N8694E

Part: MEGAPHONE — DAMAGED (ZONE 200) · airframe 30,556 hrs · 15,252 cycles

FWD MEGAPHONE DAMAGED. REMOVED AND REPLACED MEGAPHONE IAW AMM 25-64-00

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 30,349 hrs · 15,143 cycles

FO SIDE AFT FLASHLIGHT TEST LIGHT NOT WORKING. R&R BATTERY PACK PER M/M SIP

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 30,301 hrs · 15,117 cycles

FWD INBOARD FA FLASHLIGHT WILL NOT CHARGE. REPLACED THE FWD INBOARD FA FLASHLIGHT PER AMM 25-64-00. OPC GOOD.

Part: WEDGE — DELAMINATED (ZONE 500 FLAP) · airframe 29,413 hrs · 14,643 cycles

LEFT WING I/B MAIN FLAP O/B T/E WEDGE IS DELAMINATED<[01] REMOVED AND REPLACED LEFT WING I/B MAIN FLAP O/B T/E WEDGE IAW SOPM 20-50-01 AND AMM 20-50-11-910-801.;[02] VERIFIED CORRECTIVE ACTION

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 29,413 hrs · 14,643 cycles

L/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 AND LBL34 WL167.68<[01] REMOVED; REPLACED AND INSTALLED NEW L/H BS663 UPPER ATTACH ANGLE LBL 6 TO LBL 65PER SRM 51-40-02-0G-0; DWG144A7100 REV: -; DWG 111A7000 REV: -; DWG 111A1000 REV: -.AND DWG 111A1000 REV: B.

Part: LENS — DAMAGED (ZONE 200) · airframe 29,413 hrs · 14,643 cycles

FWD RT OWE SIDEWALL FWD EMERGENCY EXIT LIGHT LENS DAMAGED. REMOVED AND REPLACED FWD R/H OWE SIDEWALL FWD EMERGENCY EXIT LIGHT LENS IAW SOPM 20-50-01.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 29,413 hrs · 14,643 cycles

R/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL9 AND RBL34 WL167.68. REMOVED; REPLACED AND INSTALLED NEW R/H BS663 UPPER ATTACH ANGLE RBL 6 TO RBL 65 WL 167.68 PER SRM 51-40-02-0G-0; DWG144A7100 REV: - DWG 111A7000 REV: - DWG 111A1000 REV: -. AND DWG 111A1000 REV: B.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 29,413 hrs · 14,643 cycles

PASSENGER CABIN FLOOR PANEL 231XF IS DELAMINATED. PASSENGER CABIN FLOOR PANEL 231XF WITH DELAMINATED WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, AND; DWG 144A5810 ID:0126.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 29,413 hrs · 14,643 cycles

PASSENGER CABIN FLOOR PANEL 242CF IS DELAMINATED. DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 242CF FLOOR PANEL IAW SRM 53-00-50-2R-0.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 29,413 hrs · 14,643 cycles

PASSENGER CABIN FLOOR PANEL 241AF IS DELAMINATED. PASSENGER CABIN FLOOR PANEL 241AF WITH DELAMINATED WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 144A5810 ID:0127.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 29,413 hrs · 14,643 cycles

PASSENGER CABIN FLOOR PANEL 241DF IS DELAMINATED. DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241DF FLOOR PANEL IAW SRM 53-00-50-2R-0.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 29,413 hrs · 14,643 cycles

PASSENGER CABIN FLOOR PANEL 241BF IS DELAMINATED AND DAMAGED PLACARD, DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241BF FLOOR PANEL IAW SRM 53-00-50-2R-0.

Part: HOUSING — DAMAGED (ZONE 200) · airframe 29,413 hrs · 14,643 cycles

OWE CENTER ISLE EMERGENCY EXIT HOUSING ASSY SIDE BUMPERS DAMAGED REQUIRES REPLACEMENT. (LENS FALL OUT)<[01] REMOVED AND REPLACED OWE CENTER ISLE EMERGENCY EXIT HOUSING ASSY IAW SIP AMM AMM D633A101-SWA;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FAIRING — PULLED (ZONE 500) · airframe 29,403 hrs · 14,635 cycles

DURING INSPECTION OF#3 CANOE FAIRING FOUND 3 PULLED FASTENERS. <[01] PART INFO ONLY; [02] REMOVED AND REPLACED #3 FLAP AFT FAIRING REF AMM 27-51-18 UP TO STEP 5.G.3.; [03] FINISHED INSTALLATION OF #3 AFT FLAP FAIRING FROM STEP 5.G.3 ON REF AMM 27-51-18.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 29,249 hrs · 14,554 cycles

AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED AFT SERVICE DOOR EXTERIOR EMERGENCY LAMP IAW AMM TASK 33-51-04. OPS CHECK GOOD

Part: COVER — MISSING (ZONE 200) · airframe 29,237 hrs · 14,547 cycles

FLIGHT ATTENDANT REPORTED EXIT SIGN MISSING ROW 14 ABC<[01] INSTALLED LENS COVER PER AMM 33-51-01

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 28,606 hrs · 14,205 cycles

LEFT SIDE OVERWING EMERGENCY EXIT ROW LIGHTS INOP<[01] R&R'D BATTERY PACK IAW AMM 33-51-06;[02] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: LENS — LOOSE (ZONE 200) · airframe 28,489 hrs · 14,141 cycles

EXIT SIGN COVER; MID CABIN; FELL OFF.<[01] RESECURED EXIT SIGN LENS MID CABIN AISLE PER M/M 33-51-03.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 28,220 hrs · 13,991 cycles

FWD FLASHLIGHT CHARGING INDICATOR INOPERATIVE. INSTALLED SEAL AND OPS CHECKED FLASHLIGHT PER M/M 25-64-00, NO FAULTS NOTED.

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 28,005 hrs · 13,872 cycles

EMERGENCY EXIT LIGHT COVER ROW 14A MISSING.<[01] INSTALLED LH OVERWING EXIT SIGN LENS; PERFORMED EMERGENCY LIGHTS OPERATION TEST PER AMM 33-51-00; NO DEFECTS NOTED.

Part: LENS — DETACHED (ZONE 200) · airframe 27,359 hrs · 13,518 cycles

EXIT SIGN OFF MID CABIN.<[01] RE-INSTALLED EXIT SIGN LENS COVER REF APPLICABLE STEPS IN AMM 33-51-01. OPS CHECK GOOD

Part: PANEL — DEBONDED (ZONE 100) · airframe 27,206 hrs · 13,439 cycles

WING TO BODY FAIRING PANEL 192CL DISBANDED AT EDGE. REF.TTG8QVJS7H<[01] ACCOMPLISHED PERMANENT REPAIR TO PANEL 192CL; PER SRM 53-40-70-1A-1. AND RESTORED FINISH PER AMM;51-21-99.;[02] EDITED: ADDED DAMAGE REPAIR TYPE

Part: HOOK AND LOOP — DETACHED (R2 GIRT BAR) · airframe 26,499 hrs · 13,053 cycles

AFT SERVICE DOOR (R2) SLIDE GIRT REQUIRES ADJUSTMENT< HOOK AND LOOP STRIP ON GIRT FOUND NOT ATTACHED TO BACKING PAN. SECURED HOOK AND LOOP ON GIRT TO BACKING PAN PER AMM 20-10-06.

Part: GIRT BAR — OUT OF ADJUST (AFT DOOR) · airframe 26,499 hrs · 13,053 cycles

AFT ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] AFT ENTRY DOOR SLIDE VELCRO STRIP ON GIRT FOUND NOT ATTACHED TO BACKING PAN. SECURED VELCRO ON GIRT TO BACKING PAN PER AMM 20-10-06.

Part: COOLER — DISCONNECTED (NR 2 IDG) · airframe 26,482 hrs · 13,044 cycles

GEN 2 DRIVE LIGHT ILLUMINATED; DISCONNECTED IDG<[01] R & RD #2 ENGINE IDG IAW AMM REF 24-11-11 AND R & RD #2 ENGINE IDG COOLER IAW AMM REF 24-11-21 OPS AND LEAK CHECKED GOOD

Part: IDG — DISCONNECTED (NR 2) · airframe 26,482 hrs · 13,044 cycles

GEN 2 DRIVE LIGHT ILLUMINATED; DISCONNECTED IDG<[01] R & RD #2 ENGINE IDG IAW AMM REF 24-11-11 AND R & RD #2 ENGINE IDG COOLER IAW AMM REF 24-11-21 OPS AND LEAK CHECKED GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,467 hrs · 13,036 cycles

SEVERAL EXTERIOR AND INTERIOR EMERGENCY LIGHTS INOPERATIVE.<[01] PERFORMED POWER SUPPLY - BATTERY PACK REPLACEMENT AT POSITIONS (M1670); (M1671); (M1672); (M1695) AND (M2335) AS PER REF AMM 33-51-06-960-805. REMOVED AND REPLACED BATTERY PACK M1676 AND PERFORMED INSTALLATION TEST FOR ALL EMERGENCY BATTERY PACKS THAT WERE REPLACED AS PER B737 AMM 33-51-06-960-805. TEST PASSED.;[02] VERIFIED STEP 1<BR><BR>AUDIT C/W REF MPM 52.02.02

Part: FAIRING — CRACKED (ZONE 100) · airframe 26,467 hrs · 13,036 cycles

FAIRING PANEL 194HL FASTENER HOLE (1EA) CRACKED<[01] APPLIED REPAIR TO DAMAGED AREA AT PANEL 194HL AS PER B737 SRM 51-70-01-2R-0 PARAG 4.L-M-N. APPLIED TOPCOAT AT REPAIR AREA ON PANEL 194HL AS PER B737 AMM 51-21-99-300-802 PARAG 3.C.3.

Part: FRAME — CRACKED (BS 312 LBL 33) · airframe 26,467 hrs · 13,036 cycles

PASSENGER CABIN STA 312 WL282 LBL 33 CRACKED (ABOVE L-1 DOOR CUTOUT).<[01] TASK ACCOMPLISHED ON GENERAL EA\ M-22-153-01244;[02] VERIFIED STEP 1

Part: WINGLET — DAMAGED (LT WING) · airframe 26,467 hrs · 13,036 cycles

LEFT WINGLET/SCIMITAR WRAP AROUND ACCESS PANEL HAS 1EA ELONGATED HOLE<[01] REPAIRED DAMAGE HOLE AT LAFT WINGLET/SCIMITAR WRAP ACCESS PANEL AS PER SRM 51-70-04-2R-9. MATERIAL USED EA9390 PO #2061896.<BR>PERFORMED ULTRASOUND INSPECTION OF REPAIRED AREA AND MINIMUM OF 6 INCHES ALL AROUND USING CONTACT THROUGH TRANSMISSION ULTRASONIC REF B737 NDT PT 1; 51-01-01; NDT PT4 51-00-02. NO DAMAGE NOTED<BR> TOOL: EPOCH 650 B/C: 168106 DUE: 12/11/24;[02] VERIFIED STEP 1.

Part: FLOORBEAM — CORRODED (BS 948) · airframe 26,467 hrs · 13,036 cycles

ACCOMPLISH REPAIR OF STA 947.5 FLOOR BEAM<[01] ACCOMPLISHED REPAIR OF FLOOR BEAM STA 947.5 PER SRM 53-70-51-2R-5-B00675 (REPAIR 5 - SECTION 47 - LARGE CORROSION DAMAGE ON THE UPPER CHORD OF THE FLOOR BEAM AT STA 947.5 - PERMANENT).;[02] RE-INSTALLED ALL ADJACENT STRUCTURE REMOVED FOR REPAIR ACCESS PER SRM 51-40-02-0G-0; BOEING DWG# 147A8501; #147A5650;[03] RII: VERIFIED STEPS 1 AND 2;[04] CORRECTION FOR STEP 3 SHOULD BE A RII STEP;[05] (RII) FINAL INSPECTION; VERIFIED STEP #1 AND #2.

Part: SUPPORT ANGLE — CORRODED (BS 927-948) · airframe 26,467 hrs · 13,036 cycles

CORROSION AT FLOOR STRUCTURE STABILIZER ANGLE AT STA 927-947.5 LBL-24<[01] REMOVED; FABRICATED; AND INSTALLED NEW ANGLE PN#147A5430-7 AT FLOOR STRUCTURE STA 927-947.5 LBL-24. PER SRM 51-40-02-0G-0 AND BOEING DWG 147A5400 SHEET 21;[02] VERIFIED STEP 1

Part: FLOOR PANEL — PEELING (AFT CABIN) · airframe 26,467 hrs · 13,036 cycles

MAIN CABIN AFT WET AREA PANEL#242UF HAS UPPER SKIN PEELING IN MULTIPLE AREAS.<[01] RECEIVED NEW FLOOR PANEL # 242UF AND INSTALL ON TTG8Q00T3WTC;[02] FINAL INSPECTION; VERIFIED STEP #1.

Part: FLOOR SUPPORT — CORRODED (BS 951 RBL 50) · airframe 26,467 hrs · 13,036 cycles

CORROSION AFT CABIN WET AREA FLOOR SUPPORT INTERCOSTAL @ RBL 50 STA 951 MKD DOT<[01] REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL AT STA 951 RBL 50 REF B 737-800 SRM 51-40-02-0G-0;[02] CORRECTION STEP 1 DWN # 147A5650;[03] VERIFIED STEP 1 AND 2.<BR><BR>AUDIT C/W REF MPM 52.02.02

Part: FLOOR SUPPORT — CORRODED (BS 951 RBL 25) · airframe 26,467 hrs · 13,036 cycles

CORROSION AFT CABIN WET AREA FLOOR SUPPORT INTERCOSTAL @ RBL 24.75 STA 951<[01] REMOVED AND INSTALLED NEW AFT CABIN WET AREA FLOOR SUPPORT INTERCOSTAL @ RBL 24.75 STA 951 PER REF SRM 51-40-02-0G-0 AND DWG 147A5650 SHEET 105;[02] RII VERIFIED CORRECTIVE ACTION.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 26,467 hrs · 13,036 cycles

AFT CABIN WET AREA FLOOR SUPPORT INTERCOSTAL TOP SKIN @ LBL 24.75 STA 951 MKD DOT<[01] INSTALLED NEW FLOOR SUPPORT INTERCOSTAL AT STA 951 LBL 24.75 REF B 737-800-SRM 51-40-02-0G-0;[02] CORRECTION STEP 1 DWN # 147A650;[03] REMOVED AND REPLACED NEW INTERCOSTAL PART NO. 147A5660U3 AT AFT CABIN WET AREA STA. 947.5 TO 967 LBL 24.75 REF. SRM 51-40-02-0G-0 AND DWG 147A5650;[04] STEPS 1-3 INCORRECT REFERENCES. <BR>CORRECTION TO STEPS 1-3:<BR>REMOVED DAMAGED BEYOND LIMITS INTERCOASTAL; AND INSTALLED NEW INTERCOASTAL P/N 147A5660U3 AT AFT CABIN WET AREA LBL 24.75 STA 951. REFERENCES: SRM 53-70-51-1A-1 ; SRM 51-40-02-0G-0 AND BOEING DWG# 147A5650 SHEET 55.;[05] VERIFIED STEP 4.

Part: FLOORBEAM — CORRODED (BS 948 LBL25) · airframe 26,467 hrs · 13,036 cycles

CORROSION *** AFT CABIN WET AREA FLOOR BEAM TOP SKIN @ LBL 24.75 STA 947.5 MKD DOT<[01] EXFOLIATION CORROSION FOUND OUT OF LIMITS AT STA 947.5 LBL 24.75 UPPER FLANGE. REFERENCES: SRM 53-70-51-1A-1; DWG SHEET 147A5504 SHEET 38. REPAIR OF UPPER FLANGE WILL BE ACCOMPLISHED ON CUSTOMER TASK CARD: TTG8Q00TXP7Q;[02] FINAL INSPECTION; VERIFIED STEP #1.

Part: FLOORBEAM — CRACKED (BS 540 LBL1) · airframe 26,467 hrs · 13,036 cycles

MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ LBL 1 STA 540 MKD DOT<[01] REMOVED AND REPLACED MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK @ LBL 1 STA 540 AS PER 51-40-02-0G-0.;[02] EDIT TO CORRECTIVE ACTION STEP1: REMOVED AND REPLACED MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK @ LBL 1 STA 540 AS PER SRM B737-800 51-40-02-0G-0.;[03] EDIT TO CORRECTIVE ACTION STEP1 AND 2: REMOVED AND REPLACED MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK @ LBL 1 STA 540 AS PER SRM B737-800 51-40-02-0G-0. DWG. NO 143A5240 PG 1;[04] FINAL INSPECTION; VERIFIED STEP #3.

Part: FLOORBEAM — CORRODED (BS 948) · airframe 26,467 hrs · 13,036 cycles

CORROSION *** AFT CABIN WET AREA FLOOR BEAM TOP SKIN @ RBL 50 STA 947.5 MKD DOT<[01] EXFOLIATION CORROSION FOUND OUT OF LIMITS AT STA 947.5 RBL 50 UPPER FLANGE. REFERENCES: SRM 53-70-51-1A-1; DWG SHEET 147A5504 SHEET 38. REPAIR OF UPPER FLANGE WILL BE ACCOMPLISHED ON TTG8Q00TXP7Q;[02] (RII) FINAL INSPECTION; VERIFIED STEP #1.

Part: SUPPORT BRACKET — CRACKED (BS 867 S26L) · airframe 26,467 hrs · 13,036 cycles

AFT CARGO COMPARTMENT SUPPORT BRACKET CRACKED BELOW WASTE MID POST S-26L STA 867 MKD DOT<[01] REMOVED AND INSTALLED NEW AFT CARGO COMP NEW SUPPORT BRACKET BELOW WASTE MID POST S-26L STA 867 P/N: 149A8109U114 PO# 2059779 PER SRM 51-40-02-0G-0;[02] REMOVED AND INSTALLED NEW AFT CARGO COMP NEW SUPPORT BRACKET BELOW WASTE MID POST S-26L STA 867 P/N: 149A8109U114 PO# 2059779 PER SRM 51-40-02-0G-0 AND PER IPC 53-42-51-06 FIGURE 505.;[03] CORRECTION STEP # 1AND 2 REMOVED AND INSTALLED NEW AFT CARGO COMP NEW SUPPORT BRACKET BELOW WASTE MID POST S-26L STA 867 P/N: 149A8109U114 PO# 2059779 PER SRM 51-40-02-0G-0 AND PER IPC 53-42-51-06 FIGURE 505.;[04] VERIFIED STEP 3.

Part: FLOORBEAM — CORRODED (BS 948) · airframe 26,467 hrs · 13,036 cycles

CORROSION *** AFT CABIN WET AREA FLOOR BEAM TOP SKIN @ RBL 24.75 STA 947.5 MKD DOT<[01] EXFOLIATION CORROSION FOUND OUT OF LIMITS AT STA 947.5 RBL 24.75 UPPER FLANGE. REFERENCES: SRM 53-70-51-1A-1; DWG SHEET 147A5504 SHEET 38. REPAIR OF UPPER FLANGE WILL BE ACCOMPLISHED ON CUSTOMER TASK CARD: TTG8Q00TXP7Q;[02] FINAL INSPECTION; VERIFIED STEP #1.

Part: FLOORBEAM — CRACKED (BS 540 RBL 1) · airframe 26,467 hrs · 13,036 cycles

MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ RBL 1 STA 540 MKD DOT<[01] REMOVED AND REPLACED MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK AT RBL 1 STA 540 AS PER SRM 51-40-02-0G-0.;[02] EDIT TO CORRECTIVE ACTION STEP1: REMOVED AND REPLACED MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK @ RBL 1 STA 540 AS PER SRM B737-800 51-40-02-0G-0.;[03] EDIT TO CORRECTIVE ACTION STEP1 AND 2: REMOVED AND REPLACED MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK @ RBL 1 STA 540 AS PER SRM B737-800 51-40-02-0G-0. DWG. NO 143A5240 PG 1;[04] FINAL INSPECTION; VERIFIED STEP #3.

Part: POST — CORRODED (LAVATORY DOOR) · airframe 26,467 hrs · 13,036 cycles

MAIN CABIN FWD LAV DOOR POST CORRORED AT THE BOTTOM<[01] REMOVED AND REPLACED FWD LAV A DOOR POST AS PER REF CMM 25-40-40;[02] VERIFIED STEP 1

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 26,467 hrs · 13,036 cycles

AFT CARGO DOOR CUTOUT SURROUND STRUCTURE ;THRESHOLD HAS SEVERAL CORROSION NOTED.<[01] REMOVED AND REPLACED AFT CARGO DOOR CUTOUT SURROUND STRUCTURE THRESHOLD WEB AS PER SRM 51-40-02-0G-0 AND DWG 146A8340 SHEET 21;[02] REMOVED AND REPLACED AFT CARGO DOOR CUTOUT SURROUND STRUCTURE THRESHOLD WEB AS PER SRM 51-40-02-0G-0 AND DWG 146A8340 SHEET 21 USED TOOL B/C:169123 NO DUE DATE;[03] VERIFIED STEP 2.

Part: FLASHLIGHT — NO TEST (AFT CABIN) · airframe 26,147 hrs · 12,866 cycles

AFT F/A FLASHLIGHT WOULD NOT TEST<[01] R&R FLASHLIGHT ASSY REF AMM 25-64-00

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 25,616 hrs · 12,585 cycles

EMERGENCY EXIT/SALIDA SIGN FELL OFF. MID CABIN<[01] INSTALLED OVERHEAD EMERGENCY EXIT LENS COVER IAW SIP.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 24,543 hrs · 12,005 cycles

EMERGENCY LIGHTS IN AFT GALLEY LEFT SIDE INOP<[01] R&RD BATTERY PACK AND CHARGER ASSY

Part: CHARGER — INOPERATIVE (ZN 200 FUS TOP) · airframe 24,543 hrs · 12,005 cycles

EMERGENCY LIGHTS IN AFT GALLEY LEFT SIDE INOP<[01] R&RD BATTERY PACK AND CHARGER ASSY

Part: SIGN — BROKEN (ZN 200 FUS TOP) · airframe 23,992 hrs · 11,689 cycles

RH; AFT; OVER WING EMERGENCY EXIT SIGN IS BROKEN RH AFT OVER WING EMERGENCY EXIT SIGN IS BROKEN<[01] REMOVED AND REPLACED RH;AFT; OVER WING EMERGENCY EXIT SIGN LENS IAW AMM 33-51-01.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 23,863 hrs · 11,609 cycles

LEFT FWD EMERGENCY ESCAPE SLIDE LIGHT INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06 OPS CHECK GOOD.

Part: COVER — MISSING (ZN 200 FUS TOP) · airframe 23,145 hrs · 11,193 cycles

OVERWING EXIT CEILING SIGN COVER MISSING<[01] INST NEW FWD FACING LENS IAW S.I.P.

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 23,100 hrs · 11,166 cycles

F/A FLASHLIGHT CAPT SIDE CLOSEST TO THE DOOR IS INOP<[01] SECURED LOOSE FLASHLIGHT PER AMM 25-64-00. OPS CHECKS GOOD.

Part: SNUBBER — OUT OF RIG (ZN 800 DOOR) · airframe 22,503 hrs · 10,823 cycles

AFT ENTRY DOOR DIFFICULT TO OPERATE<[01] R&R AFT ENTRY DOOR SNUBBER IAW AMM 52-13-51

Part: BATTERY — INOPERATIVE (ZN 200 FUS TOP) · airframe 22,051 hrs · 10,567 cycles

F/A AIRCRAFT LEFT OUTBOARD FLASHLIGHT INOP<[01] REMOVED AND REPLACED AFT L/H OUTBOARD FLASHLIGHT BATTERY PER AMM 25-64-00. OPS CHECK GOOD. REF LP 1671811

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,656 hrs · 10,346 cycles

R1 DOOR INTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK (M2816) AT BS 310 IAW AMM 33-51-06.

Part: STRIP — LOOSE (ZN 200 FUS TOP) · airframe 21,467 hrs · 10,237 cycles

LIGHT STRIP ON FLOOR ROW 12 IS LOOSE.<[01] SECURED LIGHT STRIP PER M/M 33-51-15

Part: FLASHLIGHT — FAILED · airframe 20,418 hrs · 9,628 cycles

1 AFT CABIN FLASHLIGHT WILL NOT TEST / [01] REMOVED AND REPLACED 1EA AFT CABIN FLASHLIGHT PER AMM 25-64-00. OPS CHECK GOOD.

Part: TIE DOWN — MISSING (FWD CARGO BAY) · airframe 19,718 hrs · 9,216 cycles

FWD CARGO AFT OF DOOR FLOOR PLATE FLUSH RIVETED TIE DOWN MISSING AND METAL DISTORTED. / [01] REPLACED TIE DOWN PER SRM 51-40-02;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR TIE DOWN REPLACEMENT.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 19,718 hrs · 9,216 cycles

ANGLE AT STA.767-794 R/H SIDE BELOW Z-ANGLE HAS CORROSION-AFT CARGO. (CARD WRITTEN TO ADD CORROSIO QUESTIONS PER MPM) / [01] REMOVED AND REPLACED L ANGLEL BELOW R/H TRANSITION ANGLE BS 767-787 PER SRM 51-40-02;[02] C/W INSPECTION.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 19,718 hrs · 9,216 cycles

ANGLE AT STA.767-794 R/H SIDE BELOW Z-ANGLE HAS CORROSION-AFT CARGO / [01] REMOVED AND REPLACED WITH NEW ANGLE 146A8125-53 PER SRM 51-40-02

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 19,718 hrs · 9,216 cycles

AFT CARGO RH Z ANGLE HAS CORROSION ON BOTTOM SIDE AT STA 767-794 / [01] REMOVED R/H SHIELD FROM STA 767-794 PER SRM 51-40-02.;[02] REMOVED AND REPLACED AFT CARGO RT TRANSITION ANGLE SHIELD FROM STA 767 TO STA 794 IAW SRM 51-40-02.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 19,718 hrs · 9,216 cycles

AFT CARGO RH Z ANGLE HAS CORROSION AT STA 847+6 MARKED IN RED. / [01] REMOVED AFT CARGO RH Z ANGLE IAW SRM 51-40-02.;[02] REMOVED AND REPLACED AFT CARGO HOLD SHIELD BETWEEN STA 847 TO STA 867; RBL 24 IAW SRM 51-40-02.;[03] C/W INSPECTION.

Part: ANGLE — CORRODED · airframe 19,718 hrs · 9,216 cycles

R/H TRANSITION ANGLE AT STA. 727C SHOWS SIGNS OF CORROSION / [01] REMOVED AND REPLACED RT TRANSITION ANGLE FROM STA 727+4 TO STA 727E +10 PER SRM 53-00-53-2R-5. SEE N/R CARD TTG8QOOCPMDZ FOR WORK PERFORMED.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 19,718 hrs · 9,216 cycles

AFT CARGO L/H TRANSITION ANGLE STA 727H TO 727I SHOWS SIGNS OF CORROSION. / [01] REMOVED DAMAGED SECTION OF L/H TRANSITION ANGLE FROM BS 727G+10 TO 807+10.;[02] FABRICATED; ALODINED; AND PRIMED REPAIR PARTS IAW SRM 53-00-53-2R-6. INSTALLATION REQUIRED.;[03] REMOVED AND REPLACED DAMAGED SECTION OF LT TRANSITION ANGLE FROM STA 727G+10 TO STA 807+10 IAW SRM 53-00-53-2R-5. FABRICATED; ALODINED; AND PRIMED REPAIR PARTS IAW SRM 53-00-53-2R-5.;[04] VERIFIED REMOVED AND REPLACED DAMAGED SECTION OF LT TRANSITION ANGLE FROM STA 727G+10 TO STA 807+10 IAW SRM 53-00-53-2R-5. FABRICATED; ALODINED; AND PRIMED REPAIR PARTS IAW SRM 53-00-53-2R-5.

Part: TRANS PANEL — CORRODED (AFT CARGO BAY) · airframe 19,718 hrs · 9,216 cycles

AFT CARGO L/H TRANSITION ANGLE STA 727I TO 727J SHOWS SIGNS OF CORROSION. / [01] DEFECT REPAIRED ON CARD TTG8Q00CPMF5.;[02] CW

Part: ANGLE — CORRODED · airframe 19,718 hrs · 9,216 cycles

R/H TRANSITION ANGLE AT STA. 727A SHOWS SIGNS OF CORROSION / [01] REMOVED DAMAGED SECTION FROM STA TO 727+4 TO 727E+12; FABRICATED; ALODINED; AND PRIMED REPAIR PARTS IAW SRM 53-00-53-2R-6. INSTALLATION OF REPAIR PARTS REQUIRED.;[02] INSTALLED REPAIR PART PER SRM 53-00-53-2R-5.;[03] VERIFIED INSTALLED REPAIR PART PER SRM 53-00-53-2R-5.;[04] INSTALLED BONDED NUTPLATES ON 03 JUN AT 09:00AM ON RT TRANSITION ANGLE PER SRM 51-40-10.

Part: SUPPORT ANGLE — CRACKED (RH WING) · airframe 19,718 hrs · 9,216 cycles

RIGHT WING T/E SHELF PANEL AT FLAP DEFLECTION RIB HAS SUPPORT ANGLE CRACKED ON OUTBOARD END. (MARKED) / [01] REMOVED RIGHT T/E SHELF PANEL SUPPORT ANGLE IN IAW SRM 51-40-02.;[02] INSTALLED RIGHT T/E SHELF PANEL IAW SRM 51-40-02.;[03] CW

Part: ANGLE — CORRODED (AFT CARGO) · airframe 18,939 hrs · 8,770 cycles

GENERATED NEW FAULT DUE TO RII REQUIREMENTS. ORIGINAL FAULT; CORROSION FOUND IN AFT CARGO ON RIGHT TRANSITION ANGLE BETWEEN STA. 727I AND 787. [TTG8Q00B325B] / [01] HANHLY SOUVORAVONG (TECHNICIAN); 01-MAR-2022 19:39 UTC<BR>REMOVED RIGHT HAND TRANSITION ANGLE FROM STA. 727F+12 TO STA. 787 PER SRM 53-00-53-2R-6 REPAIR 6[11] C/W RII INSPECTION <BR>10. TONI KERNS (TECHNICIAN); 02-MAR-2022 07:43 UTC <BR>HANHLY SOUVORAVONG (TECHNICIAN); 02-MAR-2022 01:54 UTC <BR>REMOVED AND REPLACED TRANSITION ANGLE SECTION FROM STA. 727F+12 TO STA. 787 PER SRM 53-00-53-2R-6 REPAIR 6.

Part: ANGLE — CORRODED (AFT CARGO) · airframe 18,939 hrs · 8,770 cycles

CORROSION FOUND IN AFT CARGO ON RIGHT TRANSITION ANGLE BETWEEN STA. 727I AND 787. / [01] REMOVED RIGHT HAND TRANSITION ANGLE FROM STA. 727F+12 TO STA. 787 PER SRM 53-00-53-2R-6 REPAIR 6;[02] FABRICATED NEW ZEE ANGLE AND SPLICE PLATE FROM BAC1496-377 7075-T62 CLAD FORMED CHANNEL PER SRM 53-00-53-2R-6 REPAIR 6;[03] TREATED AND PRIMED REPAIR PARTS AND REWORK AREA PER SRM 51-20-01;[04] OK TO INSTALL;[05] INSTALLED NEW TRANSITION ANGLE IN-BETWEEN 727F+12 TO STA. 787 PER SRM 53-00-53-2R-6 REPAIR 6;[06] VERIFIED;[07] CLICK BOND NUT PLATE INSTALLED ON FAULT NO: TTG8Q00B31ZX;[08] REMOVED AND REPLACED TRANSITION ANGLE SECTION FROM STA. 727F+12 TO STA. 787 PER SRM 53-00-53-2R-6 REPAIR 6.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 18,939 hrs · 8,770 cycles

FOUND CORROSION ON AFT CARGO FLOOR PANEL 140CF / [01] REMOVED AFT CARGO FLOOR PANEL 140CF IAW AMM 25-52-10;[02] REMOVED AND REPLACED DAMAGED FLOOR PANEL PER AMM 25-52-10.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 18,939 hrs · 8,770 cycles

CORROSION FOUND ON AFT CARGO FLOOR PANEL 140BF RIGHT SIDE. / [01] REMOVED AND REPLACED DAMAGED FLOOR PANEL PER AMM 25-52-10.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 18,939 hrs · 8,770 cycles

CORROSION FOUND ON AFT CARGO FLOOR PANEL 140EF RIGHT SIDE. / [01] REMOVED AND REPLACE DAMAGED FLOOR PANEL PER AMM 25-52-10.

Part: SUPPORT BEAM — CORRODED (FUSELAGE)

LOGBOOK N# 1697420 : ***CORROSION**** SUPPORT BEAM ARE CORRODED AT ATTACHED POINT UNDER FWD CARGO PANELS 121DW. /

Part: NONE — CORRODED (FUSELAGE)

LOGBOOK N# 1697420 : ***CORROSION**** SUPPORT BEAM ARE CORRODED AT ATTACHED POINT UNDER FWD CARGO PANELS 122FW. / EVALUATED CORROSION AREA UNDER FWD CARGO PANEL 122FW; FOUND Z CHANNEL - SIDE PLATE OUT OF LIMITS PER B737 SRM 53-00-53-1A-2 ; REPLACED DAMAGE Z CHANNEL - SIDE PLATE FROM BS 500A TO BS 500I PER REF B737 SRM 51-40-02-0G-0 ; DWG 143A7500 AND REPAIR 53-00-53-2R-5

Part: LIGHT — DETACHED (CENTER ISLE) · airframe 7,821 hrs · 17,204 cycles

CENTER ISLE EMERG. EXIT SIGN FELL OFF / RESECURED EMERG. EXIT SIGN PER M/M 33-51-20

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN)

FWD FLT ATTENDENT INBD EMERGECY FLASH LIGHT INOP / REPLACED FORWARD F/A ONBOARD FLASHLIGHT BATTERY PER SIP OPS CHECKS OK CLEARING 91608

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 7,756 hrs · 17,079 cycles

FWD FLT ATTENDENT INBD EMERGECY FLASH LIGHT INOP / R/R BATTERY

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,494 hrs · 7,440 cycles

AFT OVERHEAD EMERGENCY LIGHTS INOP / ACCOMPLISHED POWER SUPPLY-BATTERY PACK DEEP CYCLE PROCEDURE IAW AMM 33-51-06.

Part: LIGHT — FAULTED (LT OVERWING) · airframe 16,465 hrs · 7,428 cycles

LH FWD OVERWING EMERGECNY DOOR SIDE LIGHT FLICKERS. ( CABIN INTERIOR ILLUM BOEING SKY INTERIOR PHOTOLUMINESCENT ) /

Part: LIGHT — FAULTED (LT OVERWING) · airframe 16,465 hrs · 7,428 cycles

LH FWD OVERWING EMERGECNY DOOR SIDE LIGHT FLICKERS. ( CABIN INTERIOR ILLUM BOEING SKY INTERIOR PHOTOLUMINESCENT ) /

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 14,173 hrs · 6,231 cycles

FORWARD SERVICE DOOR SLIDE PARTIALLY FELL OUT OF CLAM DOOR. REINSTALLED SLIDE IAW TASK 725-61-06.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 14,137 hrs · 6,217 cycles

AFT FLT. ATTD. EMERGENCY FLASHLIGHT WAS INOPERATIVE. R & R THE FLASHLIGHT IAW MM 25-64-00.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 13,968 hrs · 6,139 cycles

ON FWD ENTRY DOOR, GIRT BARS ARE DIFFICULT TO LATCH AND STOW. (BOTH TO ENGAGE AND RELEASE TO STOW) REPOSITION GIRT BAR IAW AMM 25-66-01; CKD OK.

Part: SKIN — CRACKED (EXT POWER DOOR) · airframe 12,912 hrs · 5,621 cycles

EXTERNAL POWER DOOR OPENING HAD CRACKED OUTER SKIN AT 6 O'CLOCK POSITION. / REPAIRED EXTERNAL POWER DOOR PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 9,272 hrs · 4,008 cycles

R2 DOOR EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 7,757 hrs · 3,363 cycles

EXIT SIGN LOOSE OVER BETWEEN ROWS 14 AND ROW 15. SECURED SIGN PER SIP.

Part: LENS — LOOSE (CABIN) · airframe 7,074 hrs · 3,086 cycles

SIDE WALL EXIT LIGHT LENS LOOSE AT ROW 15 DEF. SECURED LENS PER MM.