N8691A

Part: LENS — DETACHED (ZONE 200) · airframe 31,548 hrs · 15,746 cycles

EMER EXIT SIGN ROW 15 CENTER AISLE FELL OFF. SECURED OVERHEAD EMERGENCY EXIT LENS COVER PER AMM SIP.

Part: CONDENSER — POPPED (ZONE 100) · airframe 31,239 hrs · 15,592 cycles

APPROX 1000 AGL HEARD LOUD POPPING SOUND. LOUD AIR RUSHING SOUND THAT MADE IT DIFFICULT TO HEAR IN COCKPIT. FAS HEARD SAME LOUD NOISE AND RUSHING AIR NOISE. MIXED WATER AND ICE CRYSTALS AND UNCOMMANDED TEMP CHANGES. NO PRESS CHANGES AND DUCT PRESSURE REMAINED STEADY AT 35PSI. R & R THE LT PACK TEMP BULB IAW AMM 21-51-60. R & R LT TEMP CONTROL VALVE IAW AMM 21-51-10. FINISHED INSTALL OF CONDENSER AND RE HEATER REF AMM 21-51-12 AND AMM 21-51-13. INSTALLED/REPLACED BOTH WATER EXTRACTORS AND ASSOCIATED LINES AND DUCTING REF AMM 12-51-14. OPS CHECKS GOOD/NO ICE FORMATION.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 29,720 hrs · 14,814 cycles

AFT FA JUMPSEAT CAPTS SIDE 1 FLASHLIGHT INOP.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 29,657 hrs · 14,779 cycles

LIGHT ABOVE AFT RIGHT OVERWING EMERGENCY EXIT IS FLASHING ON AND OFF.<[01] EMERGENCY LIGHTS UNAFFECTED BY LIGHT STRIP PER AMM 33-51-00. OK TO CONTINUE PER MEL 33-2-04; SP-1B; AUTH: 260977;[02] OPERATIONAL CHECK OF AFT RH OVERWING EXIT LIGHT GOOD PER AMM 33-20-00. MEL CLEARED.

Part: LENS — BROKEN (ZONE 200) · airframe 29,396 hrs · 14,640 cycles

AFT OVERHEAD COVE PANEL EMERGENCY EXIT LIGHT LENSE IS BROKEN<[01] REMOVED AND INSTALLED NEW AFT OVERHEAD COVE PANEL EMERGENCY EXIT LIGHT ASSEMBLY PER AMM 33-51-03. OPS CHECK GOOD.;[02] INSPECTED AS REQUIRED; CORRECTIVE ACTION #1

Part: SLIDE — LOOSE (ZONE 800) · airframe 29,396 hrs · 14,640 cycles

FWD ENTRY DOOR SLIDE FWD ATTACH SCREW LOOSE.<[01] SECURED SCREW PER SOPM 20-50-01;[02] C/W INSPECTION

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 29,396 hrs · 14,640 cycles

CABIN FLOOR INTERCOSTAL STA-540 BL-0 TO RBL-24 CRACKED AT RBL-1 (MARKED)<[01] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.;[02] INSPECTION COMPLETED FOR WORK ACCOMPLISHED; REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.;[03] INSPECTION COMPLETED FOR WORK ACCOMPLISHED; REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 29,396 hrs · 14,640 cycles

BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT APPROXIMATELY RBL 9.<[01] REMOVED FASTENERS IN FUEL TANK ONLY OF 663 VAPOR BARRIER ANGLE ON R/H SIDE PER SRM 51-40-02;[02] CUT AND REMOVED VAPOR BARRIER ATTACH ANGLE ON STA. 663 FROM APPROXIMATELY RBL 6? TO RBL 17? PER SRM 57-10-10-2R-5.;[03] VERIFIED WORK SIGNED IN CA#1 AND #2 ....... RII;[04] C/W HFEC OF OPEN HOLES IN REPAIR AREA FOR SRM 57-10-10-2R-5 PER NDT PART 6 51-00-00 PROD. 16 ---- NO DEFECTS NOTED;[05] C/W DVI OF REPAIR AREA FOR REPAIR SRM 57-10-10-2R-5 ---- NO DEFECTS NOTED;[06] TRIMMED AND LOCATED REPLACEMENT ANGLE FOR 663 VAPOR BARRIER<BR>RH SIDE PER SRM 57-10-10-2R-5. PART NUMBER 111A1322U10;[07] VERIFIED WORK SIGNED IN CA#6 RII..........TRIMMED AND LOCATED REPLACEMENT ANGLE FOR 663 VAPOR BARRIER<BR>RH SIDE PER SRM 57-10-10-2R-5. PART NUMBER 111A1322U10;[08] RII - FORMED SPLICE ANGLE FROM 0.071 IN. 2024-T3 CLAD PER SRM 57-10-10-2R-5.[17] CAP SEALED REPAIR FASTENERS IN FUEL TANK PER SRM 51-10-10-2R-5.;[18] REPAIRED BS 663 VAPOR BARRIER ATTACH ANGLE BETWEEN RBL 6 AND RBL 17 PER SRM 57-10-10-2R-5;[19] VERIFIED CORRECTIVE ACTION STEPS 17 AND 18;[20] VERIFIED REPAIR IS COMPLETE PER SRM 57-10-10-2R-5 AND LEAK CHECKED GOOD.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 29,396 hrs · 14,640 cycles

BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT APPROXIMATELY LBL 9.<[01] REMOVED FASTENERS IN FUEL TANK ONLY OF VAPOR BARRIER ANGLE ON L/H SIDE PER SRM 51-40-02;[02] CUT AND REMOVED VAPOR BARRIER ATTACH ANGLE ON STA. 663 FROM APPROXIMATELY LBL 6? TO LBL 17? PER SRM 57-10-10-2R-5.;[03] VERIFIED WORK SIGNED IN CA#1 AND #2 ....... RII;[04] C/W HFEC OF OPEN HOLES IN REPAIR AREA FOR SRM 57-10-10-2R-5 PER NDT PART 6 51-00-00 PROD. 16 ---- NO DEFECTS NOTED;[05] C/W DVI OF REPAIR AREA FOR REPAIR SRM 57-10-10-2R-5 ---- NO DEFECTS NOTED;[06] TRIMMED AND LOCATED REPLACEMENT ANGLE FOR 663 VAPOR BARRIER<BR>L/H SIDE PER SRM 57-10-10-2R-5. PART NUMBER 111A1322U9;[07] VERIFIED WORK SIGNED IN CA# 6 RII...........TRIMMED AND LOCATED REPLACEMENT ANGLE FOR 663 VAPOR BARRIER<BR>L/H SIDE PER SRM 57-10-10-2R-5. PART NUMBER 111A1322U9;[08] RII - FORMED SPLICE ANGLE FROM 0.071 IN. 2024-T3 CLAD PER SRM 57-10-10-2R-5.;[09] VERIFIED WORK SIGNED IN CA#8 RII...........FORMED SPLICE ANGLE FROM 0.071 IN. 2024-T3 CLAD PER SRM 57-10-10-2R-5.;24] L/H 663 VAPOR BARRIER ATTACH ANGLE WAS REPAIRED PER SRM 57-10-10-2R-5 AND EA M-24-157-0234.; REF CORRECTIVE ACTIONS 1 THRU 23.;[25] LINE 24 <BR>INSPECTED AS REQUIRED

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 29,038 hrs · 14,459 cycles

FWD MEGAPHONE INOP <[01] R&R FWD MEGAPHONE IAW AMM 25-64-00.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 27,196 hrs · 13,479 cycles

2 AFT GALLEY FLASHLIGHTS INOP<[01] REMOVED AND REPLACED FLASHLIGHTS PER 25-64-00 AMM AND CMM 25-60-02. NOTE: NEW EXPIRATION DATE IS 08-2029.

Part: OVERHEAT LOOP — FAULTY (ZONE 100) · airframe 27,196 hrs · 13,479 cycles

WING BODY OVERHEAT LEFT SIDE; EXTINGUISHED 7 OR 8 MINUTES AFTER COMPLETING QRH PROCEDURES<[01] REF FIM 26-18 TASK 801 AND 802. PERFORMED BITE. FAULT 14 DISPLAYED. INSPECTED APPLICABLE DUCTS FOR LEAKS; NONE NOTED. OK TO CONTINUE ON MEL 26-12-01 SP 1 AUTH #209673;[02] FAULT CODE 14 DISPLAYED. FOUND M1761 OVHT DETECTOR BAD REMOVED AND REPLACED PER AMM 26-18-02.

Part: LAMP — MISSING (EMERGENCY LIGHT) · airframe 27,102 hrs · 13,420 cycles

OVERWING EXIT SIGN AT ROW 14 CA SIDE MISSING (AT BOTTOM)<[01] R&R XIT SIGN LAMP PER AMM 33-51-01. OPS CHECK GOOD

Part: MEGAPHONE — MISSING (ZONE 200) · airframe 26,896 hrs · 13,304 cycles

AFT GALLEY BULLHORN MISSING VOLUME KNOB<[01] R AND R AFT MEGAPHONE IAW AMM 25-64-00 OPS CK GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,301 hrs · 12,996 cycles

WHILE PERFORMING EMERGENCY LIGHT TEST IAW SWA AMM 33-51-00-720-801 FOUND AISLE LIGHTS IN AFT CABIN INOP<[01] REMOVED AND REPLACED 2 EA AFT CABIN EMERGENCY BATTERY PACKS (OVER L2 AND R2) AND OPS CHECK GOOD IAW SWA B737-800 AMM 33-51-06-960-805.;[02] REMOVED AND REPLACED 2 EA AFT CABIN EMERGENCY BATTERY PACKS (OVER L2 AND R2) AND OPS CHECK GOOD IAW SWA B737-800 AMM 33-51-06-960-805. COMPLETED CARD OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,301 hrs · 12,996 cycles

WHILE PERFORMING TEST IAW SWA AMM 33-51-00-720-801; FOUND AISLE LIGHTS AT R/H STA 500 TO STA 589 INOP<[01] REMOVED; REPLACED AND PERFORMED A GOOD CHECK OF THE EMERGENCY AISLE LIGHTS AT R/H STA 500 TO STA 589 IAW SWA AMM 33-51-06.;[02] 02 - INSPECTED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 26,301 hrs · 12,996 cycles

EMERGENCY BATTERY PACK AT L/H SEAT 20ABC WILL NOT CHARGE<[01] 01 - REMOVED AND REPLACED PER B737 AMM33-51-960-805. OPS CHECK GOOD IAW B737 AMM 33-51-06-960-805;[02] - REMOVED AND REPLACED PER B737 AMM33-51-06-960-805. OPS CHECK GOOD IAW B737 AMM 33-51-06-960-805. STEP 1. AMM REFERENCE INCORRECT.;[03] VERIFIED REMOVED AND REPLACED PER B737 AMM33-51-06-960-805. OPS CHECK GOOD IAW B737 AMM 33-51-06-960-805. OPS CHECK GOOD.

Part: STRAP — CRACKED (BS 727) · airframe 26,301 hrs · 12,996 cycles

AFT CARGO 727 BHD STRAP 144A2617-5 IS CRACKED<[01] REMOVED AND REPLACED AFT CARGO 727 BHD STRAP 144A2617-5 PER BOEING DWG 144A2600 REV-A AND B737-800 SRM 51-40-02.;[02] VERIFIED REMOVAL AND REPLACEMENT OF R/H STRAP AT STA. 727 BHD144A2617-5 PER BOEING DWG 144A2600 REV-A AND B737-800 SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (ZN 100 FUS LOWER) · airframe 26,301 hrs · 12,996 cycles

FWD PIT R/H SIDE; CLIP CRACKED AT FWD SIDE OF BS 500H APPROX. STRINGER S-26R.<[01] REMOVED AND REPLACED FWD PIT R/H SIDE; CLIP AT FWD SIDE OF BS 500H; S-26R IAW BAC DWG 143A7505 REV. B AND B737-800 SRM 51-40-02. PO# 1087457.1;[02] VERIFIED REMOVAL AND REPLACEMENT OF FORWARD PIT R/H SIDE CLOP AT FORWARD SIDE BS 500H STR. 26L IAW BAC DWG 143A7505 REV. B AND B737-800 SRM 51-40-02. PO# 1087457.1

Part: STIFFENER — CRACKED (AFT) · airframe 26,301 hrs · 12,996 cycles

AFT FLOOR PANEL 140AF STIFFENER PLATE 453A2611-12 CRACKED IN 2 PLACES<[01] REMOVED AND REPLACED AFT FLOOR PANEL 140AF STIFFENER PLATE 453A2611-12; PO #: 1089820.1 PER B737-800 SRM 51-40-02.;[02] VERIFIED REMOVAL AND REPLACEMENT OF AFT FLOOR PANEL 140AF STIFFENER PLATE 453A2611-12; PO #: 1089820.1 PER B737-800 SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (ZN 100 FUS LOWER) · airframe 26,301 hrs · 12,996 cycles

FWD PIT R/H SIDE; CLIP CRACKED AT AFT SIDE OF BS 500H APPROX. STRINGER S-26R.<[01] REMOVED AND REPLACED FWD PIT R/H SIDE; CLIP AT AFT SIDE OF BS 500H; S26R PER BAC DWG 143A7505 REV. B AND B737-800 SRM 51-40-02. PO#: 1087455.1;[02] VERIFIED REMOVAL AND REPLACEMENT OF CRACKED CLIP AT AFT SIDE BS 500H STR. 26 R PER BAC DWG 143A7505 REV. B AND B737-800 SRM 51-40-02. PO#: 1087455.1

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 26,301 hrs · 12,996 cycles

MAIN CABIN CRACK FOUND ON PANEL BREAK UNDER PANEL 231XF DOT L625<[01] REPLACED LH PLATE UNDER FLOOR PANEL 231 UF AND 231XF IAW B37-800 SRM 51-40-02-0G-0 AND BAC DWG 143A5240 REV: - & B.;[02] REPLACED LH PLATE UNDER FLOOR PANEL 231 UF AND 231XF IAW B37-800 SRM 51-40-02-0G-0 AND BAC DWG 143A5240 REV: - & B.

Part: STRINGER CLIP — CRACKED (ZN 100 FUS LOWER) · airframe 26,301 hrs · 12,996 cycles

FWD PIT R/H SIDE; STRINGER CLIP CRACKED AT FWD SIDE OF BS 500I APPROX. STRINGER S-26R.<[01] REMOVED AND REPLACED STRINGER CLIP PN: 143A1010-48 PO# 1090043.1 IAW B737-800 SRM 51-40-02 & BAC DWG# 143A1234 REV. A.;[02] VERIFIED REMOVAL AND REPLACEMENT OF STRINGER CLIP PN: 143A1010-48 PO# 1090043.1 IAW B737-800 SRM 51-40-02 & BAC DWG# 143A1234 REV. A.

Part: RIB — WORN (RT WING) · airframe 26,301 hrs · 12,996 cycles

RIGHT WING TIP AREA; WING RIB 27( AT WBL 658.17) HAS 3 EACH WEAR MARKS AT O/B SURFACE.<

Part: STRAKE — CORRODED (LT WING) · airframe 26,301 hrs · 12,996 cycles

L/H WINGLET AREA; STRAKE HAS CORROSION AT THE TIP AREA.<[01] REMOVED CORROSION FROM AREA IAW B737-800 SRM 57-31-01. ORIGINAL THICKNESS IS .050'. REMOVED .039' OF MATERIAL. REMAINING THICKNESS IS .011'. FOUND TO BE OUT OF LIMITS. TOOL# T8224M CAL DUE: 07/NOV/24. REMOVED STRAKE TIP CAP IAW B737-800 SRM 51-40-02. RECEIVED NEW STRAKE TIP CAP PN: 737-2571-11 BN: 4570052 IAW B737-800 AIPC 57-31-00-02. LOCATED AND DRILLED STRAKE TIP CAP IAW 737-800 SRM 51-40-05. APPLIED TOPCOAT IAW B737-800 MMS 57-21-300-801. INSTALLED NEW L/H WINGLET STRAKE TIP CAP IAW B737-800 SRM 51-40-02 & AIPC 57-31-00-02.;[02] L/H WINGLET AREA; STRAKE HAS CORROSION AT THE TIP AREA.

Part: STRINGER CLIP — CRACKED (ZN 100 FUS LOWER) · airframe 26,301 hrs · 12,996 cycles

FWD PIT L/H SIDE; CLIP CRACKED AT FWD SIDE OF BS 500H APPROX. STRINGER S-26L.<[01] REMOVED AND REPLACED FWD PIT L/H SIDE; CLIP AT FWD SIDE OF BS 500H APPROX. STRINGER S-26L PER BOEING DWG 143A7505 REV-B AND B737-800 SRM 51-40-02.;[02] VERIFIED REMOVAL AND REPLACEMENT OF CLIP FWD SIDE OF BS 500H APPROX. STRINGER S-26L PER BOEING DWG 143A7505 REV-B AND B737-800 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 927-947 LBL52) · airframe 26,301 hrs · 12,996 cycles

AFT CABIN WET AREA INTERCOSTAL STA.927-947 LBL52 HAS CORROSION AT STA.947<[01] REMOVED AND REPLACED INTERCOSTAL PN 147A5690-3 IAW B737-800 SRM 51-40-02 AND BAC DWG 147A5690;[02] VERIFIED REMOVED AND REPLACED INTERCOSTAL PN 147A5690-3 IAW B737-800 SRM 51-40-02 AND BAC DWG 147A5690

Part: SKIN — CORRODED (LT WINGLET) · airframe 26,301 hrs · 12,996 cycles

L/H WINGLET TIP HAS CORROSION AT THE TOP.<[01] REMOVED DAMAGE ON L/H WINGLET TIP IAW B737-800 SRM 57-30-01 REPAIR 6;[02] REMOVED DAMAGE ON L/H WINGLET TIP IAW B737-800 SRM 57-30-01 REPAIR 6

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 26,301 hrs · 12,996 cycles

AFT CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED * PARTS RACK ITEM *<[01] REPAIRED AFT CARGO DOOR AFT CORNER SCUFF PLATE PER B737-800 SRM 53-60-15-2R-1.;[02] VERIFIED REPAIR AFT CARGO DOOR A CORNER SCUFF PLATE PER B737-800 SRM 53-60-15-2R-1.

Part: FLOOR SUPPORT — CORRODED (BS 947 LBL52) · airframe 26,301 hrs · 12,996 cycles

AFT WET AREA INTERCOSTAL AT BS 947 LBL 52 SHOWS SIGNS OF CORROSION DOT L639<[01] REMOVED AND REPLACED INTERCOSTAL PN 147A5660Y2 IAW B737-800 SRM 51-40-02 AND BAC DWG 147A5660;[02] VERIFIED REMOVED AND REPLACED INTERCOSTAL PN 147A5660Y2 IAW B737-800 SRM 51-40-02 AND BAC DWG 147A5660

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 26,301 hrs · 12,996 cycles

R/H HORIZONTAL L/E AREA; UPPER SLIDING SEAL CRACKED AT THE LOWER AFT CORNER.<[01] REPLACED RH UPPER SLIDE SEAL IAND INSTALLED IAW B737-800 AMM 53-31-31-400-802; B737-800 SRM 51-40-02-0G-0.;[02] VERIFIED REMOVAL AND INSTALLATION OF R/H UPPER SLIDE SEAL IAW B737-800 AMM 53-31-31-400-802; B737-800 SRM 51-40-02-0G-0. TOOL NUMBER T8352R CAL DUE DATE 18/JUL/2024

Part: WEB — CORRODED (ZN 200 FUS TOP) · airframe 26,301 hrs · 12,996 cycles

AFT WET AREA AFT OF L2 DOOR AT 986 EVIDENCE OF CORROSION FOUND ON WEB STRUCTURE DOT L632<[01] REMOVED AND REPLACED WEB ASSY PN 147A5712U34 STA.986.5-1016 LBL 27.95-LBL43 IAW B737-800 SRM 51-40-02 AND BAC DWG 147A5700 REV- T05868-187 CAL DUE 16JUL24; T8356U CAL DUE 22MAY24;[02] REMOVED AND REPLACED WEB ASSY PN 147A5712U34 STA.986.5-1016 LBL 27.95-LBL43 IAW B737-800 SRM 51-40-02 AND BAC DWG 147A5700 REV- T05868-187 CAL DUE 16JUL24; T8356U CAL DUE 22MAY24

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 26,301 hrs · 12,996 cycles

L/H HORIZONTAL L/E AREA; UPPER SLIDING SEAL CRACKED AT THE LOWER AFT CORNER.<[01] REMOVED AND REPLACED LH UPPER SLIDE SEAL IAW B737-800 AMM 53-31-31-400-802.;[02] TOOL NUMBER T8352R CAL DUE DATE 18/JUL/2024.;[03] VERIFIED REMOVAL AND INSTALLATION OF L/H UPPER SLIDE SEAL IAW B737-800 AMM 53-31-31-400-802. TOOL NUMBER T8352R CAL DUE DATE 18/JUL/2024.

Part: FLOORBEAM — CORRODED (BS 947 LBL52) · airframe 26,301 hrs · 12,996 cycles

AFT WET AREA FLOOR BEAM BS 947 LBL 52 SHOWS SIGNS OF CORROSION DOT L631<[01] REMOVED AND REPLACED CORRODED SECTION OF FLOOR BEAM AT STA. 947.5 LEFT SIDE IAW B737-800 SRM 53-70-51-2R-5-B00675.;[02] VERIFIED REMOVED AND REPLACED CORRODED SECTION OF FLOOR BEAM AT STA. 947.5 LEFT SIDE IAW B737-800 SRM 53-70-51-2R-5-B00675.

Part: WEB — CRACKED (BS 986) · airframe 26,301 hrs · 12,996 cycles

AFT WET AREA AFT OF L2 DOOR AT 986 EVIDENCE OF CRACK FOUND ON WEB STRUCTURE DOT L633<[01] PERFORMED SURFACE HFEC ON BLEND AREA IAW B737 NDTM 51-00-00 PROC 23. USING T8257K CAL 28SEP24. NO CRACKS NOTED. WEB REMOVED AND REPLACED ON FAULT TTG8Q00T35FB;[02] PERFORMED SURFACE HFEC ON BLEND AREA IAW B737 NDTM 51-00-00 PROC 23. USING T8257K CAL 28SEP24. NO CRACKS NOTED. WEB REMOVED AND REPLACED ON FAULT TTG8Q00T35FB

Part: TRIM MOTOR — INOPERATIVE (STABILIZER) · airframe 26,172 hrs · 12,928 cycles

ELECTRONIC STABILIZER TRIM DID NOT WORK IN FLIGHT LANDED FLAPS 15; OVERWEIGHT BY 5100# NO HOT BRAKE ISSUES ELECTRONIC STABILIZER TRIM DID NOT WORK IN FLIGHT LANDED FLAPS 15 OVERWEIGHT BY 5100# NO HOT BRAKE ISSUES<[01] REMOVED AND REPLACED STAB TRIM MOTOR AS PER MM 27-41-71 OPS CHK GOOD ACCOPLISHED OVERWEIGHT LANDING INSP AS PER MM 05-51-35

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 26,014 hrs · 12,840 cycles

DURING WALK AROUND; FOUND DELAM AT R/H I/B AFT FLAP ON A PRIOR REPAIR DELAM ON EXISTING REPAIR AT R/H I/B AFT FLAP. 13 FROM I/B EDGE 3 FROM TRAILING EDGE. DELAM AREA 6 BY 6. SEE ATTACHED PIC FOR DETAILS.<[01] CW EA 24-157-00828

Part: AUTOTHROTTLE SYS — UNKNOWN · airframe 25,996 hrs · 12,833 cycles

UNCOMMANDED THROTTLE REDUCTION ON CLIMBOUT AND AGAIN AT APPROX 2400FT AGL. NO RE-OCCURRENCE AFTER THAT<[01] COMPLIED WITH A/T BITE PROCEDURE IAW FIM TASK 22-31 (801). NO HISTORY OR CURRENT FAULTS NOTED AT THIS TIME. A/C OK FOR SERIVE.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 25,495 hrs · 12,557 cycles

LT INBOARD MAIN FLAP DELAMINATED AT AFT EDGE O/B OF FLAP LOWER SKIN OF TRAILING EDGE WEDGE ASSY... LT INBOARD MAIN FLAP DELAMINATED AT AFT EDGE O/B OF FLAP<[01] REMOVED THE LEFT MAIN FLAP TRAILING EDGE WEDGE;[02] REMOVED AND REPLACED LT INBOARD MAIN FLAP AFT WEDGE ASSY. PER. AMM REF.20-50-11 AND SRM REF. 51-40-02.;[03] REFERENCED TSR 202400674 REFERRED DWR 113A2100-73; PL AND SHEET 209

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 25,495 hrs · 12,557 cycles

RT INBOARD MAIN FLAP DELAMINATED AFT EDGE O/B OF FLAP AT WEDGE ASSY LOWER SKIN. RT INBOARD MAIN FLAP DELAMINATED AFT EDGE O/B OF FLAP<[01] REMOVED R/H INB FLAP WEDGE PER SRM 51-40-02;[02] REMOVED AND REPLACED RT. INBOARD MAIN FLAP AFT WEDGE ASSY. PER. AMM REF. 20-50-11 AND SRM REF. 51-40-12.REFERENCED TSR # 202400674 REFERRED DWR 113A2100-73; PL AND SHEET 209.

Part: MEGAPHONE — INOPERATIVE (ZN 200 FUS TOP) · airframe 24,176 hrs · 11,792 cycles

MEGAPHONE INOP<[01] R&R MEGAPHONE IAW AMM 25-64-00

Part: MEGAPHONE — FAILED (ZN 200 FUS TOP) · airframe 24,175 hrs · 11,791 cycles

FLIGHT ATTENDANT MEGAPHONE WILL NOT TEST; NO BLINKING GREEN LIGHT<[01] RR BATTERIES IAW AMM 25-64-00

Part: FLASHLIGHT — FAILED (ZN 200 FUS TOP) · airframe 24,151 hrs · 11,779 cycles

AFT FLASHLIGHT RED LIGHT BLINKING AFT FLASHLIGHT REF LIGHT BLINKING<[01] REMOVED AND REPLACED FLASHLIGHT BATTERY ON AFT L/H INBD REF AMM 25-64-00

Part: BATTERY — DISCHARGED (ZN 200 FUS TOP) · airframe 23,986 hrs · 11,683 cycles

BATTERY FOR L/H FWD ENTRY EMERGENCY EXIT LIGHTS REQUIRES REPLACEMENT DUE TO LOW CHARGE<[01] R/R BATTERY FOR FWD ENTRY EMERGENCY EXIT LIGHTS IAW AMM 33-51-06

Part: FLAP — PULLED (ZN 500 LEFT WING) · airframe 23,736 hrs · 11,539 cycles

LEFT WING; OUTBOARD AFT FLAP HAS DELAMINATION OF LOWER WING SKIN ON INBOARD SIDE MEASURING 26 IN LONG AND 10 IN WIDE. MULTIPLE SCREWS ALSO PULLED THROUGH<[01] REPLACED LEFT OUTBOARD AFT FLAP ASSY REF AMM 27-51-22.;[02] REPLACED LEFT OUTBOARD AFT FLAP ASSY REF AMM 27-51-22.;[03] C/W

Part: GIRT BAR — LOOSE (ZN 200 FUS TOP) · airframe 22,847 hrs · 11,020 cycles

DOOR MOUNTED GIRT BAR HOLDING HOOK IS LOOSE<[01] REINSTALL FASTENER ON GIRT BAR HOOK PER SRM 51-40-02

Part: FLASHLIGHT — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 22,054 hrs · 10,546 cycles

2 OUT OF 4 AFT F/A POS FLASHLIGHTS INOP. REMOVED AND REPLACED BATTERIES AT NOTED LOCATIONS IAW AMM 25-64-00. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 21,405 hrs · 10,206 cycles

AFT CABIN JUMP SEAT FLASHLIGHT INOP / [01] REMOVED AND REPLACED AFT CABIN JUMP SEAT FLASHLIGHT IAW AMM 225-64-00

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 20,301 hrs · 9,572 cycles

AFT LEFT FLASH EMERGENCY FLASH LIGHT INOP / [01] R&R PER AMMJ 25-64-00

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 20,252 hrs · 9,541 cycles

R1 DOOR EMERGENCY LIGHTS INOP / [01] R&RED EMERGENCY BATTERY PACK M2816 PER AMM 33-51-06.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 20,164 hrs · 9,492 cycles

AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP / [01] RELAMPED IAW AMM 33-51-04

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 19,680 hrs · 9,210 cycles

IN THE CABIN; AT STA. 540; LEFT AND RIGHT BREAK AWAY INTERCOSTAL BENEATH FLOOR PANEL CRACKED. / [01] REMOVED AND REPLACED INTERCOSTAL AT BS 540 PER SRM 51-40-02

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 19,680 hrs · 9,210 cycles

FWD CARGO; RH SIDE BAFFLE CRACKED ST STA 500C-500D / [01] REMOVED DAMAGED BAFFLE PER SRM 51-40-02.;[02] REMOVED AND REPLACED FWD CARGO; RH SIDE BAFFLE ST STA 500C-500D PER SRM 51-40-02

Part: BAFFLE — CRACKED (FWD CARGO) · airframe 19,680 hrs · 9,210 cycles

FWD CARGO RT BAFFLE CRACKED BETWEEN STA 500F - STA 500G. / [01] REMOVED DAMAGED BAFFLE PER SRM 53-30-53-2R-1. USED REPAIR 1 TO MAKE INSTALLATION EASIER OF REPLACEMENT BAFFLE WITH A WIRE BUNDLE GOING THROUGH THE FWD LIGHTNING HOLE PER SRM 53-30-53-2R-1.;[02] REMOVED DAMAGED BAFFLE PER SRM 53-30-53-2R-1. USED REPAIR 1 TO MAKE INSTALLATION EASIER OF REPLACEMENT BAFFLE WITH A WIRE BUNDLE GOING THROUGH THE FWD LIGHTNING HOLE PER SRM 53-30-53-2R-1.;[03] REMOVED AND REPLACED FWD CARGO RT BAFFLE BETWEEN STA 500F - 500G PER SRM 53-30-53-2R-1.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 19,680 hrs · 9,210 cycles

FWD CARGO; LH BAFFLE CRACKED AT STA 500C-500D / [01] R/R LH BAFFLE IAW SRM 51-40-02

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 19,680 hrs · 9,210 cycles

FWD CARGO; RH SIDE BAFFLE CRACKED ST STA 500E-500F / [01] REMOVED AND REPLACED BAFFLE PER SRM 51-40-02.;[02] REMOVED AND REPLACED BAFFLE PER SRM 51-40-02.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 19,680 hrs · 9,210 cycles

AFT CARGO COMPARTMENT RH TRANSITION ANGLE HAS NUMEROUS AREAS OF CORROSION STA-767- 787 (MARKED) / [01] DAMAGE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED AFT CARGO TRANSITION ANGLE FROM STA 767 TO 787 PER SRM 51-40-02.;[03] REMOVED AND REPLACED AFT CARGO COMPARTMENT RH TRANSITION ANGLE STA-767- 787 PER SRM 51-40-02

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 19,680 hrs · 9,210 cycles

AFT CARGO COMPARTMENT SUPPORT ANGLE CRACKED FOR WASTE TANK COMPARTMENT POST STA-867 LBL-18 (MARKED) / [01] REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-40-02;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR SUPPORT ANGLE REPLACEMENT.

Part: ANGLE — CORRODED (FWD CARGO) · airframe 19,680 hrs · 9,210 cycles

FWD CARGO: R/H TRANSITION ANGLE HAS NUMEROUS AREAS OF CORROSION FROM STA 500A-500I. REMOVED TRANSITION ANGLE PER SRM 51-40-02;FABRICATED NEW R/H TRANSITION ANGLE FROM STA. 500A-500I PER SRM 53-00-53-2R-5. INSPECTED FABRICATED NEW R/H TRANSITION ANGLE FROM STA. 500A-500I; REMOVED AND REPLACED FWD CARGO R/H TRANSITION ANGLE FROM STA 500A-500I PER SRM 53-00-53-2R-5 AND EA;REMOVED AND REPLACED FWD CARGO R/H TRANSITION ANGLE FROM STA 500A-500I PER SRM 53-00-53-2R-5 AND EA 22-153-01370.

Part: ANGLE — CORRODED (FWD CARGO) · airframe 19,680 hrs · 9,210 cycles

FWD CARGO: AFT FLOOR SUPPORT ANGLE AT STA 500I FROM LBL24-RBL24 HAS NUMEROUS AREAS OF CORROSION. / [01] REMOVED; AND REPLACED AFT FLOOR SUPPORT ANGLE AT STA 500I FROM LBL24-RBL24 . REF. SRM. 51-40-05;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR REPLACEMENT OF FLOOR ANGLE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,680 hrs · 9,210 cycles

L/H TRANSITION ANGLE HAS NUMEROUS AREAS OF CORROSION FROM STA 500C+11 - STA 500D+15 (M) CUT OUT CORRODED SECTION FROM STA 500C+9 TO 500E+9 AND FABRICATED; TREATED; AND PRIMED NEW TRANSITION ANGLE SECTION IAW SRM 53-00-53-2R-6. CUT OUT CORRODED SECTION FROM STA 500B+10 TO 500E+9. LOCATED AND AND MATCH DRILLED NEW SECTION OF TRANSITION ANGLE IAW SRM 53-00-53-2R-6. FABRICATED AND DRILLED SPLICE PLATES IAW SRM 53-00-53-2R-6; FABRICATED TAPERED SHIMS IAW SRM 51-30-01 FIGURE 10. ALODINED AND PRIMED ALL REPAIR PARTS IAW AMM 51-21-72. REMOVED FABRICATED AND REPLACED FORWARD CARGO COMPARTMENT LT TRANSITION ANGLE FORM STA 500B +10 TO STA 500E +9 LBL 24; AND WL 156 IAW SRM 53-00-53-2R-5; EA 22-153-01437-WIP1.

Part: SUPPORT BRACKET — BROKEN (LH WING) · airframe 19,680 hrs · 9,210 cycles

LEFT WING PNEUMATIC DUCT SUPPORT BRACKET BROKEN AT STA 540 ; 58 INCHES LBL. MARKED; PIC INCLUDED. / [01] L/H WING PNEUMATIC DUCT SUPPORT BRACKET (212A9104-1) REMOVED; REPLACED; AND LEAK CHECKED ON WORK ORDER # 12250R522;[02] C/W INSPECTION.

Part: WEB — CRACKED (RH WING) · airframe 19,680 hrs · 9,210 cycles

R/H WING UPPER FIXED T/E PANEL AT INBD DEFLECTION RIB HAS EVIDENCE OF ATTACH WEB CRACKED THROUGH FASTENER HOLE.(MARKED) / [01] R&R CLIP AND ANGLE PER SRM 51-40-02;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR REPLACEMENT OF CLIP AND ANGLE.

Part: ANGLE — CRACKED (LH WING) · airframe 19,680 hrs · 9,210 cycles

LEFT WING TRAILING EDGE SHELF PANEL AT DEFLECTION RIB AREA HAS CRACKED ANGLE ON INBOARD SIDE. (MARKED) / [01] ACCOMPLISHED HFEC OF BEND RADIUS OF NEW PART NO DEFECTS NOTED PER NDT PART 6 51-00-00 PROC. 23;[02] REMOVED FABRICATED AND REPLACED LT WING DEFLECTION RIB ANGLE BRACKET 115A2156-17 PER DWG 115A2156 AND SMAL 0270669630.

Part: ANGLE — CRACKED (LH WING) · airframe 19,680 hrs · 9,210 cycles

LEFT WING TRAILING EDGE INBOARD SHELF PANEL HAS CRACKED ANGLE. (MARKED) / [01] REMOVED AND REPLACED ANGLE AND SEAL RETAINER IAW SRM 51-40-02.

Part: ANGLE — CRACKED (LH WING) · airframe 19,680 hrs · 9,210 cycles

LEFT WING TRAILING EDGE SHELF PANEL AT DEFLECTION RIB AREA HAS CRACKED ANGLE ON OUTBOARD SIDE. (MARKED) / [01] REMOVED AND REPLACED ANGLE PER SRM 51-40-02.

Part: BULKHEAD — CRACKED (AFT CARGO BAY) · airframe 19,680 hrs · 9,210 cycles

AFT CARGO FWD BULKHEAD PANEL IS CRACKED 142NW / [01] REMOVED AND REPLACED PANEL WITH NEW REPLACEMENT PANEL PER AMM 25-52-06.;[02] INSPECTED WORK PERFORMED.

Part: NONE — BROKEN · airframe 19,347 hrs · 9,019 cycles

EMERGENCY LIGHT IN FWD CABIN OVERHEAD CEILING MOUNT BROKEN / [01] REINSTALLED FWD ISLE OVERHEAD LIGHT ASSY PER AMM 33-51-03.

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 15,693 hrs · 7,056 cycles

AFT L/H F/A JUMPSEAT OUTBOARD FLASHLIGHT BLINKING RED ON TEST ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) / CLOSING DMA 0413100R/R BATTERY @ AFT F/T ATT OUTBD FLASHLITE OPS CK GOOD PER M/M 33-51-20CLR# 85084

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 13,134 hrs · 5,767 cycles

R1 DOOR EMERGENCY LIGHT INOP WHILE TROUBLESHOOTING R1 DOOR EMERGENCY LIGHT FOUND CONNECTOR D40042P NOT CONNECTED. CONNECTED D40042P CONNECTOR AND PERFORMED OPERATIONAL TEST IAW B737 AMM'S 33-51-01-960-802 AND 33-51-00-710-801 TEST GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,428 hrs · 5,449 cycles

R/H AFT EMERGENCY EXIT SIDEWALL LIGHT INOP. / R&R PHOTOLUMINESCENT IAW AMM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 10,150 hrs · 4,455 cycles

R1 DOOR EVACUATION SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER SRM.

Part: SENSOR — DIRTY (LANDING GEAR) · airframe 8,855 hrs · 3,884 cycles

LANDING GEAR WOULD NOT RETRACT. CYCLED GEAR EXTEND DOOR AND GEAR RETRACTED. CLEANED LANDING GEAR S1186 SENSOR PER MM. OPS CK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 6,870 hrs · 3,028 cycles

AFT FLIGHT ATTENDANT INBOARD EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT PER MM.

Part: FAIRING — CRACKED (LWR FUSELAGE)

PANEL 191FL HAS FWD CORNER CRACKED ( MX NOTE ) / REPAIRED DAMAGE PER SRM 57-30-70-2R-01 CL# 41209

Part: FAIRING — CRACKED (LWR FUSELAGE) · airframe 5,006 hrs · 2,205 cycles

PANEL 191FL HAS FWD CORNER CRACKED ( MX NOTE ) / REPAIRED DAMAGE PER SRM 57-73-70-22-01 CL# 41209

Part: SCREW — MISSING (R2 DOOR) · airframe 2,726 hrs · 1,212 cycles

R2 DOOR EMERGENCY EVAC SLIDE HINGE SCREW MISSING AT 4B-24. REPAIRED HINGE ASSEMBLY PER CMM.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 2,726 hrs · 1,212 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF ADJUST. ADJUSTED GIRT PER MT.

Part: LIGHT — LOOSE (ROW 2) · airframe 120 hrs · 63 cycles

CABIN EMERGENCY LIGHT ABOVE ROW 2 IS LOOSE. SECURED THE LIGHT IAW MM.