N254WN

Part: FASTENER — LOOSE (GIRT BAR) · airframe 62,577 hrs · 37,673 cycles

FWD SERVICE DOOR GIRT BAR WILL NOT STOW PROPERLY. COMPLIED WITH EA M-23-125-01839. INSTALLED FWD SERVICE DOOR GIRT BAR STOW FASTNER

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 62,254 hrs · 37,487 cycles

FWD ENTRY EXTERIOR LIGHT IS INOP <[01]. REMOVED AND REPLACED LAMP ON L1 DOOR EMERGENCY LAMP (EXTERIOR) PER AMM 33-51-04.

Part: SENSOR — FAULTY (ZONE 200) · airframe 61,588 hrs · 37,090 cycles

TRAILING EDG FLAPS FAILED TO EXTEND ASYMMETRY LOCKED FLAPS AT 0-1 LANDED FLAPS UP. BRAKE COOLING PWB INDICATED NORMAL PROCEDURES AND PARK AT GATE <[01]. TROUBLE SHOT FOUND BAD #1 T/E FLAP SKEW SENSOR REMOVED AND REPLACED #1 T/E FLAP SKEW SENSOR OPS CHECKED ND TESTED NO DEFECTS FOUND REF AMM 27-59-01.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 61,420 hrs · 36,992 cycles

EMERGENCY LIGHT INOP STOWBIN 13 FED<[01] RELAMPED EMERGENCY LIGHT AT STOWBIN 13 FED AND OPS CHECK GOOD IAW SWA B737-700 AMM 33-51-03-960-801. <BR><BR>PO 1092574.1;[02] RELAMPED EMERGENCY LIGHT AT STOWBIN 13 FED AND OPS CHECK GOOD IAW SWA B737-700 AMM 33-51-03-960-801.<BR><BR>PO 1092574.1

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 58,345 hrs · 35,076 cycles

CRACK FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2024-121780<[01] REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DWG 453A1610 SHEET 7 REV C MATERIAL USED: P/N: 2024T3-080 P.O: 2023 195509.;[02] REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DWG 453A1610 SHEET 7 REV C MATERIAL USED: P/N: 2024T3-080 P.O: 2023 195509.

Part: PLATE — DETERIORATED (GIRT BAR) · airframe 58,345 hrs · 35,076 cycles

DETERIORATE GIRT BART FITTING PLATE (2EA) AND SHIM (2EA) OF ENTRY DOOR AT FWD GALLEY AREA 2024-121730<[01] REPLACED GIRT BART FITTING PLATE (2EA) AND SHIM (2EA) OF ENTRY DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801;[02] TASK CARD COMPLETE.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 58,345 hrs · 35,076 cycles

BROKEN ENTRY DOORWAY LINNING HANDLE AND NUTS AT AFT GALLEY AREA 2024-121715<[01] REPLACED ENTRY DOORWAY LINNING HANDLE AND NUTS AT AFT GALLEY AREA IAW SOPM-20-50-01 REV. 38;[02] CERTIFIED WORK PERFORMED

Part: PLATE — DETERIORATED (GIRT BAR) · airframe 58,345 hrs · 35,076 cycles

DETERIORATE GIRT BAR FITTING PLATE (2EA) AND SHIM (2EA) SERVICE DOOR AT FWD GALLEY AREA 2024-121731<[01] REPLACED GIRT BAR FITTING PLATE (2EA) AND SHIM (2EA) SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 AMM 26-66-02-400-801;[02] TASK CARD COMPLETE.

Part: PLATE — CORRODED (BS 1006-1016) · airframe 58,345 hrs · 35,076 cycles

CORROSION PLATE LOCATE LBL3 BTW BS1016 TO BS1006 AFT GALLEY AREA 2024-121682<[01] REPLACED PLATE LOCATE LBL3 BTW BS1016 TO BS1006 AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 147A5600 SHEET 1 REV H<BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[02] REPLACED PLATE LOCATE LBL3 BTW BS1016 TO BS1006 AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 147A5600 SHEET 1 REV H<BR>SEE INDIVIDUAL SIGNSOFF BELOW.JOB COMPLETE.

Part: ANGLE — CRACKED (RT WING) · airframe 58,345 hrs · 35,076 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS278 RT WING 2024-121671<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS278 RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] TASK COMPLETED

Part: ANGLE — CRACKED (BS 663) · airframe 58,345 hrs · 35,076 cycles

CRACK ANGLE LOCATED BS663.75 AND RBL41 AT CENTER SECTION 2024-121673<[01] TOOL USED TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25.;[02] REPLACED ANGLE LOCATED BS663.75 AND RBL41 AT CENTER SECTION IAW B737-700 SRM 51-40-02 AND DWG 111A1000 REV. <BR>SEE INDIVIDUAL SIGNOFF BELOW;[03] CORRECTED STEP 2<BR>REPLACED ANGLE LOCATED BS663.75 AND RBL41 AT CENTER SECTION IAW B737-700 SRM 51-40-02 AND DWG 111A1000 REV:A<BR>SEE INDIVIDUAL SIGNOFF BELOW;[04] REPLACED ANGLE LOCATED BS663.75 AND RBL41 AT CENTER SECTION IAW B737-700 SRM 51-40-02 AND DWG 111A1000 REV:A<BR>SEE INDIVIDUAL SIGNOFF BELOW <BR>AS RII

Part: LATCH — INCORRECT (SEAT) · airframe 58,345 hrs · 35,076 cycles

SEAT ASSEMBLY RH DOUBLE EXIT NO RECLINE 1.0 INCH UPRIGHT ONE WAY FOOD TRAY LACH ON POSITION 11D 11E 11F 2024-121658<[01] REPLACED ASSEMBLY RH DOUBLE EXIT NO RECLINE 1.0 INCH UPRIGHT ONE WAY FOOD TRAY LACH ON POSITION 11D 11E 11F IAW B/E AEROSPACE CMM-25-21-42 Ï¿½TEM 10C PAGE 10108 REV.5;[02] CORRECTED STEP 1: REPLACED SEAT FOODTRAY LATCH ASSEMBLY ON POSITION 11D 11E 11F (3 EA) IAW B/E AEROSPACE CMM-25-21-42 REV 5. STEP 3. S. (8) PAGE 7010 FIGURE 8 ITEM -10C PAGE 10108;[03] CERTIFIED STEP 2 COMPLETED

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 58,345 hrs · 35,076 cycles

CORROSION ON PLATE ACCESS PANEL 653BB IB MIDFLAP AT RT WING 2024-121697<[01] REPLACED PLATE ACCESS PANEL 653BB IB MIDFLAP AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] TASK COMPLETED

Part: SKIN — CRACKED (RT NR 8 SLAT) · airframe 58,345 hrs · 35,076 cycles

CRACK LOWER SURFACE SLAT 8 AT RT WING 2024-121617<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN. 200053402.DUE DATE. 24-AUG-24;[02] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN. 200053402.DUE DATE. 24-AUG-24 USED ON STEP 5;[03] REPAIRED LOWER SURFACE SLAT 8 AT RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 FIG 202;ALTERNATIVE 1 SHEET 1. SEE INDIVIDUAL SIGNSOFF BELOW.;[04] REPAIRED LOWER SURFACE SLAT 8 AT RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 FIG 202;ALTERNATIVE 1 SHEET 1. SEE INDIVIDUAL SIGNSOFF BELOW.

Part: PLATE — CRACKED (RT WING) · airframe 58,345 hrs · 35,076 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 214 AT RT WING 2024-121620<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 214 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] CERTIFIED STEP 1 COMPLETED

Part: ANGLE — CRACKED (LT WING) · airframe 58,345 hrs · 35,076 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS265 AT LT WING 2024-121626<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS265 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG # 115A2930 SHEET 7 REV. - SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS265 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG # 115A2930 SHEET 7 REV. - SEE INDIVIDUAL SIGN OFF BELOW

Part: SKIN — CRACKED (LT NR 2 SLAT) · airframe 58,345 hrs · 35,076 cycles

CRACK LOWER SURFACE SLAT 2 AT LT WING 2024-121618<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN. 200053402.DUE DATE. 24-AUG-24;[02] REPAIRED LOWER SURFACE SLAT 2 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202. SEE INDIVIDUAL SIGNSOFF BELOW.;[03] REPAIRED LOWER SURFACE SLAT 2 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202. SEE INDIVIDUAL SIGNSOFF BELOW.

Part: PLATE — CORRODED (BS 787-807) · airframe 58,345 hrs · 35,076 cycles

CORROSION BILGE AREA PLATE LOCATED BTW BS 787 TO BS 807 AT RBL 20 AND WL 155.5 AT AFT CARGO COMPARTMENT 2024-121566<[01] REPLACED PLATE LOCATED BTW BS 787 TO BS 807 AT RBL 20 AND WL 155.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 146A8340 SHEET 22 REV A. SEE INDIVIDUAL SIGNOFFS BELOW;[02] JOB COMPLETED AND CERTIFIED RII

Part: SHIELD — CORRODED (BS 767-787 RBL21) · airframe 58,345 hrs · 35,076 cycles

CORROSION BILGE AREA SHIELD PLATE BTW BS 767 TO BS 787 AT RBL 21 AND WL 155.5 AT AFT CARGO COMPARTMENT 2024-121567<[01] REPLACED SHIELD PLATE BTW BS 767 TO BS 787 AT RBL 21 AND WL 155.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081; SHEET 31; REV -. SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED SHIELD PLATE BTW BS 767 TO BS 787 AT RBL 21 AND WL 155.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081; SHEET 31; REV -. SEE INDIVIDUAL SIGNOFF BELOW.

Part: SUPPORT — CORRODED (BS 727-767 RBL21) · airframe 58,345 hrs · 35,076 cycles

CORROSION SUPPORT ZEE BTW BS 727 TO BS 767 AT RBL 21 AND WL 155.5 AT AFT CARGO COMPARTMENT 2024-121569<[01] ULTRASONIC EQUIPMENT USED P/N: 35DL; S/N: 091419910; DUE DATE: 13-MAR-24;[02] REPLACED SUPPORT ZEE LOC LOC BS 727 TO BS 767 AT RBL 21 AND WL 155.5 AT AFT CARGO COMPARTMENT IAW 737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG:146A7500 SHEET:85 REV:A<BR>SEE INDIVIDUAL SIGNOFF BELOW;[03] CORRECTIVE ACTION CERTIFIED

Part: ANGLE — CORRODED (BS 767-787 RBL21) · airframe 58,345 hrs · 35,076 cycles

CORROSION BILGE AREA ANGLE LOCATED BTW BS 767 TO BS 787 AT RBL 21 AND WL 155.5 AT AFT CARGO COMPARTMENT 2024-121568<[01] REPLACED ANGLE LOCATED BTW BS 767 TO BS 787 AT RBL 21 AND WL 155.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081; SHEET 31; REV -.SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED ANGLE LOCATED BTW BS 767 TO BS 787 AT RBL 21 AND WL 155.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081; SHEET 31; REV -.SEE INDIVIDUAL SIGNOFF BELOW.

Part: CASE — CORRODED (FUEL QTY IND) · airframe 58,345 hrs · 35,076 cycles

CORROSION LEADING EDGE FUEL QUANTITY INDICATOR CASE AT RT WING 2024-121577<[01] REPLACED REFUEL PANEL (P15) IAW B737-700 AMM 28-21-00-000-801 AND AMM 28-21-00-400-801 AND TEST IS OK. SEE FOR INDIVIDUAL SIGNOFF BELOW.;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SHEAR TIE — CRACKED (BS 277 S10R) · airframe 58,345 hrs · 35,076 cycles

CRACK TIE CLIP LOCATED BS277 AND S-10R AT FWD GALLEY AREA 2024-121486<[01] REPLACED TIE CLIP AND FASTENERS LOCATED BS277 AND S-10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02; AND B737-700 DWG 141A11110 SHEET 18 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1. REPLACED TIE CLIP AND FASTENERS LOCATED BS277 AND S-10R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 B737-700 DWG 141A1110 SHEET 18 REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED TIE CLIP AND FASTENERS LOCATED BS277 AND S-10R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 B737-700 DWG 141A1110 SHEET 18 REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 58,345 hrs · 35,076 cycles

CRACK INSPAR RIB 120.30 AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2024-121487<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 600D; S/N 200048001 DUE DATE 01-MAY-24 USED ON STEP 4 AND 5;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 600D; S/N 200048001 DUE DATE 01-MAY-24 USED ON STEP 7;[03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 142811019 DUE DATE 23 JAN 25.;[04] REPAIRED INSPAR RIB 120.30 AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737 700 SRM 55-10-09-2R-5 REPAIR 5.SEE INDIVIDUAL SIGN OFF BELOW;[05] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FRAME — CRACKED (BS 312 S5-6L) · airframe 58,345 hrs · 35,076 cycles

CRACK FRAME ON BS 312 BETWEEN S-5L TO S-6L FWD GALLEY AND LAV 2024-121484<[01] REPAIRED FRAME ON BS 312 BETWEEN S-5L TO S-6L FWD GALLEY AND LAV IAW M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPAIRED FRAME ON BS 312 BETWEEN S-5L TO S-6L FWD GALLEY AND LAV IAW M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW.

Part: UNKNOWN — CRACKED (BS 303 S17L) · airframe 58,345 hrs · 35,076 cycles

CRACK INNER CHORD LOCATED BS 303.9 AND S-17L AT FWD GALLEY AREA 2024-121443<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A21147758 DUE DATE: 21/NOV/24;[02] REPLACED INNER CHORD AND FASTENERS LOCATED BS 294 TO BS 360 AND S-17L AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-40-02; SRM B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #141A8110; SHEET 9; REV A.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED INNER CHORD AND FASTENERS LOCATED BS 294 TO BS 360 AND S-17L AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-40-02; SRM B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #141A8110; SHEET 9; REV A.<BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: FLOOR SUPPORT — CRACKED (BS 277-295 BL 0) · airframe 58,345 hrs · 35,076 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-121442<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG NO. 141A5400; SHEET 20; REV.-<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG NO. 141A5400; SHEET 20; REV.-<BR>RII ITEM<BR>SEE INDIVIDUAL SIGNS-OFF BELOW

Part: PLATE — CORRODED (BS 1016-1032) · airframe 58,345 hrs · 35,076 cycles

CORROSION FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 BTW BL 0 TO LBL 42 AND WL 208.9 AT AFT GALLEY AREA 2024-121463<[01] REPLACED FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 BTW BL 0 TO LBL 42 AND WL 208.9 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG: 147A5600 SHEET: 32 REV: B <BR>SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 BTW BL 0 TO LBL 42 AND WL 208.9 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG: 147A5600 SHEET: 32 REV: B <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOOR SUPPORT — CRACKED (BS 344-360 RBL32) · airframe 58,345 hrs · 35,076 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 32 FWD GALLEY AND LAV 2024-121460<[01] REPLACED NEW WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 32 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG #141A5400 SHEET 33 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOOR SUPPORT — CRACKED (BS 344-360 RBL12) · airframe 58,345 hrs · 35,076 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 12 FWD GALLEY AND LAV 2024-121450<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 12 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING NO. 141A5400; SHEET 13; REV.-<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1 <BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 12 FWD GALLEY IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING NO. 141A5400; SHEET 13; REV.-<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 2<BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 12 FWD GALLEY IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DRAWING NO. 141A5400; SHEET 13; REV.-<BR>SEE INDIVIDUAL SIGN OFF BELOW;[04] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 12 FWD GALLEY IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DRAWING NO. 141A5400; SHEET 13; REV.-<BR>SEE INDIVIDUAL SIGN OFF BELOW ITEM RII

Part: STUB FRAME — CRACKED (BS 294 S17R) · airframe 58,345 hrs · 35,076 cycles

CRACK FLOOR STRUCTURE ON STUB FRAME LOCATED BS 294.5 AND S-17R AT FWD GALLEY AREA 2024-121461<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 210138103 AND DUE DATE: 02-MAY-24.;[02] TOOL USED ON STEP 6: EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022235; DUE DATE: 07-SEP-24;[03] PERFORMED REPAIR ON STUB FRAME LOCATED BS 294.5 AND S-17R AT FWD GALLEY AREA IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7<BR>SEE INDIVIDUAL SIGNOFF BELOW;[04] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOOR SUPPORT — CRACKED (BS 328-344 LBL46) · airframe 58,345 hrs · 35,076 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 328 TO BS 344 AND LBL 46 FWD GALLEY AND LAV 2024-121447<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 328 TO BS 344 AND LBL 46 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG NO. 141A5400; SHEET 44; RE. -<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CORRODED (BS 1016-1032) · airframe 58,345 hrs · 35,076 cycles

CORROSION FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT RBL 2 AND WL 208.9 AT AFT GALLEY AREA 2024-121472<[01] REPLACED FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT RBL 2 AND WL 208.9 AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG:147A5730 SHEET:23 REV:C SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT RBL 2 AND WL 208.9 AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG:147A5730 SHEET:23 REV:C SEE INDIVIDUAL SIGNOFF BELOW.JOB COMPLETE .

Part: LENS — DETERIORATED (EMERGENCY LIGHT) · airframe 58,345 hrs · 35,076 cycles

DETERIORATED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA 2024-121464<[01] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA IAW SOPM-20-50-01 REV-N.38;[02] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA IAW SOPM-20-50-01 REV-N.38

Part: FLOOR SUPPORT — CRACKED (BS 344-360 LBL 1) · airframe 58,345 hrs · 35,076 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND LBL 1 FWD GALLEY AND LAV 2024-121453<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND LBL 1 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG #141A5400 SHEET 32 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT ANGLE — CRACKED (BS 500D S19R) · airframe 58,345 hrs · 35,076 cycles

CRACK BODY FAIRING SUPPORT ANGLE BS 500D LEVEL STRINGER 19R AT LOWER FUSELAGE 2024-121341<[01] REPLACED SUPPORT ANGLE ANGLE AND FASTENERS ON BODY FAIRING BS 500D LEVEL STRINGER 19R AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02; 51-10-02 AND DWG 116A3010; SHEET 9; REV C. SEE INDIVIDUAL SIGNOFFS BELOW;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: BRACKET — CRACKED (BS 540 RBL 7) · airframe 58,345 hrs · 35,076 cycles

CRACK BRACKET ASSY BS 540 AND RBL 7 AT AIR CONDITIONING BAY 2024-121432<[01] REPLACED BRACKET ASSY LOCATED BS 540 AND RBL 7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] REPLACED BRACKET ASSY LOCATED BS 540 AND RBL 7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.JOB COMPLETE.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 58,345 hrs · 35,076 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2024-121314<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A23357775;DUE DATE:31-JAN-25.;[02] TOOL USED ON STEP#4; TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N:1753759; CAL DUE DATE:12-APR-24;[03] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975

Part: PRESSURE DECK — CRACKED (ZN 100 FUS LOWER) · airframe 58,345 hrs · 35,076 cycles

CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB BTW RBL 39 TO RBL 50 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH:0.316 INCH APPROX. 2024-121306<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[03] REPAIRED HORIZONTAL PRESSURE DECK WEB LOC BTW RBL 38 TO RBL 60 MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 PARAGRAPH 4. <BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[04] REPAIRED HORIZONTAL PRESSURE DECK WEB LOC BTW RBL 38 TO RBL 60 MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 PARAGRAPH 4. <BR>SEE INDIVIDUAL SIGNSOFF BELOW.<BR>CERTIFIED AS RII

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,345 hrs · 35,076 cycles

INOP BATTERY PACK ON POSITION CENTER CABIN RT SIDE AT PASSENGER CABIN 2024-121261<[01] REPLACED BATTERY PACK ON POSITION CENTER CABIN RT SIDE AT PASSENGER CABIN IAW B737-700 AMM-33-51-06-960-805 ?TEST IS OK?;[02] COMPLETE TASK CERTIFIED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,345 hrs · 35,076 cycles

INOP BATTERY PACK ON POSITION CENTER CABIN LT SIDE AT PASSENGER CABIN 2024-121260<[01] REPLACED BATTERY PACK ON POSITION CENTER CABIN LT SIDE AT PASSENGER CABIN IAW B737-700 AMM-33-51-06-960-805 ?TEST IS OK?;[02] COMPLETE TASK CERTIFIED

Part: VAPOR BARRIER — CRACKED (BS 663 RBL 36) · airframe 58,345 hrs · 35,076 cycles

CRACK BODY STATION 663.75 VAPOR BARRIER LOCATED LBL 36; WL 159 AT MAIN WHEEL WELL COMPARTMENT 2024-121228<[01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 07-NOV-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196127 DUE DATE: 25/JAN/25.;[03] TOOL USED SCALE P/N: CR5200 S/N: 8343110809 DUE DATE: 21 FEB 24.;[04] TOOL USED HOT BONDER P/N: HCS9200B; S/N: 15102320; DUE DATE: 25-JAN-25.;[05] TOOL USED SCALE P/N: CL5000 S/N: AE-408753 DUE DATE: 27-JUL-24.;[06] ULTRASONIC EQUIPMENT USED P/N: EPOCH 650; S/N: 190859705 AND DUE DATE: 23-OCT-24.;[07] REPAIRED VAPOR BARRIER LOCATED LBL 36; WL 159 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10 SEE INDIVIDUAL SIGN OFFS BELOW;[08] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 58,086 hrs · 34,923 cycles

MISSING EXIT SIGN FWD GALLEY AT FOOT LEVEL BY TRASH CAN<[01] REPLACED EXIT LENS AT FWD GALLEY IAW AMM 33-51?01

Part: SIGN — UNSECURE (ZN 200 FUS TOP) · airframe 58,071 hrs · 34,915 cycles

EMERGENCY EXIT LIGHT SIGN ROW 12 IS UNSECURED<[01] REINSTALLED CENTER AISLE OVERHEAD EXIT SIGN PER AMM 33-51-01

Part: SIGN — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 57,059 hrs · 34,264 cycles

EXIT SIGN AT THE OVERWING IN THE AISLE HAS FALLEN OFF<[01] REATTACHED EXIT SIGN AT THE OVERWING AISLE I/A/W SIP.

Part: LIGHT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 56,907 hrs · 34,163 cycles

CABIN CENTER AISLE O/H E/E EXIT LIGHT NOT SECURE AT EMERGENCY ROWS<[01] RESECURED CABIN CENTER AISLE O/H E/E EXIT LIGHT AT EMERGENCY ROWS IN REF TO AMM 33-51-01

Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 55,893 hrs · 33,509 cycles

PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES AND COUNTERSINKS.<[01] REMOVED AND REPLACED PER SRM 53-51-01.

Part: COVER — INOPERATIVE (ZN 200 FUS TOP) · airframe 55,652 hrs · 33,343 cycles

VELCROW ON EMERGENCY EXIT COVER INOP. A/C RIGHT<[01] REMOVED AND REPLACED VELCRO ON EMERGENCY EXIT HATCH COVER PANEL PER AM 20-10-06

Part: COVER — MISSING (ZN 800 DOOR) · airframe 54,900 hrs · 32,851 cycles

FWD SERVICE DOOR EMERGENCY LIGHT COVER MISSING. REPLACED FWD SERVICE DOOR EMERGENCY LIGHT COVER IAW AMM 33-51-01.

Part: WEB — CORRODED · airframe 52,929 hrs · 31,519 cycles

CORROSION WEB LOCATED BTW BS294.5 TO BS303.9;WL 174.1 AND LBL 47 AT EQUIPMENT ELECTRONIC COMP. 2022-192878 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[02] REPLACED WEB LOCATED BTW BS294.5 TO BS303.9;WL 174.1 AND LBL 47 AT EQUIPMENT ELECTRONIC COMPARTMENT IAW B737-700 SRM 51-10-02 AND DRAWING 141A1350 REV:D; SEE INDIVUDUAL SIGNOFF BELOW.;[03] REPLACED WEB LOCATED BTW BS294.5 TO BS303.9;WL 174.1 AND LBL 47 AT EQUIPMENT ELECTRONIC COMPARTMENT IAW B737-700 SRM 51-10-02 AND DRAWING 141A1350 REV:D; RII SEE INDIVUDUAL SIGNOFF BELOW.

Part: PLATE — CRACKED (FWD FUSELAGE) · airframe 52,929 hrs · 31,519 cycles

CRACK ON PLATE BTW STA 312 AT LEVEL STRINGER 17R AT EQUIPMENT EL ECTRONIC COMP 2022-192879 / [01] REPLACED PLATE (STABILIZER STRAP) BTW STA 312 TO BS 344 AT LEVEL STRINGER 17R AT EQUIPMENT EL ECTRONIC COMP IAW SRM B737-700 51-10-02 AND DRAWING 141A5400 REV-A; SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CORRECTED STEP 1.<BR>REPLACED PLATE (STABILIZER STRAP) BTW STA 312 TO BS 344 AT LEVEL STRINGER 17R AT EQUIPMENT EL ECTRONIC COMP IAW SRM B737-700 51-10-02; 51-40-02 DRAWING 141A5400 REV-A; SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPLACED PLATE (STABILIZER STRAP) BTW STA 312 TO BS 344 AT LEVEL STRINGER 17R AT EQUIPMENT EL ECTRONIC COMP IAW SRM B737-700 51-10-02; 51-40-02 DRAWING 141A5400 REV-A; SEE INDIVIDUAL SIGNOFFS BELOW.

Part: INTERCOSTAL — CORRODED (AFT CARGO BAY) · airframe 52,929 hrs · 31,519 cycles

CORROSION INTERCOSTAL LOCATED BETWEEN BS 787 AND BS 807 S-25R AT WL 156 AT AFT CARGO COMPARTMENT 2022-192851 / [01] REPLACED INTERCOSTAL LOCATED BETWEEN BS 787 TO BS 807 S-25R AT WL 156 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 AND DRAWING 146A0081 REV:-; SEE INDIVIDUAL SIGNOFF BELOW.;[02] TASK COMPLETED ; RII <BR> SEE INDIVIDUAL SIGNOFF BELOW.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 52,929 hrs · 31,519 cycles

CORROSION ANGLE LOCATED AT BS 947 BETWEEN S-25R AND S-26L WL156 AFT BULKHEAD AT AFT CARGO COMPARTMENT 2022-192870 / [01] REPLACED BRACKET AND FASTENERS LOCATED AT BS 947 BETWEEN S-25R AND S-26L WL156 AFT BULKHEAD AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DWG 149A8110 REV B; SEE INDIVIDUAL STEP SIGNS OFF BELOW.;[02] REPLACED BRACKET AND FASTENERS LOCATED AT BS 947 BETWEEN S-25R AND S-26L WL156 AFT BULKHEAD AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DWG 149A8110 REV B; SEE INDIVIDUAL STEP SIGNS OFF BELOW.<BR>RII

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 52,929 hrs · 31,519 cycles

CRACK ANGLE - SUPPORT LOCATED AT BS 867 AT LEVEL S-26L AFT CARGO COMPARTMENT 2022-192871 / [01] REPLACED ANGLE AND FASTENER LOCATED AT BS 867 AT LEVEL S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING 149A8102 REV E. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] REPLACED ANGLE AND FASTENER LOCATED AT BS 867 AT LEVEL S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING 149A8102 REV E. SEE INDIVIDUAL STEP SIGN OFFS BELOW RII

Part: TRACK — CRACKED (AFT CARGO) · airframe 52,929 hrs · 31,519 cycles

CRACK TRACK RBBL 13.84 AT BS787 AFT CARGO COMPARTMENT 2022-192852 / [01] TOOL USED PN NORTEC 500D SN N500X1693P030456 DUE DATE 26-JAN-23;[02] CALIPER P/N: 500-197-30; S/N: B20189521; DUE DATE: 03-DEC-22.;[03] REPAIRED CARGO TRACK LOCATED RBBL 13.84 AND BTW BS 747 TO BS 787 AFT CARGO COMPARTMENT IAW SRM B737-700 53-00-53-2R-3 REPAIR 3 FIGURE 203 ALTERNATIVE 1 AND 2; SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPAIRED CARGO TRACK LOCATED RBBL 13.84 AND BTW BS 747 TO BS 787 AFT CARGO COMPARTMENT IAW SRM B737-700 53-00-53-2R-3 REPAIR 3 FIGURE 203 ALTERNATIVE 1 AND 2; SEE INDIVIDUAL SIGNOFF BELOW.<BR>CERTIFIED AS RII

Part: ANGLE — CRACKED (AFT CARGO) · airframe 52,929 hrs · 31,519 cycles

CRACK ANGLE - SUPPORT LOCTED BETWEEN BS 907 AND BS 927 BETWEEN S-25R AND S-27R AFT POSITION AFT CARGO COMPARTMENT 2022-192854 / [01] REPLACED NEW NGLE AND FASTENER I.A.W SRM B737-700 51-40-02;SRM B737-700 51-10-02 ITEM 9 AND DRAWING 147A7221 REV-; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] REPLACED NEW NGLE AND FASTENER I.A.W SRM B737-700 51-40-02;SRM B737-700 51-10-02 ITEM 9 AND DRAWING 147A7221 REV-; SEE INDIVIDUAL STEP SIGN OFFS BELOW<BR>CERTIFIED AS RII

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 52,929 hrs · 31,519 cycles

CORROSION STRAP LOCATED BETWEEN BS 767 AND BS 787 AT LEVEL S-25R AND S-25L WL156 BILGE AREA AT AFT CARGO COMPARTMENT 2022-192861 / [01] REPLACED STRAP LOCATED BETWEEN BS 767 AND BS 787 AT LEVEL S-25R AND S-25L WL156 BILGE AREA AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9.;[02] TASK COMPLETED

Part: NONE — CRACKED · airframe 52,929 hrs · 31,519 cycles

CUSTOMER REQUEST-CRACK ON VAPOR BARRIER LWR LEFT WEB STA 663.75 LBL 48 2022-192849 / [01] TOOL USED CALIPER P/N 500-197-30; S/N A18234378; DUE DATE: 21-SEP-22.;[02] TOOL USED= HOT BONDER P/N: HCS9200B-AV; S/N: 18196119; DUE DATE: 24-FEB-23.;[03] TOOL USED= SCALE P/N: SP202; S/N: B527136635; DUE DATE: 16-SEP-22;[04] REPAIRED VAPOR BARRIER LWR LEFT WEB STA 663.75 LBL 48 AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10;[05] REPAIRED VAPOR BARRIER LWR LEFT WEB STA 663.75 LBL 48 AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10<BR>RII;[06] CORRECTED STEP 5 <BR>REPAIRED VAPOR BARRIER LWR LEFT WEB STA 663.75 LBL 48 AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10<BR>SEE INDIVIDUAL SIGN OFFS BELOW <BR>RII

Part: ANGLE — CRACKED (AFT CARGO BAY) · airframe 52,929 hrs · 31,519 cycles

CRACK ANGLE - SUPPORT LOCATED AT BS727 AT FWD BULKHEAD AREA AFT CARGO COMPARTMENT 2022-192850 / [01] REPLACED ANGLE SUPPORT LOCATED AT BS727 AT FWD BULKHEAD AREA AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 144A2600 REV- SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] REPLACED ANGLE SUPPORT LOCATED AT BS727 AT FWD BULKHEAD AREA AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 144A2600 REV- SEE INDIVIDUAL STEP SIGN OFFS BELOW

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 52,929 hrs · 31,519 cycles

CORROSION STRAP LOCATED AT BS 887 WL 156 AT LEVEL S-25R AND 25L BILGE AREA AT AFT CARGO COMPARTMENT 2022-192859 / [01] REPLACED STRAP LOCATED AT BS 887 WL 156 AT LEVEL S-25R AND 25L BILGE AREA AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9.;[02] CORRECTED STEP 1; REPLACED STRAP LOCATED AT BS 887 WL 156 AT LEVEL S-25R AND 25L BILGE AREA AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9. SEE INDVIDUAL SINGOFFS BELOW.;[03] REPLACED STRAP LOCATED AT BS 887 WL 156 AT LEVEL S-25R AND 25L BILGE AREA AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9. SEE INDVIDUAL SINGOFFS BELOW.

Part: INTERCOSTAL — CORRODED (AFT CARGO BAY) · airframe 52,929 hrs · 31,519 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 747 AND BS 767 S-25R WL 156 AT AFT CARGO COMPARTMENT 2022-192865 / [01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 747 AND BS 767 S-25R WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A7502 REV. : - AND B737-700 SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 747 AND BS 767 S-25R WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A7502 REV. : - AND B737-700 SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII

Part: NONE — CRACKED · airframe 52,929 hrs · 31,519 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS 907 AND BS 927 BETWEEN S-25R AND S-27R FWD POSITION AFT CARGO COMPARTMENT 2022-192869 / [01] REPLACED NEW NGLE AND FASTENER I.A.W SRM B737-700 51-40-02;SRM B737-700 51-10-02 ITEM 9 AND DRAWING 147A7221 REV-; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] REPLACED NEW NGLE AND FASTENER I.A.W SRM B737-700 51-40-02;SRM B737-700 51-10-02 ITEM 9 AND DRAWING 147A7221 REV-; <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 52,929 hrs · 31,519 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2022-192825 / [01] TOOL USED; DIGITAL CALIPER P/N: 500-197-30 S/N: A21146543 DUE DATE:11-OCT-22.;[02] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 52,929 hrs · 31,519 cycles

CRACK AROUND HOLES ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2022-192804 / [01] TOOL USED: CALIPER P/N: 500-464 S/N: 15331932 DUE DATE: 26-OCT-22.;[02] CORRECTIVE ACTION 1 ENTERED BY ERROR.<BR>CORRECTED TOOL USED IS CALIPER P/N: 500-464 S/N: 15331926 DUE DATE: 28-SEP-22.;[03] TOOL USED: HOT BONDER P/N HCS9200B S/N 18175478 DUE DATE 05-AUG-22.;[04] TOOL USED: SCALE P/N: 1863T62 S/N: AE-40571 DUE DATE: 19-MAY-22.;[05] TOOL USED: HOTBONDER P/N HCS9200B S/N 18175478 DUE DATE 05-AUG-22.;[06] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 99180027; DUE DATE: 07-SEP-22;[07] REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10 . SEE INDIVIDUAL SIGNOFFS BELOW.;[08] JOB TASK COMPLETED.

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 52,929 hrs · 31,519 cycles

CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2022-192805 / [01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV. - . SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV. - . SEE INDIVIDUAL SIGNOFF BELOW<BR>CERTIFIED AS RII <BR>TASK COMPLETED

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 52,929 hrs · 31,519 cycles

CRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2022-192806 / [01] REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV.- . SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 REV.- . SEE INDIVIDUAL SIGNOFF BELOW.<BR>CERTIFIED AS RII <BR>TASK COMPLETED

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 52,929 hrs · 31,519 cycles

CRACK SUPPORT BRACKET LOCATED BS 1016 BTW STR2L TO STR2R AT UPPER FUSELAGE 2022-192793 / [01] REPLACED SUPPORT BRACKET LOCATED BS 1016 BTW STR2L TO STR2R AT UPPER FUSELAGE I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 176A3101 SHEET 4<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: PANEL — CRACKED (R/H HORIZ. STAB.) · airframe 52,929 hrs · 31,519 cycles

CRACK SEAL - PLATE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2022-192826 / [01] REPLACED SEAL-PLATE ON ACCESS PANEL 343AT AT RH HORIZONTAL STAB I.A.W SRM B737-700 51-40-02;[02] REPLACED SEAL-PLATE ON ACCESS PANEL 343AT AT RH HORIZONTAL STAB I.A.W SRM B737-700 51-40-02

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 52,929 hrs · 31,519 cycles

CRACK GUSSET LOCATED BS500D AND STR21R FWD CARGO COMPARTMENT 2022-192807 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[02] REPLACED GUSSET LOCATED BS500D AND STR21R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A9481 REV A SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] REPLACED GUSSET LOCATED BS500D AND STR21R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A9481 REV A SEE INDIVIDUAL STEP SIGN OFFS BELOW<BR>CERTIFIED AS RII

Part: RIB — CRACKED (VERTICAL STAB) · airframe 52,929 hrs · 31,519 cycles

CRACK ON RIB 8 ACCESS PANEL 321A AT VERTICAL STABILIZER 2022-192706 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.;[02] REPLACED RIB 8 AND FASTENERS LOC. ACCESS PANEL 321 AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND DWG 174A0103 REV. -. SEE INDIVIDUAL SINGOFFS BELOW.;[03] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PANEL — ERODED (VERT. STAB.) · airframe 52,929 hrs · 31,519 cycles

EROSION ACCESS PANEL 321A AT VERTICAL STABILIZER 2022-192704 / [01] TOOL USED: CALIPER P/N 500-464 S/N 15331932 DUE DATE 26-OCT-22.;[02] TOOL USED: HOTBONDER P/N HCS9200B-AV S/N 18196119 DUE DATE 24-FEB-2023.;[03] TOOL USED: MULTIMETER P/N: FLUKE87 S/N: 42180179 DUE DATE: 21-FEB-23.;[04] REPAIRED ACCESS PANEL 321A AT VERTICAL STABILIZER AS PER B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGNOFFS BELOW;[05] REPAIRED ACCESS PANEL 321A AT VERTICAL STABILIZER AS PER B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGNOFFS BELOW

Part: SERVICE DOOR — CORRODED (FUSELAGE) · airframe 52,929 hrs · 31,519 cycles

CORROSION TOILET SERVICE DOOR 145AL AT LEVEL STR24L; WL158 AT LOWER FUSELAGE 2022-192700 / [01] REMOVED AND REPLACED TOILET SERVICE DOOR 145AL AT LEVEL STR24L; WL158 AT LOWER FUSELAGE IAW B737-700 AMM 52-49-07 SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK CARD COMPLETED

Part: ACCESS PANEL — CRACKED (R/H WING) · airframe 52,929 hrs · 31,519 cycles

CRACK ACCESS PANEL 661BB TRAILING EDGE AROUND HOLES RT WING 2022-192583 / [01] TOOL USED: CALIPER P/N: 500-464 S/N: 15331932 DUE DATE: 26-OCT-22.;[02] CORRECTIVE ACTION 1 ENTERED BY ERROR CORRECTED TOOL IS CALIPER P/N: 500-464 S/N: 15331926 DUE DATE: 28-SEP-22.;[03] TOOL USED: HOT BONDER P/N HCS9200B S/N 18175478 DUE DATE 05-AUG-22.;[04] TOOL USED: SCALE P/N: 1863T62 S/N: AE-40571 DUE DATE: 19-MAY-22.;[05] TOOL USED: HOTBONDER P/N HCS9200B S/N 18175478 DUE DATE 05-AUG-22.;[06] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 99180027 ; DUE DATE: 07-SEP-22;[07] REPAIRED ACCESS PANEL 661BB TRAILING EDGE AROUND HOLES RT WING AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10 . SEE INDIVIDUAL SIGNOFFS BELOW.;[08] JOB TASK COMPLETED.

Part: PANEL — DEBONDED (R/H WING) · airframe 52,929 hrs · 31,519 cycles

CUSTOMER REQUEST - DEBONDED IB MAIN FLAP T/E WEDGE PANEL AT RT WING. 2022-192659 / [01] TOOL USED CALIPER P/N 500-464 S/N 15331926 DUE DATE 28 SEP 22;[02] UT TOOL USED: AUDIBLE BOND TESTER; P/N: S-3; S/N: 064; DUE DATE: 12-JUL-22;[03] TOOL USED HOT BONDER P/N HCS9200B S/N 15102320 DUE DATE 16 JAN 23;[04] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18175478 DUE DATE: 05-AUG-22 . POSITECTOR 6000 P/N:NS2 S/N:138341 DUE DATE: 25-JUN-22;[05] TOOL USED; SCALE P/N:CL5000 S/N:AE-409560 DUE DATE: 19-MAY-22;[06] REPAIRED IB MAIN FLAP T/E WEDGE PANEL AT RT WING AS PER B737-700 SRM 57-53-01-2R-18 REPAIR 18 AND B737-700 SRM 51-70-10-2R-0 REPAIR GENERAL. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] CORRECTIVE ACTION 6 ENTERED BY ERROR.<BR><BR>PERFORMED INTERIM REPAIR ON IB MAIN FLAP T/E WEDGE PANEL AT RT WING AS PER B737-700 SRM 57-53-01-2R-18 REPAIR 18 AND B737-700 SRM 51-70-10-2R-0 REPAIR GENERAL. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] PERFORMED INTERIM REPAIR ON IB MAIN FLAP T/E WEDGE PANEL AT RT WING AS PER B737-700 SRM 57-53-01-2R-18 REPAIR 18 AND B737-700 SRM 51-70-10-2R-0 REPAIR GENERAL. SEE INDIVIDUAL SIGNOFFS BELOW. RII COMPLETED

Part: PLATE — CORRODED (AFT CARGO BAY) · airframe 52,929 hrs · 31,519 cycles

CORROSION ON PLATE ON AFT CARGO COMP OVER PANEL 140CF AFT CARGO COMP 2022-192591 / [01] REPLACED PLATE ON AFT CARGO COMP OVER PANEL 140CF AFT CARGO IAW SRM B737-700 51-40-02;[02] TASK COMPLETED; RII

Part: PLATE — CRACKED (L/H FUSELAGE) · airframe 52,929 hrs · 31,519 cycles

CRACK INBOARD FAN COWL PLATE ON INTERNAL AREA ON ENGINE 1 2022-192554 / [01] REPLACED PLATE LOC. INBOARD FAN COWL INTERNAL AREA ON ENGINE 1. IAW B737-700 SRM 51-40-02-0G-0 AND 51-10-02 ITEM (9. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CORRECTED STEP 1: REPLACED PLATE LOC. INBOARD FAN COWL INTERNAL AREA ON ENGINE 1. IAW B737-700 SRM 51-40-02-0G-0 AND 51-10-02 ITEM (9). SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPLACED PLATE LOC. INBOARD FAN COWL INTERNAL AREA ON ENGINE 1. IAW B737-700 SRM 51-40-02-0G-0 AND 51-10-02 ITEM (9). SEE INDIVIDUAL SIGNOFFS BELOW<BR>TASK COMPLETED

Part: LIGHT — FAILED · airframe 52,536 hrs · 31,273 cycles

ONE EACH EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK / [01] R&R EMERGENCY BATTERY PACK AT LOCATION M01675 PER M/M 33-51-06

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 52,350 hrs · 31,174 cycles

FOUND CRACK ON AFT CARGO FLOOR PANEL OVER 15? INCHES AND EDGE WORN OUT ; / [01] OKAY TO CONT PER MEL 25-16-01 SP 1B AUTH# 44326 <BR><BR>P/N REQUIRED 144A5810-128; [02] R&R AFT CARGO FLOOR PANEL 140BF AMM 25-52-10

Part: BATTERY — FAULTY (CABIN) · airframe 51,690 hrs · 30,780 cycles

FWD CABIN EMERGENCY FLASHLIGHT INDICATOR NOT FLASHING REFERENCE TTG8Q0093D7P FOR ACFT 212 ; / [01] REMOVED AND REPLACED FWD CABIN EMERGENCY LIGHT BATTERY PER AMM 25-64-00

Part: NONE — FAILED · airframe 51,371 hrs · 30,597 cycles

SUPPLEMENTAL INFORMATION: WHEN EXTENDING FLAPS FOR LANDING WITH FLAP HANDLE AT 2, TRAILING EDGE FLAP ASYMMETRY OCCURRED. RIGHT FLAP BARELY MOVED AND LEFT FLAP MOVED PARTWAY TOWARD 1. NO ROLLING TENDENCY NOTED. / FSEU BITE CK SHOWS FC#27-52260 (TE FLAP SNSR R). TROUBLESHOT IAW FIM#27-51-820, R&R RH FLAP TRANSMITTER (T428) IAW MM#27-58-01, OPS CHECKS GOOD.

Part: VAPOR BARRIER — CRACKED · airframe 49,108 hrs · 29,303 cycles

FOUND CRACK ON VAPOR BARRIER LOWER LEFT WEB STA 663.75 LBL 48 LENGTH: 2'. CRACK IS WITHIN ALLOWABLE DAMAGE LIMITS, PER SRM 57-10-10-1A-2(4) NOT MORE THAN 16 INCH ZONE 1. PERFORMED INTERMIN REPAIR, PER SRM57-10-10-1A-2(4)(A). VISUAL INSPECTION OF REPAIR AREA AT 1200 FLT CYCLES OR MORE FREQUENTLY. ENSURE CRACK HAS NOT GROWN PAST THE INTERIM SEAL. IF ADDITIONAL DAMAGE IS FOUND DURING VISUAL INSPECTION AND THE COMBINED DAMAGE IS MORE THAN 20 INCHES, THEN YOU MUST REPLACE INTERIM REPAIR WITH PERMANENT REPAIR. MORE THAN ONE CRACK IS PERMITTED ON THE LEFT AND RIGHT OF BL 0.0.

Part: WEB — CRACKED (RT WING) · airframe 48,902 hrs · 29,179 cycles

RIGHT WING UPPER TRAILING EDGE PANEL SUPPORT WEB INBOARD OF DEFLECTION CONTROL RIB CRACKED IN UPPER OUTBOARD CORNER / REMOVED AND REPLACED RIGHT WING UPPER TRAILING EDGE PANEL SUPPORT WEB INBOARD OF DEFLECTION CONTROL IAW SRM 51-40-02

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 48,902 hrs · 29,179 cycles

RH HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED SLIDING SEAL PER AMM 53-31-31

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 48,902 hrs · 29,179 cycles

FWD. CARGO COMPARTMENT DISTRIBUTION BAY; STA. 540; FLOOR PANEL BREAKS L/H AND R/H OF BL0 ARE CRACKED / REMOVED AND REPLACED FLOOR PANEL BREAKS L/H AND R/H PER SRM 51-10-02 AND SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,822 hrs · 28,490 cycles

FORWARD EMERGENCY EXIT LIGHT BULB ABOVE L/H OWE IS OUT. / REMOVED; REPLACED AND PERFORMED GOOD FUNCTIONAL TEST OF FORWARD EMERGENCY EXIT LIGHT BULB ABOVE L/H OWE IAW AMM 33-51-01-960-801 STEP 2.C.(1)(A) (3) AND (2);(4).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,822 hrs · 28,490 cycles

LEFT AFT ESCAPE SLIDE EMERGENCY EXIT LIGHT L732 IS OUT. / REMOVED; REPLACED AND PERFORMED GOOD FUNCTIONAL TEST OF LEFT AFT ESCAPE SLIDE EMERGENCY EXIT LIGHT BULB (L732) IAW AMM 33-51-04-960-801 STEP 2.F.(1)(A) (B);(D);(2).

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 47,822 hrs · 28,490 cycles

LH HORIZONTAL STAB IS CRACKED ON RIB ASSY 4; STAB STA 120.30; ON STIFFENER 4; LOWER PART / REPAIRED L/H HORIZONTAL STABILIZER RIB ASSY 4; STAB STA 120.3 ON STIFFENER 4 LOWER PART IAW SRM 55-10-09-2R-4 89004U 12MAY20

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 47,822 hrs · 28,490 cycles

LH HORIZONTAL STAB IS CRACKED ON RIB ASSY 4; STAB STA 120.30; ON STIFFENER 3; LOWER PART / REPAIRED L/H HORIZONTAL STABILIZER RIB ASSY 4; STAB STA 120.30 ON STIFFENER REV 3 LOWER PART IAW SRM 55-10-09-2R-5. 89004U 12MAY20

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,822 hrs · 28,490 cycles

RH HORIZONTAL STAB HAS CRACKS ON RIB ASSY 4; STAB STA 120.30 ON STIFFENER 3 LOWER SIDE. / REMOVED DAMAGE AND INSTALLED REPAIR PORTS AT R/H HORIZONTALL STAB RIB ASSY 4; STAB STA 120.30 ON STIFFENER 3 LOWER SIDE IAW. SRM 55-10-09-2R-4 88920U 08MAY20 (REFERENCE U160893)

Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 47,822 hrs · 28,490 cycles

LEFT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFING DAMAGE FORWARD OF BS 1016. REMOVED AND REPLACED LH CLOSURE SKATE ANGLE BS 1006 BS 1016 PER SRM 5140020G0; DWG 147A0030; DWG 147A0070 AND DWG 147A3200; NO SRM ALLOWABLE DAMAGE.

Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 47,822 hrs · 28,490 cycles

RIGHT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFING DAMAGE FORWARD OF BS 1016. REMOVED AND REPLACED RH CLOSURE SKATE ANDGLE PER SRM 5140020G0 AND DWG 147A0030; DWG 147A0070; DWG 147A3200 NO SRM ALLOWABLE DAMAGE.

Part: ANGLE — CHAFED (FUSELAGE) · airframe 47,822 hrs · 28,490 cycles

LEFT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS CHAFING DAMAGE AFT OF BS 1016. REPAIRED CLOUSURE ANGLE AT BS 1016 PER SRM 5380712R6.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,822 hrs · 28,490 cycles

RH HORIZONTAL STAB INSPAR RIB AT STA 120.3 AFT LOWER FLANGE IS CRACKED O/B SIDE / REMOVED DAMAGE PART AND INSTALLED REPAIR PARTS AT RH HORIZONTAL STAB INSPAR RIB AT 120.30 AFT LWR FLANGE O/B SIDE IAW. EA 20-155-00551 REV IR. 88920U 15MAY20 ER 20-02566 REV IR.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,822 hrs · 28,490 cycles

RH HORIZONTAL STAB INSPAR RIB AT STA 120.3 FWD LOWER FLANGE IS CRACKED O/B SIDE / REMOVED THE DAMAGE PART AND INSTALLED REPAIR PART AT RH HORIZONTAL STAB INSPAR SIB AT STA 120.3 FWD LOWER FLANGES O/B SIDE IAW. SRM 55-10-09-2R-5. 88920U 13MAY20

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,822 hrs · 28,490 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT L.B.L 31; W.L. 154. / REPAIRED CRACKS AT L.B.L 31; W.L. 154 AT B.S. 663 LOWER COMPOSITE BULKHEAD IAW SRM 51-70-04-2R-10.

Part: WEB — CRACKED (FUSELAGE) · airframe 47,822 hrs · 28,490 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT L.B.L 31; W.L. 154. ACCESS AS REQUIRED . AND REINSTALL. / REMOVED AND REINSTALLED VAPOR BARRIER WEB BS 663 AT L.B.L 31; W.L 154 PER SRM 51-40-02; REF DWG; 111A1000; 149A7216; AND 111A1151; 111A1001 AND AMM 53-51-21-000-802; 53-51-21-400-802; 20-10-21-400-801 20-10-21-000-801. LOWER COMPOSITE BULKHEAD WAS REPAIRED ON V161013

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 47,822 hrs · 28,490 cycles

BULB SEAL ATTACH ANGLE IS CRACKED JUST ABOVE #1 ENGINE AFT FAIRING TIP; LEFT WING ORSS 264. / REMOVED AND REPLACED BULB SEAL ATTACH ANGLE ABOVE #1 ENGINE AFT FAIRING TIP; LEFT WING ORSS 264 P/N 115A2953-1 IAW. SRM 51-40-02 AND AIPC 57-50-00-25 88920U 09MAY20

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 47,822 hrs · 28,490 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / WELDED CRACK ON FCB FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 IAW SRM # 53-30-15-2R-1 PARA 4.13(2) AND (4) & (5)

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 47,822 hrs · 28,490 cycles

DURING COMPLETION OF CCN: 753-201-00-02 FOUND HORIZONTAL PRESSURE DECK TO BE CRACKED AT BS 664 LBL 31 WL201. / REPAIRED HORIZONTAL PRESSURE DECK AT BS 663-BS 675 LBL 30 TO LBL 60 WL 201 IAW SRM 53-40-57-2R-2 REPAIR 2

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,822 hrs · 28,490 cycles

RH HORIZONTAL STAB HAS CRACKS ON RIB ASSY 4; STAB STA 120.30; ON STIFFENERS 2 AND 3; LOWER PART. / REMOVED DAMAGE AND INSTALLED REPAIR PARTS AT R/H HORIZONTAL STAB ON RIB ASSY 4; STAB STA 120.30 ON STIFFENER 2 LOWER PART IAW. SRM 51-40-02. AND DWG 182A4001; DWG. 182A3001; DWG 182A2401 88920U 15MAY20 SRM 55-10-09-2R-4

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 47,822 hrs · 28,490 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / WELDED AFT CARGO BAY FWD CORNER SCUFF PLATE USING FR4043 FILER ROD LOT # 1131213 IAW SRM # 53-60-15-2R-1 PARA 4.B.(2) AND (4). 57609U 13MAY20

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 47,822 hrs · 28,490 cycles

LH HORIZONTAL STAB IS CRACKED ON RIB ASSY 4; STAB STA 120.30; ON STIFFENER 2; LOWER PART. / REPAIRED L/H HORIZONTAL STABILIZER RIB ASSY 4; STAB STA 120.30 ON STIFFENER 2 LOWER PART IAW SRM 55-10-09-2R-5 89004U 12MAY20

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,777 hrs · 28,461 cycles

LEFT EMERGENCY OVER WING LIGHT INOP / R&R BATTERY FOR LEFT OVERWING EMERGENCY LIGHT PER M/M 35-51-06

Part: FLOOR PANEL — CRACKED (FWD CARGO COMPT) · airframe 46,190 hrs · 27,436 cycles

FWDCARGOPANEL 12 DCF CRACKED FLOOR / REMOVED AND REPLACED FWD CARGO FLOOR PANEL IAW AMM 25-52-10

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 46,109 hrs · 27,384 cycles

R2 DOOR EMERGENCY EXIT SLIDE OUT OF ITS CONTAINER. / REPOSITIONED SLIDE PER MT.

Part: PROXIMITY SWITCH — FAULTY (LE SLAT) · airframe 45,311 hrs · 26,851 cycles

SUPPLEMENTAL INFORMATION, DIVERSION/DECLARED EMERGENCY, LEADING EDGE FLAPS TRANSIT LIGHT (#3) WITH TE FLAPS IN ANY POSITION. R&R #3 SLAT INBOARD PROXIMITY SWITCH IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 45,181 hrs · 26,768 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. R&R EMERGENCY LIGHT BATTERIESPER AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 44,205 hrs · 26,142 cycles

AFT-FACING OVERWING EXIT SIGN LENS MISSING. R&R SIGN ASSEMBLY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,562 hrs · 24,452 cycles

R1 DOOR EXTERIOR SLIDE LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: HOUSING — DAMAGED (CABIN) · airframe 41,562 hrs · 24,452 cycles

PASSENGER CABIN FORWARD LAVATORY EMERGENCY LIGHT HOUSING DAMAGED ON AFT WALL LOWER AREA NEAR L1 DOOR. R&R LIGHT HOUSING IAW AMM.

Part: FITTING — LOOSE (L1 DOOR) · airframe 41,562 hrs · 24,452 cycles

L1 DOOR ESCAPE SLIDE FORWARD FLOOR GIRT BAR FITTING ADAPTER PLATE INSTALLATION LOOSE. SECURED FITTING IAW AMM.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 41,562 hrs · 24,452 cycles

FORWARD LAV FIRE DETECTOR SIREN DOES NOT SOUND ON DETECTION. R&R SMOKE DETECTOR IAW AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

A/C BAY UPPER CHORD CRACKED AT BS 663, RBL 8. REPAIRED CHORD IAW EA AND MM.

Part: WEB — CRACKED (CABIN) · airframe 41,562 hrs · 24,452 cycles

AFT CABIN FLOOR HORIZONTAL WEB IS CRACKED BS 987; RBL 45; WL 208. / REPLACED AFT CABIN SHEAR WEB AT STATION 987 TO 1016 RBL 45 IAW BOEING DWG 147A5730REV C REMOVAL AND INSTALLATION OF SHEAR WEB ACCOMPLISHED ON X760949 SAM 326 E237946 ITEM 1 AND 9; SAM 326 E237986 ITEM 1

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 41,562 hrs · 24,452 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140CF FWD TRANSITION STRIP HAS SURFACE CORROSION. / REPLACED; PART # 146A9401-4 SI # 3530573; A TAG# WN 0694 IAW B737-700 DWG 146A7500 REV H. PART PLACED ON SHELF WILL BE INSTALL ON WORK CARD 37513 1600 0027; & J JAPNEL-141-CLOSE.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,562 hrs · 24,452 cycles

PASSENGER CABIN FLOOR PANEL 241AAF UPPER SURFACE HAS MULTIPLE LINES OF DELAMINATION. / REPAIRED PASSENGER CABIN FLOOR PANEL 241 AAF UPPER SURFACE ENTIRE AREA IAW B737 SRM 53-00-50-2R-1. CURED IN OVEN FOR 1 HR AT 150 DEGREES. IN AT 1:00PM OUT AT 2:00PM. .

Part: FLOOR PANEL — DENTED (CABIN) · airframe 41,562 hrs · 24,452 cycles

PASSENGER CABIN FLOOR PANEL 242AF HAS A DENT ON THE INBD EDGE 16 INCHES FROM THE FWD EDGE. / REPAIRED PASSENGER CABIN FLOOR PANEL 242AF I/B EDGE 16' FROM THE FWD EDGE IAW B737 SRM 53-00-50-2R-4 CURED IN OVEN FOR 1HR IN AT 9:30AM-OUT AT 10:30AM A94393 A49522 A44883

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,562 hrs · 24,452 cycles

PASSENGER CABIN FLOOR PANEL 241ACF UPPER SURFACE HAS MULTIPLE LINES OF DELAMINATION. / REPAIRED PASSENGER CABIN FLOOR PANEL 241ACRF OF UPPER SURFACE 1 PLY DEEP DELAMINATION IPW B737-700 SRM 53-00-50-2R-0 REV 64 AND B737-700 SRM 53-00-50-2R-1 REV 64. FLOOR PANEL READY TO BE INSTALLED AFTER 1:30AM 25MAY18. A80188; A59144; A86613; A97437; A06044

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,562 hrs · 24,452 cycles

PASSENGER CABIN FLOOR PANEL 241ADF UPPER SURFACE HAS MULTIPLE LINES OF DELAMINATION. / EVALUATED; PREPPED; CLEANED AND REPAIRED MULTIPLE AREASOF UPPER SURFACE SKIN DAMAGE TO FLOORBOARD 241 ADF IAW B737 SRM 53-00-50-2R-1 PAR 3 (A;C-F;K1;L1;M1) REV 64

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 41,562 hrs · 24,452 cycles

PASSENGER CABIN FLOOR PANEL 242CF HAS A PUNCTURE 37.5 INCHES FROM THE FWD EDGE CENTERLINE. / REPAIRED CABIN FLOOR PANEL 242CF 37.5 INCHES FROM THE FWD EDGE CENTERLINE I/A/W 737-700 SRM 53-00-50-2R-0 REV 64; SRM 53-00-50-2R-0 GENERAL REV 64.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,562 hrs · 24,452 cycles

PASSENGER CABIN FLOOR PANEL 242VF UPPER SURFACE HAS MULTIPLE LINES OF DELAMINATION. / REPAIRED TOP SKIN OF FLOOR PANEL 242VF AS REQ IAW B737 SRM 53-00-50-2R-1 REPAIR 1 PAR 3 (A-C;EM) REV 64. A19298; A80188; A59142; A24893; A17133; A06044

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 41,562 hrs · 24,452 cycles

PASSENGER CABIN FLOOR PANEL 241DF UPPER SURFACE HAS MULTIPLE LINES OF DELAMINATION. / EVALUATED AND REPAIRED PASSENGER CABIN FLOOR PANEL 241DF OF UPPER SURFACE TOP LAYER DELAMINATION WITH NO DAMAGE TO COMPOSITE SUBSTRATE IAW B737-700 SRM 53-00-50-2R-1 REV 64 AND B737-700 SRM 53-00-50-2R-0 REPAIR GENERAL REV64 A59144;A94393

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R&R INTERCOSTAL IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

RT CREASE BEAM CORRODED AT BS 727C. REPAIRED CREASE BEAM IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 294.5 TO BS 312, RBL 15. R&R INTERCOSTAL IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

RT CREASE BEAM CORRODED BETWEEN BS 727E TO BS 747. R&R CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

LT CREASE BEAM WEB CORRODED BETWEEN BS 787 TO BS 807. REPAIRED WEB IAW SRM & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

LT CREASE BEAM WEB CORRODED AT BS 727B, AFT SIDE. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

LT CREASE BEAM WEB CORRODED BETWEEN BS 767 TO BS 787. REPAIRED WEB IAW SRM & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

R2 DOOR CREASE BEAM CORRODED. R&R CREASE BEAM DWG AND SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

LT CREASE BEAM WEB CORRODED BETWEEN BS 747 TO BS 767. REPAIRED WEB IAW EA.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 41,562 hrs · 24,452 cycles

FWD WET AREA FLOOR STRUCTURE INTERCOASTAL IS CRACKED AT STA. 328 LBL. 46. / REMOVED AND REPLACED INTERCOSTAL; P/N 141A5410U140 AT STA 328 LBL 46 IAW B737 DRAWING 141A5400 REV- AND SRM 51-40-02-0G-0 PARA 7.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

PASSENGER CABIN T-CAP CORRODED AT BS 986.5, BETWEEN RBL 20 TO RBL 45. REPAIRED T-CAP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

RT CREASE BEAM CORRODED AT BS 787. R&R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

LT CREASE BEAM WEB CORRODED BETWEEN BS 727C TO BS 727D, AFT SIDE. REPAIRED WEB IAW SRM & EA.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 41,562 hrs · 24,452 cycles

RUDDER MIDDLE COUNTER BALANCE WEIGHT IS CORRODED. / REMOVED AND REPLACED RUDDER MIDDLE BALANCE WEIGHT IAW CMM 55-40-09

Part: SPLICE — CORRODED (AFT CARGO BAY) · airframe 41,562 hrs · 24,452 cycles

AFT CARGO PIT R/H SHIELD SPLICE HAS CORROSION AS MARKED. / REMOVED AND REPLACED AFT CARGO PIT R/H SHIELD SPLICE IAW BOEING DWG 146A8127 REV: - AND B737 SRM 51-40-02-0G-0

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

AFT PIT RT Z-ANGLE CORRODED BETWEEN BS 727D+10 TO BS 767. R&R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

FORWARD CARGO COMPARTMENT RT SIDE SHIELD (Z-ANGLE) CORRODED BETWEEN BS 495 TO BS 500A. R&R SHIELD IAW SRM AND DWG.

Part: SIGN — DAMAGED (CABIN) · airframe 41,562 hrs · 24,452 cycles

G1 GALLEY LOWER EMERGENCY EXIT SIGN DAMAGED. R&R SIGN PER AMM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

FORWARD CARGO COMPARTMENT BULKHEAD SUPPORT BRACKET GUSSET CRACKED AT BS 500D, STR 15L. R&R GUSSET IAW DWG.

Part: SEAL — CRACKED (LT WING) · airframe 41,562 hrs · 24,452 cycles

LEFT WING TE SUPT RIB FOR BULB SEAL CRACKED ABOVE SAILTAIL. / REMOVED AND REPLACE SEAL ROTAINER ON LEFT HAND TE SUPT RIB ABOVE SAIL TAIL IAW SRM 51-40-02-0G-0 AND SOPM 20-50-01

Part: WEB — CORRODED (FWD CARGO BAY) · airframe 41,562 hrs · 24,452 cycles

FWD CARGO DOOR CUTOUT LOWER THRESHOLD WEB HAS CORROSION IN SEVERAL PLACES (MARKED IN BLACK) / REMOVED AND REPLACED FWD CARGO DOOR LOWER THRESHOLD WEB IAW BOEING DWG 143A 8330 AND 737-700 SRM 51-40-02 AND 737-700 SRM 51-40-05

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,562 hrs · 24,452 cycles

FORWARD CARGO COMPARTMENT BULKHEAD SUPPORT BRACKET GUSSET CRACKED AT BS 500D, STR 15R. R&R GUSSET IAW SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 39,969 hrs · 23,439 cycles

L1 DOOR SLIDE FELL OUT OF THE CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED THE SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,413 hrs · 23,079 cycles

R1 DOOR OUTSIDE EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 39,198 hrs · 22,930 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R & R THE BATTERY IAW AMM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 39,198 hrs · 22,930 cycles

SUPPLEMENTAL INFORMATION: L/H HORIZONTAL STAB.. FWD. UPPER SLIDING SEAL IS CRACKED / R&R'D L/H HORIZONTAL STAB.. FWD. UPPER SLIDING SEAL REF AMM 53-31-31.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 39,198 hrs · 22,930 cycles

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

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR SLIDE) · airframe 39,198 hrs · 22,930 cycles

L2 DOOR SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED THE GIRT BAR IAW MT AND MM.

Part: BRACKET — LOOSE (L1 DOOR GIRT BAR) · airframe 37,570 hrs · 21,934 cycles

L1 DOOR SLIDE GIRT BAR BRACKET LOOSE. SECURED THE HOOKS IAW SRM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 37,449 hrs · 21,860 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: LANYARD — LOOSE (R2 DOOR SLIDE) · airframe 35,709 hrs · 20,827 cycles

R2 DOOR EMERGENCY SLIDE LANYARD RETAINING CLIP LOOSE. SECURED THE LANYARD IAW SIP.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,404 hrs · 20,652 cycles

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

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,404 hrs · 20,652 cycles

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

Part: STRAP — CORRODED (BS 770) · airframe 35,326 hrs · 20,606 cycles

AFT CARGO FLOOR PANEL TEE STRAP CORRODED AT BS 770. R & R THE TEE STRAP IAW DWG & SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,822 hrs · 20,310 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST, BETWEEN LOCATIONS M1668 & M1669. R & R BATTERY PACK IAW AMM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 33,818 hrs · 19,731 cycles

LEFT WW PRESS BULKHEAD CRACKED AT BS 663, LBL 34. REPAIRED BULKHEAD IAW EA.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 33,690 hrs · 19,647 cycles

FORWARD WINDSCREEN EMER PHOTO LUMINESCENT LIGHT STRIP LOOSE. SECURED STRIP IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 33,412 hrs · 19,490 cycles

OVERWING EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 32,690 hrs · 19,078 cycles

L1 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 32,512 hrs · 18,971 cycles

EMERGENCY EXIT LIGHT LENS COVER BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 28,590 hrs · 16,742 cycles

CREASE BEAM INNER CHORD CORRODED AT BS 318 LBL 58. REPAIRED CHORD IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,590 hrs · 16,742 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS 312 TO 328 LBL 44. R & R INTERCOSTAL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,590 hrs · 16,742 cycles

SEAT TRACK CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,590 hrs · 16,742 cycles

SEAT TRACK CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,590 hrs · 16,742 cycles

FLOORBEAM UPPER T CAP CORRODED AT BS 986.5 RBL 44. REPAIRED T CAP IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,590 hrs · 16,742 cycles

SEAT TRACK CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 28,590 hrs · 16,742 cycles

STRAP CORRODED BETWEEN BS 1016+9 TO 1016+12, LBL 3. R & R STRAP IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,590 hrs · 16,742 cycles

SEAT TRACK CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,590 hrs · 16,742 cycles

RIGHT HORIZONTAL STABILIZER INTERNAL RIB ANGLE 26 INCHES OTBD OF INBD END CRACKED AT UPPER & LOWER AFT FASTENER LOCATIONS. R & R RIB ASSEMBLY IAW DWG & SRM.

Part: ANGLE — CRACKED (RT HORIZ STAB) · airframe 28,590 hrs · 16,742 cycles

RIGHT HORIZONTAL STABILIZER INTERNAL RIB ANGLE 35 INCHES OTBD OF INBD END CRACKED AT UPPER & LOWER AFT FASTENER LOCATIONS. R & R ANGLE IAW DWG.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 28,590 hrs · 16,742 cycles

MAIN LANDING GEAR WW FWD PRESS BULKHEAD WEB CRACKED AT BS 663 RBL 34.0. REPAIRED WEB IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 28,590 hrs · 16,742 cycles

FLIGHT DECK LT NR 3 FIXED WINDOW FRAME POST E - F, CRACK INDICATION IN 2ND TO BOTTOM WINDOW PANE ATTACH FASTENER HOLE. REPAIRED POST IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 28,590 hrs · 16,742 cycles

FLIGHT DECK LT FIXED NR 1 WINDOW FRAME TOP OTBD CORNER CRACKED. REPAIRED FRAME IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 28,590 hrs · 16,742 cycles

FLIGHT DECK RT NR 3 FIXED WINDOW FRAME POST E - F, CRACK INDICATION IN 2ND TO BOTTOM WINDOW PANE ATTACH FASTENER HOLE. REPAIRED POST IAW ACO.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 28,590 hrs · 16,742 cycles

MAIN LANDING GEAR WW FWD PRESS BULKHEAD WEB CRACKED AT BS 663 RBL 42.5. REPAIRED WEB IAW SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 28,200 hrs · 16,519 cycles

MID CABIN EMER EXIT LIGHT BATTERY PACKS INOPERATIVE. R & R BATTERY PACKS IAW AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 28,200 hrs · 16,519 cycles

FORWARD ENTRY EMER EXIT LIGHT BATTERY PACKS INOPERATIVE. R & R BATTERY PACKS IAW AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 28,200 hrs · 16,519 cycles

CEILING AFT ENTRY EMER EXIT LIGHT BATTERY PACKS INOPERATIVE. R & R BATTERY PACKS IAW AMM.

Part: DOOR — CRACKED (RT MLG) · airframe 28,951 hrs · 16,952 cycles

RIGHT MLG INNER DOOR FWD HINGE FWD UPPER ATTACH FASTENER HOLE CRACKED. REPAIRED DOOR IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 27,122 hrs · 15,895 cycles

FWD ENTRY FWD SIDEWALL EMERGENCY LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: PLATE — LOOSE (R1 DOOR) · airframe 23,544 hrs · 13,801 cycles

R1 DOOR ESCAPE SLIDE COVER 2EA ATTACH PLATES LOOSE. SECURE PLATES PER MM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 23,544 hrs · 13,801 cycles

RIGHT WING FIXED TRAILING EDGE PANEL SEAL SUPPORT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM AND SRM.

Part: CHARGER — FAILED (CABIN) · airframe 23,544 hrs · 13,801 cycles

BATTERY PACK BASE UNIT/CHARGER WOULD NOT TEST WHEN RED TEST BUTTON PUSHED IN AT MO1669 RIGHT WING. REMOVED AND REPLACED BATTERY PACK BASE/CHARGER UNIT PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 23,544 hrs · 13,801 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1669 AND M1674. REMOVED AND REPLACED BATTERIES PER AMM AND SSM.

Part: SIGN — LOOSE (CABIN) · airframe 22,719 hrs · 13,329 cycles

EMERGENCY EXIT LIGHT HANGING DOWN IN MID CABIN. RE-SECURED EMERGENCY EXIT SIGN PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,269 hrs · 13,059 cycles

RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: COVER — CRACKED (CABIN) · airframe 21,539 hrs · 12,607 cycles

LEFT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER AMM.

Part: LENS — CRACKED (CABIN) · airframe 21,539 hrs · 12,607 cycles

LEFT EEPLS LENS CRACKED AT ROW 11. REMOVED AND REPLACED LENS PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 21,539 hrs · 12,607 cycles

LEFT EEPLS WIRE COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER AMM.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 20,983 hrs · 12,272 cycles

L1 DOOR EMERGENCY EXIT LIGHT FELL OFF. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 20,938 hrs · 12,241 cycles

LEFT EEPLS COVER MISSING AT ROW 2. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 20,301 hrs · 11,896 cycles

EEPLS TRACK COVER CRACKED BETWEEN ROWS 2 AND 17. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 20,301 hrs · 11,896 cycles

RT HORIZONTAL STAB LOWER SKIN CRACKED AT STAB STATION 157.10. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 19,107 hrs · 11,209 cycles

EEPLS LENS BROKEN AT ROW 2. REMOVED AND REPLACED LENS ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 19,042 hrs · 11,171 cycles

EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 18,444 hrs · 104,822 cycles

EEPLS LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 16,874 hrs · 9,903 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET CLIP LOOSE. SECURED BRACKET PER MT.

Part: LENS — MISSING (CABIN) · airframe 16,232 hrs · 9,530 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER MISSING AT ROW 23. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,221 hrs · 9,525 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERWING EEPLS INOP. RELAMPED PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,621 hrs · 8,592 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP BETWEEN ROW 12 TO ROW 18. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,610 hrs · 8,587 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 14,101 hrs · 8,295 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT LT BULKHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 13,436 hrs · 7,897 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 12,889 hrs · 7,567 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: GUARD — BROKEN (EMERGENCY LIGHT) · airframe 12,258 hrs · 7,199 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT SWITCH SPRING LOADED GUARD BROKEN. REMOVED AND REPLACED GUARD PER MM.

Part: HOLDER — LOOSE (GIRT BAR) · airframe 12,258 hrs · 7,199 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOLDER LOOSE. SECURED HOLDER PER MM.

Part: CAP — BROKEN (CABIN) · airframe 10,351 hrs · 6,047 cycles

FWD EEPLS TRACK END CAP BROKEN. R&R ENDCAP PER MM.

Part: LENS — LOOSE (CABIN) · airframe 7,004 hrs · 3,988 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 5,306 hrs · 2,993 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 4,570 hrs · 2,580 cycles

EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 4,282 hrs · 2,417 cycles

EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,307 hrs · 736 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 15 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 1,113 hrs · 617 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 18 ABC. RELAMPED PER MM.