N8655D

Part: STOP FITTING — OUT OF ADJUST (ZONE 700) · airframe 36,750 hrs · 17,893 cycles

AFTER TAKEOFF RAISED GEAR HANDLE TO UP POSITION, GEAR CAME UP UPON MOVING GEAR HANDLE TO OFF POSITION RECEIVED A RED NOSE GEAR LIGHT AND COULD HEAR THAT THE GEAR EXTENDED. OK CONTINUE PER MEL 32-16-01, SP1. ADJUSTED RT NLG DOOR AFT STOP IAW AMM 32-22-11-000-802. PERFORMED OPS TEST OF NLG IAW AMM 32-33-00-710-801. OP CHKD OK. INSPECTED IAW AMM 32-22-11-000-802-NG.

Part: COVER — UNSECURE (ZONE 800) · airframe 36,250 hrs · 17,633 cycles

L2 DOOR SLIDE COVER WINDOW NOT SECURE. SECURED L2 DOOR SLIDE COVER IAW SOPM 20-50-12.

Part: HANDLE — LOOSE (ZONE 800) · airframe 36,017 hrs · 17,504 cycles

R2 DOOR ASSIST HANDLE LOOSE. SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31.

Part: HANDLE — LOOSE (ZONE 800) · airframe 36,017 hrs · 17,504 cycles

L1 DOOR ASSIST HANDLES (BOTH) LOOSE. SECURED BOTH L1 DOOR ASSIST HANDLES IAW AMM 52-11-31.

Part: HANDLE — UNSECURE (ZONE 800) · airframe 36,017 hrs · 17,504 cycles

R1 DOOR ASSIST HANDLE LOOSE DOOR SIDE. SECURED R1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31.

Part: BATTERY — NO TEST (ZONE 200) · airframe 33,947 hrs · 16,418 cycles

FWD FA FLASHLIGHT INOP<[01] R & R FWD F.A. FLASHLIGHT BATTERY. OPS CK GOOD PER AMM 25-64-00

Part: POWER SUPPLY — INOPERATIVE (ZN 200 FUS TOP) · airframe 33,505 hrs · 16,179 cycles

FWD L/H ENTRY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED FWD L/H EMERGENCY POWER SUPPLY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805;[02] REMOVED AND REPLACED FWD L/H EMERGENCY POWER SUPPLY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805

Part: FLAP — DELAMINATED (ZN 600 RIGHT WIN) · airframe 33,505 hrs · 16,179 cycles

R/H O/B AFT FLAP HAS SIGN OF DELAMINATION AT THE I/B AFT CORNER AREA. R/H O/B AFT FLAP HAS SIGNS OF DEMLAMINTION AT THE I/B AFT CORNER AREA.<[01] R/H O/B AFT FLAP REMOVED AND REPLACED IAW B737-800 AMM 27-51-22;[02] VERIFIED R/H O/B AFT FLAP REMOVED AND REPLACED IAW B737-800 AMM 27-51-22

Part: BRACKET — CRACKED (ZN 600 RIGHT WIN) · airframe 33,505 hrs · 16,179 cycles

RIGHT WING TRAILING EDGE WEB AT AFT PYLON AREA HAS A CRACKED BRACKET. STREAMERED<[01] REMOVED AND REPLACED BRACKET 115A6260-2 PO#1084100.3 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A;[02] REMOVED AND REPLACED BRACKET 115A6260-2 PO#1084100.3 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,505 hrs · 16,179 cycles

CR: (MH) FLOOR PANEL 232JF DELAM REQ. REMOVE AND REPLACE<[01] C/W T/C REMOVED AND REPLACED FLOOR PANEL 232JF;[02] REMOVED AND REPLACED NEW FLOOR PNL 232JF IAW B737-800 AMM 53-21-00-401;[03] VERIFIED REMOVED AND REPLACED NEW FLOOR PNL 232JF IAW B737-800 AMM 53-21-00-401

Part: BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 33,505 hrs · 16,179 cycles

LEFT WING TRAILING EDGE WEB AT AFT PYLON AREA HAS A CRACKED BRACKET OUTBOARD END OF WEB.<[01] REMOVED AND REPLACED BRACKET 115A6260-1 PO#110490.1 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A;[02] REMOVED AND REPLACED BRACKET 115A6260-1 PO#110490.1 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,505 hrs · 16,179 cycles

CR: (MH) FLOOR PANEL 241RF DELAM REQ. REMOVE AND REPLACE<[01] REMOVED AND REPLACED PANEL 241RF IAW B737NG AMM 53-21-00-401;[02] REMOVED AND REPLACED PANEL 241RF IAW B737NG AMM 53-21-00-401

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,505 hrs · 16,179 cycles

CR: (MH) FLOOR PANEL 231LF DELAM/ PUNCTURE REQ. REMOVE AND REPLACE<[01] REMOVED AND REINSTALLED FLOOR PANEL 231LF IAW B737 AMM 53-21-00<BR>TOOL: T03830-22<BR>DUE: 23/JAN/25;[02] REMOVED AND REINSTALLED FLOOR PANEL 231LF IAW B737 AMM 53-21-00<BR>TOOL: T03830-22<BR>DUE: 23/JAN/25<BR> VERIFIED

Part: DOUBLER — CRACKED (ZONE 100) · airframe 33,505 hrs · 16,179 cycles

EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER CRACKED<[01] ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4;[02] VERIFIED ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4;[03] VERIFIED ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4;[04] VERIFIED ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4

Part: PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 33,505 hrs · 16,179 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD PANEL 121HW HAS 2EA DELAMINATED MARKS (DOT K049)<[01] REPAIRED PANEL 121HW OF 2 PUNCTURES IAW B737-800 AMM 25-00-00-300-801;[02] 02 - INSPECTED PER [AMM 25-00-00-300-801-NG (CRUSHED-CORE AND SANDWICH PANEL REPAIR - PERMANENT)]

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 33,505 hrs · 16,179 cycles

R/H VAPOR BARRIER ANGLE CRACKED AT APPROX RBL 8<[01] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW VAPOR BARRIER ATTACH ANGLE; CHANNEL; STIFENER AND FITTING AT WING SECTION REAR SPART R/H FROM STA RBL 5 TO RBL 65 IAW B737-800 SRM 57-10-10-2R-5 ACCOMPLISHED A OPEN HOLE HFEC INSPECTION OF ALL OPEN HOLES ON THE R/H VAPOR BARRIER REPLACEMENT AREA IAW 737 NDT MAN. PT. 6; 51-00-00 PROC. 16. USING T8257I DUE 03 OCT. 25. NO INDICATIONS WERE NOTED AT THIS TIME. CAP SEALED TANK FASTENERS IAW B737 AMM 51-31-00-390-805.;[02] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW VAPOR BARRIER ATTACH ANGLE; CHANNEL; STIFENER AND FITTING AT WING SECTION REAR SPART R/H FROM STA RBL 5 TO RBL 65 IAW B737-800 SRM 57-10-10-2R-5 ACCOMPLISHED A OPEN HOLE HFEC INSPECTION OF ALL OPEN HOLES ON THE R/H VAPOR BARRIER REPLACEMENT AREA IAW 737 NDT MAN. PT. 6; 51-00-00 PROC. 16. USING T8257I DUE 03 OCT. 25. NO INDICATIONS WERE NOTED AT THIS TIME. CAP SEALED TANK FASTENERS IAW B737 AMM 51-31-00-390-805.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 33,505 hrs · 16,179 cycles

L/H VAPOR BARRIER ANGLE CRACKED AT APPROX LBL 8.<[01] REMOVED DAMAGE; FORMED PARTS; ALODINED; PRIMED AND INSTALLED REPAIR PARTS AT VAPOR BARRIER ATTACH ANGLE L/H. STA LBL 5 TO LBL20 APROX. IAW B737-800 SRM 57-10-10-5-2R. ACCOMP. HFEC CUT EDGES; IAW B737 NDT MAN. 51-00-00 PROC.23; PT6. NO CRACK INDICATIONS FOUND. CAP SEALED TANK FASTENERS IAW B737 AMM 51-31-00-390-805.;[02] 02 - INSPECTED PER [SRM 57-10-10-2R-5-B01456 (REPAIR 5 - WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR - PERMANENT)]

Part: COVER — MISSING (ZONE 200) · airframe 33,430 hrs · 16,135 cycles

LEFT AFT EMERGENCY EXIT SIDEWALL; EMERGENCY EXIT LIGHT LENS MISSING.(PHOTO ATTACHED.)<[01] INSTALLED REPLACEMENT EMERGENCY EXIT LIGHT LENS COVER PER SIP.

Part: SEAT — LOOSE (ZONE 200) · airframe 33,430 hrs · 16,135 cycles

CABIN SEAT ROW LOOSE IN FLOOR TRACK 12DEF; 2DEF; 3DEF<[01] RE-SECURED PASSENGER SEAT ROWS AT 3DEF; 12DEF; AND 2DEF PER AMM 25-22-00.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 33,383 hrs · 16,109 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] REVAMPED L1 EMERGENCY DOOR LIGHT IAW AMM 33-51-04 OPS CHECK GOOD

Part: HANDLE — UNSECURE (AFT PAX DOOR) · airframe 32,432 hrs · 15,573 cycles

AFT ENTRY DOOR INBOARD DOOR HANDLE CAM HOUSING SAFETY WIRE BROKEN.<[01] RE-SECURED AFT ENTRY DOOR INBOARD DOOR HANDLE CAM HOUSING W SAFETY WIRE REF AMM 52-13-00.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 32,432 hrs · 15,573 cycles

CABIN FLOOR BOARD PANEL BREAK ASSEMBLY AT STA. 540 CRACKED AT INBOARD END L/H OF CENTER IN A/C DISTRIBUTION BAY.<[01] REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.;[02] IS: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.<BR><BR>SHOULD BE: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240 SHEET 3 AND SHEET 11.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 32,432 hrs · 15,573 cycles

CABIN FLOOR BOARD PANEL BREAK ASSEMBLY AT STA. 540 CRACKED AT INBOARD END RIGHT OF CENTER IN A/C DISTRIBUTION BAY.<[01] REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.;[02] IS: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.<BR><BR>SHOULD BE: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240 SHEET 3 AND SHEET 11.

Part: CONNECTOR — DISCONNECTED (SPEED TRNSDCER) · airframe 31,358 hrs · 14,982 cycles

ANTI-SKID INOP LIGHT ILLUMINATED ON TAKEOFF.<[01] FOUND #3 WHEEL SPIN TRANSDUCER CONNECTOR NOT INSTALLED. SECURED PER AMM 20-61-13. OPS CK GOOD PER AMM 32-42-00

Part: SIGN — INOPERATIVE (ZN 200 FUS TOP) · airframe 30,676 hrs · 14,625 cycles

OVERWING EXIT CEILING EMERGENCY EXIT SIGN INOP<[01] REMOVED AND REPLACED OVERWING AISLE CEILING EMERGENCY EXIT SIGN. OPS CHECK GOOD. REF AMM 33-51-03

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 30,394 hrs · 14,473 cycles

AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] RELAMPED AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK NORMAL.

Part: SIGN — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 30,316 hrs · 14,433 cycles

EMERGENCY EXIT SIGN CAME OFF.<[01] RESECURED EXIT ROW SIGN. OPS CHECK GOOD. REF AMM 11-32-01.

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 28,549 hrs · 13,429 cycles

OVERWING EXIT SIGN LENS MISSING<[01] INSTALLED EMERGENCY EXIT SIGN LENS AS PER REF AMM 33-51-01

Part: SEAT BACK — OUT OF POSITION (ZN 200 FUS TOP) · airframe 28,532 hrs · 13,421 cycles

14D SEAT RECLINES INTO EXIT ROW<[01] SECURED SEAT RECLINE AT 14D PER CMM 25-22-46

Part: SLIDE — OUT OF LIMITS (ZN 800 DOOR) · airframe 27,739 hrs · 12,983 cycles

AFT ENTRY DOOR SLIDE PRESSURE IN RED<[01] REMOVED AND INSTALLED SLIDE PER AMM 25-66-01

Part: SIGN — CRACKED (ZN 200 FUS TOP) · airframe 26,727 hrs · 12,442 cycles

EMERGENCY 'EXIT' LIGHT; R/H LOWER SIDE FWD GALLEY LENS IS CRACKED. / [01] REMOVED AND REPLACED EXIT SIGN - LIGHT ASSEMBLY ON R/H LOWER FWD GALLEY PER AMM 33-51-01. EXIT SIGN OPS CHECKED GOOD PER AMM 33-51-00.;[02] VERIFIED DANIEL LEBLANC (TECHNICIAN); 03-NOV-2022 02:34 UTC<BR>REMOVED AND REPLACED EXIT SIGN - LIGHT ASSEMBLY ON R/H LOWER FWD GALLEY PER AMM 33-51-01. EXIT SIGN OPS CHECKED GOOD PER AMM 33-51-00.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

FWD CARGO COMPARTMENT LH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 490 TO 500 (MARKED) (REF. TTG8Q00FFPCA) / [01] DUE TO OTHER DAMAGE THAT IS OUT OF LIMITS PER SRM 53-00-53-1A-2; THIS SECTION OF TRANSITION ANGLE FROM STA 480+10' TO STA 500I WILL BE REMOVED AND REPLACED REF FAULT #S TTG8Q00FH1JY AND TTG8Q00FH8OJ.;[02] DUE TO OTHER DAMAGE THAT IS OUT OF LIMITS PER SRM 53-00-53-1A-2; THIS SECTION OF TRANSITION ANGLE FROM STA 480+10' TO STA 500I WILL BE REMOVED AND REPLACED REF FAULT #S TTG8Q00FH1JY AND TTG8Q00FH8OJ.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500E-500F REFERENCE [TTG8Q00FFPBL] / [01] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT OF LIMITS DAMAGE AT OTHER LOCATIONS.;[02] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500G-500H REFERENCE [TTG8Q00FFPBL] / [01] SECTION OF TRANSITION ANGLE UP TO STATION 500G+9 WILL BE REPLACED AS NOTED ON CARD TTG8Q00FGJJX DUE TO OUT OF LIMITS DAMAGE AT OTHER LOCATIONS. REMOVED DAMAGE AT STATIONS 500G+11 AND 500G+19 PER SRM 51-10-02. REMOVED .001 INCH OF MATERIAL AT THOSE LOCATIONS. REMAINING MATERIAL THICKNESS IS .039 INCH AND IS WITHIN LIMITS PER SRM 53-00-53-1A-2. OKAY TO TREAT AND PRIME.;[02] INSPECTED AS REQUIRED. OK TO TREAT AND PRIME STA. 500G+11' AND STA. 500G+19. VERIFIED SECTION OF TRANSITION ANGLE UP TO STATION 500G+9 WILL BE REPLACED AS NOTED ON CARD TTG8Q00FGJJX DUE TO OUT OF LIMITS DAMAGE AT OTHER LOCATIONS.;[03] TREATED AND RESTORED PRIMER AT STATIONS 500G+11 AND 500G+19 PER SRM 51-20-01.;[04] TREATED AND RESTORED PRIMER AT STATIONS 500G+11 AND 500G+19 PER SRM 51-20-01. SEE ADDITIONAL SIGNOFFS. C/W INSPECTION;[05] TREATED AND RESTORED PRIMER AT STATIONS 500G+11 AND 500G+19 PER SRM 51-20-01. SEE ADDITIONAL SIGNOFFS. C/W INSPECTION

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500C-500D REFERENCE [TTG8Q00FFPBL] / [01] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.;[02] INSPECTED AS REQUIRED. THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500B-500C REFERENCE [TTG8Q00FFPBL] / [01] REMOVED DAMAGE PER SRM 51-10-02. REMOVED .001 INCH OF MATERIAL AT STATIONS 500B+2 AND 500B+7. REMAINING MATERIAL AT THOSE LOCATIONS IS .039 INCH AND IS WITHIN LIMITS PER SRM 53-00-53-1A-2. OKAY TO TREAT AND PRIME REWORKED AREAS AT THE TWO GIVEN LOCATIONS.;[02] REMOVED DAMAGE PER SRM 51-10-02 AT STATION 500B+15. REMOVED .013 INCH OF MATERIAL. REMAINING THICKNESS AT THIS LOCATION IS .027 INCH AND IS OUT OF LIMITS PER SRM 53-00-53-1A-2. REPLACE DAMAGED SECTION OF TRANSITION ANGLE AS NOTED IN STEP 1.;[10] CHANGED REPAIR TYPE FROM MINOR TO MAJOR AS PER INSTRUCTIONS IN EA M-22-153-01550.;[11] INSTALLED NEW R/H TRANSITION ANGLE FROM STATION 500B+10 TO 500G+9. ALL WORK REFERENCE TO SRM 53-00-53-2R-5; AND EA M-22-153-01550.;[12] 11. CAO TRAN (TECHNICIAN); 29-OCT-2022 03:14 UTC<BR>INSTALLED NEW R/H TRANSITION ANGLE FROM STATION 500B+10 TO 500G+9. ALL WORK REFERENCE TO SRM 53-00-53-2R-5; AND EA M-22-153-01550.<BR>C/W RII INSPECTION.;[13] C.W. ALL TASKS.

Part: DOME NUT — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

DOME NUT HAS CORROSION INSIDE OF HOLE AT AFT WET AREA STA. 986.5 RBL 43. / [01] REMOVED DOME NUT AT RBL 43 TO FOM PER SRM 51-40-02. ATTEMPTED TO REMOVE CORROSION FROM HOLE PER SRM 51-10-02. CORROSION IS STILL PRESENT IN HOLE. CONTACTED ENGINEERING FOR FURTHER INSTRUCTION.;[02] REAMED HOLE UP TO .360IN TO REMOVE CORROSION PER SRM 51-10-02. ALTHOUGH REMAINING CORROSION ON UNDER SIDE REMOVAL IS OUT OF LIMITS. THIS DAMAGE WILL CUT OUT AND REPAIRED PER SRM 53-70-51-2R-6 ALTERNATIVE 4.;[03] CUT OUT DAMAGE IAW SRM 53-70-51-2R-6; ALTERNATIVE 4.;[04] ACCOMPLISHED A HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION ALONG THE CUT EDGES TO MAKE SURE THERE ARE NO CRACKS. REFER TO 737 NDT PART 6; 51-00-00; PROCEDURE 4 OR 737 NDT PART 6; 51-00-00; PROCEDURE 23. (NO DEFECTS NOTED)<BR><BR>ACCOMPLISHED AN OPEN HOLE AND COUNTERSUNK HFEC INSPECTION OF (1) INITIAL FASTENER HOLE IN THE REPAIR AREA. REFER TO 737 NDT PART 6; 51-00-00; PROCEDURE 16 AND 737 NDT PART 6 53-00-00 PROCEDURE 3. NO DEFECTS NOTED<BR><BR>ACCOMPLISHED A DETAILED INSPECTION OF THE ADJACENT STRUCTURE IN THE REPAIR AREA. NO DEFECT NOTED;[05] FABRICATED REPAIR PARTS IAW SRM 53-70-51-2R-6; ALTERNATIVE 4. OK TO INSTALL.[07] REPAIRED PER SRM 53-70-51-2R-6; ALTERNATIVE 4 .;[08] C/W INSPECTION.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500F-500G REFERENCE [TTG8Q00FFPBL] / [01] REMOVED DAMAGE AT STATION 500F+11. REMOVED .023 INCH OR MATERIAL. REMAINING MATERIAL THICKNESS IS .017 INCH AND IS OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX.;[02] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

AFT WET AREA INTERCOSTAL LOCATED BETWEEN STA 947.5-967; RBL 50 HAS CORROSION ON UPPER SURFACE AT LAV MOUNT BASE. / [01] BLENDED CORROSION ON MACHINED INTERCOSTAL P/N 147A5660-22 PER SRM 51-10-02. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL THICKNESS = .200?; REMAINING THICKNESS = .174?.;[02] VERIFIED CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] REMOVED AND REPLACED INTERCOSTAL BETWEEN STA. 947.5 TO STA. 967 AT RBL 50 PER SRM 51-40-02.;[04] VERIFIED INTERCOSTAL BETWEEN STA. 947.5 TO STA. 967 AT RBL 50 WAS REMOVED AND REPLACED.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

AFT CARGO PIT R/H TRANSITION ANGLE HAS NUMEROUS AREAS OF CORROSION FROM STA 727H+12 TO 767 / [01] REMOVED CORROSION PER SRM. 51-10-02 MATERIAL FOUNDED OUT OF LIMITS PER SRM. 53-00-53-1A-02 ;;[02] REMOVE EXITING TRANSITION ANGLE FROM STA.727 H +10 TO STA. 767 LOCATED AND DRILLED TRANSITION ANGLE PART # BAC1496-377 ; PER SRM. 53-00-53-2R-5 TREATED AND PRIMED REPAIR PART PER SRM 51-20-02 ;INSTALLED BONDING NUT PLACES PER SRM 51-40-10;[03] C/W INSPECTION.;[04] INSTALLED NEW SECTION TRANSITION ANGLE FROM STA.727 H +10 TO STA. 767 PER SRM 53-00-53-2R 5;[05] C/W INSPECTION.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500D-500E REFERENCE [TTG8Q00FFPBL] / [01] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT OF LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.;[02] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

AFT LAV. LH; AFT RH MOUNT (INBD); MOUNT HAS CORROSION. AROUND BASE. / [01] BLENDED CORROSION ON MACHINED INTERCOSTAL P/N 147A5660-3 PER SRM 51-10-02. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL THICKNESS = .200?; REMAINING THICKNESS = .175?.;[02] VERIFIED CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] INTERCOSTAL REPLACED ON FAULT TTG8Q00FFYWH.;[04] CORRECTION FOR CA #3 - REPLACED INTERCOSTAL P/N 147A5660-3 UNDER L/H AFT LAV; INBD MOUNT PER SRM 51-40-02.;[05] VERIFIED C/A # 4 : BRIAN PENCE (TECHNICIAN); 25-OCT-2022 21:22 UTC<BR>CORRECTION FOR CA #3 - REPLACED INTERCOSTAL P/N 147A5660-3 UNDER L/H AFT LAV; INBD MOUNT PER SRM 51-40-02.

Part: BEAM — CORRODED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

AFT WET AREA; RH LAV. AFT MOUNT OUTBD; HAS CORROSION AROUND BASE. / [01] BLENDED CORRODED AREA PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL PART THICKNESS = .180?; REMAINING THICKNESS AFTER BLEND OUT = .089?. CORRODED PART #147A5504-8.05] FLAP PEEN THE CUT EDGE OF THE STA-947 FLOOR BEAM FROM APPROXIMATELY RBL 9' TO RBL 59' PER SRM 53-70-51-2R-5;[06] VERIFIED FLAP PEEN ALONG CUT EDGE OF STA.947 FLOOR BEAM REPAIR;[07] OBTAINED PREFABRICATED T-CHORD FROM STORES MPN 53700002-001. LOCATED AND PILOTED VERTICAL FLANGE OF -1 REPLACEMENT T-CHORD PER SRM 53-70-51-2R-5; ALTERNATIVE 2. LOCATED AND PILOTED -2 REPAIR SPLICE ANGLES PER SRM 53-70-51-2R-5; ALTERNATIVE 2 AND EA 22-153-03130-WIP1 (TTG8Q00FKR7P).;[08] ACCOMPLISHED FLAP PEEN OF CUT EDGE OF PART [1] T-CHORD IAW SRM 53-70-51-2R-5 AND SOPM 20-10-03.;[09] INSPECTED FLAP PEEN OF CUT EDGE OF PART [1] T-CHORD;[10] FABRICATED REPAIR PARTS PER SRM 53-70-51-2R-5.14] TREATED AND PRIMED REPAIR PARTS PER SRM 53-70-51-2R-5. OK TO INSTALL REPAIR PARTS.;[[16] INSTALLED REPAIR PARTS PER SRM 53-70-51-2R-5; ALTERNATIVE 2.;[18] REPAIR ACCOMPLISHED IAW SRM 53-70-51-2R-5; ALTERNATIVE 2 AND EA 22-153-03130.;

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 26,727 hrs · 12,442 cycles

R/H HORIZONTAL STAB. AFT UPPER SLIDING SEAL FWD TRACK CRACKED / [01] R&R'D TRACK PER SOPM 20-50-01;[02] VERIFIED C/A #1.

Part: FLOOR PANEL — WARPED (ZN 100 FUS LOWER) · airframe 26,727 hrs · 12,442 cycles

AFT CARGO FLOOR PANEL 140BF HAS MULTIPLE DENTS AND WAVINESS BETWEEN FLOOR SUPPORTS. / [01] FABRICATED FLOOR PANEL AFT. CARGO #140BF PER BOEING DRAWING #453A2610;[02] C/W INSPECTION.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 26,727 hrs · 12,442 cycles

WITH THE EMERGENCY LIGHTS IN TEST MODE; NONE OF THE EMERGENCY LIGHTING IN THE FWD GALLEY AREA OPERATE. / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT STA 310;317L;500CL;500CR;565L;565R;727R AND STA 952R PER MM 33-51-06;[02] VERIFIED 1. CHRISTOPHER KENNEDY (TECHNICIAN); 22-OCT-2022 15:31 UTC <BR>REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT STA 310;317L;500CL;500CR;565L;565R;727R AND STA 952R PER MM 33-51-06;[03] OPS CHECKS GOOD PER AMM 33-51-00.;[04] INSPECTED AS REQUIRED. CORRECTIVE ACTION #3

Part: NONE — OUT OF POSITION (PAX CABIN) · airframe 26,359 hrs · 12,230 cycles

CEILING EXIT SIGN AT EMERGENCY EXIT ROW MISSING FORWARD COVER / [01] INSTALLED NEW COVER ON THE EMERGENCY EXIT SIGN IN THE CEILING. NO OTHER DEFECTS NOTED AT THIS TIME. REF AMM 33-51-00

Part: LIGHT — OUT OF POSITION · airframe 25,558 hrs · 11,756 cycles

OVERHEAD EXIT SALIDAS CEILING SIGN BY OVER WING EXIT CAME OFF / [01] SECURED OVERHEAD EMERGENCY EXIT SIGN COVER IAW AMM 33-51-01

Part: COVER — OUT OF POSITION (OVERWING EXIT) · airframe 25,385 hrs · 11,660 cycles

AIRCRAFT FORWARD OVERWING EXIT SIGN ON CABIN CEILING HAS COME OFF / [01] RESECURED OVERWING EXIT LIGHT COVER IAW M/M 33-51-01

Part: LENS — MISSING (MID CABIN) · airframe 25,302 hrs · 11,610 cycles

MID CABIN OVERHEAD EMERGENCY EXIT PLASTIC LENS MISSING [FACING FORWARD] / [01] SNAPPED EMERGENCY EXIT LENS BACK ON PER AMM 33-51-01

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 24,615 hrs · 11,230 cycles

R2 SLIDE BECAME DISLODGED / [01] REPACKED R2 SLIDE PER MT 725-61-06.

Part: LENS — MISSING (CABIN) · airframe 23,975 hrs · 10,882 cycles

AISLE OVER WING EXIT SIGN MISSING LENS ; / [01] INSTALLED AISLE OVER-WING EXIT SIGN LENS REF AMM 33-51-01

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 23,780 hrs · 10,770 cycles

EMERGENCY EXIT SIGN AFT OF LEFT OVERWING EXIT DOOR AND EMERGENCY LIGHTS AT 16ABC TO 23ABC INOP ; / [01] REMOVED & REPLACED BATTERY PACK CHARGER (M1670) IAW AMM 33-51-06. NO HELP; REQUIRES BATTERY PACK; PLACED BATTERY PACK ON ORDER.; [02] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06

Part: FLOOR SUPPORT — BENT (AFT CARGO) · airframe 20,423 hrs · 9,025 cycles

AFT CARGO FLOOR FWD BULKHEAD FLOOR ANGLE BENT / REMOVED AND REPLACED PER SRM 51-40-02.

Part: CARGO TRACK — CORRODED (BS 867) · airframe 20,423 hrs · 9,025 cycles

AFT CARGO RAIL ASSEMBLY HAS CORROSION AT BS 867 +12 RBL 8 / ACCOMPLISHED SRM 53-00-53-2R-3 REPAIR ALT 1 STA 867 + 7 - 887 (S/N A1314370)

Part: ANGLE — CORRODED (BS 500A-500I) · airframe 20,423 hrs · 9,025 cycles

FWD CARGO; R/H TRANSITION ANGLE HAS CORROSION AROUND SEVERAL NUTPLATE HOLES STA 500A TO 500I / REPAIRED PER SRM 53-00-53-2R-5 AND EA 20-153-02159 (PN # 146A7502-340) (SA-M 326 ATTACHED: A1314343)

Part: ANGLE — CORRODED (BS 500-500C) · airframe 20,423 hrs · 9,025 cycles

FWD CARGO; L/H TRANSITION ANGLE HAS CORROSION AROUND SEVERAL NUTPLATE HOLES STA 500 TO 500C / REMOVED + REPLACED TRANSITION ANGLE. REF. SRM. 53-00-53-2R-5; AND E.A. 20-153-02159.

Part: ANGLE — CORRODED (BS 500I) · airframe 20,423 hrs · 9,025 cycles

FWD CARGO; AFT BULKHEAD LOWER ANGLE HAS SEVERAL AREAS OF CORROSION STA 500I RBL24 TO LBL24 / REMOVED AND REPLACED FWD CARGO AFT BULKHEAD LOWER ANGLE AT ATA. 500I PER SRM 51-40-02. P/N 143A9485-35 (SA-M 326 ATTACHED: A1314355)

Part: ANGLE — CORRODED (BS 787) · airframe 20,423 hrs · 9,025 cycles

CORROSION ON NUTPLATE STRIP B5 787+3 + B5787+5 UNDERSIDE OF R/H TRANSITION ANGLE / REMOVED AND REPLACED PER SRM 51-40-02 ( PN # 146A8128-G)

Part: ANGLE — CORRODED (BS 500C-500I) · airframe 20,423 hrs · 9,025 cycles

FWD CARGO; L/H TRANSITION ANGLE HAS CORROSION AROUND SEVERAL NUTPLATE HOLES STA 500C TO 500I / REMOVED + REPLACED TRANSITION ANGLE. REF. SRM. 53-00-53-2R-5; E.A. 20-153-02159.P/N 146A7502-33

Part: ANGLE — CORRODED (BS 767-787) · airframe 20,423 hrs · 9,025 cycles

AFT CARGO ANGLE BELOW + ATTACH TO R/H TRANSITION ANGLE HAS CORROSION AROUND SEVERAL NUTPLATES (MARKED) B5767-B5787 / REMOVED AND REPLACED PER SRM 51-40-02

Part: ANGLE — CORRODED (BS 727H-727I) · airframe 20,423 hrs · 9,025 cycles

AFT CARGO R/H TRANSITION ANGLE HAS MULTIPLE AREAS OF CORROSION B5 727H- 727I / REMOVED AND REPLACED R/H TRANSITION FROM BS 727H+10 THRU 767 PER SRM 53-00-53-2R-5 (S/N A1314364)

Part: ANGLE — CORRODED (BS 767-787) · airframe 20,423 hrs · 9,025 cycles

AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT MULTIPLE AREAS BOTH UPPER + LOWER SURFACE B5 767- B5 787 / REMOVED AND REPLACED PER SRM 51-40-02

Part: ANGLE — CORRODED (BS 727I-767) · airframe 20,423 hrs · 9,025 cycles

AFT CARGO R/H TRANSITION ANGLE HAS LARGE AREAS OF CORROSION BOTH UPPER + LOWER SURFACE B5 727I-767 / R/H TRANSITION ANGLE WAS REPLACED FROM 727H +10 THRU BS 767 ON NR# D469439

Part: SUPPORT — CORRODED (BS 767) · airframe 20,423 hrs · 9,025 cycles

AFT CARGO FLOOR PANEL SUPPORT STRIP AT B5 767+5 HAS CORROSION AT MULTIPLE SCREW HOLES / REMOVED AND REPLACED WITH NEW FLOOR STRIP PER SRM 51-40-02 (PN # 146A9401-4)

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 20,423 hrs · 9,025 cycles

FWD CARGO FLOOR PNL 121ZBC IS DAMAGED. / REMOVED AND REPLACED FLOOR PANEL PER AMM 25-52-10.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · airframe 20,423 hrs · 9,025 cycles

PANEL 532 EB HAS EVIDENCE OF CORROSION / REPLACED PANEL WITH SERVICABLE PANEL T0 BE INSTALLED ON W/O 698428

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · airframe 20,423 hrs · 9,025 cycles

PANEL 532 GB HAS EVIDENCE OF CORROSION / REPLACED PANEL WITH SERVICEABLE PANEL TO BE INSTALLED ON W/O 698428

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 20,423 hrs · 9,025 cycles

ON THE RIGHT WING; JUST INBD OF THE DELECTION RIB. THE ATTACH ANGLE IS CRACKED. (OTBD END OF LOWER BULB SEAL.) / REMOVED AND DAMAGED ANGLE PER SRM 51-40-02; 104029. INSTALLED NEW ATTACH ANGLE PER SRM 51-40-02.

Part: STRAKE — DAMAGED (RT WINGLET) · airframe 20,423 hrs · 9,025 cycles

FOUND DAMAGE ON RH WINGLET LOWER STRAKE TRAILING EDGE. / R+R R/H WINGLET STRAKE PER A.I.P FINALL INSTALL WILL BE ACCOMPLISHED ON TASK CARD 757-31-02POS P/H P/N OFF/ON 737-2510-4 S/N OFF 12225406/001 S/N ON 1254031/001

Part: RADOME — DAMAGED (NOSE) · airframe 19,577 hrs · 8,606 cycles

RADOME HAS MANY LARGE HOLES IN BOOT / REPLACED RADOME ROFM/M 53-52-00POS ONLY TAG 97797 P/N OFF/ON 1001002-7B S/N OFF NRD-0268 S/N ON C205766-02

Part: SIGN — OUT OF POSITION (EMERGENCY LIGHT) · airframe 17,298 hrs · 7,584 cycles

CEILING MOUNTED EXIT SIGN AT THE OVERWING EXIT OUT OF POSITION. / REPOSITIONED EXIT SIGN PER SIP.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 15,774 hrs · 6,883 cycles

PANEL 193AL HAS DELAMINATION ON LEADING EDGE 7' FROM TOP OF PANEL 13' LONG 3/4' WIDE 5 PLYS DEEP.ACCOMPLISHED EA TASKS AS REQUIRED PER REPAIR-53EA-06466; SEE ALSO SA-M 943T V009237 FOR FURTHER ACTION.PERMANENT ACTION REQUIRED:PERFORM A PERMANENT REPAIR PER SRM 51-70-04; OTHER APPLICABLE PERMANENT REPAIR; OR REMOVE AND REPLACE THE P/N 149A7655-21 PANEL. / ACCOMPLISHED PERMANENT REPAIR PER 51-70-05.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 15,019 hrs · 6,550 cycles

PANEL 193AL HAS DELAMINATION ON LEADING EDGE 7' FROM TOP OF PANEL 13' LONG 3/4' WIDE 5 PLYS DEEP. / ACCOMPLISHED EA TASKS AS REQUIRED PER REPAIR-53EA-06466; SEE ALSO SA-M 943T V009237 FOR FURTHER ACTION.PERMANENT ACTION REQUIRED:PERFORM A PERMANENT REPAIR PER SRM 51-70-04; OTHER APPLICABLE PERMANENT REPAIR; OR REMOVE AND REPLACE THE P/N 149A7655-21 PANEL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 12,571 hrs · 5,498 cycles

FORWARD AFT EMERGENCY FLASHLIGHT BATTERIES DIM. R&R BATTERIES AMM.

Part: HOLDER — LACK OF LUBE (R2 DOOR) · airframe 12,947 hrs · 5,644 cycles

R2 DOOR GIRT BAR HOLDERS WAS STIFF AND DIFFICULT TO OPERATE. LUBED GIRT BAR HOLDER PER SIP.

Part: RETAINER — CRACKED (NLG WHEEL WELL) · airframe 12,468 hrs · 5,456 cycles

NLG WHEEL WELL FWD R/H CORNER SEAL RETAINER CRACKED. (P/N 141A6910-20) / VERIFIED; LOCATED AND DRILLED NEW P/N:141A6910U20 IAW B737-800 SRM 51-40-05-0G-0 DWG:141A7500 REV: F TAG A67793

Part: RETAINER — CRACKED (NLG WHEEL WELL) · airframe 12,468 hrs · 5,456 cycles

NLG WHEEL WELL R/H SEAL RETAINER CRACKED. (P/N 141A7514-6) / REMOVED AND REPLACED NLG W/W R/H SEAL RETAINER I/A/W SRM 51-40-02 AND BOEING DWG 141A0611

Part: STRINGER — CRACKED (FUSELAGE) · airframe 12,467 hrs · 5,455 cycles

SUPPLEMENTAL INFORMATION: STRINGER 24L BETWEEN STA 277 AND 285 IS CRACKED AND BENT / COMPLIED WITH INTERIM REPAIR PER EA# REPAIR-53EA-05164. PERMANENT REPAIRS REQUIRED WITHIN ONE FLIGHT CYCLE NON REVENUE PER EA# REPAIR-53EA-05164 REFERENCE MX NOTE ON LOG PAGE # 0704209

Part: STRINGER — CRACKED (BS 277-285) · airframe 12,467 hrs · 5,455 cycles

STRINGER 24L CRACKED BETWEEN BS 277 TO 285. REPAIRED THE STRINGER IAW EA.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 12,467 hrs · 5,455 cycles

STRINGER CLIP CRACKED AT BS 277, STRINGER 26L. REPAIRED THE STRINGER CLIP EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 12,467 hrs · 5,455 cycles

STRINGER CRACKED BETWEEN BS 277 TO BS 285, STR 25L. REPAIRED STRINGER IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 12,467 hrs · 5,455 cycles

SUPPLEMENTAL INFORMATION: STRINGER 25L BETWEEN BS 277 AND 285 IS CRACKED AND BENT / COMPLIED WITH INTERIM REPAIR PER EA# REPAIR-53EA-05164. PERMANENT REPAIRS REQUIRED WITHIN ONE FLIGHT CYCLE NON REVENUE PER EA# REPAIR-53EA-05164 REFERENCE MX NOTE ON LOG PAGE # 0704209

Part: STRINGER CLIP — CRACKED (MAIN CABIN) · airframe 12,467 hrs · 5,455 cycles

SUPPLEMENTAL INFORMATION: STRINGER CLIP AT STA 277; STR 26L IS CRACKED/ DAMAGED/ BUCKLED / COMPLIED WITH INTERIM REPAIR PER EA# REPAIR-53EA-05164 PERMANENT REPAIRS REQUIRED WIHTIN ONE NON-REVENUE FLIGHT CYCLE PER EA# REPAIR-53EA-05164 REFERENCE MX NOTE ON LOG PAGE 0704209

Part: NONE — CRACKED (LT HORIZ STAB) · airframe 10,073 hrs · 4,394 cycles

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

Part: BRACKET — LOOSE (GIRT BAR) · airframe 9,515 hrs · 4,158 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED GIRT BAR PER AMM.

Part: LENS — MISSING (CABIN) · airframe 4,292 hrs · 1,895 cycles

OVERHEAD OVERWING EMER LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 3,021 hrs · 1,309 cycles

R1 DOOR EGRESS LIGHT LENS BROKEN. R & R LENS IAW SIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 2,080 hrs · 919 cycles

R1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 2,080 hrs · 919 cycles

R1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 2,024 hrs · 894 cycles

LEFT AFT EMER EXIT LIGHT LENS FELL OFF. REINSTALLED LENS IAW SIP.

Part: LENS — MISSING (CABIN) · airframe 1,937 hrs · 858 cycles

LEFT EMER EXIT COVER LENS MISSING AT ROW 16. INSTALLED LENS IAW SIP.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 1,743 hrs · 772 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM & MT.

Part: SIGN — LOOSE (CABIN) · airframe 763 hrs · 345 cycles

RIGHT EMER EXIT SIGN LOOSE AT ROW 13. SECURED SIGN IAW SIP.