N948WN

Part: COFFEEMAKER — BURNED (ZONE 200) · airframe 49,347 hrs · 30,268 cycles

FLT ATT. REPORTED BURNING SMELL FROM FWD COFFEE POT WITH POWER ON AND WARMER OFF. REPLACED FWD COFFEE MAKER IAW AMM 25-30-01; OPS/LEAK CHECKS GOOD

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 49,078 hrs · 30,104 cycles

EMERGENCY EXIT SIGN CAPT SIDE INOP. R & R EMERGENCY EXIT SIGN LAMP IAW AMM 33-51-01.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 48,955 hrs · 30,027 cycles

EMERGENCY LIGHTS AT ROWS 3 AND 6 DEF INOPERATIVE. R & R THE BATTERY PACK AND POWER SUPPLY M01674 IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 48,697 hrs · 29,869 cycles

FWD MEGAPHONE INOPERATIVE. REMOVED AND REPLACED THE MEGAPHONE IAW AMM 25-64-00-SWA-804-NG-01.

Part: PANEL — CRACKED (ZONE 100) · airframe 46,827 hrs · 28,737 cycles

WING-TO-BODY LOWER AFT FAIRING PANEL 194GL CRACK DAMAGE FROM BOTTOM TO TOP LEFT AND TOP RIGHT<[01] REMOVED AND REPLACED AFT FAIRING 194GL PER AMM 53-51-21

Part: SWITCH — BROKEN (ZONE 200) · airframe 46,118 hrs · 28,289 cycles

AFT F/A LIGHTING PANEL EMERGENCY EXIT LIGHT SWITCH COVER SPRING BROKEN.<[01] R/R EMERGENCY LIGHT SWITCH AT AFT FA PANEL REF AMM 23-42-03

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 44,708 hrs · 27,405 cycles

LFT AFT EMERGENCY SLIDE LIGHT INOP<[01] REMOVED AND REPLACED LFT AFT EMERGENCY SLIDE LIGHT PER AMM 33-51-04

Part: FUSE — DEFECTIVE (EMERGENCY LIGHT) · airframe 44,502 hrs · 27,272 cycles

CUSTOMER WALK FOUND AFT GALLEY CEILING EMERGENCY EXIT SIGN INOP.<[01] PERFORMED T/S AS PER WDM REF 33-51-14 AND FOUND 1 BATTERY PACK POWER SUPPLY FUSE DEFECTIVE. REPLACED 1 BATTERY POWER PACK SUPPLY FUSE AS PER WDM REF 33-51-14 AND AMM REF 33-51-06-960-804. INSTALLATION TEST FOUND NORMAL.;[02] CORRECTION TO STEP 1:<BR>PERFORMED T/S AS PER WDM REF 33-51-14 AND FOUND CONNECTOR D40026P LOOSE. RE-CONNECTED CONNECTOR AND PERFORMED INSTALLATION TEST. TEST FOUND NORMAL.;[03] CORRECTION TO STEP 2:<BR>PERFORMED T/S AS PER WDM REF 33-51-14 AND FOUND CONNECTOR D40026P LOOSE. RE-CONNECTED CONNECTOR AND PERFORMED INSTALLATION TEST AS PER AMM REF 33-51-00-710-801. TEST FOUND NORMAL.;[04] VERIFIED STEP1 AND STEP2 ENTRY ERROR. AND STEP#3 RE-CONNECTED CONNECTOR AND PERFORMED INSTALLATION TEST NORMAL.

Part: CONNECTOR — DEFECTIVE (EMERGENCY LIGHTS) · airframe 44,502 hrs · 27,272 cycles

CUSTOMER WALK FOUND AFT GALLEY CEILING EMERGENCY EXIT SIGN INOP.<[01] PERFORMED T/S AS PER WDM REF 33-51-14 AND FOUND 1 BATTERY PACK POWER SUPPLY FUSE DEFECTIVE. REPLACED 1 BATTERY POWER PACK SUPPLY FUSE AS PER WDM REF 33-51-14 AND AMM REF 33-51-06-960-804. INSTALLATION TEST FOUND NORMAL.;[02] CORRECTION TO STEP 1:<BR>PERFORMED T/S AS PER WDM REF 33-51-14 AND FOUND CONNECTOR D40026P LOOSE. RE-CONNECTED CONNECTOR AND PERFORMED INSTALLATION TEST. TEST FOUND NORMAL.;[03] CORRECTION TO STEP 2:<BR>PERFORMED T/S AS PER WDM REF 33-51-14 AND FOUND CONNECTOR D40026P LOOSE. RE-CONNECTED CONNECTOR AND PERFORMED INSTALLATION TEST AS PER AMM REF 33-51-00-710-801. TEST FOUND NORMAL.;[04] VERIFIED STEP1 AND STEP2 ENTRY ERROR. AND STEP#3 RE-CONNECTED CONNECTOR AND PERFORMED INSTALLATION TEST NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,502 hrs · 27,272 cycles

MULTIPLE EMERGENCY EXIT LIGHTS THROUGHOUT A/C INSIDE CABIN AND EXTERIOR FOUND INOP<[01] REMOVED AND REPLACED PAX EMERGENCY LIGHT BATTERY PACKS AT POSITION M1675; M1670;M1669 & M1673 I/A/W BOEING AMM 31-51-06-960-805; OPS CHECK NORMAL

Part: SPLICE — DAMAGED (ZONE 200) · airframe 44,502 hrs · 27,272 cycles

REJECT- STEP 1; SUBSTEP 11 OF TTG8Q00S9CVY HOLES OBLONG AND TOOLING MARKS PRESENT ON ANGLE AND SPLICE<[01] FABRICATED NEW REPAIR ANGLE AND SPLICE; LOCATED AND DRILLED NEW REPAIR ANGLE AND SPLICE REF SRM 57-10-10-2R-05; SRM 51-40-05-0G-0<BR>REPAIR ANGLE MADE OF 2024 T3 .063 P.O.# 2007319<BR>REPAIR SPLICE MADE OF 2024 T3 .071 P.O.# 2059117;[02] VERIFIED FABRICATION OF NEW REPAIR ANGLE AND SPLICE

Part: ANGLE — DAMAGED (UNKNOWN) · airframe 44,502 hrs · 27,272 cycles

REJECT- STEP 1; SUBSTEP 11 OF TTG8Q00S9CVY HOLES OBLONG AND TOOLING MARKS PRESENT ON ANGLE AND SPLICE<[01] FABRICATED NEW REPAIR ANGLE AND SPLICE; LOCATED AND DRILLED NEW REPAIR ANGLE AND SPLICE REF SRM 57-10-10-2R-05; SRM 51-40-05-0G-0<BR>REPAIR ANGLE MADE OF 2024 T3 .063 P.O.# 2007319<BR>REPAIR SPLICE MADE OF 2024 T3 .071 P.O.# 2059117;[02] VERIFIED FABRICATION OF NEW REPAIR ANGLE AND SPLICE

Part: HANDLE — DAMAGED (PAX DOOR) · airframe 44,502 hrs · 27,272 cycles

FWD PASSENGER ENTRY DR (L-1) ASSIST HANDLE NUTPLATES DAMAGED<[01] REMOVED AND FREPLACED NUTPLATES AT FWD PASSENGER ENTREY DOOR (L-1) ASSIST HANDLE. REF SRM. 51-40-02-0G-0;[02] VERIFIED STEP 1

Part: SKIN — CRACKED (LT NR 6 SPOILER) · airframe 44,502 hrs · 27,272 cycles

CRACK FOUND AT L/H WING SPOILER #6 LOWER SURFACE SKIN; 14' FROM I/B EDGE AND 1.8' FROM AFT EDGE.<[01] REMOVED AND REPLACED #6 SPOILER. BOEING 737-700; AMM 27-62-12-401-NG;[02] VERIFIED REMOVAL AND REPLACEMENT OF #6 SPOILER.

Part: FLOOR SUPPORT — CRACKED (BS 312-328 LBL45) · airframe 44,502 hrs · 27,272 cycles

MAIN CABIN FLOOR SUPPORT BETWEEN STA 312 AND 328 LBL 45' HAS A CRACK AT UPPER SURFACE MKD (107-002)<[01] REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT BETWEEN STA 312 AND 328 LBL 45' PER REF SRM 51-40-02-0G AND DWG 141A5400;[02] VERIFIED REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT BETWEEN STA 312 AND 328 LBL 45'.

Part: FLOOR SUPPORT — MISSING (BS 540) · airframe 44,502 hrs · 27,272 cycles

MAIN CABIN FLOOR SUPPORT BREAK UPPER WEB MISSING AT STA 540 LBL 1' WL 208.1 MKD (107-001)<[01] NSTALLED NEW SUPPORT BREAK AT MAIN CABIN AT STA. 540;FROM LBLL1 TO LBL 24; PER REF SRM 51-40-02-0G-0 AND DRAWING # 143A5240;[02] CORRECTION STEP 1; INSTALLED NEW SUPPORT BREAK AT MAIN CABIN AT STA. 540;FROM LBLL1 TO LBL 24; PER REF SRM 51-40-02-0G-0 AND DRAWING # 143A5240;[03] VERIFIED REMOVED AND INSTALLED NEW SUPPORT BREAK AT MAIN CABIN AT STA. 540;FROM LBLL1 TO LBL 24.

Part: SUPPORT ANGLE — CRACKED (BS 663) · airframe 44,502 hrs · 27,272 cycles

CRACK FOUND AT FASTENER HOLE OF R/H VAPOR BARRIER UPPER SUPPORT ANGLE (ONLY) AT RBL 54.<[01] ACCOMPLISHED REPAIR AT RT. VAPOR BARRIER UPPER ANGLE PER REF SRM 51-40-02-0G-0 AND SRM57-10-10-2R-5;[02] VERIFIED STEP 1;[03] VERIFIED STEP 1

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 44,502 hrs · 27,272 cycles

FWD WET AREA PANEL 221BF HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES (INSERT)<[01] RECEIVED NEW FLOOR PANEL 221BF; IT WILL BE INSTALLED ON TTG8Q00S8MY0.;[02] VERIFIED STEP 1

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 44,502 hrs · 27,272 cycles

FWD WET AREA PANEL 221CF HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES (INSERT)<[01] RECEIVED NEW FLOOR PANEL 221CF; IT WILL BE INSTALLED ON TTG8Q00S9CW0.;[02] VERIFIED STEP 1

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 44,502 hrs · 27,272 cycles

FWD WET AREA PANEL 221AF HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES (INSERT)<[01] RECEIVED NEW FLOOR PANEL 221AF; IT WILL BE INSTALLED ON TT8Q00S8MY2.;[02] STEP 1: ENTER IN ERROR.<BR>RECEIVED NEW FLOOR PANEL 221AF; IT WILL BE INSTALLED ON TTG8Q00S8MY2.;[03] VERIFIED SUB-STEP 2

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 44,502 hrs · 27,272 cycles

HORIZONTAL STAB. L/H & L/E (PANEL 331B) HAS EVIDENCES CRACK AT STA 86.66; BOTTOM POSITION.<[01] REMOVED AND REPLACED DAMAGE RIB AT L/H HORIZONTAL L/E STA. 75.00 PANEL 331B PER REF SRM 51-40-02-0G-0 AND DRAWING # 186A1303;[02] VERIFIED REMOVED AND REPLACED DAMAGE RIB AT L/H HORIZONTAL L/E STA. 75.00 PANEL 331B.;[03] ALL STEPS COMPLETED.

Part: PRESSURE DECK — CRACKED (BS 663 LBL 33) · airframe 44,502 hrs · 27,272 cycles

CRACK FOUND AT HORIZONTAL PRESSURE DECK WEB STA 663 LBL 33. CRACK LENGTH:0.281'<[01] REPAIRED AREA AS REQUIRED PER SRM 51-40-02-0G-0;51-31-00-309-804

Part: FLOOR SUPPORT — CRACKED (BS 540 RBL 1) · airframe 44,502 hrs · 27,272 cycles

MAIN CABIN CENTER CABIN FLOOR SUPPORT BREAK CRACKED @ RBL 1 STA 540 WL 208.1 MKD DOT<[01] REMOVED AND INSTALLED FLOOR SUPPORT AT MAIN CABIN CENTER RBL STA 540 WL 208.1 PER REF SRM 51-40-02-0G;[02] CORRECTION: REMOVED AND INSTALLED FLOOR SUPPORT AT MAIN CABIN CENTER RBL STA 540 WL 208.1 PER REF SRM 51-40-02-0G DWG: 143A5240;[03] VERIFIED REPLACEMENT

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 44,502 hrs · 27,272 cycles

CRACK - RIGHT VAPOR BARRIER STA. 663.75 AND RBL 45 (LOCATED JUST ABOVE HYD SERVICE PUMP HANDLE.<[01] APPLIED REPAIR AT RIGHT VAPOR BARRIER STA. 663.75 AND RBL 45 ON BOTH SIDE PER B737SRM 51-70-04-2R-10 PARAGRAPH 4.F AND 737 SRM 51-70-04-2R-0 PARAGRAPH 4.N.2 MATERIAL USED RESIN EY 3804 PO#2059060 FIBERGLASS PO#2061599 AND TOOL USED TEMPERATURE CONTROL ID;ID 170006; DUE DATE 06-01-24;[02] VERIFIED STEP 1

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 44,091 hrs · 27,020 cycles

20C EMERGENCY LIGHT LENS LOOSE.<[01] RESECURED EMERGENCY AISLE LIGHT LENS AT SEAT 20C PER AMM 33-51-03

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 44,073 hrs · 27,007 cycles

FORWARD ENTRY EMERGENCY SLIDE/OVERWING LIGHT OUT.<[01] R & R FORWARD EMERGENCY SLIDE/OVERWING LIGHT PER AMM 33-51-04. OPS CHECK GOOD.

Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 43,222 hrs · 26,494 cycles

FLIGHT ATTENDANTS REPORTE FORWARD SERVICE DOOR GIRT BAR IS DIFFICULT TO ARM<[01] REPOSITIONED FWD SERVICE DOOR SLIDE IN THE COMPARTMENT & OPERATIONAL TEST CHECKED GOOD PER MT 725-61-06. REF. BARCODE: TTGQ00C810X.;[02] REPOSITIONED FWD SERVICE DOOR SLIDE IN THE COMPARTMENT & GIRT BAR OPERATIONAL TEST CHECKED GOOD PER MT 725-61-06. REF. BARCODE: TTGQ00C810X.

Part: FRAME — CRACKED (ZN 400 NACELLE/P) · airframe 43,014 hrs · 26,354 cycles

#1 ENGINE AFT PYLON HAS A CRACK IN THE AFT 'A' FRAME. CRACK IS 1 INCH LONG AND STOPS IN THE FRAME RADIUS.<[01] PERFORMED EA M-23-154-01884 (737-700/-800 - SWA-REPAIR- CRACK; #1/#2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY- TIME LIMITED)&NBSP;&NBSP;&NBSP;&NBSP;&NBSP;TTG8Q00NPC7K;[02] ACCOMPLISHED NDT PART 6; 51-00-00; PROCEDURE 12. CRACK IS CONFIRMED AND NO FURTHER DAMAGE NOTED.

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 42,771 hrs · 26,189 cycles

FORWARD R1 SERVICE DOOR DIFFICULT TO REMOVE AND INSTALL GIRT BAR<[01] REPOSITIONED SLIDE PACK IN COVER REF AMM 25-66-01.

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 42,728 hrs · 26,162 cycles

F/A REPORTS FWD SERVICE GURT BAR IS DIFFICULT TO ARM<[01] PERFORMED INSPECTION OF FWD SERVICE DOOR ESCAPE SLIDE. VERIFIED PROPER GIRT BAR ENGAGEMENT INTO FITTINGS. OPS CHECK GOOD PER AMM 25-66-01.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 42,531 hrs · 26,033 cycles

M1674 BATTERY PACK IS OUT; MULTIPLE EMERGENCY LIGHTS OUT<[01] R/R M1674 BATTERY PACK PER AMM 33-51-06. OPS CHECKS GOOD.

Part: SLIDE — LOOSE (ZN 800 DOOR) · airframe 41,394 hrs · 25,287 cycles

AFT ENTRY DOOR SLIDE FELL OUT<[01] REINSTALLED AFT ENTRY DOOR SLIDE IAW AMM 25-66-01

Part: PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 40,880 hrs · 24,922 cycles

RH IB SHELF PANEL 651FB HAS A DELAMINATION ON LOWER SKIN. REMOVED RH IB SHELF PANEL 651FB IAW AMM 57-50-02. INSTALLED R/H I/B SHELF PANEL 651FB IAW AMM 57-50-02.

Part: FAIRING — DELAMINATED (ZN 100 FUS LOWER) · airframe 40,880 hrs · 24,922 cycles

RH AFT LOWER WING TO BODY FAIRING HAS TWO DELAMINATED AREAS DUE TO #3 TIRE TREAD DAMAGE. R&R RH AFT LOWER WING TO BODY FAIRING IAW AMM 53-51-21.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,154 hrs · 24,416 cycles

LH GROUND EMERGENCY FLOODLIGHT INOP / [01] RE LAMPED LH GROUND EMERGENCY FLOOD LIGHT REF AMM 33-51-03

Part: NONE — OUT OF POSITION (OVERWING EXIT) · airframe 40,027 hrs · 24,329 cycles

EXIT SIGN NEXT TO EXIT DOOR (OVER WING; FO SIDE) IS UNSECURED / [01] REMOVED AND REPLACED THE EXIT SIGN ABOVE THE RIGHT WING NEAR THE EMERGENCY EXIT DOOR PER S.I.P.

Part: BATTERY PACK — FAILED · airframe 39,248 hrs · 23,793 cycles

EMERGENCY LIGHT BATTERY PACK AT 17A FAILED CAPACITY TEST / [01] FOUND BATTERY PACK DISLODGED; MOUNT HARDWARE LOOSE. SECURED HARDWARE AND PACK. CAPACITY CHECKS GOOD PER AMM 33-51-00

Part: LIGHT — BURNED (L2 DOOR) · airframe 38,917 hrs · 23,567 cycles

BURNED EMERGENCY LIGHT AND ENTRY LIGHT AFT ENTRY DOOR (2 EA) 2022-168948 / [01] REPLACED BURNED EMERGENCY LIGHT AND ENTRY LIGHT AFT ENTRY DOOR (2 EA) IAW B737-700 AMM 33-51-01-960-801 AND PERFORMED TEST IS GOOD;[02] CERTIFIED STEP 1; PERFORMED TEST; TEST OK. COMPLETED

Part: LIGHT — BURNED (L/H CABIN) · airframe 38,917 hrs · 23,567 cycles

BURNED EMERGENCY LIGHT OVERHEAD STOWAGE BIN ROW 23 LT (1 EA) 2022-168949 / [01] REPLACED EMERGENCY LIGHT OVERHEAD STOWAGE BIN ROW 23 LT (1 EA) IAW B737-700 AMM 33-51-03-960-801 AND PERFORMED TEST IS GOOD;[02] CERTIFIED STEP 1; PERFORMED TEST; TEST OK. COMPLETED

Part: LIGHT — BURNED (FWD GALLEY) · airframe 38,917 hrs · 23,567 cycles

BURNED EMERGENCY LIGHT FWD GALLEY (1 EA) 2022-168947 / [01] REPLACED EMERGENCY LIGHT FWD GALLEY (1 EA) IAW B737-700 AMM 33-51-01-960-801 AND PERFORMED TEST IS GOOD;[02] CERTIFIED STEP 1; PERFORMED LIGHT TEST; TEST OK. COMPLETED

Part: LIGHT — BROKEN · airframe 38,917 hrs · 23,567 cycles

BROKEN LAVATORY EXIT ASSEMBLY INDICATOR ON AFT LAVATORY AT AFT GALLEY AREA (1 EA) 2022-168905 / [01] REPLACED LAVATORY EXIT ASSEMBLY INDICATOR ON AFT LAVATORY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM-33-51-01-960-802;[02] CORRECTED STEP 1: REPLACED LAVATORY EXIT ASSEMBLY INDICATOR ON AFT LAVATORY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM-33-51-01-960-802 AND PERFORMED OPERATIONAL TEST IS GOOD;[03] REPLACED LAVATORY EXIT ASSEMBLY INDICATOR ON AFT LAVATORY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM-33-51-01-960-802 AND PERFORMED OPERATIONAL TEST IS GOOD. COMPLETED

Part: BRACKET — ELONGATED (R/H HORIZ. STAB.) · airframe 38,917 hrs · 23,567 cycles

ELONGATED HOLE LEADING EDGE BRACKET LOCATED AT OUTBOARD EDGE AT RT HORIZONTAL STABILIZER 2022-168889 / [01] REPLACED BRACKET AND FASTENERS LOCATED LEADING EDGE AT OUTBOARD EDGE AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND DWG 186A1240 REV B. SEE INDIVIDUAL SING-OFF BELOW.;[02] REPLACED BRACKET AND FASTENERS LOCATED LEADING EDGE AT OUTBOARD EDGE AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND DWG 186A1240 REV B. SEE INDIVIDUAL SING-OFF BELOW. COMPLETED

Part: INTERCOSTAL — DAMAGED (PAX CABIN) · airframe 38,917 hrs · 23,567 cycles

MACHINE WEB INTERCOSTAL LOCATED BS 685 TO BS 705 AND STR 14L PASSENGER CABIN 2022-168893 / [01] TOOL USED DIGITAL CALIPER P/N 500-193-30 S/N 0000291 DUE DATE 16-SEP-22.;[02] MACHINED WEB INTERCOSTAL (1EA) MATERIAL P/N 7050-T7451; LOCATED BS 685 TO BS 705 AND STR 14L PASSENGER CABIN; IAW DWG 144A7510 REV(B) AND B737-700 SRM 53-40-04-0I-1. TOOL USED: POWER PACK P/N FMK0003223 S/N PE0412/63335 DUE DATE: 26-JAN-23. MULTIMETER P/N FLUKE 179 S/N 97210603 DUE DATE: 24-DEC-22. THERMOMETER P/N 42510A S/N 200813258 DUE DATE: 29-JUN-22. FABRICATION OF PART (WEB INTERCOSTAL) WAS PERFORMED IN ACCORDING WITH AEROMAN LOCAL PARTS FABRICATION PROCESS AND IS DOCUMENTED ON FORM LOCAL FABRICATED PARTS REPORT FOR MACHINING METHOD QA-019/18-AEM-F FOR MACHINING PARTS. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] JOB COMPLETED

Part: LIGHT — INOPERATIVE · airframe 38,917 hrs · 23,567 cycles

INOP LOWER SIDEWALL EMERGENCY BATTERY PACK BTW STA 597 TO STA 616 LT SIDE AT PASSENGER CABIN 2022-168883 / [01] REPLACED LOWER SIDEWALL EMERGENCY BATTERY PACK BTW STA 597 TO STA 616 LT SIDE AT PASSENGER CABIN IAW B737-700 AMM-33-51-06-960-805 AND PERFORMED OPERATIONAL TES IS GOOD;[02] CORRECTED STEP 1: REPLACED LOWER SIDEWALL EMERGENCY BATTERY PACK BTW STA 597 TO STA 616 LT SIDE AT PASSENGER CABIN IAW B737-700 AMM-33-51-06-960-805 AND PERFORMED OPERATIONAL TEST IS GOOD;[03] REPLACED LOWER SIDEWALL EMERGENCY BATTERY PACK BTW STA 597 TO STA 616 LT SIDE AT PASSENGER CABIN IAW B737-700 AMM-33-51-06-960-805 AND PERFORMED OPERATIONAL TEST IS GOOD

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 38,917 hrs · 23,567 cycles

CRACK LEADING EDGE RIB LOCATED AT LE STA 95.96 AT RT HORIZONTAL STABILIZER 2022-168891 / [01] TOOL USED CALIPER PN 500-752-20 SN B21038254 CAL DUE DATE 11 AUG 22;[02] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.;[03] INSTALLED FASTENERS AND RIB ON LEADING EDGE LOC. AT STA 95.96 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1001 REV: A SHEET 7. SEE INDIVIDUAL SIGN-OFF BELLOW;[04] INSTALLED FASTENERS AND RIB ON LEADING EDGE LOC. AT STA 95.96 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1001 REV: A SHEET 7. RII VERIFIED

Part: INTERCOSTAL — DAMAGED (PAX CABIN) · airframe 38,917 hrs · 23,567 cycles

MACHINE WEB INTERCOSTAL LOCATED BS 685 TO BS 705 AND STR 14R PASSENGER CABIN 2022-168892 / [01] TOOL USED DIGITAL CALIPER P/N 500-193-30 S/N 0000291 DUE DATE 16-SEP-22;[02] TOOL USED POWER PACK P/N:FMK0003223;S/N:PE0412/63335;DUE DATE:26-JAN-23;THERMOMETER P/N:42510A;S/N:200813258;DUE DATE:29-JUN-22.MULTIMETER P/N:FLUKE 1587;S/N:99180027;DUE DATE:07-SEP-22.;[03] MACHINED NEW WEB INTERCOSTAL (1 E/A) LOCATED ON BS 685 TO BS 705 AND STR 14R PASSENGER CABIN IAW DWG 144A7510 REV. B; B737-700 SRM 53-40-04-0I-1; BAC5019 AND BAC5736. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] JOB COMPLETED

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 38,917 hrs · 23,567 cycles

CRACK LEADING EDGE RIB LOCATED AT LE STA 86.66 AT RT HORIZONTAL STABILIZER 2022-168890 / [01] TOOL USED CALIPER PN 500-752-20 SN B21038254 CAL DUE DATE 11 AUG 22.;[02] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.;[03] INSTALLED FASTENERS AND RIB ON LEADING EDGE LOC. AT STA 86.66 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1001 REV: A SHEET 7. SEE INDIVIDUAL SIGN-OFF BELLOW;[04] INSTALLED FASTENERS AND RIB ON LEADING EDGE LOC. AT STA 86.66 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1001 REV: A SHEET 7. RII VERIFIED

Part: WEB — CRACKED (FWD CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CRACK WEB LOC. ON STA500A TO STA500B AND STR 25L TO STR 26L FWD CARGO COMPARTMENT 2022-168869 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 190023010 DUE DATE: 14-FEB-23;[02] REPLACED WEB LOC. ON STA 500A TO STA 500B AND STR 25L TO STR 26L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7505 REV B.;[03] STEP 2 VERIFIED AND CORRECTIVE ACTION COMPLETED: ITEM RII REPLACED WEB LOC. ON STA 500A TO STA 500B AND STR 25L TO STR 26L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7505 REV B.

Part: PANEL — CRACKED (RH WING) · airframe 38,917 hrs · 23,567 cycles

CRACK ACCESS PANEL 632NB AT RT WING (1 EA) 2022-168859 / [01] REPLACED ACCESS PANEL 632NB AT RT WING IAW SRM 51-10-02-0G-0 THE INSTALLATION WILL BE COMPLETED WITH TTG8Q00B0DPK;[02] CORRECTED STEP 1<BR>REPLACED ACCESS PANEL 632NB AT RT WING IAW SRM 51-10-02-0G-0 THE INSTALLATION IS DOCUMENT WITH TTG8Q00B0DPK;[03] COMPLETE TASK CERTIFIED

Part: INTERCOSTAL — CRACKED (FWD GALLEY) · airframe 38,917 hrs · 23,567 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND BL 0 FWD GALLEY AND LAV 2022-168799 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 AND DRAWING 141A5400 REV:A;[02] CORRECTED STEP 1 <BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 AND DRAWING 141A5400 REV:A SEE INDIVIDUAL SIGNOFF BELOW;[03] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 AND DRAWING 141A5400 REV:A SEE INDIVIDUAL SIGNOFF BELOW COMPLETED RII

Part: INTERCOSTAL — CRACKED (FWD GALLEY) · airframe 38,917 hrs · 23,567 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 11 FWD GALLEY AND LAV 2022-168801 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 11 FWD GALLEY AND LAV IA W B737-700 SRM 51-40-02 AND DRAWING 141A5400 REV: A;[02] CORRECTED STEP 1 <BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 11 FWD GALLEY AND LAV IA W B737-700 SRM 51-40-02 AND DRAWING 141A5400 REV: A SEE INDIVIDUAL SIGNOFF BELOW;[03] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 11 FWD GALLEY AND LAV IA W B737-700 SRM 51-40-02 AND DRAWING 141A5400 REV: A SEE INDIVIDUAL SIGNOFF BELOW COMPLETED RII

Part: INTERCOSTAL — CRACKED (FWD GALLEY) · airframe 38,917 hrs · 23,567 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 BL 0 FWD GALLEY AND LAV 2022-168797 / [01] INSTALLED INTERCOSTAL AND FASTENERS LOCATED BS277 TO BS294.5 BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 REV -<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] INSTALLED INTERCOSTAL AND FASTENERS LOCATED BS277 TO BS294.5 BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 REV -<BR>SEE INDIVIDUAL SIGNOFFS BELOW<BR>TASK COMPLETED

Part: INTERCOSTAL — CRACKED (FWD GALLEY) · airframe 38,917 hrs · 23,567 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND RBL 11 FWD GALLEY AND LAV 2022-168803 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND RBL 11 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 13 REV -.SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND RBL 11 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 13 REV -.SEE INDIVIDUAL SIGNOFF BELOW COMPLETED RII

Part: ANGLE — CORRODED (FUSELAGE) · airframe 38,917 hrs · 23,567 cycles

CORROSION ANGLE LOCATED BETWEEN BS312 TO BS328 AT RBL59 AND WL208.1 AT FWD GALLEY AREA 2022-168798 / [01] REPLACED ANGLE LOCATED BETWEEN BS312 TO BS328 AT RBL59 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DWG 141A8310 REV: -;[02] CORRECTED STEP 1 <BR>REPLACED ANGLE LOCATED BETWEEN BS259.50 TO BS332.10 AT RBL59 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DWG 141A8310 REV:- SEE INDIVIDUAL SIGN-OFFS BELOW;[03] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: BRACKET — CORRODED (FUSELAGE) · airframe 38,917 hrs · 23,567 cycles

CORROSION SUPPORT BRACKET LOCATED BS344 AT LBL58 AND WL208.1 AT FWD GALLEY AREA 2022-168800 / [01] REPLACED SUPPORT BRACKET LOCATED BS344 AT LBL58 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9;[02] REPLACED SUPPORT BRACKET LOCATED BS344 AT LBL58 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9

Part: BEAM — CORRODED (FUSELAGE) · airframe 38,917 hrs · 23,567 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BS986.5 AT RBL43 AND WL208.1 AT AFT GALLEY AREA 2022-168811 / [01] ULTRASONIC THICKNESS GAGE P/N:38DLPLUS; S/N: 120398603; DUE DATE: 18-OCT-22;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 500D; SN:N500X12101V022240; DUE DATE: 27-JAN-23;[03] PERFORMED REPAIR FLOOR STRUCTURE BEAM LOCATED BS986.5 AT RBL43 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 FIGURE 204 SHEET 1 ALTERNATIVE 3.<BR><BR>SEE INDIVIDUAL SIGNOFFS BELLOW;[04] PERFORMED REPAIR FLOOR STRUCTURE BEAM LOCATED BS986.5 AT RBL43 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 FIGURE 204 SHEET 1 ALTERNATIVE 3.

Part: ANGLE — CORRODED (FWD FUSELAGE) · airframe 38,917 hrs · 23,567 cycles

CORROSION ANGLE LOCATED BS312 TO BS328 AT LBL60 AND WL208.1 AT FWD GALLEY AREA 2022-168806 / [01] REPLACED ANGLE AND FASTENER LOC. BS312 TO BS328 AT LBL60 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; DWG 141A8110 REV. ?<BR>PART NUMBER USED: 141A8112-20;[02] CORRECTED STEP1. <BR>REPLACED ANGLE AND FASTENER LOC. BS312 TO BS328 AT LBL60 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; DWG 141A8110 REV. ? <BR>PART NUMBER USED: 141A8112-20<BR>SEE INDIVIDUAL SIGNOFFS BELLOW;[03] COMPLETE TASK CERTIFIED RII

Part: WEB — CRACKED (L/H WING) · airframe 38,917 hrs · 23,567 cycles

CRACK INTERNAL CAVITY TRAILING EDGE WEB LOCATED ORRS 271 APPROX AT LT WING 2022-168778 / [01] REPLACED WEB AND FASTENERS LOCATED ORRS 271 APPROX AT LT WING IAW B737-700 SRM 51-40-02 DWG:115A2512 REV:-<BR><BR>SEE INDIVIDUAL SIGNOFFS BELLOW .;[02] REPLACED WEB AND FASTENERS LOCATED ORRS 271 APPROX AT LT WING IAW B737-700 SRM 51-40-02 DWG:115A2512 REV:-<BR><BR>SEE INDIVIDUAL SIGNOFFS BELLOW .

Part: BRACKET — CRACKED (AFT CARGO) · airframe 38,917 hrs · 23,567 cycles

CRACK BRACKET LOCATED ON BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2022-168780 / [01] INSTALLED NEW FITTING AND FASTENERES LOCATED BS947.5 STRINGER 26L IAW B737-700 SRM 51-40-02 AND DWG 149A8103 REV - <BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] INSTALLED NEW FITTING AND FASTENERES LOCATED BS947.5 STRINGER 26L IAW B737-700 SRM 51-40-02 AND DWG 149A8103 REV -<BR>SEE INDIVIDUAL SIGNOFFS BELOW.<BR>TASK COMPLETED

Part: PLATE — CRACKED (R/H WING) · airframe 38,917 hrs · 23,567 cycles

CRACK REAR SPAR CORRUGATED PLATE AT IRSS 214 APPROX AT RT WING 2022-168779 / [01] REPLACED CORRUGATED PLATE AND FASTENERS LOC. ON REAR SPAR AT IRSS 214 APPROX AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 115A2001 REV: -;[02] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: INTERCOSTAL — CRACKED (PAX CABIN) · airframe 38,917 hrs · 23,567 cycles

CRACK WEB INTERCOSTAL LOCATED BS685 TO BS706 AND STR14R AT PASSENGER CABIN 2022-168786 / [01] REPLACED WEB INTERCOSTAL; ANGLES (2EA) AND STRAP LOC BS685 TO BS706 AND STR14R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02;DWG 144A7500 REV A;[02] CORRECTED STEP 1 REPLACED WEB INTERCOSTAL; LOC BS685 TO BS706 AND STR14R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02;DWG 144A7500 REV A<BR> SEE INDIVIDUAL SIGNOFF;[03] REPLACED WEB INTERCOSTAL; LOC BS685 TO BS706 AND STR14R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02;DWG 144A7500 REV A <BR> SEE INDIVIDUAL SIGNOFF BELOW. COMPLETED RII

Part: INTERCOSTAL — CRACKED (PAX CABIN) · airframe 38,917 hrs · 23,567 cycles

CRACK WEB INTERCOSTAL LOCATED BS685 TO BS706 AND STR14L AT PASSENGER CABIN 2022-168785 / [01] INSTALLED WEB INTERCOSTAL ANGLES(2E/A) ; STRAP(1E/A) AND FASTENERS LOCATED BS685 TO BS706 AND STR14L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 144A7500 SHEET 6 ; REV A<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] INSTALLED WEB INTERCOSTAL ANGLES(2E/A) ; STRAP(1E/A) AND FASTENERS LOCATED BS685 TO BS706 AND STR14L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 144A7500 SHEET 6 ; REV A <BR>SEE INDIVIDUAL SIGNOFFS BELOW<BR><BR>RII ACCOMPLISHED

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 38,917 hrs · 23,567 cycles

CORROSION CREASE BEAM FLOOR STRUCTURE LOCATED BS867 AT LEVEL LBL69 AND WL208.1 AT PASSENGER CABIN 2022-168789 / [01] TOOL USED: ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130060401; DUE DATE: 26-JAN-23<BR>TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22;[02] TOOL USED : EDDY CURRENT TOOL; P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 02 JUN 22.;[03] PERFORMED PERMANENT REPAIR ON CREASE BEAM FLOOR STRUCTURE LOCATED BS867 AT LEVEL LBL69 AND WL208.1 AT PASSENGER CABIN IAW EA#22-153-01201-WIP1 & 22-153-01201-WIP2;[04] PERFORMED PERMANENT REPAIR ON CREASE BEAM FLOOR STRUCTURE LOCATED BS867 AT LEVEL LBL69 AND WL208.1 AT PASSENGER CABIN IAW EA#22-153-01201-WIP1 & 22-153-01201-WIP2. CERTIFIED RII;[05] PERFORMED PERMANENT REPAIR ON CREASE BEAM FLOOR STRUCTURE LOCATED BS867 AT LEVEL LBL69 AND WL208.1 AT PASSENGER CABIN IAW EA#22-153-01201-WIP1 & 22-153-01201-WIP2

Part: SUPPORT ANGLE — CRACKED (PAX CABIN) · airframe 38,917 hrs · 23,567 cycles

CRACK SUPPORT ANGLE LOCATED BS291.5 TO BS294.5 AND STR17R AT PASSENGER CABIN 2022-168760 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS291.5 TO BS294.5 AND STR17R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 DWG: DWG 141A8310 REV -;[02] COMPLETE TASK CERTIFIED RII

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 25R AND RBL 21 AT AFT CARGO COMPARTMENT 2022-168766 / [01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 25R AND RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 146A7500 REV:-;[02] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 25R AND RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 146A7500 REV:-<BR>ITEM RII

Part: TIE CLIP — CRACKED (PAX CABIN) · airframe 38,917 hrs · 23,567 cycles

CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2022-168759 / [01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW SRM 51-40-02;51-10-02 ITEM 9 DWG 141A1110 REV -;[02] CERTIFIED WORK PERFORMED RII

Part: INTERCOSTAL — CRACKED (PAX CABIN) · airframe 38,917 hrs · 23,567 cycles

CRACK WEB INTERCOSTAL LOCATED BS294.5 TO BS303.9 AND STR16L AT PASSENGER CABIN 2022-168765 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN. 60009161631; DUE DATE: 03-DEC-22;[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] TOOLS USED: POWER PACK P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 26-JAN-23; MULTIMETER P/N: FLUKE 87; S/N: 42180179; DUE DATE: 21-FEB-23; THERMOMETER P/N: 42510A; S/N: 200813258; DUE DATE: 29-JUN-22.;[04] PERFORMED REPAIR - FUSELAGE - INTERCOSTAL - BTW BSTA 294.5 & BSTA 303.9 AND AT S-16L IAW EA 22-153-01139-WIP1 [TTG8Q00BWCMV]; EA 22-153-01139 [TTG8Q00C6KUK]<BR>SEE INDIVIDUAL SIGNOFFS BELOW.;[05] PERFORMED REPAIR - FUSELAGE - INTERCOSTAL - BTW BSTA 294.5 & BSTA 303.9 AND AT S-16L IAW EA 22-153-01139-WIP1 [TTG8Q00BWCMV]; EA 22-153-01139 [TTG8Q00C6KUK] <BR>SEE INDIVIDUAL SIGNOFFS BELOW.<BR>TASK COMPLETED

Part: PANEL — ELONGATED (WING TO BODY) · airframe 38,917 hrs · 23,567 cycles

ELONGATED HOLE ACCESS PANEL 191HR AT LOWER FUSELAGE (2 EA) 2022-168723 / [01] REPLACED PANEL 191HR AT LOWER FUSELAGE (2 EA) IAW B737-700 AMM 53-51-400-803;[02] CORRECTED STEP 1<BR>REPLACED PANEL 191HR AT LOWER FUSELAGE (2 EA) IAW B737-700 AMM 53-51-21-400-803;[03] CERTIFIED STEP 2 COMPLETE

Part: THRESHOLD — CORRODED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CORROSION BILGE AREA LOWER SILL THRESHOLD LOCATED BTW BS 787 TO BS 847 AT LEVE STR 25R AND RBL 25 AT AFT CARGO COMPARTMENT 2022-168761 / [01] REPLACED FASTENERS AND THRESHOLD LOCATED BTW BS 787 TO BS 847 AT LEVE STR 25R AND RBL 25 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 Ï¿½TEM 9 AND DWG 146A8340 SHEET 28; REV:?;[02] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 807 AT LEVEL STR 25L AND LBL 21 AT AFT CARGO COMPARTMENT 2022-168764 / [01] REPLACED NEW SUPPORT ZEE LOCATED BTW BS 727 TO BS 807 AT LEVEL STR 25L AND LBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A7500-16 SEE INDIVIDUAL SIGNOFFS BELOW;[02] 0605;[03] STEP 2 <BR>BY ENTER IN ERROR;[04] CORREECTED STEP 1<BR>REPLACED NEW SUPPORTSUPPORT ZEE AND SPLICE LOCATED BTW BS 727 TO BS 807 PLUS 40 INCH (847) AT LEVEL STR 25L AND LBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A7500-16 REV: -;[05] STEP 4 VERIFIED AND CORRECTIVE ACTION COMPLETED: ITEM RII : REPLACED NEW SUPPORTSUPPORT ZEE AND SPLICE LOCATED BTW BS 727 TO BS 807 PLUS 40 INCH (847) AT LEVEL STR 25L AND LBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A7500-16 REV: -

Part: FRAME — CRACKED (PAX CABIN) · airframe 38,917 hrs · 23,567 cycles

CRACK FRAME LOCATED BS312 AND BETWEEN STR5L TO STR6L AT PASSENGER CABIN 2022-168763 / [01] TOOL USED PN NORTEC 500D SN N500X1693P030456 DUE DATE 26-JAN-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 REPAIR ON FRAME LOCATED BS312 AND BETWEEN STR5L TO STR6L AT PASSENGER CABIN IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 SEE INDIVIDUAL SIGNOFF BELOW;[04] PERFORMED REPAIR ON FRAME LOCATED BS312 AND BETWEEN STR5L TO STR6L AT PASSENGER CABIN IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 SEE INDIVIDUAL SIGNOFF BELOW. CERTIFIED RII

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CORROSION FLOOR STRUCTURE SHIELD PLATE LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R AND RBL 20 AT AFT CARGO COMPARTMENT 2022-168745 / [01] REPLACED SHIELD PLATE LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R AND RBL 20 AT AFT CARGO COMPARTMENT IAW DGW 146A0081 REV-;[02] REPLACED SHIELD PLATE LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R AND RBL 20 AT AFT CARGO COMPARTMENT IAW DGW 146A0081 REV-. RII VERIFIED

Part: STRINGER — CORRODED (FWD CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CORROSION STRINGER 26R BS 540; WL 148.5 PLUS 4 INCHES FWD CARGO COMPARTMENT 2022-168658 / REPAIRED STRINGER 26R BS 540; WL 148.5 PLUS 4 INCHES FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND B737-700 SRM 51-40-02 MADE REPAIR PARTS STRINGER SECTION (1 E/A); CHANNEL (1 E/A) AND ANGLES (2 E/A) MATERIAL P/N: 7075-T0/0.045/0.050 IN. PO:2021-183871; 2021-139514 . HEAT TREATED AND CONVERTED FROM 7075-T0 TO CONDITION 7075-T6 IAW BAC 5602 TABLE IV AND TABLE X. 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. SEE INDIVIDUAL SIGN-OFF BELOW;[05] REPAIRED STRINGER 26R BS 540; WL 148.5 PLUS 4 INCHES FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND B737-700 SRM 51-40-02 MADE REPAIR PARTS STRINGER SECTION (1 E/A); CHANNEL (1 E/A) AND ANGLES (2 E/A) MATERIAL P/N: 7075-T0/0.045/0.050 IN. PO:2021-183871; 2021-139514 . HEAT TREATED AND CONVERTED FROM 7075-T0 TO CONDITION 7075-T6 IAW BAC 5602 TABLE IV AND TABLE X. 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. SEE INDIVIDUAL SIGN-OFF BELOW

Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 38,917 hrs · 23,567 cycles

CRACK ACCESS PANEL 544BB AT LT WING 2022-168656 / [01] TOOL USED CALIPER P/N:500-464 S/N:15331932 DUE DATE: 26 OCT 22.;[02] TOOL USED: CALIPER P/N:500-464 S/N:15331926 DUE DATE:28-SEP-22;[03] TOOL USED: SCALE P/N:SCA-301 S/N:AE-412135 DUE DATE:14-MAR-23.;[04] TOOL USED HOT BONDER PN:HCS9000B-AV ; SN:18164925 DUE DATE 16-JAN-23.;[05] TOOL USED: MULTIMETER P/N: FLUKE87 S/N: 42180179 DUE DATE 21/FEB/23.;[06] REPAIRED ACCESS EPANEL 544BB AT LT WING IAW B737-700 SRM 57-53-70-2-R-5 REPAIR 5. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] JOB TASK COMPLETED.

Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 38,917 hrs · 23,567 cycles

CRACK ACCESS PANEL 542BB AT LT WING 2022-168655 / [01] TOOL USED CALIPER P/N:500-464 S/N:15331932 DUE DATE: 26 OCT 22.;[02] TOOL USED PN USM 35X; SN. 2787A; DUE DATE. 15-JUL-22;[03] REPAIRED ACCESS PANEL 542BB AT LT WING AS PER 22-157-01138 WIP1. SEE INDIVIDUAL SIGN OFFS BELOW.;[04] REPAIRED ACCESS PANEL 542BB AT LT WING AS PER 22-157-01138 WIP1. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: BRACKET — CRACKED (BS 540) · airframe 38,917 hrs · 23,567 cycles

CRACK SUPPER BRACKET LOCATED BS540 AND RBL8 AT LOWER FUSELAGE 2022-168647 / [01] REPLACED BRACKET LOCATED BS540 AND RBL8 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND 51-10-02;[02] COMPLETE TASK CERTIFIED

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,917 hrs · 23,567 cycles

CRACK SUPPORT BRACKET LOCATED BS540 AND LBL8 AT LOWER FUSELAGE 2022-168646 / [01] REPLACED BRACKET LOCATED BS540 AND LBL8 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND 51-10-02;[02] COMPLETE TASK CERTIFIED

Part: TRACK — CRACKED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CRACK TRACK RBBL 13.84 LOCATED AT BS 727E AFT CARGO COMPARTMENT 2022-168643 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 500D; SN:N500X12101V022240; DUE DATE:27-JAN-23;[02] FAULT RESOLVED IN FAULT TTG8Q00BLSRQ;[03] STEP 2 VERIFIED AND CORRECTIVE ACTION COMPLETED: FAULT RESOLVED IN FAULT TTG8Q00BLSRQ .

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS 907 AND BS 927 AND STRINGER 26R AFT CARGO COMPARTMENT 2022-168640 / [01] REPLACED ANGLE-SUPPORT LOCATED BETWEEN BS 907 AND BS 927 AND STRINGER 26R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 147A7221 SHEET 28 REV -<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED ANGLE-SUPPORT LOCATED BETWEEN BS 907 AND BS 927 AND STRINGER 26R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 147A7221 SHEET 28 REV - <BR>SEE INDIVIDUAL SIGNOFF BELOW .COMPLETED

Part: TRACK — CRACKED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CRACK TRACK RBBL 13.84 LOCATED AT BS 767 AFT CARGO COMPARTMENT 2022-168644 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 500D; SN:N500X12101V022240; DUE DATE:27-JAN-23;[02] TOOL USED CALIPER P/N: DIGITAL 150; S/N: 76210621256; DUE DATE: 02-FEB-23.;[03] PERFORMED REPAIR CARGO TRACK BTW BS 727D TO BS 787 RBBL 13.84 REPAIR PART [1] TRACK EXTRUSION MATERIAL USED BAC1520-1397 PO#2022 127682 AND [2] TRACK SPLICE MATERIAL USED BAC1509-100688 PO#2021 241191 IAW B-737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGN OFFS BELOW;[04] STEP 3 VERIFIED AND CORRECTIVE ACTION COMPLETED: ITEM RII PERFORMED REPAIR CARGO TRACK BTW BS 727D TO BS 787 RBBL 13.84 REPAIR PART [1] TRACK EXTRUSION MATERIAL USED BAC1520-1397 PO#2022 127682 AND [2] TRACK SPLICE MATERIAL USED BAC1509-100688 PO#2021 241191 IAW B-737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (BS 663) · airframe 38,917 hrs · 23,567 cycles

CRACK ANGLE LOCATED BS663.75 AND LBL28 AT LOWER FUSELAGE 2022-168648 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.;[02] INSTALLED ANGLE (ONLY FASTENERS COMMON TO VAPOR BARRIER) LOCATED BS 663 AND BTW LBL 5 TO LBL 65 AT LOWER FUSELAJE IAW B737-700 SRM 51-40-02 AND DWG #111A1000 REV A.<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[03] CORRECTED STEP 2 <BR>INSTALLED ANGLE LOCATED BS 663 AND BTW LBL 5 TO LBL 65 AT LOWER FUSELAJE IAW B737-700 SRM 51-40-02 AND DWG #111A1000 REV A.<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[04] CORRECTED STEP 3<BR>INSTALLED ANGLE LOCATED BS663.75 AND LBL28 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND DWG #111A1000 REV A.<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[05] CORRECTED STEP 4<BR>REPLACED ANGLE LOCATED BS663.75 AND LBL28 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND DWG #111A1000 REV A.<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[06] REPLACED ANGLE LOCATED BS663.75 AND LBL28 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND DWG #111A1000 REV A.RII VERIFIED

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CRACK ANGLE - SUPPORT LOCATED AT BS 867 AND BETWEEN STRINGER 26L AND STRINGER 27L AFT CARGO COMPARTMENT 2022-168639 / [01] REPLACED SUPPORT ANGLE LOCATED AT BS 867 AND BETWEEN STRINGER 26L AND STRINGER 27L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9;AND SRM 51-40-02;[02] CERTIFIED WORK PERFORMED

Part: VAPOR BARRIER — DEBONDED · airframe 38,917 hrs · 23,567 cycles

CUSTOMER REQUEST DEBONDED EXISTING REPAIR ON VAPOR BARRIER LT AT BS663 2022-168583 / [01] TOOL USED: CALIPER P/N 500-464 S/N 15331926 DUE DATE 28-SEP-22.;[02] TOOL USED HOT BONDER P/N HCS9000B-AV S/N 14081912 DUE DATE 04-JUN-22;[03] TOOL USED SCALE P/N CL5000 S/N AE-39087 DUE DATE 07-JUL-22;[04] TOOL USED HOT BONDER P/N HCS9000B-AV S/N 14081912 DUE DATE 04-JUN-22;[05] TOOL USED SCALE P/N CL5000 S/N AE-39087 DUE DATE 07-JUL-22;[06] REPAIRED VAPOR BARRIER LT AT BS663 IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED. RII COMPLETED.

Part: PLATE — CRACKED (L/H WING) · airframe 38,917 hrs · 23,567 cycles

CRACK REAR SPAR CORRUGATED PLATE AT IRSS 214 AT LT WING 2022-168605 / [01] INSTALLED NEW CORRUGATED PLATE AND FASTENERS LOC. ON REAR SPAR AT IRSS 214 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 REV: -;[02] CORRECTED STEP 1. REPLACED CORRUGATED PLATE LOC. ON REAR SPAR AT IRSS 214 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2001 REV: -;[03] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS 727B AND BS 727E CEILING AREA LEFT SIDE AFT CARGO COMPARTMENT 2022-168569 / [01] REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS 727B AND BS 727E CEILING AREA LEFT SIDE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING 149A9490 REV: -;[02] REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS 727B AND BS 727E CEILING AREA LEFT SIDE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING 149A9490 REV: -<BR>COMPLETED

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CRACK GUSSET LOCATED BS500D;STRINGER 19L FWD CARGO COMPARTMENT 2022-168566 / [01] REPLACED GUSSET AND FASTENERS LOCATED BS500D; STRINGER 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV -<BR>SEE INDIVIDUAL SIGNOFF;[02] REPLACED GUSSET AND FASTENERS LOCATED BS500D; STRINGER 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV - <BR>SEE INDIVIDUAL SIGNOFF. RII COMPLETED

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CRACK GUSSET LOCATED BS500D; STRINGER 19R FWD CARGO COMPARTMENT 2022-168565 / [01] REPLACED GUSSET AND FASTENERS LOCATED BS500D; STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV - <BR>SEE INDIVIDUAL SIGNOFF;[02] REPLACED GUSSET AND FASTENERS LOCATED BS500D; STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV - <BR>SEE INDIVIDUAL SIGNOFF. RII COMPLETED

Part: ANGLE — BROKEN (FWD CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

BROKEN ANGLE - CLIP LOCATED BS 500C; STRINGER 26R FWD CARGO COMPARTMENT 2022-168567 / [01] REPLACED ANGLE AND FASTENERS LOCATED BS 500C; STRINGER 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG:143A7505 REV:-;[02] CORRECTED STEP 1 <BR><BR>REPLACED ANGLE AND FASTENERS LOCATED BS 500C; STRINGER 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG:143A7505 REV:-<BR><BR>SEE INDIVIDUAL SIGNOFFS BELLOW;[03] CERTIFIED STEP 2 COMPLETE RII <BR>IAW B737-700 SRM 51-40-02 DWG:143A7505 REV:-

Part: SUPPORT BRACKET — CRACKED (PAX CABIN) · airframe 38,917 hrs · 23,567 cycles

CRACK FLOOR STRUCTURE SUPPORT BRACKET LOCATED AT STA. 540 AND LBL 0.07 TO LBL 24.82 AT PASSENGER CABIN 2022-168563 / [01] REPLACED SUPPORT BRACKET LOCATED AT STA. 540 AND LBL 0.07 TO LBL 24.82 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A0060 REV A;[02] CERTIFIED WORK PERFORMED

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-168556 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A18135080; DUE DATE 31-JUL-22.;[02] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-30-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] TASK COMPLETED.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2022-168555 / [01] TOOL USED: DIGITAL CALIPER P/N:500-193-30; S/N: 0000291; DUE DATE: 16/SEP/22.;[02] REPAIRED BY WELDS AFT CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1; REPAIR 1. PARAGRAPH 4.B. STEP ( 2 ) AND STEPS ( 4 ) TO ( 7 ) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] TASK COMPLETED

Part: BULKHEAD — CRACKED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CRACK BULKHEAD PANEL 141PW AT AFT CARGO COMPARTMENT 2022-168468 / [01] EVALUATED CRACK BULKHEAD PANEL 141PW AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 AMM 25-52-00-200-806 PARAGRAPH 6.D. (3) (4). DAMAGE SIZE: L=0.76IN; AND REPAIRED AS PER B737-700 AMM 25-52-01-300-804 PARAGRAPH 3.F. TOOL USED= CALIPER P/N: 500-197-30; S/N: A21042060; DUE DATE: 11-AUG-22;[02] EVALUATED CRACK BULKHEAD PANEL 141PW AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 AMM 25-52-00-200-806 PARAGRAPH 6.D. (3) (4). DAMAGE SIZE: L=0.76IN; AND REPAIRED AS PER B737-700 AMM 25-52-01-300-804 PARAGRAPH 3.F. TOOL USED= CALIPER P/N: 500-197-30; S/N: A21042060; DUE DATE: 11-AUG-22. VERIFIED

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 38,917 hrs · 23,567 cycles

CORROSION STRAP LOCATED ON FLOOR PANEL 140CF AT LEVEL STA 792 AND RH SIDE AT AFT CARGO COMPARTMENT 2022-168501 / [01] REPLACED STRAP LOCATED ON FLOOR PANEL 140CF AT LEVEL STA 792 AND RH SIDE AT AFT CARGO COMPARTMENT IAW B737-700 SRMK 51-40-02;[02] CORRECTED STEP 1<BR>REPLACED STRAP LOCATED ON FLOOR PANEL 140CF AT LEVEL STA 792 AND RH SIDE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;[03] REPLACED STRAP LOCATED ON FLOOR PANEL 140CF AT LEVEL STA 792 AND RH SIDE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. COMPLETED

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 37,278 hrs · 22,547 cycles

FWD ENTRY DOOR SLIDE CAME OUT OF BAG AND CONTAINER ; / [01] R&RD FWD ENTRY DOOR SLIDE PER 25-66-01 MM

Part: BEAM — DAMAGED (NOT REPORTED) · airframe 36,783 hrs · 22,254 cycles

REAR BEAM-LEFT LOCK PIN HOLE OUT OF ROUND ; / [01] R AND R BEAM IAW CMM 25 11 39; [02] C/W JIC

Part: HOOK AND LOOP — LOOSE (L2 DOOR) · airframe 36,155 hrs · 21,870 cycles

FA REPORTS LEFT REAR SLIDE INFLATION HANDLE IS EXPOSED WHEN SLIDE IS ARMED. ; / RETTACHED VELCRO COVER IAW SIP.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 35,358 hrs · 21,404 cycles

FWD SVC DOOR ESCAPE SLIDE CASE LATCH BROKEN. REPOSITIONED SLIDE IN SLIDE COMPARTMENT, PER MT 725-61-06. OPERATIONS CHECK NORMAL.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,135 hrs · 20,627 cycles

LH OVERWING SIDEWALL EMERGENCY EXIT LOCATOR LIGHT INOP / FOUND CONNECTOR D03670 DISCONNECTED; RESECURED OPS CHECK GOOD; REF AMM 33-51-01

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,052 hrs · 20,585 cycles

MAIN ENTRY DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. R & R EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD PER AMM 33-51-06.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 34,012 hrs · 20,565 cycles

FORWARD SECTION OF LEFT SKATE ANGLE HAS MATERIAL CHAFFED; MISSING AT BS 1005 TO BS 1016. / REMOVED AND REPLACED LEFT FWD SKATE ANGLE PER SRM 51-40-02 AND AMM 51-21-73

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 34,012 hrs · 20,565 cycles

LEFT SKATE ANGLE HAS MATERIAL LOSS; CHAFFING AT BS 1106 TO 1109. / REPAIRED SKATE ANGLE PER SRM 53-80-71-2R-6.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,012 hrs · 20,565 cycles

CRACK INDICATION @ STA 242 16.5 ' ABOVE STR 17L. MARKED. / FACT AS A RESULT OF POST REPAIR INSPECTION

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 34,012 hrs · 20,565 cycles

LEFT HORIZONTAL STAB #5 RIB AT SSTA 129.50 3RD STIFFENER IS CRACKED. / REPAIRED LEFT HORZ STAB 3RD STIFFENER ON RIB #5; STAB STA 129.50 PER SRM 55-10-09-2R-4.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 34,012 hrs · 20,565 cycles

THE #2 SEAT TRACK HAS WEAR ON THE TOP OF THE TRACK AT APPROXIMATELY STA 520. / REMOVED FLOORBOARDS COMMON TO REPAIR AREA; REMOVED DAMAGED PORTION OF TRACK AND REPAIRED SEAT TRACK PER SRM 53-00-52-2R-4; REINSTALLED FLOORBOARDS COMMON TO REPAIR AREA PER AMM 53-21-00. SEE CARD FOR INDIVIDUAL SIGN OFFS

Part: HOOK — CORRODED (EMERGENCY EXIT) · airframe 34,012 hrs · 20,565 cycles

R/H EMERGENCY EXIT; LIFE LINE HAS CORROSION ON THE HOOK. (CORROSION IS LIMITED TO ESCAPE ROPE HOOK; NOT AIRCRAFT STRUCTURE) / R&R R/H EMERGENCY EXIT; LIFE LINE PER AMM 25-61-10.

Part: HOOK — CORRODED (EMERGENCY EXIT) · airframe 34,012 hrs · 20,565 cycles

L/H EMERGENCY EXIT; LIFE LINE HAS CORROSION ON THE HOOK. (CORROSION IS LIMITED TO ESCAPE ROPE HOOK; NOT AIRCRAFT STRUCTURE) / R&R L/H EMERGENCY EXIT; LIFE LINE PER AMM 25-61-10.

Part: ATTACH ANGLE — MISSING (LT WING) · airframe 34,012 hrs · 20,565 cycles

LH WING DEFLECTION RIB INBOARD SIDE; SHELF PNL ATTACH ANGLE BENT AND MISSING FASTENERS. / REMOVED AND REPLACED LH WING DEFLECTION RIB ATTACH CLIP PER SRM 51-40-02.

Part: BRACKET — BROKEN (ACCESS PANEL) · airframe 34,012 hrs · 20,565 cycles

FORWARD L/H MOUNT BRACKET FOR FUSELAGE ACCESS PANEL 192E IS BROKEN. / REMOVED AND REPLACED PER SRM 51-40-02.

Part: COVER — MISSING (CABIN) · airframe 33,404 hrs · 20,162 cycles

EMERGENCY LIGHT SWITCH COVER MISSING AFT. / INSTALLED SWITCH COVER PER WPM.

Part: SEAL — CRACKED (RH HOR STAB) · airframe 33,121 hrs · 19,984 cycles

RIGHT HORIZONTAL STABILIZER FORWARD RIGHT UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FORWARD LEFT UPPER SLIDING SEAL PER AMM 53-31-31

Part: SEAL — CRACKED (LH HOR STAB) · airframe 33,121 hrs · 19,984 cycles

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

Part: FLOOR PANEL — CRACKED (FWD CARGO COMPT) · airframe 31,180 hrs · 18,706 cycles

FWD CARGO BIN AFT FLOOR PNL HAS A 7' TEAR/CRACK ALONG FLOOR BEAM / REMOVED AND REPLACED PER AMM. 25-52-01

Part: COVER — DAMAGED (EXIT SIGN) · airframe 30,413 hrs · 18,231 cycles

RT OVERWING EMERGENCY SIDEWALL LIGHT SIGN DAMAGED. R&R COVER PER MM.

Part: HOOK AND LOOP — LOOSE (EMERGENCY EXIT) · airframe 29,982 hrs · 17,940 cycles

RT OVERWING EMERGENCY EXIT HOOK AND LOOP HOLDING COVER FOR STRAP LOOSE. R&R HOOK AND LOOP IAW SIP.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 29,955 hrs · 17,921 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 28,967 hrs · 17,264 cycles

STIFFENER EXTENSION CRACKED; R/H MLG W/W-STA 663; RBL 25. / REMOVED AND REPLACED PER SRM 51-40-02.

Part: STRIP — CRACKED (AFT CARGO BAY) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO FWD CAPSTRIP AT STA727+4 IS BROKEN. / REMOVED AND REPLACED CAP STRIP ASSEMBLY AT STA 727+4 AFT CARGO IAW SRM 51-40-02.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 27,699 hrs · 16,455 cycles

FWD CARGO L/H AFT BAFFLE @ LBL21 STA.500C-500D CRACKED / REMOVED AND REPLACED BAFFLE LBL 21 AT STA 500C-500D PER SRM 51-40-02.

Part: SUPPORT — CRACKED (CABIN) · airframe 27,699 hrs · 16,455 cycles

FLOOR SUPPORT CRACKED AT STA 540 BL 0 / REPLACED LEFT AND RIGHT BREAK PANEL ASSEMBLIES PER SRM 51-40-02.

Part: FAIRING — DELAMINATED (LEFT WING) · airframe 27,699 hrs · 16,455 cycles

FORWARD FLAP TRACK FAIRING 543AB HAS DENT AND DELAMINATION. / REPAIRED #2 FWD. FLAP TRACK SUPPORT FAIRING PER SRM 51-70-05-2R-1. REMOVED & INSTALLED FWD. FAIRING PER M/M 27-51-28

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,699 hrs · 16,455 cycles

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

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 27,699 hrs · 16,455 cycles

FWD CARGO BIN AFT FLRBD SUPPORT ANGLE CORRODED STA 500D LBL 24 TO RBL 24. / REMOVED AFT BULKHEAD SUPPORT ANGLE ; LOCATED; DRILLED AND COUNTERSUNK NEW PART AS PER AMM 51-40-05 AND 51-40-08. INSTALLED NEW AFT BULKHEAD SUPPORT ANGLE AS PER SRM 51-010-02 & 51-40-02.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO COMPARTMENT TRANSITION ANGLE HAS CORROSION AROUND FASTNER HOLES L/H SIDE BETWEEN STA.727C AND STA.727D MARKED / REMOVED AND REPLACED L/H TRANSITION ANGLE FROM STA. 727+4 TO STA. 847 PER SRM 51-40-02.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO COMPARTMENT TRANSITION ANGLE HAS CORROSION AROUND FASTNER HOLES L/H SIDE BETWEEN STA.727E AND STA.747 MARKED / L/H TRANSITION ANGLE IS REMOVED AND REPLACED ON N/R G551881 FROM STA. 727+4 TO STA. 847.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO COMPARTMENT TRANSITION ANGLE HAS CORROSION AROUND FASTNER HOLES L/H SIDE BETWEEN STA.787 AND STA.807 MARKED. / L/H TRANSITION ANGLE IS REMOVED AND REPLACED ON N/R G551881 FROM STA. 727+4 TO STA. 847.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CAP CORRODED BETWEEN BS 787 TO BS 767, RBL 15. REPAIRED CAP PER EA.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO COMPARTMENT TRANSITION ANGLE HAS CORROSION AROUND FASTNER HOLES R/H SIDE BETWEEN STA.767 AND STA.787 MARKED / REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA 767 TO STA 787 PER SRM 51-40-02.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO COMPARTMENT TRANSITION ANGLE HAS CORROSION AROUND FASTNER HOLES R/H SIDE BETWEEN STA.727C AND STA.727D MARKED / REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA 727 TO STA 767 PER SRM 51-40-02.

Part: PANEL — ELONGATED (LOWER EXT FUSELA) · airframe 27,699 hrs · 16,455 cycles

WING TO BODY FAIRING PANEL 191D HAS 2EA. ELONGATED SCREW HOLES AT T/E ROW. MKRD / REPAIRED PANEL PER SRM 51-70-05.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO FWD SCUFF PLATE CRACKED. / REPAIRED PER RO#7530063-B0R. TO BE INSTALL ON TASK CARD 753-140-00-02Y.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO BULLNOSE SCUFF PLATE CRACKED. / REPAIRED PER RO#7530061-FHR. TO BE INSTALL ON TASK CARD 753-140-00-02Y.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO AFT SCUFF PLATE CRACKED. / REPAIRED PER RO#7530220-AMR. TO BE INSTALL ON TASK CARD 753-140-00-02Y.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 27,699 hrs · 16,455 cycles

FWD CARGO FWD SCUFF PLATE CRACKED. / REPAIRED PER RO# 7530028-AQR. TO BE INSTALLED ON TASK CARD 753-140-00-01Y.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 27,699 hrs · 16,455 cycles

FWD CARGO AFT SCUFF PLATE CRACKED. / REPAIRED PER RO# 7530065-AUR. TO BE INSTALLED ON TASK CARD 753-140-00-01Y.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 27,699 hrs · 16,455 cycles

FWD CARGO BULLNOSE SCUFF PLATE CRACKED. / REPAIRED PER RO# 7530064-DXR. TO BE INSTALLED ON TASK CARD 753-140-00-01Y.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 27,047 hrs · 16,043 cycles

LOG BOOK ENTRY REQUIRED; R/H HORIZ STAB HAS CRACK ON THE #4 INSPAR RIB; VERTICAL STIFFENER 3 VERIFIED VIA HFEC (TRANSFERED FROM LOGBOOK PAGE 0141479) / REPAIRED R/H HORIZONTAL STAB #4 INSPAR RIB VERTICAL STEFFENER #3 IAW SRM 55-10-09-2R-4. UPDATED LOG BOOK.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,047 hrs · 16,043 cycles

RT HORIZONTAL STABILIZER NR 4 INSPAR RIB CRACKED BETWEEN VERTICAL STIFFENERS 2 AND 3. REPAIRED RIB IAW SRM.

Part: NONE — CRACKED (RT HORIZ STAB) · airframe 27,047 hrs · 16,043 cycles

LOGBOOK ENTRY REQUIRED; R/H HORIZ STAB HAS CRACKS ON THE #4 INSPAR RIB; VERTICAL STIFFENERS 2 VERIFIED VIA HFEC (TRANSFERED FROM LOGBOOK PAGE 0141479) / REPAIRED R/H HORIZ. STABILIZER; #4 INSPAR RIB; VERTICAL STEFFENER 2; IAW SRM 55-10-09-2R-4 REPAIR 4. UPDATED LOG BOOK .

Part: NONE — CRACKED (RT HORIZ STAB) · airframe 27,047 hrs · 16,043 cycles

LOGBOOK ENTRY REQUIRED; R/H HORIZ STAB HAS CRACKS ON THE #4 INSPAR RIB; #4 VERTICAL STIFFENER VERIFIED VIA HFEC (TRANSFERED FROM LOGBOOK PAGE 0141480) / REPAIRED R/H HORIZONTAL STAB #4 INSPAR RIB #4 VERTICAL STIFFNER IAW SRM 55-10-09-2R-4.

Part: STIFFENER — CRACKED (HORIZONTAL STAB.) · airframe 27,048 hrs · 16,043 cycles

RIGHT HORIZONTAL STAB NR 4 IN SPAR RIB NR 4, VERTICAL STIFFENER CRACKED. REPAIRED THE STIFFENER IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 26,656 hrs · 15,813 cycles

EMERGENCY LIGHT INOP AT THE RT FWD END. R & R THE EMERGENCY LIGHT SECTION IAW MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 25,658 hrs · 15,155 cycles

LEFT EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED THE LENS IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,604 hrs · 15,121 cycles

R/H OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: SPLICE STRAP — CORRODED (FUSELAGE) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO COMPARTMENT SPLICE STRAP CORRODED BETWEEN BS 727D TO BS 727E, BOTH SIDES OF STRAP. R&R STRAP PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO THRESHOLD REINFORCEMENT STRAP INBOARD OF WEB SUPPORT CORRODED BETWEEN BS 799 TO BS 847, AROUND NUTPLATE HOLES. REPAIRED SUPPORT PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,699 hrs · 16,455 cycles

FORWARD CARGO BIN WEB UNDER DOOR THRESHOLD CORRODED. REPAIRED WEB PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,699 hrs · 16,455 cycles

AFT CARGO THRESHOLD SUPPORT WEB CORRODED BETWEEN BS 794 TO BS 847. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,699 hrs · 16,455 cycles

LOWER LIP OF EXTERNAL POWER RECEPTACLE CUTOUT CRACKED. REPAIRED CUTOUT PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 24,285 hrs · 14,308 cycles

R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE ASSEMBLY IAW MT.

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR SLIDE) · airframe 24,252 hrs · 14,289 cycles

R2 DOOR SLIDE GIRT BAR OUT OF ADJUST. ADJUST GIRT BAR IAW SIP.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 21,680 hrs · 12,768 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOWER FLAP OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: SIGN — LOOSE (CABIN) · airframe 21,542 hrs · 12,695 cycles

CENTER CABIN EMERGENCY EXIT ROW SIGN LOOSE. SECURED SIGN PER AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 20,983 hrs · 12,359 cycles

RIGHT MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 35.0. REPAIRED WEB IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 20,513 hrs · 12,085 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1670. R & R BATTERY PACK IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 20,513 hrs · 12,085 cycles

MAIN CABIN CTR CEILING EMER EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 18,287 hrs · 10,764 cycles

EMERGENCY LIGHT BATTERY M1668 FAILED CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 18,287 hrs · 10,764 cycles

EMERGENCY LIGHT BATTERY M1675 FAILED CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 18,287 hrs · 10,764 cycles

EMERGENCY LIGHT BATTERY M1674 FAILED CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 18,287 hrs · 10,764 cycles

EMERGENCY LIGHT BATTERY M1672 FAILED CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 18,287 hrs · 10,764 cycles

EMERGENCY LIGHT BATTERY M1673 FAILED CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 18,287 hrs · 10,764 cycles

EMERGENCY LIGHT BATTERY M1669 FAILED CHECK. R & R BATTERY IAW MM.

Part: LIGHT — WORN (CABIN) · airframe 18,279 hrs · 10,760 cycles

EEPLS WORN FWD OF SEAT ROW 1 DEF. R & R EEPLS IAW MM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 18,279 hrs · 10,760 cycles

FORWARD CARGO FLOOR SUPPORT CRACKED AT STATION 540, FWD ACFT DISTRIBUTION BAY AREA. R & R SUPPORT IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 16,724 hrs · 9,868 cycles

R2 DOOR EMER LIGHT EXIT LENS BROKEN. REPAIRED LENS IAW EA.

Part: COVER — LOOSE (CABIN) · airframe 14,587 hrs · 8,630 cycles

L1 DOOR LOWER EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.

Part: SIGN — BROKEN (CABIN) · airframe 13,148 hrs · 7,806 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 10,223 hrs · 6,066 cycles

RIGHT FWD GALLEY EMERGENCY LIGHT LENS BROKEN. REMOVED & REPLACED LIGHT ASSY IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 9,861 hrs · 5,836 cycles

CLEAR EMERGENCY LIGHT LENS BROKEN AT 20 ABC. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 9,663 hrs · 5,713 cycles

FWD ENTRY EMERGENCY EXIT SIGN LENSE FELL OFF. REMOVED AND REPLACED FWD ENTRY EMERGENCY EXIT LIGHT ASSY IAW M/M, OPS CHECKS GOOD PER MM.

Part: COVER — MISSING (CABIN) · airframe 8,794 hrs · 5,173 cycles

RIGHT EEPLS COVER MISSING AT ROW 20. INSTALLED COVER PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,794 hrs · 5,173 cycles

LEFT EEPLS INOP AT ROW 11. RELAMPED EEPLS PER AMM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 8,429 hrs · 4,938 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER M/M AND MT.

Part: COVER — LOOSE (CABIN) · airframe 7,605 hrs · 4,413 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER M/M.

Part: LENS — CRACKED (CABIN) · airframe 6,895 hrs · 3,998 cycles

LT EGRESS LENS CRACKED AT ROW 1. REMOVED AND REPLACED LENS PER M/M.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 6,179 hrs · 3,600 cycles

FWD LT BULLNOSE EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — BROKEN (CABIN) · airframe 5,574 hrs · 3,236 cycles

FWD EELS COVER BROKEN. R&R COVER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 5,368 hrs · 3,115 cycles

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

Part: COVER — MISSING (CABIN) · airframe 4,797 hrs · 2,785 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 4,796 hrs · 2,785 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 4,796 hrs · 2,785 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 3,610 hrs · 2,073 cycles

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

Part: COVER — MISSING (CABIN) · airframe 3,387 hrs · 1,951 cycles

FWD EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 2,703 hrs · 1,571 cycles

FWD EEPLS LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 2,619 hrs · 1,518 cycles

AFT SERVICE DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 1,136 hrs · 660 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 1,067 hrs · 622 cycles

REAR COFFEEMAKERS HAD BEEN SMOKING AND FLAMES. FLIGHT ATTENDANTS SHUT THEM DOWN. REMOVED AND REPLACED AFT COFFEEMAKERS PER MM.