANEL 551DB IAW SRM 51-40-02-0G-0 AND DRAWING 115A2001 REV -

Part: ANGLE — CORRODED (LEFT WING) · airframe 53,796 hrs · 28,089 cycles

LEFT WING REAR SPAR TANK 1 AFT BOOST PUMP UPPER BONDING STRAP HAS CORROSION AT ATTACH ANGLE / REMOVED CORRODED BONDING STRAPS AND UPPER ATTACH ANGLE. INSTALLED SERVICEABLE BONDING STRAPS AND ATTACH ANGLES. PERFORMED ELECTRICAL BOND OF END-CAP AND BONDING STRAP/ANGLE. TEST IS GOOD PER AMM 28-22-41-400-801

Part: SHIELD — CORRODED (FWD CARGO RH) · airframe 53,796 hrs · 28,089 cycles

FORWARD CARGO PIT AFT SHIELD STA 492-500A RBL 24 HAS CORROSION AROUND FASTENER HOLES ON UPPER SURFACE (PREVIOUSLY BLENDED) / REMOVED CORROSION ON FWD CARGO AFT SHIELD STA 492 - 500A RBL 24 IAW SRM 51-10-02-0G-0; ORIGINAL .032 REMAIN .027 LOSS .005; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. INSTALLED AFT SHIELD STA 492 - 500A RBL 24 IAW SRM 51-40-02-0G-0 + B DWG 143A0080 P/N 143A8126-31 TOOL 29270 CAL 6/19/19

Part: GUSSET — CRACKED (BS 500D) · airframe 53,796 hrs · 28,089 cycles

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

Part: ANGLE — CRACKED (BS 500B) · airframe 53,796 hrs · 28,089 cycles

FORWARD CARGO PIT RIGHT SIDE BAFFLE CLIP FORWARD SIDE OF BS. 500B FRAME CRACKED. R&R BAFFLE CLIP IAW DWG & SRM.

Part: NONE — CRACKED (FWD CARGO LH) · airframe 53,796 hrs · 28,089 cycles

FORWARD CARGO PIT LEFT SIDE BAFFLE CLIP AFT SIDE OF STA 440 FRAME IS CRACKED / REMOVED AND REPLACED FWD CARGO PIT LEFT SIDE BAFFLE CLIP AFT SIDE OF STA 440 FRAME IAW B-737 SRM 51-40-02-0G-0 AND DWG 143A7505 REV B ATAG A17245

Part: BRACKET — CRACKED (LEFT WING) · airframe 53,796 hrs · 28,089 cycles

LEFT WING TRAILING EDGE MIDSPAN BULKHEAD AFT SEAL RETAINER BRACKET AFT OF LATERAL WEB IS CRACKED / REMOVED AND REPLACED LEFT WING TRAILING EDGE MIDSPAN BULKHEAD AFT SEAL RETAINER BRACKET IAW BOEING DWG 115A2930 RE:- AND B737 SRM 51-40-02-0G-0 'A' TAG A70611 P/N 115A2982-9

Part: NONE — CRACKED (FWD CARGO LH) · airframe 53,796 hrs · 28,089 cycles

FORWARD CARGO PIT LEFT SIDE BAFFLE CLIP AFT SIDE OF STA 500C FRAME IS CRACKED / REMOVED BAFFLE CLIP FROM STA 500C L/H FWD PIT IAW SRM 51-40-02-0G-0; VERIFIED NEW PART IAW DWG 143A7505 REV. B P/N 143A7502UG LOCATED AND DRILLED NEW BAFFLE CLIP IAW SRM 51-40-05-0G-0. INSTALLED NEW BAFFLE CLIP AT STA 500C L/H FWD PIT IAW SRM 51-40-02-0G-0 TAG A82647

Part: BRACKET — CRACKED (RIGHT WING) · airframe 53,796 hrs · 28,089 cycles

RIGHT WING T/E ABOVE PYLON SAIL TAIL; LOWER SEAL SUPPORT BRACKET IS CRACKED. / REMOVED AND REPLACED LOWER SEAL SUPPORT BRACKET RIGHT WING T/E ABOVE PYLON SAIL TAIL IAW BOEING DWG 115A2930 REV AND B737 SRM 51-40-05-0G-0; 51-40-02-0G-0 'A' TAG A86357 P/N 115A2953-2

Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 53,796 hrs · 28,089 cycles

FORWARD CARGO PIT RIGHT SIDE Z-ANGLE STA 500A-500B RBL 24 HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION; 100% LOSS ; OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2. REMOVED AND REPLACED FWD PIT Z ANGLE FROM STA 500 A TO 500 D IAW B737-700 DWG 143A7500 REV:- ; SRM 51-40-02-0G-0 P/N 143A7501-4.

Part: ANGLE — CRACKED (LEFT WING) · airframe 53,796 hrs · 28,089 cycles

LEFT WING TRAILING EDGE REAR SPAR IRSS 142 ATTACH ANGLE FOR UPPER SUPPORT BEAM IS CRACKED / REMOVED AND REPLACED LEFT WING TRAILING EDGE REAR SPAR IRSS 142 ATTACH ANGLE IAW B737-700 SRM 51-40-02-0G-0; AIPC 57-50-00-34

Part: BAFFLE — CRACKED (FWD CARGO LH) · airframe 53,796 hrs · 28,089 cycles

FORWARD CARGO PIT LEFT SIDE BAFFLE STA 500-500A LBL24 NUTPLATE HOLE IS CRACKED (AS SEEN FROM BOTTOM) / REMOVED; INSTALLED NEW ; LOCATED; DRILLED BAFFLE FWD FWD CARGO L/H STA 500-500A LBL 24 I/A/W B737-700 SRM 51-40-02; SRM 51-40-05; BOEING DWG# 143A7505 P/N# 143S7510 ATAG# A68982

Part: FLAP — DELAMINATED (LT WING) · airframe 53,316 hrs · 27,814 cycles

LT WING OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAMINATED. REPAIRED AFT FLAP PER EA.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 53,170 hrs · 27,724 cycles

FOUND CORROSION ON TEE ASSEMBLY AFT BAG BIN STA 7726 ASSEMBLY NO# 146A9401-4 / REMOVED AND REPLACED FLLOR PNL TEE ASSEMBLY AFT BAG BIN STA 7726 IAW AMM 25-52-10

Part: PANEL — DELAMINATED (FWD FUSELAGE) · airframe 52,976 hrs · 27,600 cycles

ON WALK AROUND FOUND RAM AIR AFT DOOR PANEL DELAMINATED. / REPAIRED PANEL PER CMM 21-53-02 AND SRM 51-70-04. SEE ATTACHED SAM 326 FOR DETAILS.

Part: BATTERY — FAILED (CABIN) · airframe 52,222 hrs · 27,145 cycles

AFT GALLEY EMERGENCY LIGHT BATTERY FAILED DEEP CYCLE TEST. R&R BATTERY PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 51,690 hrs · 26,804 cycles

LT EMERGENCY EXIT SIGN IN AFT GALLEY LOOSE. SECURED SIGN PER SRM.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 51,196 hrs · 26,505 cycles

EMERGENCY LIGHT SWITCH GUARD BROKEN. R&R SWITCH GUARD IAW AMM.

Part: LUG — BROKEN (RT WING) · airframe 50,019 hrs · 25,819 cycles

RIGHT WING MID FLAP BEAM PANEL ROD SUPPORT EAR BROKEN OFF. REPAIRED THE LUG IAW SRM.

Part: TRACK — CRACKED (CABIN) · airframe 48,919 hrs · 25,159 cycles

SEAT TRACK CRACKED @ 15E; 12E; 5E. / REMOVED AND REPLACED PER SIP.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 47,389 hrs · 24,221 cycles

RH HORIZONTAL STABILIZER UPPER SLIDER SEAL CRACKED. / RH HORIZONTAL STAB UPPER SLIDER SEAL CRCKED REPLACED WITH NEW SLIDE SEAL ATAG A38141 PIN 181A8025-2 IAW ACO 8454-53

Part: SLIDE — LOOSE (R1 DOOR) · airframe 46,759 hrs · 23,855 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE LOOSE. SECURED THE SLIDE IAW MT.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 46,225 hrs · 23,517 cycles

FWD GALLEY LH EMERGENCY LIGHT FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 46,016 hrs · 23,390 cycles

FORWARD ENTRY DOOR EXIT SIGN LENS MISSING. INSTALLED LENS PER SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,175 hrs · 22,342 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY FAILED AT LOCATION M01674. R & R BATTERY PACK IAW AMM.

Part: COLLAR — BROKEN (L1 DOOR) · airframe 44,175 hrs · 22,342 cycles

L1 DOOR SLIDE GIRT BAR RETAINING COLLAR BROKEN. R & R COLLAR IAW MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,904 hrs · 22,194 cycles

LEFT WING EXTERIOR EMER EXIT LIGHT AFT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 43,129 hrs · 21,755 cycles

RIGHT BULLNOSE EMER LIGHT COVER LOOSE AT ROW 13. SECURED COVER IAW AMM.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 41,738 hrs · 20,937 cycles

R2 DOOR LOWER OUTLET EMER EXIT SIGN LIGHT LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,072 hrs · 18,844 cycles

LEFT EXTERNAL OVERWING EMER LIGHT INOPERATIVE. RELAMPED LIGHT ASSEMBLY IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,072 hrs · 18,844 cycles

LEFT INTERCOSTAL CRACKED AT BS 1016. R & R INTERCOSTAL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,072 hrs · 18,844 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,072 hrs · 18,844 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 38,072 hrs · 18,844 cycles

STRINGER CRACKED AT BS 926, STRINGER 18R. REPAIRED STRINGER IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 38,072 hrs · 18,844 cycles

AFT CARGO BAY BULKHEAD STRAP CRACKED AT BS 727, RBL 40. R & R STRAP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,072 hrs · 18,844 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,072 hrs · 18,844 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,072 hrs · 18,844 cycles

FRAME CRACKED AT BS 360, STRINGER 8L. REPAIRED FRAME IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,072 hrs · 18,844 cycles

FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW ER & EA.

Part: CONNECTOR — BROKEN (CABIN) · airframe 38,072 hrs · 18,844 cycles

L2 DOOR ESCAPE SLIDE LIGHT CONNECTOR BROKEN. R & R CONNECTOR IAW MM.