N480WN

Part: SEAL — CRACKED (ZONE 300) · airframe 70,744 hrs · 42,176 cycles

LEFT HORIZONTAL STAB UPPER SLIDING SEAL CRACKED. REMOVED AND REPLACED SLIDING SEAL AND OPS CHECKED GOOD IAW AMM 53-31-31.

Part: SEAL — CRACKED (ZONE 300) · airframe 70,744 hrs · 42,176 cycles

RT HORIZONTAL STAB UPPER SLIDING SEAL CRACKED. REMOVED AND REPLACED RH HORIZONTAL STAB UPPER SLIDING SEAL REF AMM 53-31-31.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 70,744 hrs · 42,176 cycles

AFT L/H EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 70,287 hrs · 41,869 cycles

LEFT OVERWING EMERGENCY EXIT WINDOW LIGHT INOP. REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHT LAMP PER AMM 33-21-00-960-801-NG. OPS CHECKED GOOD.

Part: HANDLE — LOOSE (ZONE 800) · airframe 69,582 hrs · 41,441 cycles

FWD ENTRY DOOR UPPER ASSIST HANDLE IS LOOSE. RE SECURED FWD ENTRY DOOR UPPER ASSIST HANDLE REF AMM 20-50-11.

Part: ENGINE — POWER LOSS (NR 2) · airframe 69,222 hrs · 41,220 cycles

ON TAKEOFF; BOTH THROTTLES AND N1S CAME UP TO OVER 40%. #1 N1 CAME RIGHT UP TO 95.8%; #2 STAYED BACK AT JUST OVER 40%. BOTH THROTTLES CAME UP TO NORMAL POSITION<[01] PERFORMED INSPECTION OF #2 ENGINE FUEL PUMP IMPELLER IAW AMM 73-11-01. NO DEFECTS NOTED AT THIS TIME. PERFORMED INSPECTION OF PS3 LINE RUNNING FROM #2 ENGINE EEC TO HPC PORT PER ENGINEERING REQUEST. NO DAMAGE OR BLOCKAGE NOTED TO PS3 LINE ALONG THE ENTIRETY OF THE LINE.;[02] REF FIM 73-05 TASK 814. CW EEC BITE PROCEDURE; NO FAULTS FOUND. CW STEPS E(5)-(7) NO ERRATIC SIGNALS NOTED. PER ENGINEERING REQUEST COMPLY WITH TEST 8-ACCELERATION CHECK AMM 71-00-00-700-824-F00;[03] REFERENCE TASK ID: TTG8Q010KDVR FOR PREVIOUS WORK PERFORMED. ACCOMPLISHED TEST 8?ACCELLERATION TEST PER M/M 71-00-00. OPS CHECKS OK.

Part: SIGN — DETACHED (ZONE 200) · airframe 67,001 hrs · 39,826 cycles

EMERGENCY EXIT SIGN AT THE R/H OVER WING EXIT FELL OFF<[01] INSTALLED NEW EMERGENCY EXIT SIGN LENS BELOW RH OVERWING EXIT IAW AMM 33-51-01

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 66,683 hrs · 39,621 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED L1 DOOR EXTERIOR EMERGENCY LIGHT AS PER B737 AMM 33-51-04-960-802. OPERATIONAL TEST PASSED.;[02] VERIFIED STEP 1.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 66,683 hrs · 39,621 cycles

FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE IN THE PASSENGER CABIN.<[01] PERFORMED T/S OF THE EMERGENCY LIGHT SYSTEM AS PER B737 WDM 31-51-12 AND FOUND THE BATTERY PACK AT POSITION M1674 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT POSITION M1674 PER REF B737 AMM 33-51-06-960-805. PERFORMED OPERATIONAL TEST OF NEW BATTERY PACK AT POSITION M1674 PER REF B737 AMM 33-51-06-960-805; TEST PASSED.;[02] CORRECTION TO STEP 1:<BR>PERFORMED T/S OF THE EMERGENCY LIGHT SYSTEM AS PER B737 WDM 33-51-12 AND FOUND THE BATTERY PACK AT POSITION M1674 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT POSITION M1674 PER REF B737 AMM 33-51-06-960-805. PERFORMED OPERATIONAL TEST OF NEW BATTERY PACK AT POSITION M1674 PER REF B737 AMM 33-51-06-960-805; TEST PASSED.;[03] VERIFIED STEP 2.

Part: PANEL — CORRODED (ZONE 100) · airframe 66,683 hrs · 39,621 cycles

FOUND PANEL 192F WITH LIGHT SURFACE CORROSION AT ANTENNA BASE AND BONDING SEAL DAMAGE<[01] RECEIVED NEW PANEL 192F<BR>PART:654A0004-613<BR>PANEL WILL BE INSTALL ON (TTG8Q00TMJJR);[02] VERIFIED STEP 1<BR><BR>AUDIT C/W REF. MPM 52.02.02

Part: ANGLE — CORRODED (ZONE 100) · airframe 66,683 hrs · 39,621 cycles

*CORROSION* LATERAL TRANSITION ANGLE UPPER SURFACE STA 947 AT LBL 3 APPROX S-27L WL 156. 1245-003 AFT CARGO COMPARTMENT.<[01] REMOVED AND REPLACED TRANSITION ANGLE AT AFT CARGO STA 947 AT LBL 21- RBL 21 PER SRM 51-40-02-0G-0 AND DWG# 149A8118;[02] VERIFIED STEP 1<BR><BR>AUDIT C/W REF. MPM 52.02.02

Part: ANGLE — CORRODED (ZONE 100) · airframe 66,683 hrs · 39,621 cycles

AFT CARGO AT STA 727 RBL 21 S-25R WL 156 FLOOR SUPPORT ANGLE HAS A RUSTED FASTENER NUT - VIEWED FROM UNDERSIDE. 124-013<[01] REMOVED AND REPLACED NUT AT AFT CARGO AT STA 727 RBL 21 S-25R WL 156 FLOOR SUPPORT ANGLE PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 2<BR><BR>AUDIT C/W REF. MPM 52.02.02

Part: SEAL — DETERIORATED (ZONE 600 FLAP) · airframe 66,683 hrs · 39,621 cycles

INBOARD FLAP UPPER SKIN RIGHT WING PANEL 653ET SEAL DETERIORATED.<[01] REMOVED AND REPLACED SEAL AT R/W INBOARD FLAP UPPER SKIN RIGHT WING PANEL 653ET PER REF SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION STEP 1

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 66,683 hrs · 39,621 cycles

CABIN FLOOR PANEL 242DF WITH UPPER SKIN AREA DELAMINATED / TORN.<[01] RECEIVED FLOOR PANEL 242DF WILL BE INSTALLED ON TTG8Q00TMJLS.;[02] VERIFIED STEP 1 <BR><BR>AUDIT C/W MPM 52.02.02

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 66,683 hrs · 39,621 cycles

CABIN FLOOR PANEL 242CF UPPER SKIN WITH DELAMINATED / TORN AREAS.<[01] RECEIVED FLOOR PANEL 242CF WILL BE INSTALLED ON TTG8Q00TMK0C;[02] VERIFIED STEP 1<BR><BR>AUDIT C/W MPM 52.02.02

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 66,683 hrs · 39,621 cycles

CRACK FOUND AT INTERNAL MAIN CABIN HORIZONTAL PRESSURE WEB STA 673 RBL 42.<[01] ACCOMPLISHED R/H PRESSURE DECK WEB REPAIR BETWEEN STA 663.75 TO STA 675 AND BETWEEN RBL 30 TO RBL 60 IN REF B737-700 SRM 53-40-51-2R-2 FIG 202.;[02] VERIFIED STEP 1<BR><BR>AUDIT C/W REF. MPM 52.02.02;[03] ALL TASK STEPS C/W

Part: PLATE — LOOSE (ZONE 600) · airframe 66,683 hrs · 39,621 cycles

RIGHT WING DEFLECTOR RIB TO DEFLECTOR PANEL AT SERRATED PLATES LOOSE<[01] ACCOMPLISHED REPAIR AT RIGHT WING DEFLECTOR RIB UPPER TAB IN REF B737-700 SRM 57-51-02-2R-4; VIEW A-A AND 57-51-02-2R-1; VIEW B-B.;[02] VERIFIED STEP 1

Part: LIGHT — MISSING (CABIN) · airframe 66,408 hrs · 39,450 cycles

ESCAPE PATH EGRESS STRIP MISSING AT SEAT 24C<[01] REPLACED MISSING PHOTO ILLUMINATION STRIP PER AMM 33-51-15

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 66,221 hrs · 39,328 cycles

EMERGENCY LIGHTS NEAR FO OWE FLICKER THEN GO OUT.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)] FWD OF FO OWE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 66,090 hrs · 39,239 cycles

EMERGENCY AISLE EXIT SIGN MISSING<[01] FOUND AND INSTALLED LENS REF AMM 33-51-01

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,599 hrs · 38,938 cycles

L1 SLIDE LIGHT AND ASSOCIATED INTERIOR LIGHTED SIGNS INOP.<[01] R&R'D BATTERY PACK M1675 PER AMM 33-51-06.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,637 hrs · 38,354 cycles

R/H SLIDE/OVERWING EMERGENCY LIGHT INOP<[01] RELAMPED R/H SLIDE/OVERWING EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.

Part: ISOLATOR — CRACKED (ZN 800 DOOR) · airframe 64,147 hrs · 38,052 cycles

FWD SERVICE DOOR AFT SLIDE ATTACH ISOLATOR CRACKED<[01] R&R FWD SERVICE DOOR AFT SLIDE ATTACH ISOLATOR IAW AMM 52-41-00.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,132 hrs · 38,042 cycles

2 BULLNOSE EMERGENCY LIGHT AND OVERWING EMERGENCY LIGHT INOP<[01] PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW 33-51-00.OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,426 hrs · 37,582 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED OPS CHECK GOOD REF AMM 33-51-04

Part: LENS — LOOSE (ZN 200 FUS TOP) · airframe 63,172 hrs · 37,422 cycles

FORWARD SERVICE DOOR; EMERGENCY EXIT LENSE-LOOSE.<[01] OK TO CONTINUE ON TLD PER EA M-21-133-00720; SECURED LENSE IN POSITION ABOVE FWD SERVICE DOOR.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,032 hrs · 37,325 cycles

RH OVERWING EMERGENCY EXIT LIGHT INOP<[01] RELAMPED RH OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-04. OPERATIONAL CHECK GOOD.

Part: SLIDE — LOOSE (ZN 200 FUS TOP) · airframe 62,887 hrs · 37,234 cycles

R1 DOOR SLIDE GIRT BAR STOW BRACKET LOOSE<[01] R&R?ED R1 DOOR SLIDE GIRT BAR STOW BRACKET FASTENER PER SRM 51-40-02.<BR>R&R?ED R1 DOOR SLIDE CONTAINER PER MT 725-61-06 TO FOM<BR>SLIDE NOT REMOVED FROM CONTAINER.

Part: SKIN — DEBONDED (NR 8 SLAT) · airframe 62,240 hrs · 36,808 cycles

#8 SLAT T/E #8 SLAT T/E REPAIR DISBOND AND MISSING. REPAIRED #8 SLAT TE PERMANENT REPAIR PER SRM 57-42-01-2R-6.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CRACK ON WEB INTERCOSTAL ON BS 312 TO BS 294.5 RBL 16 AT PASSENGER CABIN 2022-287891 / [01] REPLACED OF NEW WEB INTERCOSTAL AND FASTENERS LOC ON BS 312 TO BS 294.5 RBL 16 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A5400 REV: A.;[02] CORRECTED STEP 1<BR>REPLACED OF NEW WEB INTERCOSTAL AND FASTENERS LOC ON BS 312 TO BS 294.5 RBL 16 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A5400 REV: A.SEE INDIVIDUAL SIGN OFF BELLOW.;[03] REPLACED OF NEW WEB INTERCOSTAL AND FASTENERS LOC ON BS 312 TO BS 294.5 RBL 16 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A5400 REV: A.SEE INDIVIDUAL SIGN OFF BELLOW.<BR>CERTIFIED AS RII

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CRACK INDICATION ON FASTENER HOLE OF INNER CHORD LOCATED AT BS 294.5 AT RBL 10 AND WL 208.1 2022-287889 / [01] REPLACED INNER CHORD LOCATED BETWEEN BS 259.50 TO BS 360.00 AND WL 208.1 IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 141A8510 REV - ; 143A5900 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INNER CHORD LOCATED BETWEEN BS 259.50 TO BS 360.00 AND WL 208.1 IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 141A8510 REV - ; 143A5900 REV - SEE INDIVIDUAL SIGN OFF BELOW. ITEM RII

Part: DOOR — CRACKED (L/H MLG) · airframe 60,471 hrs · 35,653 cycles

CRACK CENTER DOOR ON LT MAIN LANDING GEAR 2022-287881 / [01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: B20189511 DUE DATE: 16-SEP-22;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[03] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030456 DUE DATE: 26 JAN 23.;[04] PERFORMED PERMANENT REPAIR ON CENTER DOOR ON LT LANDING GEAR I.A.W SRM B737-700 52-80-02-2R-3 REPAIR 3; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[05] REJECT MISSING ULTRASONIC INSPECT ON REPAIR PARTS FITTING ITEM 1 AND ANGLE ITEM 3 CENTER DOOR LT MLG REQUIRED ON TABLE 201 REPAIR MATERIAL B737-700 SRM 52-80-02-2R-3. FAULT RAISED TTG8Q00D4W88.;[06] VERIFIED CERTIFIED INSPECTION REPORT AND THIS MATERIAL HAS BEEN ULTRASONICALLY INSPECTION MATERIAL USED PO: 2021 223579 IAW SRM B737-700 51-10-02;[07] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: BRACKET — CRACKED (R/H WING) · airframe 60,471 hrs · 35,653 cycles

CRACK SUPPORT BRACKET LOCATED ON ORSS 273 TRAILING EDGE AT RT WING 2022-287873 / [01] REPLACED SUPPORT BRACKET LOCATED ON ORSS 273 TRAILING EDGE AT RT WING I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] REPLACED SUPPORT BRACKET LOCATED ON ORSS 273 TRAILING EDGE AT RT WING I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9

Part: PLATE — CRACKED (L/H WING) · airframe 60,471 hrs · 35,653 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING 2022-287863 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 REV. -. SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: LENS — DETERIORATED (AFT CABIN) · airframe 60,471 hrs · 35,653 cycles

DETERIORATED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA 2022-287867 / [01] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-802 3. C. (10);[02] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-802 3. C. (10)

Part: SUPPORT ANGLE — CRACKED (AFT CARGO) · airframe 60,471 hrs · 35,653 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 12 INCH BETWEEN STR26R TO STR27R AT AFT CARGO COMPARTMENT 2022-287846 / [01] MADE ANGLE SUPPORT LOCATED BS 907 PLUS 12 INCH BETWEEN STR26R TO STR27R AT AFT CARGO COMPARTMENT IAW DRAWING 147A7221 REV D;[02] REPLACED SUPPORT ANGLE LOCATED BS 907 PLUS 12 INCH BETWEEN STR26R TO STR27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 147U7221 REV D;[03] REPLACED SUPPORT ANGLE LOCATED BS 907 PLUS 12 INCH BETWEEN STR26R TO STR27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 147U7221 REV D SEE INDIVIDUAL SING OFF BELOW;[04] REPLACED SUPPORT ANGLE LOCATED BS 907 PLUS 12 INCH BETWEEN STR26R TO STR27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 147U7221 REV D SEE INDIVIDUAL SING OFF BELOW AS RII;[05] REPLACED SUPPORT ANGLE LOCATED BS 907 PLUS 12 INCH BETWEEN STR26R TO STR27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 147U7221 REV D SEE INDIVIDUAL SING OFF BELOW

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 60,471 hrs · 35,653 cycles

CORROSION ON CHANNEL SIDEPLATE LOCATED BETWEEN BS492 TO BS500A RBL21 AND WL156 AT LEVEL FLOOR STRUCTURE AT FWD CARGO COMPARTMENT 2022-287799 / [01] REPLACED CHANNEL SIDEPLATE LOCATED BETWEEN BS492 TO BS500A RBL21 AND WL156 AT LEVEL FLOOR STRUCTURE AT FWD CARGO COMPARTMENT IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-143A0080 REV: -;[02] CORRECTED STEP 1 <BR>REPLACED CHANNEL SIDEPLATE LOCATED BETWEEN BS492 TO BS500A RBL21 AND WL156 AT LEVEL FLOOR STRUCTURE AT FWD CARGO COMPARTMENT IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-143A0080 REV:- SEE INDIVIDUAL SIGN OF BELOW;[03] REPLACED CHANNEL SIDEPLATE LOCATED BETWEEN BS 492 TO BS500A RBL21 AND WL156 AT LEVEL FLOOR STRUCTURE AT FWD CARGO COMPARTMENT IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-143A0080 REV:- RII; SEE INDIVIDUAL SIGN OF BELOW

Part: SUPPORT ANGLE — CRACKED (AFT CARGO) · airframe 60,471 hrs · 35,653 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 7 INCH BETWEEN STR26R TO STR27R AT AFT CARGO COMPARTMENT 2022-287842 / [01] REPLACED SUPPORT ANGLE LOCATED BS 907 PLUS 7 INCH BETWEEN STR26R TO STR27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 147A7221 REV D.;[02] REPLACED SUPPORT ANGLE LOCATED BS 907 PLUS 7 INCH BETWEEN STR26R TO STR27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 147A7221 REV D SEE INDIVIDUAL SING OFF BELOW;[03] REPLACED SUPPORT ANGLE LOCATED BS 907 PLUS 7 INCH BETWEEN STR26R TO STR27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 147A7221 REV D SEE INDIVIDUAL SING OFF BELOW AS RII

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CRACK INTERNAL STRUCTURE ACCESS DOOR WEATHER RADAR SUPPORT ANGLE AT LOWER NOSE COMPARTMENT (1 EA) 2022-287737 / [01] REPLACED SUPPORT ANGLE LOCATED INTERNAL STRUCTURE ACCESS DOOR WEATHER RADAR AT LOWER NOSE COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 141A9194 REV D SEE INDIVIDUAL SING OFF BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CRACK FLOOR STRUCTURE WEB BTW BS 312 TO BS 328 AT RBL 30 AT PASSENGER CABIN 2022-287712 / [01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AT RBL 30 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 141A5400 REV -;[02] CORRECTED STEP 1.<BR>REPLACED WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AT RBL 30 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 141A5400 REV -. SEE INDIVIDUAL SIGN OFF BELLOW.;[03] REPLACED WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AT RBL 30 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 141A5400 REV -. SEE INDIVIDUAL SIGN OFF BELLOW.<BR>CERTIFIED AS RII

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CORROSION FLOORBEAM ON BS 312 AT LBL 14 AND WL 208.1 AT PASSENGER CABIN 2022-287708 / [01] TOOL USED PRECISION RADIUS GAUG P/N:2204A3 S/N:AE-408656 DUE DATE:29-JAN-23;[02] 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.;[03] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030456 DUE DATE: 26 JAN 23.;[04] PERFORMED PERMANENT REPAIR ON FLOORBEAM ON BS 312 AT LBL 14 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 53-10-51-2R-17 REPAIR 17 SEE INDIVIDUAL SIGN OF BELOW;[05] TASK CARD COMPLETED <BR>RII

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CORROSION FLOORBEAM ON BS 294.5 AT RBL 10 AND WL 208.1 AT PASSENGER CABIN 2022-287707 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210136503 DUE DATE: 11-APR-23<BR><BR>TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210136503 DUE DATE: 11-APR-23;[02] TOOL 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;[03] PERFORMED PERMANENT REPAIR ON FLOORBEAM ON BS 294.5 AT RBL 10 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16 SEE INDIVIDUAL SIGN OF BELOW;[04] TASK CARD COMPLETED <BR>RII

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CORROSION FLOORBEAM ON BS 328 AT RBL 40 AND WL 208.1 AT PASSENGER CABIN 2022-287709 / [01] TOOL USED ULTRASONIC GAGE P/N: 45MG; S/N: 130061901; DUE DATE: 08-APR-23.;[02] PERFORMED PERMANENT REPAIR ON FLOORBEAM ON BS 328 AT RBL 40 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 53-10-51-2R-7 SEE INDIVIDUAL SIGN OFF BELOW;[03] PERFORMED PERMANENT REPAIR ON FLOOR BEAM ON BS 328 AT RBL 40 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 53-10-51-2R-7 SEE INDIVIDUAL SIGN OFF BELOW<BR>CERTIFIED AS RII

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CRACK FLOOR STRUCTURE WEB BTW BS 270 TO BS 294.5 AT BL 0 AT PASSENGER CABIN 2022-287711 / [01] REPLACED WEB ON FLOOR STRUCTURE WEB BTW BS 270 TO BS 294.5 AT BL 0 AT PASSENGER CABIN IAW B737-700 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 141A5400 REV- SEE INDIVIDUAL SING OFF BELOW;[02] REPLACED WEB ON FLOOR STRUCTURE WEB BTW BS 270 TO BS 294.5 AT BL 0 AT PASSENGER CABIN IAW B737-700 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 141A5400 REV- SEE INDIVIDUAL SING OFF BELOW<BR>CERTIFIED AS RII

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CORROSION FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT RBL 28 AND WL 208.1 AT PASSENGER CABIN 2022-287634 / [01] REPLACED FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT RBL 28 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING # 147A5730 REV:C SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT RBL 28 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 451-40-02 AND DRAWING # 147A5730 REV:C SEE ;RII INDIVIDUAL SIGN OFF BELOW;[03] REPLACED FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT RBL 28 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING # 147A5730 REV:C ;RII .SEE INDIVIDUAL SIGN OFF BELOW

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CRACK FRAME BS 312 BT STR 5L TO STR 6L AT PASSENGER CABIN 2022-287643 / [01] PERFORMED PERMENENT REPAIR ON FRAME 312 BTW S-5 TO S-6 LH SIDE I.A.W EA M-22-153-01244;[02] PERFORMED PERMENENT REPAIR ON FRAME 312 BTW S-5 TO S-6 LH SIDE I.A.W EA M-22-153-01244<BR><BR>RII ACCOMPLISHED

Part: FLOOR PANEL — BROKEN (FWD GALLEY) · airframe 60,471 hrs · 35,653 cycles

BROKEN FLOOR PANEL 221BF AT AT FWD GALLEY AREA 2022- 287618 / [01] REPAIRED PANEL 221BF AT FWD GALLEY AREA I.A.W EA 22-153-01793-WIP1 AND EA SUMMARY 22-153-01793;[02] REPAIRED PANEL 221BF AT FWD GALLEY AREA I.A.W EA 22-153-01793-WIP1 AND EA SUMMARY 22-153-01793

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CORROSION FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT LEVEL LBL 3 AND WL 208.1 AT PASSENGER CABIN 2022-287641 / [01] REPLACED FLOOR STRUCTURE PLATE BTW BS 1006 TO BS 1032 AT LEVEL LBL 3 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A5600 REV. B SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED FLOOR STRUCTURE PLATE BTW BS 1006 TO BS 1032 AT LEVEL LBL 3 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A5600 REV. B SEE INDIVIDUAL SIGN OFF BELOW.<BR><BR>RII ACCOMPLISHED

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CORROSION FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT LEVEL RBL 3 AND WL 208.1 AT PASSENGER CABIN 2022-287637 / [01] REPLACED FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT LEVEL RBL 3 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING # 147A5730 REV: C SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT LEVEL RBL 3 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING # 147A5730 REV: C ;RII .SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CORROSION FLOORBEAM ON BS 986 AT RBL 35 AND WL 208.1 AT PASSENGER CABIN 2022-287622 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N:N500X1693P030456; CAL DUE DATE: 26-JAN-23;[02] PERFORMED REPAIR ON FLOOR BEAM ON BS 986 AT RBL 35 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 53-70-51-2R-4 THIS REPAIR IS CATEGORY A. SEE INDIVIDUAL SIGN OFF BELOW;[03] PERFORMED REPAIR ON FLOORBEAM ON BS 986 AT RBL 35 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 53-70-51-2R-4 THIS REPAIR IS CATEGORY A. SEE INDIVIDUAL SIGNS OFF BELOW. RII ITEM

Part: ACCESS PANEL — DELAMINATED (L/H WING) · airframe 60,471 hrs · 35,653 cycles

DELAMINATED ACCESS PANEL 521TB AT LT WING 2022-287616 / [01] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 13061394 DUE DATE: 05/AUG/22.;[02] TOOL USED: SCALE P/N: SCA-301 S/N: AE-412123 DUE DATE: 14-MAR-23;[03] REPAIRED ACCESS PANEL 521TB AT LT WING IAW B737-700 SRM 57-41-01-2R-6 REPAIR 6. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] TASK COMPLETED. RII COMPLETED.

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CRACK ACCESS PANEL 191AL BODY FAIRING AT LOWER FUSELAGE 2022-287621 / [01] TOOL USED: CALIPER P/N: 500-464 S/N: 15331926 DUE DATE: 28-SEP-22;[02] TOOL USED HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 28-FEB-23.;[03] TOOL USED SCALE P/N: CL5000; S/N: AE-408753; DUE DATE: 01-APR-23.;[04] TOOL USED: SCALE: P/N: SCA-301 S/N:AE-412124 DUE DATE:14-MAR-23;[05] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22;[06] REPAIRED ACCESS PANEL 191AL BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED.

Part: BATTERY — INOPERATIVE (L/H CABIN) · airframe 60,471 hrs · 35,653 cycles

INOP EMERGENCY EXIT LIGHT BATTERY UNDER EMERGENCY EXIT DOOR AT PASSENGER CABIN (1 EA) 2022-287608 / [01] INSTALLED EMERGENCY EXIT LIGHT BATTERY UNDER EMERGENCY EXIT DOOR AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-06-960-804 STEP 4.E (5) (6).;[02] CORRECTED STEP 1: INSTALLED EMERGENCY EXIT LIGHT BATTERY UNDER EMERGENCY EXIT DOOR AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-06-960-804 STEP 4.E (5) (6). TEST IS OK;[03] CORRECTED STEP 2: REPLACED EMERGENCY EXIT LIGHT BATTERY UNDER EMERGENCY EXIT DOOR LH SIDE AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-06-960-804 STEP 4.E (5) (6). TEST IS OK;[04] CERTIFIED WORK PERFORMED.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 60,471 hrs · 35,653 cycles

CRACK CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-287580 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A18135080; DUE DATE: 31-JUL-22.;[02] REPAIRED CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFF BELOW.;[03] TASK COMPLETED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CRACK ANGLE FLOOR STRUCTURE ON BS 697 AT BL 0 AT PASSENGER CABIN 2022-287589 / [01] REPLACED ANGLE OF FLOOR STRUCTURE ON BS 697 AT BL 0 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 273A9112 REV - AND DWG 273A9110 REV. A;[02] REPLACED ANGLE OF FLOOR STRUCTURE ON BS 697 AT BL 0 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 273A9112 REV - AND DWG 273A9110 REV. A.. RII ITEM

Part: BRACKET — CORRODED (R/H PYLON) · airframe 60,471 hrs · 35,653 cycles

CORROSION BRACKET STRUT FAIRING LOC. FWD UPPER AREA AT RT PYLON 2022-287587 / [01] REPLACED BRACKET STRUT FAIRING LOC. FWD UPPER AREA AT RT PYLON I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 311A2511 REV.C.;[02] CORRECTED STEP 1<BR>REPLACED BRACKET STRUT FAIRING LOC. FWD UPPER AREA AT RT PYLON I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 311A2511 REV.C. MEASURES OF CORROSION ARE: L:0.542? W:0.324? RT: 0.020? TOOL USED CALIPER P/N: 500-197-30 S/N: A21043164 DUE DATE: 01-SEP-22;[03] REPLACED BRACKET STRUT FAIRING LOC. FWD UPPER AREA AT RT PYLON I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 311A2511 REV.C. MEASURES OF CORROSION ARE: L:0.542? W:0.324? RT: 0.020? TOOL USED CALIPER P/N: 500-197-30 S/N: A21043164 DUE DATE: 01-SEP-22

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CRACK ANGLE FLOOR STRUCTURE ON BS 697 AT RBL 24.75 AT PASSENGER CABIN 2022-287591 / [01] TOOL 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 NEW ANGLE ON FLOOR STRUCTURE ON BS 697 AT RBL 24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND DWG 111A6000 REV -. SEE INDIVIDUAL SIGN OFF BELLOW.;[03] REPLACED NEW ANGLE ON FLOOR STRUCTURE ON BS 697 AT RBL 24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND DWG 111A6000 REV -. SEE INDIVIDUAL SIGN OFF BELLOW.<BR>CERTIFIED AS RII

Part: STUB FRAME — CRACKED (FWD GALLEY) · airframe 60,471 hrs · 35,653 cycles

CRACK SERVICE DOOR CUT OUT FWD LOWER STUB FRAME BS 294 AT FWD GALLEY AREA 2022-287586 / [01] TOOL: USED POWER PAK; P/N: WCI-20; S/N: 2503AT; DUE DATE: 27-FEB-23; COLD WORKING KITS; PN: STD 4-4-N; SN: AE-37966; DUE DATE: 09-DEC-22.; PULLER UNIT; PN: LB-20; SN: 3541; DUE DATE: 02-MAR-23;[02] REPLACED STUB FRAME SERVICE DOOR CUT OUT FWD LOWER BS 294.5 FWD GALLEY AREA IAW SRM B737-700 51-40-02; DRAWING # 141A8370 REV-D; DRAWING# 141A8430 REV-B; SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPLACED STUB FRAME SERVICE DOOR CUT OUT FWD LOWER BS 294.5 FWD GALLEY AREA IAW SRM B737-700 51-40-02; DRAWING # 141A8370 REV-D; DRAWING# 141A8430 REV-B; RII ; SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 60,471 hrs · 35,653 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.750 INCH 2022-287600 / [01] TOOL USED : EDDY CURRENT TOOL; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 26 JAN 23.;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030456 DUE DATE: 26 JAN 23.;[03] PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.500 INCH FROM FRONT SPAR IAW SRM B737-700 55-10-01-2R-11 REPAIR 11. SEE INDIVIDUAL SING-OFF BELOW;[04] PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.500 INCH FROM FRONT SPAR IAW SRM B737-700 55-10-01-2R-11 REPAIR 11. SEE INDIVIDUAL SING-OFF BELOW AS RII

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 60,471 hrs · 35,653 cycles

CRACK TIE CLIP BS 270 STR 10R AT PASSENGER CABIN 2022-287585 / [01] REPLACED TIE CLIP BS 270 STR 10R AT PASSENGER CABIN IAW SRM B737-700 51-40-02 AND DRAWING 141A1110 REV:- SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED TIE CLIP BS 270 STR 10R AT PASSENGER CABIN IAW SRM B737-700 51-40-02 AND DRAWING 141A1110 REV:-<BR>RII ACCOMPLISHED <BR> SEE INDIVIDUAL SIGNOFF BELOW

Part: SKIN — CRACKED (R/H HORIZ. STAB.) · airframe 60,471 hrs · 35,653 cycles

CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.125 INCH 2022-287601 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN. 60009161631; DUE DATE: 03-DEC-22;[02] TOOL USED : EDDY CURRENT TOOL; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 26 JAN 23.;[03] PERFORMED REPAIR ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.500 INCH FROM FRONT SPAR IAW B737-700 SRM 55-10-01--2R-11 REPAIR 11. SEE INDIVIDUAL SIGN-OFF BELOW;[04] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PANEL — CRACKED (AFT CARGO) · airframe 60,471 hrs · 35,653 cycles

CRACK ACCESS PANEL 142NWB AT AFT CARGO COMPARTMENT 2022-287459 / [01] REPAIRED BULKHEAD PANEL 142NWB AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-805. TOOL USED :CALIPER P/N:500-197-30 ; S/N:A21041924; DUE DATE: 10SEP22. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPAIRED BULKHEAD PANEL 142NWB AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-805. TOOL USED :CALIPER P/N:500-197-30 ; S/N:A21041924; DUE DATE: 10SEP22. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 60,471 hrs · 35,653 cycles

CRACK FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT 2022-287508 / [01] REPLACED FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT IAW DRAWING 453A1610-2 REV D;[02] REPLACED FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT IAW DRAWING 453A1610-2 REV D B737-700 AMM 25-52-01-201-801 MATERIAL USED A90RG1W-48144 PO USE 2021-123272/001;[03] REPLACED FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT IAW DRAWING 453A1610-2 REV D B737-700 AMM 25-52-01-201-801 MATERIAL USED A90RG1W-48144 PO USE 2021-123272/001

Part: LENS — OUT OF POSITION (R1 DOOR) · airframe 59,809 hrs · 35,240 cycles

DOOR 1 R EMER EXIT SIGN NEAR FLOOR; ARROW POINTING WRONG DIRECTION / [01] INSTALLED EXIT LENS FOR R1 DOOR IAW AMM 33-51-01. OPS CHK GOOD. A/C OK FOR SERVICE.

Part: FLOORBOARD — PULLED (FUSELAGE) · airframe 58,874 hrs · 34,680 cycles

A22-06; PASSENGER CABIN FLOORBOARD; UPPER SURFACE; FACE SHEET PLIES PULLING. ; CORRECTION: FLOOROARD 232SF / [01] EVALUATED PANEL 232SF AND FOUND AREA OF PULLED FIBER ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A REV 74. CLEAN AND PREP AREA FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR3A;C;D&E. BONDED REPAIR PLIES. IAW B737-700 SRM 53-00-50-2R-1 PAR3K-M REV74. AAR DIGITAL THERMOMETER 30347 150DEG 3HRS. REPAIRED AREA OF PULLED FIBER'S ON UPPER SURFACE OF PANEL 232SF. IAW B737-700 SRM 53-00-50-2R-1 SRM 53-00-50-2R-0.

Part: NONE — PULLED (FUSELAGE) · airframe 58,874 hrs · 34,680 cycles

A22-07; PASSENGER CABIN FLOORBOARD 242BF; UPPER SURFACE; FACE SHEET PLIES PULLING. ; / [01] EVALUATED FLOOR PANEL 242BF AND FOUND PULLED FIBERS ON UPPER FACESHEET THE LENGTH OF THE BOARD. DAMAGE TO PANEL IS BEYOND ECONOMICAL REPAIR. PANEL TO BE REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 REV. 73<BR><BR>REPLACED PANEL BY FABRICATING NEW PANEL OUT OF FLOORBOARD STOCK (WN0742) IAW SRM 53-00-50-2R-0 RE. 73 TABLE 204 AND BOEING DWG 144A5810-2<BR><BR>INSTALLED INSERTS IN PANEL IAW BAC 5085 REV. F SECT. 8.4.2.2. INSERTS (SL5107A3-410) ADHESIVE (A89701); [02] OK

Part: FLOORBOARD — PULLED (FUSELAGE) · airframe 58,874 hrs · 34,680 cycles

PAX CABIN FLOORBOARD 231XF; UPPER SURFACE; FACE SHEET PLIES PULLING.<EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAS SRM 53-00-50-2R-1. TAP TEST GOOD. CLEANED AND PREPARED IAW SRM 53-00-50-2R-1 STEP 3 A C E F. VERIFIED MATERIAL IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201. RESIN A94085 FABRIC A24484 NEED OK TO BOND STEP 1 OK OK TO BOND BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K THRU M AND SRM 53-00-50-2R-0 REPAIR GENERAL STEP 5 J K L N O R. CURED AT 150 DEG OVEN B0-06 EXP 11-20-2021. TAP TEST GOOD. REPAIRED PASSENGER CABIN FLOORBOARD 231XF UPPER SURFACE IAW SRM 53-00-50-2R-1 REPAIR 1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.

Part: FLOORBOARD — PULLED (FUSELAGE) · airframe 58,874 hrs · 34,680 cycles

A22-08; PASSENGER CABIN FLOORBOARD 232RF; UPPER SURFACE; FACE SHEET PLIES PULLING. ; / [01] EVALUATED PANEL 232RF AND FOUND NO PULLED PLIES. FOUND DAMAGE TO CORE ON EDGE'S. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-10 REP 10 PAR1A REV 74. CLEAN AND PREP AREA'S FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-10 PAR3A-D. APPLIED POTTING COMPOUND TO EDGE'S. IAW B737-700 SRM 53-00-50-2R-10 PAR3E-G. AAR DIGITAL THERMOMETER 30347 125DEG 5HRS. (72836); [02] REPAIRED AREA'S OF EDGE DAMAGE TO CORE ONLY ON PANEL 232RF. IAW B737-700 SRM 53-00-50-2R-10 REP 10; SRM 53-00-50-2R-0 REP GEN.; [03] STEPS 1 AND 2 OK

Part: FLOORBOARD — PULLED (FUSELAGE) · airframe 58,874 hrs · 34,680 cycles

PAX CABIN FLOORBOARD 241BF, UPPER SURFACE, SHEET PLIES PULLING. EVALUATED DAMAGE TO UPPER SURFACE DAMAGE IS REPAIRABLE IAW SRM 53-00-50-2R-1 REPAIR 1. NO DELAMINATION NOTED. CLEANED AND PREPPED REPAIR AREA IAW SRM 53-00-50-2R-1 REPAIR 1 PAR 3 AND SRM 53-00050-2R-0 REPAIR GENERAL. BONDED REPAIR PLIES ON UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 REPAIR 1 PAR 3 STEPS KLAND M AND IAW B737 SRM 53-00-50-2R-0 REPAIR GENERAL. CURED AT 150 DEGREES FOR 4 HOURS THERMOMETER AAR30347 CAL DUE 4/29/22. TAP TEST GOOD. REPAIRED PASSENGER CABIN FLOORBOARD 241BF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 REPAIR 1 AND IAW B737 SRM 53-00-50-2R-0 REPAIR GENERAL.

Part: FLOORBOARD — PULLED (FUSELAGE) · airframe 58,874 hrs · 34,680 cycles

PAX CABIN FLOORBOARD 241AF. UPPER SURFACE, SHEET PLIES PULLING.<EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. TAP TEST GOOD. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A C E-F AND SRM 53-00-50-2R-0 REPAIR GENERAL STEP 5 A B D-E. VERIFIED MATERIAL IAW SRM 53-00-50-2R-1. BONDED REPAIR IAW SRM 53-00-5-2R-1 STEP 3 K-M AND SRM 53-00-50-2R-0 REPAIR GENERAL STEP 5 J-L N O R. CURED AT 150 DEGREES (OVEN B0-06 EXP 11-20-21). TAP TEST GOOD. REPAIRED PASSENGER CABIN FLOOR BOARD 241AF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.

Part: FLOORBOARD — PULLED (FUSELAGE) · airframe 58,874 hrs · 34,680 cycles

PAX CABIN FLOORBOARD 231ZF, UPPER SURFACE SHEET PLIES PULLING. EVALUATED PANEL 231ZF AND FOUND NO DAMAGE TO PLIES ON UPPER SURFACE. FOUND DAMAGE TO CORE ON EDGE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-10 REP 10 PAR 1A. CLEAN AND PREP AREA'S FOR REPAIR. IAW SRM 53-00-50-2R-10 PAR3A-D. APPLIED POTTING COMPOUND TO EDGE OF PANEL & SANDED DOWN. IAW SRM 53-00-50-2R-10 PAR3E-G. REPAIRED CORE EDGE DAMAGE ON PANEL 231ZF IAW SRM 53-00-50-2R-10 SRM 53-00-50-2R-0.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,951 hrs · 33,554 cycles

R/H EMERGENCY EXT. LIGHT CLOSE TO TRAILING EDGE FLAP INOP / RELAMPED R/H EXT. EMERGENCY LIGHT LOCATED CLOSE TO TRAILING EDGE FLAP PER AMM 33-51-04 OP CHECK GOOD

Part: PANEL — DAMAGED (WNG-BDY FAIRING) · airframe 56,120 hrs · 33,063 cycles

193B PANEL HAS SEVERAL FASTENER HOLE LOCATIONS ELONGATED / REMOVED AND REPLACED PNL 193B REF AMM 53-40-70; 53-40-71 SRM 53-40-02

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 55,950 hrs · 32,968 cycles

FWD SERVICE DOOR ESCAPE SLIDE BOTTLE PRESS IN THE RED. REMOVE & REPLACE FWD SERVICE DOOR SLIDE, IAW MT 725-61-06. OK FOR SERVICE RAR 77721.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 55,348 hrs · 32,582 cycles

FA REPORTS FWD SERVICE DOOR GERT BAR DIFFICULT TO ENGAGE AND REMOVE. ADJUSTED GIRT BAR. OPS CHECK GOOD. REF AMM 25-66-01

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,251 hrs · 32,519 cycles

LEFT OVERWING OUTER EXIT LIGHT WAS OUT. REMOVED AND REPLACED THE BULB AND PERFORMED AN OPS CHECK IAW AMM 33-51-04-960-801. CHECKED GOOD.

Part: FLOORBEAM — DAMAGED (BS 540 LBL45-65) · airframe 55,251 hrs · 32,519 cycles

PANEL BREAK BS 540 LBL 45-65 WL 208 TOP SURFACE IS DAMAGED / LOCATED AND DRILLED NEW BREAK PANEL AT BS540 LBL45-65 WL208 I.A.W. DWG 143A5240 AND SRM 51-40-05-0G-0 FIGURE 2 OK TO INSTALL 57800C 28JUN20 INSP 267 6-28-20 INSTALLED NEW BREAK PANEL I.A.W. DWG 143A5240 AND SRM 51-40-02-0G-0 4.7.

Part: NUT PLATE — CORRODED (AFT CARGO) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ON AFT CARGO BAY NUT PLATE STRAP BS787-794; RBL20; WL155. / REMOVED & REPLACED ACB NUT PLATE STRAP BS 787-794; RBL20; WL155 IAW SRM 51-40-02; SRM 51-40-05; & DWG #146A0081

Part: NUT PLATE — CORRODED (AFT CARGO) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ON AFT CARGO BAY NUT PLATE STRAP BS840-847; RBL20; WL156. / REMOVED & REPLACED ACB NUT PLATE STRAP BS 840-847; RBL 20; WL 156 IAW SRM 51-40-02; SRM 51-40-05; DWG #146A8340.

Part: NUT PLATE — CORRODED (AFT CARGO) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ON AFT CARGO BAY NUT PLATE STRAP BS794-801; RBL20; WL155. / REMOVED & REPLACED ACB NUTPLATE STRAP BS 794-801; RBL 20; WL 155 IAW SRM 51-40-02; SRM 51-40-05; & DWG #146A8340.

Part: RUB STRIP — CRACKED (HORIZONTAL STAB) · airframe 55,251 hrs · 32,519 cycles

LT HORIZ STAB UPPER SLIDE SEAL RUB GUIDE IS CRACKED / REMOVED CRACKED RUB GUIDE FROM LT HORIZ STAB UPPER SLIDE SEAL IAW SOPM 20-50-01 56306U 18JUN20 LEAD 41 18JUN20 REPLACED THE LT HORZ STAB UPPER SLIDE SEAL RUB GUIDE IAW MM 53-31-31-400-802 STEPS 3E(24-25).

Part: MOUNT — CORRODED (BS 990-998) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** CORROSION ON DRAIN MAST MOUNTING STRUCTURE IN AREA AFT OF AFT CARGO AT BS 998- BS 990 WL 187 / REMOVED AND REPLACED DRAIN MAST MOUTING STRUCTURE IN AREA CARGO B.S. 986-1006 STR 24L-25L WL187 PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 147A7443 AND AMM 38-31-01-400-802 RESISTANCE CHECK AND DRAIN MAST INSTALLATION TEST GOOD

Part: PRESSURE WEB — CORRODED (BS 1018) · airframe 55,251 hrs · 32,519 cycles

CORROSION FOUND ON THE PRESSURE WEB INNER SURFACE AT BS 1018, LBL 2, WL 186. REPAIRED IAW EA 20-153-00975, REV IR, AND ER 20-02796, REV IR.

Part: STRAP — CRACKED (BS 805) · airframe 55,251 hrs · 32,519 cycles

AFT CARGO BAY SUB THRESHOLD UPPER STRAP CRACKED AT BS805; RBL21; WL156. / REMOVED DAMAGED STRAP IAW SRM CH 51-40-02. 87696U 18JUN20 INSTALLED NEW ACB SUB THRESHOLD UPPER STRAP BS 767+7-847+14; RBL21; WL156 IAW SRM 51-40-02; SRM 51-40-05; DWG #146A0081. DWG #146A8120; DWG #146A8340

Part: STRINGER CLIP — CORRODED (BS 947.5) · airframe 55,251 hrs · 32,519 cycles

STRINGER CLIP AT BS 947.5, STRINGER 19R HAD CORROSION. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 147A0020.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ACB BS 947 SIDEWALL TO BULKHEAD SUPPORT RBL 22 WL 156 HAS CORROSION / REMOVED AND REPLACED ACB B.S. 947 SIDEWALL TO BULKHEAD SUPPORT RBL 22 -RBL 52 WL 156 PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 149A8110 AND DWG 149A8117

Part: SUPPORT — CORRODED (BS 727-767) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ACB SIDEWALL SUPPORT BS 727-767 RBL 22 WL 156 HAS CORROSION / REMOVED AND INSTALLED ACB SIDEWALL SUPPORT PO# 789433/1 AT BS727-767 RBL22 WL156 IAW SRM 51-40-02-0G-0 AND DWG 146A7500

Part: SPLICE STRAP — CORRODED (AFT CARGO FLOOR) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ACB FLOOR STRAP BS 887 RBL 15 WL 156 HAS CORROSION / CORROSSION FOUND OUT OF LIMITS DUE TO NO LIMITS GIVEN IN SRM. REMOVED LOCATED DRILLED & INSTALLED NEW ACB FLOOR STRAP PER SRM 51-40-02-0G-0; SRM 51-40-08; DWG 146A7500; DWG 149A8104

Part: WEB — CORRODED (BS 450-480) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** FORWARD CARGO BAY SUB THRESHOLD WEB BS 450-480 RBL 25 WL 156 / REMOVED FORWARD CARGO BAY SUBTHRESHOLD WEB BS450-480 RBL 25 LOCATED; DRILLED; COUNTERSUNK. INSTALLED NUTPLATES; INSTALLED FORWARD CARGO BAY SUBTHRESHOLD WEB BS 450-480 RBL 25 IAW SRM 51-40-02; SRM 51-40-08; SRM 51-40-05; DWG #143A8330 7191U 22JUN20

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ACB BULKHEAD SUPPORT BS 947 LBL 11-RBL 22 WL 156 HAS CORROSION / REMOVED AND REPLACED ACB BULKHEAD SUPPORT B.S. 947 LBL 11 - RBL 22 WL 156 PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 149A8117 AND DWG 149A8110

Part: SHIELD — CORRODED (AFT CARGO) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ACB SHIELD BS 847-867 RBL 22 WL 156 HAS CORROSION / REMOVED AND REPLACED DAMAGED SHIELD DUE TO NO LIMITS PER SRM IAW SRM CH 51-40-02 AND DRAWING #146A0081.

Part: SUPPORT — CRACKED (BS 907) · airframe 55,251 hrs · 32,519 cycles

R/H SIDEWALL SUPPORT IS CRACKED BS 907 RBL 21 WL 156 / REMOVED DAMAGED SUPPORT AT RBL 21 BS 887-947.5 IAW SRM CH 51-40-02. LOCATED AND DRILLED REPLACEMENT SUPPORT IAW SRM CH 51-40-05 AND DRAWING #147A7500 SHT. 19. 87696C 18JUN20. INSP 52 18JUN20 OK TO INSTALL. 87696C 29JUN20 INSP 52 29JUN20 INSTALLED SUPPORT AT BS 887-947.5 RBL 21 IAW SRM CH 51-40-02 AND DRAWING #147A7500

Part: SUPPORT — CORRODED (BS 727-787) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ACB SIDEWALL SUPPORT BS 727-787 LBL 22 WL 156 HAS CORROSION / REMOVED AND INSTALLED NEW ACB SIDEWALL SUPPORT P.O #795658 AT BS 727-787 LBL 22 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 146A7500

Part: FRAME — CORRODED (BS 947) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ACB BS 947 FRAME LBL 10 WL 156 HAS CORROSION / REMOVED CORROSION IN AN AREA OF 2.3X7.4. REMOVED .011'. FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1 FIG 102 DETAIL C. REMOVED FASTENERS PER SRM 51-40-02-0G-0. ACB BS 947 FRAME STR 23L TO 23R WILL BE REPLACED ON CUSTOMER CARD #U180355. ACCESSED & RESTORED STRUCTURE PER DWG 147A7500; DWG 149A8104; DWG 149A8103

Part: INTERCOSTAL — CRACKED (BS 927-947) · airframe 55,251 hrs · 32,519 cycles

INTERCOSTAL IS CRACKED BS 927 - 947, RBL 22, WL 156. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-40-02, LOCATED AND DRILLED A NEW INTERCOSTAL IAW SRM 51-40-05, AND DRAWING 147A7500, SHEET 19. INSTALLED THE NEW INTERCOSTAL IAW SRM 51-40-02, AND DRAWING 147A7500.

Part: WEB — CORRODED (BS 792-847) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ACB SUBTHRESHOLD WEB 792-847 RBL 23 WL 156 HAS CORROSION / REMOVED WEB LOCATED; DRILLED; COUNTERSUNK AND INSTALLED ACB WEB IAW SRM 51-40-02; SRM 51-40-05; SRM 51-40-08; DWG# 146A8340 7191U 25JUN20

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ACB SHIELD SUPPORT ANGLE HAS CORROSION BS 767-787 RBL 22 WL 156 / REMOVED ACB SHIELD SUPPORT ANGLE; LOCATED; DRILLED; INSTALLED NEW SUPPORT ANGLE IN ACB BS767-267 RBL22 IAW SRM 51-40-02; SRM 51-40-05 DWG# 146A0081 7191U 23JUN20 DWG#146A8123

Part: SHIELD — CORRODED (BS 767-792) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** ACB SHIELD HAS CORROSSION BS 767-792 RBL 22 WL 156 HAS CORROSION / REMOVED ACB SHIELD BS767-792 RBL 22 RECEIVED NEW SHIELD LOCATED; DRILLED INSTALLED NEW SHIELD IN ACB BS 767-792 RBL 22 IAW SRM 51-40-02; SRM 51-40-05 DWG #146A0081 7191U 23JUN20

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,251 hrs · 32,519 cycles

WASTE TANK ENCLOSURE ANGLE CRACKED BS 867 LBL 10 WL 156 / REPLACED WASTE TANK ENCLOSURE ANGLE AT B.S.867; LBL10; WL156 PER SRM 51-40-02; 51-40-05 AND DWG. 149A8102.

Part: CARGO TRACK — CORRODED (BS 827) · airframe 55,251 hrs · 32,519 cycles

AFT CARGO BAY, RT CARGO TRACK AT BS 827+18, RBL 14, WL 156 WAS CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW DRAWINGS 146A7500, 146A0061, AND EA 20-153-00963, REV IR.

Part: GUSSET — CRACKED (AFT CARGO) · airframe 55,251 hrs · 32,519 cycles

AFT CARGO BAY FRAME TO SHIELD GUSSET CRACKED BS767; RBL23; WL156. / REMOVED CRACKED FRAME TO SHIELD GUSSET AT BS767; RBL23; WL156 PER SRM 51-40-02-0G-0. 1035C 17JUN20 RECEIVED NEW GUSSET LOCATED; DRILLED NEW GUSSET IAW SRM 51-40-05 BK TO INSTALL GUSSET 7191U 23JUN20 1035C 23JUN20 INSP 15 23JUN20 INSTALLED GUSSET IN ACB BS767 RBL23 IAW SRM 51-40-02 7191U 23JUN20 DWG #146A0081

Part: FLOOR SUPPORT — CORRODED (BS 747-767 RBL22) · airframe 55,251 hrs · 32,519 cycles

CORROSION ACB INTERCOSTAL 747-767 RBL 22 WL 156 HAS CORROSION / INTERCOSTAL IS PART OF FLOOR TO SIDEWALL SUPPORT ASSY THAT IS BEING REPLACED ON SWA CARD #U180325

Part: ANGLE — CORRODED (FUSE) · airframe 55,251 hrs · 32,519 cycles

***CORROSION*** FORWARD CARGO BAY AT BS 500D LOWER BULKHEAD SUPPORT ANGLE RBL20 TO LBL20 WL 156 / REMOVED AND REPLACED LWR BULKHEAD SUPPORT ANGLE AT FCB BS 500D WL 156 BETWEEN RBL20 TO LBL20 IAW SRM 51-40-02; DWG #143A7902 AND DWG #143A9481

Part: STRINGER CLIP — CORRODED (BS 887) · airframe 55,251 hrs · 32,519 cycles

CORROSION FOUND ON THE STRINGER CLIP BS 887, STRINGER 23L, WL 156. EVALUATED THE CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, DWG 147A0060, AND DWG 147A3287.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 55,251 hrs · 32,519 cycles

FLOOR SUPPORT CRACKED BS328-344 LBL45 WL208 / REPLACED CRACKED FLOOR SUPPORT AT BS 328 - 344 LBL 45 WL 208 PER SRM 51-40-02-0G-0 AND DWG # 141A5400. 57449U 17JUN20

Part: ANGLE — CRACKED (BS 695) · airframe 55,251 hrs · 32,519 cycles

CRACKED VERTICAL ANGLE, BS 695, BL 0, WL 207, RT SIDE OF. BEAM. REMOVED AND REPLACED THE VERTICAL ANGLE IAW SRM 51-40-02-0G-0, AND DWG 273A9110.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 55,251 hrs · 32,519 cycles

FLOOR SUPPORT CRACKED BS312-328 LBL45 WL208 / REPLACED CRACKED FLOOR SUPPORT AT BS 312 - 328 LBL 45 WL 208 PER SRM 51-40-02-0G-0 AND DWG # 141A5400. 57449U 17JUN20

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 55,251 hrs · 32,519 cycles

LT HORIZ STAB UPPER FWD SLIDE SEAL IS CRACKED. / REMOVED & REPLACED WITH NEW LT HORIZ STAB UPPER FWD SLIDE SEAL IAW AMM 53-31-31-000-802 & AMM 53-31-31-400-802 56304U 18JUN20

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,251 hrs · 32,519 cycles

RIGHT HORIZONTAL STAB RIB AT HSS 120.30, THIRD VERTICAL STIFFENER WAS CRACKED. REPAIRED THE STIFFENER IAW SRM 55-10-09-2R5, SRM 51-40-02-0G-0, AMM 51-31-08-390-805, DRAWINGS 002A0001, 182A1500, 182A2401, AND 182A3001.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,251 hrs · 32,519 cycles

RIGHT HORIZONGAL STAB RIB AT HSS 92.70, THIRD VERTICAL STIFFENER WAS CRACKED. REPAIRED STIFFENER IAW SRM 55-10-09-2R4.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,251 hrs · 32,519 cycles

LEFT HORIZONTAL STAB RIB AT HSS 120.30, SECOND VERTICAL STIFFENER WAS CRACKED. REPAIRED THE STIFFENER IAW SRM 55-10-09-2R4, SRM 51-40-02-OG-1, DWGS 182A2401, 182A3001, AND 182A1500.

Part: STIFFENER — CRACKED (R/H HORIZ. STAB.) · airframe 55,251 hrs · 32,519 cycles

RIGHT HORIZONTAL STAB RIB AT HSS 92.70, SECOND VERTICAL STIFFENER WAS CRACKED. REPAIRED THE STIFFENER IAW SRM 55-10-09-2R4, SRM 51-40-02-OG-0, DRAWINGS 182A1500, 182A3001, AND 002A0001.

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 55,251 hrs · 32,519 cycles

BS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE WAS CRACKED AT RBL 10, WL 164. REMOVED AND REPAIRED THE ATTACH ANGLE IAW SRM 57-10-10-2R-5, PARA 4, STEPS A-O.

Part: SKIN — CORRODED (BS 907-1006) · airframe 55,251 hrs · 32,519 cycles

CORROSION ON EXTERNAL FUSELAGE SKIN AT BS 907 - 1006, WL 306, LBL 10 - RBL 10. REPAIRED THE SKIN IAW ER 20-02767, REV IR, AND EA 20-153-00965, REV IR.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,251 hrs · 32,519 cycles

RT HORIZONTAL STAB RIB AT HSS 92.70, FORTH VERTICAL STIFFENER WAS CRACKED. REPAIRED THE STIFFENER IAW SRM 55-10-09-2R-4.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,251 hrs · 32,519 cycles

LEFT HORIZONTAL STAB RIB AT HSS 120.30, FORTH VERTICAL STIFFENER WAS CRACKED. REPAIRED THE STIFFENER IAW SRM 55-10-09-2R-4.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 55,251 hrs · 32,519 cycles

LT HORIZONTAL STAB REMOVABLE L/E HAD A CRACKED RIB AT L/E HSS 78.29. REMOVED AND REPLACED THE RIB IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 & DWG 186A1001, SHT 10.

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 55,251 hrs · 32,519 cycles

BS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE WAS CRACKED AT LBL 10, WL 164. REMOVED AND REPAIRED THE ATTACH ANGLE IAW SRM 57-10-10-2R-5, PARA 4, STEPS A-O.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,251 hrs · 32,519 cycles

LEFT HORIZONTAL STAB RIB AT HSS 120.30, THIRD VERT STIFFENER WAS CRACKED. REPAIRED STIFFENER IAW SRM 55-10-09-2R-4.

Part: PRESSURE DECK — CRACKED (BS 665) · airframe 55,251 hrs · 32,519 cycles

FOUND HORIZONTAL PRESSURE DECK WEB TO BE CRACKED AT BS 665 LBL 31. REMOVED AND REPAIRED IAW SRM 53-40-51-2R-2, REPAIR 2, FIG 203.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,150 hrs · 32,457 cycles

EXTERIOR EMERGANCY LIGHT AFT OF AFT SERVICE DOOR INOP / RELAMPED EXTERIOR EMERGANCY LIGHT AFT OF AFT SERVICE DOOR IAW AMM 33-51-02

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,930 hrs · 31,061 cycles

R/H OVERWING DOOR MOST FORWARD BULB INOP JUST BELOW EMERGENCY EXIT SIGN. R&R BULB IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 52,879 hrs · 31,029 cycles

PHOTOLUMINESCENT LIGHT STRIP DAMAGED AT 1ST SECTION ON LOWER R/H SIDE. / R&R STRIP PER AMM.

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 51,382 hrs · 30,095 cycles

FLIGHT DECK FLOOR PANEL BEHIND CENTER PEDESTAL (APPROXIMATELY 10") HAD LARGE DENT/ OIL CANNING WITH NUMEROUS SMALL DENTS. / REPAIRED FLOOR PANEL IAW EA.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 51,245 hrs · 30,002 cycles

WING TO BODY PANEL 193B HAS NOMEROUS FASTNER HOLES WORN / ELONGATED. PANEL HOLES ARE FOR FASTENERS 013-20_AND 33-38 REF. TABLE 1 OF PAGES 14 AND 15. / REMOVED & REPLACED PANEL 193B REF SRM 51-40-02.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 50,578 hrs · 29,580 cycles

DIVERSION, LEADING EDGE FLAPS TRANSIT ILLUMINATED ON TWO SEPARATE OCCASIONS AT FL360. LEADING EDGE DEVICE NR 1 ALSO ILLUMINATED AUTO THROTTLES ALSO CAME BACK AS PLANE ATTEMPTED TO SLOW TO M.70M. R&R CONTROL PANEL PER SWPM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,768 hrs · 29,030 cycles

FUSELAGE FORWARD CARGO PIT FLOORBEAM LT INTERCOSTAL CRACKED AT BS 540. R&R INTERCOSTAL PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 49,768 hrs · 29,030 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 49,768 hrs · 29,030 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 49,768 hrs · 29,030 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,768 hrs · 29,030 cycles

FUSELAGE FORWARD CARGO PIT FLOOR BEAM RT INTERCOSTAL CRACKED AT BS 540. R&R INTERCOSTAL PER SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 49,554 hrs · 28,899 cycles

RT OVERWING EMERGENCY LIGHT SIGN INOP. R&R LIGHT ASSEMBLY PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,554 hrs · 28,899 cycles

RT EMERGENCY LIGHT INOP AT ROW 6. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,554 hrs · 28,899 cycles

RT EMERGENCY LIGHT INOP AT ROW 2. R&R BATTERY PACK PER AMM.

Part: BRACKET — BROKEN (LEFT WING) · airframe 49,554 hrs · 28,899 cycles

L/H WING T/E PANEL 551FB PANEL L/E SUPPORT BRACKET BROKEN / REMOVED AND REPLACED BRACKET PER SRM 50-40-02

Part: FAIRING — CRACKED (RT WING) · airframe 49,554 hrs · 28,899 cycles

#6 SUPPORT FAIRING HAS A CRACK ON INSIDE OF FAIRING IN AREA WHERE ADJUST LINK AND ATTACH BEAM CONTACT. / REPAIRED IAW EA 1-A57-6168 AND SRM 51-70-05-2R-11.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 4,954 hrs · 28,899 cycles

LT MAIN LANDING GEAR WHEEL WELL L-ANGLE CRACKED AT STA 663, LBL25. R&R ANGLE PER SRM.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 4,954 hrs · 28,899 cycles

LT MAIN LANDING GEAR WHEEL WELL ANGLE CRACKED AT STA 663, LBL25. R&R ANGLE PER SRM.

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 49,554 hrs · 28,899 cycles

FWD CARGO APROX. STA.492-500A R/H SIDE TRANSITION ANGLE HAS CORROSION OUT OF LIMITS. / REMOVED AND REPLACED PER SRM 51-40-02

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 49,554 hrs · 28,899 cycles

FWD CARGO STA. 480 TO 500D L/H TRANSITION ANGLE HAS LIGHT CORROSION AROUND NUTPLATE HOLES. / REPAIRED L/H TRANSITION PER SRM 53-00-53-2R-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,554 hrs · 28,899 cycles

NR 4 SEAT TRACK CORRODED ON UPPER CROWN BETWEEN BS 540 TO BS 727B. R&R CROWN PER SRM.

Part: SCUFF PLATE — BROKEN (AFT CARGO BAY) · airframe 49,554 hrs · 28,899 cycles

AFT CARGO DOOR SURROUND FWD CORNER SCUFF PLATE OB FLANGE HAS PIECE BROKEN OFF (MARKED) / PLATE REPAIRED ON REPAIR ORDER # 7530063-B5R. PLATE TO BE INSTALLED ON ROUTINE TASK CARD # 753-721-00-01.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 49,554 hrs · 28,899 cycles

AFT CARGO DOOR SURROUND AFT CORNER SCUFF PLATE CRACKED AT INBOARD EDGE. REPAIRED PLATE PER TC.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 49,554 hrs · 28,899 cycles

LT MAIN WHEEL WELL VERTICAL PRESSURE BULKHEAD CRACKED AT BS 663, BETWEEN LBL 32.5 TO LBL 33. REPAIRED BULKHEAD PER SRM.

Part: PLATE — CRACKED (RT WING) · airframe 49,554 hrs · 28,899 cycles

RT WING TRAILING EDGE WAFFLE PLATE CRACKED OUTBOARD OF NR 6 FLAP TRACK AT RSS 264. R&R WAFFLE PLATE IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 49,554 hrs · 28,899 cycles

RT WING TRAILING EDGE WAFFLE PLATE CRACKED INBOARD OF NR 6 FLAP TRACK. R&R WAFFLE PLATE IAW SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 49,554 hrs · 28,899 cycles

AFT CARGO DOOR AFT THRESHOLD CRACKED / PLATE REPAIRED ON REPAIR ORDER # 7530337-A2R. PLATE TO BE INSTALLED ON ROUTINE TASK CARD # 753-721-00-01.

Part: PLATE — CRACKED (LT WING) · airframe 49,554 hrs · 28,899 cycles

LT WING TRAILING EDGE WAFFLE PLATE CRACKED AND MISSING FASTENER INBOARD OF NR 1 PYLON. R&R WAFFLE PLATE IAW SRM.

Part: RETAINER — CORRODED (RT WING) · airframe 49,554 hrs · 28,899 cycles

RT WING UPPER SHELF PANEL AT DEFLECTION RIB FWD SEAL RETAINER CRACKED / REMOVED AND REPLACED SEAL RETAINER PER SRM 51-10-02 AND SRM 51-40-02.

Part: RETAINER — CRACKED (LT WING) · airframe 49,554 hrs · 28,899 cycles

AT LEFT ORSS 271 BULB SEAL RETAINER BRACKET IS CRACKED. / REMOVED AND REPLACED SEAL RETAINER BRACKET PER SRM 51-40-02.

Part: RETAINER — CRACKED (RT WING) · airframe 49,554 hrs · 28,899 cycles

RT WING UPPER SHELF PANEL AT DEFLECTION RIB AFT SEAL RETAINER CRACKED / REMOVED AND REPLACED SEAL RETAINER PER SRM 51-10-02 AND SOPM 20-50-01.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 49,554 hrs · 28,899 cycles

RUDDER BALANCE WEIGHT IS CORRODED / REPLACED RUDDER COUNTER BALANCE WEIGHT PER CMM 55-40-09. SEE OTHER SIGN OFFS FOR INDIVIDUAL TASKS.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 49,053 hrs · 28,558 cycles

AIR TURNBACK/DECLARED EMERGENCY, CLIMBING THROUGH FL200, OUTER PANE L1 COCKPIT WINDSHIELD CRACKED. R&R L1 WINDOW IAW MM.

Part: FLOOR PANEL — CRACKED (FWD CARGO COMPT) · airframe 48,897 hrs · 28,459 cycles

FWD CARGO FLOOR LINER BIN B HAS CRACK MIDDLE OF FLOOR. / REFERENCE CLOSING LP0071595 R&R'D FWD CARGO FLOOR PANEL IAW AMM 25-52-10 & EA 1-725-4163 OK FOR SERVICE CLEARING #64639

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 48,614 hrs · 28,292 cycles

RIGHT MID CABIN LOWER LIGHTED EMERGENCY EXIT SIGN BROKEN. R & R THE SIGN IAW AMM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 48,059 hrs · 27,958 cycles

RT PHOTO LUMINESCENT STRIP LOOSE AT ROW 1. R&R STRIP IAW SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,084 hrs · 26,717 cycles

EXTERNAL POWER ACCESS DOOR CUTOUT CRACKED AT THE CENTER LATCH LANDING. REPAIRED CUTOUT PER SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 43,936 hrs · 25,470 cycles

EMERGENCY EXIT LIGHT BATTERY M1673 FAILED CAPACITY TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 43,936 hrs · 25,470 cycles

EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 43,936 hrs · 25,470 cycles

EMERGENCY EXIT LIGHT BATTERY M1670 FAILED CAPACITY TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 43,059 hrs · 24,941 cycles

RIGHT EMERGENCY EXIT LIGHT FAILED BATTERY CAPACITY CHECK BETWEEN ROW 8 TO ROW 13. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 43,059 hrs · 24,941 cycles

RIGHT OVERWING EMERGENCY LIGHT FAILED A BATTERY CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 43,059 hrs · 24,941 cycles

MID CEILING EMERGENCY EXIT LIGHT BROKEN AT BS 627. R & R THE LIGHT IAW AMM.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 43,059 hrs · 24,941 cycles

FORWARD CARGO BAY STRINGER CLIP CRACKED AT BS 500D, STRINGER 19L. R & R THE STRINGER CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 43,059 hrs · 24,941 cycles

FORWARD CARGO BAY STRINGER CLIP CRACKED AT BS 500D, STRINGER 19R. R & R THE STRINGER CLIP IAW SRM & DWG.

Part: WEB — CORRODED (BS 986) · airframe 43,059 hrs · 24,941 cycles

WEB CORRODED AT BS 986, RBL 50. R & R THE WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (BS 787) · airframe 43,059 hrs · 24,941 cycles

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

Part: FRAME — CRACKED (BS 727D) · airframe 43,059 hrs · 24,941 cycles

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

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 43,059 hrs · 24,941 cycles

R2 DOOR THRESHOLD LOWER CHORD CORRODED. R & R CHORD IAW DWG.

Part: FRAME — CRACKED (BS 480) · airframe 43,059 hrs · 24,941 cycles

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

Part: FLOORBEAM — CORRODED (BS 986) · airframe 43,059 hrs · 24,941 cycles

FLOORBEAM CORRODED AT BS 986, RBL 54. REPAIRED THE FLOORBEAM IAW SRM.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 43,059 hrs · 24,941 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL BULKHEAD SUPPORT ANGLE CRACKED AT RBL 40. REPAIRED THE BULKHEAD ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,059 hrs · 24,941 cycles

FORWARD WET AREA FLOOR SUPPORT LATERAL INTERCOSTAL CORRODED AT BS 270, LBL 6. REPAIRED LATERAL INTERCOSTAL IAW EA.

Part: FRAME — CRACKED (BS 727B) · airframe 43,059 hrs · 24,941 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,059 hrs · 24,941 cycles

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

Part: FRAME — CRACKED (BS 827) · airframe 43,059 hrs · 24,941 cycles

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

Part: BRACKET — CORRODED (L1 GIRT BAR) · airframe 43,059 hrs · 24,941 cycles

L1 DOOR THRESHOLD GIRT BAR BRACKETS ARE CORRODED. R & R THE BRACKET IAW SRM.

Part: FRAME — CRACKED (BS 360) · airframe 43,059 hrs · 24,941 cycles

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

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 43,059 hrs · 24,941 cycles

R1 DOOR CUTOUT LOWER INNER THRESHOLD CHORD CORRODED. R & R CHORD IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 43,059 hrs · 24,941 cycles

LEFT WING FIXED T/E BEHIND PYLON FAIRING ON T/E ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (BS 500C) · airframe 43,059 hrs · 24,941 cycles

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

Part: FRAME — CRACKED (BS 747) · airframe 43,059 hrs · 24,941 cycles

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

Part: BULKHEAD — CRACKED (BS 663) · airframe 43,059 hrs · 24,941 cycles

LEFT WHEEL WELL FORWARD BULKHEAD CRACKED AT BS 663.75, LBL 39. REPAIRED THE BULKHEAD IAW EA 1-A53-3376.

Part: FRAME — CRACKED (BS 727D) · airframe 43,059 hrs · 24,941 cycles

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

Part: BEAM — CORRODED (FUSELAGE) · airframe 43,059 hrs · 24,941 cycles

AFT CARGO FLOOR STRUCTURE BEAM CORRODED AT BS 772.5, RBL 8. REPAIRED BEAM IAW EA.

Part: CARGO TRACK — CORRODED (BS 787-847) · airframe 43,059 hrs · 24,941 cycles

AFT CARGO TRACK CORRODED BETWEEN BS 787 - 847, RBL 12. R & R CARGO TRACK IAW SRM.

Part: WEB — CORRODED · airframe 43,059 hrs · 24,941 cycles

AFT CARGO DOOR CUTOUT LOWER WEB CORRODED IN SEVERAL PLACES. R & R THE WEB IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,059 hrs · 24,941 cycles

LOWER BULKHEAD CHORD CRACKED AT BS 540, BETWEEN STR 22R TO STR 23R. REPAIRED CHORD IAW EA.

Part: COVER — DETACHED (EMERGENCY LIGHTS) · airframe 43,049 hrs · 24,935 cycles

AFT OVERWING CEILING EMERGENCY EXIT LIGHT LENS COVER FELL OFF. INSTALLED THE COVER IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 37,709 hrs · 21,909 cycles

R2 DOOR EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,382 hrs · 21,730 cycles

M1675 EMER BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,382 hrs · 21,730 cycles

M1672 EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,382 hrs · 21,730 cycles

M1669 EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM & DWG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,369 hrs · 21,118 cycles

L1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LIGHT IAW AMM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 36,211 hrs · 21,026 cycles

FLIGHT DECK NR 1 WINDOW FRAME INNER CORNER LT UPPER SIDE CRACKED. REPAIRED FRAME IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,211 hrs · 21,026 cycles

CENTER WING BOX FRONT SPAR SHEAR FITTING CRACKED AT BS 540 LBL 15.04. REPAIRED FITTING IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,211 hrs · 21,026 cycles

CENTER WING BOX FRONT SPAR SHEAR FITTING CRACKED AT BS 540 LBL 32.40. REPAIRED FITTING IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 36,211 hrs · 21,026 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME CRACKED NEAR UPPER CORNER. REPAIRED IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 36,211 hrs · 21,026 cycles

RIGHT FLIGHT DECK E - F POST WINDOW FRAME AT APPROX 9:00 POSITION TO .297 INCHES CRACKED. REPAIRED FRAME IAW SI.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 36,211 hrs · 21,026 cycles

LEFT FLIGHT DECK WINDOW FRAME APPROX AT 4:00 POSITION TO .297 INCHES CRACKED. REPAIRED FRAME IAW SI.

Part: DOOR — CRACKED (LT MLG) · airframe 36,113 hrs · 20,972 cycles

LEFT MLG INNER DOOR HINGE ATTACH POINTS CRACKED. R & R DOOR IAW MM.

Part: DOOR — CRACKED (RT MLG) · airframe 36,113 hrs · 20,972 cycles

RIGHT MLG INNER DOOR HINGE ATTACH POINTS CRACKED. R & R DOOR IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 36,083 hrs · 20,953 cycles

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

Part: SIGN — LOOSE (EXIT SIGN) · airframe 35,355 hrs · 20,513 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT SIGN LENS LOOSE. SECURED SIGN IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,095 hrs · 19,768 cycles

FWD ENTRY THRESHOLD EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: MODULE — FAULTY (CABIN) · airframe 33,240 hrs · 19,270 cycles

EMERGENCY LIGHTS STAY ON WITH COCKPIT EMERGENCY EXIT LIGHT SWITCH OFF. FOUND AFT FLIGHT ATTENDANT STATION EMERGENCY LIGHT PUSH BUTTON SWITCH S2 FAULTY. R & R AFT LIGHTING ATTEND PANEL MODULE IAW SIP & MM.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 31,297 hrs · 18,145 cycles

RIGHT OVERWING EMERGENCY EXIT HANDLE COVER FELL OFF. RE-INSTALLED COVER PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,785 hrs · 17,840 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST & LIGHT BULB, OP CHECK GOOD PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 29,637 hrs · 17,176 cycles

LEFT EEPLS COVERS CRACKED BETWEEN ROW 4 TO ROW 15. REMOVED & REPLACED COVERS PER AMM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 29,637 hrs · 17,176 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED HOOKS PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,245 hrs · 16,926 cycles

FORWARD LAV MOUNTED EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 29,245 hrs · 16,926 cycles

FORWARD LAVATORY AFT WALL EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 29,245 hrs · 16,926 cycles

AFT EEPLS BROKEN AT BS 820. REMOVED AND REPLACED EEPLS IAW AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,245 hrs · 16,926 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,245 hrs · 16,926 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.50. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,245 hrs · 16,926 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 101.90. REPAIRED SKIN PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 29,245 hrs · 16,926 cycles

FORWARD GALLEY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 28,667 hrs · 16,586 cycles

EEPLS COVER LOOSE. REMOVED AND REPLACED COVER PER M/M.

Part: RETAINING CLIP — CRACKED (GIRT BAR) · airframe 28,591 hrs · 16,540 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR COLLAR RETAINING CLIP CRACKED. REMOVED AND REPLACED CLIP PER AMM.

Part: RETAINING CLIP — CRACKED (GIRT BAR) · airframe 28,591 hrs · 16,540 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR COLLAR RETAINING CLIP CRACKED. REMOVED AND REPLACED CLIP PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 23,517 hrs · 13,626 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 22,142 hrs · 12,827 cycles

DURING SCHEDULED 6Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 142. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 20,761 hrs · 12,023 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW 1 TO ROW 10. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 20,761 hrs · 12,023 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW 16 TO ROW 22. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 19,671 hrs · 11,325 cycles

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

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 19,473 hrs · 11,199 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 17. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 19,473 hrs · 11,199 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 17. REMOVED AND REPLACED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 17,432 hrs · 9,998 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,416 hrs · 9,989 cycles

DURING SCHEDULED HC1 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT FWD OF AFT CARGO DOOR INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 17,416 hrs · 9,989 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 17,416 hrs · 9,989 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LENS — OUT OF POSITION (CABIN) · airframe 16,720 hrs · 9,555 cycles

R1 EMERGENCY EXIT DOOR LIGHT LENS FELL OFF. SECURED LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 15,430 hrs · 8,807 cycles

EEPLS LENS LOOSE AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 15,430 hrs · 8,807 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 15,418 hrs · 8,798 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,971 hrs · 8,539 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,928 hrs · 7,342 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHTS) · airframe 12,446 hrs · 7,076 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 12. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 12,416 hrs · 7,056 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 12,294 hrs · 6,969 cycles

EEPLS INOP AT ROW 13 DEF. FOUND LOOSE WIRE. SECURED WIRE PER WDM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 11,397 hrs · 6,431 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 8,198 hrs · 4,602 cycles

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

Part: FITTING — LOOSE (L1 DOOR) · airframe 7,716 hrs · 4,322 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FWD GIRT BAR FITTING PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,370 hrs · 4,130 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LIGHT COVER CRACKED AT ROW 11 ABC TO ROW 13 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,370 hrs · 4,130 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 7,370 hrs · 4,130 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 7,370 hrs · 4,130 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LIGHT COVER CRACKED AT ROW 4 ABC TO ROW 5 ABC. REMOVED AND REPLACED, EEPLS COVER IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 6,766 hrs · 3,784 cycles

FOUND EEPLS STRIP LOOSE AT ROW 1 ABC. SECURED EEPLS STRIP PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 6,683 hrs · 3,734 cycles

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

Part: TRACK — LOOSE (CABIN) · airframe 6,162 hrs · 3,416 cycles

EEPLS TRACK LOOSE AT ROW 1. SECURED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 6,141 hrs · 3,406 cycles

EEPLS TRACK LENS MISSING AT FWD END. INSTALLED LENS PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 6,055 hrs · 3,360 cycles

EEPLS COVER LOOSE AT FWD END. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 5,676 hrs · 3,144 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 2,897 hrs · 1,621 cycles

EMERGENCY EXIT LIGHT LENS MISSING NEXT TO R2 DOOR. INSTALLED LENS ASSY PER MX NOTE. LATER AT MCO REMOVED AND REPLACED LIGHT ASSY PER MM.