N8657B

Part: GIRT BAR — LOOSE (ZONE 800) · airframe 36,478 hrs · 17,944 cycles

FWD ENTRY GRIT BAR LOOSE CLIP. REINSTALLED FWD ENTRY GIRT BAR CLIP PER AMM 25-66-00

Part: BLEED AIR SYS — LEAKING (ZONE 600) · airframe 33,663 hrs · 16,345 cycles

RIGHT DUCT PRESSURE OFF THE SCALE HIGH @ 10;000 FEET RIGHT DUCT PRESSURE OFF THE SCALE HIGH @ 10000 FEET<[01] UPON INSPECTION; FOUND PRSOV LEAKING EXCESSIVELY. REMOVED AND REPLACED PRSOV IAW AMM 36-11-04.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 33,347 hrs · 16,219 cycles

SEAT ROW 8ABC EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED AND OPS CHECKED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 8ABC GOOD IAW B737-800 33-51-03-960-805;[02] REMOVED AND REPLACED AND OPS CHECKED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 8ABC GOOD IAW B737-800 33-51-03-960-805. VERIFIED WORK AND WORK ENTRIES.

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 33,347 hrs · 16,219 cycles

R/H ECS BAY AFT AREA; ANGLE ATTACHED TO THE LOWER REAR SPAR CRACKED AT BS 663 APPROX. RBL-40<[01] REMOVED RH VAPOR BARRIER ATTACHMENT ANGLE; VAPOR BARRIER CHANNEL SUPPORT FROM STA RBL45 TO RBL 65; STIFFENER AT STA RBL33 APPOX; AND FITTING AT RBL 70; FORMED RH VAPOR BARRIER ATTACHMENT ANGLE; INSTALLED NEW RH VAPOR BARRIER ATTACHMENT ANGLE; VAPOR BARRIER CHANNEL SUPPORT FROM STA RBL45 TO RBL 65; STIFFENER AT STA RBL33 APPROX; AND FITTING AT RBL 70; REF BAC DWG 111A1000 REV - AND B737-NG SRM 51-40-02;[02] REMOVED RH VAPOR BARRIER ATTACHMENT ANGLE; VAPOR BARRIER CHANNEL SUPPORT FROM STA RBL45 TO RBL 65; STIFFENER AT STA RBL33 APPOX; AND FITTING AT RBL 70; FORMED RH VAPOR BARRIER ATTACHMENT ANGLE; INSTALLED NEW RH VAPOR BARRIER ATTACHMENT ANGLE; VAPOR BARRIER CHANNEL SUPPORT FROM STA RBL45 TO RBL 65; STIFFENER AT STA RBL33 APPROX; AND FITTING AT RBL 70; REF BAC DWG 111A1000 REV - AND B737-NG SRM 51-40-02

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 33,347 hrs · 16,219 cycles

L/H ECS BAY AFT AREA; ANGLE ATTACHED TO THE LOWER REAR SPAR CRACKED AT BS 663 APPROX. LBL-40.<[01] REMOVED LH VAPOR BARRIER ATTACHMENT ANGLE; VAPOR BARRIER CHANNEL SUPPORT FROM STA LBL45 TO LBL 65; STIFFENER AT STA LBL33 APPOX; AND FITTING AT LBL 70; FORMED LH VAPOR BARRIER ATTACHMENT ANGLE; INSTALLED NEW LH VAPOR BARRIER ATTACHMENT ANGLE; VAPOR BARRIER CHANNEL SUPPORT FROM STA LBL45 TO LBL 65; STIFFENER AT STA LBL33 APPROX; AND FITTING AT LBL 70; REF BAC DWG 111A1000 REV - AND B737-NG SRM 51-40-02;[02] REMOVED LH VAPOR BARRIER ATTACHMENT ANGLE; VAPOR BARRIER CHANNEL SUPPORT FROM STA LBL45 TO LBL 65; STIFFENER AT STA LBL33 APPOX; AND FITTING AT LBL 70; FORMED LH VAPOR BARRIER ATTACHMENT ANGLE; INSTALLED NEW LH VAPOR BARRIER ATTACHMENT ANGLE; VAPOR BARRIER CHANNEL SUPPORT FROM STA LBL45 TO LBL 65; STIFFENER AT STA LBL33 APPROX; AND FITTING AT LBL 70; REF BAC DWG 111A1000 REV - AND B737-NG SRM 51-40-02

Part: FLAP — DELAMINATED (ZN 600 RIGHT WIN) · airframe 33,347 hrs · 16,219 cycles

R/H WING O/B AFT FLAP DELAMINATED AT THE I/B AFT CORNER.<[01] REMOVED DELAMINATED R/W I/B AFT FLAP (PN:113A3700-28 SN:005141); RECEIVED NEW R/W I/B AFT FLAP (PN:113A3700-8 SN:000362); FOUND TO BE BAD FROM STOCK. R/W I/B AFT FLAP (PN:113A3700-8 SN:000362) TO BE REMOVED AND REPLACED ON SWA-ID: TTG8Q00X9R8M HAECO OPS: 36233;[02] REMOVED DELAMINATED R/W I/B AFT FLAP (PN:113A3700-28 SN:005141); RECEIVED NEW R/W I/B AFT FLAP (PN:113A3700-8 SN:000362); FOUND TO BE BAD FROM STOCK. R/W I/B AFT FLAP (PN:113A3700-8 SN:000362) TO BE REMOVED AND REPLACED ON SWA-ID: TTG8Q00X9R8M HAECO OPS: 36233

Part: PANEL — CRACKED (ZN 200 FUS TOP) · airframe 33,347 hrs · 16,219 cycles

STA 540 B.LINE 0 PANEL BRAKER LEFT AND RIGHT CORNER HAS CRACK. DOT P833<[01] REMOVED AND REPLACED 2 EACH PANEL BREAKS REF BAC DWG 143A0060 REV - AND B737-NG 51-40-02;[02] REMOVED AND REPLACED 2 EACH PANEL BREAKS REF BAC DWG 143A0060 REV - AND B737-NG 51-40-02

Part: FLOORBOARD — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,347 hrs · 16,219 cycles

C/R (AH) MAIN CABIN FLOORBOARD 242LF HAS DELAMINATION<[01] REMOVED; RECIEVED AND INSTALLED FLOORBOARD 242LF IAW B737NG AMM 53-21-00 AND B737NG AIPC 53-21-51.<BR><BR>PART#146A5610-457<BR>PO: 1107024.4;[02] REMOVED; RECIEVED AND INSTALLED FLOORBOARD 242LF IAW B737NG AMM 53-21-00 AND B737NG AIPC 53-21-51.<BR><BR>PART#146A5610-457<BR>PO: 1107024.4

Part: FLOORBOARD — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,347 hrs · 16,219 cycles

C/R (AH) MAIN CABIN FLOORBOARD 242CF HAS DELAMINATION<[01] REMOVED AND REPLACED PANEL 242CF IAW B737NG AMM53-21-00<BR>TOOL ID T05867-175 CAL DUE 12/18/2024;[02] VERIFIED REMOVED AND REPLACED PANEL 242CF IAW B737NG AMM53-21-00<BR>TOOL ID T05867-175 CAL DUE 12/18/2024

Part: FLOORBOARD — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,347 hrs · 16,219 cycles

C/R (AH) MAIN CABIN FLOORBOARD 232RF HAS DELAMINATION<[01] REMOVED; RECIEVED AND INSTALLED CABIN FLOORBOARD 232RF IAW B737NG AMM 53-21-00 AND B737NG AIPC 53-21-00<BR><BR>PART# 144A5810-124<BR>PO:0;[02] REMOVED; RECIEVED AND INSTALLED CABIN FLOORBOARD 232RF IAW B737NG AMM 53-21-00 AND B737NG AIPC 53-21-00<BR><BR>PART# 144A5810-124<BR>PO:0

Part: FLOORBOARD — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,347 hrs · 16,219 cycles

C/R (AH) MAIN CABIN FLOORBOARD 231KF HAS DELAMINATION<[01] RECIEVED AND INSTALLED NEW CABIN FLOORBOARD IAW B737NG AIPC 53-21-51 AND B737NG AMM 53-21-00. <BR><BR>FLOOR BOARD PART#143A5810-522<BR>PO: 1107024.1;[02] REMOVED; RECIEVED AND INSTALLED NEW CABIN FLOORBOARD IAW B737NG AIPC 53-21-51 AND B737NG AMM 53-21-00.<BR><BR>FLOOR BOARD PART#143A5810-522<BR>PO: 1107024.1;[03] REMOVED; RECIEVED AND INSTALLED NEW CABIN FLOORBOARD IAW B737NG AIPC 53-21-51 AND B737NG AMM 53-21-00.<BR><BR>FLOOR BOARD PART#143A5810-522<BR>PO: 1107024.1

Part: FLOORBOARD — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,347 hrs · 16,219 cycles

C/R (AH) MAIN CABIN FLOORBOARD 232KF HAS DELAMINATION<[01] REMOVED OLD PANEL 232KF AND INSTALLED NEW PANEL 232KF P/N 143A5810-526 PO: 1107042.1 IAW B737NG AMM 53-21-00-401-NG;[02] REMOVED OLD PANEL 232KF AND INSTALLED NEW PANEL 232KF P/N 143A5810-526 PO: 1107042.1 IAW B737NG AMM 53-21-00-401-NG. VERIFIED REPLACEMENT OF FLOORBOARD PANEL

Part: FLOORBOARD — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,347 hrs · 16,219 cycles

C/R (AH) MAIN CABIN FLOORBOARD 241KF HAS DELAMINATION<[01] REMOVED; RECIEVED AND INSTALLED FLOORBOARD 241KF IAW B737NG AMM 52-21-00. AND B737NG AIPC 53-21-51.<BR><BR>PART#146A5810-458<BR>PO: 1107024.5;[02] REMOVED; RECIEVED AND INSTALLED FLOORBOARD 241KF IAW B737NG AMM 52-21-00. AND B737NG AIPC 53-21-51.<BR><BR>PART#146A5810-458<BR>PO: 1107024.5

Part: FLOORBOARD — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,347 hrs · 16,219 cycles

C/R (AH) MAIN CABIN FLOORBOARD 242GF HAS DELAMINATION<[01] REMOVED; RECIEVED AND INSTALLED FLOORBOARD 242GF IAW B737NG AMM 53-21-00 AND B737NG AIPC 53-21-51<BR><BR>PART#146A5810-457<BR>PO: 1107024.6;[02] REMOVED; RECIEVED AND INSTALLED FLOORBOARD 242GF IAW B737NG AMM 53-21-00 AND B737NG AIPC 53-21-51<BR><BR>PART#146A5810-457<BR>PO: 1107024.6

Part: FLOORBOARD — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,347 hrs · 16,219 cycles

C/R (AH) MAIN CABIN FLOORBOARD 232HF HAS DELAMINATION<[01] REMOVED AND REPLACED PANEL 232HF IAW B737NG AMM 53-21-00;[02] REMOVED AND REPLACED PANEL 232HF IAW B737NG AMM 53-21-00. VERIFIED REPLACEMENT OF FLOORBOARD.

Part: BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 33,347 hrs · 16,219 cycles

LEFT WING DEFLECTION CONTROL RIB ATTACH BRACKET ON O/B SIDE IS CRACKED. DOT K065 AND STREAMER ATTACHED.<[01] REMOVED AND REPLACED LEFT WING DEFLECTION CONTROL RIB ATTACH BRACKET PN:115A6260-1 PO: 1107031.1 IAW B737-800 SRM 51-40-02; AIPC 57-42-51-03;[02] VERIFIED REMOVED AND REPLACED LEFT WING DEFLECTION CONTROL RIB ATTACH BRACKET PN:115A6260-1 PO: 1107031.1 IAW B737-800 SRM 51-40-02; AIPC 57-42-51-03

Part: DOOR — MISSING (LAV SERVICE) · airframe 32,566 hrs · 15,784 cycles

ON WALKAROUND CREW REPORTED TO MX LAV SERVICE DOOR MISSING<[01] OK. TO CONTINUE ON CDL PER AUTH #210325;[02] INSTALLED NEW LAV SERVICE DOOR IAW AMM 52-49-07 OPS CHECK GOOD

Part: GUIDE ARM — OUT OF ADJUST (ZONE 800) · airframe 32,305 hrs · 15,648 cycles

AIRCRAFT FAILED TO PRESSURIZE AFTER TAKE OFF. FWD SERVICE DOOR SHOWS DAY LIGHT. MAX ALT 12000FT CABIN ALT FOLLOWED FLIGHT ALT. . DOOR WARN NEVER DISPLAYED.<[01] ADJUSTED FWD SERVICE DOOR GUIDE ARM PER AMM 52-41-00. R&R'D SENSOR ASSY FOR S194 PER AMM 52-71-11. OPS CK GOOD

Part: SENSOR — FAULTED (ZONE 800) · airframe 32,305 hrs · 15,648 cycles

AIRCRAFT FAILED TO PRESSURIZE AFTER TAKE OFF. FWD SERVICE DOOR SHOWS DAY LIGHT. MAX ALT 12000FT CABIN ALT FOLLOWED FLIGHT ALT. . DOOR WARN NEVER DISPLAYED.<[01] ADJUSTED FWD SERVICE DOOR GUIDE ARM PER AMM 52-41-00. R&R'D SENSOR ASSY FOR S194 PER AMM 52-71-11. OPS CK GOOD

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 32,147 hrs · 15,560 cycles

R/H SIDE EMERGENCY LIGHTS INOP FIRST 3 OVERHEADBIN<[01] REMOVED AND REPLACED BATTERY PACK M2335 IAW AMM 33-51-06 OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 32,147 hrs · 15,560 cycles

R/H MID CABIN EMERGENCY LIGHTS EXIT SIGNS INOP<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1695 IAW AMM 33-51-06 OPS CHECK GOOD

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 31,555 hrs · 15,241 cycles

AFT CARGO PIT PANEL 141DW HAS CRACKS AND RIVETS WORN THROUGH IN SEVERAL PLACES<

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 30,917 hrs · 14,902 cycles

CREW REPORTS EMERGENCY LIGHT COVER ON THE FWD CEILING BULLNOSE BROKEN<[01] OKAY TO CONTINUE PER MEL 33-15-02 SP1;[02] REPLACED EMERGENCY AISLE LIGHT COVER REF AMM 33-51-03.

Part: LIGHT — LOOSE (ZN 200 FUS TOP) · airframe 30,007 hrs · 14,391 cycles

OVER WING EXIT SIGN FACE COVER IN CEILING LOOSE<[01] R&R OVERWING EXIT EMERGENCY LIGHT ASSY REF AMM 33-51-01; PERFORMED OPS CHECK OF LIGHTS REF 33-51-00; OPS CHECK GOOD.

Part: LIGHT — MISSING (ZN 200 FUS TOP) · airframe 29,260 hrs · 13,950 cycles

EMERGENCY EXIT LIGHT ASSY BY AFT LH LAV MISSING<[01] INSTALLED NEW EMERGENCY EXIT LIGHT ASSY. IAW AMM 33-51-01; EMERGENCY LIGHTS OPS CHECK GOOD.

Part: SLIDE — OUT OF ADJUST (ZN 800 DOOR) · airframe 29,040 hrs · 13,826 cycles

AFT ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] REATTACHED VELCRO TO THE BACKING PAN SHELF IN REF MT 725-230-00-03

Part: COVER — LOOSE (ZN 200 FUS TOP) · airframe 29,040 hrs · 13,826 cycles

EXIT SIGN COVER FELL OFF SIGN AT OVERWING<[01] SECURED EXIT SIGN COVER AT OVERWING IAW B737 AMM 33-51-01.

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 29,040 hrs · 13,826 cycles

RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31.

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 29,040 hrs · 13,826 cycles

LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LEFT FWD UPPER HORIZONTAL STAB SLIDING SEAL PER AMM 53-31-31

Part: COVER — LOOSE (ZN 200 FUS TOP) · airframe 28,945 hrs · 13,776 cycles

CENTER EMERGENCY EXIT COVERS FELL OFF<[01] INSTALLED BOTH LENS COVERS ON CENTER AISLE EMERGENCY EXIT SIGN PER AMM 33-51-01

Part: SIGN — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 28,682 hrs · 13,621 cycles

OVERHEAD EXIT ROW SIGN MID CABIN FELL OFF.<[01] REINSTALLED REF. AMM 33-51-03

Part: SIGN — INOPERATIVE (ZN 200 FUS TOP) · airframe 28,553 hrs · 13,551 cycles

PART OF THE EXIT SIGN IS MISSING ABOVE THE ISLE AT ROW 14.<[01] INSTALLED CENTER CABIN EMERGENCY EXIT LENSE AS PER AMM 33-51-00.

Part: STRIP — INOPERATIVE (ZN 200 FUS TOP) · airframe 28,492 hrs · 13,521 cycles

PHOTO LUMINESCENCE LIGHT STRIP FO SIDE FIRST ROW VERY DIM OR NOT WORKING<[01] R&R PHOTOLUMINESCENT STRIP AT ROW 1 DEF IAW AMM 33-51-15. OPS CK GOOD.

Part: GIRT BAR — OUT OF ADJUST (ZN 900 LAV/GALLE) · airframe 26,643 hrs · 12,489 cycles

AFT ENTRY DOOR SLIDE GIRT IS CATCHING DURING CLOSING OF DOOR. / [01] REMOVED AND REPLACED SLIDE ON LINE #1833.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,643 hrs · 12,489 cycles

SEVERAL CABIN EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY PACKS PER AMM 33-51-06.

Part: FAIRING — DELAMINATED (RT WING) · airframe 26,643 hrs · 12,489 cycles

RH WING #6 CANOE FAIRING CONE UPPER SURFACE HAS TWO AREAS OF DELAMINATION (MARKED) / [01] REMOVED AND INSTALLED MM 27-51-18.

Part: WEB — CORRODED (BS 792-847) · airframe 26,643 hrs · 12,489 cycles

AFT CARGO COMPARTMENT THRESHOLD WEB HAS AREAS OF CORROSION FORM STA 792-847. / [01] BLENDED AREA PER SRM 51-10-02. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1. REMOVED DAMAGED WEB PER SRM 51-40-02.;[02] LOCATED HOLES AND DRILLED IN NEW WEB PER SRM 51-40-02.INSTALLED NUTPLATES TO WEB PER SRM 51-40-02;[03] VERIFIED CORRECTIVE ACTION #2;[04] COUNTERSUNK ATTACHMENT HOLES PER SRM 51-40-02. TREATED AND PAINTED ALL ADDED HOLES PER SRM 51-20-01 AND AMM 51-21-72.;[05] VERIFIED COUNTERSUNK ATTACHMENT HOLES PER SRM 51-40-02. TREATED AND PAINTED ALL ADDED HOLES PER SRM 51-20-01 AND AMM 51-21-72.;[06] OK TO INSTALL WEB.;[07] REMOVED AND REPLACED AFT CARGO THRESHOLD WEB I.A.W SRM 51-40-02.

Part: ANGLE — CORRODED (ZN 200 FUS TOP) · airframe 26,643 hrs · 12,489 cycles

EVIDENCE OF CORROSION ON FWD SERVICE DOOR THRESHOLD Z ANGLE. B.S. 294 - 328 RBL 58 / [01] BLENDED OUT CORROSION AT FWD SERVICE DOOR THRESHOLD UPPER SURFACE OF EXTRUDED ANGLE STA 294 - 328; RBL 58 PER SRM 51-10-02. DAMAGE FOUND OUT OF LIMITS PER SRM 53-10-15-1A-2 FIG. 103; DETAIL D.;[02] REMOVED AND REPLACED ANGLE PER SRM 51-10-02 AND SRM 51-40-02

Part: ANGLE — CORRODED (BS 787-807) · airframe 26,643 hrs · 12,489 cycles

AFT CARGO FLOOR TRANSITION ANGLE HAS AREAS OF CORROSION AROUND FASTENER HOLES FROM STA 787-807 LBL 21. REMOVED CORROSION PER SRM 51-10-02.FOUND TO BE WITHIN LIMITS PER SRM 53-00-53-1A-2. TREATED AND PRIMED THE AREA PER SRM 51-20-01. REMOVED CORROSION PER SRM 51-10-02.FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A-2.

Part: FLAP — DELAMINATED (ZN 500 LEFT WING) · airframe 26,643 hrs · 12,489 cycles

LEFT WING O/B AFT FLAP HAS LARGE AREA OF DELAMINATION LOCATED ON UPPER AND LOWER SURFACE OF INBOARD END. / [01] OK TO INSTALL SERVICEABLE FLAP;[02] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22;[03] VERIFIED CORRECTIVE ACTION STEP #2;[04] VERIFIED CORRECTIVE ACTION STEP #2;[05] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22;[06] VERIFIED CORRECTIVE ACTION #5

Part: FASTENER — PULLED (LT INLET) · airframe 26,643 hrs · 12,489 cycles

ON THE #1 ENGINE INLET LIP SKIN EXTERNAL SURFACE, THERE ARE TWO FASTENERS BELOW THE INBD SEAM THAT ARE PULLING THROUGH. REMOVED FASTENERS IAW SRM 51-40-02. REAMED HOLES TO FIRST OVERSIZE IAW SRM 54-10-01-1A-2 TABLE 101. PERFORMED FASTENER HOLE PROBE INSPECTION IAW NDT PART 6-51-00-00 PROCEDURE 16. NO DEFECTS NOTED.

Part: FASTENER — PULLED (NR 1 INLET) · airframe 26,643 hrs · 12,489 cycles

ON THE #1 ENGINE INLET LIP SKIN EXTERNAL SURFACE; THERE ARE TWO FASTENERS ABOVE THE INBD SEAM THAT ARE PULLING THROUGH. / [01] REMOVED 2 EACH LOOSE FASTENERS AT #1 ENGINE INLET LIP SKIN EXTERNAL SURFACE; ABOVE I/B SEAM PER SRM 51-40-02. REAMED FASTENER HOLES TO FIRST OVERSIZE PER SRM 54-10-01-1A-2 TABLE 101.;[02] INSPECTED WORK PERFORMED IN C/A #!;[03] PERFORMED FASTENER HOLE PROBE INSPECTION PER 737NDT PART 6 51-00-00 PROCEDURE 16. NO DEFECTS NOTED;[04] INSTALLED NEW FASTENERS PER SRM 54-10-01-1A-2 AND SRM 51-40-02;[05] C/W INSPECTION OF STEP #4;[06] REMOVED AND REPLACED FASTENERS PER SRM 54-10-01-1A-2

Part: BULKHEAD — CRACKED (AFT CARGO) · airframe 26,643 hrs · 12,489 cycles

AFT CARGO COMPARTMENT; FWD BULKHEAD PNL 142NW IS CRACKED. / [01] REPAIRED PER CMM 25-00-66.;[02] C/W

Part: FASTENER — LOOSE (LT INLET) · airframe 26,643 hrs · 12,489 cycles

ON THE NR 1 ENGINE INLET LIP SKIN EXTERNAL SURFACE. THERE ARE THREE FASTENERS ABOVE THE OTBD SEAM THAT ARE PULLING THROUGH. REMOVED LOOSE FASTENERS IAW SRM 51-40-02. REAMED FASTENER HOLES TO FIRST OVERSIZE IAW SRM 54-10-01-1A-2 TABLE 101. PERFORMED FASTENER HOLE PROBE INSPECTION IAW NDT PART 6-51-00-00 PROCEDURE 16. NO DEFECTS NOTED. INSTALLED NEW FASTENERS IAW SRM 54-10-01-1A-2 AND SRM 51-40-02.

Part: GIRT BAR — OUT OF POSITION (FWD SERVICE DOOR) · airframe 26,233 hrs · 12,238 cycles

FORWARD SERVICE DOOR GIRT BAR HOLDER IS LOOSE / [01] GIRT BAR RETAINER CLIPS OP NORMAL PER M/M 25-66-01

Part: NONE — OUT OF POSITION (CABIN FLOOR) · airframe 26,201 hrs · 12,221 cycles

EMERGENCY FLOOR PATH LIGHTING STRIP FWD OF ROW 12 ABC LOOSE / [01] RESECURED EMER FLOOR PATH LIGHTING STRIP PER SIP AND AMM 33-51-15

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 23,366 hrs · 10,617 cycles

FWD ENTRY SLIDE; OVER DOOR EXIT; AND LOWER LEFT ENTRY EMERGENCY EXTI LIGHTS INOP. NEEDS BATTERY PACK. / R&R M01675 CHARGER ASSY AND BATTERY PACK PER M/M 33-51-0

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 23,366 hrs · 10,617 cycles

FWD SERVICE SLIDE EMERGENCY LIGHT; FWD OVER DOOR EXIT LIGHT; AND FWD SERVICE LOWER EXIT EMERGENCY LIGHTS INOP REQURIES NEW BATTERY PACK / R&R EMERGENCY LIGHT BATTERY PACK OPS CHECK GOOD REF AMM 33-51-06

Part: CHARGER — INOPERATIVE (CABIN) · airframe 23,366 hrs · 10,617 cycles

FWD ENTRY SLIDE; OVER DOOR EXIT; AND LOWER LEFT ENTRY EMERGENCY EXTI LIGHTS INOP. NEEDS BATTERY PACK. / R&R M01675 CHARGER ASSY AND BATTERY PACK PER M/M 33-51-0

Part: GCU — BURNED (NR 2) · airframe 23,337 hrs · 10,598 cycles

NORMAL FLAP 5 TAKE OFF. DURING FLAP RETRACTION MASTER CAUTION ILLUMINATE WITH ASSOCIATED OVERHEAD; HYD; ANTI ICE & ELEC LIGHTS. 2 GOOD ENGINES & 2 GOOD GENS. F/A'S SMELLED FUMES AND WE DECLARED AN EMERGENCY AND RETURNED TO THE AIRPORT. F.O. LOST ALL CDS INSTERMENTATION. RIGHT SIDE CABIN WAS DARK. WE MADE AN OVERWEIGHT SMOOTH LANIDNG. FLAPS STUCK AT POSITION 1. / FOUND #2 GENERATOR CONTROL UNIT BURNED UP. R&R #2 GCU PER AMM 24-21-81. ALL SYSTEMS OPS CK NORMAL REF LOG PAGE 1949682; 1949623 FOR CONDITIONAL INSPECTIONS ISSUE# 3530713#2 GCU PN OFF/ON 762185J SN OFF AAA6015931 SN ON AAA6018181

Part: PLATE — CRACKED (R2 DOOR)

AFT SERVICE DOOR LOWER SILL PLATE CRACKED / REMOVED AND REPLACED AFT SERVICE DOOR SILL PLATE IAW SOPM 20-50-01 AND S.I.P.INSP : 112254

Part: LENS — OUT OF POSITION (EMERGENCY LIGHT) · airframe 9,884 hrs · 21,984 cycles

EXIT SIGN AT MID-CABIN LOOKING AFT IS UPSIDE DOWN / RE-POSITIONED LENSE PER AMM 33-51-01

Part: HANDLE — BROKEN (R1 DOOR) · airframe 21,004 hrs · 9,348 cycles

PULL HANDLE FOR FWD SERVICE DOOR BROKEN. / R/R PULL HANDLE @ FWD SVC. DOOR OPS CK GOOD PER M/M 52-41-20

Part: HANDLE — BROKEN (R1 DOOR) · airframe 20,967 hrs · 9,331 cycles

FWD SERVICE DOOR PULL HANDLE BROKEN / RESECURED PRE SIP

Part: SLIDE — OUT OF TOLERANCE (L1 DOOR) · airframe 20,411 hrs · 9,034 cycles

FWD ENTRY DOOR (L1) SLIDE GAUGE IS IN RED. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE ASSEMBLY, IAW SWA WORK INSTRUCTION NO 725-61-06 A TAG YF0100 POS: L1 TAG/GRB NO: 139798 P/N OFF: 5A3307-7 S/N OFF: BNG8456 P/N ON: 5A3307-7 S/N ON: BNG18047.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,411 hrs · 9,034 cycles

AFT CARGO COMPARTMENT ANGLE BELOW FWD SHIELD AT BS 767-787; RBL 24; WL 156; IS CORRODED / REMOVED CORROSION AT AFT CARGO ANGLE BELOW FWD SHIELD AT STA 767-787 RBL 24 IA-W SRM 51-10-02-0G-0. VERIFIED MATERIAL LOSE ORIGINAL 0.050 REMOVED .015 REMAIN .035 ALLOWABLE 10% FOUND OUT OF LIMITS USED AAR TOOL #29271 25MAR21 DUE DATE I-A-W SRM 53-60-15-1A-1. REMOVED ANGLE I-A-W SRM 51-40-02-0G-0 DRILLED NEW ANGLE I-A-W SRM 51-40-05-0G-0 AND BOEING DWG 146A0081 REV: A INSTALLED NEW ANGLE I-A-W SRM 51-40-02-0G-0 AND BOEING DWG 146A0081 REV: A P/N 146A8125-53

Part: ANGLE — CORRODED (AFT CARGO) · airframe 20,411 hrs · 9,034 cycles

AFT CARGO COMPARTMENT; AFT BULKHEAD; FLOOR ANGLE; BS947; RBL 24-18; WL 156 CORRODED / REMOVED CORROSION AFT CARGO COMPARTMENT; AFT BULKHEAD FLOOR ANGLE STA 947 RBL 24 - 18 IAW B737 SRM 51-10-02-0G-0 ITEM 15. ORIGINAL 'T' .080 REMAINING .078 LOSS .002. NO PUBLISHED ALLOWABLE LIMITS FOUND. REMOVED AND REPLACE FLOOR ANGLE (BRACKET) IAW B737 SRM 51-40-02-0G-0 AND DWG 149A8117 REV -

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,411 hrs · 9,034 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140AF CORRODED / MEASURED LENGTH OF CORROSION DAMAGE TO BE = 42' LIMIT = 20' PANEL 140AF IS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102 FABRICATED NEW PANEL IAW AMM 25-52-01-201-801 AND DWG 453A2610 REV E TREATED AND PRIMED PANEL IAW AMM 51-21-41-370-802 AND AMM 51-21-42-340-804

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 20,411 hrs · 9,034 cycles

FWD CARGO COMPT. FLOOR PANEL 120DF HAS CORROSION AROUND EDGES / EVALUATED CORROSION ON FWD CARGO FLOOR PANEL # 120DF DAMAGE EXCEEDS 20IN TOTAL LENGTH OUT OF LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW PANEL IAW AMM 25-52-01-201-801 APPLIED CHEMICAL CONVERSION AND PRIMER IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804

Part: STRIP — CORRODED (BS 773 L-RBL 20) · airframe 20,411 hrs · 9,034 cycles

AFT CARGO COMPARTMENT; FLOOR PANEL LATERAL UNION STRIP; BS773; RBL20-LBL20; WL 156 CORRODED / REPLACED DEFECTIVE PART FOR NEW PART ON PARTS RACK; VERIFIED PART AS MPN 1469401-4 IAW AIPC 53-41-11-26; ITEM 95. PART IS AFT CARGO COMPT. FLOOR PANEL LATERAL UNION STRIP. BS 773 AND INSTALLED ON SAM 565S WN5596

Part: ANGLE — CRACKED (BS 663) · airframe 20,411 hrs · 9,034 cycles

RIGHT HAND PACK BAY; HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 RBL 10 IS CRACKED 3RD FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. MARKED. / RH A/C BAY AT BS 663; UPPER HORIZONTAL ANGLE COMMON TO THE LOWER SIDE OF CENTER FUEL TANK; AT RBL 10. CUTOUT DAMAGED ANGLE. FABRICATED NEW REPAIR PARTS; INSTALLED REPAIR ANGLES; AND CAP SEALED; AND FILLET SEALED IAW SRM 57-10-10-2R-5 REPAIR 5. LEAK CHECKED REPAIR IAW AMM 28-11-00-790-801. LEAK CHECK GOOD.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 20,411 hrs · 9,034 cycles

AFT CARGO COMPARTMENT RT Z-ANGLE CORRODED FROM BS 727B-767; RBL 24; WL 156. REMOVED CORROSION AT AFT CARGO COMPARTMENT RT Z-ANGLE STA 727B-767 RBL 24, IAW B737 SRM 51-10-02-0G-0 ITEM 15. ORIGINAL 'T' .040 REMAINING .013 LOSS .013 FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-53-1A-2 FIG 103. CUTOUT DAMAGE SECTION BETWEEN 727F AND 727G. FABRICATED AND INSTALLED REPAIR Z-ANGLE STA 727F TO 767 RBL 24, IAW B737 SRM 53-00-53-2R-5 REPAIR 5. P/N 146A7502-52.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 20,411 hrs · 9,034 cycles

CABIN FLOOR SUPPORT AT STA 540 BL0 -LBL25 UNDER PANEL 231UF IS CRACKED / REMOVED AND REPLACED CABIN FLOOR PANEL BREAK AT STA 540 BL0 - LBL 25 IAW SRM 51-40-02-0G-0 AND BOEING DWG # 143A0060 REV A APPLIED CIC IAW AMM 51-21-91-620-802

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,411 hrs · 9,034 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140DF CORRODED / EVALUATED CORROSION ON AFT CARGO COMPARTMENT FLOOR PANEL 140DF AND FOUND LENGTH OF ACCUMULATED CORROSION DAMAGE TO EXCEED THE 20' MAXIMUM ALLOWED OUT OF LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW PANEL 140DF IAW AMM 25-52-01-201-801 AND BOEING DWG # 453A2610 REV B TREATED AND PRIMED IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804 A TAG 66777

Part: RAIL — CORRODED (FUSELAGE) · airframe 20,411 hrs · 9,034 cycles

FWD PIT LATERAL FLOOR SUPPORT UPPER SURFACE CORRODED AT STA 500I FROM RBL24 TO LBL24 AND W/L157 / NO LIMITS PUBLISHED; FOUND PART OUT OF LIMITS. 100% MATERIAL LOSS ON FWD PIT LATERAL FLOOR SUPPORT (RAIL) STA 500I RBL 24 TO LBL 24. REMOVED AND REPLACED RAIL P/N 143A9485-35 TAG # WN8765 IAW B737 SRM 51-40-02-0G-0 AND DWG 143A9481 REV. -

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 20,411 hrs · 9,034 cycles

CABIN FLOOR PANEL 231TF HAS SMALL PUNCTURE 3' FROM FWD EDGE AND 7' FROM INBOARD EDGE. REPAIRED CABIN FLOORPANEL 231TF PUNCTURED, IAW B737 SRM 53-00-50-2R-1 AND B737 SRM 53-00-50-2R-0 A34018; A87102; A72547.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 20,411 hrs · 9,034 cycles

FWD CARGO COMPT. FLOOR PANEL 120AF HAS CORROSION AROUND EDGES / EVALUATED CORROSION AROUND EDGES ON FWD CARGO COMPT FLOOR PANEL 120AF AND FOUND TOTAL ACCUMULATED CORROSION DAMAGE TO EXCEED THE 20' MAXIMUM ALLOWED OUT OF LIMITS IAW SRM 53-00-53-1A-1 NEW PANEL 120AF FABRICATED IAW AMM 25-52-01-201-801 AND BOEING DWG 453A1610 REV B TREATED AND PRIMED IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804 A TAG C06776 453A1610-104

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 20,411 hrs · 9,034 cycles

FWD CARGO COMPT. FLOOR PANEL 120CF HAS CORROSION AROUND EDGES / MEASURED CORROSION DAMAGE TO BE = 27' LIMIT = 20' PANEL 120CF IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102 FABRICATED NEW PANEL 120CF IAW AMM 25-52-01-201-801 AND DWG 453A1610 REV - TREATED AND PRIMED IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804

Part: CHANNEL — CRACKED (R/H WING) · airframe 20,411 hrs · 9,034 cycles

RIGHT WING UPPER FIXED T/E PANEL; JUST INBD OF DEFLECTION CONTROL RIB; SUPPORT ANGLE UPPER FLANGE CRACKED THROUGH OTBD FASTENER. / R/H WING FIXED T/E SUPPORT ANGLE CHANNEL CRACKED. DRILLED AND REMOVED CRACKED CHANNEL I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ANGLE CHANNEL I/A/W SRM 51-40-05-0G-0 ALSO BOEING DWG 115A2512 REV: B. INSTALLED NEW R/H WING NEW SUPPORT ANGLE CHANNEL I/A/W SRM 51-40-02-0G-0 ALSO BOEINGDWG 115A2512 REV: B.

Part: ANGLE — CRACKED (BS 663) · airframe 20,411 hrs · 9,034 cycles

LT A/C BAY AT BS 663 UPPER ANGLE IS CRACKED, JUST OUTBOARD OF KEEL BEAM AT LBL 8. LT A/C BAY AT BS 663 UPPER ANGLE, JUST OUTBOARD OF KEEL BEAM AT LBL 8, CUTOUT DAMAGED ANGLE. FABRICATED NEW REPAIR PARTS, INSTALLED REPAIR ANGLES, IAW SRM 57-10-10-2R-5 REPAIR 5. CAP SEALED AND FILLET SEALED, IAW SRM 57-10-10-2R-5. LEAK CHECKED REPAIR, IAW AMM 28-11-00-790-801. LEAK CHECK GOOD.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,411 hrs · 9,034 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140CF CORRODED / AFT CARGO FLOOR PNL 140CF IS CORRODED PNL 140CF IS 'OUT OF LIMITS' IS HAS MORE THAN 20' ACCUMULATED OF CORROSION IAW SRM 53-00-53-1A-1 FIG 102 FABRICATED NEW PNL 140CF IAW AMM 53-00-53-1A-1 STEP F (2) (3) (4) ALSO AMM 25-52-01-201-801 ALODINED AND PRIMED IAW AMM 51-21-41-370-801 AND AMM 51-21-72-370-802

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,411 hrs · 9,034 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140BF CORRODED / EVALUATED CORROSION AT AFT CARGO COMPARTMENT FLOOR PANEL 140BF FOUND CORROSION EXCESS 20' IN IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW PANEL 140BF IAW AMM 25-52-01-201-801 AND BOEING DWG # 453A2610 REV E

Part: FLOOR SUPPORT — CORRODED (BS 500A-500I) · airframe 20,411 hrs · 9,034 cycles

FWD PIT RIGHT FLOOR SUPPORT Z ANGLE UPPER SURFACE CORRODED FROM STA 500A+10' TO STA 500I AT RBL 24 AND W/L 157. REMOVED CORROSION AT RT Z ANGLE STA 500A TO 500I AS MARKED, IAW SRM 51-10-02-0G-0 AND SRM 53-00-53-1A-2. VERIFIED WITH 10X MAGNIFICATION. ORIGINAL THICKNESS .040' AT STA 500A+10 .034'; STA 500C+18 .035'; STA 500D+10 .032' AND STA 500H+17 .033'. ALL OUT OF LIMITS, IAW SRM 53-00-53-1A-1 FIG 103. TOOL: 36644 DUE: 08/24/21. REMOVED OUT OF LIMITS FWD CARGO RT Z ANGLE FROM STA 500A TO 500I AND INSTALLED RT ZANGLE REPAIR PARTS, IAW SRM 53-00-53-2R-5. APPLIED CIC IAW SRM 53-00-53-2R-5 STEP N P/N 146A7501-188.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 20,411 hrs · 9,034 cycles

AFT CARGO COMPARTMENT FLOOR SHIELD BS767-787; RBL 24; WL 156 CORRODED / REMOVED CORROSION AT AFT CARGO FLOORSHIELD BS767 - 787 RBL 24 I-A-W 51-10-02-0G-0. VERIFIED MATERIAL LOOSE ORIGINAL .050 REMOVED .012 REMAIN .038 ALLOWABLE 10% FOUND OUT OF LIMITS USED AAR TOOL #26646 DUE 10/07/2021 IAW SRM 53-60-15-1A-1. REMOVED SHIELD I-A-W SRM 51-40-02-0G-0. DRILLED NEW SHIELD I-A-W SRM 51-40-05-0G-0 AND BOEING DWG 146A0081 REV: A INSTALLED NEW SHIELD I-A-W SRM 51-40-02-0G-0 AND BOEING DWG 146A0081 REV: A

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,411 hrs · 9,034 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140EF CORRODED / EVALUATED CORROSION ON AFT CARGO COMPARTMENT FLOOR PANEL 140EF CORROSION IS MORE THAN 20' IN LONG IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW FLOOR PNL 140EF IAW AMM 25-52-01-201-801 AND BOEING DWG # 453A2610 REV C

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 20,411 hrs · 9,034 cycles

AFT CARGO COMPARTMENT LT Z-ANGLE CORRODED FROM BS 727E-807; LBL 24; WL 156. REMOVED CORROSION AT AFT CARGO COMPARTMENT LT Z-ANGLE STA 727E TO 807 LBL 24, IAW B737 SRM 51-10-02-0G-0 ITEM 15. ORIGINAL 'T' .040 REMAINING .028 LOSS .012. FOUND TO BE OUT OF LIMITS, IAW B737 SRM 53-00-53-1A-2 FIG 103. CUTOUT DAMAGE SECTION AT BETWEEN STA 727E AND 727F. FABRICATED AND INSTALLED REPAIR Z-ANGLE STA 727F TO 847 LBL 24, IAW B737 SRM 53-00-53-2R-5 REPAIR 5. P/N 146A7502-31.

Part: FLAP — DELAMINATED (L/H WING) · airframe 15,633 hrs · 6,814 cycles

ENTRY FOR DELAY PURPOSES - LEFT OTBD FLAP CANOE FAIRING DELAMINATION / R/R FWD CANOE FAIRING

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 15,552 hrs · 6,777 cycles

L1 DOOR GIRT BAR LOOSE. ADJUSTED GIRT BAR RETAINER TENSION PER SIP AND AMM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 15,252 hrs · 6,644 cycles

CENTER CABIN EMERGENCY EXIT LIGHT LENS COVER CAME OFF. / REINSTALLED COVER IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 14,956 hrs · 6,513 cycles

MID CABIN OVHD EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 14,934 hrs · 6,502 cycles

L/H WING AFT FIXED TRAILING EDGE UPPER SUPPORT BRACKET CRACKED THRU O/B MOST FASTENER CRACK VERIFIED PER 737 NDT 51-00-00 FIG 23. CRACK IS 3/4 INCH INBOARD OF FASTENER AND 1/2 INCH OUTBOARD OF FASTENER. D124 / R&R'D UPPER SUPPORT BRACKET PER SRM 51-40-02

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 12,023 hrs · 5,259 cycles

LEFT AFT EMERGENCY EXIT LIGHT LENS WAS MISSING. INSTALLED THE LENS IAW SIP & AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 10,517 hrs · 4,590 cycles

MID CABIN CEILING EXIT LIGHT LENS LOOSE. / SECURED LENS PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,592 hrs · 4,157 cycles

LEFT AFT ENTRY EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 9,495 hrs · 4,117 cycles

LT AFT LAV EMERGENCY LIGHT LENS LOOSE. SECURED LENS PER SIP.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,588 hrs · 3,720 cycles

SUPPLEMENTAL INFORMATION: ANGLE CRACKED BS 370 BETWEEN STRINGER 17-18 L/H / REMOVED AND REPLACED ANGLE BS 370 BETWEEN STRINGER 17-18 L/H IAW SRM 51-40-02-0G-0

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 8,588 hrs · 3,720 cycles

PASSENGER FLOOR PANEL 221GF HAS DAMAGE AROUND THE INSERT AT THE SECOND HOLE AFT ON THE L/H SIDE / REPAIRED DAMAGE AROUND THE INSERT AT THE SECOND HOLE AFT ON THE L/H SIDE OF PASSENGER FLOOR PANEL 221GF IAW SRM 53-00-50-2R-9. 57066U 05/25/17

Part: ANGLE — CRACKED (BS 370) · airframe 8,585 hrs · 3,719 cycles

ANGLE CRACKED AT BS 370, BETWEEN STRINGER 17 TO 18L. R & R THE ANGLE IAW SRM.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 8,399 hrs · 3,642 cycles

CENTER AISLE OVERWING EMERGENCY EXIT SIGN COVER CAME OFF. SECURED THE COVER IAW SIP.

Part: COVER — MISSING (CABIN) · airframe 456 hrs · 205 cycles

AFT GALLEY EMER EXIT LIGHT COVER MISSING. INSTALLED COVER IAW AMM.