N757LV

Part: NONE — NONE · airframe 77,797 hrs · 45,752 cycles

FUEL QTY DROPPED 1100 LBS IN LEFT WING IN 20 MINUTES; WITH IMBALANCE OF 1100LBS. SHUT ENGINE DOWN PER QRH. AFTER BURNING FUEL FROM ENG 2; BALANCE WAS ACHIEVED / [01] PERFORMED DRIP STICK MEASURE ON LEFT WING FOUND TO BE ACCURATE.ALSO PERFORMED CROSSFEED VALVE FUNCTIONAL TEST I.A.W 28-22-00 AND SUMP THE LEFT WING I.A.W. 12-11-00. ALSO PERFORM ENG RUN ON #1 ENG I.A.W. 71-00-00 NO LEAKS FOUND

Part: PANEL — DELAMINATED (ZN 500 LEFT WING) · airframe 77,756 hrs · 45,729 cycles

LEFT WING PANEL 521 YB OUTBOARD EDGE DELAMINATED. 2INCHES FROM LEADING EDGE. 1.5 INCH WIDE BY 3 INCH LONG / [01] ACCOMPLISHED TEMP REPAIR PER EA-GENERAL CLEANED; TAP TESTED;INSTALLED 2 LAYERS OF SPEED TAPE AND REINSTALLED PANEL.;[02] COMPLIED WITH EA; #TTG8Q00FKV43

Part: LIGHT — OUT OF POSITION · airframe 77,225 hrs · 45,368 cycles

FA REPORTS AFT EXIT SIGN FELL OFF / [01] R/R'D AFT SIGN ASSY. PER MM 33-51-01.

Part: TAB — LOOSE (R1 DOOR) · airframe 77,084 hrs · 45,290 cycles

FA ADVISES THAT THE FWD SERVICE DOOR SLIDE MANUEL INFLATION PULL TAB HANGS OUT WHEN THE GIRT BAR IS ARMED / [01] RESECURED VELCRO NEAR GIRT BAR ON FWD SERVICE DOOR ESCAPE SLIDE PER AMM 25-66-01

Part: FLAP — DELAMINATED (RH WING) · airframe 76,979 hrs · 45,218 cycles

FLAP WAS FOUND WITH DELAMINATION / [01] FLAP REMOVED AND REPLACED. OPS AND ADJUSTMENT CHECKS GOOD IAW AMM 27-51-12;[02] C/W OPS AND ADJUSTMENT CHECK

Part: ENGINE — FAILED (RH ENG) · airframe 75,469 hrs · 44,286 cycles

AT 38000 FT THE R/H #2 ENG OIL/QAUATIY SHOWS 20 % ENG INSTRURMENTS FLASHED WHITE BOX AND OTHER ENGINE INSTRUMENTS ARE NORMAL. DECENT #2 QUAITY SLOWY WENT DOWN TO 7 % ON FINAL APPROCH. AT GATE #2 ; SHOWS 20% / [01] REMOVED AND REPLACED #2 ENGINE PER MT 771-00-01 SEE TTG8Q0064PRL FOR INDIVIDUAL SIGN OFFS; [02] VERIFIED

Part: RIB — CRACKED (RL/H HORIZ. STAB) · airframe 74,896 hrs · 43,938 cycles

CRACK LEADING EDGE RIB STA 86.66 AT RT HORIZONTAL STABILIZER ; 2021-462044 / [01] REPLACED LEADING EDGE RIB STA 86.66 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 186A1001 SHEET 4 REV. A; [02] UPDATED CORRECTIVE ACTION <BR>REPLACED LEADING EDGE RIB STA 86.66 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 186A1001 SHEET 4 REV. A. SEE INDIVIDUAL SIGNOFFS BELOW; [03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: NONE — CRACKED (FUSELAGE) · airframe 74,896 hrs · 43,938 cycles

CRACK ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 0.07 CENTER SECTION ; 2021-462040 / [01] REPLACED ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 0.07 CENTER SECTION IAW DWG 273A9112 REV-AND SRM B737 51-10-02 ITEM 9; [02] CORRECTED STEP 1. REPLACED ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 0.07 CENTER SECTION IAW DWG 273A9112 REV-AND SRM B737 51-10-02 ITEM 9 SEE INDIVIDUAL SINGNOFFS BELLOW; [03] REPLACED ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 0.07 CENTER SECTION IAW DWG 273A9112 REV-AND SRM B737 51-10-02 ITEM 9 SEE INDIVIDUAL SINGNOFFS BELLOW RII.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 74,896 hrs · 43,938 cycles

CRACK ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 24.5 CENTER SECTION ; 2021-462041 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: 38615K71; S/N: AE-40585; DUE DATE: 07-JUL-22.; [02] REPLACED ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 24.5 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 111A6000 REV. A; [03] UPDATED CORRECTIVE ACTION.<BR>REPLACED ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 24.5 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 111A6000 REV. A. SEE INDIVIDUAL SIGNOFFS BELOW.; [04] REPLACED ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 24.5 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 111A6000 REV. A. SEE INDIVIDUAL SIGNOFFS BELOW.<BR>RII

Part: NONE — CORRODED (AFT CARGO BAY) · airframe 74,896 hrs · 43,938 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 794.3 STR 25R WL 156 RBL2184 AT AFT CARGO COMPARTMENT ; 2021-461994 / [01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 794.3 STR 25R WL 156 RBL 21.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; AND DWG 146A0081 SHEET 7 REV C. SEE INDIVIDUAL SIGNOFFS BELOW; [02] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 794.3 STR 25R WL 156 RBL 21.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; AND DWG 146A0081 SHEET 7 REV C. SEE INDIVIDUAL SIGNOFFS BELOW.. RII ITEM

Part: NONE — CORRODED (FUSELAGE) · airframe 74,896 hrs · 43,938 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 STR 25L WL156 LBL21.84 AT AFT CARGO COMPARTMENT ; 2021-461995 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 STR 25L WL156 LBL21.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 53-00-53-2R REPAIR 6 FIGURE 203 SHEET 1 AND DRAWING # 146A7500 REV B.; [02] UPDATED CORRECTIVE ACTION.<BR>REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 STR 25L WL156 LBL21.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 53-00-53-2R REPAIR 6 FIGURE 203 SHEET 1 AND DRAWING # 146A7500 REV B. SEE INDIVIDUAL SIGNOFFS BELOW; [03] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 STR 25L WL156 LBL21.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 53-00-53-2R REPAIR 6 FIGURE 203 SHEET 1 AND DRAWING # 146A7500 REV B. SEE INDIVIDUAL SIGNOFFS BELOW.. RII ITEM

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 74,896 hrs · 43,938 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 STR 25R WL156 RBL21.84 AT AFT CARGO COMPARTMENT ; 2021-461993 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 STR 25R WL156 RBL21.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; AND DWG 146A7500 REV. A. SEE INDIVIDUAL SIGNOFFS BELOW.; [02] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 STR 25R WL156 RBL21.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; AND DWG 146A7500 REV. A. SEE INDIVIDUAL SIGNOFFS BELOW... RII ITEM

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,896 hrs · 43,938 cycles

CRACK ANGLE - CLIP LOCATED BS 400 AND STRINGER 26L AT FWD CARGO COMPARTMENT ; 2021-461990 / [01] TOOL USED DIGITAL CALIPER<BR>P/N: 500-172-30 S/N: 15237811 DUE DATE:11 MAY 22; [02] REPLACED ANGLE CLIP LOCATED AT BS 400 AND STR 26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9; SRM B737-700 51-40-02 AND DWG: 143A7505 REV B.; [03] REPLACED ANGLE CLIP LOCATED AT BS 400 AND STR 26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9; SRM B737-700 51-40-02 AND DWG: 143A7505 REV B. SEE INDIVIDUAL SIGN OFF BELOW; [04] TASK COMPLETED; RII; SEE INDIVIDUAL SIGN OFF BELOW

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,896 hrs · 43,938 cycles

CRACK BILGE AREA TIE CLIP LOCATED STA 500D AND STR 26L AT FWD CARGO COMPARTMENT ; 2021-461992 / [01] REPLACED TIE CLIP AND FASTENER LOCATED STA 500D AND STR 26L AT FWD CARGO COMPARTMENT ; I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A1225 REV - .; [02] REPLACED TIE CLIP AND FASTENER LOCATED STA 500D AND STR 26L AT FWD CARGO COMPARTMENT ; I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A1225 REV - .<BR>RII

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 74,896 hrs · 43,938 cycles

CRACK BILGE AREA TIE CLIP LOCATED STA 500D AND STR 26R AT FWD CARGO COMPARTMENT ; 2021-461991 / [01] REPLACED TIE CLIP AND FASTENER LOCATED STA 500D AND STR 26R AT FWD CARGO COMPARTMENT ; I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A1225 REV - .; [02] REPLACED TIE CLIP AND FASTENER LOCATED STA 500D AND STR 26R AT FWD CARGO COMPARTMENT ; I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A1225 REV - .<BR>RII

Part: ANGLE — CRACKED (R/H WING) · airframe 74,896 hrs · 43,938 cycles

CRACK ANGLE TRAILING EDGE AREA OF ACCESS PANEL 651GB AT RT WING ; 2021-461958 / [01] REPLACED ANGLE TRAILING EDGE AREA OF ACCESS PANEL 651GB AT RT WING IAW SRM B737-700-51-10-02 ITEM 9; 51-40-02 AND DRAWING 115A3700 REF. Y REV. DATE 30NOV01; REPLACED ANGLE DUE TO NO FOUND ALLOWABLE DAMAGE IN SRM B737-700.; [02] STEP 1 COMPLETE

Part: ANGLE — CRACKED (R/H WING) · airframe 74,896 hrs · 43,938 cycles

CRACK ANGLE TRAILING EDGE BETWEEN WS 236 TO WS 285 ON REAR SPAR AT RT WING ; 2021-461956 / [01] REPLACED ANGLE LOCATED TRAILING EDGE BETWEEN WS 236 TO WS 285 ON REAR SPAR AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG #115A2930 SHEET 8 REV -.; [02] CERTIFIED WORK PERFORMED.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 74,896 hrs · 43,938 cycles

INOP UPPER BATTERY PACK ON FWD AREA GALLEY (2EA) ; 2021-461844 / [01] REPLACED POWER SUPPLY-BATTERY PACK M1674; M1675 ON FWD PAX CABIN; LIGHTS TEST ARE OK. IAW AMM 33-51-06-960-805; [02] CERTIFIED STEP 1; TEST OK.<BR>TASK CARD COMPLETED

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,896 hrs · 43,938 cycles

CRACK STRINGER 25R AT BS 540 FWD CARGO COMPARTMENT ; 2021-461921 / [01] TOOL USED: ULTRASONIC EQUIPMENT: P/N: 45 MG; S/N: 130064101 DUE DATE: 11-MAR-22; [02] TOOL USED EDDY CURRENT PN/ NORTEC 600D; SN/60009161631; DUE DATE/ 01DEC21; [03] TOOL USED PRECISION RADIUS GAUGE P/N: 2204A3 ; S/N: AE-408657 DUE DATE : 02-NOV-21; [04] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 21-JAN -22; [05] PERFORMED PERMANET REPAIR ON STRINGER 25R BETWEEN BS 500C AND BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG # 143A3230 REV :-. SEE INDIVIDUAL SIGNOFFS BELOW.; [06] PERFORMED PERMANENT REPAIR ON STRINGER 25R BETWEEN BS 500C AND BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG # 143A3230 REV :-. SEE INDIVIDUAL SIGNOFFS BELOW.; [07] PERFORMED PERMANENT REPAIR ON STRINGER 25R BETWEEN BS 500C AND BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG # 143A3230 REV :-. SEE INDIVIDUAL SIGNOFFS BELOW. RII

Part: SKIN — CRACKED (GSD CUTOUT) · airframe 74,896 hrs · 43,938 cycles

CRACK ON INTERNAL SKIN CUT OUT LOWER POSITION GROUND SERVICE DOOR 114AR ; 2021-461865 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 500D; S/N :00X12101V022233; DUE DATE: 02-JUN-22; [02] REPAIRED EXTERNAL SKIN CUT OUT LOWER POSITION (EGPR SURROUND DOUBLER) GROUND SERVICE DOOR 114AR IAW SRM B737-700 53-10-15-2R-4 REPAIR 4; [03] REPAIRED EXTERNAL SKIN CUT OUT LOWER POSITION (EGPR SURROUND DOUBLER) GROUND SERVICE DOOR 114AR IAW SRM B737-700 53-10-15-2R-4 REPAIR 4; SEE INDIVIDUAL SIGN OFF BELOW; [04] REPAIRED EXTERNAL SKIN CUT OUT LOWER POSITION (EGPR SURROUND DOUBLER) GROUND SERVICE DOOR 114AR IAW SRM B737-700 53-10-15-2R-4 REPAIR 4; SEE INDIVIDUAL SIGN OFF BELOW.AS RII.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,896 hrs · 43,938 cycles

CRACK STRINGER 26L AT BS 540 FWD CARGO COMPARTMENT ; 2021-461919 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N 45MG; S/N: 130061901; DUE DATE: 11 MAY 22.; [02] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22; [03] TOOL USED PRECISION RADIUS GAUGE P/N: S167C ; S/N: AE-27601 DUE DATE : 16-JUL-22; [04] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [05] REPAIRED STRINGER 26L LOCATED BS 500D + 10 TO BS 540 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.; [06] CORRECTED STEP 5.<BR><BR>REPAIRED STRINGER 26L LOCATED BS 500D + 10 TO BS 540 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW.; [07] TASK CARD COMPLETED <BR>SEE INDIVIDUAL SIGNOFF BELOW.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,896 hrs · 43,938 cycles

CRACK STRINGER 26R AT BS 540 FWD CARGO COMPARTMENT ; 2021-461920 / [01] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22; [02] TOOL USED PRECISION RADIUS GAUGE P/N: 2204A3 ; S/N: AE-408657 DUE DATE : 02-NOV-21; [03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 21-JAN-22; [04] REPAIRED STRINGER 26R LOCATED BS 500D + 10 TO BS 540 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW.; [05] REPAIRED STRINGER 26R LOCATED BS 500D + 10 TO BS 540 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW. RII

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,896 hrs · 43,938 cycles

CRACK STRINGER 21L AT BS 540 FWD CARGO COMPARTMENT ; 2021-461917 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 35DL S/N: 091419910 DUE DATE: 30-NOV-21.; [02] TOOL USED PN NORTEC 600D SN 60009161631 DUE DATE 01-DEC-21; [03] TOOL USED PRECISION RADIUS GAUGE P/N: S167C ; S/N: AE-27601 DUE DATE : 16-JUL-22; [04] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [05] REPAIRED STRINGER 21L LOCATED BS 500D +10 TO BS 540 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.; [06] REPAIRED STRINGER 21L LOCATED BS 500D +10 TO BS 540 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW. TASK COMPLETED; [07] REPAIRED STRINGER 21L LOCATED BS 500D +10 TO BS 540 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW. TASK COMPLETED RII

Part: STRINGER — CRACKED (FUSELAGE) · airframe 74,896 hrs · 43,938 cycles

CRACK STRINGER 25L AT BS 540 FWD CARGO COMPARTMENT ; 2021-461918 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N 45MG; S/N: 130061901; DUE DATE: 11 MAY 22.; [02] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22; [03] TOOL USED PRECISION RADIUS GAUGE P/N: S167C ; S/N: AE-27601 DUE DATE : 16-JUL-22; [04] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [05] REPAIRED STRINGER 25L LOCATED BS 500D + 10 TO BS 540 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.; [06] CORRECTED STEP 5.<BR><BR>REPAIRED STRINGER 25L LOCATED BS 500D + 10 TO BS 540 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW.; [07] CORRECTED STEP 6.<BR><BR>REPAIRED STRINGER 25L LOCATED BS 500D + 10 TO BS 540 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.; [08] TASK CARD COMPLETED <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: LIGHT — BROKEN (CABIN) · airframe 74,896 hrs · 43,938 cycles

BROKEN GALLEY 1 EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA ; 2021-461580 / [01] REPLACED GALLEY 1 EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 PERFORMED OPERATIONAL TEST IS OK; [02] TASK CARD COMPLETED

Part: NONE — CRACKED (R/H WING) · airframe 74,896 hrs · 43,938 cycles

CRACK EXTERNAL SKIN LOCATED SLAT 6 AT LEVEL SLAT STATION 202.45 AT RT WING ; 2021-461484 / [01] REMOVED ACCESS PANEL 623DB AND FLEX SKIN LOC SLAT 6 AT LEVEL SLAT STATION 202.45 AT RT WING IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND NOT FOUND DAMAGE; [11] PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED SLAT 6 AT LEVEL SLAT STATION 202.45 AT RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 PARAGRAPH 4; ALTERNATIVE 1; FIGURE 202 SHEET 3. SEE INDIVIDUAL SIGNOFFS BELOW

Part: NONE — CRACKED (L/H WING) · airframe 74,896 hrs · 43,938 cycles

CRACK EXTERNAL SKIN LOCATED SLAT 4 AT LEVEL SLAT STATION 85.19 AT LT WING ; 2021-461488 / [01] REMOVED ACCESS PANEL 522DB AND FLEX SKIN LOC SLAT 4 AT LEVEL SLAT STATION 85.19 LT WING IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND NOT FOUND DAMAGE; [25] INSTALLED REPAIR WASHERS LOC.REPAIR AREA EXTERNAL SKIN SLAT 4 AT LEVEL SLAT STATION 85.19 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; [26] OK TO INSTALL REPAIR PARTS: [1]DOUBLER; [2]FILLER AND FASTENERS LOC. EXTERNAL SKIN SLAT 4 AT,NG,NRC,2021-11-08 02:09:17,22Y,Y,MX,0,0,,CRACK EXTERNAL SKIN LOCATED SLAT 4 AT LEVEL SLAT STATION 85.19 AT LT WING ; 2021-461488"

Part: LINE — BROKEN (HYD SYSTEM) · airframe 74,289 hrs · 43,594 cycles

HAD A LOSS OF HYDRAULIC QTY. IN FLIGHT; COMPLIED WITH QRH FOR LOSS OF HYD A; NORMAL LANDING SPEED; TOUCH DOWN WAS NORMAL. ; / [01] FOUND NOSE LANDING GEAR TRANSFER CYLINDER HYDRAULIC LINE BROKEN. REMOVED AND REPLACED HYDRAULIC LINE PER A.M.M. 29-11-00 AND A.M.M. 32-33-41. NO LEAKS NOTED.

Part: LENS — DETACHED (EMERGENCY LIGHTS) · airframe 72,717 hrs · 42,671 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN LENS FELL OFF. DMA # 0414460 R & R EXIT 1 BL ASSEMBLY ON L1 ENTRANCE, REF AMM 35-51-01 CL NR 64016.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 72,484 hrs · 42,511 cycles

L2 AFT EMERGENCY SLIDE IS LOOSE. INSPECTED L2 SLIDE, IAW AMM 25-66-01 NO DEFECTS FOUND R1 SLIDE SLIGHTLY LOOSE. REMOVED RESECURED, IAW MT 725-61-06, AIRCRAFT OK FOR SERVICE.

Part: HMU — SLOW (NR 1 ENGINE) · airframe 71,610 hrs · 41,944 cycles

WAIVE DESCENDING FOR TURBULENCE 400-380 NO PROBLEMS NOTED AFTER DESCENT AND LEVELING @ 380 ENGINE WAS SLOW TO POWER UP (AUTO THROTTLES ON) DESCENDED TO 360 AND #1 ENGINE WAS HOVERING @ 55% AND SLOWLY ROLLING BACK/DECENDED @ IDLE ENG FAIL LIGHT CAME ON /DECENDED TO 20K ENGINE SPOOLED BACK UP IN DESCENT. PERFORMED FIM TASK 73-05 TASK 805 'ENG FAIL MESSAGE' ALL STEPS SATISFACTORY. CHANGED HMU PER STEP E12. R+R'D #1 ENG HMU PER M/M 73-21-10. ALL OPS AND LEAK CHECKS GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 71,537 hrs · 41,905 cycles

EMERGENCY EXIT LIGHTING FLOOR STRIP AT ROW 8 LOOSE. SECURED FLOOR PROXIMITY LIGHT STRIP PER AMM 33-51-15.

Part: LIGHT — BROKEN (CABIN) · airframe 70,982 hrs · 41,563 cycles

CENTER AISLE EMERGENCY LIGHT BROKEN. / R&R LIGHT ASSEMBLY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,715 hrs · 41,390 cycles

L1 DOOR EMERGENCY LIGHT INOP. R&R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,616 hrs · 41,324 cycles

LT OVERWING EXIT DOOR SIDEWALL LIGHT INOP. R&R LIGHT ASSEMBLY PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 70,192 hrs · 41,071 cycles

L1 DOOR SLIDE NEEDED REPACKED. / STOWED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 69,957 hrs · 40,920 cycles

R/H EMERGENCY EXIT DOOR, LOWER AFT LIGHT IS INOP. / RELAMPED R/H EMERGENCY EXIT DOOR, LOWER AFT LIGHT.

Part: DOUBLER — DEBONDED (LOWER EXT FUSELA) · airframe 69,957 hrs · 40,920 cycles

FAIRING PANEL #192F DME ANTENNA NUTPLATE DOUBLER COMMON TO FAIRING IS DISBONDED / INSTALLED FAIRING PANEL 192F DME ANTENNA NUTPLATE IAW AMM 51-31-00-390-801 AND BOEING DWG 149A7752

Part: SUPPORT ANGLE — CORRODED (BS 947) · airframe 69,957 hrs · 40,920 cycles

AFT CARGO BAY BULKHEAD TO FLOOR PANEL LOWER SUPPORT ANGLE CORRODED AT BS. 947, RBL 24. / R&R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED · airframe 69,957 hrs · 40,920 cycles

FLOOR SUPPORT CRACKED AT BS 277-294 BL 0 WL 208 / REMOVED CRACK DAMAGED FLOOR SUPPORT AT BS277-294 BL0 WL208 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0 OK TO INSTALL 13656R INSP 387 10/19/19 INSTALLED NEW FLOOR SUPPORT AT BS277-294 BL0 WL208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 13656R 19OCT19

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 69,957 hrs · 40,920 cycles

FLOORPANEL 221BF HAS DELAMINATION AND BROKEN INSERTS / REPLACED FLOOR PANEL 221BF DUE TO DELAMINATION AND BROKEN INSERTS. FLOOR PANEL 221BF WILL BE INSTALLED ON NRC T986172. PER SRM 51-10-02-0G-0 PARAGRAPH 9

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,957 hrs · 40,920 cycles

DAMAGED FUSELAGE SKIN BS 1040+6" TO 1040+13" STR 1" ABOVE 23R TO 2" ABOVE 24R REQUIRES SKIN REPAIR (REFERENCE CUSTOMER CARDS T986010,T986011,T986013, T986014, T986015, T986016, T986018). / REPAIR TO FUSELAGE SKIN AT BS 1040+6" TO BS 1040+13" 1" ABOVE STR 23R TO 2" ABOVE STR 24R ACCOMPLISHED PER EA 1-753-35954 REV IR AND ER 19-05315 REV IR.

Part: SUPPORT ANGLE — CORRODED (BS 947) · airframe 69,957 hrs · 40,920 cycles

BULKHEAD TO FLOOR PANEL LOWER SUPPORT ANGLE CORRODED AT BS. 947, RBL 20. / R&R ANGLE PER DWG AND SRM.

Part: STRAP — CORRODED (AFT CARGO) · airframe 69,957 hrs · 40,920 cycles

***CORROSION*** ON TENSION STRAP AT AFT CARGO BAY BS 847 RBL8 WL163. MARKED / AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 FIG 103.D LOCATED AND DRILLED REPLACEMENT TENSION STRAP AT AFT CARGO BAY BS785- 862; RBL8; WL163; IAW SRM 51-40-05-0G-0; INSTALLED REPLACEMENT STRAP IAW SRM 51-40-02-0G-0 AND DWG 146A8120

Part: SPLICE — CORRODED (BS 767 FLOORBEAM) · airframe 69,957 hrs · 40,920 cycles

AFT CARGO BAY FLOOR PANEL SUPPORT SPLICE CORRODED AT BS. 767+6, BETWEEN LBL 19 TO RBL 19. / R&R SPLICE PER WO.

Part: FLOOR SUPPORT — CORRODED (BS 727-727B) · airframe 69,957 hrs · 40,920 cycles

AFT CARGO BAY FLOOR SUPPORT RAIL CORRODED AROUND FASTENER HOLE BETWEEN BS. 727+5 TO BS. 727B+10, RBL2.7. / REPAIRED SUPPORT RAIL PER SRM.

Part: SUPPORT — CORRODED (727D FLOORBEAM) · airframe 69,957 hrs · 40,920 cycles

AFT CARGO BAY FLOOR PANEL SUPPORT SPLICE CORRODED AT BS. 727D+6, BETWEEN LBL 19 TO RBL 19. / R&R SUPPORT SPLICE PER PO.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 69,957 hrs · 40,920 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN AT BS. 727+4 TO BS. 767, RBL 21. / R&R SUPPORT ASSEMBLY PER DWG AND SRM.

Part: SHIELD — CORRODED (BS 767-787) · airframe 69,957 hrs · 40,920 cycles

FORWARD SHIELD CORRODED AT AFT CARGO BAY BETWEEN BS. 767 TO BS. 787, RBL 21. / R&R SHIELD IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 887-947) · airframe 69,957 hrs · 40,920 cycles

AFT CARGO BAY ON TRACK AROUND FASTENER HOLE CORRODED BETWEEN BS. 887 TO BS. 947, LBL 3. / R&R TRACK PER SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 727-887) · airframe 69,957 hrs · 40,920 cycles

AFT CARGO BAY TRACK TIE DOWN CORRODED BETWEEN BS. 7274 TO BS. 887, LBL 17. / R&R TRACK ASSEMBLY PER SRM AND DWG.

Part: WEB — CORRODED (BS 767-787) · airframe 69,957 hrs · 40,920 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS. 767 TO BS. 787, RBL 5. / R&R INTERCOSTAL WEB IAW SRM.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 69,957 hrs · 40,920 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 847, LBL 21. / R&R SUPPORT PER SRM & DWG.

Part: FLOORBEAM — CORRODED (BS 887) · airframe 69,957 hrs · 40,920 cycles

AFT CARGO BAY FLOOR PANEL SUPPORT SPLICE CORRODED AT BS. 887, BETWEEN RBL 19 TO LBL 13. / R&R SUPPORT SPLICE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,957 hrs · 40,920 cycles

FOUND CRACKED SUPPORT ANGLES BEHIND WATER SERVICE PANEL AT ACB BS907+9 RBL12 WL170. MARKED / REMOVED & REPLACED THE SUPPORT ANGLES BEHIND WATER SERVICE PAN A.C.B. BS 907+9 RBL 12 WL 170 INSTALLED PER SRM 51-40-02-0G-0 AND AIPC 52-49-00-02

Part: FRAME — DENTED (FUSELAGE) · airframe 69,957 hrs · 40,920 cycles

DENT ON THE FRAME AT AFT CARGO BAY BS 727C 3" ABOVE S-22R WL173. / REPAIRED PER: EA 1-753-35959 REV IR AND ATS ER 19-05297 REV IR.

Part: SUPPORT — CORRODED (BS 400-500D) · airframe 69,957 hrs · 40,920 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 400 TO BS. 500D, LBL 24. / R&R SUPPORT PER SRM & DWG.

Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,957 hrs · 40,920 cycles

BULKHEAD HOLE 8R OUT OF TOLERANCE AT BS. 1016, STR. 3R. / REPAIRED BULKHEAD HOLE 8R IAW SI.

Part: FORMER — CRACKED (FUSELAGE) · airframe 69,957 hrs · 40,920 cycles

FAIRING FORMER IS CRACKED AT BS 663 LBL 27 WL 142 / CUT & REMOVED 1' X 2' AREA OF FAIRING FORMER BS 663 LBL 27 WL 142 PER SRM 51-10-02-0G-0. & REPAIRED FAIRING FORMER AT BS 663 LBL 27 WL 142 AS PER ER-19-05160 REV IR AND EA 1-753-35929 REV IR. 56040C 02NOV19

Part: FORMER — CRACKED (CENTER WING) · airframe 69,957 hrs · 40,920 cycles

FAIRING FORMER IS CRACKED AT BS 663 RBL 27 WL 142 / REPAIRED PER: EA 1-757-16635 REV IR AND ATS ER 19-05139 REV IR

Part: SUPPORT ANGLE — CORRODED (FWD CARGO BAY) · airframe 69,957 hrs · 40,920 cycles

***CORROSION*** FORWARD CARGO BAY R/H BULKHEAD SUPPORT ANGLE BS 500D WL 160 RBL 27-30 / REMOVED FWD CARGO AFT BULKHEAD R/H SUPPORT BS500D RECEIVED NEW R/H SUPPORT FORM PO #265319 LOCATED; DRILLED; COUNTER SINK AND INSTALLED R/H SUPPORT BS500D IAW SRM 51-40-02 SRM 51-40-05; SRM 51-40-08; DWG #143A7902 7191U 14OCT19

Part: SHIELD — CORRODED (BS 500-500A) · airframe 69,957 hrs · 40,920 cycles

FORWARD CARGO BAY ON SHIELD CORRODED BETWEEN BS. 500 TO BS. 500A, RBL 24. / R&R SHIELD IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 69,957 hrs · 40,920 cycles

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

Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,957 hrs · 40,920 cycles

BULKHEAD HOLE 7R OUT OF TOLERANCE AT BS. 1016, STR. 3R. / REPAIRED BULKHEAD HOLE 7R IAW SI.

Part: WEB — CORRODED (BS 400-492) · airframe 69,957 hrs · 40,920 cycles

FORWARD CARGO BAY ON SUB THRESHOLD WEB CORRODED BETWEEN BS. 40 TO BS. 492.2, RBL 28. / R&R WEB PER SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 69,957 hrs · 40,920 cycles

FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO LBL 25. R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 400-500D) · airframe 69,957 hrs · 40,920 cycles

FORWARD CARGO BAY CARGO TRACK CORRODED BETWEEN BS. 400 TO BS. 500D, RBL 15. / R&R TRACK IAW SRM AND DWG.

Part: SEAT TRACK — DAMAGED (BS 480-520) · airframe 69,957 hrs · 40,920 cycles

SEAT TRACK MECHANICAL DAMAGED BETWEEN BS. 480 TO BS. 520, LBL 45. / R&R TRACK AW DWG & SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 69,957 hrs · 40,920 cycles

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

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 69,957 hrs · 40,920 cycles

FLOOR SUPPORT CRACKED BETWEEN BS. 312 TO BS. 328, LBL 45. R&R FLOOR SUPPORT PER SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (BS 500D) · airframe 69,957 hrs · 40,920 cycles

FORWARD CARGO BAY LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS. 500D, BETWEEN RBL 18 TO LBL 20. / R&R SUPPORT IAW SRM & DWG.

Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,957 hrs · 40,920 cycles

BULKHEAD HOLE 9R OUT OF TOLERANCE AT BS. 1016, STR. 3R. / REPAIRED BULKHEAD HOLE 9R IAW SI.

Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,957 hrs · 40,920 cycles

BULKHEAD HOLE 8L OUT OF TOLERANCE AT BS. 1016, STR. 3L. / REPAIRED BULKHEAD IAW SI.

Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,957 hrs · 40,920 cycles

BULKHEAD HOLE 9L OUT OF TOLERANCE AT BS. 1016, STR. 3L. / REPAIRED BULKHEAD HOLE 9L IAW SI.

Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,957 hrs · 40,920 cycles

BULKHEAD HOLE 7L OUT OF TOLERANCE AT BS. 1016, STR. 3L. / REPAIRED BULKHEAD HOLE IAW SI.

Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,957 hrs · 40,920 cycles

BULKHEAD HOLE 6R OUT OF TOLERANCE AT BS. 1016, STR 2R. / REPAIRED BULKHEAD HOLE IAW SI.

Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 69,957 hrs · 40,920 cycles

VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT BS. 663, BETWEEN RBL 5 TO RBL 18. R&R SECTION OF UPPER ATTACH ANGLE IAW SRM.

Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,957 hrs · 40,920 cycles

BULKHEAD HOLE 5L OUT OF TOLERANCE AT BS. 1016, STR. 2L. / REPAIRED BULKHEAD HOLE IAW SI.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,957 hrs · 40,920 cycles

CORROSION CROWN SKIN SURFACE CORROSION AT VARIOUS LOCATIONS ALONG DORSAL FIN AREA, BS872 TO BS1017, LBL12 TO RBL12. MOD. / REPAIRED CROWN SKIN CORROSION DAMAGE IAW ER 19-05190 AND EA 1-753-35962.

Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,957 hrs · 40,920 cycles

BULKHEAD HOLE 6L OUT OF TOLERANCE AT BS. 1016, STR. 2L. / REPAIRED BULKHEAD HOLE IAW SI.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,957 hrs · 40,920 cycles

L/H HORIZONTAL STABILIZER #4 RIB, AT STAB. STA. 120.30, STIFFENER #3 SHOWED CRACK INDICATION. / REPAIRED #3 STIFFENER IAW SRM & DWG.

Part: SEAL RING — CRACKED (CENTER WING) · airframe 69,957 hrs · 40,920 cycles

BS 663 VAPOR BARRIER UPPER SEAL RETAINER IS CRACKED RBL 20 WL 140 / REMOVED AND INSTALLED NEW VAPOR BARRIER SEAL RETAINER AT BS 663 RBL 20 WL 140 PER SRM 51-40-02 AND AIPC 57-11-00-02

Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,957 hrs · 40,920 cycles

BULKHEAD HOLE 5R OUT OF TOLERANCE AT BS. 1016, STR. 2R. / REPAIRED BULKHEAD HOLE IAW SI.

Part: PLATE — CRACKED (AFT CARGO) · airframe 69,957 hrs · 40,920 cycles

AFT CARGO BAY STIFFENER PLATE COMMON TO FWD FLOOR PANEL BS 727+8' RBL 2 WL 156 IS CRACKED / RECEIVED NEW AFT CARGO STIFFENER PLATE BS 727+8 ON PO# 764987 INSTALL WELL BE WORK ON CARD # JPANEL-141-CLOSE

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,957 hrs · 40,920 cycles

R1 DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / REPAIRED DOOR IAW MM.

Part: CAP — CRACKED (FWD CARGO) · airframe 69,957 hrs · 40,920 cycles

FORWARD CARGO BAY L/H FLOOR TO SIDEWALL CAP STRIP FWD SPLICE PLATE IS CRACKED / RECIEVED NEW FCB L/H FLOOR TO SIDEWALL CAP STRIP FWD SPLICE PLATE. TO BE INSTALLED ON CARD JPANEL-121-CLOSE

Part: PANEL — BROKEN (FUSELAGE) · airframe 69,957 hrs · 40,920 cycles

PANEL 191FR HAS A BROKEN CORNER AT UPPER EDGE FWD END OF PANEL CUT OUT / PANEL 191FR WITH A BROKEN CORNER AT UPPER EDGE; FWD END OF PANEL OUT-OUT WAS REPAIRED PER SRM 51-70-05-2R-6.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 69,957 hrs · 40,920 cycles

L/H WING #1 SLAT CRACKED AROUND THE FASTENER AT LEADING EDGE NOSE TO SKIN AT ACTUATOR RIBS. / REPAIRED #1 SLAT SKIN IAW SRM.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 69,879 hrs · 40,867 cycles

RH WING T/E FLAP SUPPORT SEAL BRACKET IS CRACKED BEHIND PYLON / R & R BRACKET PER SRM 51-10-02 & SRM 51-70-02.

Part: WINDOW — OBSTRUCTED (R1 DOOR) · airframe 69,879 hrs · 40,867 cycles

R1 DOOR SLIDE WINDOW VIEW OBSTRUCTED. REMOVED AND REPLACED R1 DOOR SLIDE WINDOW PER MT# 72-61-06 AND AMM 52-66-01.

Part: BULKHEAD WEB — CANNING (BS 1016) · airframe 69,559 hrs · 40,640 cycles

AFT PRESSURE BULKHEAD OIL CANNING AT BS. 1016, BETWEEN STR. 1L TO STR. 2L, FASTENERS INSTALLED WITH HEADS ON THE FORWARD SIDE. REPAIRED BULKHEAD PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,741 hrs · 40,116 cycles

LT OVERWING EXIT FLUORESCENT LIGHT INOP. R&R LIGHT IAW AMM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 68,288 hrs · 39,830 cycles

RT FORWARD VAPOR BARRIER CRACKED. REPAIRED BARRIER PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 68,130 hrs · 39,733 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTER FACE CORRODED ON PREVIOUS SPOT FACE. REPAIRED LUG PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 68,130 hrs · 39,733 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG OUTER FACE CORRODED ON PREVIOUS SPOT FACE. REPAIRED LUG PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 68,130 hrs · 39,733 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING-UPPER INBOARD LUG OUTER FACE CORRODED. REPAIRED LUG PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 68,130 hrs · 39,733 cycles

RT GEAR FORWARD TRUNNION RT LOWER OUTBOARD LUG CORRODED. REPAIRED LUG PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,839 hrs · 39,541 cycles

FORWARD STABILIZER H DRUM UPPER LT SUPPORT LINK OUTBOARD SUPPORT STRUCTURE CRACKED IN RADIUS AT BS 202, LBL 4.6. REPAIRED FLOORBEAM PER EA.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 67,835 hrs · 39,540 cycles

CABIN FORWARD RT PHOTO LUMINESCENT STRIP LOOSE AT GALLEY AREA. SECURED STRIP PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 65,834 hrs · 38,234 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 65,834 hrs · 38,234 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PER MM.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 65,690 hrs · 38,152 cycles

R1 DOOR ESCAPE SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BAR IAW AMM.

Part: LATCH — BROKEN (L2 GIRT BAR) · airframe 65,266 hrs · 37,870 cycles

L2 DOOR EMERGENCY AFT GIRT BAR LATCH BROKEN. R & R LATCH IAW AMM.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 64,443 hrs · 37,351 cycles

G4 GALLEY EMERGENCY EXIT LIGHT CONNECTOR WIRING DAMAGED. REPAIRED THE WIRE IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,443 hrs · 37,351 cycles

DEFECT TRANSFERRED FROM LOG PAGE 0300158. DEFECT AFT PRESSURE BULKHEAD SKIN CRACKED AT THE DOME WEB LAP SPLICE COMMON TO THE APEX OF PRESSURE DOME S-7R LOWER FASTENER. TRANSFER RED FROM NRC D230846. / THE DAMAGE IS REPAIRED BY ATS ER 18-01091 REV IR AND SWA EA 1-753-32151 REV IR

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,443 hrs · 37,351 cycles

AFT PRESSURE BULKHEAD SKIN DOME WEB CRACKED AT BS 1016, BETWEEN STR 7L TO STR 7R. REPAIRED WEB PER ER AND EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,108 hrs · 37,144 cycles

LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 63,858 hrs · 36,984 cycles

MAIN DECK FLOOR BOARD #221GF IS MISSING AN INSERT AND FWD O/B CORNER IS BROKEN / INSTALLED NEW INSERT AND REPAIRED CORNER OF PNL 221GF REF CMM 25-00-66

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,859 hrs · 36,984 cycles

LT WHEEL WELL FORWARD WALL FUEL VAPOR CRACKED. REPAIRED VAPOR PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,771 hrs · 36,930 cycles

FORWARD CABIN EMERGENCY EXIT LIGHT INOP AT LOCATION M1675. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (FWD CABIN) · airframe 63,771 hrs · 36,930 cycles

FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW MM.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 63,771 hrs · 36,930 cycles

UPPER BULKHEAD ATTACH ANGLE CRACKED AT BS 663, LBL 8. REPAIRED ANGLE IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

R1 DOOR STUB FRAME CRACKED AT BS 294 LOWER BOTTOM. REPAIRED STUB FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

REAR SPAR VERTICAL PRESSURE DECK ANGLE CRACKED AT BS 663, BETWEEN RBL 25 TO RBL 45. REPAIRED ANGLE IAW EA.

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

AFT CARGO PIT DOORWAY LOWER SILL WEB STA 794 - 827 HAS CORROSION ON UPPER SURFACE / BLENDED OUT CORROSION ON AFT CARGO LOWER SILL WEB IAW B737-700 SRM 51-10-02-0G-0. ORIGINAL THICKNESS 0.045'; MATERIAL LOSS 0.020'; THE AREA FOUND TO BE OUT OF LIMIT IAW B737-SRM 53-60-15-1A-1. LOCATED AND DRILLED NEW WEB IAW B737-700 SRM 51-40-05 INSTALLED THE WEB IAW B737-700 SRM 51-40-02 AND DWG 146A8340 REV A. APPLIED CIC THE NEW INSTALLED WEB IAW B737-700 AMM 51-21-91-620-802.

Part: SCUFF PLATE — CORRODED (AFT CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

AFT CARGO COMPARTMENT FWD THRESHOLD RETAINER PLATE IS CORRODED. / OUT OF ALLOWABLE LIMITS ON AFT CARGO PIT THRESHOLD RETAINER PLATE IAW 53-60-15-1A-1 OBTAINED NEW THRESHOLD PLATE PN 453A2611-1 A26899 IAW IPC 25-52-10-02

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

FWD CARGO BAFFLE CLIP CRACKED BS 500C LBL 26. MARKED. / REMOVED EXISTING / UNSERVICEABLE FWD CARGO BAFFLE CLIP @ STA 500C LBL 26 AND INSTALLED P/N 143A7502-13 BAFFLE CLIP IAW SRM 51-40-02 AND BOEING DWG 143A7505 ATAG # A01852

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

FWD CARGO L/H #2 FLOOR CAPSTRIP IS CORRODED ON BOTTOM SIDE. / FOWARD CARGO L/H #2 FLOOR CAPSTRIP CORROSION IS MORE THAN 3.0 INCHES IN LENGTH OUT OF LIMITS I/A/W B737 SRM 53-0-53-1A-1. RECEIVED A NEW CAPSTRIP P/N 453A1611-11 A TAG A19695 I/A/W B737 SRM 53-30-53-01-1 AND AIPC 25-52-10-01

Part: WEB — CORRODED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

FORWARD CARGO THRESHOLD CLOSE OUT WEB CORRODED. R&R WEB IAW SRM AND DWG.

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 63,771 hrs · 36,930 cycles

PAX CABIN FLOOR BOARD 241ABF; UPPER SURF COMPOSITE FIBERS PULLED. / REPAIRED CABIN FLOOR BOARD 241 ABF IAW B737 SRM 53-00-50-2R-0 PARA 2A AND SRM 53-00-50-2R-1 REPAIR 1 PARA 3 A26382 A83873 A30641 A97437

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

AFT CARGO PIT LOWER SILL STRUCTURE UNDERSIDE STRAP STA 787 - 796 RBL 20 HAS CORROSION AROUND NUTPLATES / MATERIAL LOSS WAS 100% IN SAME AREA OF STRAP. ORIGINAL THICKNESS IS 0.215'; THE AREA WAS FOUND TO BE OUT OF LIMIT IAW B737-700 SRM 53-60-15-1A-1. REMOVED STRAP IAW B737-700 SRM 51-40-02. LOCATED AND DRILLED NEW STRAP IAW B737-700 SRM 51-40-05-0G-0; INSTALLED THE NEW UNDERSTRAP IAW B737-700 SRM 51-40-02 AND DWG 146A8120 REV E. APPLIED CIC IAW B737-700 AMM 51-21-91-620-802

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 63,771 hrs · 36,930 cycles

PAX CABIN FLOOR BOARD 241AAF; UPPER SURF COMPOSITE FIBERS PULLED. / REPLACED CABIN FLOOR BOARD 241 AAF IAW B737 SRM 53-00-50-2R-0 PARA 1 A AND PARA 4A PANEL BMS 4-23 TY 11 AND INSERTS SLP5182A3 A30641 AND SLS5182A3-400 A97437 & DWG 147A5810 REV A

Part: SCUFF PLATE — CORRODED (FWD CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

FWD CARGO COMPARTMENT; AFT THRESHOLD DOUBLER PLATE IS CORRODED ON BOTTOM SIDE. / CORROSION AT FORWARD CARGO COMPARTMENT AFT THRESHOLD DOUBLER PLATE IS MORE THAN 3.0 INCHES IN LENGTH. OUT OF LIMITS PER B737 SRM 53-00-53-1A-1 5.A.(1)1). RECEIVED A NEW THRESHOLD DOUBLER PLATE P/N 453A1611-26; ATAG A20876 I/A/W B737 SRM 53-30-53-01-1 FIGURE AND AIPC 25-52-10-01

Part: SCUFF PLATE — CORRODED (FWD CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

FWD CARGO COMPARTMENT; FWD THRESHOLD DOUBLER PLATE IS CORRODED ON BOTTOM SIDE. / CORROSION IN FORWARD CARGO COMPARTMENT FWD THRESHOLD DOUBLER PLATE IS MORE THAN 3.0 INCHES IN LENGTH. OUT OF LIMITS PER B737 SRM 53-00-52-1A-1 5A(1)(B)1). RECEIVED A NEW THRESHOLD DOUBLER P/N 453A1611-25; ATAG A19379 I/A/W B737 SRM 53-30-53-01-1 FIGURE 2 AND AIPC 25-52-10-01

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

AFT CARGO PIT DOORWAY LOWER SILL STRUCTURE FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 794, RBL 21. R&R SHIELD IAW DWG AND SRM.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

FWD CARGO BAFFLE CLIP CRACKED BS 500B LBL 26. MARKED. / REMOVED EXISTING / UNSERVICEABLE FWD CARGO BAFFLE CLIP @ STA 500B AND INSTALLED P/N 143A7502-13 BAFFLE CLIP IAW SRM 51-40-02 AND BOEING DWG 143A7505 ATAG # A01852

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

FWD CARGO FLOOR R/H FWD CAPSTRIP IS CORRODED ON BOTTOM SIDE. / FOWARD CARGO FLOOR R/H FOWARD CAPSTRIP CORROSION IS MORE THAN 3.0 LENGTH OUT OF LIMITS I/A/W 53-00-53-1A-1 5A.(1)(B). RECIEVED A NEW STRAP P/N 453A1611-5 ATAG 19402 I/A/W B737 SRM 53-30-53-01-1 AND AIPC 25-52-10-01

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 63,771 hrs · 36,930 cycles

PASSENGER CABIN FLOOR BOARD 241YF TOP SIDE DISBONDED / REPAIRED DAMAGE ON FLOOR PANEL 241 YF BONDED REPAIR PLY ON TOP SURFACE AND CURED TAP TEST GOOD IAW B737-700 SRM 53-00-50-2R-0 SRM 53-00-50-2R-1

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

AFT CARGO COMPARTMENT RT Z ANGLE CORRODED BETWEEN BS 727B TO BS 767. R&R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

AFT CARGO COMPARTMENT LT Z ANGLE CORRODED BETWEEN BS 727B TO BS 807. R&R Z ANGLE IAW SRM.

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

FWD CARGO FLOOR R/H AFT CAPSTRIP IS CORRODED ON BOTTOM SIDE. / FOWARD CARGO FLOOR R/H AFT CAPSTRIP CORROSION IS MORE THAN 3.0 INCHES LENGTHM OUT OF LIMITS I/A/W B737 SRM 53-00-5-1A-1 5.(1)(B) RECVEIVED A NEW CAPSTRIP P/N 453A1611-12. ATAG WN4262 I/A/W B737 SRM 53-30-53-01-1 AND AIPC 25-52-10-01

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

AFT CARGO PIT DOORWAY LOWER SILL STRUCTURE UPPER STRAP STA 784 - 817 RBL 20 HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION FROM AFT CARGO PIT DOORWAY LOWER SILL UPPER STRAP. ORG THICKNESS 0.100;MATERIAL LOSS IS .012 OUT OF SRM 53-60-15-1A-1 ALLOWABLE LIMIT.REMOVED UPPER STRAP FROM STA 775 TO 861 AND INSTALLED NEW STRAP IAW SRM 51-40-02 AND DWG 146A8120 REV A SHEET 10.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

FORWARD CARGO Z ANGLE CORRODED BETWEEN BS 500A TO BS 500D, RBL 24. R&R Z ANGLE IAW SRM.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 63,771 hrs · 36,930 cycles

PAX CABIN FLOOR BOARD 242UF DISBONDED AT AFT O/B EDGE / PREPPED; CLEANED AND REPAIRED DELAM DAMAGE TO LOWER FACESHEET AT AFT O/B EDGE ON FLOORBOARD 242UF IAW B737 SRM 53-00-50-2R-9 PAR 4 (A-K1; L1;M1) REV 62

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

FORWARD CARGO Z SHIELD CORRODED BETWEEN BS 440 TO BS 440-6, RBL 24. R&R Z SHIELD IAW DWG AND SRM.

Part: FLOOR PANEL — EXPOSED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

PASSENGER CABIN; FORWARD WET AREA; FLOOR PANEL 222BF; MULTIPLE LARGE AREAS OF EXPOSED COMPOSITE FIBERS ALONG FWD; INBOARD; AFT EDGES; AND CENTER OF UPPER SURFACE. 12 INCHES FWD OF AFT EDGE. / REPAIRED PASSENGER CABIN FWD WET AREA FLOOR PANEL 222BF ALONG FWD I/B AFT EDGES AND CENTER OF UPPER SURFACE UAW B737 SRM 53-00-50-2R-0 REPAIR GENERAL AND B737 SRM 53-00-50-2R-1 REPAIR 1 REV 62. IN OVEN AND CURED AT 150 DEGREE FOR 2 HRS. OVEN E0-01 EXP 10-31-17 A51273; A26386

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

FWD CARGO L/H #1 FLOOR CAPSTRIP IS CORRODED ON BOTTOM SIDE. / FOWARD CARGO L/H #1 FLOOR CAPSTRIP CORROSION IS MORE THAN 3.0 INCHES IN LENGTH; OUT OF LIMITS I/A/W B737 SRM 53-00-53-1A-1 5.A.(1)(B). RECEIVED A NEW CAPSTRIP P/N 453A1611-6. A TAG WN6057 I/A/W B737 SRM 53-30-53-01-1 AND AIPC 25-52-10-01

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

FWD CARGO L/H #3 FLOOR CAPSTRIP IS CORRODED ON BOTTOM SIDE. / FOUND CARGO L/H #3 FLOOR CAPSTRIP CORROSION IS MORE THAN 3.0 INCHES IN LENGTH; OUT OF LIMITS I/A/W B737 SRM 53-00-53-1A-1 RECIEVED A NEW CAPSTRIP P/N 453A1611-10 I/A/W B737 SRM 53-30-53-01-1

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 63,771 hrs · 36,930 cycles

PAX CABIN FLOOR BOARD 241 EDGE DELAMINATED. / REPAIRED FLOOR BOARD 241 ADF EDGE DELAMINATION IAW SRM 737-700 SRM 53-00-50-2R-1U REV 62 SRM 53-00-50-2R-0 REV 62

Part: SUPPORT ANGLE — CORRODED (MAIN CABIN) · airframe 63,771 hrs · 36,930 cycles

FWD ENTRY LOWER SILL THRESHOLD INBD SUPPORT ANGLE CORRODED BS 313 TO BS 328 LBL 61' MARKED. / REMOVED EXISTING / UNSERVICEABLE THRESHOLD SUPPORT ANGLE AND INSTALLED NEW / SERVICEABLE ANGLE P/N 141A8112-2 IAW SRM 51-40-02 AND BOEING DWG 141A8112 REV E A TAG # WN 2188 TOOL # 36649 CAL DUE 07-05-18

Part: SUPPORT ANGLE — CORRODED (MAIN CABIN) · airframe 63,771 hrs · 36,930 cycles

FWD ENTRY LOWER SILL THRESHOLD CENTER SUPPORT ANGLE CORRODED BS 313 TO BS 328 LBL 63' MARKED. / REMOVED EXISTING / UNSERVICEABLE THRESHOLD CENTER SUPPORT ANGLE AND INSTALLED NEW / SERVICEABLE THRESHOLD CENTER SUPPORT PN 141A8112-4 IAW SRM 51-40-02 AND BOEING DWG 141A8112 REV E A TAG # AD 7600 TOOL # 36649 CAL DUE 07-05-18

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 63,771 hrs · 36,930 cycles

FORWARD WET AREA STA 355 LBL 0 DRILL START AND CRACK AT FASTENER HOLE ON INTERCOSTAL. / REMOVED AND REPLACED INTERCOSTAL STA 340 TO 360 LBL 0 IAW SRM 51-40-02 AND BOEING DRW 141A5410 REV U

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

R1 CREASE CORRODED BETWEEN BS 312 TO BS 340 UPPER SURFACE. R&R CREASE BEAM IAW SRM & DWG.

Part: SEAL — TORN (LT HORIZ STAB) · airframe 63,771 hrs · 36,930 cycles

LEFT HORIZONTAL STABILIZER; LOWER STAB SEAL PANEL 334AB; TRAILING EDGE OF SEAL IS TORN AT INBOARD END. / RECEIVED SEAL PANEL (NEW) PN 7270984; DRILLED HOLES TO MATCH UNSERVICEABLE PANEL IAW SRM 51-20-07-0G-0;STEP 4. COUNTERSUNK HOLES IAW SRM 51-40-08-0G-0; STEP 4-5. PRIMED NEW PANEL IAW AMM 51-21-72-370-802: STEP E4(B)& F. PAINTED PANEL IAW AMM 51-21-73-370-804; STEP 4(D-E) ATAG WN0819

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

INTERCOSTAL CRACKED AT BS 274+2, LBL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: WEB — CORRODED (FWD CARGO BAY) · airframe 63,771 hrs · 36,930 cycles

FWD CARGO THRESHOLD CLOSE OUT WEB CORRODED AS MARKED / FWD CARGO THRESHOLD CLOSE OUT WEB CORRODED AS MARKED BLENDED CORROSON AND FOUND ORIGINAL T .063' REMAIN T .040' REMOVED .023' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVED OLD WEB AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0 AND BOEING DWG # 143A8330

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 63,771 hrs · 36,930 cycles

L1 DOOR FORE AND AFT GIRT BAR STRUCTURE CORRODED. R&R GIRT BAR ASSEMBLY IAW AMM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 63,771 hrs · 36,930 cycles

RH HORIZ STAB; FWD SPAR; LWR SLIDING SEAL HAS 2 CRACKS AT FWD ATTACH FTGS. / RH HORIZ SPAR LWR SLIDING SEAL HAS 2 CRACKS AT FWD EDGE REPLACED LOWER SLIDING SEAL DURING ACO 8454-53 SLIDING SEAL TRACK MODIFICATION IAW ACO 8454-53 STEP 7K

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

R1 DOOR LOWER SILL INNER THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 294.5 TO BS 328, RBL 57. R&R STRAP IAW SRM & AMM.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 63,771 hrs · 36,930 cycles

PASSENGER CABIN STA APROX 338 LBL 47 PREVIOUS REPAIR HAS POSSIBLE CRACK AT FASTENER HOLE (MKD) / REMOVED CRACK INTERCOSTAL AND REPLACED WITH A NEW INTERCOSTAL AT PASSENGER CABIN FROM STA 328 TO 344 LBL 47 IAW SRM 51-40-02-0G-0 STEP 7 AND BOEING DWG # 141A5400 REV - TAG # A99891

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

R2 CREASE BEAM INNER CHORD CORRODED BETWEEN BS 955 TO BS 992, RBL 48. R&R CREASE BEAM IAW DWG AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

AFT WET AREA T-CAP CORRODED AT BS 986.5, BETWEEN LBL 46 TO RBL 46, ON UPPER AND LOWER SURFACE. R&R T CHORD IAW SRM AND EA.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 63,771 hrs · 36,930 cycles

RH HORIZ STAB; FWD UPR SLIDING SEAL CRACKED AT LWR OTBD CORNERS. / RH HORZ STAB FWD UPPER SLIDING SEAL CRACKED. REPLACED UPPER RH SLIDING SEAL PN 181A8025-2 ATAG A22163 IAW AMM 53-31-31-400-802

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

RT ANGLE CRACKED AT BS 663. R&R ANGLE IAW DWG & SRM.

Part: RETAINER — CRACKED (RT WING) · airframe 63,771 hrs · 36,930 cycles

RIGHT WING PANEL AFT OF PYLON; BULB SEAL BRACKET CRACKED AT LOWER BOLT. / REMOVED AND INSTALLED A NEW BULB SEAL BRACKET AT RIGHT WING PANEL AFT OF PYLON I/A/W B737 SRM 51-40-02-0G-0

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

LT BULKHEAD FORWARD SIDE, DIAGONAL ANGLE STIFFENER CRACKED AT BS 663. R&R STIFFENER IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,771 hrs · 36,930 cycles

RT MAIN LANDING GEAR TOP PRESSURE DECK WEB CRACKED AT BS 663+2, RBL 41. REPAIRED WEB IAW EA.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 63,771 hrs · 36,930 cycles

LT WING TRAILING EDGE SUPPORT BRACKET CRACKED. R&R BRACKET IAW SRM AND DWG.

Part: PLATE — CRACKED (LT WING) · airframe 63,771 hrs · 36,930 cycles

LT WING TRAILING EDGE ABOVE PYLON SAIL TAIL WIGGLE PLATE CRACKED AT FASTENERS. R&R WIGGLE PLATE ASSEMBLY IAW SRM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 63,771 hrs · 36,930 cycles

LT WING TRAILING EDGE JUST BOARD OF FLAP DEFLECTION CONTROL RIB PANEL SUPPORT BRACKET CRACKED AT OUTBOARD END. R&R BRACKET IAW SRM AND DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,771 hrs · 36,930 cycles

LT MAIN LANDING GEAR TOP PRESSURE DECK CRACKED AT BS 663+1.5, LBL 31. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,771 hrs · 36,930 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 63,771 hrs · 36,930 cycles

LT WING LEADING EDGE NR 2 SLAT LOWER SKIN AT ACTUATOR CRACKED. REPAIRED NR 2 SLAT PER SRM.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 63,771 hrs · 36,930 cycles

MAIN WHEEL WELL PANEL 193B HAS A DENT WITH DELAM ON EXTERIOR SURFACE 7.5' FROM FORWARD EDGE AND 20.5' FROM RIGHT EDGE / REPAIRED MAIN WHEEL WELL PANEL 193 EXTERIOR SURFACE 7.5 ' FROM FORWARD EDGE AND 20.5 ' FROM RIGHT SIDE EDGE IAW SRM 51-70-04-2R-1 REV 62 PER SRM 53-40-70-2R-1 TABLE 201 REV 62

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,771 hrs · 36,930 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 42. REPAIRED WEB IAW SRM.

Part: O-RING — FAILED (HYD TRANSMITTER) · airframe 63,155 hrs · 36,546 cycles

NR 1 ENGINE, HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED. HYDRAULIC QUANTITY INDICATED AS LOW AS 7%. FOUND A BROKEN O-RING ON PRESSURE TRANSMITTER. R & R THE O-RING IAW AMM.

Part: LENS — LOOSE (SLIDE LIGHT) · airframe 61,817 hrs · 35,732 cycles

L2 DOOR SLIDE LIGHT LENS LOOSE. R & R THE LENS IAW MT AND AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,817 hrs · 35,732 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY CHECK AT LOCATION M1669. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 61,817 hrs · 35,732 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY CHECK AT LOCATION M1672. R & R THE BATTERY PACK IAW AMM.

Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 60,701 hrs · 35,072 cycles

L1 DOOR EMERGENCY EVAC SLIDE INDICATOR LOW PRESSURE. R & R THE SLIDE IAW MT.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,872 hrs · 34,547 cycles

L1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. R & R THE CHARGER IAW MM.

Part: SUPPORT FRAME — CRACKED (FUSELAGE) · airframe 59,582 hrs · 34,386 cycles

LEFT WING TO BODY PANEL 191L FORWARD SUPPORT FRAME CRACKED. R & R FRAME IAW SRM.

Part: MOUNT — LOOSE (R2 DOOR) · airframe 59,582 hrs · 34,386 cycles

R2 DOOR EMERGENCY EVAC SLIDE AFT SLIDE MOUNT LOOSE. R & R MOUNT IAW SRM.

Part: LENS — MISSING (EXIT SIGN) · airframe 58,838 hrs · 33,971 cycles

AFT GALLEY DOOR EXIT SIGN COVER MISSING. INSTALLED LENS IAW SIP.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,769 hrs · 33,366 cycles

LEFT HORIZONTAL STABILIZER RIB STATION 129.50, CRACKED AT 2ND STIFFENER. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,769 hrs · 33,366 cycles

LEFT HORIZONTAL STABILIZER RIB STATION 111.10, CRACKED AT 3RD STIFFENER. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,769 hrs · 33,366 cycles

RIGHT HORIZONTAL STABILIZER, RIB 120.3 BOTTOM PORTION OF NR 3 STIFFENER CRACKED. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,769 hrs · 33,366 cycles

RIGHT HORIZONTAL STABILIZER RIB 129.5, BOTTOM PORTION OF NR 3 STIFFENER CRACKED. R & R RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

NUMBER 1 RT WINDOW FRAME CRACKED, AT OTBD UPPER CORNER. REPAIRED FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

FRAME CRACKED AT BS 597, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

FRAME CRACKED AT BS 727A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

FRAME CRACKED AT BS 559, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

FRAME CRACKED AT BS 520, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,769 hrs · 33,366 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,641 hrs · 33,289 cycles

AFT LT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,641 hrs · 33,289 cycles

FORWARD LT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 57,233 hrs · 33,057 cycles

R2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: BUMPER — MISSING (R2 DOOR) · airframe 56,575 hrs · 32,675 cycles

R2 DOOR SLIDE COVER AFT END CAP BUMPER MISSING. INSTALLED BUMPER IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,197 hrs · 32,471 cycles

LEFT EGRESS LIGHTS INOPERATIVE AT BELLY FAIRING. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,197 hrs · 32,471 cycles

RIGHT EGRESS LIGHTS INOPERATIVE AT BELLY FAIRING. RELAMPED LIGHT IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 55,780 hrs · 32,233 cycles

RIGHT OVERWING EMER EXIT LENS BROKEN. R & R LENS IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,393 hrs · 32,020 cycles

LEFT OVERWING EXIT SIDEWALL LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: HOLDER — LACK OF LUBE (R2 DOOR) · airframe 54,189 hrs · 31,337 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR HOLDER AT AFT SERVICE DOOR STICK. LUBED GIRT BAR HOLDER IAW SIP.

Part: LENS — MISSING (CABIN) · airframe 53,770 hrs · 31,081 cycles

MID CABIN EXIT SIGN LENS MISSING. INSTALLED LENS IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 52,440 hrs · 30,335 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. R & R LIGHT ASSEMBLY IAW AMM.

Part: GUIDE ARM — OUT OF ADJUST (R2 DOOR) · airframe 52,225 hrs · 30,219 cycles

R2 DOOR EMERGENCY EXIT DOOR OUT OF ADJUSTMENT. ADJUSTED GUIDE ARM IAW MM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 51,487 hrs · 29,785 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET CLIPS LOOSE. SECURED CLIPS IAW SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,791 hrs · 29,342 cycles

SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,791 hrs · 29,342 cycles

SEAT TRACK INBD FLANGE AFT HOLES CRACKED AT STATION 727B, LBL 24.75. REPAIRED TRACK IAW EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 50,791 hrs · 29,342 cycles

BELT FRAME CRACKED AT STATION 727D, STRINGER 9R. REPAIRED FRAME IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,791 hrs · 29,342 cycles

SEAT TRACK INBD FLANGE AFT HOLES CRACKED AT STATION 727B, LBL 45.50. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,791 hrs · 29,342 cycles

SEAT TRACK OTBD FLANGE FWD & AFT HOLES CRACKED AT STATION 727B, LBL 45.5. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,791 hrs · 29,342 cycles

SEAT TRACK OTBD FLANGE FWD HOLES CRACKED AT STATION 727B, RBL 24.75. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,791 hrs · 29,342 cycles

SEAT TRACK OTBD FLANGE FWD HOLES CRACKED AT STATION 727B, RBL 45.50. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,791 hrs · 29,342 cycles

SEAT TRACK OTBD FLANGE FWD & AFT HOLES CRACKED AT STATION 727B, LBL 24.75. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,791 hrs · 29,342 cycles

SEAT TRACK INBD FLANGE AFT HOLES CRACKED AT STATION 727B, RBL 45.50. REPAIRED TRACK IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,791 hrs · 29,342 cycles

LT WING NR 1 SLAT LOWER LE SKIN CRACKED AT ACTUATOR FITTING. R & R SKIN IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,791 hrs · 29,342 cycles

LT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,791 hrs · 29,342 cycles

RT WING NR 7 SLAT LOWER LE SKIN CRACKED AT ACTUATOR FITTING. R & R SKIN IAW MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,791 hrs · 29,342 cycles

RT HORIZONTAL STABILIZER LOWER SKIN PANEL CRACKED AT STATION 129.5 INBD SIDE OF RIB 10.5" FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,791 hrs · 29,342 cycles

LT NR 3 WINDOW FRAME E-F FASTENER HOLE NR 8 CRACKED AT 10:00 & 4:00 O'CLOCK LOCATION. REPAIRED HOLE IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 48,868 hrs · 28,182 cycles

LEFT WING O/B AFT FLAP LOWER I/B END UPPER SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: RETAINER — CRACKED (LT WING) · airframe 48,817 hrs · 28,152 cycles

LEFT WING I/B FIXED UPPER T/E FORWARD SEAL RETAINER CRACKED. REMOVED AND REPLACED SEAL RETAINER PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 48,817 hrs · 28,152 cycles

LEFT WING O/B AFT FLAP I/B TRAILING EDGE LOWER SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP PER M/M.

Part: RETAINER — CRACKED (LT WING) · airframe 48,817 hrs · 28,152 cycles

LEFT WING I/B FIXED UPPER T/E AFT SEAL RETAINER CRACKED. REMOVED AND REPLACED SEAL RETAINER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,031 hrs · 27,038 cycles

L1 DOOR EMERGENCY EXTERIOR LIGHT INOP. RELAMPED LIGHT ASSY IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,816 hrs · 26,897 cycles

LEFT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW EA.

Part: COVER — OUT OF POSITION (EVAC SLIDE) · airframe 45,518 hrs · 26,130 cycles

R1 DOOR ESCAPE SLIDE GIRT PULL HANDLE COVER OUT OF POSITION. REPOSITIONED COVER PER M/M.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 45,518 hrs · 26,130 cycles

R2 DOOR ESCAPE SLIDE HAS EXCESSIVE GIRT EXPOSED OUT OF SLIDE COVER. RE-INSTALLED R2 SLIDE PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,788 hrs · 25,698 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 44,485 hrs · 25,510 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,469 hrs · 25,494 cycles

DURING SCHEDULED 12Y CHECK, RT MID CABIN EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST AT STA 603. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,469 hrs · 25,494 cycles

DURING SCHEDULED 12Y CHECK, RT AFT CABIN EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST AT STA 603. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — CRACKED (CABIN) · airframe 44,468 hrs · 25,493 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT SIDEWALL EMERGENCY EXIT LIGHT LENS CRACKED. R&R LENS PER MM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,468 hrs · 25,493 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX BULKHEAD ATTACH ANGLE CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED ANGLE PER ACO.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,749 hrs · 25,074 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC EXTERIOR SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,724 hrs · 24,493 cycles

DURING SCHEDULED MV2 CHECK FOUND, RT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 18. RELAMPED PER MM.

Part: COVER — MISSING (CABIN) · airframe 42,014 hrs · 24,108 cycles

RT EEPLS COVER MISSING. SECURED COVER PER MM.

Part: HMU — FAULTY (NR 1 ENGINE) · airframe 38,829 hrs · 22,282 cycles

AIR TURNBACK, NR 1 ENGINE COMPRESSOR STALLED. REMOVED AND REPLACED NR 1 ENGINE HMU PER MM.

Part: COVER — BROKEN (CABIN) · airframe 37,082 hrs · 21,254 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 36,899 hrs · 21,134 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 639. REPAIRED BEAM PER EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 36,009 hrs · 20,588 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 36,009 hrs · 20,588 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: BATTERY — FAILED (CABIN) · airframe 35,629 hrs · 20,368 cycles

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

Part: BATTERY — ACTIVATED (FLASHLIGHT) · airframe 35,346 hrs · 18,779 cycles

AFT OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 35,345 hrs · 20,204 cycles

AFT O/B EMERGENCY FLASHLIGHT BATTERY INDICATOR LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 34,451 hrs · 19,685 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN LENS MISSING. REPLACED SIGN ASSY PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 33,999 hrs · 19,402 cycles

R2 WINDOW ARCED IN COCKPIT. REMOVED AND REPLACED WINDOW PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 32,773 hrs · 18,656 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,389 hrs · 18,437 cycles

BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 16 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,201 hrs · 17,161 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CORRODED BETWEEN BS 986 AND BS 1006, LBL 45. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,201 hrs · 17,161 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,149 hrs · 17,129 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 47 TO LBL 47. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 30,149 hrs · 17,129 cycles

DURING SCHEDULED 8Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED INBOARD AFT CORNER. REPAIRED FLAP PER SRM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 29,688 hrs · 16,866 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: PUMP — LEAKING (HHYDRAULIC SYS) · airframe 29,169 hrs · 16,552 cycles

DIVERSION - HYDRAULIC -A- SYSTEM LEAKED TO ZERO. REMOVED AND REPLACED HYDRAULIC ELECTRIC PUMP PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · 16,304 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,501 hrs · 16,172 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 4 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 28,225 hrs · 16,027 cycles

DURING SCHEDULED HC1 CHECK, FOUND RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 128, 24 INCHES AFT OF FRONT SPAR. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 27,469 hrs · 15,604 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · 15,592 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: BULKHEAD — CANNING (AFT CABIN) · airframe 20,923 hrs · 11,869 cycles

DURING SCHEDULED HC2 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD OIL CANNED AT STR 2L. REPAIRED AFT PRESS BULKHEAD PER SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,789 hrs · 11,232 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD LT EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 19,012 hrs · 10,803 cycles

INFLIGHT SHUTDOWN, DIVERSION, DECLARED EMERGENCY. NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AT FL 410, FOLLOWED QRH, SHUT DOWN ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,823 hrs · 10,699 cycles

DURING SCHEDULED 5Y CHECK, FOUND FLOORBEAM AT BS 772, BETWEEN LBL 3 AND RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,065 hrs · 10,245 cycles

DURING SCHEDULED MV3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS AT ROWS 13 ABC, 22 ABC, INOP. RELAMPED EMERGENCY EXIT LIGHTS PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 17,081 hrs · 9,722 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER DAMAGED AT MID CABIN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 17,801 hrs · 9,722 cycles

DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 1 ABC, BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 14,864 hrs · 8,495 cycles

DURING SCHEDULED MS CHECK, FOUND SEVERAL EEPLS TRACK COVERS DAMAGED. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 9,827 hrs · 5,658 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTED. ADJUSTED SLIDE PER MM.

Part: COVER — BROKEN (CABIN) · airframe 9,827 hrs · 5,658 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER BROKEN AT ROW NR 9. REMOVED AND REPLACED COVER PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 3,036 hrs · 1,783 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY & AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSEBLIES OUT OF ADJUST. ADJUSTED GIRT ASSEBLIES PER MM.

Part: COMPUTER — MALFUNCTIONED (STALL MANAGEMENT) · airframe 2,386 hrs · 1,397 cycles

ABORTED TAKEOFF, NR 2 L/E SLAT AND L/E FLAP TRANSIT LIGHT ILLUMINATED PRIOR TO TAKEOFF AND WARNING HORN SOUNDED. REMOVED AND REPLACED NR 1 STALL MANAGEMENT COMPUTER PER MM.