N7861J

Part: RIB — CRACKED (ZONE 300) · airframe 55,751 hrs · 37,483 cycles

CRACK ON FRONT SPAR UPPER FLANGE INSPAR RIB 120.30 LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON RIB IAW EA 25-155-02690-WIP1 REV A, EA 25-155-02690, AND SRM 55-10-09-2R, REPAIR 5.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

TWO CRACKS ON VAPOR BARRIER BS 663.75 LH SIDE MAIN WHEEL WELL COMPARTMENT. THIS FAULT IS RESOLVED ON FAULT TTG8Q01564Z0.

Part: SILL DRAIN — CORRODED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

CORROSION LOWER SILL LOCATED BETWEEN STA794.3 TO STA847 AND RBL24 WL156 AT AFT CARGO COMPARTMENT. REPLACED LOWER SILL LOCATED BETWEEN STA794.3 TO STA847 AND RBL24 WL156 AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 146A8340; SHEET 21; REV-.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 55,751 hrs · 37,483 cycles

CRACK SUPPORT ANGLE BETWEEN BS 291.5 TO BS 294.5 AT LEVEL STRINGER 17R PASSENGER CABIN. REPLACED SUPPORT ANGLE LOC. BETWEEN BS 291.5 TO BS 294.5 AT LEVEL STRINGER 17R PASSENGER CABIN IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, DWG 141A8310 SHEET 25; REV.

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 55,751 hrs · 37,483 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHT LT SIDE 7 EA AND RT SIDE 7 EA. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING IAW AMM 33-51-15-400-802.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

CRACK ON VAPOR BARRIER BS 663.75 LH SIDE MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER BS 663.75 LH SIDE MAIN WHEEL WELL COMPARTMENT IAW SRM 51-70-04-2R-10 REPAIR 10.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY . REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY IAW SRM 51-40-02-0G-0.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND DWG 212A1101; SHEET 3 REV-.

Part: TIE CLIP — CRACKED (ZONE 200) · airframe 55,751 hrs · 37,483 cycles

CRACK TIE CLIP BS 277 AND STRINGER 10R PASSENGER CABIN. REPLACED TIE CLIP AND FASTENERS LOC.BS 277 AND STRINGER 10R PASSENGER CABIN IAW SRM 51-40-02; SRM B737-700 51-10-02 PARAGRAPH 9; DWG 141A1110 SHEET:18 REV:- AND DWG 141A8380 SHEET:14 REV-.

Part: STRAP — CORRODED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

CORROSION STRAP LOCATED BETWEEN BS787 TO BS794 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BETWEEN BS787 TO BS794 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 146A0081 SHEET: 25 REV: A.

Part: ACCESS PANEL — CRACKED (ZONE 200) · airframe 55,751 hrs · 37,483 cycles

CRACK ANGLE ACCESS PANEL 844DZ AT AFT GALLEY DOOR. REPLACED ANGLE ACCESS PANEL 844DZ AT AFT GALLEY DOOR DUE TO ALLOWABLE DAMAGE NOT FOUND IN SRM 52-10-02-1A-4; MEASURE OF CRACK IS: 0.310'. ANGLE REPLACED IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWING 411A2119 SH 71 REV -.

Part: STRAP — CORRODED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

CORROSION STRAP LOCATED BETWEEN BS794 TO BS807 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BETWEEN BS794 TO BS807 AND WL154 FROM STR25R TO STR26R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 146A8340 SHEET: 21 REV: -.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

CRACK TRACK LBBL 17.24 LOCATED BS767 AFT CARGO COMPARTMENT. REPAIRED CARGO TRACK LOC LBL17.24 BTW BS 747 TO BS 787 IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

CRACK CHANNEL SUPPORT LOCATED STA727 AND RBL 3 AT AFT CARGO COMPARTMENT. REPLACED CHANNEL SUPPORT LOCATED STA727 AND RBL 3 AT AFT CARGO COMPARTMENT IAW B737 700 SRM 51-10-02-0G STEP 9 AND DWG 144A2600 SHEET 566 REV -.

Part: RIB — CRACKED (ZONE 300) · airframe 55,751 hrs · 37,483 cycles

CRACKED INSPAR RIB LOCATED STAB STA 120.30 AND 34 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 55-10-09-2R-4, REPAIR 4, FIG 202, DETAIL A.

Part: RIB — CRACKED (ZONE 300) · airframe 55,751 hrs · 37,483 cycles

CRACKED INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 55-10-09-2R-4, REPAIR 4 FIG 202, DETAIL A.

Part: WEB — CORRODED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

CORROSION SHIELD WEB FLOOR STRUCTURE LOCATED BETWEEN STA767 TO STA794.3 AND RBL21 WL156 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOC. ON FLOOR STRUCTURE BETWEEN STA767 TO STA794.3 AND RBL21 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 25 REV A.

Part: RIB — CRACKED (ZONE 300) · airframe 55,751 hrs · 37,483 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 19 INCHES FROM FRONT EDGE LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 51-40-02, AND SRM 55-10-09-2R-4, REPAIR 4, FIG 202, DETAIL A.

Part: GUSSET — DAMAGED (ZN 100 FUS LOWER) · airframe 55,751 hrs · 37,483 cycles

ELONGATED HOLE GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 143A7902; SHEET: 174; REV-.

Part: RIB — CRACKED (ZONE 300) · airframe 55,751 hrs · 37,483 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCHES FROM FRONT EDGE LT HORIZONTAL STAB.

Part: RIB — CRACKED (ZONE 300) · airframe 55,751 hrs · 37,483 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 34 INCH FROM FRONT EDGE AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB IAW SRM 55-10-09-2R-5, REPAIR 5, FIG 204, DETAIL A.

Part: RIB — CRACKED (ZONE 300) · airframe 55,751 hrs · 37,483 cycles

CRACK INSPAR RIB LOCATED STAB STA120.30 AND 19 INCHES FROM FRONT EDGE LT HORIZONTAL STAB.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 55,751 hrs · 37,483 cycles

CRACK STIFFENER ASSY FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL 0 AND RBL 24.75 PASSENGER CABIN. REPLACED STIFFENER ASSY FLOOR STRUCTURE AND FASTENERS LOCATED BS 540 BETWEEN BL 0 AND RBL 24.75 PASSENGER CABIN IAW B737-700 SRM-51-10-02 ITEM 9 AND B737-700 SRM 51-40-02. AND DRAWING 143A0060; SHEET 44; REV A.

Part: ANGLE — CRACKED (ZONE 200) · airframe 55,751 hrs · 37,483 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75 AT PASSENGER CABIN. REPLACED ANGLE ON FLOOR STRUCTURE LOCATED BS 695 AND RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DWG: 273A9110 SHEET: 6 REV: A.

Part: BEAM — CRACKED (ZONE 800) · airframe 55,751 hrs · 37,483 cycles

CRACK INDICATION ON RADIUS OF FORWARD SERVICE DOOR 141A6536-14 BEAM #4.LENGTH OF CRACK: 0.625 IN. EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER FOR REPAIR. REPLACED TRACE BEAM NR 4 BTW BS 299.10 AND 328.87, FWD SERVICE DOOR IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02; DWG 141A6516 SHEET 92; 94 AND 96 REV-. AND DWG 141A6535; SHEET 13; REV-.

Part: ANGLE — CRACKED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

CRACKED ANGLE LOCATED BS 695 AND BL0 FWD SIDE. REPLACED ANGLE IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.

Part: ANGLE — CRACKED (ZONE 100) · airframe 55,751 hrs · 37,483 cycles

CRACKED ANGLE LOCATED BS 695 BL0 AFT SIDE. REPLACED ANGLE IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 55,263 hrs · 37,183 cycles

SEAT ROW 6ABC EMERGENCY LIGHT OUT. RELAMPED SEAT ROW 6ABC EMERGENCY AREA LIGHT. OPS CHECK GOOD PER AMM 33-51-03.

Part: UNKNOWN — ODOR (CABIN) · airframe 54,803 hrs · 36,897 cycles

F/A REPORTS SMELL OF SMOKE IN THE AFT CABIN<[01] C/W SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW AMM 05-51-56 AND FIM 21-00 TASK 806. NO DEFECTS NOTED AT THIS TIME. AIRCRAFT OK FOR SERVICE.

Part: LOCK — OUT OF ADJUST (ZONE 200) · airframe 54,737 hrs · 36,861 cycles

PASSENGER CABIN SEAT EXIT ROW 11C IS RECLINING.<[01] ADJUSTED HYDRO-LOCK PER AMM 25-22-00;[02] INSPECTED C/A 1. ROBERT FRENZEL (TECHNICIAN); ADJUSTED HYDRO-LOCK PER AMM 25-22-00

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 53,732 hrs · 36,285 cycles

ON CLIMB OUT THROUGH 9000 FEET; AIRCRAFT SHUDDERED AND ENGINE #1 N1 BEGAN CYCLING THROUGH 80% AND 90% N1. ENGINE REDUCED TO 50% N1 AND ENGINE INDICATIONS WERE NORMAL AT 50% N1 AND BELOW FOR REMAINDER OF FLIGHT<[01] ACCOMPLISHED BORESCOPE INSPECTION OF #1 ENGINE BOOSTER PER AMM 72-00-00-200-803-F00; HPC PER AMM 72-00-00-200-803-F00. HPT BLADES PER 72-00-00-200-807-F00; LPT PER AMM 72-00-00-200-808-F00. NO DEFECTS NOTED BEYOND AMM LIMITS. REMOVED AND REPLACED HMU AND MAIN FUEL PUMP PER MT 773-11-00. NO FIX . REMOVED AND REPLACED #1 ENG REF MT 771-00-01 TTG8Q0064PHE. OPS AND LEAK CHECKS GOOD.

Part: COVER — MISINSTALLED (ZONE 200) · airframe 53,088 hrs · 35,891 cycles

AFT SERVICE DOOR HAS THE INCORRECT DIRECTION EMERGENCY LENS COVER.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]

Part: BALANCE WEIGHT — CORRODED (ZN 300 STABILIZE) · airframe 52,393 hrs · 35,438 cycles

RUDDER BALANCE WEIGHT HAS EVIDENCE OF CORROSION<[01] R AND R RUDDER BALANCE WEIGHT PER EA 24-155-02244

Part: DOUBLER — CRACKED (EXTER PWR DOOR) · airframe 51,079 hrs · 34,620 cycles

GROUND POWER DOOR CUTOUT DOUBLER AFT EDGE FOUND CRACK<[01] PERFORMED HFEC OF THE CUTOUT REF 737 NDT MANUAL PART 6 51-00-00 PROCEDURE 23. NO DEFECTS NOTED AT THIS TIME.;[02] TRIMMED GROUND POWER DOOR SURROUND DOUBLER AS REQUIRED PER SRM 53-10-15-2R-4 ZONE 1;[03] REMOVED DAMAGE IAW SRM 53-10-15-2R-4

Part: EXTINGUISHER — LEAKING (COCKPIT) · airframe 51,000 hrs · 34,573 cycles

COCKPIT FIRE EXTINGUISHER HAS A SLOW LEAK.<[01] REPLACED COCKPIT FIRE EXTINGUISHER PER AMM 26-26-01.

Part: TRANSMITTER — FAULTY (ZN 100 FUS LOWER) · airframe 50,465 hrs · 34,244 cycles

ON FINAL AFTER SELECTING FLAPS 10 FROM FLAPS 5 FLAPS SPLIT-LEFT INDICATED 6 RIGHT =8 LANDED FLAPS 5 POSITION-AFTER LANDING FLAPS INDICATED 5;PSEU LIGHT AFTER LANDING 27-52261<[01] REMOVED AND REPLACED R/H FLAP POSITION TRANSMITTER PER AMM 27-58-01 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

EMERGENCY EXIT LIGHT IN BETWEEN FWD RECESSED CEILING LIGHTS INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF FWD RECESSED CEILING EMERGENCY EXIT LIGHT IAW AMM 33-51-03-960-801.;[02] JOB COMPLETE.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

BULLNOSE EMERGENCY EXIT LIGHT INOP AT SEAT ROW 4ABC<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF BULLNOSE EMERGENCY EXIT LIGHT AT SEAT ROW 4ABC IAW AMM 33-51-03-960-801.;[02] JOB COMPLETE.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

EMERGENCY EXIT LIGHT ON L/H OWE FWD OF WINDOW LIGHT INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY EXIT LIGHT ON FWD SIDE OF L/H OWE WINDOW LIGHT IAW AMM 33-51-03-960-801.;[02] JOB COMPLETE.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

EMERGENCY EXIT AREA LIGHT AT SEAT ROW 16FED IS INOP<[01] REMOVED AND REPLACED AREA LIGHT LAMP AT SEAT ROW 16FED OPS CHECK GOOD IAW AMM 33-51-03-960-801.;[02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

LWH OVERWING EXIT LIGHT FWD OF DOOR CUTOUT IS BROKEN.<[01] REPLACED LWH OVERWING EXIT LIGHT FWD OF DOOR AND GOOD OPERATIONAL TEST PER AMM 33-51-01-960-802.;[02] VERIFIED

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

CRACKED BREAK PANEL STA 540; LBL 1; WL 208.<[01] COMPLETED STEPS 1-2; OK TO INSTALL STEP 3.;[02] REMOVED AND REPLACED BREAK PANEL AT BS 540 LBL 1 WL 208 PER SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-00 AND DWG # 143A5240

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

CRACKED BREAK PANEL STA 540; RBL 1; WL 208.<[01] UPDATED TABLE;[02] COMPLETED STEPS 1-2; OK TO INSTALL STEP 3.;[03] REMOVED & INSTALLED NEW BREAK PANEL AT BS 540 RBL 1 WL 208 PER SRM 5140-02-0G-0 AND SRM 51-40-05-0G-0 AND BOEING DWG 143A5240

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED THE CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(4) AND BAC 5975 &NBSP;&NBSP;&NBSP;&NBSP;&NBSP;APPLIED A CHEMICAL CONVERSION COATING TO BARE ALUMINUM SURFACES PER SOPM 20-43-03; TYPE 2; CLASS A OR C AND SRM 53-60-15-2R-1 PARAGRAPH 4.B. (6) :&NBSP;&NBSP;&NBSP;&NBSP;&NBSP;APPLIED TWO LAYERS OF BMS 10-11; TYPE 1 PRIMER TO THE INNER SURFACES OF CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(7); REFER TO SOPM 20-41-02;[02] VERIFIED CORRECTIVE ACTION #1

Part: SKIN — CORRODED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

CORROSION ON EXTERNAL FUSELAGE SKIN BS887 STR25R TO STR25L<[01] CORRECTION TO TASK DETAIL SHOULD STATE ' CORROSION ON EXTERNAL FUSELAGE SKIN BS887 STR25R TO STR25L FWD OF BUTT JOINT ';[02] REMOVED CORROSION IN AN AREA OF 7.80' X 0.5 0' REMOVED 0.004' ORIGINAL THICKNESS 0.080' FOUND TO BE IN LIMITS PER SRM 53-00-01-1A-5. REAPPLIED PROTECTIVE FINISH AS SRM 53-00-01-1A-5.

Part: STRAP — ELONGATED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

AAI: REF: NRC: T684603: FWD CARGO COMPARTMENT: FRAME STRAP HAS AN ELONGATED FASTENER HOLE AT STA 492.4; STR 23R.<[01] OVERSIZED HOLE TO ROUND CONDITION PER EA 23-153-02732

Part: ANGLE — MISINSTALLED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

AAI: REF: NRC: TTG8Q00A1SR1: FWD CARGO COMPARTMENT: REPAIR ANGLE HAS IMPROPERLY INSTALLED FASTENER AND HOLE ELONGATED AT STA 500A; STR 25R.<[01] REMOVED; REPLACED AND INSTALLED NEW CLIP AT BS 500A STR 25R WL 156 PER SRM 51-40-02-0G-0 AND DWG 143A7505;[02] VERIFIED JOB COMPLETE

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 49,620 hrs · 33,734 cycles

R/H HORIZONTAL STABILIZER HAS A CRACKED RIB AT STA.129.50; 2ND VERTICAL STIFFENER FROM L/E<[01] VERIFIED APPLICABILITY OF SRM 55-10-09-2R-4 REPAIR 4.;[02] VERIFIED CORRECTIVE ACTION 1;[03] REMOVED CRACK DAMAGE RIGHT HAND HORIZONTAL STABILIZER INPSAR RIB AT STA 129.50 2ND VERTICAL STIFFENER FROM LEADING EDGE AND INSTALLED REPAIR IAW SRM 55-10-09-2R-4 REPAIR 4.;[04] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 49,620 hrs · 33,734 cycles

L/H HORIZONTAL STABILIZER 4TH VERTICAL STIFFENER FROM L/E IS CRACKED AT BS 129.5; INSPAR RIB 5<[01] REMOVED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER 4TH VERTICAL STIFFENER FROM LEADING EDGE AT STAB STA 129.50 INSPAR RIB 5 AND INSTALLED REPAIR IAW SRM 55-10-09-2R-4 REPAIR 4.;[02] VERIFIED APPLICABILITY OF SRM 55-10-09-2R-4 REPAIR 4.;[03] VERIFIED CORRECTIVE ACTION 1;[04] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

PANEL 222BF FWD O/B CORNER IS DELAMINATED<[01] DELAMINATION AT FWD O/B CORNER ON FLOOR PANEL 222BF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] JOB COMPLETE.

Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6 RBL11.5 WL156<[01] CORROSION ON STRAP FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED AS PER SRM 51-10-02.;[02] VERIFIED CORRECTIVE ACTION 1;[03] RECEIVED NEW AFT CARGO BAY FLOOR SPLICE STRAP BS727D+6 ON PO # 936406 INSTALL WILL BE ON CARD # TTG8Q00M72SC;[04] VERIFIED CORRECTIVE ACTION #3;[05] ADDED PARTS REQUIREMENT;[06] TASK COMPLETE

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] REMOVED AND REPLACED ACB L/H FLOOR TO SIDEWALL SUPPORT PLATE BS 727+4 TO BS 847; LBL 22; WL 156 IAW SRM 51-40-02-0G-0; DWG#146A7500.;[02] VERIFIED CORRECTIVE ACTION #1

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727C TO BS767 RBL22 WL156<[01] REMOVED AND REPLACED ACB R/H FLOOR TO SIDEWALL SUPPORT PLATE BS 727+4 TO BS 767; RBL 22; WL 156 IAW SRM 51-40-02-0G-0; DWG#146A7500;[02] VERIFIED CORRECTIVE ACTION #1

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

CRACKED INTERCOSTAL BS 380-400 LBL 1 WL 208.<[01] REMOVED; REMPLACED AND INSTALLED NEW ANGLE INTERCOSTAL BS 380-400 LBL 1 WL 208. PER SRM 51-40-02-0G-0 AND DWG 143A5400.;[02] VERIFIED CORRECTIVE ACTION #1

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 49,620 hrs · 33,734 cycles

R/H HORIZONTAL STABILIZER HAS A CRACKED #6 INSPAR RIB VERTICAL STIFFENER 2ND FROM THE L/E STAB STA 138.70<[01] FAULT RAISED IN ERROR; CLOSING CARD;[02] VERIFIED CORRECTIVE ACTION 1. FAULT IS BEING CLOSED

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

CRACKED INTERCOSTAL BS 380-400 LBL 13 WL 208.<[01] REMOVED; REPLACED AND INSTALLED NEW INTERCOSTAL AT BS 380-400 LBL 13 WL 208 PER SRM 51-40-02-0G-0 AND DWG 141A5400;[02] VERIFIED CORRECTIVE ACTION #1

Part: SEAT TRACK — CORRODED (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

L/H CABIN SEAT TRACK HAS CORROSION IN WELL AT BS 539+2; 663+15; 706+6; 706+17; 727+12; RBL 45; WL 208 L/H IS INCORRECT; R/H CABIN SEAT TRACK IS CORRECT<[01] FAULT RAISED IN ERROR; CLOSING CARD;[02] VERIFIED FAULT RAISED IN ERROR; CLOSING CARD

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

CRACKED INTERCOSTAL BS 344-360 LBL 1 WL 208.<[01] REMOVED; REPLACED AND INSTALLED NEW INTERCOSTAL AT BS 344-360 LBL 1 WL 208 PER SRM 51-40-02-0G-0 AND DWG 141A5410.;[02] VERIFIED CORRECTIVE ACTION #1

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

CRACKED INTERCOSTAL BS 312-328 LBL 45 WL 208.<[01] REMOVED; REPLACED AND INSTALLED NEW INTERCOSTAL AT BS 312-328 LBL 45 WL 208 PER SRM 51-40-02-0G-0 AND DWG 141A5400;[02] VERIFIED CORRECTIVE ACTION #1

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 49,620 hrs · 33,734 cycles

L/H HORIZONTAL STABILIZER HAS A CRACKED VERTICAL STIFFENER 3RD FROM L/E AT INSPAR RIB 6 CORRECTION: STAB STA 129.5 (INSPAR RIB 5)<[01] REMOVED CRACK DAMAGE LEFT HAND HORIZONTAL STABILIZER INPSAR RIB AT STA 129.50 3RD VERTICAL STIFFENER FROM LEADING EDGE AND INSTALLED REPAIR IAW SRM 55-10-09-2R-4 REPAIR 4.;[02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

Part: SUPPORT — CORRODED (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

CORROSION ON FLOOR SUPPORT BS 270-277 LBL 10 WL 208.<[01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 270-277 LBL 10 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5600;[02] VERIFIED CORRECTIVE ACTIONS AND MEASUREMENT FIELDS. CARD COMPLETE

Part: PLATE — BROKEN (ZN 500 LEFT WING) · airframe 49,620 hrs · 33,734 cycles

LEFT WING LOWER TRAILIING EDGE WIGGLE PLATE @RSS 261 ABOVE #1 PYLON AFT TIP O/B FASTENER BROKEN<[01] REMOVED AND REPLACED WIGGLE PLATE AT ORSS 261 IAW SRM 51-40-02-0G-0; AIPC 57-50-00-30 ITEM 345 & BAC DRAWING #115A2001 SH29.<BR>UPDATED PART REQUIREMENT.;[02] VERIFIED CORRECTIVE ACTION 1

Part: SUPPORT ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 49,620 hrs · 33,734 cycles

LEFT WING; UPPER T/E PANEL BETWEEN SPOILERS #5 AND #6; LOWER SURFACE SUPPORT ANGLE IS CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT<[01] REMOVED AND REPLACED RIGHT WING UPPER FIXED T/E PANEL BETWEEN #5 AND #6 SPOILERS; LOWER SURFACE SUPPORT ANGLE CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT WITH NEW FITTING PART#115A2953-1 IAW SRM 51-40-02-0G-0 & AIPC 57-50-00-25 ITEM 272.;[02] VERIFIED

Part: SUPPORT ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 49,620 hrs · 33,734 cycles

LEFT WING; T/E COVE SEAL SUPPORT ANGLE CRACKED AT UPPER ATTACH POINT ABOVE #1 PYLON AFT TIP<[01] REMOVED AND REPLACED LT WING T/E COVE SEAL SUPPORT ANGLE ABOVE #1 PYLON IAW MM 20-50-11-910-801<BR>CAL TOOL ID#PER2331 DUE 03/2024; PER2300 DUE 09/2023;[02] VERIFIED CORRECTIVE ACTION #1

Part: SUPPORT ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 49,620 hrs · 33,734 cycles

RIGHT WING UPPER FIXED T/E PANEL BETWEEN #7 AND #8 SPOILERS; LOWER SURFACE SUPPORT ANGLE IS CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT<[01] REMOVED AND REPLACED RIGHT WING UPPER FIXED T/E PANEL BETWEEN #7 AND #8 SPOILERS; LOWER SURFACE SUPPORT ANGLE CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT WITH NEW FITTING PART#115A2953-2 IAW SRM 51-40-02-0G-0 & AIPC 57-50-00-25.;[02] VERIFIED JOB COMPLETE

Part: STIFFENER — CORRODED (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

STIFFENER ON TOP OF FLOOR WEB AT BS 1016 HAS CORROSION AT RBL 3.<[01] REMOVED STIFFENER ON TOP OF FLOOR WED AT BS 1016 RBL 3. PER SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED DAMAGE STIFFENER BS1016-BS1028 RBL3 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5730.;[03] VERIFIED CORRECTIVE ACTION 2;[04] VERIFIED MEASUREMENT TABLE

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

CRACK FOUND IN 663 VAPOR BARRIER AT RBL 55 WL 160<[01] REMOVED AND REPLACED RH 663 VAPOR BARRIER WEB IAW SRM 51-40-02 AND DWG 111A1000.;[02] RII VERIFIED CORRECTIVE ACTION ITEM 1.;[03] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE.

Part: FLOOR PANEL — BROKEN (ZN 200 FUS TOP) · airframe 49,620 hrs · 33,734 cycles

CABIN FLOOR PANEL 242WF IS BROKEN.<[01] CABIN FLOOR PANEL 242WF WITH BROKEN LOWER SKIN O/B EDGE WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] FINAL INSPECTION. JOB COMPLETE.

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8 W.L. 160.<[01] CLEANED AREA AT BS663 LBL8 WL160 AS PER AMM 51-21-21; UPON FURTHER INVESTIGATION NO CRACK WAS FOUND; ONLY DEFECT NOTED WAS CHIPPED AND MISSING PAINT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. NDI CONFIRMATION REQUIRED.;[03] REQUEST N.D.I. TO VERIFY CRACK FREE CONDITION.;[04] HFEC INSPECTED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS1465 CAL DUE: 09/2023;[05] APPLIED CHEMICAL CONVERSION COATING AND PRIMED TO SUSPECTED AREA PER MM 51-21-41-370-802 AND MM 51-21-72-370-804; NO FURTHER ACTION REQUIRED;[06] VERIFIED CORRECTIVE ACTION #5

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 49,620 hrs · 33,734 cycles

IB AND OB SEAL STRIKE PLATES CRACKED IB AND OB SEAL STRIKE PLATES CRACKED. #1 AFT FLAP TRACK FAIRING #544BB<[01] STEP 1 COMPLETE;[02] STEP 2 COMPLETE;[03] VERIFIED STEP 2 COMPLETE.;[04] REMOVED AND REPLACED I/B AND O/B SEAL STRIKE PLATE ON #1 AFT FLAPTRACK FAIRING IAW AMM 27-51-28-820-801;[05] VERIFIED STEPS 1;2 COMPLETE AND CORRECTION ACTION ITEM 4; CARD COMPLETE.

Part: SHIELD — CRACKED (NR 2 NACELLE) · airframe 49,620 hrs · 33,734 cycles

#2 ENGINE O/B FAN COWL OIL DOOR SHIELD IS CRACKED. R & R #2 ENGINE O/B FAN COWL OIL DOOR SHIELD PER; SRM 51-40-02-0G-0- AND CMM 71-13-30. VERIFIED REMOVED AND REPLACED #2 ENGINE O/B FAN COWL OIL DOOR SHIELD PER; SRM 51-40-02-0G-0- AND CMM 71-13-30. VERIFIED CORRECTIVE ACTION COMPLETE; AND VERIFIED MEASUREMENT TABLE COMPLETE.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 49,620 hrs · 33,734 cycles

PANEL 543BB IB/OB MID SEAL STRIKE PLATES CRACKED<[01] PARTIAL UPDATE STEP 1;[02] STEP 2 COMPLETE;[03] VERIFIED STEPS 2 COMPLETE.;[04] REMOVED AND REPLACED I/B AND O/B SEAL STRIKE PLATE ON 543BB AFT FLAPTRACK FAIRING IAW AMM 27-51-28-820-802;[05] VERIFIED STEPS 1;2 COMPLETE AND CORRECTION ACTION ITEM 4; CARD COMPLETE.

Part: SHIELD — CRACKED (ZN 400 NACELLE/P) · airframe 49,620 hrs · 33,734 cycles

#1 ENGINE I/B FAN COWL OIL ACCESS DOOR SHIELD IS CRACKED.<[01] REMOVED AND REPLACED #1 ENGINE I/B FAN COWL OIL ACCESS DOOR SHIELD PER SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED REMOVED AND REPLACED #1 ENGINE I/B FAN COWL OIL ACCESS DOOR SHIELD PER SRM 51-40-02-0G-0 AND CMM 71-13-30;[03] UPDATED MEASUREMENTS;[04] VERIFIED CORRECTIVE ACTION #2.<BR>VERIFIED MEASUREMENTS.

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

PANEL 191HL OUTER SKIN IS CRACKED.<[01] VERIFIED STEPS 1-3 AND THE MEASUREMENT TABLE.;[02] PANEL 191HL WITH OUTER SKIN IS CRACKED WAS REPAIR IAW SRM 51-70-05-2R-2.;[03] VERIFIED CORRECTIVE ACTION ITEM 2.

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 49,620 hrs · 33,734 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 45; W.L. 165.<[01] REMOVED AND REPLACED BS 663 LWR COMPOSITE BLKHD UPPER ATTACH ANGLE WL 165 IAW SRM 51-40-02 AND DWG 111A1000.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETE

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 49,123 hrs · 33,426 cycles

RIGHT AISLE EMERGENCY LIGHT #1 INOP.<[01] TROUBLESHOT RIGHT AISLE EMERGENCY AREA LIGHT #1. REPLACED LAMP WITH NO FIX. FOUND POWER SUPPLY FUSE BAD. REPLACED FUSE WITH NO FIX. REPLACED POWER SUPPLY WITH NO FIX. FOUND ASSEMBLY PIN BROKEN. REPLACED REA LIGHT ASSEMBLY PER AMM 33-51-03. OPS CHECK GOOD AT THIS TIME.

Part: POWER SUPPLY — INOPERATIVE (ZN 200 FUS TOP) · airframe 49,033 hrs · 33,366 cycles

EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK INOP AT (M2335)<[01] R/R EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK AT (M2335) IAW AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 49,033 hrs · 33,366 cycles

EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK INOP AT (M2335)<[01] R/R EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK AT (M2335) IAW AMM 33-51-06. OPS CHECK GOOD.

Part: BRACKET — BROKEN (ZN 100 FUS LOWER) · airframe 48,554 hrs · 33,047 cycles

LOWER FUSELAGE KEEL BEAM PANEL 192E; FEW R/H HANGER BRACKET BROKEN.<[01] REMOVED AND REPLACED HANGER BRACKET PER SRM 51-40-02

Part: PANEL — ELONGATED (FUSELAGE) · airframe 46,688 hrs · 31,816 cycles

PANEL 193B HOLES ELONGATED / [01] REMOVED MATCH DRILLED AND INSTALLED NEW 193B PANEL PER SRM 51-40-02.

Part: SLIDE — OUT OF ADJUST · airframe 44,855 hrs · 30,609 cycles

QC CABIN WALK: R-2 DOOR SLIDE SKIRT HITTING DOOR THRESHOLD WHEN OPENING/CLOSING DOOR ; / [01] ACCOMPLISHED ESCAPE SLIDE PACK INSTALLATION (UNSCHEDULED) STEP 6 D. VERIFIED STEPS (E) AND (F). REF; B737-700 AMM 25-66-01-400-804. OPERATED DOOR SEVERAL TIMES NO DEFECTS NOTED.; [02] VERIFIED STEP 1

Part: PANEL — CRACKED · airframe 44,855 hrs · 30,609 cycles

LOWER FUSELAGE PANEL 193D HAS (3 EACH) FASTENER HOLES CRACKED ; / [01] REMOVED PANEL 193D FOR ACCESS AS PER AMM 53-51-21-000-802; [02] PREPARED FOR REPAIR AT PANEL 193D AS PER B 737-700 SRM 51-70-04-2R-9; [03] VERIFIED STEPS 1 AND 2; [04] REPAIRED AT PANEL 193D AS PER B737-700 SRM 51-70-04-2R-9 MATERIAL USED PO.1731995; PO1150387; PO.1713932; [05] VERIFIED STEP 4; [06] APPLIED TOPCOAT ON LOWER FUSELAGE PANEL 193D REF B-737 AMM 51-21-73-370-803; [07] VERIFIED STEP 6; [08] CORRECTION TO STEP 4: REPAIRED AT PANEL 193D AS PER B737-700 SRM 53-40-70 AND 51-70-04-2R-9 MATERIAL USED PO.1731995; PO1150387; PO.1713932; [09] VERIFIED STEP 8; [10] OK TO REINSTALL PANEL 193D; [11] RE-INSTALLED PANEL 193D AS PER AMM 53-51-21

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 44,855 hrs · 30,609 cycles

EMERGENCY LIGHTS INOP AT OVERHEAD BINS POSITIONS 14LH; 17LH; 24LLH AND EXIT SIGN AT BIN 18 LH. ; EMERGENCY LIGHTS INOP AT OVERHEAD INS POSITIONS 14LH; 17LH; 24LLH AND EXIT SIGN AT IN 18 LH. / [01] REMOVED AND REPLACED POWER SUPPLY BATTERY PACK AT M1690 POSITION AS PER AMM 33-51-06-960-805.PERFORMED INSTALLATION TEST FOUND NORMAL.; [02] VERIFIED STEP 1; [03] REMOVED AND REPLACED BATTERY PACK AT M1690 AS PER REF B737-AMM-33-51-06-960-805. INSTALLATION TEST NORMAL AT POSITIONS 14LH; 17LH; 24LH AND EXIT SIGN AT BIN 18LH.; [04] VERIFIED CORRECTION IN STEP 3

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,855 hrs · 30,609 cycles

SUPPLEMENTAL INFORMATION: EMERGENCY LIGHT BATTERY PACK M1672 DID NOT PASS CAPACITY CHECK. ; EMERGENCY LIGHT ATTERY PACK M1672 DID NOT PASS CAPACITY CHECK. / [01] REMOVE AND REPLACED BATTERY PACK M1672 PER AMM 33-51-06-960-805.TEST NORMAL<BR>AAR TAG WN12332.; [02] VERIFIED STEP 1

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 44,855 hrs · 30,609 cycles

AFT EXTERIOR OVERWING EMERGENCY LIGHTS LH AND RH SIDE INOP. / [01] ADJUSTED AFT EXTERIOR OVERWING EMERGENCY LIGHTS LH AND RH LAMPS AS PER B737 AMM 33-51-04-960-801. PERFORMED OPS CHECK; FOUND NORMAL AS PER B737 AMM 33-51-04-960-801.; [02] VERIFIED STEP 1

Part: PANEL — ELONGATED · airframe 44,855 hrs · 30,609 cycles

SUPPLEMENTAL INFORMATION: PANEL 194E FWD EDGE; MIDDLE FASTENER HOLE SHOWS EVIDENCE OF STRESS CRACKS ; / [01] MEASURMENTS; [02] PERFORMED TAP TEST ON PANEL #194E AND FOUND NO WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL; ONLY DAMAGED FASTNER HOLE AS PER B737 NDTM 51-05-01; [03] PREPARED DAMAGED AREA ON WING TO BODY FAIRING PANEL #194E FOR REPAIR AS PER B737 SRM 51-70-05-2R-8 AND SRM 53-60-70-2R-1; [04] VERIFIED STEPS 1; 2 AND 3; [05] REPAIRED DAMAGE AREA ON WING TO BODY FAIRING #194E AS PER BOEING 737 SRM 51-70-05-2R-8. MATERIAL USED HCS2401-015-10 PO#1749325.; [06] VERIFIED REPAIR; [07] APPLIED TOP COAT ON PANEL 194E FWD EDGE REF B 737 AMM 51-21-73-370-803; [08] VERIFIED; [09] CORRECTION TO STEP 5: REPAIRED DAMAGE AREA ON WING TO BODY FAIRING #194E AS PER BOEING 737 SRM 51-70-05-2R-8 AND SRM 53-60-70-2R-1. MATERIAL USED HCS2401-015-10 PO#1749325.; [10] VERIFIED STEP # 9

Part: BATTERY — LOW (AFT CABIN) · airframe 44,855 hrs · 30,609 cycles

AFT L/H WINDSCREEN FLASH LIGHT BATTERIES DRAINED 2EA. ; / [01] REPLACED AFT L/H WINDSCREEN FLASHLIGHT BATTERIES IAW BOEING 737-700 AMM 25-64-00-900-806-NG; [02] INSPECTION DUE DATE: FEB 23; [03] VERIFIED STEPS 1 AND 2

Part: NONE — ELONGATED (R/H HORIZ. STAB.) · airframe 44,855 hrs · 30,609 cycles

SUPPLEMENTAL INFORMATION: R/H HORIZONTAL STAB. I/B LOWER T/E GAP COVER PANEL # 343AB HAS 1 EACH RUBBER SEAL WITH ELONGATED HOLES; SLIDING METAL AND AFT RED PLASTIC SEAL WORN ; / [01] REMOVED AND REPLACED SEAL AND SLIDINNG METAL SEAL AS PER B737-700 SRM51-40-02 0G-0-A00729; [02] VERIFIED

Part: NONE — ELONGATED (R/H HORIZ. STAB.) · airframe 44,855 hrs · 30,609 cycles

SUPPLEMENTAL INFORMATION: R/H HORIZONTAL STAB. UPPER GAP COVER PANEL # 343AT HAS 2 EACH RUBBER SEAL WITH ELONGATED HOLES AND SLIDING METAL SEAL WORN ; / [01] REMOVED AND REPLACED 2EA RUBBER SEALS AND 1 EA SLIDING METAL SEAL AS PER REF B737-700 SRM 51-40-02-0G-0; [02] VERIFIED

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 44,855 hrs · 30,609 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO STRG 25L BETWEEN STA500 AND STA500A FOUND BAFFLE SUPPORT CRACK AT UPPER RADIUS ; / [01] REMOVED AND REPLACED BAFFLE AT FWD CARGO COMPARTMENT STRG 25L BETWEEN STA 500 AND STA 500A IN REF SRM 51-40-02-OG-0; [02] VERIFIED STEP 1

Part: SUPPORT — CORRODED (BS 500D S25L) · airframe 44,855 hrs · 30,609 cycles

FWD CARGO LT FLOOR TO SIDE SUPPORT CORRODED AT BS 500D S25L REMOVED CORROSION ON FLOOR SUPPORT & FOUND OUT LIMITS. ORIGINAL MAT. .040' REMOVED .040' REMAINING 0.000' IAW SRM 51-10-02 & SRM 53-00-53-1A-2. REMOVED DAMAGED SECTION, FABRICATED A NEW FLOOR TO SIDE SUPPORT & SPLICE PLATE. LOCATED & DRILLED THE NEW PARTS IAW SRM 53-00-53-2R-5 & SRM 51-40-02-0G-0. TREATED REPAIR & SPLICE WITH ALODINE & PRIMER IAW AMM. 51-21-72. INSTALLED PARTS & SPLICE REPAIR IAW SRM 53-00-53-2R-5.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 44,855 hrs · 30,609 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO STRG 25L BETWEEN STA 500B AND STA 500C BAFFLE SUPPORT CRACK AT UPPER ATTACHING RIVETS ; / [01] REMOVED AND REPLACED BAFFLE AT FWD CARGO STRG 25L BETWEEN STA 500B AND STA 500C AS PER SRM 51-40-02-0G-0; [02] VERIFIED STEP 1; [03] VERIFIED STEP 1

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 44,855 hrs · 30,609 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPARTMENT DOOR CUT OUT SCUFF PLATE FWD CORNER HAS A CRACK ; / [01] RECEIVED NEW PART P/N 654A0004-1323; PO#1746222.<BR>THIS PART WILL BE INSTALL ON CARD TTG8Q003BN03; [02] VERIFIED RECEIVED NEW PART P/N 654A0004-1323; PO#1746222. <BR>THIS PART WILL BE INSTALLED ON CARD TTG8Q003BN03

Part: ANGLE — CRACKED (FUSELAGE) · airframe 44,855 hrs · 30,609 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO STRG 25L BETWEEN STA 500A AND STA 500B FOUND BAFFLE CRACK AT ATTACING RIVETS ; / [01] REMOVED FWD CARGO BAFFLE AT STRG 25L BETWEEN STA 500A AND STA 500B AS PER REF SRM 51-40-02-0G-0; [02] VERIFIED STEP 1; [03] FABRICATED REPAIR ANGLE FROM 7075-T6 0.032' CLAD PO#1641456 AS PER SRM 53-3053-2R-1 REPAIR 1; [04] RECEIVED NEW BAFFLE P/N 143A7510-11; PO#1751958; [05] FABRICATED REPAIR ANGLE FROM 7075-T6 0.032' CLAD PO#1641456 AS PER SRM 53-30-53-2R-1 REPAIR 1; [06] VERIFIED STEP 4; [07] VERIFIED STEP 5; [08] PERFORMED HFEC INSP ON FABRICATED REPAIR ANGLE. IAW B 737 NDT PART 6 51-00-00 PROCE 23. TOOL NORTEC 600. BC 166317. CALIB DUE 10-20-22. NO CRACKS FOUND.; [09] PERFORMED HFEC HOLE PROBE INSPECTION ON ALL INITIAL FASTENER HOLE LOCATIONS WITHIN REPAIR AREA IAW NDTM PART 6; 51-00-00; PROCEDURE 16. NO CRACKS.<BR>[NORTEC 600; B/C 166317 ;CALIB.DUE-10/22]; [10] PERFORMED GVI OF REPAIR PARTS. NO DEFECTS NOTED; [11] TREATED AND PRIMED BAFFLE ASSY AND REPAIR ANGLE AS PER B737-7 AMM 51-21-41 AND 51-21-72.; [12] OK TO INSTALL BAFFLE AND REPAIR ANGLE; [13] REMOVED AND REPLACED BAFFLE AND ACCOMPLISHED ANGLE REPAIR AS PER B737-7 SRM 53-30-53-2R-1 FIG. 202.; [14] VERIFIED STEP 13; [15] C/W

Part: STIFFENER — CRACKED (RH HOR STAB) · airframe 44,855 hrs · 30,609 cycles

SUPPLEMENTAL INFORMATION: RT. HOR. STAB INSPAR RIB ASSY NO. 5 (STAB STA 129.50) STIFFENER NO. 3 CRACKED ; / ] CUT AND REMOVED THE DAMAGE FROM THE VERTICAL STIFFENER OF THE RIB ASPER B 737-700 SRM 55-10-09-2R-4 REPAIR-4;23. CRACK NOTED; EQUIP: NORTEC 600 B/C 166317 CAL DUE: 10/22; [10] CUTOUT THE DAMAGED AREA AT RIB ASSY #5 STIFFENER #3 RH HORIZONTAL ASPER B737-700 SRM 55-10-09-2R-4 REPAIR 4; PERFORMED HFEC INSP. ON CUTOUT @ R/T HORIZ. STAB INSPAR RIB ASSY #5 (STAB STA 129.50) STIFFENER #3 IAW B737 NDT PART 6 51-00-00 PROC. 23. NO CRACKS; EQUIP: NORTEC 600 B/C 166317 CAL DUE: 10/22 LOCATED AN DRILLED FASTENER HOLES REPAIR AT RIB#5 STIFFENER #3 ASPER B737-700SRM 55-10-09-2R-4 REPAIR 4 FIGURE 202; ] TREATED AND PRIMED FASTENER HOLES AND REPAIR AREA AT RH HORIZONTAL. RIB #5 STIFFENER #3 ASPER B 737-700 AMM 51-21-72-370-804 AND 51-21-41-370-802; OK TO INSTALL REPAIR PARTS AT RH HORIZONTAL. RIB #5 STIFFENER #3 INSTALLED REPAIR PARTS AT RH HORIZONTAL RIB #5 STIFFENER #3 ASPER B737-700 SRM 51-40-02-0G-0 AND 55-10-09-2R-4 REPAIR 4INSTALLED RIB #5 AT RT HORIZONTAL STBZ STA 129.50 AS PER B737-700 SRM 55-10-09-2R-4] OK TO INSTALL WEB AT STA 111.10 TO STA175.50; INSTALLED WEB AT RH HORIZONTAL STA 111.10 TO 175.50 ASPER B 737-700 SRM 51-40-02-0G-0;RECORDED MEASUREMENTS;ACCOMPLISHED REPAIR ON INSPAR RIB ASSY NO 5 STIFFENER NO. 3 AT RT HORZ. STAB AS PER REF B737-700 SRM 55-10-09-2R-4 REPAIR-4;

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 44,855 hrs · 30,609 cycles

FWD CARGO STRG 25R BETWEEN STA 500A AND STA 500B BAFFLE SUPPORT CRACK AND AFT ATTACHING BRACKET ALSO CRACK ; / [01] PERFORMED HFEC INSP ON BAFFLE SUPPORT. IAW B 737 NDT PART 6 51-00-00 PROCE 23.TOOL NORTEC 600. BC 166317. CALIB DUE 10-20-22. CRACK INDICATION; 10' FROM FRONT; LENGTH 0.25'.; [02] REMOVED BAFFLE AT FWD CARGO STRG 25R BETWEEN STA 500A AND STA 500B AS PER 51-40-02-0G-0; [03] VERIFIED STEP 2; [04] RECEIVED NEW BAFFLE P/N143A7510-12; PO#1751958.<BR>FABRICATED REPAIR ANGLE FROM 7075-T6 0.032' PO#1553587 AS PER SRM 53-30-53-2R-1 REPAIR 1; [05] VERIFIED STEP 4; [06] PERFORMED HFEC INSP ON FABRICATED REPAIR ANGLE. IAW B 737 NDT PART 6 51-00-00 PROCE 23. TOOL NORTEC 600. BC 166317. CALIB DUE 10-20-22. NO CRACKS FOUND.; [07] PERFORMED HFEC HOLE PROBE INSPECTION ON ALL INITIAL FASTENER HOLE LOCATIONS WITHIN REPAIR AREA IAW NDTM PART 6; 51-00-00; PROCEDURE 16. NO CRACKS.<BR>[NORTEC 600; B/C 166317 ;CALIB.DUE-10/22]; [08] PERFORMED GVI OF REPAIR PARTS. NO DEFECTS NOTED; [09] TREATED AND PRIMED NEW BAFFLE AND REPAIR ANGLE AS PER B737-7 AMM 51-21-41 AND 51-21-72.; [10] OK TO INSTALL NEW BAFFLE AND REPAIR ANGLE; [11] REMOVED AND REPLACED BAFFLE;ATTACHING BRACKET AND INSTALLED ANGLE REPAIR AS PER B737-7 SRM 53-30-53-2R-1 AND SRM 51-40-02.; [12] VERIFIED STEP 11.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 44,855 hrs · 30,609 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPARTMENT AFT SCUFF PLATE CORNER CRACKED ; / [01] RECEIVED NEW PART P/N 654A0004-338; PO#1746222.; [02] VERIFIED STEP 1; [03] RECEIVED NEW AFT SCUFF PLATE AND LOCATED NEW FASTENER HOLES AS PER B737-7 SRM 51-40-02; [04] VERIFIED STEP 3; [05] NEW SCUFF PLATE TO BE INSTALL ON TASK CARD #TTG8Q003BN03.; [06] VERIFIED STEP 5

Part: SCUFF PLATE — CRACKED (AFT CARGO DOOR) · airframe 44,855 hrs · 30,609 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO DOOR SCUFF PLATE AFT CORNER; CRACKED. DOT#208-75 ; / [01] RECEIVED SCUFF PLATE 146A8341-9 REPAIRED BY JL WELDING; WORK ORDER # 16188 AND PO # 413250; [02] REFER TO FAULT TTG8Q003BMYY FOR INSTALLATION OF SCUFF PLATE; [03] VERIFIED STEPS 1 AND 2

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 44,855 hrs · 30,609 cycles

AFT CARGO DOOR SCUFF PLATE FWD CORNER; CRACKED. DOT#208-76 ; / [01] RECEIVED SCUFF PLATE 146A8341-7 REPAIRED BY JL WELDING; WORK ORDER # 16188 AND PO # 413250; [02] REFER TO FAULT TTG8Q003BMYY FOR INSTALLATION OF SCUFF PLATE; [03] VERIFIED STEPS 1 AND 2

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,469 hrs · 29,763 cycles

EMERGENCY EXIT BATTERY M1674 LIGHTS DID NOT WORK. / R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,469 hrs · 29,763 cycles

EMERGENCY EXIT BATTERY M1675 LIGHTS DID NOT WORK. / R&R BATTERY PACK PER AMM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 43,469 hrs · 29,763 cycles

EMERGENCY EXIT BATTERY M1673 LIGHTS DID NOT WORK. / R&R BATTERY M1673 PER AMM.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 43,469 hrs · 29,763 cycles

PANEL 193CL HAS DELAMINATONS ON THE INNER SURFACE OF THE CORE AREA / PANEL 193CL DELAMINATIONS ON THE INNER SURFCE OF THE CORE AREA REPAIRED IAW SRM 51-70-05-2R-2 PER SRM 53-40-70-2R-1

Part: BRACKET — CRACKED (L2 DOOR) · airframe 43,469 hrs · 29,763 cycles

CRACKED SUPPORT BRACKET ON AED AFT LOWER GATE SUPPORT PANEL 844DZ. (MARKED) / REPLACED SUPPORT BRACKET ON AED AFT LOWER GATE SUPPORT PANEL 844DZ IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0. 57193U; 17OCT19.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,469 hrs · 29,763 cycles

AFT CARGO BAY INTERCOSTAL CORRODED AT NUT PLATE HOLES BETWEEN BS. 767 TO BS. 787, RBL 21. / R&R INTERCOSTAL PER SRM & DWG.

Part: SUPPORT BRACKET — CRACKED · airframe 43,469 hrs · 29,763 cycles

CRACKED SUPPORT BRACKET ON ASD AFT LOWER GATE SUPPORT PANEL 834DZ. (MARKED) / REPLACED SUPPORT BRACKET ON ASD AFT LOWER GATE SUPPORT PANEL 834DZ IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0. 57193U; 17OCT19.

Part: WEB — CRACKED (L/H WING) · airframe 43,469 hrs · 29,763 cycles

L/W TRAILING EDGE CURVED BULB SEAL RETAINER AFT OF TRANSVERSE WEB CRACKED / REMOVED AND REPLACED SEAL RETAINER L/W TRAILING EGDE AFT OF TRANSVERSE WEB IAW SRM 51-40-02-0G-01 FASTENERS IAW AIPC 57-50-00-25 898134 10-12-19

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,469 hrs · 29,763 cycles

***CORROSION*** BS986 FLOOR BEAM LBL45 WL208. / REMOVED CORROSION AND REPAIRED I.A.W EA 1-A53-8241 R3

Part: GUSSET — CRACKED (BS 500D) · airframe 43,469 hrs · 29,763 cycles

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

Part: SHIELD — CORRODED (BS 737-787) · airframe 43,469 hrs · 29,763 cycles

AFT CARGO BAY SHIELD FORWARD OF THE CARGO DOOR CORRODED BETWEEN BS. 767 TO BS. 787, RBL 23. / R&R SHIELD PER SRM & DWG.

Part: WEB — CORRODED (CARGO THRESHOLD) · airframe 43,469 hrs · 29,763 cycles

AFT CARGO BAY SUB THRESHOLD WEB HAS AREAS OF CORRODED BETWEEN BS. 807 TO BS. 827, RBL 27. / R&R SUB THRESHOLD WEB PER SRM & DWG.

Part: ANGLE — CORRODED (BS 767-787) · airframe 43,469 hrs · 29,763 cycles

AFT CARGO BAY ANGLE UNDER SHIELD CORRODED ON THE FORWARD END BETWEEN BS. 767 TO BS. 787, RBL 23. / R&R ANGLE PER SRM & DWG.

Part: SUPPORT PLATE — CORRODED (BS 727-767) · airframe 43,469 hrs · 29,763 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAD AREAS CORRODED BETWEEN BS. 727 TO BS. 767, RBL 23. / R&R SUPPORT PLATE IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,469 hrs · 29,763 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 727 TO BS. 847, LBL 23. / R&R SUPPORT IAW SRM AND DWG.

Part: FAIRING — CRACKED (LEFT WING) · airframe 43,469 hrs · 29,763 cycles

LT FLAP FWD FAIRING 544AB INNER SKIN CRACKED BELOW SEAL RETAINER / DAMAGED FAIRING 544AB WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR. 9 (POS:544AB;TAG NO.:586027;P/N OFF/ON:113A9110-1;S/N OFF:1462;S/N ON:WN7820)

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 43,469 hrs · 29,763 cycles

FORWARD ENTRY CENTER EXIT LIGHT LENS DISCOLORED. / R&R LENS PER AMM.

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 43,469 hrs · 29,763 cycles

R/H OVER WING EXIT SIDEWALL LIGHT LENSES DISCOLORED. / R&R LENSES IAW AMM.

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 43,469 hrs · 29,763 cycles

AFT ENTRY CENTERLINE EMERGENCY EXIT LIGHT LENSES DISCOLORED. / R&R LENSES IAW AMM.

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 43,469 hrs · 29,763 cycles

R1 DOOR EXIT LIGHT LENSES DISCOLORED. / R&R LENSES PER AMM.

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 43,469 hrs · 29,763 cycles

L1 DOOR EXIT LIGHT LENSES DISCOLORED. / R&R LENSES PER AMM.

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 43,469 hrs · 29,763 cycles

L/H OVER WING EXIT SIDEWALL LIGHT LENSES DISCOLORED. / R&R LENSES IAW AMM.

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 43,469 hrs · 29,763 cycles

L2 DOOR EXIT LIGHT LENSES DISCOLORED. / R&R LENSES IAW AMM.

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 43,469 hrs · 29,763 cycles

R2 DOOR EXIT LIGHT LENSES DISCOLORED. / R&R LENSES IAW AMM.

Part: GIRT BAR — OUT OF POSITION (R2 DOOR) · airframe 43,210 hrs · 29,583 cycles

R2 DOOR SLIDE GIRT BAR HANGING LOW, OUT OF POSITION. REPOSITIONED GIRT BAR PER MT.

Part: SEAL — CRACKED (L/H HORIZ. STAB.) · airframe 43,210 hrs · 29,583 cycles

LEFT HORIZ STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED LEFT HORIZ STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31 AND SRM 51-40-02.

Part: SEAL — CRACKED (R/H HORIZ. STAB.) · airframe 43,210 hrs · 29,583 cycles

RIGHT HORIZ STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED RIGHT HORIZ STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31 AND SRM 51-40-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 41,422 hrs · 28,432 cycles

DIVERSION, UPON TAKEOFF FROM LAS GEAR DISAGREE. PERFORM QUICK REFERENCE HANDBOOK DIVERT TO PHX. ALL INDICATIONS NORMAL. PERFORMED GEAR RETRACTION, OPERATED NORMAL PER FIM TASK.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 40,752 hrs · 27,978 cycles

SUSPECT FAULTY CROSSFEED VALVE RESULTING IN AN IMBALANCE OF FUEL. R&R ENGINE FUEL CROSSFEED VALVE PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,873 hrs · 26,768 cycles

EXTERNAL POWER DOOR CUTOUT CRACKED AFT CORNER. REPAIRED CUTOUT PER SRM.

Part: FITTING — CRACKED (FED) · airframe 37,789 hrs · 26,080 cycles

FWD ENTRY DOOR UPPER AFFT TORQUE TUBE FITTING UPPER MOUNT SCREW HOLE HAS TWO CRACKS COMING OUT OF IT (MARKED). VERIFIED WITH HFEC NDT 51- 00-00 PART 6 PROCEDURE 23 / COMPLETED INSTALLATION OF FWD ENTRY DOOR; LEAK AND OPS CHECK GOOD REF AMM 52-11-00. TAG NO: 325302 PN ON: 141A6150-3M SN ON: 000819 PN OFF: SN OFF: 001718

Part: CRANK ASSY — MISSING (L1 DOOR) · airframe 37,789 hrs · 26,080 cycles

FORWARD ENTRY DOOR UPPER TORQUE TUBE AFT CRANK MISSING. R&R DOOR PER AMM.

Part: GUARD — MISSING (LIGHT SWITCH) · airframe 36,837 hrs · 25,471 cycles

AFT EMERGENCY LIGHT SWITCH COVER MISSING SPRING. R & R THE SWITCH GUARD IAW MM.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 36,837 hrs · 25,471 cycles

FWD CARGO BAY AFT CORNER SCUFF PLATE CRACKED / REPAIRED FWD CARGO BAY AFT CORNER SCUFF PLATE CRACKED PER EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 36,837 hrs · 25,471 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED / REPAIRED PER FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED PER EA 1-A53-2076 REV. 11

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 36,837 hrs · 25,471 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED / REMOVED AND REPLACED AFT CARGO BAY AFT CORNER SCUFF PLATE IAW MM 53-11-02-420-801 P/N. 7530220. 80641U 15SEPT2017. PRIOR TO REPLACEMENT WITH A SERVICABLE UNIT; CORNER SCUFF PLATE WAS WELDED PER EA 1-A53-2076 REV.11. SCUFF PLATE CRACKED AGAIN ON INSTALLATION; SERVIVEABLE UNIT WAS INSTALLED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

AFT CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 927 TO BS 947, RBL 20. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 794, RBL 20. R&R SUPPORT IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 36,837 hrs · 25,471 cycles

R/H HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STA 92.70, LOWER END OF THE FIRST VERTICAL STIFFENER FROM THE FRONT. REPAIRED RIB IAW SRM.

Part: SLIDE — FRAYED (R2 DOOR) · airframe 36,837 hrs · 25,471 cycles

R2 DOOR EMERGENCY ESCAPE SLIDE GIRT FRAYED. R&R SLIDE IAW MT.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 20. REPAIRED SUPPORT IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

AFT CARGO BAY SUB THRESHOLD CORRODED BETWEEN BS 791 TO BS 847, RBL 20. REPAIRED THRESHOLD IAW SRM.

Part: ANGLE — CRACKED (RIGHT WING) · airframe 36,837 hrs · 25,471 cycles

(RIGHT WING) T/E COVE SEAL RETAINING ANGLE CRACKED ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED RIGHT WING T/E COVE SEAL RETAINING ANGLE ABOVE #2 PYLON AFT TIP. IAW. SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 36,837 hrs · 25,471 cycles

LT WING UPPER TRAILING EDGE U SUPPORT BEAM TO REAR SPAR ATTACH ANGLE CRACKED AT RSS 80. R&R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, BETWEEN LBL15 TO RBL 15. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 36,837 hrs · 25,471 cycles

RT WING UPPER TRAILING EDGE PANEL SUPPORT ANGLE CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT. R&R ANGLE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 947, RBL 20. R&R SUPPORT IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 36,837 hrs · 25,471 cycles

RT WING LOWER TRAILING EDGE PANEL WAFFLE PLATE ATTACH FITTING CRACKED. R&R FITTING PER SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FORWARD CARGO BAY SUB THRESHOLD CORRODED BETWEEN BS 440 TO BS 495, RBL 20. R&R WEB PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 20. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

AFT CARGO BAY GRILL LINER SUPPORT CORRODED AT BS 727D, BETWEEN STR 22L TO STR 24L. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FORWARD CARGO AFT CENTER FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED BETWEEN LBL 21 TO RBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FORWARD CARGO AFT LT FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT LBL 22. R&R ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (LT WING) · airframe 36,837 hrs · 25,471 cycles

LT WING FIXED LEADING EDGE CRACKED AT WBL 71.24. R&R FRAME IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

AFT CARGO BAY PANEL 141PW AFT BULKHEAD SUPPORT BRACKET LOWER ANGLE CRACKED. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

AFT CARGO BAY GRILL LINER SUPPORT CORRODED AT BS 787, BETWEEN STR 22L TO STR 24L. REPAIRED SUPPORT IAW SRM AND DWG.

Part: PLATE — CRACKED (LEFT WING) · airframe 36,837 hrs · 25,471 cycles

LW LOWER FIXED TRAILING EDGE WIGGLE PLATE CRACKED JUST IB OF #1 PYLON TAILCONE / REMOVED AND REPLACED L/W LOWER FIXED T/E WIGGLE PLATE I/B OF #1 PYLON PER S.R.M. 51.40.02.0G.0 STEPS 4.B. AND PER BOEING DWG 115A2001

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 435 TO BS 440, RBL 30. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 493 TO BS 516, RBL 30. R&R SUPPORT IAW SRM AND DWG.

Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

PASSENGER CABIN WINDOW FRAME BETWEEN BS 685 TO BS 707 RT 2 LOWER NUT PLATE RECEPTACLES CORRODED. R&R NUTPLATES IAW SRM AND DWG.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

LT CABIN WINDOW FRAME CORRODED BETWEEN BS 707 TO BS 727. R&R FRAME IAW SRM & DWG.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

LT WINDOW FRAME CORRODED BETWEEN BS 500C TO BS 500B. R&R FRAME IAW SRM & DWG.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

LT CABIN WINDOW FRAME CORRODED BETWEEN BS 687 TO BS 707. R&R FRAME IAW SRM & DWG.

Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

PASSENGER CABIN WINDOW FRAME BETWEEN BS 639 TO BS 664, LT 2 LOWER NUT PLATE RECEPTACLES CORRODED. R&R NUTPLATES IAW SRM AND DWG.

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 36,837 hrs · 25,471 cycles

FCB FLOOR PANEL 120BF IS CORRODED / APPLICABILITY STATEMENT IAW SRM 53-30-53-01-1 FOR ID AND SRM 53-00-53-1A-1 FOR ALLOWABLE DAMAGE ARE APPLICABLE. REMOVED CORROSION ON AREA OF 12' X 2' X .010 ORIGINAL THICKNESS .071 FOUND TO BE OUT OF LIMITS IAW SRM 53-0053-1A-1. FABRICATED FLOOR PANEL 120BF OUT OF 2024T3 .071 LOT #1301872-1 AND APPLIED CONVERSION COATING AND PRIMER IAW SRM 51-20-01-0G-0 BOEING DWG #453A1610

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 36,837 hrs · 25,471 cycles

FCB FLOOR PANEL 120CF IS CORRODED / FABRICATED FORWARD CARGO FLOOR PANEL 120CF OUT OF 0.071 2029 T3 CIAD ITEM #2024T3 #0.071 LOT #1291186 IAW AMM 25-52-01-201-801 & BOEING DRAWING #453A1610. APPLIED CHEMICAL COVERSION COATING AND PRIMER PER AMM 51-21-41-370-802 & AMM 51-21-72-370-804. 57006U 14SEP17

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 36,837 hrs · 25,471 cycles

ACB FLOOR PANEL 140BF IS CORRODED / FABRICATED NEW FLOOR PANEL #140BF IAW SRM 53-60-53- 0I-1;SRM 51-40-05 AND DWG 453A2610. PRIOR TO FABRICATING PANEL; EVALUATED PANEL 140BF PER SRM 53-00-53-1A-1 PAR 5.A(1)(6) AND FOUND IT TO BE OUT OF LIMITS DUE TO MORE THEN 30% DAMAGED AREA.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 36,837 hrs · 25,471 cycles

ACB FLOOR PANEL 140AF IS CORRODED / OK TO APPLY CHEMICAL COVERSION COATING & PRIMER. FABRICATED ACB FLOOR PANEL 140AF OUT OF 0.071 2024T3 CIAD ITEM #2024T3# 0.071 X 48 SH-C LOT #1301872-1 IAW AMM 25-52-01-201-801 & BOEING DRAWING #4533A2610. 57006U 08SEP17 LEAD77 08SEP17 INSP390 09/08/17 APPIED CHEMICAL COVERSION COATING & PRIMER IAW AMM 51-21-72-370-804 & AMM 51-21-41-370-802. 51006U 08SEP17

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 36,837 hrs · 25,471 cycles

ACB FLOOR PANEL 140DF IS CORRODED / FABRICATED.NEW FLOOR PANEL #140DF IAW.SRM 53-70-53- 0I-1 SRM 51-40-05 AND DWG 453A2610. PRIOR TO FABRICATING PANEL; EVALUATED PANEL 140DF PER SRM 53-00-1A-1 PARAGRAPH 5 (A)(1)(B) AND FOUND IT TO BE OUT OF LIMITS DUE TO MORE THEN 30% DAMAGED AREA.

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 36,837 hrs · 25,471 cycles

FWD CABIN FLOOR PANEL 221DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 221DF WITH UPPER SKIN HAVING MULTIPLE AREASOF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 36,837 hrs · 25,471 cycles

LT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT STAB STA 92.70, LOWER END OF THE 3RD VERTICAL STIFFENER FROM THE FRONT. REPAIRED RIB IAW EA AND ER.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FLOOR INTERCOSTAL CRACKED AT BS 322, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 36,837 hrs · 25,471 cycles

FWD CABIN FLOOR PANEL 221EF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 221EF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 36,837 hrs · 25,471 cycles

FWD CABIN FLOOR PANEL 221GF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 221GF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FLOOR INTERCOSTAL CRACKED AT BS 323, RBL 31. R&R INTERCOSTAL IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 36,837 hrs · 25,471 cycles

RT HORIZONTAL STAB IN SPAR RIB AT 92.70 IS CRACKED ON THE LOWER END OF THE 3RD VERTICAL STIFFENER FROM THE FRONT. / REMOVED CRACK DAMAGE FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

L1 DOOR FORWARD GIRT BAR ATTACH FITTING CORRODED. R&R FITTING IAW SRM & DWG.

Part: NONE — CORRODED (MAIN CABIN) · airframe 36,837 hrs · 25,471 cycles

***CORROSION*** ON L/H MOPSILL; BS-302 TO BS-348; WL-207 / REMOVED AND REPLACED L/H FWD MOPSILL PER SRM 51-40-02 & DWG #141A8110

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 36,837 hrs · 25,471 cycles

RT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT 92.70, LOWER END OF THE 2ND VERTICAL STIFFENER FROM THE FRONT. REPAIRED RIB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

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

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 36,837 hrs · 25,471 cycles

FWD CABIN FLOOR PANEL 221BF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 221BF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 36,837 hrs · 25,471 cycles

FWD CABIN FLOOR PANEL 221CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 221CF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,837 hrs · 25,471 cycles

FLOOR INTERCOSTAL CRACKED AT BS 272, LBL 27. R&R INTERCOSTAL IAW DWG AND SRM.

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 36,837 hrs · 25,471 cycles

FWD CABIN FLOOR PANEL 222CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD CABIN FLOOR PANEL 222CF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 36,837 hrs · 25,471 cycles

FLOOR SUPPORT CRACKED AT BS-540; RBL-23; WL-207. / REMOVED AND REPLACED FLOOR SUPPORT AT BS 540 BL-0 TO RBL-25 WL 207 IAW SRM 51-40-02-0G-0 56208U 20AUG17 AND BOEING DWG D.R #143A0060 REV A

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 36,837 hrs · 25,471 cycles

RT HORIZONTAL STAB IN SPAR RIB AT 92.70 IS CRACKED ON THE LOWER END OF THE 4TH VERTICAL STIFFENER FROM THE FRONT. / REPAIRED RT. HORIZ. STAB IN-SPAR RIB AT 92.70 ON LOWER END OF THE 4TH VERTICAL STIFFENER FROM THE FRONT IAW EA 1-755-3795 REV IR AND ER 17-03850 REV IR.

Part: SCUFF PLATE — CORRODED (MAIN CABIN) · airframe 36,837 hrs · 25,471 cycles

R/H AFT MOP SILL IS CORRODED / LOCATED AND DRILLED NEW MOPSILL AT AFT SERVICE DOOR IAW SRM 51-40-05. INSTALLED IAW SRM 51-40-02 AND DWG 147A8501 88324U 22AUG17

Part: SCUFF PLATE — CORRODED (MAIN CABIN) · airframe 36,837 hrs · 25,471 cycles

L/H AFT MOP SILL IS CORRODED / LOCATED AND DRILLED NEW MOPSILL AT AFT ENTRY DOOR IAW SRM 51-40-05. INSTALLED IAW SRM 51-40-02 AND DWG 147A8501 88324U 23AUG17

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 36,837 hrs · 25,471 cycles

RT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 29. REPAIRED WEB IAW ER AND EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 36,837 hrs · 25,471 cycles

LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW SRM.