N7734H

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES ON ACCESS PANEL 195AL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCES PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES OF ACCESS PANEL 194DL WING TO BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES ON ACCESS PANEL 194HL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES ON ACCESS PANEL 194CR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES ON ACCESS PANEL 195AR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.

Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES ON THE ACCESS PANEL 661BB AT TRAILING EDGE, RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING T/E IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES ON ACCESS PANEL 194CL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES ON ACCESS PANEL 195BL OF THE BODY FAIRING FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES ON ACCESS PANEL 195BR, BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9.

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES ON ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-9, REPAIR 9.

Part: SKIN PANEL — CRACKED (ZONE 300) · airframe 62,889 hrs · 34,830 cycles

CRACK INDICATION FOUND ON THE LT HORIZONTAL STAB LOWER SKIN PANEL HSS 193.9 RIB & 16 INCHES FROM FRONT SPAR, INBD SIDE OF RIB. CRACK LENGTH: 0.900 INCH. REPAIRED HORIZONTAL STAB LOWER SKIN IAW SRM 51-40-02, SRM 55-10-01-2R-11, REPAIR 11.

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES ON ACCESS PANEL 193CR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8.

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 62,889 hrs · 34,830 cycles

ELONGATED HOLES ON ACCESS PANEL 561BB AT THE RT WING T/E. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: WIRE — DETERIORATED (ZONE 200) · airframe 62,889 hrs · 34,830 cycles

DETERIORATED ELECTRICAL WIRING OF EMERGENCY EXIT LIGHT ON CEILING PANEL 231YDC. REPLACED EMERGENCY EXIT LIGHT IAW AMM 33-51-01-960-802, PERFORMED AN OPS TEST. TESTED OK.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

CRACK ON THE FWD CORNER OF THE SCUFF PLATE IN FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 62,889 hrs · 34,830 cycles

CRACK INDICATION ON STUB FRAME, BETWEEN BS 294.5 - 296.5, S8 - 9R IN THE FWD GALLEY DOOR AREA. CRACK LENGTH: 0.875 IN. REPLACED THE STUB FRAME IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, & DWG 141A8370, SHEET 10, REV D.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 62,889 hrs · 34,830 cycles

CRACK ON THE FWD CORNER OF THE SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.

Part: SENSOR — FAULTY (TE FLAP) · airframe 62,075 hrs · 34,286 cycles

WITH FLAP 1 SELECTED FLAPS REMAINED AT 0 AND WOULD NOT EXTEND. FOLLOWED QRH. ALTERNATE FLAPS WERE USED AND PERFORMED 0 FLAP LANDING<[01] TS AND FOUND FC 27-53251 #2 SKEW IN FSEU; AHM RECORDED A 50 UNIT DIFFERENCE FOR PAIR 2/7. ACMS SHOWED ERRATIC MOTION ON #2 SKEW. REMOVED AND REPLACED #2 SKEW SENSOR REF MM 27-59-01 OPS TEST GOOD

Part: SEAT — OUT OF ADJUST (ZONE 200) · airframe 61,982 hrs · 34,233 cycles

SEAT 11 D RECLINES TOO FAR INTO EXIT ROW, SEAT 11D ADJUSTED RECLINE LOCK PER AMM 25-22-00.

Part: LENS — MISSING (ZONE 200) · airframe 61,240 hrs · 33,816 cycles

R/H OVERWING EMER EXIT LIGHT LENS MISSING.<[01] REPLACED MISSING LIGHT COVER ON R/H SIDE OVERWING EMER EXIT PER AMM 33-51-01.

Part: BRACKET — CRACKED (ZONE 400) · airframe 60,660 hrs · 33,477 cycles

#2 ENG. HIGH STAGE REGULATOR BRACKET HAS A CRACK.

Part: POWER SUPPLY — DEPLETED (ZN 200 FUS TOP) · airframe 59,560 hrs · 32,810 cycles

AIRCRAFT ON GROUND POWER EMER EXIT LIGHTS IN ARMED POSITION HALF THE EMERGENCY EXIT LIGHTS ARE ON.<[01] RECHARGED & RESET FWD POWER SUPPLY L&R PER AMM 33-51-06. OPS CHK OK.

Part: OVERHEAT SENSOR — FAULTED (ZONE 400) · airframe 59,296 hrs · 32,645 cycles

LEFT WING BODY OVERHEAT LIGHT ILLUMINATED IN CLIMB THEN EXTINGUISHED WHEN ENGINE 1 BLEED SWITCH TURNED OFF<[01] REPLACED M1761 OVHT DETECTOR ON #1 ENGINE FWD STRUT CAVITY IAW AMM 26-18-02; OPS CHECKS GOOD; FAULT CLEARED

Part: BRACKET — CRACKED (ZONE 800) · airframe 58,801 hrs · 32,347 cycles

DOOR PANEL 834 DZ AFT MOUNTING BRACKET CRACKED. REPLACED AFT SVC DOOR PANEL 834 DZ AFT MOUNTING BRACKET PER AMM 20-50-11. REPLACED AFT ENTRY DOOR PANEL 834 DZ PER AMM 52-13-31.

Part: SLIDE — DISLODGED (FWD SERVICE DOOR) · airframe 57,569 hrs · 31,559 cycles

SLIDE FROM FWD SERVICE DOOR FELL OUT<[01] REPACKED FWD SERVICE DOOR SLIDE PER MT725-61-06

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 57,072 hrs · 31,251 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 0.775 INCHES. 2024-78606<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE: 15-FEB-24 WAS USED ON STEP 5;[02] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE: 20-JUN-24 WAS USED ON STEP 8;[03] REPAIRED RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN BTW STAB STA 189.6 TO STAB STA 198.93. AND BTW 12 INCH FROM FRONT SPAR AND 12.500 INCH OF THE REAR SPAR IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 SEE INDIVIDUALS SIGN OFF BELOW;[04] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLOORBEAM — CRACKED (BS 540 BL0-LBL25) · airframe 57,072 hrs · 31,251 cycles

PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75. 2024-78600<[01] REPLACED PANEL BREAK AND FASTENER FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO LBL 24.75 PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G PARAGRAPH 9 AND DWG 143A0060 SHEET 46 REV-.;[02] CORRECTED STEP 1 .<BR>REPLACED PANEL BREAK FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO LBL 24.75 PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A0060 SHEET 46 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED PANEL BREAK FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO LBL 24.75 PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A0060 SHEET 46 REV-. SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII

Part: FLOORBEAM — CRACKED (BS 540 BL0-RBL25) · airframe 57,072 hrs · 31,251 cycles

AAI REPORT: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75. 2024-78599<[01] REPLACED PANEL PANEL BREAK FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO RBL 24.75 PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A0060 SHEET 46 REV.;[02] CORRECTED STEP 1 <BR>REPLACED PANEL PANEL BREAK FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO RBL 24.75 PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A0060 SHEET 46 REV.SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPLACED PANEL PANEL BREAK FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO RBL 24.75 PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A0060 SHEET 46 REV.SEE INDIVIDUAL SIGNOFFS BELOW

Part: BRACKET — CRACKED (BS 663) · airframe 57,070 hrs · 31,250 cycles

CRACK ON BRACKET LOCATED BETWEEN RBL54.21 TO RBL 45.64 AT VAPOR BARRIER RT SIDE 2024-78542<[01] REPLACED BRACKET LOCATED BTW RBL 54.21 TO RBL 45.64 AT VAPOR BARRIER RT SIDE. IAW B737-700 SRM 51-10-02 & DWG # 111A1001; SHEET 378 & REV A.;[02] REPLACED BRACKET LOCATED BTW RBL 54.21 TO RBL 45.64 AT VAPOR BARRIER RT SIDE. IAW B737-700 SRM 51-10-02 & DWG # 111A1001; SHEET 378 & REV A.

Part: ANGLE — CRACKED (RT WING TE) · airframe 57,072 hrs · 31,251 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS266 DEFLECTION CONTROL RIB AT RT WING 2024-78551<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS266 DEFLECTION CONTROL RIB AT RT WING IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 8 REV -;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS266 DEFLECTION CONTROL RIB AT RT WING IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 8 REV -

Part: WEB — CRACKED (RT WING TE) · airframe 57,072 hrs · 31,251 cycles

CRACK WEB TRAILING EDGE LOCATED ORSS266 DEFLECTION CONTROL RIB AT RT WING 2024-78552<[01] REPLACED WEB TRAILING EDGE LOCATED ORSS266 DEFLECTION CONTROL RIB AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02;[02] REPLACED WEB TRAILING EDGE LOCATED ORSS266 DEFLECTION CONTROL RIB AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02

Part: HOUSING — CORRODED (FUEL QTY IND) · airframe 57,072 hrs · 31,251 cycles

CORROSION INTERNAL CAVITY LEADING EDGE FUEL QUANTITY INDICATOR HOUSING RT WING 2024-78554<[01] REPLACED FUEL QUANTITY INDICATOR HOUSING RT WING IAW B737-700 SRM 51-40-02; TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED

Part: ANGLE — CRACKED (BS 663 RBL 41) · airframe 57,072 hrs · 31,251 cycles

CRACK ON ANGLE LOCATED BS663 AND RBL41. PERFORMED LEAK CHECK ON ANGLE IAW B737-700 AMM 28-11-00-790-80 NOT FOUND LEAK. CORRECTED STEP 2<BR>PERFORMED LEAK CHECK ON ANGLE LOCATED BS663 AND RBL41 WING CENTER SECTION IAW B737-700 AMM 28-11-00-790-801 NOT FOUND LEAK.;[04] CORRECTED STEP 3<BR>PERFORMED LEAK CHECK ON ANGLE LOCATED BS663 AND RBL41 WING CENTER SECTION IAW B737-700 AMM 28-11-00-790-801 NOT FOUND LEAK. SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPLACED ANGLE LOCATED BS663 AND RBL41 WING CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9; DRAWING 111A1000 SHEET 226 REV A AND DRAWING 111A1000 SHEET 190 REV?.

Part: ANGLE — CRACKED (RT WING TE) · airframe 57,072 hrs · 31,251 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS273 DEFLECTION CONTROL RIB AT RT WING 2024-78553<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS273 DEFLECTION CONTROL RIB AT RT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A6200 SHEET 11 REV B;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS273 DEFLECTION CONTROL RIB AT RT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A6200 SHEET 11 REV B

Part: BRACKET — CRACKED (RT WING TE) · airframe 57,072 hrs · 31,251 cycles

CRACK BRACKET TRAILING EDGE LOCATED AT LEVEL IRSS140 AT RT WING 2024-78556<[01] REPLACED BRACKET TRAILING EDGE LOCATED AT LEVEL IRSS140 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2000 SHEET 22 REV A.;[02] REPLACED BRACKET TRAILING EDGE LOCATED AT LEVEL IRSS140 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2000 SHEET 22 REV A.

Part: FLOOR SUPPORT — CRACKED (BS 380-400 RBL10) · airframe 57,072 hrs · 31,251 cycles

CRACK ON ANGLE FLOOR STRUCTURE LOCATED BTW BS 380 TO BS 400 RBL 10 AND WL 208 AT PASSENGER CABIN 2024-78499<[01] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED BTW BS 380 TO BS 400 RBL 10 AND WL 208 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A5400 SHEET: 38 REV: A . SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED BTW BS 380 TO BS 400 RBL 10 AND WL 208 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A5400 SHEET: 38 REV: A . SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOOR SUPPORT — CRACKED (BS 380-400 BL0) · airframe 57,072 hrs · 31,251 cycles

CRACK ON ANGLE FLOOR STRUCTURE LOCATED BTW BS 380 TO BS 400 BL0 AND WL 208 PASSENGER CABIN 2024-78495<[01] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED BTW BS 380 TO BS 400 BL0 AND WL 208 PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A5400 SHEET: 91 REV: - . SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED BTW BS 380 TO BS 400 BL0 AND WL 208 PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A5400 SHEET: 91 REV: - . SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOOR SUPPORT — CRACKED (BS 380-400 RBL41) · airframe 57,072 hrs · 31,251 cycles

CRACK ON ANGLE FLOOR STRUCTURE LOCATED BTW BS 380 TO BS 400 RBL 41 AND WL 208 AT PASSENGER CABIN 2024-78500<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; TEMPERATURE PID CTRL P/N 48YFL11 S/N AE-31448 DUE DATE 20 JUL 24.;[02] REPLACED ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 AND WL 208 AT PASSENGER CABIN I.A.W B737-700 SRM51-10-02 ITEM 9 AND DWG#138A5400 SHEET:38; REV:A SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOOR SUPPORT — CRACKED (BS 380-400 LBL13) · airframe 57,072 hrs · 31,251 cycles

CRACK ON ANGLE FLOOR STRUCTURE LOCATED BTW BS 380 TO BS 400 LBL 13 AND WL 208 AT PASSENGER CABIN 2024-78497<[01] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED BTW BS380 TO BS 400 LBL 13 AND WL 208 AT PASSENGER CABIN; IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 Ï¿½TEM 9; AND BOEING 737-700 DWG 143A5400 SHEET 38 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED BTW BS380 TO BS 400 LBL 13 AND WL 208 AT PASSENGER CABIN; IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 Ï¿½TEM 9; AND BOEING 737-700 DWG 143A5400 SHEET 38 REV A. SEE INDIVIDUAL SIGN OFF BELOW.

Part: PLATE — CRACKED (LT WING) · airframe 57,072 hrs · 31,251 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS215 AT LT WING 2024-78511<[01] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED AT LEVEL IRSS215 AT LT WING. IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2001 SHEET 36 REV - SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED AT LEVEL IRSS215 AT LT WING. IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2001 SHEET 36 REV - SEE INDIVIDUAL SIGN OFFS BELOW.JOB COMPLETED.

Part: ANGLE — CRACKED (LT WING TE) · airframe 57,072 hrs · 31,251 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS272 DEFECTION CONTROL RIB AT LT WING 2024-78515<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS272 DEFECTION CONTROL RIB AT LT WING IAW B737-700 SRM 51-10-02-0G PARAGRAPH 9; 51-40-02-0G-0 AND DWG 115A2930 SHEET 7 REV-.;[02] CORRECTED STEP 1 REPLACED ANGLE TRAILING EDGE LOCATED ORSS272 DEFECTION CONTROL RIB AT LT WING IAW B737-700 SRM 51-10-02-0G PARAGRAPH 9; 51-40-02-0G-0 AND DWG 115A2930 SHEET 7 REV-MEASURE OF CRACK 0.545 TOOL USED DIGITAL CALIPER P/N 500-752-20 S/N B21014945 DUE DATE 04-DEC-24.;[03] REPLACED ANGLE TRAILING EDGE LOCATED ORSS272 DEFECTION CONTROL RIB AT LT WING IAW B737-700 SRM 51-10-02-0G PARAGRAPH 9; 51-40-02-0G-0 AND DWG 115A2930 SHEET 7 REV-MEASURE OF CRACK 0.545 TOOL USED DIGITAL CALIPER P/N 500-752-20 S/N B21014945 DUE DATE 04-DEC-24.

Part: PLATE — CRACKED (LT WING) · airframe 57,072 hrs · 31,251 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS411 AT LT WING 2024-78509<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS411 AT LT WING IAW B737-700 SRM 51-10-02 AND DWG 115A3700 SHEET 43 REV A. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] COMPLETE TASK CERTIFIED

Part: SUPPORT ANGLE — CRACKED (BS 907-927) · airframe 57,072 hrs · 31,251 cycles

CRACK ANGLE - SUPPORT BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT 2024-78474<[01] REPLACED ANGLE- SUPPORT BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT IAW B737-700 51-10-02 AND DWG 147A7221 SHEET 24 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT CHANNEL — CORRODED (BS 767-795) · airframe 57,072 hrs · 31,251 cycles

CORROSION CHANNEL SUPPORT BETWEEN BS 767 TO BS 795 LEVEL STRINGER 25R AFT CARGO COMPARTMENT 2024-78473<[01] REPLACED CHANNEL SUPPORT AND FASTENERS LOC. BETWEEN BS 767 TO BS 795 LEVEL STRINGER 25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 146A0081; SHEET: 31; REV: ?. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED CHANNEL SUPPORT AND FASTENERS LOC. BETWEEN BS 767 TO BS 795 LEVEL STRINGER 25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 146A0081; SHEET: 31; REV: ?. <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SUPPORT — CORRODED (BS 727D-767) · airframe 57,072 hrs · 31,251 cycles

CORROSION SUPPORT ZEE BETWEEN BS 727D TO BS 767 AND RBL 21 AFT CARGO COMPARTMENT 2024-78472<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 24-JUL-24;[02] REPLACED SUPPORT ZEE BETWEEN BS 727D TO BS 767 AND RBL 21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-01 AND DWG 146A7502 SHEET 26 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT — CORRODED (BS 727A-807) · airframe 57,072 hrs · 31,251 cycles

CORROSION SUPPORT ZEE BETWEEN BS 727A TO BS 807 AND LBL 21 AFT CARGO COMPARTMENT 2024-78471. REPLACED SUPPORT ZEE LOC. BETWEEN BS 727 TO BS 847 AND LBL 21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 146A7502 SHEET 27 REV- .

Part: BRACKET — DETERIORATED (GIRT BAR) · airframe 57,072 hrs · 31,251 cycles

DETERIORATED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT FWD GALLEY AREA 2024-78436<[01] REPLACED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT FWD GALLEY AREA IAW BOEING SOPM-20-50-01 REV.38;[02] COMPLETED

Part: FLOOR SUPPORT — CRACKED (BS 695 BL0) · airframe 57,072 hrs · 31,251 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS695 AT LEVEL BL0 AT PASSENGER CABIN 2024-78439<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN-25. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 23-JAN-25.;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS695 AT LEVEL BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 DWG: 273A9110 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS695 AT LEVEL BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 DWG: 273A9110 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.

Part: GIRT BAR — DETERIORATED (PAX DOOR) · airframe 57,072 hrs · 31,251 cycles

DETERIORATED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT AFT GALLEY AREA 2024-78427<[01] REPLACED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT AFT GALLEY AREA IAW BOEING 737-700 AMM 25-66-02-400-801;[02] COMPLETE TASK CERTIFIED

Part: GIRT BAR — DETERIORATED (SERVICE DOOR) · airframe 57,072 hrs · 31,251 cycles

DETERIORATED SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT FWD GALLEY AREA 2024-78437<[01] REPLACED SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT FWD GALLEY AREA IAW BOEING SOPM-20-50-01 REV.38;[02] REPLACED SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT FWD GALLEY AREA IAW BOEING SOPM-20-50-01 REV.38

Part: BRACKET — DETERIORATED (GIRT BAR) · airframe 57,072 hrs · 31,251 cycles

DETERIORATED SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT AFT GALLEY AREA 2024-78428<[01] REPLACED SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT AFT GALLEY AREA IAW BOEING 737-700 AMM25-66-02-400-801;[02] COMPLETE TASK CERTIFIED

Part: SUPPORT ANGLE — CRACKED (BS 867 S2-3R) · airframe 57,072 hrs · 31,251 cycles

CRACK SUPPORT ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-78351<[01] REPLACED SUPPORT ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 STEP 9 AND DWG#146A7901 SHET:66 REV: A.;[02] CORRECTED STEP 1 REPLACED SUPPORT ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 STEP 9 AND DWG#146A7901 SHEET:66 REV: A.;[03] REPLACED SUPPORT ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 STEP 9 AND DWG#146A7901 SHEET:66 REV: A.

Part: SUPPORT ANGLE — CRACKED (BS 927-948) · airframe 57,072 hrs · 31,251 cycles

CRACK ANGLE - SUPPORT LOCATED BTW BS 927 TO BS 947.5 RBL 2 AT AFT GALLEY AREA 2024-78220 CRACK ANGLE - SUPPORT(CHORD) LOCATED BTW BS 927 TO BS 947.5 BL 0 AT AFT GALLEY AREA<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; TEMPERATURE PID CTRL P/N 48YFL11 S/N AE-31448 DUE DATE 20 JUL 24.;[02] REPLACED ANGLE SUPPORT(CHORD) LOCATED BTW BS 927 TO BS 947.5 BL 0 APPROX AT AFT GALLEY AREA I.A.W SRM 51-40-02-0G-0 AND DWG 147A5400 SHEET 22 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FITTING — DAMAGED (BS 1016) · airframe 57,072 hrs · 31,251 cycles

ELONGATED HOLE FITTING LOCATED BS 1016 UPPER AREA AT PASSENGER CABIN 2024-78318<[01] REPLACED FITTING LOCATED BS 1016 UPPER AREA AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING 148A2230 REV C SEE INDIVIDUALS SIGN OFF BELOW;[02] CORRECTED STEP 1; REPLACED FITTING LOCATED BS 1016 UPPER AREA AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING 148A2230 SHEET 8 REV C SEE INDIVIDUALS SIGN OFF BELOW;[03] REPLACED FITTING LOCATED BS 1016 UPPER AREA AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING 148A2230 SHEET 8 REV C SEE INDIVIDUALS SIGN OFF BELOW

Part: FLOORBEAM — CORRODED (BS 987 RBL 43) · airframe 57,072 hrs · 31,251 cycles

CORROSION ON HOLES FLOOR BEAN LOCATED BS 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA (3 POINTS ) 2024-78302<[01] TOOL USED ON STEP 6; THICKNESS GAGE; P/N: 45MG; S/N: 232017609; DUE DATE: 22-SEP-24.;[02] TOOL USED IN STEP 10: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21-JUL-24;[03] TOOL USED IN STEP 11: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21-JUL-24;[04] REPAIRED FLOOR BEAN LOCATED BS 986.5 BETWEEN RBL36 TO RBL47 WL 208.1 AT AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED FLOOR BEAN LOCATED BS 986.5 BETWEEN RBL36 TO RBL47 WL 208.1 AT AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII INSPECTED.

Part: LIGHT — DETERIORATED (CABIN) · airframe 57,072 hrs · 31,251 cycles

DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) 2024-78298<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW BOEING SOPM 20-50-12 REV. 56.;[02] COMPLETE TASK CERTIFIED

Part: FLOORBEAM — CORRODED (BS 986) · airframe 57,072 hrs · 31,251 cycles

CORROSION ON FLOOR BEAM LOCATED BS 986.5 RBL 8 WL 208.5 AT AFT GALLEY AREA 2024-78304<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN: 232017609; DUE DATE: 22-FEB-24;[02] TOOL USED IN STEPS 8 AND 9: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21-JUL-24;[03] PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE BEAM BS 986.5 BETWEEN RBL9 TO LBL1 WL 208.5 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFFS BELOW.;[04] RII COMPLETED JOB

Part: FLOOR SUPPORT — CRACKED (BS 344-360 LBL12) · airframe 57,072 hrs · 31,251 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 12 FWD GALLEY AND LAV 2024-78203<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOC. FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 12 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 141A5400 REV: A.;[02] CORRECTED STEP 1.<BR>REPLACED WEB - INTERCOSTAL AND FASTENERS LOC. FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 12 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 141A5400 REV: A. SEE INDIVIDUAL SIGNOFF BELOW.;[03] CORRECTED STEP 2.<BR>REPLACED WEB - INTERCOSTAL AND FASTENERS LOC. FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 12 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 141A5400; SHEET: 46; REV: A. SEE INDIVIDUAL SIGNOFF BELOW;[04] REPLACED WEB - INTERCOSTAL AND FASTENERS LOC. FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 12 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 141A5400; SHEET: 46; REV: A. SEE INDIVIDUAL SIGNOFF BELOW

Part: FLOORBEAM — CORRODED (BS 987 LBL 43) · airframe 57,072 hrs · 31,251 cycles

CORROSION FLOOR BEAM LOCATED BS 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2024-78225<[01] STEP 5 TOOL USED ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130066701; CAL DUE DATE: 09-JUN-24;[02] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 190023010. DUE DATE: 24-JUL-24.;[03] REPAIRED FLOOR BEAM LOCATED BS 986.5 BTW LBL36 TO LBL46 WL 208.1 AT AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED FLOOR BEAM LOCATED BS 986.5 BTW LBL36 TO LBL46 WL 208.1 AT AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII INSPECTED.

Part: FLOOR SUPPORT — CORRODED (BS 295-312) · airframe 57,072 hrs · 31,251 cycles

CORROSION WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 294.5 TO BS 312 LBL 12 WL 208.1 FWD GALLEY AND LAV 2024-78209<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS FLOOR STRUCTURE LOCATED BTW BS 294.5 TO BS 312 LBL 12 WL 208.1 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 141A5600 SHEET 1 AND 2 REV N.;[02] CORRECTED STEP 1 REPLACED WEB - INTERCOSTAL AND FASTENERS FLOOR STRUCTURE LOCATED BTW BS 294.5 TO BS 312 LBL 12 WL 208.1 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 141A5600 SHEET 1 AND 2 REV N SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED WEB - INTERCOSTAL AND FASTENERS FLOOR STRUCTURE LOCATED BTW BS 294.5 TO BS 312 LBL 12 WL 208.1 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 141A5600 SHEET 1 AND 2 REV N SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOOR SUPPORT — CRACKED (BS 344-360 BL0) · airframe 57,072 hrs · 31,251 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 BL 0 FWD GALLEY AND LAV 2024-78202<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEETS 32 REV -. SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLOORBEAM — CRACKED (BS 295 RBL 53) · airframe 57,072 hrs · 31,251 cycles

CRACK FLOOR BEAM 294.5 LOCATED RBL 53 WL 208.1 AT FWD GALLEY AREA. REPAIRED FLOOR BEAM BS 294.5 LOCATED RBL 16 RBL 60 WL 208.1 AT FWD GALLEY AREA I.A.W B737-700 SRM 53-10-51-2R-16 REPAIR 16.

Part: UNKNOWN — CRACKED (BS 304 LBL55) · airframe 57,072 hrs · 31,251 cycles

CRACK INNER CHORD LOCATED BS 303.9 LBL 55 AT FWD GALLEY AREA. REPLACED INNER CHORD LOCATED BS277 TO BS360 LBL 55 AT FWD GALLEY AREA. IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 PARAGRAPH 9 ;DWG 142A0050 SHEET 15 REV-.

Part: FLOOR SUPPORT — CRACKED (BS 277-295 BL0) · airframe 57,072 hrs · 31,251 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 BL 0 FWD GALLEY AND LAV 2024-78207<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 277 TO BS 294.5 BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 20 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 277 TO BS 294.5 BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 20 REV - SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOOR SUPPORT — CRACKED (BS 312-328 LBL46) · airframe 57,072 hrs · 31,251 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 LBL 46 FWD GALLEY AND LAV 2024-78206<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 312 TO BS 328 LBL 46 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 26 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 312 TO BS 328 LBL 46 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 26 REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOOR SUPPORT — CRACKED (BS 344-360 RBL33) · airframe 57,072 hrs · 31,251 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 33 FWD GALLEY AND LAV 2024-78204<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 33 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A5400 SHEET 33; REV -. SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 33 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A5400 SHEET 33; REV -. SEE INDIVIDUAL SIGNOFF BELOW

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 57,072 hrs · 31,251 cycles

(CUSTOMER REQUEST) CRACK ON VAPOR BARRIER WEB LOCATED ON RBL 45 AT WING CENTER SECTION 2024-78152<[01] TOOL USED: CALIPER P/N: 500-464 S/N:B17030933 DUE DATE: 07-NOV-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 25-JAN-25.;[03] TOOL USED. SCALE PN: CR5200; SN: 8343150722; DUE DATE: 13-FEB-24;[04] TOOL USED IN STEP 13: UT EQUIPMENT; P/N: EPOCH 650; S/N: 190859705; DUE DATE: 23-OCT-24;[05] REPAIRED VAPOR BARRIER WEB LOCATED ON RBL 45 AT WING CENTER SECTION IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] REPAIRED VAPOR BARRIER WEB LOCATED ON RBL 45 AT WING CENTER SECTION IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10 RII COMPLETED

Part: SCUFF PLATE — CRACKED (FWD DOOR SILL) · airframe 57,072 hrs · 31,251 cycles

CRACK ON SCUFF PLATE FWD SERVICE DOOR 2024-78078<[01] TOOL USED DIGITAL CALIPER P/N:500-752-20;S/N:B21015879;DUE DATE:14-JAN-25.;[02] TOOL USING RADIOMETER/PHOTOMETER P/N: XRP-3000; S/N: 1753759; DUE DATE: 12-APR-24;[03] REPAIRED SCUFF PLATE FWD SERVICE DOOR IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.REFER TO INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED SCUFF PLATE FWD SERVICE DOOR IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.REFER TO INDIVIDUAL SIGN OFF BELOW.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 57,072 hrs · 31,251 cycles

CRACK LEADING EDGE SKIN LOWER SURFACE SLAT 1 ACCTUATOR RIB SLAT STATION 451.97 AT LT WING 2024-78032<[01] TOOL USED ON STEP 5; EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N:210136503; DUE DATE: 23-MAY-24;[02] PERFORMED PERMANENT REPAIR ON LEADING EDGE SKIN LOWER SURFACE SLAT 1 IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8.SEE INDIVIDUAL SIGN OFF BELOW.;[03] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 57,072 hrs · 31,251 cycles

INOP EMERGENCY LIGHT ASSY OVERHEAD STOWAGE BIN 5 LH AT PASSENGER CABIN. REPLACED EMERGENCY LIGHT ASSY OVERHEAD STOWAGE BIN 5 LH AT PASSENGER CABIN IAW B737-700 AMM 33-51-03-960-802. TESTED OK.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,321 hrs · 30,786 cycles

FWD ENTRY DOOR EMERGENCY LIGHTS INOP.<[01] REPLACED EMERGENCY LIGHTS POWER SUPPLY BATTERY PACK FOR FWD. ENTRY DOOR IAW AMM 33-51-06.

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 56,321 hrs · 30,786 cycles

FOUND FWD ENTERY LOWER EMERGENCY EXIT SIGN LENS BROKEN.<[01] REMOVED AND REPLACED FWD ENTERY LOWER EMERGENCY EXIT SIGN LENS IAW AMM 33-51-01.

Part: SEAT BACK — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 55,888 hrs · 30,527 cycles

11D RECLINE NEEDS TO BE DISABLED FOR EMERGENCY ROW.<[01] DISABLED 11D SEAT RECLINE IAW CMM 25-21-42

Part: HANDLE — LOOSE (ZN 800 DOOR) · airframe 55,888 hrs · 30,527 cycles

L1 DOOR BOTH ASSIST HANDLES LOOSE.<[01] RESECURED BOTH L1 ASSIST HANDLES IAW AMM 52-11-31.

Part: LIGHT — INOPERATIVE · airframe 52,074 hrs · 28,006 cycles

AFT ENTRY CEILING EMERGENCY EXIT SIGN INOP. / [01] RELAMPED AFT ENTRY CEILING EMERGENCY EXIT SIGN AS PER REF B737 AMM 33-51-01-960-801 LIGHTS TEST OK;[02] VERIFIED STEP 1

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 52,074 hrs · 28,006 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. / [01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER B737 AMM 33-51-04-960-801. TEST OK;[02] VERIFIED STEP 1.

Part: BATTERY PACK — INOPERATIVE · airframe 52,074 hrs · 28,006 cycles

EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1670 INOP. / [01] REMOVED & REPLACED EMERGENCY LIGHT AT BATTERY PACK M1670 AS PER REF B737 AMM 33-51-06-960-805 AND PERFORMED OPERATIONAL TEST . TEST PASS;[02] VERIFIED STEP 1.

Part: SPOILER — DELAMINATED (R/H WING) · airframe 52,074 hrs · 28,006 cycles

SPOILER #7 HAS DELAMINATION AT O/B FWD CORNER UPPER SURFACE APRX. 8'X5'. / [01] REMOVED #7 GROUND SPOILER PANEL REFERENCE AMM 27-62-12-000-801.;[02] VERIFIED STEP 1. OK TO INSTALL SERVICEABLE GROUND SPOILER PANEL.;[03] REPLACED #7 GROUND SPOILER PANEL REFERENCE AMM 27-62-12-400-801. PENDING ADJUSTMENT AND TEST. TORQUE WRENCH B/C 16671.;[04] VERIFIED STEP 3.;[05] ACCOMPLISHED #7 GROUND SPOILER ADJUSTMENT REFERENCE AMM 27-62-00-820-804. TORQUE WRENCH B/C 166742.;[06] VERIFIED STEP 5.;[07] ACCOMPLISHED INBOARD #7 GROUND SPOILER FUNCTIONAL TEST REFERENCE AMM 27-62-12-000-802. CHECKED NORMAL.;[08] VERIFIED STEP 7.

Part: ANGLE — CRACKED (RH HOR STAB) · airframe 52,074 hrs · 28,006 cycles

FOUND 1EACH ANGLE - STOP CRACKED LENGH .750' AT RT HORIZ.STAB. I/B BALANCE PANEL BETWEEN EL STA. 39.02 THRU EL STA 66.54 / [01] REMOVED AND REPLACED BRACKET (ANGLE - STOP AT RT HORIZ. STAB. I/B BALANCE PANEL EL STA 39.02 THRU EL SRA 66.54 PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED BRACKET REPLACEMENT.

Part: LENS — DAMAGED · airframe 52,074 hrs · 28,006 cycles

EXIT SIGN LENS IS DAMAGED AT G-1. / [01] REMOVED AND REPLACED EXIT SIGN LENS AT G-1 IAW B737-700 AMM 33-51-01-960-801.;[02] VERIFIED LENS REPLACEMENT.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 52,074 hrs · 28,006 cycles

R2 DOOR INNER LOWER PAN ASSY AFT INNER BRACKET WITH CRACK APROX. .750'. REMOVED R2 DOOR LOWER PAN ASSY FOR ACCESS TO REPLACE BRACKET PER B737-700 SRM 51-40-02-0G-0.REMOVED CRACKED BRACKET FROM R2 DOOR LOWER PAN ASSY PER B737-700 SRM 51-40-02-0G-0.LOCATED AND DRILLED NEW BRACKET P/N 411A2129-320 PER B737-700 SRM 51-10-02-0G-0; TREATED; PRIMED AND PAINTED NEW BRACKET PER B737-700 SRM 51-20-01-0G-0; AMM 51-21-72-370-804 AND AMM 51-21-73-370-803. INSTALLED NEW BRACKET AT R2 DOOR AFT INNER PAN ASSY. PER B737-700 SRM 51-40-02-0G-0 AND DRAWING #411A2119; INSTALLED R2 LOWER PAN ASSY REMOVED ON STEP #1 PER B737-700 SRM 51-40-02-0G-0;

Part: SUPPORT BRACKET — CRACKED · airframe 52,074 hrs · 28,006 cycles

WATER SEPARATOR ROD SUPPORT BRACKET CRACKED AT R/H KEEL BEAM AREA STA 560 RBL7 / REMOVED PANEL #192E TO GAIN ACCESS FOR BRACKET REMVAL PER B737-700 AMM 53-51-21-000-802. REMOVED CRACKED BRACKET PER B737-700 SRM 51-40-02-0G-0. FABRICATED BRACKET P/N 213A9440-31 PER DRAWING 213A9440 BY OUTSIDE VENDOR PO#1771822. MATERIAL USED 7050 T7451 PO#1769469. VERIFIED BRACKET FABRICATION.OK TO APPLIED PRIMER. PRIMED NEW BRACKET PER B737-700 AMM 51-21-72-370-804. INSTALLED NEW BRACKET PER B737-700 SRM 51-40-02-0G-0 AND DRWG #144A7110. VERIFIED BRACKET INSTALLATION. OK TO INSTALL ACCESS PANELS #192E. INSTALLED ACCESS PANEL #192E PER B737-7200 AMM 53-51-21-400-802.

Part: SHIELD — CRACKED (FWD CARGO) · airframe 52,074 hrs · 28,006 cycles

FWD CARGO COMP. AFT SHIELD BETW. STA 492.4 THRU STA 500A STR 25R RBL 25 HAS .750' CRACK AT LOWER AREA / [01] REPLACED FWD CARGO COMP. AFT SHIELD BETWEEN STA 492.4 THRU STA 500A STR 25R RBL 25 REF. B737-700 SRM 51-40-02-0G-0. SHIELD WILL BE INSTALLED ON FWD CARGO MOC. CARD #TTG8Q004F9KZ;[02] VERIFIED REPLACEMENT AND TTG8Q004F9KZ.

Part: ANGLE — CRACKED (AFT CARGO) · airframe 52,074 hrs · 28,006 cycles

AFT OF AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE AFT END SUPPORT FITTING CRACKED @ END RADIUS AREA S-26L STA 947.5 MKD DOT 002 / [01] REMOVED ANGLE FITTING CRACKED AT AFT CARGO STA 947.5 LBL 21 AS PER REF B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW FITTING P/N 149A8113U6 AS PER REF B737-700 SRM 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2. OK TO INSTALL NEW FITTING.;[04] INSTALLED NEW FITTING AT AFT CARGO STA 947.5 LBL 21 AS PER REF B737-700 SRM 51-40-02-0G-0 AND DWG # 149A8103;[05] VERIFIED STEP 4.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 52,074 hrs · 28,006 cycles

CORROSION FOUND AFT CARGO DOOR CUTOUT FWD SHIELD HAS SPOTS OF CORROSION. / [01] REMOVED CORROSION FROM AFT CARGO CUTOUT FWD SHIELD AS PER REFERENCE B737-700 SRM 51-10-02-0G-0.;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.021' <BR>TOOL USED : OLYMPUS 27MG B/C 172139 CAL DUE:04/23;[04] EVALUATED REWORKED AREA. ORIGINAL THICKNESS .050' MATERIAL LOST .029' REMAINING THICKNESS .021'. OUT OF LIMITS AS PER REFERENCE B737-700 SRM 53-60-15-1A-1;[05] LOCATED AND DRILLED NEW SHIELD P/N 146A8127U12 AS PER REF B737-700 SRM 51-40-05-0G-0. THE NEW SHIELD WILL BE INSTALLED IN ITEM TTG8Q004EJYR;[06] VERIFIED STEP 5.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 52,074 hrs · 28,006 cycles

FWD CARGO FLOOR PANEL # 120BF HAS CORROSION AT FWD RH CORNER AREA. / [01] SMOOTH OUT AREA ON FWD CARGO FLOOR PANEL #120BF PER B737-700 SRM 51-10-02-0G-0;[02] VERIFIED CORROSION REMOVAL.;[03] AFTER CORROSION REMOVAL FOUND OUT OF LIMITS DUE TO LENGTH OF DAMAGE PER B737-700 SRM 53-00-53-1A-1;[04] CERTIFIED;[05] REPLACED FWD CARGO COMP. FLOOR PANEL #120BF REF. B737-700 AMM #25-52-10-400-801. FLOOR PANEL #120BF WILL BE INSTYALLED ON CARD #TTG8Q00BLQJ2;[06] VERIFIED STEP 5.

Part: FRAME — CRACKED (L1 DOOR) · airframe 52,074 hrs · 28,006 cycles

CRACK FOUND ON STA 312 ABOVE L1 DOOR CUTOUT. / TRIMMED OUT THE DAMAGED AREA OF THE UPPER CHORD AT STA 312 AS SHOWN IN FIGURE 202. DAMAGE REMOVAL LIMITS AS PER REFERENCE B737-700 SRM 53-10-07-2R-1. REMOVED FASTENERS FROM UPPER CHORD STA 312 BETWEEN S-5L AND S-6L TO GET ACCESS AS PER REFERENCE B737-700 SRM 51-40-02-0G-0.FABRICATED ANGLE REPAIR AS PER REF B737-700 SRM 53-10-07-2R-1 TABLE 201. BAC 5602; ACCOMPLISHED HEAT TREATMENT AT FABRICATED ANGLE AS PER REF B737-700 SRM 53-10-07-2R-1 TABLE 201. BAC 5602; NO CRACKS LOCATED AND DRILLED FABRICATED ANGLE AS PER REF B737-700 SRM 51-40-05-0G-0;TREATED AND PRIMED FABRICATED PART AS PER REF B737-700 SOPM 20-43-03 AND SOPM 20-41-02;TREATED AND PRIMED BARE SURFACE OF THE REPAIR AREA AS PER REF B737-700 SOPM 20-43-03 AND SOPM 20-41-02 INSTALLED FABRICATED ANGLE AT STA 312 ABOVE L1 DOOR CUTOUT AS PER REF SRM 53-10-07-2R-1

Part: RIB — CRACKED (RH HOR STAB) · airframe 52,074 hrs · 28,006 cycles

RH HORIZONTAL STABILIZER RIB# 5 STIFFENER 4 CRACK. CUT OUT DAMAGED AREA FROM VERTICAL STIFFENER PER B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG. 202.CUT OUT DAMAGED AREA AT WEB PER B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG. 202. PERFORMED HFEC AT CUT OUT IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS PERFORMED HFEC HOLE PROBE INSPECTION ON ALL REMOVED FASTENER LOCATIONS WITHIN REPAIR AREA IAW NDTM PART 6; 51-00-00; PROCEDURE 16. NO CRACKS. ACCOMPLISHED A GENERAL VISUAL INSPECTION OF REWORKED AREAS. NO DEFECTS NOTED.TREATED AND PRIMED REPAIR PARTS AND REWORKED AREA PER B737-700 SRM 51-20-01-0G-0 AND AMM 51-21-72-370-8O4. INSTALLED REPAIR PARTS AT R/H HORIZ. STAB. RIB #5 STIFFENER 4 PER B737-700 SRM 55-10-09-2R-4 FIG. 202 DETAIL A.

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 52,074 hrs · 28,006 cycles

FWD CARGO SIDEWALL GUSSET ANGLE AT S-19R AND STA 500 CRACKED / [01] REMOVED FWD CARGO SIDEWALL GUSSET ANGLE AT S-19R AND STA 500D AS REF SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW GUSSET P/N 143A9481-5 PER B737-700 SRM 51-10-02-0G-0;[03] VERIFIED DRILLING.<BR>OK TO INSTALL NEW GUSSET.;[04] INSTALLED NEW GUSSET AT S-19R AND STA 500D AS REF SRM 51-40-02-0G-0 AND DRWG #143A7902;[05] VERIFIED STEP 4.

Part: RIB — CRACKED (VERT. STAB.) · airframe 52,074 hrs · 28,006 cycles

DORSAL FIN PANEL 321A FWD FITTING CRACK. DORSAL FIN PANEL 321A FWD RIB CRACK / [01] REMOVED DORSAL FIN 321A FWD RIB AS PER REF B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW RIB P/N 174A1108 AS PER REF B 737-700 SRM 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2. OK TO INSTALL NEW RIB.;[04] INSTALLED NEW RIB AT DORSAL FIN PANEL 321A AS PER REF B737-700 SRM 51-40-02-0G-0 AND DWG #174A1008;[05] VERIFIED STEP 4.

Part: BRACKET — CRACKED (R/H WING) · airframe 52,074 hrs · 28,006 cycles

RH WING T/E DEFLECTION CONTROL PANEL AFT SEAL RETAINER BRACKET CRACK. / [01] REMOVED AND REPLACE RIGHT WING T/E DEFLECTION CONTROL PANEL AFT SEAL RETAINER (BULKHEAD) PER B737-700 SRM 51-40-02-0G-0 (PERFORMED BY MAGNO SOLANO #1934);[02] VERIFIED REPLACEMENT.

Part: CAP — CRACKED (AFT CARGO BAY) · airframe 52,074 hrs · 28,006 cycles

AFT CARGO COMP. RT SIDE CAPSTRIP BETWEEN STA 727D THRU STA 807 RBL 25 WITH 1' CRACK / [01] REPLACED AFT CARGO COMP. RT SIDE BETW. STA 727D THRU 807 CAPSTRIP REF. B737-700 AMM 25-52-10-400-801. THIS CAPSTRIP WILL BE INSTALLED ON AFT CARGO COMP. MOC CARD #TTG8Q004EJYR;[02] VERIFIED STEP #1.

Part: GAUGE — ERRATIC (COCKPIT) · airframe 51,763 hrs · 27,803 cycles

RAPUID FUEL IMBALANCE ON CLIMB. IMBALANCE APPROX. 800# BY APPROX. 12;000'. QRH/CROSSFEED REGAINED BALANCE; AND GAUGES OPERATED NORMALLY REST OF FLIGHT. / [01] PERFORMED FIM 28-41 TAKS 801 NO DEFECTS FOUND; OK FOR SERVICE.

Part: SENSOR — FAULTY (LT FLAP SKEW) · airframe 50,620 hrs · 27,096 cycles

TRAILING EDGE FLAP DISAGREE FLAP SELECTED 1 LEFT INDICATED 0.5 RIGHT INDICATED 0 NO HARD LANDING ; / [01] TROUBLESHOT PER FIM 27-59 TASK 802 FOUND MECHANICAL RIG WITHIN LIMITS SUSPECTED #2 T/E FLAP SKEW SENSOR BAD R/R PER AMM 27-59-01 OPS C.K GOOD

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 50,501 hrs · 27,021 cycles

FA REPORTS FWD SERVICE DOOR SLIDE APRON IS EXCESSIVELY LONG AND GETTING HUNG UP ; / [01] RESECURED LOOSE GIRT BAR PER SIP; SERVICE SLIDE APRON MOVES FREELY AS REQUIRED

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 49,276 hrs · 26,313 cycles

LEFT HORIZONTAL STABILIZER TO BODY UPPER SLIDING SEAL IS CRACKED. ; / REMOVED & REPLACED L/H UPPER SLIDING SEAL PER AMM 53-31-31; REMOVED & REPLACED L/H UPPER SLIDING SEAL PER AMM 53-31-31

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 49,276 hrs · 26,313 cycles

RIGHT HORIZONTAL STABILIZER TO BODY UPPER SLIDING SEAL IS CRACKED. ; / R AND R SLIDING SEAL PER M/M REF 53-31-31; R AND R SLIDING SEAL PER M/M REF 53-31-31

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 48,555 hrs · 25,913 cycles

R2 EXTERIOR EMERGENCY LIGHT INOP RELAMP NO HELP. / CLOSING DMA #0708517 R & R BATTERY PACK AT M1672. OP'S CK'S GOOD IAW AMM 33-51-06 CL #71254

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,299 hrs · 25,754 cycles

FWD GALLEY EMERGENCY LIGHTS INOPERABLE. R & R EMERGENCY BATT PACK, PER AMM 33-51-06.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,208 hrs · 25,697 cycles

EXTERNAL EMERGENCY LIGHT BY R2 DOOR INOPERABLE. RELAMPED IAW AMM 33-51-04. OPERATIONS CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,159 hrs · 25,670 cycles

DENT WITH GOUGE ON FUSELAGE SKIN AT STATION 747+3 BELOW STRINGER 19L. OUT OF LIMITS, PER SRM 53-00-01-1A-1. REPAIRED DAMAGE AT STA 747+3, PER EA 20-153-02572 AND SRM 53-00-01-2R-3 REPAIR 3. THIS IS A CATEGORY B REPAIR WHERE DOUBLER EXTENDS FARTHER THAN ADJACENT STRINGER.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,010 hrs · 24,947 cycles

EXTERIOR EMERGENCY EXIT LIGHT INOP AT AFT ENTRY DOOR (L2). RELAMPED L2 EXTERIOR EMERGENCY EXIT LIGHT IAW AMM REF 33-51-04.

Part: SEAT — LOOSE (ROW 1ABC) · airframe 46,989 hrs · 24,936 cycles

SEAT ROW 1ABC LOOSE IN TRACK / TIGHTENED DOWN SEAT ROW 1ABC IN TRACK PER AMM 25-22-00.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 46,865 hrs · 24,857 cycles

FORWARD SERVICE DOOR ESCAPE SLIDE IS PACKET IMPROPERLY. REPACKED FWD SERVICE DOOR ESCAPE SLIDE, ACCOMPLISHED ON MT CARD NR 725-61-06SF.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,865 hrs · 24,857 cycles

RIGHT OVERWING EXIT EMERGENCY LIGHT AT LWR FWD CORNER, 1 EA BULB INOPERATIVE. RELAMPED RT OVERWING EXIT EMERGENCY LIGHT AT LWR FWD CORNER AND PERFORMED A GOOD FUNCTIONAL TEST IAW AMM 33-51-01-960-801.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,865 hrs · 24,857 cycles

EXIT LOCATOR AT LT OVERWING DOOR HAS A BURNED OUT BULB. RELAMPED EXIT LOCATOR AT LT OVERWING DOOR AND PERFORMED A GOOD FUNCTIONAL CHECK PER AMM 33-51-01-960-801.

Part: FRAME — CHAFED (FUSELAGE) · airframe 46,865 hrs · 24,857 cycles

LOWER WTB FAIRING FORMER BELOW LT MLG W/W FOUND TO BE CHAFED BS 663-673 LBL 25 WL 145. RECEIVED NEW FRAME P/N 149A7214-19 FROM STORES; REF PO 778662. REMOVED LOWER WTB FAIRING FORMER BELOW LT MLG WW HAS CHAFE DAMAGE. LOCATED AT BS663-673; LBL25; WL145 IAW SRM 51-40-02 LOCATED AND DRILLED NEW PART IAW SRM 51-40-05. INSTALLED FAIRING FORMER PER SRM 51-40-02 AND DWG 149A7216.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 46,865 hrs · 24,857 cycles

BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 39 WL 150. REMOVED AND INSTALLED REPAIRED 663 LWR COMPOSITE BULKHEAD THAT WAS CRACKED ALL IN ACCORDANCE WITH SRM-51-40-03 AMM-53-51-21-000-802; 53-51-21-00-803; DWGS-111A1001 SHT-378; 111A7000 SHT-42; 111A1000 SHT-226; 144A7100 SHT-76 AND 111A1151 SHT-5.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 46,865 hrs · 24,857 cycles

BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 39 WL 150. LOWER COMPOSITE BULKHEAD BS663 CRACK AT LBL39 WL150 WAS REPAIRED IAW SRM 51-70-04-2R-10.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 46,865 hrs · 24,857 cycles

AFT CARGO COMPARTMENT- DAMAGED FLOOR PNL #140BF. / FABRICATED NEW ACB FLOOR PANEL 140BF FROM 071 2024T3; LOT# 1430776-1 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 46,865 hrs · 24,857 cycles

AFT CARGO COMPARTMENT- DAMAGED FLOOR PNL #140CF. / FABRICATED NEW ACB FLOOR PANEL 140CF FROM 071 2024T5; LOT#1430776-1 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 46,865 hrs · 24,857 cycles

AFT CARGO COMPARTMENT- DAMAGED FLOOR PNL #140DF. / FABRICATED NEW ACB FLOOR PANEL 140DF FROM 071 2024T3; LOT# 143A299-1 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 46,865 hrs · 24,857 cycles

FWD CARGO BAY FLOOR PNL# 120CF IS DAMAGED / FABRICATED NEW FCB FLOOR PANEL 120CF FROM 071 2024T3; LOT# 143A299-1 PER AMM 25-52-01-201-801 AND DWG 453A1610

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 46,865 hrs · 24,857 cycles

AFT CARGO COMPARTMENT- DAMAGED FLOOR PNL #140AF. / FABRICATED NEW ACB FLOOR PANEL 140AF FROM 071 2024T3; LOT# 1430776-1 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: VAPOR BARRIER — CRACKED (L/H MLG W/W) · airframe 45,248 hrs · 23,835 cycles

8' CRACK IN L/H WHEEL WELL VAPOR BARRIER AT LBL 40.0 / ACCOMPLISHED INTERIM REPAIR IAW SRM 57-10-10-1A-2.

Part: PANEL — ELONGATED (LOWER EXT FUSELA) · airframe 45,075 hrs · 23,727 cycles

WING TO BODY FAIRING PANEL 193B HAS ENLARGE FASTNER HOLES AT LOCATIONS 1-4; 6; 8-10; 13-15; 21 & 24-38 / REMOVED AND REPLACED PNL 193B REF AMM 53-51-21

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 45,075 hrs · 23,727 cycles

OVER R2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. / R&R LENS PER SIP.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 44,353 hrs · 23,276 cycles

L/H WHEEL WELL FORWARD BULKHEAD VAPOR BARRIER CRACKED AT LBL 40.0 10" FROM THE BOTTOM EDGE OF THE BARRIER. / REPAIRED BARRIER PER EA & SRM.

Part: BATTERY PACK — WEAK (CABIN) · airframe 43,999 hrs · 23,058 cycles

BATTERY PACK LOW OUTPUT. R&R BATTERY PACK PER AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 43,127 hrs · 22,505 cycles

R1 DOOR SLIDE OUT OF ADJUST. REPACKED SLIDE PER MT.

Part: RETAINING CLIP — LOOSE (R2 DOOR) · airframe 42,490 hrs · 22,079 cycles

R2 DOOR GIRT BAR RETAINING CLIP LOOSE. ADJUSTED CLIP PER SIP.

Part: COVER — BROKEN (EXIT SIGN) · airframe 41,811 hrs · 21,646 cycles

LT OVERWING EGRESS DIRECTIONAL ARROW SIGN COVER BROKEN. R&R COVER PER SIP.

Part: LENS — BROKEN (CABIN) · airframe 41,002 hrs · 21,124 cycles

RT OVERWING EXIT LIGHT LENS BROKEN. R&R LENS PER MM.

Part: SIGN — MISSING (L1 DOOR) · airframe 40,681 hrs · 20,909 cycles

L1 DOOR EXIT SIGN MISSING RED ARROW. R&R SIGN PER CMM.

Part: LENS — FADED (CABIN) · airframe 40,671 hrs · 20,903 cycles

RT EMERGENCY DOOR OVERHEAD LIGHT LENS FADED. R&R LENS PER AMM.

Part: LENS — FADED (CABIN) · airframe 40,671 hrs · 20,903 cycles

LT EMERGENCY DOOR OVERHEAD LIGHT LENS FADED. R&R COVER PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,563 hrs · 20,844 cycles

FORWARD ENTRYWAY EMERGENCY LIGHT BULB INOP ON FORWARD LAV. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,563 hrs · 20,844 cycles

RT EMERGENCY EXIT LIGHTS FORWARD OF OVERWING EXIT ON SIDEWALL BULB INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,563 hrs · 20,844 cycles

LT EMERGENCY EXIT LIGHTS FORWARD OF OVERWING EXIT ON SIDEWALL BULB INOP. RELAMPED LIGHT PER AMM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 40,563 hrs · 20,844 cycles

EMERGENCY LIGHT ON G4 BULB INOP. R&R FUSE PER MM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 40,563 hrs · 20,843 cycles

FORWARD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / REPLACED FCB. AFT CORNER SCUFF PLATE P/N 654A0004-338 P.O. NO 685207/13. IAW. IPC. 53-13-00-08 AND DWG 143A8330 INSTALLATION WILL BE ACCOMPLISH ON CUSTOMER CARD. NBR. 753-140-00-01Y

Part: ANGLE — CORRODED (FUSELAGE) · airframe 40,563 hrs · 20,843 cycles

AFT CARGO SIDEWALL TO BULKHEAD ANGLE CORRODED AT BS 947, RBL 18. R&R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (AFT CARGO BAY) · airframe 40,563 hrs · 20,843 cycles

STANCHION ATTACH ANGLE IS CRACKED AT BS 866 LBL 10 WL 166. / LOCATED AND DRILLED STANCHION ATTACH ANGLE AT BS 866 LBL 10 WL 166 IAW DWG. # 149A8109 DWG. # 149A8102 AND AIPC 53-42-51-06. OK TO INSTALL 93016C 06/21/18 INSP 357 6/21/18 INSTALLED STANCHION ATTACH ANGLE AT BS 866 LBL 10 WL 166 IAW SRM 51-40-02-0G-0 AND AIPC 53-42-51-06.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,563 hrs · 20,843 cycles

INTERCOSTAL SUPPORT CORRODED BETWEEN BS 300 TO BS 355, STR 23L. REPAIRED SUPPORT PER EA.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 40,563 hrs · 20,843 cycles

FWD SERVICE DOOR #4 BEAM IS CRACKED AT I/B SIDE OF RADIUS. / FWD SERVICE DOOR #4 BEAM WAS REMOVED & REPLACED ON WORK ORDER # 507267. 8931U 18JUN18 ADDITIONAL WORK WILL BE ACCOMPLISHED ON CUSTOMER CARD: T790509

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 40,563 hrs · 20,843 cycles

LT HORIZONTAL STAB INSPAR RIB AT STAB STA. 120.3 IS CRACKED AT THE 2ND VERTICAL STIFFENER ON LOWER END / TRIMMED CRACK OUT 1' X 0.334'; NDI NO DEFECTS NOTED; REPAIRED IAW SRM 55-10-09-2R-4; LH. H. STAB RIB STA 120.3 #2 STIFFENER

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 40,563 hrs · 20,843 cycles

LT HORIZONTAL STAB INSPAR RIB AT STAB STA. 120.3 IS CRACKED AT THE 3RD VERTICAL STIFFENER AT THE LOWER END / TRIMMED CRACK OUT 1' X 0.334'; NDI NO DEFECTS NOTED; REPAIRED IAW SRM 55-10-04-2R-4; LH H. STAB RIB STA 120.3 #3 SIFFENER

Part: SPLICE PLATE — CORRODED (AFT CARGO BAY) · airframe 40,563 hrs · 20,843 cycles

***CORROSION*** ACB FLOOR SPLICE PLATE HAS CORROSION B.S.887; RBL21; WL156. / ACB. FLOOR SPLICE.PLATE.WITH CORROSION.ON BS 887; RBL 21; WL 156. NO ALLOWABLE DAMAGE. FOUND ON SRM. FOUND TO BE. OUT OF LIMITS AND REPLACED. IAW SRM 51-10-02-0G-0 PAR 9. REMOVED FABRICATED AND INSTALLED NEW. FLOORSPLICE.PLATE.ON ACB AT BS 887 IAW.SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG. 146A7500

Part: RIB — CORRODED (LT HORIZ STAB) · airframe 40,563 hrs · 20,843 cycles

LT HORIZONTAL STAB INSPAR RIB AT STAB STA. 120.3 IS CRACKED AT THE 4TH VERTICAL STIFFENER AT THE LOWER END / TRIMMED CRACK OUT 1' X 0.334'; NDI NO DEFECTS NOTED; REPAIRED IAW SRM 55-10-09-2R-4; LH H. STAB. RIB STA 120.3 #4 STIFFENER

Part: CAP SEAL — CORRODED (AFT CARGO BAY) · airframe 40,563 hrs · 20,843 cycles

***CORROSION*** ACB FLOOR TO SIDEWALL SUPPORT HAS CORROSION B.S.867-947; RBL22; WL156. / REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT B.S 867-887 IAW 146A7501 AWD SRM 51-40-02 FLOOR TO SIDE WALL SUPPORT B.S. 887-B.S.947 & DWG 147A7902 AND DWG 147A7500 SRM 51-40-02

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 40,563 hrs · 20,843 cycles

SEAT TRACK SUPPORT CORRODED UNDERNEATH UPPER FLANGE STA 500D-520 LBL 24.75 / REMOVED AND REPLACED SEAT TRACK BS 480-520 LBL 25 IAW ATS ER# 18-03061 REV IR AND EA# 1-753-32858 REV IR

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 40,563 hrs · 20,843 cycles

FLOOR SUPPORT BROKEN AT BS 540, LBL 1. R&R SUPPORT PER SRM.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 40,563 hrs · 20,843 cycles

RUDDER COUNTER BALANCE WEIGHT IS CORRODED / REMOVED AND REPLACED; WITH SERVICABLE PART; RUDDER COUNTER BALANCE WEIGHT IAW CMM 55-40-09 PG 703 PAR (3)(A) AND SRM 51-60-07-0G-0 PG 9 OF 41 STEP (11)(C)2)D)

Part: SUPPORT ANGLE — CORRODED (MAIN CABIN) · airframe 40,563 hrs · 20,843 cycles

***CORROSION*** L.H. OVER WING EXIT LOWER SILL SIDEWALL 'FLAPPER' SUPPORT ANGLE; CENTER ATTACH POINT / REMOVED; FABRICATED AND INSTALLED NEW LH OVER WING EXIT LOWER SILL SIDEWALL FLAPPER SUPPORT ANGLE (STOP ASSY-SILL) PER SRM 51-40-02 AND DWG 411A2854

Part: SKIN — CORRODED (LWR FUSELAGE) · airframe 40,563 hrs · 20,843 cycles

***CORROSION*** CORROSION ON EXTERNAL FUSELAGE SKIN AT AREA COMMON TO FCB SCUFF PLATES BS 440 TO BS 480 +12 BETWEEN STR 24R AND 25R (MARKED) / REPAIRED PER EA 1-753-32934 REV IR AND ER 18-03093 REV IR.

Part: RETAINER SEAL — CRACKED (LT WING) · airframe 40,563 hrs · 20,843 cycles

(LEFT WING) COVE SEAL RETAINER CRACKED ABOVE #1 PYLON AFT TIP / REMOVED AND REPLACED (LEFT WING) COVE SEAL RETAINER ABOVE #1 PYLON AFT TIP P/N. 115A2953-1 IAW. AIPC 57-50-00-25 AND SRM 51-40-02. 88920U 10JUN18

Part: RETAINER SEAL — CRACKED (RT WING) · airframe 40,563 hrs · 20,843 cycles

(RIGHT WING) T/E COVE SEAL RETAINER CRACKED ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED (RIGHT WING) T/E COVE SEAL RETAINER ABOVE # PYLON AFT TIP P/N. 115A2953-2 IAW. AIPC 57-50-00-25 AND SRM 51-40-02. 88920U 10JUN18

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 40,563 hrs · 20,843 cycles

***CORROSION*** NOTED ON AFT CABIN FLOOR STRAP (BS 1016 / RBL 17.5 / WL 207.5). / CORROSION ON AFT CABIN FLOOR STRAP AT BS 1016 RBL 17.5 WL 207.5 WAS REMOVED; INSPECTED AND REPAIRED IAW EA 1-753-32831 REV IR AND ER 18-02960 REV IR (ORIGINAL ATTACHED CARD T790308

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · airframe 40,563 hrs · 20,843 cycles

***CORROSION*** CORROSION ON FWD CABIN FLOOR SUPPORT AT BS 312; LBL 55; WL 208 (MARKED) / REMOVED AND REPLACED FWD CABIN FLOOR SUPPORT AT BS 312; LBL 55; WL 208 WITH ITEM #141A5220-2 IAW SRM 51-40-02-0G-0 AND AIPC 53-42-00-29.

Part: WEB — CORRODED (MAIN CABIN) · airframe 40,563 hrs · 20,843 cycles

***CORROSION*** NOTED ON AFT CABIN FLOOR WEB ASSEMBLY (BS 1020 / RBL 15 / WL 207.5). / CORROSION ON AFT CABIN FLOOR WEB ASSEMBLY AT BS 1020; RBK 15 WL 207.5 WAS REMOVED; INSPECTED AND REPAIRED IAW 1-753-32831 REV IR AND ER 18-02960 REV IR

Part: FLOOR PANEL — BROKEN (AFT CABIN) · airframe 40,563 hrs · 20,843 cycles

AFT CABIN FLOOR PANEL 242WF IS BROKEN / DUE TO THE EXTENT OF DAMAGE ON PANEL 242 WF; REPLACED WITH NEW PANEL IAW SRM 51-10-02-0G-0 PAR 9 AND AIPC 53-21-00-36B; D3 TECHNOLOGIES DRAWING D1040M0003 REV A

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 40,563 hrs · 20,843 cycles

AFT CABIN FLOOR PANEL 241XF HAS PULLED UPPER SURFACE PLIES / REPAIRED PULLED UPPER SURFACE PLIES ON AFT CABIN FLOOR 241XF IAW SRM 53-00-50-5R-1. 57066U 06/08/18

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 40,563 hrs · 20,843 cycles

CRACK FOUND ON FWD CABIN INTERCOSTAL; APPROX. BS 317; RBL 31; WL 208 (MARKED) / REMOVED AND INSTALLED NEW FWD CABIN INTERCOSTAL; APPROX BS 317; RBL 31; WL 208 ITEM # 141A5410U12 IAW SRM 51-40-02-0G-0 AND DWG # 141A5410

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,563 hrs · 20,843 cycles

INTERCOSTAL CRACKED AT BS 285, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR PANEL — BROKEN (AFT CABIN) · airframe 40,563 hrs · 20,843 cycles

AFT CABIN FLOOR PANEL 242XF IS BROKEN / DUE TO THE EXTENT OF DAMAGE ON PANEL 242XF; REPLACED WITH NEW PANEL IAW SRM 51-10-02-0G-0 PAR 9; AIPC 53-21-00-36B AND D3 TECHNOLOGIES DRAWING D1040M0003 REV A

Part: PLATE — CRACKED (LEFT WING) · airframe 38,750 hrs · 19,699 cycles

LEFT WING SHELF PANEL 561BB VERY OUTBOARD 2 EACH WIGGLE PLATE ASSY. CRACKED / R/R WIGGLE PLATE ASSY. PER SRM 51-40-02

Part: FITTING — CRACKED (LEFT WING) · airframe 38,747 hrs · 19,698 cycles

INBOARD OF #1 CANOE FAIRING WING SHELF PANEL SUPPORT ROD AND FITTING CRACKED. / REMOVED AND REPLACED SHELF PANEL SUPPORT FITTING IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (E&E BAY) · airframe 37,695 hrs · 19,057 cycles

UPPER BEAM OF INTERCOSTAL CRACKED; BETWEEN STAS 344-360; BL0. / REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 34,395 hrs · 17,072 cycles

CABIN FLOOR SUPPORT CRACKED AT BS 540, RBL 2. R & R THE FLOOR SUPPORT IAW SRM.

Part: HOOK — CORRODED (CABIN) · airframe 34,395 hrs · 17,072 cycles

LEFT EMERGENCY EXIT HATCH ESCAPE STRAP WING ATTACH HOOK CORRODED. R & R HOOK IAW AMM.

Part: HOOK — CORRODED (CABIN) · airframe 34,395 hrs · 17,072 cycles

RT EMERGENCY EXIT HATCH ESCAPE STRAP WING ATTACH HOOK CORRODED. R & R HOOK IAW AMM.

Part: BRACKET — CRACKED (LT WING) · airframe 34,395 hrs · 17,072 cycles

LT WING REAR SPAR UPPER SHELF PANEL, L-BRACKET CRACKED AT BS 265, INBD NR 5 SPOILER. R & R L-BRACKET IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 34,395 hrs · 17,072 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 45.64 TO RBL 40.00. REPAIRED WEB IAW SRM.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 33,669 hrs · 16,647 cycles

L1 DOOR SLIDE GIRT BAR ATTACH HOLD DOWN DIRTY. CLEANED GIRT BAR ASSEMBLY IAW SIP.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 33,221 hrs · 16,368 cycles

L1 DOOR SLIDE Z FOLD LOOSE. SECURED Z FOLD IAW MT.

Part: HOLDER — LACK OF LUBE (L1 DOOR) · airframe 32,696 hrs · 16,085 cycles

L1 DOOR GIRT BAR HARD TO REMOVE. LUBED GIRT BAR HOLDER IAW SIP.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 32,556 hrs · 16,003 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 32,453 hrs · 15,948 cycles

R1 WINDSHIELD ARCED. R & R WINDSHIELD IAW MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,373 hrs · 15,895 cycles

FUSELAGE SKIN CORRODED AT STATION 1016, STRINGER 20L. REPAIRED SKIN IAW EA.

Part: LENS — CRACKED (R1 DOOR) · airframe 30,183 hrs · 14,602 cycles

R1 DOOR SLIDE LENS CRACKED. R & R LENS IAW AMM.

Part: CLAMP — OUT OF ADJUST (R1 DOOR) · airframe 29,616 hrs · 14,283 cycles

R1 DOOR EMER EVAC SLIDE BRACKET CLAMP OUT OF ADJUSTMENT. ADJUSTED CLAMP IAW SIP.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 27,210 hrs · 12,912 cycles

AFT CARGO THRESHOLD WEB CORRODED BETWEEN BS 805 TO 795 RBL 21. R & R WEB IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,210 hrs · 12,912 cycles

AFT CARGO SIDEWALL TO FLOOR SUPPORT CORRODED BETWEEN BS 767 TO 727D RBL 23. REPAIRED SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,210 hrs · 12,912 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO 328 LBL 46. R & R INTERCOSTAL IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 27,210 hrs · 12,912 cycles

LEFT HORIZONTAL STABILIZER CRACKED ON RIB 129.50 3RD STIFFENER. REPAIRED RIB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,210 hrs · 12,912 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 787 TO 775 RBL 22. REPAIRED SUPPORT IAW SRM & DWG.

Part: POST — CRACKED (FUSELAGE) · airframe 27,210 hrs · 12,912 cycles

RIGHT NR 3 WINDOW FRAME E - F POST SECOND FROM BOTTOM HOLE CRACKED. REPAIRED POST IAW MOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,210 hrs · 12,912 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO 328 RBL 31. R & R INTERCOSTAL IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 27,210 hrs · 12,912 cycles

LEFT HORIZONTAL STABILIZER CRACKED ON RIB 92.70 2ND STIFFENER. REPAIRED STIFFENER IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,210 hrs · 12,912 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,210 hrs · 12,912 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,210 hrs · 12,912 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,210 hrs · 12,912 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,546 hrs · 13,099 cycles

L2 DOOR EMER EVAC SLIDE LIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 27,411 hrs · 13,020 cycles

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

Part: FLAP — LOOSE (LT WING) · airframe 27,069 hrs · 12,836 cycles

LEFT WING OTBD AFT FLAP TRACK 3 ATTACH POINT LOOSE. R & R AFT FLAP IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,069 hrs · 12,836 cycles

AFT RT EMER BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.