N7739A

Part: ACOUSTIC PANEL — DELAMINATED (ZONE 400) · airframe 61,980 hrs · 34,280 cycles

NR 2 ENGINE HAS TWO AFT ACOUSTICAL PANELS THAT ARE DELAMINATED LOCATED ABOVE AND BELOW THE 3 OCLOCK STRUT. REMOVED AND REPLACED THE AFT ACOUSTICAL PANELS IAW AMM 72-23-02.

Part: HANDLE — LOOSE (ZONE 800) · airframe 61,980 hrs · 34,280 cycles

FWD SERVICE DOOR INNER HANDLE LOOSE. SECURED FWD SERVICE DOOR INNER HANDLE IAW AMM 20-50-11.

Part: MOUNT — CRACKED (ZONE 800 SLIDE) · airframe 61,980 hrs · 34,280 cycles

FWD SERVICE DOOR AFT SLIDE MOUNT ISOLATOR CRACKED. R & R FWD SERVICE DOOR AFT SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.

Part: MOUNT — DAMAGED (ZONE 800 SLIDE) · airframe 61,980 hrs · 34,280 cycles

AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATORS DAMAGED. R & R AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATORS IAW SRM 51-40-02.

Part: HANDLE — LOOSE (ZONE 800) · airframe 61,131 hrs · 33,714 cycles

FWD ENTRY DOOR CLOSE ASSIST HANDLE IS LOOSE<[01] SECURED FWD ENTRY DOOR CLOSE ASSIST HANDLE; REF. AMM 52-11-31.

Part: FASTENER — MISSING (GIRT BAR) · airframe 60,072 hrs · 33,095 cycles

FWD SVC DOOR SLIDE COVER GRIT BAR RETAINER CLIP MISSING FASTENER. REFERENCE MXI #TTG8Q00ZZBXA<[01] SECURED FWD SVC DOOR ESCAPE SLIDE GRIT BAR AFT RETAINER CLIP IN REFERENCE TO SRM 51-40-02 AND AIPC 25-66-00.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 59,976 hrs · 33,037 cycles

FORWARD SERVICE DOOR GRIT BAR AFT RETAINER TAB LOOSE <[01]. INSTALLED HARDWARE IN FWD SVC DOOR AFT GIRT BAR IN REF TO EA M-23-125-01839.

Part: LIGHT — OUT OF ADJUST (ZONE 200) · airframe 59,860 hrs · 32,969 cycles

PASSENGER CABIN SEAT ROW 24 ABC PHOTOLUMINESCENT STRIPS HAS LARGE GAP<[01] REPLACED STRIP PER AMM 33-51-15;[02] INSPECTION C/W REPLACED STRIP PER AMM 33-51-15

Part: SEAL — CRACKED (ZONE 300) · airframe 59,860 hrs · 32,969 cycles

LEFT HAND HORIZONTAL STAB UPPER SLIDER SEAL CRACKED.<[01] REMOVED AND REPLACED SEAL PER AMM 53-31-31.;[02] C/W INSP. REMOVED AND REPLACED SEAL PER AMM 53-31-31.

Part: GIRT BAR — LOOSE (ZONE 800) · airframe 59,235 hrs · 32,590 cycles

FORWARD GALLEY DOOR GIRT BAR RETAINING BRACKET LOOSE<[01] RE-SECURE FWD GALLEY DOOR GIRT BAR BRACKET PER AMM 25-66-01.

Part: GROUND STUD — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

L1187 EMERGENCY EXIT INDICATOR LIGHT BS 304 WL229 LBL 67 INOP<[01] PERFORMED TROUBLESHOOTING PER WDM 33-51-21 FOUND WIRE W4142-0152-20 PULL FROM GROUND BLOCK GD3782-DC;[02] VERIFIED;[03] OK TO INSTALL STEP 1;[04] PERFORMED TROUBLESHOOTING PER WDM 33-51-21 FOUND WIRE W4142-0152-20 PULL FROM GROUND BLOCK GD3782-DC.<BR>TERMINATED WIRE W4142-0152 INTO GROUND BLOCK GD3782 PER SWPM 20-90-15. <BR> <BR>PERFORMED GOOD FUNCTIONAL TEST OF EMERGENCY EXIT LOCATOR LIGHT AT BS 304 WL 299 LBL 67 (LOWER; AFT; OUTBOARD EDGE OF FWD LAV) PER AMM 33-51-00-710-801.;[05] VERIFIED CORRECTIVE ACTION COMPLETE.

Part: SLIDE — NOT SEATED (ZONE 800) · airframe 57,940 hrs · 31,798 cycles

FED DOOR ESCAPE SLIDE SHROUD NOT FULLY SEATED (LOWER PIN NOT ENGAGED)<[01] REMOVED AND INSTALLED PER AMM 25-66-01-400-803-NG ESCAPE SLIDE PACK AND COVER INSTALLATION - LOWER PIN IN-SERVICE;[02] VERIFIED CORRECTIVE ACTION #1

Part: SUPPORT — CRACKED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

BREAKER PANEL AT BS 540 LBL 0 - LBL 25 CRACKED<[01] REMOVED AND REPLACED BREAKER PANEL ASSY AT BS 540 LBL 0-25 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A5240;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: SUPPORT ANGLE — BROKEN (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

SUPPORT ANGLE ON FORWARD SIDE OF BS 663 VAPOR BARRIER IS BROKEN RBL 27 WL 150<[01] LOCATED AND DRILLED 1 EA ANGLE P/N 149A7218Y8 PO# 986123 AND 1 EA CLIP P/N 149A7627U6 PO# 986130 IAW SRM 51-40-05 AND DWG 149A7216 REV: A<BR>ANGLE AND CLIP GOING TO BE INSTALL ON W/C TTG8Q00ULSUF STEP 3;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD PASSENGER COMPARTMENT WET AREA; CRACK ON INTERCOSTAL WL 208 BS 344+5 CENTERLINE.<[01] DAMAGE EXCEEDS LIMITATIONS PER SRM 53-10-51-1A-1. REMOVED AND REPLACED INTERCOSTAL AT STA 344-360; LBL 11; PER SRM 51-40-02-0G-0; REF BOEING DWG 141A5400 SHEET 34;[02] VERIFIED CORRECTIVE ACTION STEP 1.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD PASSENGER COMPARTMENT WET AREA; CORROSION ON INTERCOSTAL WL 208 BS 276+14 CENTERLINE.<[01] REMOVED AND REPLACED INTERCOSTAL AT STA 277-294; WL 208; BL-0 PER SRM 51-40-05-0G-0.;[02] VERIFIED CORRECTIVE ACTION STEP 1.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

PASSENGER CABIN FLOOR PANEL 241AF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 241AF WITH DELAMINATION WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD PASSENGER COMPARTMENT WET AREA; CRACK ON FLOOR BEAM WL 208 BS 295.5 RBL 52.<[01] REMOVED DAMAGED AREA OF FLOOR BEAM AND REPAIRED AT BS 295.5 RBL 26 TO RBL 64 WL 208 IAW SRM 53-10-51-2R-16.;[02] TASK COMPLETED;[03] VERIFIED STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD PASSENGER COMPARTMENT WET AREA; CORROSION ON INTERCOSTAL WL 208 BS 294.5 TO 312 LBL 12.<[01] VERIFIED SRM 53-10-51-1A-1 IS APPLICABLE. MATERIAL LOSS EXCEED ALLOWABLE LIMITS GIVEN THEREFORE SRM 51-10-02-0G-0 PAR.9.A(1) REPLACEMENT OF THE PART IS APPLICABLE. REMOVED INTERCOSTAL BS 294.5 TO 312 LBL 12 WL208-WL200 I.A.W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW INTERCOSTAL BS294-BS312 LBL12 WL208-WL200 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 141A5600 REV N. OK TO INSTALL. INSTALLED INTERCOSTAL AT STA 294-312; LBL 12 PER SRM 51-40-02-0G-0 AND BOEING DRAWING 141A5600 REV:N.;[02] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.;[03] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD PASSENGER COMPARTMENT WET AREA; CRACK ON INTERCOSTAL WL 208 BS 344+6 RBL 31.<[01] REMOVED AND INSTALLED REPLACEMENT INTERCOSTAL WL 208; BS 344 TO 360; RBL 31 IAW SRM 51-40-02-0G-0.;[02] REJECTION: FLOOR INTERCOSTAL INSTALATION AT STA 344 RBL 31 HAS 2 MISSING FASTENERS AND ONE PARTIALY INSTALLED FASTENER. SEE FAULT [TTG8Q00UWKUX];[03] CORRECTED REJECTION ITEMS ON TASK TTG8Q00UWKUX;[04] VERIFIED CORRECTIVE ACTION ENTRIES 1-3

Part: JUMPER — CORRODED (ZONE 500) · airframe 57,940 hrs · 31,798 cycles

CORROSION ON LOWER BONDING JUMPER TO AFT BOOST PUMP TANK #1.<[01] REMOVED AND REPLACED LOWER BONDING JUMPER TO AFT BOOST PUMP TANK #1 IAW AMM 28-22-41-400-801. SEE PREVIOUS STEPS TO VERIFY.;[02] VERIFIED CORRECTIVE ACTION STEP 1.

Part: BALANCE WEIGHT — CORRODED (ZONE 500) · airframe 57,940 hrs · 31,798 cycles

LH WING TE; LOWER O/B FIXED TE ACCESS PANEL; I/B AILERON BALANCE WEIGHT ORSS 514+14 HAS CORROSION.<[01] REMOVED AND REPLACED AILERON BALANCE WEIGHT IAW CMM 57-50-26;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: BONDING JUMPER — CORRODED (ZONE 500) · airframe 57,940 hrs · 31,798 cycles

LH WING TE; LOWER O/B FIXED TE ACCESS PANEL; AILERON TRANSMITTER BONDING JUMPER SCREW HAS CORROSION.<[01] REMOVED AND INSTALLED LH WING AILERON POSITION TRANSMITTER BONDING JUMPER GROUNDING TERMINAL IAW SWPM 20-20-10;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD SERVICE DOOR CUTOUT SURROUND STRUCTURE; AFT FACE TO THE DOOR FRAME WL 208 RBL 55 BS 291.5+4 HAS CRACK.<[01] TRIMED OUT DAMAGE PART OF THE STUB FRAME AND FABRICATED; LOCATED; DRILLED AND ISTALLED NEW CLIP AT BS 291.5+4 RBL 55 WL 208 IAW SRM 53-10-15-2R-7;[02] TASK COMPLETED;[03] VERIFIED STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: STRAP — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP WL 208; LBL 5; BS 1016+14.<[01] REMOVED AND REPLACED NEW TENSION STRAP LBL5 BS1006-BS1030 WL208 I.A.W SRM 51-40-02-0G-0.;[02] INSTALLED NEW TENSION STRAP LBL5 BS1006-BS1030 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV B;[03] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.;[04] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON FLOOR BEAM BS 986.5 LBL 35 TO 45.<[01] REMOVED AND REPAIRED BS986 L/H FLOOR BEAM UPPER CHORD RBL 36 TO RBL 48 I.A.W SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4;[02] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.;[03] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD ENTRY DOOR CUTOUT SURROUND STRUCTURE; INTERCOSTAL BS 303.9+8 S-6L HAS CRACK.<[01] HFEC INSPECTED FRAME AT BS 303.9+8' STR 6L PER 737NDT PART 6 51-00-00 PROCEDURE 23. FOUND CRACK ON EDGE OF EXISTING TRIM OUT. MARKED END OF CRACK WITH BLACK SHARPIE; CRACK MEASURES .130' IN LENGTH FROM EDGE. REMOVED CRACK BY 0.150' ON THE EXISTING TRIM OUT RADIUS AT BS 303.9+8' STR 6L IAW SRM 51-10-02. HFEC INSPECTED CUT-OUT AREA IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR>EQUIP USED: -NORTEC 600 ID: ATS2353 CAL DUE: 01/2025;[02] VERIFIED CORRECTIVE ACTION STEP 1.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

R/H UPPER ATTACH ANGLE BS 663 RBL 6 WL 165 CRACKED (MARKED) B.S. 663 R/H LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT RBL 6 W.L. 165.<[01] REMOVED AND REPLACED R/H UPPER ATTACH ANGLE VAPOR BARRIER BS 664 WL 165 IAW SRM 51-40-02 AND DWG 111A1000 REV:A

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON CROSSBEAM SEVERAL AREAS WL 208;BS 986.6; RBL 27 TO RBL 48.<[01] REMOVED AND REPAIRED BS986 R/H FLOOR BEAM UPPER CHORD RBL 34 TO RBL 48 I.A.W SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4;[02] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.;[03] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.

Part: FITTING — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT PASSENGER COMPARTMENT; VERTICAL FIN FRONT SPAR FITTING; BS 1016 CENTERLINE WL 283 CORROSION ON BOTH ATTACH POINTS GALLEY.<[01] REPLACED BOTH BUSHINGS AND CLIPS ON AFT PASSENGER COMPARTMENT;VERTICAL FIN FRONT SPAR FITTINGS; BS 1016 CENTERLINE WL 208 IAW AMM USE OF STANDARD INDUSTRY PRACTICES;[02] VERIFIED CORRECTIVE ACTION ITEM; CARD COMPLETE.

Part: SHEAR WEB — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON SHEAR WEB SEVERAL AREAS LBL 7 TO 13; BS 1016+10; 1016+16; AND LBL 17; BS 1016+5.<[01] REMOVE AND INSTALL L/H BS1016-BS1030 WL208 SHEAR WEB IAW SRM 51-40-02-0G-0;[02] REMOVED AND INSTALLED L/H BS1016-BS1030 WL208 SHEAR WEB IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV B;[03] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.;[04] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.

Part: STRAP — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP WL 208; RBL 5; BS 1006+2; 1016; 1016+10 TO 1016+14.<[01] TENSION STRAP TO BE REMOVED AND REPLACED ON CCN TTG8Q00UP776 DUE TO CORROSION DAMAGE AND NOT ALLOWABLE ENTRIES ON SRM I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] RII ITEMS TO BE ACCOMPLISHED ON TTG8Q00UP776

Part: STRAP — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP LBL 28; BS 1016+1; 1016+14; 1016+8.<[01] REMOVED AND INSTALLED NEW TENSION STRAP BS1006-BS1024 LBL28 WL208 I.A.W SRM 51-40-02-0G-0;[02] REMOVED AND INSTALLED NEW TENSION STRAP BS1006-BS1024 LBL28 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV B;[03] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.;[04] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.

Part: STRAP — CORRODED (ZONE 20) · airframe 57,940 hrs · 31,798 cycles

AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP LBL 18; BS 1016+9 TO 1016+14.<[01] REMOVED AND INSTALLED NEW TENSION STRAP BS 1006-1028 LBL 18 WL 208 IAW SRM 51-40-02-0G-0;[02] REMOVED AND INSTALLED NEW TENSION STRAP BS 1006-1028 LBL 18 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV B;[03] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.;[04] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.

Part: FORMER — CRACKED (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

R/H FAIRING FORMER BS 500D BETWEEN STRINGER 18 R/H AND 19 R/H IS CRACKED<[01] REMOVED AND REPLACED FAIRING FORMER AT BS 500D BETWEEN STR 18R TO STR 19R; WL 188 PER SRM 51-40-02 AND DWG:116A3010; ID:0029; REV: B.;[02] VERIFIED.

Part: SHEAR WEB — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON SHEAR WEB SEVERAL AREAS LBL 5; BS 1016+2; 1016+16.<[01] REMOVE AND REPLACE ACCOMPLISHED ON CCN TTG8Q00UQ37R;[02] UPDATED TABLE MEASUREMENT;[03] VERIFIED. CARD COMPLETE.

Part: STRAP — CORRODED (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

AFT PASSENGER COMPARTMENT WET AREA; CORROSION ON TENSION STRAP WL 208; RBL 18; BS 1016+12.<[01] REMOVED AND REPLACED TENSION STRAP BS 1006-1028 RBL 18 WL 208 IAW SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED TENSION STRAP BS 1006-1028 RBL 18 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV A;[03] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.;[04] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.

Part: SUPPORT PLATE — CORRODED (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] REMOVE AND REPLACE SIDEWALL SUPPORT AT ACB BETWEEN BS 727+4' TO BS 767 RBL 22 WL 156 PER SRM 51-40-02 AND BOEING DWG 146A7500 ID:0085 REV: A.;[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] REMOVED AND REPLACED ANGLE UNDER SHIELD AT ACB BETWEEN BS 767 TO BS 787+6' ;RB 21; WL 156 PER SRM 51-40-02 AND DWG:146A8123;ID:0016;REV:-;[02] REJECT: ONE SOLID RIVET HEAD DAMAGED; SEE NON-ROUTINE TTG8Q00V08GJ;[03] REMOVED AND REPLACED DAMAGED FASTENER ON FAULT TTG8Q00V08GJ<BR>PER SRM 51-40-02-0G-0 AND DWG 146A8123;[04] VERIFIED CORRECTIVE ACTION STEP 3.

Part: STRAP — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

MAIN CABIN FLOORBOARD AREA AT RBL 6; WL 208 & STA 1028 APPROX; FOUND CORROSION AT PLATE MARKED<[01] REMOVED AND INSTALLED NEW TENSION STRAP RBL6 BS1006-BS1028 WL208 I.A.W SRM 51-40-02-0G-0;[02] REMOVED AND INSTALLED NEW TENSION STRAP RBL6 BS1006-BS1028 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 REV B;[03] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.;[04] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.

Part: SHIELD — CORRODED (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AND REPLACED SHIELD AT ACB BETWEEN BS 767 TO 787+6';RBL 22; WL 156 PER SRM 51-40-02 AND DWG:146A0081;ID:0034;REV:-;[02] VERIFIED CORRECTIVE ACTION STEP 1.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

MAIN CABIN FLOORBOARD AREA AT RBL 6; WL 208 & STA 1008 APPROX; FOUND 1EA MISDRILLED HOLE AT PLATE MARKED<[01] TENSION STRAP TO BE REMOVED AND REPLACED ON CCN TTG8Q00UP776 DUE TO CORROSION DAMAGE AND NOT ALLOWABLE ENTRIES ON SRM I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] VERIFIED;[03] RII ITEMS TO BE ACCOMPLISHED ON TTG8Q00UP776

Part: STRAP — CORRODED (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6 RBL11.5 WL156<[01] EVALUATED CORROSION ON STRAP BS 767+6 RBL 11.5 WL 156; FOUND TO BE OUT OF LIMITS; RECEIVED NEW STRAP AND APPLIED WHITE ENAMEL; NEW STRAP TO BE INSTALLED ON FAULT TTG8Q00TTPUL;[02] VERIFIED CORRECTIVE ACTION STEP 1.

Part: SUPPORT PLATE — CORRODED (ZONE 100) · airframe 57,940 hrs · 31,798 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 SIDEWALL SUPPORT AT ACB BETWEEN BS727+4 TO BS 847 LBL 22 WL 156 PER SRM 51-40-02. AND BOEING DWG 146A7502 ID:0086 REV:A;[02] CORRECTION TO DRAWING REFERENCE; IT SHOULD READ INSTALLED PER DWG 146A0061 SHEET 86 AND DWG 146A7500 SHEET 85;[03] VERIFIED CORRECTIVE ACTION STEP 2.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-O PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] ATTACHED CURE SHEET.;[03] VERIFIED CORRECIVE ACTIONS 1 & 2.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241XF AFT FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 147A5810 ID: 0060.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FLOOR PANEL 232DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221EF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FLOOR PANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-O PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-O PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT FLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241VF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221BF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD FLOOR PANEL 221A UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221A UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-O PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ABF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD FLOOR PANEL 222A UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222A UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT FLOOR PANEL 242SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241XF AFT UPPER SURFACE DAMAGE HAS BE REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 147A5810 ID: 0058.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AAF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD FLOOR PANEL 222B UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222B UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD FLOOR PANEL 232BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FORWARD FLOOR PANEL 232BF UPPER SKIN; WITH AREAS OF PULLED STRANDS; WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AEF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT FLOOR PANEL 242RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242RF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FLOOR PANEL 232FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

AFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF; UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

FWD FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

RIGHT BS663 VAPOR BARRIER WEB CRACKED AT RBL17 (MARKED)<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

LEFT BS663 VAPOR BARRIER WEB CRACKED AT LBL44 (MARKED)<[01] REPAIR TO BE ACCOMPLISHED ON FAULT#TTG8Q00ULQ9C.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

RIGHT BS663 VAPOR BARRIER WEB CRACKED AT RBL40 (MARKED)<[01] RIGHT BS663 VAPOR BARRIER WEB CRACKED AT RBL40 WILL BE REPAIRED ON FAULT# TTG8Q00ULQ9Q;[02] VERIFIED.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 57,940 hrs · 31,798 cycles

LEFT VAPOR BARRIER WEB CRACKED AT LBL32 (MARKED)<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: SKIN — CRACKED (ZONE 600 SLAT) · airframe 57,940 hrs · 31,798 cycles

#7 SLAT L/E BULLNOSE IS CRACKED AT FASTENER AT ACTUATOR ATTACH POINT; MARKED<[01] UPDATED TABLE TO RII;[02] REPAIRED LEADING EDGE SLAT NOSE SKIN EXTERNAL DOUBLER REPAIR AT THE ACTUATOR RIB I.A.W &NBSP;&NBSP;&NBSP;&NBSP;&NBSP;SRM 57-42-01-2R-8

Part: SUPPORT — CRACKED (ZONE 500) · airframe 57,940 hrs · 31,798 cycles

LH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT O/B RIVET HAS CRACK.<[01] REMOVED AND REPLACED LH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL TRANSVERSE SUPPORT AND O/B RIVET PER SRM 51-40-02-0G-0 STEP 4

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

EMERGENCY BATTERY PACK M1672 FAIL CAPACITY TEST<[01] PARTS UPDATE;[02] VERIFIED;[03] REMOVED; REPLACED; AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY BATTERY PACK M1672 PER AMM 33-51-00-720-801; AND AMM 33-51-06-960-805.;[04] VERIFIED CORRECTIVE ACTION COMPLETE.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

EMERGENCY BATTERY PACK M1675 FAIL CAPACITY TEST<[01] REMOVED AND REPLACED M1675 BATTERY PACK PER AMM 33-51-06-960-805.;[02] EMERGENCY BATTERY PACK M1675 WAS REMOVED; REPLACED AND GOOD OPS CHECK WAS PERFORMED PER AMM 33-51-06-960-805<BR><BR>CARD COMPLETE;[03] VERIFIED;[04] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: SUPPORT BEAM — CRACKED (ZONE 500) · airframe 57,940 hrs · 31,798 cycles

LH WING TE: DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM ORRS 261+8 AFT END HAS CRACK.<[01] REMOVED AND REPLACED LH WING TE DEFLECTION CONTROL RIB; FIXED UPPER PANEL MID SUPPORT BEAM AFT END FITTING ORRS 261+8 IAW SRM 51-10-02-0G-0 PAR 9.A AND SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION TAKEN AND TASK CARD COMPLETED.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 57,940 hrs · 31,798 cycles

EMERGENCY BATTERY PACK M1669 FAIL CAPACITY TEST<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1669 PER AMM 33-51-06-960-805.<BR><BR>TEST STILL REQUIRED.;[02] UPDATED PARTS;[03] VERIFIED;[04] VERIFIED PARTS;[05] VERIFIED CORRECTIVE ACTION #1;[06] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1669 PER AMM 33-51-06-960-805. AND FUNCTIONAL TEST FOR EMERGENCY BATTERY PACK M1669. PER AMM 33-51-06-960-805. GOOD TEST.<BR><BR>COMPLETED STEP 1;[07] OK;[08] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 57,790 hrs · 31,704 cycles

1EA OUTSIDE EMERGENCY LIGHT L/H SIDE AFT OF WHEEL WELL INOP. REMOVED AND REPLACED PER [AMM 33-51-04-960-802-NG (SLIDE/OVERWING LIGHT - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]

Part: LANDING GEAR — MALFUNCTIONED · airframe 57,036 hrs · 31,233 cycles

GEAR RAISED NORMAL AFTER T/O. WHEN GEAR HANDLE LOWERED TO OFF NOSE GEAR EXTENDED WITH BOTH RED/GREEN NOSE GEAR LIGHTS ON. FOLLOWED QRH AND PUT GEAR HANDLE TO UP POSITION AND NOSE GEAR RETRACKED AND GEAR RAISED NORMAL AFTER T/O. WHEN GEAR HANDLE LOWERED TO OFF NOSE GEAR EXTENDED WITH BOTH RED/GREEN NOSE GEAR LIGHTS ON. FOLLOWED QRH AND PUT GEAR HANDLE TO UP POSITION AND NOSE GEAR RETRACKED AND LEFT THE GEAR HANDLE IN UP POSITION FOR REST OF FLIGHT.<[01] PERFORMED PSU BITE CK; NO FAULT HISTORY; PSU BITE CK GOOD NO FAULTS. PERFORMED NOSE GEAR SWING; NOSE GEAR AND NOSE LANDING GEAR INDICATION SYSTEMS OPS CK GOOD; NO FAULTS FOUND AS PER FIM 32-30-810; AMM 32-61-00; 07-11-21.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,386 hrs · 30,834 cycles

EXTERIOR EMERGENCY LIGHT INOP AFT OF L2 DOOR.<[01] REMOVED AND REPLACED EMERGENCY LIGHT AFT OF L2. OPS CHECK GOOD. REF 33-51-04

Part: LINK ASSY — CRACKED (ZN 700 LANDING G) · airframe 55,854 hrs · 30,507 cycles

DURING INSTALLATION OF PANEL 551FB MLG BEAM LOWER STABILIZER LINK CRACKED LINK ASSY-STAB P/N 115A1211-5<[01] C/W MT

Part: BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 55,854 hrs · 30,507 cycles

BRACKET ON AFT SPAR LEFT SIDE STATION 162.5 IS CRACKED. CW EA 23-157-03464.

Part: WIRE — DAMAGED (ZN 200 FUS TOP) · airframe 55,698 hrs · 30,408 cycles

ON APPROACH INTO BWI; ON CONFIGURATION; FLAPS SELECTED 5 DEGREES. FLAPS DID NOT MOVE. RAN TRAILING EDGE FLAP DISAGREE NNC. FLAPS TE AND LE DEVICES EXTENDED NORMALLY TO 15 DEGREES USING ALT FLAP EXT PROCEDURE.<[01] REF BARCODE # TTG8Q00PD8CV FOR WIRING REPAIR OF T/E FLAP SYSTEM. T/E FLAPS OPS CHECK GOOD IAW AMM 27-51-00. TROUBLESHOT PER WDM 27-52-11 & FOUND WIRE NUMBERS W1022-2006 & W1022-2007 DAMAGED IN THE WHEEL WELL NEXT TO #4 SKEW SENSOR .REPAIRED WIRES PER SWPM 20-10-13 AND 20-60-02.ALL SYSTEM OPERATIONAL TEST CHECKED GOOD. TEST GOOD

Part: LENS — INOPERATIVE (ZN 200 FUS TOP) · airframe 55,624 hrs · 30,359 cycles

L/H OVERWING EXIT AFT EMERGENCY LIGHT INOP<[01] R&R CABIN OVERWING EXIT LIGHT AND BOTH LIGHT LENSES PER AMM 33-51-01

Part: PLUG — FAULTY (ZN 100 FUS LOWER) · airframe 54,917 hrs · 29,910 cycles

NO MOVEMENT OF FLAPS ON INITIAL EXTENSION. FLAPS LOCKED OUT @ 0 - NO INDICATIONS. LANDED WITH USE OF ALTERNATE FLAP EXTENSION. FLAPS EXTENDED TO 15. BRAKE COOLING MODULE INDICTED 21.4M FT/LBS. NORMAL NO MOVEMENT OF FLAPS ON INITIAL EXTENSION. FLAPS LOCKED OUT @ 0 - NO INDICATIONS. LANDED WITH USE OF ALTERNATE FLAP EXTENSION. FLAPS EXTENDED TO 15. BRAKE COOLING MODULE INDICTED 21.4M FT/LBS. NORMAL PARK @ GATE - F15 VREF/VT 136/150.<[01] PERFORMED INSULATION TEST TO T/E FLAP TRANSMITTER WIRING NO DEFECTS NOTED. FOR PRECAUTION R/R BOTH PLUG AND RECEPTACLE AT D40024 AND ALSO FLAP TRANSMITTER PLUG A/C SIDE R FORMED OPS CK ALL OPERATED NORMALLY PER 20-10-80;[02] REF FOR C/P R/R 20-51-11<BR>REF FOR INSULATION TEST 20-40-11

Part: RECEPTACLE — FAULTY (ZN 100 FUS LOWER) · airframe 54,917 hrs · 29,910 cycles

NO MOVEMENT OF FLAPS ON INITIAL EXTENSION. FLAPS LOCKED OUT @ 0 - NO INDICATIONS. LANDED WITH USE OF ALTERNATE FLAP EXTENSION. FLAPS EXTENDED TO 15. BRAKE COOLING MODULE INDICTED 21.4M FT/LBS. NORMAL NO MOVEMENT OF FLAPS ON INITIAL EXTENSION. FLAPS LOCKED OUT @ 0 - NO INDICATIONS. LANDED WITH USE OF ALTERNATE FLAP EXTENSION. FLAPS EXTENDED TO 15. BRAKE COOLING MODULE INDICTED 21.4M FT/LBS. NORMAL PARK @ GATE - F15 VREF/VT 136/150.<[01] PERFORMED INSULATION TEST TO T/E FLAP TRANSMITTER WIRING NO DEFECTS NOTED. FOR PRECAUTION R/R BOTH PLUG AND RECEPTACLE AT D40024 AND ALSO FLAP TRANSMITTER PLUG A/C SIDE R FORMED OPS CK ALL OPERATED NORMALLY PER 20-10-80;[02] REF FOR C/P R/R 20-51-11<BR>REF FOR INSULATION TEST 20-40-11

Part: TRANSMITTER — FAULTY (ZN 100 FUS LOWER) · airframe 54,597 hrs · 29,718 cycles

TRAILING EDGE FLAP DISAGREE WHEN FLAP HANDLE WAS MOVED FROM UP TO FLAPS 5. POSITION<[01] PERFORMED FSEU BITE AND FOUND FAULT CODE 27-52259. R/R LT FLAP POSITION TRANSMITTER REF AMM 27-58-01. OPS CK GOOD.

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 53,826 hrs · 29,203 cycles

RIGHT SIDE EMERGENCY 'EXIT' SIGN LENSE BROKE<[01] C/W EA M-21-133-00720 SECURED R/H OVERWING EMERGENCY EXIT SIGN LENS.

Part: MEGAPHONE — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 52,713 hrs · 28,475 cycles

F/A FWD MEGAPHONE INOP / [01] R&R FWD MEGAPHONE BATTERIES IAW AMM 25-64-00

Part: NONE — DAMAGED (PAX CABIN) · airframe 52,268 hrs · 28,178 cycles

EXIT ROW F/O SIDE EXIT LENS / [01] REMOVED AND REPLACED F/O EMER EXIT ROW EXIT LENS IAW AMM 33-51-01. A/C OK FOR SERVICE.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 52,043 hrs · 28,014 cycles

F/A REPORTS FWD ENTRY DOOR SLIDE RETAINING CLIPS; NOT SECURING SLIDE PROPERLY. / [01] ADJUSTED FWD ENTRY DOOR GRIT BAR CLIPS PER SIP.

Part: FLASHLIGHT — MISSING (FWD GALLEY) · airframe 52,033 hrs · 28,008 cycles

FWD GALLEY AREA EMERGENCY FLASH LIGHT WITH SAFETY STRAPS MISSING 1EA EACH FLASH LIGHT 2022-384092 / [01] INSTALLED FWD GALLEY AREA EMERGENCY FLASH LIGHT WITH SAFETY STRAPS 1EA EACH FLASH LIGHT IAW ASTRONIC REV. 10 DATE 01-JUL-20 CMM 25-60-02 PAGE 7001 STEP 2.B.(2); PAGE 10006 AND PAGE 10009 ITEM 16;[02] INSTALLED FWD GALLEY AREA EMERGENCY FLASH LIGHT WITH SAFETY STRAPS 1EA EACH FLASH LIGHT IAW ASTRONIC REV. 10 DATE 01-JUL-20 CMM 25-60-02 PAGE 7001 STEP 2.B.(2); PAGE 10006 AND PAGE 10009 ITEM 16

Part: WEB — ELONGATED (AFT CARGO) · airframe 52,033 hrs · 28,008 cycles

ELONGATED HOLE WEB - INTERCOSTAL BTW BS 727A TO 727B AT LEVEL LBL 21 AT AFT CARGO COMPARTMENT 2022-384048 / [01] REPLACED WEB-INTERCOSTAL LOC. BTW BS 727A TO 727B AT LEVEL LBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02;SRM 51-40-02 AND DWG 146A7500 REV - SHEET 36.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] COMPLETE TASK CERTIFIED RII

Part: ANGLE — CRACKED (R2 DOOR) · airframe 52,033 hrs · 28,008 cycles

CRACK ACCESS PANEL 844DZ SERVICE DOOR SUPPORT ANGLE AT AFT GALLEY AREA 2022-384046 / [01] REPLACED ACCESS PANEL 844DZ SERVICE DOOR SUPPORT ANGLE AT AFT GALLEY AREA IAW SRM 51-40-05-0G-0;[02] REPLACED ACCESS PANEL 844DZ SERVICE DOOR SUPPORT ANGLE AT AFT GALLEY AREA IAW SRM 51-40-05-0G-0. COMPLETED

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 52,033 hrs · 28,008 cycles

CRACK LEADING EDGE RIB AT L/E STA 114.55 AT LT HORIZONTAL STABILIZER 2022-384011 / [01] REPLACED RIB LT STA 114.55 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV:B SHEET:1 <BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] STEP 1 VERIFIED AND CORRECTIVE ACTION COMPLETED: ITEM RII REPLACED RIB LT STA 114.55 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV:B SHEET:1

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 52,033 hrs · 28,008 cycles

CRACK LEADING EDGE RIB AT L/E STA 95.96 AT LT HORIZONTAL STABILIZER 2022-384009 / [01] REPLACED NEW RIB LOCATED LEADING EDGE RIB AT L/E STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G-0 AND DWG 186A1001 REV:B SHET:1 <BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] STEP 1 VERIFIED AND CORRECTIVE ACTION COMPLETED: REPLACED NEW RIB LOCATED LEADING EDGE RIB AT L/E STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G-0 AND DWG 186A1001 REV:B SHET:1;[03] CORRECTED STEP 2 : VERIFIED AND CORRECTIVE ACTION COMPLETED ITEM RII : REPLACED NEW RIB LOCATED LEADING EDGE RIB AT L/E STA 95.96 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G-0 AND DWG 186A1001 REV:B SHET:1

Part: SUPPORT ANGLE — BROKEN (FUSELAGE) · airframe 52,033 hrs · 28,008 cycles

BROKEN SUPPORT ANGLE BS 867 BTW STR 2R AND STR 3R AT PASSENGER CABIN 2022-384008 / [01] REPLACED SUPPORT ANGLE LOCATED BS 867 BTW STR 2R AND STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A7901 SHEET: 22 REV: A.<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED STEP 1<BR>REPLACED SUPPORT ANGLE LOCATED BS 867 BTW STR 2R AND STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A7901 SHEET: 22 REV: A.;[03] REPLACED SUPPORT ANGLE LOCATED BS 867 BTW STR 2R AND STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A7901 SHEET: 22 REV: A. RII VERIFIED

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 52,033 hrs · 28,008 cycles

CRACK LEADING EDGE RIB AT L/E STA 105.26 AT LT HORIZONTAL STABILIZER 2022-384010 / [01] REPLACED RIB LT STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV:B SHEET:1 <BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] STEP 1 VERIFIED AND CORRECTIVE ACTION COMPLETED: ITEM RII : INSTALLED RIB LT STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG : 186A1001 REV: B SHEET:1

Part: STRINGER — CRACKED (FWD CARGO) · airframe 52,033 hrs · 28,008 cycles

CRACK STRINGER 26R LOCATED BS540 AT FWD CARGO COMPARTMENT 2022-384004 / [01] TOOL USED P/N 45 MG S/N 130060401 DUE DATE 23/JAN/23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23;[03] PERFORMED PERMANENT REPAIR STRINGER 26R LOCATED BTW BS500D TO BS540 IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. MATERIAL USED: ALUMINUM SHEET 7075-T0 0.045? PO: 2022 118567; CHANNEL AND ANGLES (2E/A) SHEET 7075-T0-0.050 PO: 2022 136558(CONVERTER TO 7075 T6) SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR STRINGER 26R LOCATED BTW BS500D TO BS540 IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. MATERIAL USED: ALUMINUM SHEET 7075-T0 0.045? PO: 2022 118567; CHANNEL AND ANGLES (2E/A) SHEET 7075-T0-0.050 PO: 2022 136558(CONVERTER TO 7075 T6) SEE INDIVIDUAL SIGN OFF BELOW.ITEM RII

Part: STRINGER — CRACKED (FWD CARGO) · airframe 52,033 hrs · 28,008 cycles

CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2022-384003 / [01] TOOL USED P/N 45 MG S/N 130060401 DUE DATE 23/JAN/23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[03] PERFORMED PERMANENT REPAIR STRINGER 26L LOCATED BTW BS500D TO BS540 IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. MATERIAL USED: ALUMINUM SHEET 7075-T0 0.045? PO: 2022 118567; CHANNEL AND ANGLES (2E/A) SHEET 7075-T0-0.050 PO: 2022 136558(CONVERTER TO 7075 T6) SEE INDIVIDUAL SIGN OFF BELOW.;[04] CORRECTED STEP 3: PERFORMED PERMANENT REPAIR STRINGER 26L LOCATED BTW BS500D TO BS540 IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. MATERIAL USED: ALUMINUM SHEET 7075-T0 0.045? PO: 2022 118567; CHANNEL AND ANGLES (2E/A) SHEET 7075-T0-0.050? PO: 2022 136558(CONVERTER TO 7075 T6) SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED PERMANENT REPAIR STRINGER 26L LOCATED BTW BS500D TO BS540 IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. MATERIAL USED: ALUMINUM SHEET 7075-T0 0.045? PO: 2022 118567; CHANNEL AND ANGLES (2E/A) SHEET 7075-T0-0.050? PO: 2022 136558(CONVERTER TO 7075 T6) SEE INDIVIDUAL SIGN OFF BELOW. ITEM RII

Part: STRINGER — CRACKED (FWD CARGO) · airframe 52,033 hrs · 28,008 cycles

CRACK STRINGER 23L LOCATED BS540 AT FWD CARGO COMPARTMENT 2022-384002 / [01] UT EQUIPMENT P/N: 35DL; S/N: 091419910; DUE DATE: 26-JAN-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[03] PERFORMED PERMANENT REPAIR BTW BS500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 MATERIAL USED: ALUMINUM SHEET P/N 7075-T0-0.036 PO: 2021 245499; EXTRUSION P/N BAC1493-659 PO: 2021 149606 AND EXTRUSION P/N BAC1493-249 PO: 2021 147833 SEE INDIVIDUAL SIGN OFF BELOW;[04] PERFORMED PERMANENT REPAIR BTW BS500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 MATERIAL USED: ALUMINUM SHEET P/N 7075-T0-0.036 PO: 2021 245499; EXTRUSION P/N BAC1493-659 PO: 2021 149606 AND EXTRUSION P/N BAC1493-249 PO: 2021 147833 SEE INDIVIDUAL SIGN OFF BELOW.RII

Part: STRAP — ELONGATED (AFT CARGO) · airframe 52,033 hrs · 28,008 cycles

ELONGATED HOLE STRAP LOCATED BETWEEN BS727D TO BS727E AND BETWEEN STR25L TO STR 25R AT AFT CARGO COMPARTMENT 2022-384001 / [01] REPLACED STRAP LOCATED BETWEEN BS727D TO BS727E STR25L TO STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG 146A7500 SHEET 85 REV A;[02] REPLACED STRAP LOCATED BETWEEN BS727D TO BS727E STR25L TO STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG 146A7500 SHEET 85 REV A . STRAP GOING TO INSTALLED WITH TTG8Q004DL04;[03] STEP 2 VERIFIED AND CORRECTIVE ACTION COMPLETED: REPLACED STRAP LOCATED BETWEEN BS727D TO BS727E STR25L TO STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG 146A7500 SHEET 85 REV A . STRAP GOING TO INSTALLED WITH TTG8Q004DL04

Part: RIB — CRACKED (LH HOR STAB) · airframe 52,033 hrs · 28,008 cycles

CRACK INSPAR RIB STAB STA 129.50 LOCATED AT FWD UPPER FLANGE AT LT HORIZONTAL STABILIZER 2022-384005 / [01] PERFORMED REPAIR ON LT HORIZONTAL STABILIZER INSPAR RIB STAB STA 129.50 IAW EA 22-155-02128 FAULT TTG8Q00DV37W; EA 22-155-02128-WIP1 FAULT TTG8Q00DN0MV AND EA 22-155-02128-WIP2 FAULT TTG8Q00DSJ3Z;[02] CORRECTED STEP 1<BR>PERFORMED REPAIR ON LT HORIZONTAL STABILIZER INSPAR RIB STAB STA 129.50 IAW EA 22-155-02128 FAULT TTG8Q00DV37W; EA 22-155-02128-WIP1 FAULT TTG8Q00DN0MV AND EA 22-155-02128-WIP2 FAULT TTG8Q00DSJ3Z<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[03] PERFORMED REPAIR ON LT HORIZONTAL STABILIZER INSPAR RIB STAB STA 129.50 IAW EA 22-155-02128 FAULT TTG8Q00DV37W; EA 22-155-02128-WIP1 FAULT TTG8Q00DN0MV AND EA 22-155-02128-WIP2 FAULT TTG8Q00DSJ3Z <BR>SEE INDIVIDUAL SIGNOFFS BELOW. COMPLETED

Part: SUPPORT ANGLE — CORRODED (AFT CARGO) · airframe 52,033 hrs · 28,008 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN 727 TO BS767 RBL 21.0 WL 156 AFT CARGO COMPARTMENT 2022-383979 / [01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45 MG; S/N: 130061901; DUE DATE: 08-APR-23.;[02] REPLACED SUPPORT ZEE LOCATED BETWEEN 727 TO BS767 RBL 21.0 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGNOFF BELOW;[03] REPLACED SUPPORT ZEE LOCATED BETWEEN 727 TO BS767 RBL 21.0 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9. RII VERIFIED

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 52,033 hrs · 28,008 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 794.3 WL 156 AFT CARGO COMPARTMENT 2022-383978 / [01] REPLACED WEB INTERCOSTAL LOC. BETWEEN BS 767 TO BS 794.3 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 DWG 146A0081 REV: A;[02] CORRECTED STEP 1<BR>REPLACED WEB INTERCOSTAL LOC. BETWEEN BS 767 TO BS 794.3 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 DWG 146A0081 REV: A<BR>SEE INDIVIDUAL SIGNOFFS BELLOW;[03] REPLACED WEB INTERCOSTAL LOC. BETWEEN BS 767 TO BS 794.3 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 DWG 146A0081 REV: A <BR>SEE INDIVIDUAL SIGNOFFS BELLOW. COMPLETED RII

Part: SUPPORT ANGLE — CORRODED (AFT CARGO) · airframe 52,033 hrs · 28,008 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 LBL 21 WL 156 AT AFT CARGO COMPARTMENT 2022-383977 / [01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45 MG; S/N: 130061901; DUE DATE: 08-APR-23.;[02] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BS 727 TO BS 847 LBL 21 WL 156 AT AFT CARGO COMPARTMENT IAW B73-700 SRM 51-10-02 ITEM 9 AND SRM 53-00-53-2R-5 REPAIR 5 FIGURE 202 ; SHEET 1 AND DWG 146A7500 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BS 727 TO BS 847 LBL 21 WL 156 AT AFT CARGO COMPARTMENT IAW B73-700 SRM 51-10-02 ITEM 9 AND SRM 53-00-53-2R-5 REPAIR 5 FIGURE 202 ; SHEET 1 AND DWG 146A7500 REV A. RII VERIFIED

Part: ANGLE — CRACKED (FUSELAGE) · airframe 52,033 hrs · 28,008 cycles

CRACK SUPPORT ANGLE ON BS 540 RBL 1 TO RBL 24 FLOOR STRUCTURE AT PASSENGER CABIN 2022-383942 / [01] REPLACED SUPPORT ANGLE LOC. BS 540 RBL 1 TO RBL 24 FLOOR STRUCTURE AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; DWG 143A0060 REV ?<BR>SEE INDIVIDUAL SIGNOFFS BELLOW.;[02] REPLACED SUPPORT ANGLE LOC. BS 540 RBL 1 TO RBL 24 FLOOR STRUCTURE AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; DWG 143A0060 REV ? <BR>SEE INDIVIDUAL SIGNOFFS BELLOW. COMPLETED

Part: BULKHEAD — DELAMINATED (AFT CARGO BAY) · airframe 52,033 hrs · 28,008 cycles

DELAMINATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2022-383933 / [01] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801; STEP 1(F) DWG: 453A2510 REV: E MATERIAL USED: CONOLITE P/N: BMS8-2TY45CL3GRA PO: 2022 110575;[02] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801; STEP 1(F) DWG: 453A2510 REV: E MATERIAL USED: CONOLITE P/N: BMS8-2TY45CL3GRA PO: 2022 110575

Part: LIGHT — BROKEN (FWD GALLEY) · airframe 52,033 hrs · 28,008 cycles

BROKEN LAVATORY A EMERGENCY LIGHT ASSY AT FWD GALLEY AREA 2022-383919 / [01] REPLACED LAVATORY A EMERGENCY LIGHT ASSY AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802;[02] REPLACED LAVATORY A EMERGENCY LIGHT ASSY AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 52,033 hrs · 28,008 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2022-383900 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A18229508; DUE DATE 29-SEP-22;[02] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS STEP BELOW.;[03] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] JOB COMPLETED

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 52,033 hrs · 28,008 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2022-383901 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A18229508; DUE DATE 29-SEP-22;[02] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] JOB COMPLETED

Part: POWER SUPPLY — INOPERATIVE · airframe 52,033 hrs · 28,008 cycles

INOP LOWERED CEILING PANEL EMERGENCY POWER SUPPLY LT SIDE AT AFT GALLEY AREA 2022-383860 / [01] REPLACED LOWERED CEILING PANEL EMERGENCY POWER SUPPLY LT SIDE AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06-960-806 AND PERFORMED OPERATIONAL TEST IS OK;[02] REPLACED LOWERED CEILING PANEL EMERGENCY POWER SUPPLY LT SIDE AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06-960-806 AND PERFORMED OPERATIONAL TEST IS OK. COMPLETED

Part: PLATE — CORRODED (AFT CARGO) · airframe 52,033 hrs · 28,008 cycles

CORROSION ON FLOOR PLATE LOCATED AT AFT CARGO COMPARTMENT BSTA 787 2022-383902 / [01] REPLACED FLOOR PLATE LOC. AT AFT CARGO COMPARTMENT BS787 IAW B737-700 SRM 51-40-02;[02] CORRECTED STEP 1<BR>REPLACED FLOOR PLATE LOC. AT AFT CARGO COMPARTMENT BS787 IAW B737-700 SRM 51-40-02<BR>SEE INDIVIDUAL SIGNOFFS BELLOW;[03] REPLACED FLOOR PLATE LOC. AT AFT CARGO COMPARTMENT BS787 IAW B737-700 SRM 51-40-02 <BR>SEE INDIVIDUAL SIGNOFFS BELLOW

Part: RIB — CRACKED (LH HOR STAB) · airframe 52,033 hrs · 28,008 cycles

CRACK INSPAR RIB 5 STAB STA 129.50 AT 27INCH OF FRONT SPART AT LT HORIZONTAL STABILIZER 2022-383840 / [01] ET TOOL USED: PN: NORTEC 600D; SN: 210138203; DUE DATE: 11-APR-23;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030456 DUE DATE: 26 JAN 23;[03] REPAIRED INSPAR RIB 5 LOCATED STAB STA 129.30 AND 27 INCHES FROM FRONT SPAR LT HORIZONTAL STA IAW SRM B737-700 55-10-09-2R-5 REPAIR 5 FIGURE 204;[04] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 52,033 hrs · 28,008 cycles

CRACK ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR 2022-383815 / [01] TOOL USED CALIPER PN: 500-193-30; SN: 0000285; D/D: 10/DEC/22.;[02] TOOL USED HOT BONDER PN: HCS9200B; SN: 18175478; D/D: 05/AUG/22.;[03] TOOL USED SCALE PN: 91847; SN: AE-409314; D/D: 06/JUN/23.;[04] REPAIRED ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] JOB TASK COMPLETED.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 52,033 hrs · 28,008 cycles

CRACK FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2022-383747 / [01] REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-1A-1 PARAGRAPH 5.A.(1)(A) 2) DUE TO CRACK IS COMMON TO HOLE. MEASURE OF CRACK IS: 0.730? TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A21029157 DUE DATE: 02/FEB/23<BR>MATERIAL USED P/N: 2024T3-071 P/O: 2022 139869<BR><BR>INSTALLED THIS PANEL IS DOCUMENTED ON: TTG8Q00CQ69E;[02] REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-1A-1 PARAGRAPH 5.A.(1)(A) 2) DUE TO CRACK IS COMMON TO HOLE. MEASURE OF CRACK IS: 0.730? TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A21029157 DUE DATE: 02/FEB/23 <BR>MATERIAL USED P/N: 2024T3-071 P/O: 2022 139869 <BR><BR>INSTALLED THIS PANEL IS DOCUMENTED ON: TTG8Q00CQ69E

Part: MEGAPHONE — INOPERATIVE (FED MEGAPHONE) · airframe 51,880 hrs · 27,909 cycles

FWD MEGAPHONE INOP / [01] REMOVED AND REPLACED FWD MEGAPHONE BATTERIES; OPS CHECK GOOD. REFERENCE AMM 25-64-00.

Part: HOLDER — LOOSE (R1 DOOR) · airframe 50,884 hrs · 27,284 cycles

R1 DOOR LEFT GIRT BAR HOLDER LOOSE / [01] SECURED R1 LEFT GIRT BAR HOLDER PER SIP

Part: LIGHT — LOOSE · airframe 50,740 hrs · 27,195 cycles

SMALL PLASTIC EXIT SIGN/ PLACARD NEXT TO AFT SERVICE DOOR IS LOOSE / [01] R&R AFT SERVICE DOOR EXIT SIGN COVER PER AMM 33-51-01

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 50,197 hrs · 26,861 cycles

R1 DOOR EMERGENCY SLIDE PACK DROPPED ONTO PROVO TRUCK WALKWAY. R1 DOOR WAS CRACKED OPEN. DOOR WAS ARMED WITHOUT RED SAFETY STRAP OVER WINDOW. SLIDE PACK DROPPED WHEN PROVO BEGAN TO OPEN DOOR. ; R1 DOOR EMERGENCY SLIDE PACK DROPPED ONTO PROVO TRCK WALKWAY.R1 DOOR WAS CRACKED OPEN. DOOR WAS ARMED WITHOT RED SAFETY STRAP OVER WINDOW. SLIDE PACK DROPPED WHEN PROVO EGAN TO OPEN DOOR. SLIDE DID NOT DEPLOY. / [01] REMOVED AND REINSTALLED SLIDE ASSY PER MT 725-61-00 AND M/M 25-66-00

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 49,217 hrs · 26,267 cycles

FOUND WEB CRACKED AT FLANGE ; / [01] DAMAGE LOCATED ON R/H HORIZONTAL FRONT SPAR REMOVABLE WEB STA 143.7; [02] STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLER PER SRM 55-10-10-2R-1. OK TO INSTALL DOUBLER.; [03] CORRECTIVE ACTION #2 COMPLIED WITH.; [04] C/W SRM 55-10-10-2R-1; [05] CORRECTIVE ACTION #4 C/W; [06] REMOVED RII REQUIREMENT; [07] REPAIRED PER SRM 55-10-10-2R-1; [08] CORRECTIVE ACTION #7 C/W

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 49,217 hrs · 26,267 cycles

RUDDER BEAM ARM WEIGHT SEVERLY CORRODED AND GAPPED/SEPERATED FROM THE BEAM ARM SURFACE IN SEVERAL AREAS.( SEE MULTIPLE PICS IN ATTACHMENT SECTION OF THIS FOUND FAULT) ; / [01] REMOVED AND REPLACED DAMAGED RUDDER WEIGHT PER CMM 55-40-09.; [02] C/W; [03] CW

Part: RIB — ELONGATED (HORIZONTAL STAB) · airframe 49,217 hrs · 26,267 cycles

NUMEROUS FASTENER HOLES ELONGATED ON LOWER FLANGE OF RIB ; / [01] SEE JIC TTG8Q0061W1T FOR REPLACEMENT OF STAB RIB @ STAB STA 120.30

Part: RIB — BENT (HORIZONTAL STAB) · airframe 49,217 hrs · 26,267 cycles

HORIZONTAL STAB RIB AT STAB STATION 120.30 WAS FOUND TO BE BENT AFTER REMOVAL ; / [01] SEE JIC TTG8Q0061W1T FOR REPLACEMENT OF STAB RIB @ STAB STA 120.30

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 49,217 hrs · 26,267 cycles

#4 VERTICAL STIFFENER AT R/H HORIZONTAL STAB STATION 120.30 IS CRACKED ; / [01] SEE JIC TTG8Q0061W1T FOR REPLACEMENT OF STAB RIB @ STAB STA 120.30

Part: RIB — DAMAGED (HORIZOTNAL STAB) · airframe 49,217 hrs · 26,267 cycles

R/H STAB. REMOVABLE LEADING EDGE HAS A DAMAGED RIB AT L/E STAB STA.161.04.(MARKED) ; / [01] REMOVED DAMAGED RIB PER SRM 51-40-02; [02] REMOVED AND REPLACED RIB PER SRM 51-40-02.; [03] ABOVE STEPS COMPLIED WITH.; [04] ABOVE STEPS COMPLETE; [05] CONFIRMED ALL STEPS FILLED OUT. AND PART REQUIREMENT BOX CHECKED.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 46,716 hrs · 24,810 cycles

FWD CARGO DOOR AFT SCUFF PLATE CORNER IS CRACKED.DOT 82-004. / ACCOMPLISHED WELDING REPAIR OF DAMAGE SCUFF PLATE AT FWD CARGO AFT CORNER PER REF B737 SRM 53-30-15-2R-1. INSTALLATION WILL BE ACCOMPLISHED ON CUSTOMER CARD J753-646-62-01

Part: STRAKE — DAMAGED (RT WINGLET) · airframe 46,716 hrs · 24,810 cycles

RT WINGLET VERTICAL STRAKE MISSING 3 EA NUTPLATES AND HOLES ELONGATED / REMOVED STRAP AT RT WINGLET VERTICAL STRAKE REF B737-700 SRM 51-40-02-0G-0. FABRICATED NEW REPAIR STRAP MATERIAL USED 2024-0 .063' HEAT TREAT TO T4 OR T42 AFTER FORMING. P.O#1687098 REF REG# 2016160-2 REV P1 AND INSTALLED NEW REPAIR STRAP AT RT WINGLET VERTICAL STRAKE REF REG #2016160-2 REV IR AND EA# 20-157-01498 REV IR. LATE ENTRY : INSTALLED NUT PLATE ON NEW STRAP REF B737-700 SRM 51-40-02-0G-0

Part: FLOOR SKIN — DAMAGED (COCKPIT) · airframe 46,716 hrs · 24,810 cycles

FLIGHT DECK FLOOR DAMAGE AT STA 260; REPAIR PER EA. / REMOVED FASTENERS ON REPAIR AREA PER REF. B737-700 SRM 51-40-02-0G-0 AND EA NO: 1-A53-53179 REV 1. TRIM OUT DAMAGED SECTION AT FLIGHT DECK FLOOR BS 260 PER REF. EA NO: 1-A53-33179 REV. 1. PERFORMED HFEC AT ALL EXISTINNG FASTENERS HOLES AND TRIM OUT SECTION PER REF B737 NDT PART 6 51-00-00. PROCEDURE 23 NO CRACKS NOTED. FABRICATED REPAIR PARTS 3EA MAT USED 2024T3 CLAD 0.040 AND 2024 T3 CLAD 0.050 PER REF. EA NO : 1-A53-33179 REV. 1. INSTALLED REPAIR PARTS 3EA PER REF. EA NO: 1-A53-33179 REV 1. INSTALLED NOSE LANDING GEAR WHEEL WELL UPPER SECTION PRESSURE PANEL # 114A AND 113AC PER. REF. B737-700 AMM 53-14-01-420-801; LEAK CHECK WILL BE ACCOMPLISH ON CARD # J721-00-20-01.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 46,661 hrs · 24,776 cycles

L1 DOOR SLIDE OUT OF SLIDE BRACKET / REINSTALLED L1 SLIDE PER MT 725-61-06

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 45,728 hrs · 24,211 cycles

AFT LEFT FLASHLIGHT SECURE BREAKAWAY STRAP/PLACARD BROKEN. R&R'D AFT LEFT FLASHLIGHT SECURE/BREAKAWAY STRAP/ PLACARD PER AMM 25-64-00.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 45,253 hrs · 23,915 cycles

EMERGENCY BATTERY PACK M1675 WOULD NOT CHARGE. R&R LIGHT BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,253 hrs · 23,915 cycles

EMERGENCY BATTERY PACK M1674 WOULD NOT CHARGE. R&R LIGHT BATTERY PACK IAW AMM.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 45,253 hrs · 23,915 cycles

EMERGENCY BATTERY PACK M1672 WOULD NOT CHARGE. R&R LIGHT BATTERY PACK IAW AMM.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 45,253 hrs · 23,915 cycles

EMERGENCY BATTERY PACK M1670 WOULD NOT CHARGE. R&R LIGHT BATTERY PACK IAW AMM.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 45,253 hrs · 23,915 cycles

EMERGENCY BATTERY PACK M1673 WOULD NOT CHARGE. R&R LIGHT BATTERY PACK IAW AMM.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 45,253 hrs · 23,915 cycles

EMERGENCY BATTERY PACK M2335 WOULD NOT CHARGE. R&R LIGHT BATTERY PACK IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 44,436 hrs · 23,412 cycles

ONE FORWARD FLASH LIGHT INOP. / R&R BATTERY PER AMM.

Part: LENS — MISSING (CABIN) · airframe 44,436 hrs · 23,412 cycles

FORWARD ENTRY LOWER EMERGENCY LIGHT LENS COVER MISSING DIRECTIONAL ARROW. / R&R COVER PER AMM.

Part: SENSOR — FAULTY (LE SLAT) · airframe 42,481 hrs · 22,162 cycles

DECLARED EMERGENCY, LEADING EDGE FLAPS TRANSIT INDICATION ON APPROACH. R&R S172 LEADING EDGE FLAP 3 RETRACT SENSOR PER AMM.

Part: FASTENER — MISSING (EMERGENCY EXIT) · airframe 42,474 hrs · 22,158 cycles

LT OVERWING EXIT LOWER HANDLE LOOSE. INSTALLED MISSING FASTENERS PER SIP.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 41,003 hrs · 21,243 cycles

COCKPIT EMERGENCY LIGHT INOP AT LOCATION M1675. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,003 hrs · 21,243 cycles

R1 DOOR EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,003 hrs · 21,243 cycles

LT OVERWING EXIT LIGHT INOP AT LOCATION M1668. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,003 hrs · 21,243 cycles

LAV A EXIT LIGHT INOP AT M1675. R&R BATTERY PACK PER AMM.

Part: HOUSING — CRACKED (CABIN) · airframe 41,003 hrs · 21,243 cycles

AFT ENTRY CENTER CEILING PANEL EMERGENCY EXIT LIGHT HOUSING CRACKED. R&R LIGHT HOUSING PER AMM.

Part: THRESHOLD WEB — CORRODED (FWD SERVICE DOOR) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** ON FSD THRESHOLD SUPPORT THAT ATTACHES TO THE FSD MOPSILL. / REMOVED CORROSION; FSD THRESHOLD SUPPORT ATTACHING TO THE MOPSILL WITH A REMAINING THICKNESS OF .079' FROM ORIGINAL .090'; FOUND TO BE OUT OF LIMITS; REMOVED FSD THRESHOLD SUPPORT ATTACHED TO THE MOPSILL AND REPLACED WITH NEW PER SRM 53-10-15-1A-2; SRM 51-40-05; BOEING DWG. 141A8310

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

AFT CARGO DOOR SUB THRESHOLD WEB CORRODED AT BS 827, RBL 26. R&R WEB IAW DWG AND SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

FORWARD CARGO BAY SUB WEB CORRODED AT THRESHOLD UPPER SURFACE. R&R WEB PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 24. R&R SUPPORT IAW DWG & SRM.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** UNDER ACB FLOOR STRAP COMMON TO SCUFF PLATE AT STA 787+12 RBL 20 AROUND FASTENER HOL E / REMOVED STRAP IAW SRM 51-40-02 92627C 30AUG18 INSTALLED REPLACEMENT NUT PLATE STRAP BS787-794+25 RBL 18.5 PER SRM 51-40-02-0G-0 AND DWG# 146A0081 SHEET 31.

Part: SUPPORT — CORRODED (FWD CARGO COMPT) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** ON FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT UPPER SURFACE. / REMOVED AND REPLACED FORWARD CARGO BAY AFT BULKHEAD CENTER PNL LWR SUPPORT ANGLE (RAIL ASSY) PER DWG# 143A9481 REV: B; 143A7902 REV: - AND SRM 51-40-02.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

AFT CARGO BAY AFT SHIELD CORRODED BETWEEN BS 849 TO BS 867, RBL 21. R&R SHIELD ASSEMBLY IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 496, RBL 24. R&R SUPPORT IAW SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** IN ACB UNDER STRAP INBOARD OF AFT SHIELD DOOR AT STATION 847 / REMOVED AND REPLACED NUT PLATE STRAP BS847-855.95 RBL 19.5 PER SRM 51-40-02-0G-0 AND DWG # 146A0081 SHEET 31

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

AFT CARGO DOOR RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO BS 947, RBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: TRACK — CORRODED (AFT CARGO COMPT) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** IN FWD ANCHOR HOLE ON ACB FLOOR SUPPORT INBOARD OF SHIELD STA 847+2 IN RBL 14 / REMOVED CORROSION ON CARGO TIE DOWN TRACK AT BS 847+2 RBL 14 PER SRM 51-10-02-0G-0. DAMAGE MEASURES 1.0' X 1.0' WITH 100% MATERIAL LOSS. DAMAGE IS OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED CARGO TRACK FROM BS 727+4-887 PER SRM 51-40-02-0G-0. FABRICATED TRACK SPLICE AT BS 747-10 FROM BAC1509-100688 7050-T6511 LOT# 1297327 PER SRM 53-00-53-2R-3 INSTALLED REPLACEMENT TRACK AT RBL 14 FROM BS 727+4 - BS 887 PER SRM 51-40-02-0G-0 AND DWG # 146A7500 SHEET 42

Part: BRACKET — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

AFT CARGO BAY ALONG R/H FLOOR TO SIDEWALL SUPPORT FORWARD SHIELD TO WEB BRACKET CORRODED BETWEEN BS 767 TO BS 787, RBL 21. R&R BRACKET IAW SRM IAW DWG.

Part: FRAME — CRACKED (LH NACELLE) · airframe 41,003 hrs · 21,243 cycles

#1 ENGINE I/B COWL STIFFENER FRAME FOR OIL ACCESS DO OR 3RD RIB FROM AFT END IS CRACKED. / REMOVED #1 ENGINE I/B COWL STIFFENER FRAME 'SHIELD' FOR OIL ACCESS DOOR 3RD RIB FROM AFT END. POSITIONED; - DRILLED UP; AND INSTALLED NEW STIFFENER FRAME 'SHIELD' IAW CMM 71-13-30; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. 4583C 13SEP18

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

FRAME CRACKED IN RADIUS JUST ABOVE ENTRY DOOR SURROUND AT BS 310. REPAIRED FRAME PER ER AND EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

FLOOR SUPPORT BETWEEN CRACKED BETWEEN BS 380 TO BS 400, RBL 10. REPAIRED SUPPORT PER SRM AND DWG.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 41,003 hrs · 21,243 cycles

FWD CABIN FLOOR PANEL 221BF AFT O/B CORNER IS BROKEN / DUE TO EXTENT OF DAMAGE TO BROKEN AFT O/B CORNER ON FWD CABIN FLOOR PANEL 221BF; REPLACED PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-76 ITEM 25. 57066U 8/29/18

Part: STRAP — CORRODED (CABIN) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** ON TENSION STRAP AT B.S. 1016-1030; L.B.L. 3; W.L. 208.1. / REMOVED CORROSION ON TENSION STRAP AT B.S 1016-1030 LBL 3 WL 208.1; THERE IS NO ALLOWABLE DAMAGE FOR TENSION STRAP IN THE SRM. REMOVED AND REPLACED TENSION STRAP PER SRM 51-40-02-0G-0; DWG 147A5600

Part: FRAME — CHAFED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

FAIRING ATTACH FRAME CHAFED BETWEEN BS 663 TO BS 674, LBL 27. R&R FRAME PER DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

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

Part: BEAM — CRACKED (FSD) · airframe 41,003 hrs · 21,243 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 BEAM TO BE CRACKED COMMON TO FORWARD MOST HANDLE BOX ASSEMBLY ATTACH POINT AT THE INBOARD SIDE; COMMON TO THE RADIUS. / REMOVED AND REPLACED FWD SERVICE DOOR #4 BEAM ALL WORK ACCOMPLISHED PER CUSTOMER RO# 0520055-CAR JOB #509351 (POS:#R1;TAG NO.:459596;P/N ON/OFF:141A6516-18M; S/N OFF:002152;S/N ON:002152)

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 41,003 hrs · 21,243 cycles

FWD CABIN FLOOR PANEL 221GF FWD O/B CORNER IS BROKEN / DUE TO EXTENT OF DAMAGE TO FWD O/B CORNER ON FWD CABIN FLOOR PANEL 221GF; REPLACED PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-76 ITEM 205. 57066U 8/29/18

Part: RETAINER — CRACKED (RIGHT WING) · airframe 41,003 hrs · 21,243 cycles

RIGHT WING T/E VERTICAL BULB SEAL RETAINER CRACKED ABOVE AFT PYLON TIP / REMOVED AND REPLACED R/W T/E VERTICAL BULB SEAL RETAINER ABOVE AFT PYLON TIP IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-25. 56839U 29AUG18

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** ACB; FWD SHIELD HAS AREAS OF CORROS ION; BS767 TO BS794; RBL21 / EVALUATED ABC FWD SHIELD AT BS767 TO BS794. SHIELD FOUND TO BE OUT OF LIMITS; REPAIRED BY REPLACEMENT; IAW SRM 51-40-02 SRM 51-10-02 SRM 51-40-05 DWG 146A0081

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

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

Part: STRINGER — CORRODED (AFT FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** CORROSION ON S-24R BETWEEN BS1064 AND BS1088 / REMOVED CORROSION ON STR 24R BETWEEN BS 1064 AND BS 1088 L=6'X W=2' X D=.007. REPAIRED PER ATS ER 18-04067 REV IR AND SWA EA 1-753-33282 REV IR.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727+4 TO BS 847, LBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: NONE — CRACKED (FWD CARGO LH) · airframe 41,003 hrs · 21,243 cycles

(FCB) INTERCOSTAL CLIP IS CRACKED AT B.S.400; LBL24; WL153. / REMOVED AND REPLACED INTERCOSTAL CLIP AT BS 400 LBL 24 WL 153 IAW SRM 51-40-02-0G-0 88001U 11SEP18 AND BOEING DWG 143A7505

Part: NONE — CORRODED (AFT CARGO COMPT) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** ACB; CLIP COMMON TO BS767 FRAME UPP ER CHORD AND FWD SHIELD HAS CORROSION; BS767 TO BS769.5; RBL23 / REMOVED AND INSTALLED NEW ACB CLIP. AT BS 767-769.5; RBL 23 I.A.W. SRM 51-40-02-0G-0 AND DWG. # 146A0081; SH.31 88919U 06SEP.18

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

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

Part: TRACK — CORRODED (FLIGHT DECK FLOO) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** FIRST OFFICERS 4 SEAT TRACKS HAVE CORROSION. / F/O'S 4EA SEAT TRACKS IAW AMM 25-11-11-400-801 PARA.3.D (1)-(8) 7343U 31AUG18

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

AFT CARGO BAY FLOOR SUPPORT STRAP CORRODED AT BS 727D+4, BETWEEN LBL 21 TO RBL 21. R&R STRAP IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

FORWARD CARGO BAY AFT LT LOWER BULKHEAD SUPPORT CORRODED AT BS 500D, BETWEEN STR 18L TO STR 26L. R&R SUPPORT IAW SRM AND DWG.

Part: TRACK — CORRODED (FLIGHT DECK FLOO) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** CAPTAIN'S 4 SEAT TRACKS ARE CORRODED. / R AND R CAPT'S 4EA SEAT TRACKS IAW AMM 25-11-11-400-801 PARA. 3.D.(1)-(8) 7343U 31AUG18

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,003 hrs · 21,243 cycles

AFT CARGO BAY FLOOR SUPPORT STRAP CORRODED AT BS 767+4, BETWEEN LBL 21 TO RBL 21. R&R STRAP IAW SRM AND DWG.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** ALL AROUND ON ACB FLOOR PANEL#140DF . / FABRICATED NEW ACB FLOOR PANEL 140DF FROM .071 2024T3; LOT # 1357514-1 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** ALL AROUND ON ACB FLOOR PANEL#140CF . / FABRICATED NEW ACB FLOOR PANEL 140CF FROM .071 2024T3; LOT # 1357514-1 PER DWG 453A2610 AND AMM 25-52-01-201-801

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,003 hrs · 21,243 cycles

RT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT STAB STA 129.50, 3RD VERTICAL STIFFENER FROM FORWARD EDGE. REPAIRED RIB IAW SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** ALL AROUND ON ACB FLOOR PANEL#140AF . / FABRICATED NEW ACB FLOOR PANEL 140AF FROM .071 2024T3; LOT # 1357514-1 PER DWG 453A2610 AND AMM 25-52-01-201-801

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,003 hrs · 21,243 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT SECOND FROM THE FRONT STIFFENER STAB STA 120.30. REPAIRED RIB IAW SRM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 41,003 hrs · 21,243 cycles

(L/H HOZ STAB) FWD HOZ STAB UPPER SLIDE SEAL IS CRACKED. / REMOVED & REPLACED (L/H HOZ STAB) FWD HOZ STAB UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 & 53-31-31-400-802 STEP 2D & E 5679U 29AUG18

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 41,003 hrs · 21,243 cycles

***CORROSION***ALL AROUND ON FCB FLOOR PANEL# 120CF. / FABRICATED NEW FCB FLOOR PANEL 120CF FROM .071 2024T3; LOT # 1347987-1 PER DWG 453A1610 AND AMM 25-52-01-201-801

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 41,003 hrs · 21,243 cycles

***CORROSION*** ALL AROUND ON ACB FLOOR PANEL#140BF . / FABRICATED NEW ACB FLOOR PANEL 140BF FROM .071 2024T3; LOT # 1347987-1 PER DWG 453A2610 AND AMM 25-52-01-201-801

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,003 hrs · 21,243 cycles

RT HORIZONTAL STABILIZER IN SPAR RIB AT STAB STA 120.3, 3RD VERTICAL STIFFENER FROM FORWARD EDGE CRACKED. REPAIRED RIB IAW SRM.

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 41,003 hrs · 21,243 cycles

RIGHT WING L/E PANEL 621JB DELAMINATED AT CUTOUT ON FWD EDGE / DELAMINATE CUTOUT ON FED EDGE ON 621JB PANEL HAS BEEN REPAIRED PER SRM 57-41-01-2R-1 AND SRM 51-70-05-2R-6 57543U 13SEP18.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 41,003 hrs · 21,243 cycles

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

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 41,003 hrs · 21,243 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 39,681 hrs · 20,430 cycles

LEFT OVERWING EXIT DOOR EMERGENCY LIGHT LENS FOUND LOOSE. R & R THE LENS IAW MM.

Part: COVER — BROKEN (LIGHT SWITCH) · airframe 39,352 hrs · 20,219 cycles

EMERGENCY LIGHT SWITCH COVER BROKEN. R & R THE SWITCH COVER IAW SIP.

Part: BRACKET — CRACKED (LEFT WING) · airframe 39,234 hrs · 20,137 cycles

LEFT WING FIXED TRAILING EDGE FIXED PANEL CENTER AFT BRACKET CRACKED NEXT TO DEFLECTION RIB / REMOVED AND REPLACED BRACKET PER SRM 51-40-02

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 37,366 hrs · 18,960 cycles

EMERGENCY FLASHLIGHT STRAP BROKEN. R&R STRAP PER SIP.

Part: BONDING WIRE — LOOSE (L2 DOOR) · airframe 37,181 hrs · 18,843 cycles

L2 DOOR EMERGENCY EVAC SLIDE BONDING WIRE LOOSE. SECURED WIRE PER MT.

Part: BEAM — CRACKED (FUSELAGE) · airframe 34,756 hrs · 17,376 cycles

SPAN WISE BEAM CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.75. R&R BEAM IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 34,756 hrs · 17,376 cycles

RT MAIN LANDING GEAR WELL SHELF ATTACH ANGLE INBOARD AND ABOVE NR 2 TANK AFT BOOST PUMP CRACKED. R&R ATTACH ANGLE IAW SRM.

Part: VAPOR BARRIER — LOOSE (RT MLG WW) · airframe 34,756 hrs · 17,376 cycles

RIGHT WHEEL WELL VAPOR BARRIER LOOSE AT BS 663, RBL 40. REPAIRED THE BARRIER IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 34,756 hrs · 17,376 cycles

SPAN WISE BEAM CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.75. R&R BEAM IAW SRM.

Part: VAPOR BARRIER — LOOSE (LT MLG WW) · airframe 34,756 hrs · 17,376 cycles

L/H WHEEL WELL VAPOR BARRIER LOOSE AT BS. 663, LBL 40. REPAIRED BARRIER IAW SRM.

Part: VAPOR BARRIER — LOOSE (RT MLG WW) · airframe 34,756 hrs · 17,376 cycles

LEFT WHEEL WELL VAPOR BARRIER LOOSE AT BS 663, LBL 39, APPROXIMATELY 5" BELOW BEADED WEB. REPAIRED THE VAPOR BARRIER IAW EA.

Part: BARRIER — CRACKED (RT MLG WW) · airframe 34,614 hrs · 17,292 cycles

R/H WHEEL WELL REAR SPAR VAPOR BARRIER FIBERGLASS PANEL CRACKED IN THE WING CENTER SECTION. / REPAIRED BARRIER IAW EA.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 34,219 hrs · 17,059 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. R & R COVER IAW SIP.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 32,282 hrs · 15,918 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 30,576 hrs · 14,947 cycles

FORWARD SERVICE DOOR EMER EXIT LIGHT COVER LOOSE. R & R SIGN IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 30,018 hrs · 14,632 cycles

AFT CABIN AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R EMERGENCY BATTERY PACK IAW MM.

Part: EEC — FAILED (NR 1 ENGINE) · airframe 29,069 hrs · 14,110 cycles

INFLIGHT SHUTDOWN, ERRATIC NR 1 ENG OPERATION CLIMBED AT CRUISE N, DROPPED OFF TO LESS THAN 40% & FAILED. R & R NR 1 ELECTRONIC ENG CONTROL IAW MM.

Part: LENS — UNSECURE (CABIN) · airframe 29,049 hrs · 14,094 cycles

L1 DOOR EMER EXIT LENS FELL OFF. R & R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 27,765 hrs · 13,353 cycles

R1 DOOR EMER SLIDE LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 27,765 hrs · 13,353 cycles

PRESSURE BULKHEAD WEB CRACKED AT BS 663, RBL 34.5. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 27,765 hrs · 13,353 cycles

PRESSURE BULKHEAD WEB CRACKED AT BS 663, RBL 41.0. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 27,765 hrs · 13,353 cycles

PRESSURE BULKHEAD WEB CRACKED AT BS 663, RBL 42.5. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,765 hrs · 13,353 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5, AFT FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,765 hrs · 13,353 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75 AFT TWO FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 27,765 hrs · 13,353 cycles

EMERGENCY EXIT LIGHT ASSEMBLY MOUNTED ON THE G4 GALLEY BROKEN. R & R LIGHT IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,765 hrs · 13,353 cycles

SEAT TRACK AFT TWO FASTENER HOLES CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 27,765 hrs · 13,353 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75, AFT OTBD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,656 hrs · 13,281 cycles

AFT EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: LIGHT — FAULTY (CABIN) · airframe 27,629 hrs · 13,263 cycles

ON DESCENT FLIGHT ATTENDANTS REPORTED SMELLS SIMILAR TO SMOKE & INCENSE FROM OVERHEAD 7E. R & R BULB IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 26,827 hrs · 12,814 cycles

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

Part: BRACKET — LOOSE (GIRT BAR) · airframe 26,690 hrs · 12,739 cycles

R1 DOOR SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,665 hrs · 12,726 cycles

RIGHT SIDEWALL EEPLS INOPERATIVE AT ROW 1. R & R EEPLS IAW MM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 24,361 hrs · 11,403 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW WO.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,711 hrs · 11,001 cycles

FWD CARGO INTERCOSTAL CRACKED AT BS 540 UPPER RT OF CENTER LINE. R & R INTERCOSTAL SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,711 hrs · 11,001 cycles

FWD CARGO INTERCOSTAL CRACKED AT BS 540 UPPER LT OF CENTER LINE. R & R INTERCOSTAL SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,755 hrs · 9,271 cycles

BULKHEAD LOWER WEB CRACKED AT BS 663, RBL 45. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,755 hrs · 9,271 cycles

BULKHEAD LOWER WEB CRACKED AT BS 663, LBL 43. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 20,755 hrs · 9,271 cycles

EXTERNAL POWER SERVICE DOOR CUTOUT CRACKED AT CENTER LATCH. REPAIRED SKIN IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,755 hrs · 9,271 cycles

BULKHEAD LOWER WEB CRACKED AT BS 663, RBL 51. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,755 hrs · 9,271 cycles

BULKHEAD LOWER WEB CRACKED AT BS 663, RBL 33. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 20,755 hrs · 9,271 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 20,755 hrs · 9,271 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 96 TO STA 99. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 20,755 hrs · 9,271 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 96 TO STA 98.5. REPAIRED SKIN IAW SRM.