N8623F

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK ANGLE LOCATED BS 500I & STR 28L AT FWD CARGO COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-40-02 AND DWG 143A7902, SHEET 301, REV A.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACKED ANGLE, BS 500I, STR 28R IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7902, SHEET 301, REV A.

Part: RIB — CRACKED (ZONE 300) · airframe 39,409 hrs · 19,063 cycles

CRACK RIB LOCATED LE STA 123.85 ACCESS PANEL 341B AT RT HORIZONTAL STAB. REPLACED RIB LOCATED LE STA 123.85 ACCESS PANEL 341B AT RT HORIZONTAL STAB IAW SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG: 186A1001 SHEET: 19 REV - .

Part: ANGLE — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACKED ANGLE ON ACCESS PANEL 844DZ RT SIDE AFT GALLEY DOOR. REPLACED THE ANGLE IAW SRM 51-40-02, AND 51-10-02, ITEM 9.

Part: RIB — CRACKED (ZONE 300) · airframe 39,409 hrs · 19,063 cycles

CRACK RIB LOCATED LE HSS 105.26 LT HORIZONTAL STAB. REPLACED RIB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1001, SHEET 19, REV-, DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM IAW SRM 55-10-09-1A-1, ALLOWABLE DAMAGE 1. MEASUREMENT OF CRACK IS:0.5500 INCH.

Part: BALANCE ARM — OUT OF TOLERANCE (ZONE 300) · airframe 39,409 hrs · 19,063 cycles

DURING WEIGHT AND BALANCE PROCEDURE OF RT ELEVATOR FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1EA) ON BAY 2; P/N: 183A0210-14 (1EA) AND P/N: 69-53211-2 (2EA) ON BAY 3; P/N: 183A0210-15 ON BAY 4 2025-652468. TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03767.

Part: ANGLE — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACK ON ANGLE ON ACCESS PANEL 844DZ, LT SIDE, GALLEY DOOR. REPLACED ANGLE IAW SRM 51-40-02, AND 51-10-02, ITEM 9.

Part: SUPPORT BEAM — CRACKED (ZONE 800) · airframe 39,409 hrs · 19,063 cycles

CRACK SUPPORT BEAM NR 4 LOCATED FWD GALLEY SERVICE DOOR. REPLACED BEAM 4 LOCATED FWD GALLEY SERVICE DOOR AT PASSENGER CABIN IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 141A6516; SHEET 142; REV -.

Part: BALANCE ARM — OUT OF TOLERANCE (ZONE 300) · airframe 39,409 hrs · 19,063 cycles

DURING WEIGHT AND BALANCE PROCEDURE OF LT ELEVATOR FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1EA) ON BAY 2; P/N: 183A0210-14 (1EA) AND P/N: 69-53211-2 (2EA) ON BAY 3; P/N: 183A0210-15 ON BAY 4 2025-652467. TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03766.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACK ON THE FLOORBEAM, BS 540 BTW BL 0 TO RBL 24.75, WL 208.1. REPLACED THE FLOORBEAM IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 143A0060, SHEET 64, REV-. MEASUREMENT OF CRACK IS 0.380.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS 500E TO BS 500I LBL 22 WL 156.1AT FWD CARGO COMPARTMENT, 12 POINTS. FAULT RESOLVED ON FAULT TTG8Q016272L.

Part: FRAME — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. PERFORMED PERMANENT REPAIR FRAME IAW EA M-22-153-01244.

Part: BRACKET — CRACKED (ZONE 600) · airframe 39,409 hrs · 19,063 cycles

CRACK ON BRACKET TRAILING EDGE LOCATED ORSS273 AT RT WING. REPLACED THE BRACKET TRAILING EDGE LOCATED ORSS273 AT RT WING IAW SRM 51-10-02-0G; SRM 51-40-02-0G-0 AND DWG 115A6200 SHEET 17 REV A TOOK MEASURE OF CRACK IS: 1.754 INCHES.

Part: WEB — CORRODED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CORROSION ON SHIELD WEB, BTW BS 492.4 - 500A, RBL 23, WL 208.1. REPLACED SHIELD WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A0080, SHEET 39, REV-.

Part: TIE CLIP — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK ON TIE CLIP, BS 500I, STRINGER 26R, WL 156.1. REPLACED THE TIE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A1234, SHEET 13, REV A.

Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACKED SUPPORT BRACKET, BS 867, BTW STR 2R TO STR 3R. REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A7901, SHEET 66, REV A.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CORROSION ON SUPPORT ZEE, BTW BS 500A - 500E, RBL 22, WL 156.1. THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR5) AND EA M-22-153 -01550.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 142, REV-. MEASUREMENT OF THE CRACK IS: 1.250 INCH.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACKED SUPPORT ANGLE BTW BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A5400, SHEET 154, REV -, MEASUREMENT OF THE CRAK IS 0.667 INCH.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 49 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 38, REV-. MEASUREMENT OF THE CRACK IS: 0.292 INCH.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACK ON SUPPORT ANGLE BTW BS 380 TO BS 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 138, REV -. MEASUREMENT OF THE CRACK IS 1.298

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 39,409 hrs · 19,063 cycles

CORROSION ON SUPPORT ZEE, BTW BS 500E - 500I, RBL 22, WL 156.1. FWD CARGO COMPARTMENT. FAULT RESOLVED ON FAULT TTG8Q0161PAR.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS 500 TO BS 500E LBL 22 WL 156.1, AT FWD CARGO COMPARTMENT,12 POINTS. THE DAMAGE WAS REPAIRED IAW SRM 53-00-53-2R-5 AND EA M-22-153 -01550.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK ON ANGLE CLIP FWD FACE, BS 500H, STRINGER 26R. REPLACED THE ANGLE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505 SHEET 139, REV-. MEASUREMENT OF THE CRACK: L: 0.345 INCH.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACKED INTERCOSTAL BTW BS 500A - 500B, STRINGER 26R. REPLACED THE WEB - INTERCOSTAL IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV -.

Part: NUT — DETERIORATED (ZONE 800 HANDLE) · airframe 39,409 hrs · 19,063 cycles

DETERIORATED CAM NUT ON AFT GALLEY SERVICE DOOR HANDLE. REPLACED CAM NUT IAW AMM 52-41-11-400-801, STEP 3.F (5), ITEM (I) THRU 3.F (5), ITEM (N).

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK GUSSET ANGLE, BS 500I, STRINGER 21L. REPLACED THE GUSSET ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7902, SHEET 256, REV B. REJECTED REPLACEMENT DUE TO BAD AND WRONG SEALANT APPLICATION AROUND GUSSET, APPLIED SEALANT ON GUSSET ANGLE IAW SRM 51-20-05-0G-0.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK ON ANGLE AFT FACE BS 500H, STRINGER 26R. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 139, REV-. MEASUREMENT OF CRACK: L: 0.480 INCH.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK ON THE ANGLE LOCATED AFT FACE BS 500H, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEP 9, SRM 51-40-02, AND DWG 143A7505, SHEET 139, REV-.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK ON ANGLE CLIP AFT FACE, BS 400 STRINGER 26L. MEASUREMENT OF CRACK IS L: 0.530 INCHES. REPLACED THE ANGLE CLIP IAW SRM 51-40-02-0G, SRM 51-10-02-0G, PARAGRAPH 9, AND DWG 143A7505 SHEET 137, REV-.

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 39,409 hrs · 19,063 cycles

CRACKED SEAL - BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER. REPLACED BLADE LOCATED ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER IAW SRM 51-40-02.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACKED GUSSET ANGLE, BS 500I, STRINGER 19R IN THE FWD CARGO BAY. MEASUREMENT OF THE CRACK IS L: 0.9235 INCHES. . REPLACED GUSSET ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG: 143A7902, SHEETS 256 AND 257, REV B.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK ON ANGLE CLIP FWD FACE, BS 500H, STRINGER 26L. REPLACED THE ANGLE CLIP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 139, REV-. MEASUREMENT OF CRACK IS: L: 1.905 INCH.

Part: WEB — CORRODED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CORROSION ON THE SHIELD WEB BS 767 - 792, RBL 21, WL 156.1. REPLACED THE SHIELD WEB IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 146A0081, SHEET 49, REV A.

Part: WEB — CORRODED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CORROSION WEB - INTERCOSTAL BTW BS 747 - 767, STR 25R, WL 156.4. REPLACED THE WEB - INTERCOSTAL IAW 51-40-02, AND DWG 146A7502, SHEET 50, REV-.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK ON ANGLE LOCATED BS 867, STRINGER 26L, WL 156.1. REPLACED THE ANGLE IAW SRM 51-10-02-0G, SRM 51-40-02-0G-0, AND DWG 149A8102, SHEET 19, REV A. MEASURE OF CRACK: 0.833 INCHES.

Part: FITTING — DETERIORATED (GIRT BAR) · airframe 39,409 hrs · 19,063 cycles

DETERIORATED GIRT BAR FITTING HARDWARE AND SHIMS FWD ENTRY AND SERVICE DOOR. REPLACED GIRT BAR FITTING HARDWARE AND SHIMS. INSTALLATION WILL BE ACCOMPLISHED ON TTG8R008CEXW STEP 13.

Part: WEB — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK ON WEB BTW BS 927 TO BS 947.5, STRINGER 25R. REPLACED THE WEB IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G, AND DWG 147A7500, SHEET 20, REV -.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CORROSION ON SUPPORT ANGLE, BTW BS 767 - 792, RBL 21, WL 156.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 146A8123, SHEET 16, REV -.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACK ON THE FLOORBEAM LOCATED BS 540 BTW LBL 0 TO LBL 24.75, WL 208.1. REPLACED FLOORBEAM IAW SRM 51-10-02-0G, ITEM 9, SRM 51-40-02-0G, AND DWG 143A0060, SHEET 64, REV -.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CORROSION SUPPORT ZEE, BTW BS 727F - 767, STRINGER 25R, WL 156.4. REPLACED SUPPORT ZEE IAW SRM 51-10-02-0G, ITEM 9, SRM 51-40-02-0G, SRM 53-00-53-2R-6, REPAIR 6, DWG 146A7500, SHEET 233, REV-, DWG 146A7502, SHEET 50, REV-.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK ON FWD CORNER OF SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.

Part: WEB — CORRODED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CORRODED WEB BTW BS 927 - 947.5, LBL 3, WL 156.1. WEB CLASSIFIED AS PRIMARY-OTHER IAW SRM 51-00-04. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 147A7500; SHEET 38; REV -.

Part: FITTING — DETERIORATED (ZONE 800) · airframe 39,409 hrs · 19,063 cycles

DETERIORATED GIRT BAR FITTINGS HARDWARE AND SHIMS ENTRY AND SERVICE DOOR. REPLACED GIRT BAR FITTINGS HARDWARE AND SHIMS ENTRY AND SERVICE DOOR AT AFT GALLEY AREA IAW AMM 25-66-02-400-801,

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACK INDICATION ON STUB FRAME, BETWEEN BS 294.5 - 296.5, BTW S8R TO S9R. LENGTH OF CRACK; 0.312 IN. REPLACED THE STUB FRAME AND FASTENERS IAW SRM 51-40-02, DWG 141A8370, SHEET 9, SHEET 10, REV D.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CRACK FLOOR SUPPORT BTW BS 277 TO 294.5, BL 0. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02. MEASUREMENT OF THE CRACK IS 1.0675 INCHES.

Part: SUPPORT BEAM — CRACKED (ZONE 600) · airframe 39,409 hrs · 19,063 cycles

CRACK TRAILING EDGE DEFLECTION CONTROL RIB SUPPORT BEAM AT RT WING. PERFORMED PERMANENT REPAIR ON TRAILING EDGE DEFLECTION CONTROL RIB SUPPORT BEAM AT RT WING IAW SRM 57-51-02-2R-3

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACKED FLOOR SUPPORT BTW BS 312 - 328 LBL 46 IN THE FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, ITEM 9 & DWG 141A5400, SHEET 26, REV -.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACKED FLOOR SUPPORT BTW BS 344 - 360, BL 0. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A5400, SHEET 32, REV -.

Part: STRAP — CORRODED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CORROSION ON EXITING REPAIR LOCATED BS 986.5 RBL 17 WL 208.1 AT AFT GALLEY AREA. REPLACED REPAIR STRAP AND FASTENERS LOCATED BS 986.5 RBL 10 TO RBL 22 WL 208.1 AT AFT GALLEY AREA IAW SRM 53-70-51-2R-6.

Part: PLATE — CORRODED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CORROSION ON PLATE, BS 1016 PLUS 5 INCHES, LBL 4, WL 208.1. REPLACED THE PLATE IAW SRM 51-40-02, AND DWG 147A5700, SHEET 122, REV A.

Part: SUPPORT BEAM — CRACKED (ZONE 500) · airframe 39,409 hrs · 19,063 cycles

CRACK DEFLECTION CONTROL RIB SUPPORT BEAM TRAILING EDGE AT LT WING. PERFORMED PERMANENT REPAIR ON DEFLECTION CONTROL RIB SUPPORT BEAM TRAILING EDGE AT LT WING IAW SRM 57-51-02-2R-3.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 39,409 hrs · 19,063 cycles

CRACK ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B LBL49 AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR LOCATED ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B LBL49 AT AFT CARGO COMPARTMENT IAW SRM 51-70-11-2R-0.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

CORROSION ON FLOORBEAM LOCATED BS 986.5 LBL44 WL 208.1 AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR PART STRAP, ANGLE AND FILLER ON FLOORBEAM LOCATED BS 986.5, LBL 44, WL 208.1 AT AFT GALLEY AREA IAW SRM 51-40-02, AND SRM 53-70-51-2R-6, REPAIR 6.

Part: LIGHT — BURNED OUT (ZONE 200) · airframe 39,409 hrs · 19,063 cycles

BURNED SEGMENT WINDOW EMERGENCY LIGHT ON DOOR 833 AT PASSENGER CABIN. REPLACED WINDOW EMERGENCY LIGHT ON DOOR 833 AT PASSENGER CABIN IAW AMM 33-21-00-960-805. PERFORMED OPS TEST. TESTED OK.

Part: STRAP — CORRODED (ZONE 600 LE) · airframe 39,409 hrs · 19,063 cycles

CORROSION ON OUTER WING LEADING EDGE LOWER ATTACH STRAP AT OSS 65 RT WING. OBTAINED OK TO INSTALL NUT PLATE ON OUTER WING LEADING EDGE LOWER ATTACH STRAP LOC AT OSS 65 ON RT WING. REPAIRED RH WING - O/B FIXED LEADING EDGE - ATTACH STRAP OUTBOARD - BETWEEN TRACE OSS 26.94 & OSS 109.69 IAW EA 25-157-02897 AND SRM 51-40-02 ; DWG112A4401 SHEET 55 REV A.

Part: TIRE — FAILED (ZONE 700) · airframe 39,100 hrs · 18,903 cycles

LEFT NOSE GEAR TIRE FAILED ON T/O. NO ABNORMAL ENGINE INDICATION NOTED. NO SMELL IN CABIN. PERFORMED CONDITIONAL INSPECTION 05-51-54 TIRE TREAD LOSS OR TIRE BURST REF. TTG8Q0156579 FOR REPLACEMENT OF NOSE TIRES. PERFORMED BIRD-HAIL STRIKE CONDITIONAL INSPECTION IAW AMM 05-51-18. REF. TTG8Q0156FEF FOR DAMAGED FAN BLADES.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 38,809 hrs · 18,751 cycles

AFT. AIRCRAFT LEFT EMERGENCY FLASHLIGHT INOP.<[01] R/R FLASHLIGHT BATTERY IAW MM 25-64-00 .

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 38,650 hrs · 18,666 cycles

CREW REPORTS, FWD MEGAPHONE INOPERATIVE. R & R MEGAPHONE BATTERIES IAW AMM 25-64-00.

Part: LIGHT — OUT OF POSITION (ZONE 200) · airframe 38,434 hrs · 18,553 cycles

PIECE OF PLASTIC ON FLOOR NEXT. TO ROW 1 CAPTAIN SIDE STICKING UP<[01] RETAPED PHOTOLUMINESCENT STRIP ON CAPT SIDE IAW SIP

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 38,140 hrs · 18,397 cycles

FWD ENTRY AND FWD GALLEY EMERGENCY EXIT SIGNS INOP<[01] REMOVED AND REPLACED M01675 EMERGENCY LIGHT BATTERY PACK AND CHARGER PER AMM 33-51-06.

Part: HANDLE — LOOSE (ZONE 800) · airframe 38,069 hrs · 18,356 cycles

R1 DOOR LINER ASSIST HANDLE LOOSE<[01] SECURED LOOSE R1 DOOR LINER ASSIST HANDLE IAW B737-800 AMM TASK 25-21-31-420-802.;[02] VERIFIED SECURED LOOSE R1 DOOR LINER ASSIST HANDLE IAW B737-800 AMM TASK 25-21-31-420-802.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 38,069 hrs · 18,356 cycles

L1 DOOR EMERGENCY LIGHT'S INOP (OVERHEAD AND LOWER EXIT LIGHT)<[01] REMOVED AND REPLACED 1 EA BATTERY PACK M1675 (OVER L1 DOOR) AND OPS CHECK GOOD IAW SWA B737-800 AMM 33-51-06-960-805.;[02] VERIFIED REMOVED AND REPLACED 1 EA BATTERY PACK M1675 (OVER L1 DOOR) AND OPS CHECK GOOD IAW SWA B737-800 AMM 33-51-06-960-805.

Part: BULB — BURNED OUT (ZONE 200) · airframe 38,002 hrs · 18,321 cycles

BOTH FWD OVERWING EXIT LOWER IDENTIFIERS HAVE BURNED OUT BULBS<[01] RE-LAMPED AND PERFORMED GOOD OPS CHECK OF BOTH FWD OVERWING EXIT LOWER IDENTIFIERS BULBS PER AMM 33-51-01-960-801

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 38,002 hrs · 18,321 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATT PACK M1673 ARE INOP<[01] REMOVED EMERGENCY EXIT BATTERY PACK M1673 AND INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805;[02] VERIFIED TASK C/W

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 38,002 hrs · 18,321 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATT PACK M1671 ARE INOP<[01] REMOVED EMERGENCY EXIT BATTERY PACK M1671 AND INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805;[02] VERIFIED TASK C/W

Part: SIGN — DETACHED (ZONE 200) · airframe 37,800 hrs · 18,216 cycles

ISLE EMERGENCY SIGN DETACHED. <[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-03-960-803-NG (EMERGENCY AISLE LIGHT (EAL) - LENS REPLACEMENT - PERMANENT)].

Part: TAIL CONE — ELONGATED (ZONE 500) · airframe 37,336 hrs · 17,977 cycles

NUMBER THREE AFT FLAP FAIRING HAS THREE ELONGATED FASTENER HOLES THAT ATTACH THE AFT TAIL CONE <[01]. REMOVED AND REPLACED THE #3 AFT FLAP FAIRING IAW AMM 27-51-18.;[02] REMOVED AND REPLACED THE #3 AFT FLAP FAIRING IAW AMM 27-51-18.;[03] REMOVED AND REPLACED THE #3 AFT FLAP FAIRING IAW AMM 27-51-18.

Part: COVER — OUT OF ADJUST (ZN 800 DOOR) · airframe 36,424 hrs · 17,480 cycles

LEFT FORWARD AND AFT SLIDE SIGHT COVERS LOOSE<[01] SECURED BOTH SLIDE SIGHT COVERS PER SIP.

Part: SIGN — LOOSE (ZONE 200) · airframe 35,859 hrs · 17,149 cycles

CABIN CEILING OWE EMERGENCY EXIT SIGN IS LOOSE<[01] ADJUSTED CABIN CEILING OWE EMERGENCY EXIT SIGN AS REQUIRED REFERENCING AMM 33-51-01.

Part: ENGINE — FAILED (NR 1) · airframe 34,394 hrs · 16,381 cycles

#1 ENGINE FAILURE DURING TO. REJECTED TO AT 135 KNOTS. SEVERE DAMAGE IN TURBINE SECTION FOUND ON POST FLIGHT. BOTH FIRE BOTTLES WERE DISCHARGED AFTER FIRE CREW REPORTED FLAMES IN TURBINE SECTION<[01] REMOVED AND REPLACED #1 ENGINE PER MT 771-00-01; REF: TTG8Q008QADY<BR><BR>REMOVED AND REPLACED BOTH ENGINE FIRE BOTTLES PER AMM 26-21-01; REF: TTG8Q00SKARH;[02] C/W RII REQUIREMENTS FOR THIS TASK

Part: HANDLE — BROKEN (DOOR ASSIST) · airframe 34,263 hrs · 16,310 cycles

FWD SERVICE DOOR INNER PLASTIC ASSIST HANDLE BROKE<[01] R&R. FWR SERVICE DOOR INNER PLASTIC ASSIST HANDLE<BR>REF AMM 52-41-00

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 33,603 hrs · 15,943 cycles

EMERGENCY LIGHTS INOP AT R/H OVERWING EXIT DOOR BOTH UPPER PANELS; SECOND DOOR LOWER LIGHT; AND FWD EXTERNAL LIGHT.<[01] R&R'D BATTERY PACK LOCATED AT R/H SIDEWALL AT ROW 13DEF; OP CK GOOD IAW AMM 33-51-06.;[02] VERIFIED R&R'D BATTERY PACK LOCATED AT R/H SIDEWALL AT ROW 13DEF; OP CK GOOD IAW AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 33,603 hrs · 15,943 cycles

CABIN EMERGENCY LIGHTS ON OVHD BIN BULLNOSE(VALANCE) INOP AT 5ABC; 8ABC; 12ABC; 16ABC; 19ABC AND 23ABC<[01] R&R'D BATTERY PACK LOCATED AT L/H SIDEWALL AT ROW 20ABC; OP CK GOOD IAW AMM 33-51-06.;[02] VERIFIED R&R'D BATTERY PACK LOCATED AT L/H SIDEWALL AT ROW 20ABC; OP CK GOOD IAW AMM 33-51-06

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 33,603 hrs · 15,943 cycles

CABIN EMERGENCY LIGHTS ON OVHD BIN BULLNOSE(VALANCE) INOP AT 7DEF; 10DEF; AND 14DEF.<[01] R&R'D BATTERY PACK LOCATED AT R/H SIDEWALL AT ROW 7DEF; OP CK GOOD IAW AMM 33-51-06.;[02] VERIFIED R&R'D BATTERY PACK LOCATED AT R/H SIDEWALL AT ROW 7DEF; OP CK GOOD IAW AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 33,603 hrs · 15,943 cycles

EMERGENCY LIGHTS INOP AT L/H OVERWING EXIT DOOR(#2) LOWER(INNER) AND THREE EXTERNAL LIGHTS(2 AT DOOR 1 AT WING-TO-BODY T/E)<[01] R&R'D BATTERY PACK LOCATED AT L/H SIDEWALL AT ROWS 7ABC AND 13ABC; OP CK GOOD IAW AMM 33-51-06.;[02] VERIFIED R&R'D BATTERY PACK LOCATED AT L/H SIDEWALL AT ROWS 7ABC AND 13ABC; OP CK GOOD IAW AMM 33-51-06.

Part: FLAP — DEBONDED (ZN 600 RIGHT WIN) · airframe 33,603 hrs · 15,943 cycles

RIGHT WING AFT FLAP INBOARD LOWER SIDE HAS A REPAIR AND THE METAL BOND OF THE REPAIR IS DISBONDED; AND THE TOP HAS A DELAMINATED ON THE OPPOSITE SIDE.<[01] REMOVED AND REPLACED RH OTBD AFT FLAP. IAW AMM 27-51-22 STEP A-F;[02] VERIFIED THE REMOVAL AND REPLACEMENT OF RH OTBD AFT FLAP. IAW AMM 27-51-22 STEP A-F. NO DEFECT. (RII);[03] RII- INSPECTED AS REQUIRED

Part: WEB — CRACKED (ZN 400 NACELLE/P) · airframe 33,603 hrs · 15,943 cycles

#2 ENGINE O/B FAN COWL OIL DOOR LOWER REINFORCEMENT WEB IS CRACKED.<[01] REPLACED WEB PER SRM 51-10-02 & SRM 51-40-02.;[02] C/W;[03] INSPECTED AS REQUIRED

Part: LIGHT — DAMAGED (ZN 200 FUS TOP) · airframe 33,603 hrs · 15,943 cycles

THE CEILING LIGHT BULLNOSE ON TOP OF OVERHEAD BIN 17DEF AND 18DEF IS DAMAGED.<[01] REMOVED AND REPLACED CELING LIGHT BULLNOSE PANEL PER AMM 25-21-71 AND OPS CHECK EMERGENCY LIGHT OK PER 33-51-03.

Part: WEB — CHAFED (ZN 200 FUS TOP) · airframe 33,603 hrs · 15,943 cycles

FLIGHT COMPARTMENT FLOOR STRUCTURE WEB HAS CHAFFING AT STA. 259.5-3; LBL 10. (MARKED)<[01] REPAIRED PER EA # M-153-00734.

Part: SLAT — DELAMINATED (ZN 600 RIGHT WIN) · airframe 33,603 hrs · 15,943 cycles

#8 SLAT T/E WEDGE LOWER SURFACE HAS A DELAM 4' FROM TOP 1' FROM O/B EDGE.<[01] REMOVED #8 SLAT IN REF TO AMM 27-81-21.;[02] OK TO INSTALL NEW #8 SLAT.;[03] INSTALLED NEW #8 SLAT PER M/M REF. 27-81-21.;[04] RII INSPECTION C/W FOR CA #3

Part: TAB — CRACKED (ZN 600 RIGHT WIN) · airframe 33,603 hrs · 15,943 cycles

R/H WING INBD FIXED T/E UPPER PANEL BULB SEAL WEB ATTACH TAB CRACKED AT DEFLECTION CONTROL RIB . PICTURE ATTACHED<[01] REMOVED AND REPLACED R/H WING INBD FIXED T/E UPPER PANEL WEB ATTACH TAB PER SRM 51-4-02.;[02] REMOVED AND REPLACED R/H WING INBD FIXED T/E UPPER PANEL WEB ATTACH TAB PER SRM 51-4-02. INSPECTION C/W.

Part: TAB — CRACKED (ZN 600 RIGHT WIN) · airframe 33,603 hrs · 15,943 cycles

R/H WING T/E AT APROX ORSS 261 CANNON PLUG DISCONNECT BRACKET MOUNT WEB TAB CRACKED AT RIB . PICTURE ATTACHED INFO: PART REQUIRED IS MPN 287A9152-98. NOT IN MAINTENIX SUBMITTED PAR APP DCN-038641. BOB W. 33000<[01] REMOVED R/H WING T/E AT APROX ORSS 261 CANNON PLUG DISCONNECT BRACKET MOUNT WEB TAB 'L' ANGLE IAW SRM 51-40-02.;[02] INSTALLED R/H WING T/E AT APROX ORSS 261 CANNON PLUG DISCONNECT BRACKET MOUNT WEB TAB PER SRM 51-40-02.;[03] UPDATED TO CHANGE RII VALUE IN MEASUREMENT FIELD TO 'NO'

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 33,603 hrs · 15,943 cycles

AFT CARGO COMPARTMENT; L/H SIDEPLATE/ TRANSITION ANGLE CRACKED AT STA. 767+3; LBL 24.<[01] CUT OUT DAMAGED SECTION L/H TRANSITION ANGLE FROM STA.747+11 TO STA. 787+11 PER SRM 53-00-53-REPAIR 5.;[02] FABRICATED REPAIR PARTS;LOCATED AND DRILLED; ALODINE AND PRIMED. PER SRM 53-00-53-REPAIR 5.;[03] INSTALLED BONED NUTPLATES PER SRM 53-00-53-REPAIR 5. AT 17;00 DEC/14/2023;[04] O.K TO INSTALL REPAIR PARTS.;[05] VERIFIED CORRECTIVE ACTION STEPS #1; #2; #3 AND #4 (OK TO INSTALL REPAIR PARTS.);[06] INSTALLED FABRICATED REPAIR PARTS L/H TRANSITION ANGLE FROM STA. 727J+11 TO STA. 787+11 PER SRM 53-00-53-2R-5 REPAIR 5.;[07] CUT OUT DAMAGED SECTION L/H TRANSITION ANGLE FROM STA.727J+11 TO STA. 787+11 PER SRM 53-00-53-REPAIR 5.;[08] REMOVED; FABRICATED AND INSTALLED FABRICATED REPAIR PARTS; L/H TRANSITION ANGLE FROM STA. 727J+11 TO STA. 787+11 PER SRM 53-00-53-2R-5 REPAIR 5. SEE CORRECTIVE ACTIONS FOR INDIVIDUAL SIGN OFFS.;[09] VERIFIED; C/W REMOVED; FABRICATED AND INSTALLED FABRICATED REPAIR PARTS; L/H TRANSITION ANGLE FROM STA. 727J+11 TO STA. 787+11 PER SRM 53-00-53-2R-5 REPAIR 5.

Part: FLOOR SUPPORT — CRACKED (ZN 200 FUS TOP) · airframe 33,603 hrs · 15,943 cycles

PASSENGER CABIN FLOOR SUPPORT IS CRACKED IN 2(EA) PLACES NEAR FASTENER. BS 540 RBL 1<[01] REMOVED AND REPLACED PASSENGER CABIN FLOOR ASSEMBLY SUPPORT AT STA 540 RBL 1 PER SRM 51-40-02.;[02] REMOVED AND REPLACED PASSENGER CABIN FLOOR ASSEMBLY SUPPORT AT STA 540 RBL 1 PER SRM 51-40-02. RII INSPECTION C/W.

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 33,603 hrs · 15,943 cycles

FWD ENTRY DOOR SLIDE BOX GIRT BAR RETAINER CLIP HAS 2 EA. LOOSE RIVETS<[01] SECURED 2EA FASTENERS ON FWD GIRT BAR BRACKET PER SRM 51-40-02.;[02] C/W;[03] INSPECTION C/W

Part: PANEL — CORRODED (ZN 600 RIGHT WIN) · airframe 33,603 hrs · 15,943 cycles

R/H WING FUELING SERVICE PANEL FUEL QUANTITY GUAGES BRACKET HAS AREAS OF SURFACE CORROSION. MRKD<[01] REMOVED AND REPLACED R/H WING REFUELINGF PANEL AND OPS CHECKS GOOD PER MM 28-41-61

Part: BEAM — WORN (R/H WING) · airframe 27,330 hrs · 12,353 cycles

A-061 R/H WING DEFLECTION CONTROL RIB UPPER TAB AND SUPPORT BEAM WORN AT 2 EA FASTENER HOLES ; / [01] EVALUATED WEAR - DEFLECTION CONTROL RIB UPPER TAB LOSS OF .051'; MAX ALLOWED .040' OUT OF LIMITS<BR>EVALUATED WEAR - SUPPORT BEAM ORIGINAL THICKNESS .090' LOSS OF .015' REMAINING .075' OUT OF LIMITS IAW SRM 57-51-02-1A-1 SECTION 4.D; FIGURE 108 DETAIL C AND FIGURE 108 DETAIL G.<BR>TOOL# AAR-27214 CAL DUE 08/31/22 AAR-31793 CAL DUE 11/04/22.; [02] REMOVED I/B AND O/B SERRATED PLATES IAW SRM 57-51-02-2R-4 SECTION 4.B; [03] CUT AND REMOVED DAMAGE FROM DEFLECTION CONTROL RIB UPPER TAB IAW SRM 57-51-02-2R-4 SECTION 4.E; [04] VERIFIED STEPS 1 THRU 3 C/W; [05] CUT AND REMOVED DAMAGE FROM SUPPORT BEAM IAW SRM 57-51-02-2R-1 SECTION 4.B; [06] VERIFIED STEP 5 C/W; [07] VERIFIED MATERIAL 7075-T6 .100' ATAG A39363 IAW SRM 57-51-02-2R-4 TABLE 201.; [08] VERIFIED STEP 7 C/W; [09] ACCOMPLISHED CRACK CHECK IAW B737 NDT P6 51-00-00 P23 TOOL 36303 DUE 13APR22 NO CRACKS NOTED; [10] RECEIVED -1 (O/B) DOUBLER FROM BACK SHOP W/O# 43073-6000-0001 IAW SRM 57-51-02-2R-4 TABLE 201.<BR>RECEIVED -1 (I/B) DOUBLER FROM BACK SHOP W/O# 43073-6000-0002 IAW SRM 57-51-02-2R-1 TABLE 201.; [11] LOCATED; DRILLED AND FABRICATED REPAIR PARTS IAW SRM 57-51-02-2R-1 SECTION 4.D-H AND SRM 57-51-02-2R-4 SECTION 4.I-M; [16] INSTALLED REPAIR PARTS I.A.W SRM 57-51-02-2R-4 AND SRM 57-51-02-2R-1;

Part: ANGLE — CRACKED (R/H WING) · airframe 27,330 hrs · 12,353 cycles

A-061 R/H WING UPPER FIXED TRAILING EDGE PNL JUST OUTBD OF #7 GROUND SPOILER ATTACH ANGLE CRACKED ; / [01] REMOVED ATTACHED ANGLE I.A.W SRM 51-40-02-0G-0; [02] VERIFIED NEW ATTACH ANGLE PART # 115A2156U8 ATAG: A111293 IAW DWG # 115A2512 REV:-; [03] VERIFIED STEPS 1 AND 2; [04] LOCATED AND DRILLED NEW ATTACH ANGLE IAW SRM 51-40-05; [05] VERIFIED STEP 4 C/W<BR><BR>OK TO INSTALL NEW ATTACH ANGLE; [06] INSTALLED NEW ATTACH ANGLE AT R/H WING UPPER FIXED TRAILING EDGE PNL OUTBD OF # 7 GROUND SPOILER IAW SRM 51-40-02 AND DWG # 115A2512 REV:-; [07] REMOVED AND REPLACED NEW ATTACH ANGLE AT R/H WING UPPER FIXED TRAILING EDGE PNL OUTBD OF # 7 GROUND SPOILER IAW SRM 51-40-02 AND DWG # 115A2512 REV:-; [08] ALL WORK C/W<BR>AUDIT C/W

Part: LIGHT — INOPERATIVE · airframe 27,330 hrs · 12,353 cycles

ALL EMERGENCY LIGHTS POWERED BY BATTERY PACK AT M1675 (STA 317 LBL 10) ARE INOP ; / [01] REPLACED BATTERY PACK M1675; OPS CHECK GOOD IAW AMM 33-51-06-960-805.; [02] VERIFIED STEP 1<BR>AUDIT CW

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

R/H CABIN R1 DOOR CREASE BEAM O/B ATTACH ANGLE CORRODED ; / [01] REMOVED CORROSION FROM ATTACH ANGLE AND VERIFIED MATERIAL LOSS ( FOUND OUT LIMITS THICKNESS REMOVED MORE THAN 50% ) IAW SRM 53-10-15-1A-2.; [02] REMOVED ATTACH ANGLE IAW SRM 53-10-15-1A-2: SRM 51-40-02-OG-0; [03] VERIFIED ITEMS 1 & 2; [04] VERIFIED NEW ATTACH ANGLE P/N 141A8312-5 TAG # WN6861 IAW DWG 141A8310 REV.-; [05] VERIFIED STEP 4 IS COMPLETE; [06] VERIFIED STEP 4; [07] LOCATED DRILLING HOLES AND INSTALLED NUT PLATES ON NEW ATTACH ANGLE IAW SRM 51-40-05 ; 51-40-02; [08] VERIFIED STEP 7 IS COMPLETE; [09] VERIFIED STEP 7; [10] OK TO INSTALL; [11] INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-02 AND DWG 141A8310 REV.-; [12] VERIFIED STEP 11 IS COMPLETE; [13] VERIFIED STEP 11 C/W. OK TO CIC; [14] APPLIED CORROSION INHIBITING COMPOUND IAW AMM 51-21-91-620-802; [15] VERIFIED STEP 14 IS COMPLETE; [16] COMPLETED PARTS INSTALL INFO; [17] VERIFIED STEP 14 COMPLETE. AUDITED.

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 27,330 hrs · 12,353 cycles

A-061 DOT 024. AFT CARGO PIT THRESHOLD WEB STA 787+8' TO STA 827+19' RBL 25 W/L 155 HAS SEVERAL SPOTS OF CORROSION (MARKED) ; / [01] UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .050'; LOSS .008'; REMAINING .042'. TOOL#40084; DUE 11AUG22; [02] REMOVED CORROSION IAW SRM 51-10-02 AND VERIFIED WITH 1X MAG. ORIG MAT THICKNESS .050 LOSS OF .008 WITH .042 REMAINING IS OUT OF LIMITS IAW SRM 53-60-15-1A-1; [03] VERIFIED STEP 2; [04] REMOVED AFT PIT THRESHOLD WEB IAW SRM 51-40-02 VERIFY NEW WEB P/N 146A8123-25 ATAG WN6549 IAW BOEING DWG 146A8120 REV A; [05] VERIFIED STEP 4 IS COMPLETE; [06] VERIFIED STEP 4; [07] DRILLED AND C/S NEW WEB I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 146A8120 REV:A; [08] DRILLED NEW WEB I.A.W SRM 51-40-05-0G-0 NOT SRM 51-40-02-0G-0; [09] VERIFIED STEPS 7 AND 8; [10] INSTALLED NUTPLATES TO NEW WEB I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 146A8120 REV:A; [11] APPLIED C.I.C TO WEB AND LOWER DOOR SURROUND I.A.W<BR>MM 51-21-91-620-802; [12] VERIFIED ITEMS 10 AND 11. OK TO INSTALL; [13] STARTED INSTALLING WEB I.A.W SRM 51-40-02-0G-0 AND <BR>BOEING DWG 146A8120 REV:A; [14] VERIFIED ITEM 13; [15] REMOVED AND REPLACED AFT PIT THRESHOLD WEB STA 787+8'-827+19' RBL 25 IAW SRM 51-40-02; [16] OUT OF SEQUENCE; COMPLETED INSTALLATION OF LOWER SILL WEB I.A.W SRM 51-40-02-0G-0 AND <BR>BOEING DWG 146A8120 REV:A; [17] VERIFIED STEPS 15&16; [18] AUDIT CW

Part: SHIELD — CORRODED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE SHIELD; STA 767+10 TO 792; RBL 20; WL 156 UPPER AND LOWER SURFACE HAS CORROSION. A224-22 ; / [01] REMOVED CORROSION IAW SRM 51-10-02 AND VERIFIED WITH 10X MAG. ORIGINAL MATERIAL THICKNESS .050 LOSS OF .008 WITH .042 REMIANING IS OUT OF LIMITS IAW SRM 53-60-15-1A-1 AAR TOOL #33649 CAL DUE 12AUG22; [02] VERIFIED; [03] REMOVED AFT CARGO COMPARTMENT FLOOR STRUCTURE SHIELD AT STA. 767+10 TO 792 RBL20. I.A.W. SRM 51-40-02-0G-0. WORK ACCOMPLISHED BY AAR 12025; [04] VERIFY NEW PART NUMBER 146A8127U12ATSMRO. A-TAG WN11956 I.A.W. DRAWING 146A0081. WORK ACCOMPLISHED BY AAR 12025; [05] VERIFIED STEP 3 AND 4; [06] OK TO INSTALL NEW FWD SHIELD; [07] REMOVED AND REPLACED AFT PIT FWD SHIELD STA 767+10-792 RBL 20 IAW SRM 51-40-02; [08] VERIFIED STEP 7; [09] AUDIT CW

Part: ATTACH ANGLE — CRACKED (FWD CARGO BAFFLE) · airframe 27,330 hrs · 12,353 cycles

FWD CARGO COMPARTMENT BAFFLE ATTACH CLIP BELOW Z-ANGLE IS CRACKED; FWD OF STA 500H FRAME; LBL25. REMOVED CRACKED BAFFLE CLIP BELOW Z-ANGLE IAW SRM 51-40-02-0G-0. LOCATED & DRILLED HOLES IAW SRM 51-40-05-0G-0 & DWG 143A7505 REV-. REMOVED & REPLACED BAFFLE ATTACH CLIP IAW SRM 51-40-02.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 27,330 hrs · 12,353 cycles

FWD CARGO COMPARTMENT BAFFLE ATTACH CLIP BELOW Z-ANGLE IS CRACKED; FWD OF STA 500H FRAME; RBL25. REMOVED THE CRACKED BAFFLE CLIP BELOW Z-ANGLE IAW SRM 51-40-02-0G-0. LOCATED & DRILLED HOLES IAW SRM 51-40-05-0G-0 AND DWG 143A7505 REV-. INSTALLED BAFFLE CLIP IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV-.

Part: ANGLE — CRACKED (CENTER WING) · airframe 27,330 hrs · 12,353 cycles

CUSTOMER REQUEST: RIGHT HAND PACK BAY HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 RBL 10 IS CRACKED AT FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. ; / [01] REMOVED DAMAGED SECTION OF ANGLE AND PERFORMED DVI OF REPAIR AREA; NO DEFECTS NOTED IAW SRM 57-10-10-2R-5; [02] VERIFIED NEW -1 REPLACEMENT ANGLE FABRICATED ON BACK SHOP W/O 43073-0000-0001 AND -2 SPLICE ANGLE FABRICATED ON BACK SHOP W/O 43073-0000-0002 IAW SRM 57-10-10-2R-5; [03] VERIFIED STEP 1; [04] VERIFIED STEP 2; [05] VERIFIED ITEMS 1 THROUGH 4.<BR>NO DEFECTS NOTED; [06] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTED. TOOL#36303; DUE 13APR22; [07] COMPLETED FABRICATION OF -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE IAW SRM 57-10-10-2R-5; [08] VERIFIED STEP 7; [09] VERIFIED ITEM 7 AND 8<BR>OK TO TREAT AND PRIME; [10] TREATED AND PRIMED REPAIR PARTS IAW SRM 57-10-10-2R-5; [11] VERIFIED STEP 10; [12] VERIFIED ITEMS 10 AND 11; [13] OK TO INSTALL; [14] COMPLETED INSTALLATION OF ALL REPAIR PARTS; APPLIED CAP SEAL TO TANK FASTENERS; AND PERFORMED GOOD BOND CHECK IAW SRM 57-10-10-2R-5<BR>TOOL #34006 CAL. DUE: 12/30/2022; [15] VERIFIED STEP 14 IS COMPLETE; [16] FILLET SEALED REPAIR PARTS AND APPLIED CIC TO REPAIR AREA IAW SRM 57-10-10-2R-5; [17] VERIFIED STEP 16; [18] VERIFIED ITEM 14; [19] VERIFIED ITEM 16; [20] PERFORMED LEAK CHECK OF REPAIR IAW B737 AMM 28-11-790-801. LEAK CHECKS GOOD; [21] STEP 20 C/W; [22] VERIFIED STEP IS COMPLETE; [23] AUDIT C/W

Part: FLOOR PANEL — DAMAGED (CABIN FLOOR) · airframe 27,330 hrs · 12,353 cycles

A-061 DOT 017. CABIN FLOORBOARD 221AF R/H OUTBD EDGE DAMAGED ; / [01] EVALUATED AND FOUND EDGE DAMAGE WITH DAMAGED FIBERS TO UPPER FACE SHEET AND REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 PARAGRAPH 3A;B;C;D;E;F<BR>POTTED CORE AT EDGE IAW SRM 53-00-50-2R-1 PARAGRAPH 3G;H;I;J POTTING COMPOUND--EPOCAST1619 (A101798)<BR>VERIFIED REPAIR MATERIALS AS REPAIR PLIES--BMS9-3 TYH3 (A10273); RESIN--EPOCAST 50A1/9816 (A102321) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND; [02] STEP 1 OK. OK TO BOND; [03] BONDED REPAIR PLIES; CURED 3.5 HOURS AT 150 DEGREES; TAP TEST GOOD IAW SRM 53-00-50-2R-1 PARAGRAPH 3K;L;M. OVEN-- B0-06 DUE 2-19-22<BR>INSTALLED 2 EACH INSERTS IN REPAIR AREA IAW SRM 53-00-50-2R-1 PARAGRAPH 3N AND SRM 51-00-50-2R-0 REPAIR GENERAL PARAGRAPH 5S. (A74302) (A35422) (90028); [04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL. TAP TEST GOOD

Part: FLOOR PANEL — BROKEN (CABIN FLOOR) · airframe 27,330 hrs · 12,353 cycles

A-061 DOT 015. CABIN FLOORBOARD 221BF AFT INBD CORNER TIP BROKE ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER AND LOWER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 53-00-50-2R-1 PARAGRAPH 3A;C;E;F<BR>VERIFIED REPAIR MATERIALS AS-- REPAIR PLIES--BMS9-3TYH3 (A10273); RESIN--EPOCAST 50A1/9816 (A102321) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND; [02] STEP 1 OK. OK TO BOND; [03] BONDED REPAIR PLIES; CURED 3.5 HOURS AT 150 DEGREES; TAP TEST GOOD IAW SRM 53-0-50-2R-1 PARAGRAPH 3 K;L;M. OVEN-BO-O6 DUE 2-19-22; [04] REPAIRED DAMAGE TO FLOORBOARD 221BF IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 27,330 hrs · 12,353 cycles

CABIN FLOOR PANEL 231CF; UPPER SURFACE HAS PULLED FACE SHEET PLIES. ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1 <BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3A;C;E;F <BR>VERIFIED REPAIR MATERIALS AS REPAIR PLIES-- BMS9-3TYH3 (A10273); RESIN-- EPOCAST 50A1/9816 (A100514) IAW SRM 53-00-50-2R-1 TABLE 201 <BR>NEED OK TO BOND; [02] STEP 1 OK. OK TO BOND; [03] BONDED REPAIR PLIES; CURED IN OVEN B0-06 DUE 2-19-22; TAP TEST GOOD IAW SRM 53-00-50-2R-1 STEPS 3K;L;M; [04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD; [05] VERIFIED STEPS 3-4; [06] AUDITED

Part: STRIP — CORRODED (AFT CARGO) · airframe 27,330 hrs · 12,353 cycles

DOT#03-186 AFT PIT 2EA RH CAP STRIPS CORRODED ; / [01] REMOVED CORROSION AND VERIFIED WITH 10X MAGINIFIER ALL CORROSION REMOVED IAW SRM 51-10-02-0G-0; [02] LIMITS VERIFIED; OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM<BR>BOTH CAPSTRIPS ARE SAME ORIGINAL THICKNESS AND REMAINING THICKNESS MEASUREMENTS<BR>ORIGINAL THICKNESS .063'<BR>REMAINING THICKNESS .059'<BR>AAR TOOL 36644 DATE 08-20-22; [03] VERIFIED STEPS 1 AND 2; [04] VERIFIED STEPS 1&2; [05] OK TO TREAT AND PRIME.<BR>EA ISSUED FOR REPAIR.; [06] REPAIR ACCOMPLISHED ON EA 22-125-00082-WIPI; [07] SUMMARY EA 22-125-00082 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q00A4LLW.; [08] REMOVED CORROSION FROM AFT CARGO COMPARTMENT AFT CAP STRIPS 2EA. AND REPAIRED IAW EA 22-125-00082; [09] ALL WORK C/W<BR>AUDIT C/W

Part: ANGLE — CORRODED (BS 500A-500E) · airframe 27,330 hrs · 12,353 cycles

FWD CARGO BAY Z-ANGLE CORRODED AT MULTIPLE NUTPLATE HOLES, WL 154, BS 500A+11 - 500E+7, LBL25. REMOVED CORROSION FROM THE Z ANGLE IAW SRM 51-10-02-0G-0. WITHIN LIMITS IAW SRM 53-00-53-1A-2 AND DWG 1496-444. REMOVED .002' OF .040' ORGINAL MATERIAL, .038' REMAINS.

Part: STRIP — CORRODED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

DOT#04-186 AFT PIT LH CAP STRIP #4 CORRODED ; / [01] REMOVED CORROSION AND VERIFIED WITH 10X MAGINIFIER ALL CORROSION REMOVED IAW SRM 51-10-02-0G-0; [02] LIMITS VERIFIED; OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM<BR>ORIGINAL THICKNESS .063'<BR>REMAINING THICKNESS .060'<BR>AAR TOOL 36644 DATE 08-20-22; [03] VERIFIED STEPS 1 AND 2; [04] VERIFIED STEPS 1&2; [05] ''PERFORMED EA 22-125-00082. REF. FAULT TTG8Q00A4LLW''.; [06] ALL WORK C/W<BR>AUDIT C/W

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 27,330 hrs · 12,353 cycles

A-061 DOT 016. CABIN FLOORBOARD 221BF UPPER SURFACE FIBERS PEELING ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 53-00-50-2R-1 PARAGRAPH 3A;C;E;F<BR>VERIFIED REPAIR MATERIALS AS-- REPAIR PLIES--BMS9-3TYH3 (A10273); RESIN--EPOCAST 50A1/9816 (A102321) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND; [02] STEP 1 OK. OK TO BOND; [03] BONDED REPAIR PLIES; CURED 3.5 HOURS AT 150 DEGREES; TAP TEST GOOD IAW SRM 53-0-50-2R-1 PARAGRAPH 3 K;L;M. OVEN-BO-O6 DUE 2-19-22; [04] REPAIRED DAMAGE TO FLOORBOARD 221BF IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD

Part: FLOORBOARD — PULLED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

PASSENGER CABIN FLOORBOARD 241E UPPER SURFACE HAS PULLED FIBERS. A224-10 ; / [01] EVALUATED DAMAGE TO CABIN FLOORBOARD 241E; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1. NO DELAMINATION NOTED.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;E;F; AND I.<BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; FIBERGLASS CLOTH BMS9-3 (A10273); RESIN EPOCAST 50A; (A100514).<BR><BR>REQUIRES OKAY TO BOND REPAIR PLIES.; [02] STEP 1 OK. OK TO BOND; [03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS K;L; AND M AND B737 SRM 53-00-50-2R-0 REPAIR GENERAL. CURED AT 150 DEGREES FOR 4 HOURS; TAP TEST GOOD. THERMOMETER AAR30347 CAL DUE 4/29/22.; [04] REPAIRED PASSENGER CABIN FLOORBOARD 241E IAW B737 SRM 53-00-50-2R-1 PAR 3 AND B737 SRM 53-00-50-2R-0 REPAIR GENERAL.

Part: FLOORBEAM — CORRODED (BS 986 RBL15-18) · airframe 27,330 hrs · 12,353 cycles

A-061 DOT 007. AFT CABIN FLOOR BEAM AT STA 986 RBL 15 TO RBL 18 WL 207 HAS CORROSION AT 2EA FASTENER HOLES LOWER SURFACE ; / [01] REMOVED DAMAGE FROM LOWER SURFACE OF 986 FLOOR BEAM AT 2EA FASTENER HOLES IAW SRM 51-10-02-0G-0.<BR>VERIFIED MATERIAL LOSS; ORIGINAL THICKNESS .150'; LOSS .015' ; REMAINING .135' OUT OF LIMITS IAW SRM 53-70-51-1A-1 FIGURE 104 DETAIL C.<BR>TOOL# AAR-21461 CAL DUE 08/11/22; [02] VERIFIED STEP 1 C/W; [03] ACCOMPLISHED DETAILED VISUAL INSPECTION OF REPAIR AREA NO DEFECTS FOUND IAW SRM 53-70-51-2R-6 SECTION 4.B; [04] VERIFIED MATERIAL 7075-T6 .100' ATAG A39363 IAW SRM 53-70-51-2R-6 TABLE 201.; [05] VERIFIED STEPS 3 AND 4; [06] HFEC IAW B737 NDT PART 6 51-00-00 PROCEDURE 23 AND 16. NO DEFECTS NOTED. TOOL# 40083 DUE 14SEP22; [07] REMOVED ADDITIONAL .002' AND FLAP PEENED BLENDED AREAS IAW SRM 53-70-51-2R-6 SECTION 4.E AND F.;[09] LOCATED; DRILLED AND FABRICATED REPAIR STRAP IAW SRM 53-70-51-2R-6 SECTION 4 G-K.[11] TREATED AND PRIMED REPAIR PARTS AND REPAIR AREA; FILLED BLENDED AREA IAW SRM 53-70-51-2R-6 SECTION 4. L;M;N.; [12] VERIFIED STEP 11<BR><BR>OK TO INSTALL REPAIR PARTS; [13] INSTALLED REPAIR PARTS IAW SRM 53-70-51-2R-6 SECTION 4. O-R.; [14] APPLIED CIC IAW SRM 53-70-51-2R-6 SECTION 4.S; [15] REMOVED DAMAGE FROM LOWER SURFACE OF 986 FLOOR BEAM AT 2EA FASTENER HOLES RBL15-RBL18; VERIFIED MATERIAL LOSS; ORIGINAL THICKNESS .150'; LOSS .015' ; REMAINING .135' OUT OF LIMITS. ACCOMPLISHED REPAIR IAW SRM 53-70-51-2R-6 - SEE ABOVE FOR COMPLETED WORK.

Part: FLOORBOARD — PULLED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

PASSENGER CABIN FLOORBOARD 242RF UPPER SURFACE HAS PULLED FIBERS. A224-15 ; / [01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUIND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201 RESIN (A102321); FABRIC (A10273).<BR><BR>REQUESTING OK TO BOND; [02] VERIFIED AND OK TO BOND; [03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (AAR 30347 EXP 4-29-22). TAP TEST GOOD.; [04] REPAIRED CABIN FLOOR BOARD 242RF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.

Part: FLOORBOARD — PULLED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

PASSENGER CABIN FLOORBOARD 242D UPPER SURFACE HAS PULLED FIBERS. A224-17 ; / [01] VERIFIED PANEL 242D TO HAVE DAMAGE TO UPPER PLIES AND 2 INSERTS DAMAGED. PANEL IS WITHIN LIMITS AND REPAIRABLE I/A/W BOEING 737-800 SRM 53-00-50-2R-0 (REPAIR-1) & SRM 53-00-50-2R-1 STEP(3A) WITH TAP TEST GOOD.; [02] REMOVED 2-EACH INSERTS FROM PANEL 242D I/A/W BOEING 737-800 SRM 53-00-50-2R-1 STEP(3B).; [03] CLEANED; PREPED & APLIED POTTING COMPOUND (A101798) TO PANEL 242D I/A/W BOEING 737-800 SRM 53-00-50-2R-1 STEP(3C;3E;3F;3G).; [04] CURED POTTING COMPOUND ON PANEL 242D I/A/W BOEING 737-800 SRM 53-00-50-2R-1 STEP(3H) & SRM 53-00-50-2R-0 (FIG.208). USING TOOL : AAR-30347 EXP. 29/APR/2022; [05] CLEANED & PREPPED PANEL 242D FOR FIBERGLASS (A10273) & RESIN (E82891) I/A/W BOEING 737-800 SRM 53-00-50-2R-1 STEP(3H;3I;3J); [06] VERIFIED AND OK TO BOND; [07] APPLIED & CURED FIGERGLASS TO PANEL 242D I/A/W BOEING 737-800 SRM 53-00-50-2R-1 STEPS(3J;3K;3L) & SRM 53-00-50-2R-0 (FIG.210) WITH TAP-TEST-GOOD. USING TOOL : AAR-30347 EXP. 29/APR/2022; AAR-5801 EXP. 12/OCT/2022; [08] INSTALLED INSERTS 2-EACH (A35422); 2-EACH (A95094); WITH ADHEASIVE (A65602) ON PANEL 242D I/A/W BOEING 737-800 SRM 53-00-50-2R-1 STEP(3N). TOOL: AAR-30347 EXP.04/APR/2022; [09] REPAIRED PANEL 242D I/A/W BOEING 737-800 SRM 53-00-50-2R-0 & SRM 53-00-50-2R-1.

Part: ATTACH ANGLE — CRACKED (FWD CARGO BAFFLE) · airframe 27,330 hrs · 12,353 cycles

FWD CARGO COMPARTMENT BAFFLE ATTACH CLIP BELOW Z-ANGLE IS CRACKED, FWD OF BS 500G FRAME, RBL 25. REMOVED CRACKED BAFFLE CLIP BELOW Z-ANGLE IAW SRM 51-40-02-0G-0. LOCATED & DRILLED HOLES IAW SRM 51-40-05-0G-0 & DWG 143A7505 REV-. INSTALLED BAFFLE CLIP IAW SRM 51-40-02-0G-0 & DWG 143A7505 REV-.

Part: FLOOR PANEL — CRACKED (CABIN FLOOR) · airframe 27,330 hrs · 12,353 cycles

A-061 DOT 018. CABIN FLOOR BOARD 222CF FACE SHEET CRACKED UPPER SURFACE ; / [01] EVALUATED AND FOUND MULTIPLE AREAS OF DAMAGED FIBERS TO UPPER FACE SHEET AND REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 PARAGRAPH 3A;C;E;F<BR>VERIFIED REPAIR MATERIALS AS REPAIR PLIES--BMS9-3 TYH3 (A10273); RESIN--EPOCAST 50A1/9816 (A102321) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND; [02] STEP 1 OK. OK TO BOND; [03] BONDED REPAIR PLIES; CURED 3.5 HOURS AT 150 DEGREES; TAP TEST GOOD IAW SRM 53-00-50-2R-1 PARAGRAPH 3K;L;M. OVEN-- B0-06 DUE 2-19-22; [04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL. TAP TEST GOOD

Part: ATTACH ANGLE — CRACKED (FWD CARGO BAFFLE) · airframe 27,330 hrs · 12,353 cycles

FWD CARGO COMPARTMENT BAFFLE ATTACH CLIP BELOW Z-ANGLE IS CRACKED; AFT OF STA 500H FRAME; LBL25. A177-016 ; /

Part: ANGLE — CORRODED (BS 500E-500H) · airframe 27,330 hrs · 12,353 cycles

FWD CARGO BAY Z-ANGLE CORRODED AT MULTIPLE NUTPLATE HOLES, WL 154, BS 500E+10 - 500H+16, LBL 25. REMOVED CORROSION FROM FWD CARGO LT Z-ANGLE IAW SRM 51-10-02-0G-0. WITHIN LIMITS IAW SRM 53-00-53-1A-2 AND DWG 1496-444. REMOVED .003' OF .040' ORGINAL MATERIAL .037' REMAINS.

Part: ANGLE — CRACKED (CENTER WING) · airframe 27,330 hrs · 12,353 cycles

CUSTOMER REQUEST: LEFT HAND PACK BAY HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 LBL 10 IS CRACKED AT FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. ; / [01] REMOVED DAMAGED SECTION OF ANGLE AND PERFORMED DVI OF REPAIR AREA; NO DEFECTS NOTED IAW SRM 57-10-10-2R-5; [02] VERIFIED NEW -1 REPLACEMENT ANGLE FABRICATED ON BACK SHOP W/O 43073-0000-0003 AND -2 SPLICE ANGLE FABRICATED ON BACK SHOP W/O 43073-0000-0004 IAW SRM 57-10-10-2R-5; [03] VERIFIED STEP 1; [04] VERIFIED STEP 2; [05] VERIFIED ITEMS 1 THROUGH 4.<BR>NO DEFECTS NOTED; [06] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTED. TOOL#36303; DUE 13APR22; [07] COMPLETED FABRICATION OF -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE IAW SRM 57-10-10-2R-5; [08] VERIFIED STEP 7; [09] VERIFIED ITEM 7 AND 8<BR>OK TO TREAT AND PRIME; [10] TREATED AND PRIMED REPAIR PARTS IAW SRM 57-10-10-2R-5; [11] VERIFIED STEP 10; [12] VERIFIED ITEMS 10 AND 11; [13] OK TO INSTALL; [14] COMPLETED INSTALLATION OF ALL REPAIR PARTS; APPLIED CAP SEAL TO TANK FASTENERS; AND PERFORMED GOOD BOND CHECK IAW SRM 57-10-10-2R-5<BR>TOOL #34006 CAL. DUE: 12/30/2022; [15] VERIFIED STEP 14 IS COMPLETE; [16] VERIFIED ITEM 14 RII; [17] FILLET SEALED REPAIR PARTS AND APPLIED CIC TO REPAIR AREA IAW SRM 57-10-10-2R-5; [18] VERIFIED STEP 17; [19] VERIFIED ITEM 17; [20] PERFORMED LEAK CHECK OF REPAIR IAW B737 AMM 28-11-00-790-801. LEAK CHECKS GOOD; [21] STEP 20 C/W; [22] VERIFIED STEP IS COMPLETE; [23] AUDIT C/W

Part: PLATE — CORRODED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

DOT#02-186 AFT PIT DOOR THRESHOLD AFT CORNER PLATE CORRODED ; / [01] EVALUATED CORRODED PLATE NO ALLOWABLE LIMITS FOUND IN THE SRM FOUND PLATE OUT OF LIMITS; [02] VERIFIED ITEM 1; [03] VERIFIED NEW PART # AS 453A2611-1; IAW AIPC 25-52-10-04; ITEM # 450.. A-TAG # E90168; [04] REPLACED PART ON PIT RACK.; [05] ALL WORK C/W<BR>AUDIT C/W

Part: STRIP — CORRODED (AFT PIT) · airframe 27,330 hrs · 12,353 cycles

DOT#05-186 AFT PIT LH CAP STRIP #3 CORRODED ; / [01] REMOVED CORROSION AND VERIFIED WITH 10X MAGINIFIER ALL CORROSION REMOVED IAW SRM 51-10-02-0G-0; [02] LIMITS VERIFIED; OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM<BR>ORIGINAL THICKNESS .063'<BR>REMAINING THICKNESS .059'<BR>AAR TOOL 36644 DATE 08-20-22; [03] VERIFIED STEPS 1 AND 2; [04] VERIFIED STEPS 1&2; [05] ''PERFORMED EA 22-125-00082. REF. FAULT TTG8Q00A4LLW''.; [06] ALL WORK C/W<BR>AUDIT C/W

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 27,330 hrs · 12,353 cycles

A22-011; CABIN FLOOR PANEL 232CF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3A;C;E;F<BR>VERIFIED REPAIR MATERIALS AS REPAIR PLIES-- BMS9-3TYH3 (A10273); RESIN-- EPOCAST 50A1/9816 (A100514) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND; [02] STEP 1 OK. OK TO BOND; [03] BONDED REPAIR PLIES; CURED IN OVEN B0-06 DUE 2-19-22; TAP TEST GOOD IAW SRM 53-00-50-2R-1 STEPS 3K;L;M; [04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD; [05] VERIFIED STEPS 3-4; [06] AUDITED

Part: CHANNEL — CRACKED (VERT. STAB.) · airframe 27,330 hrs · 12,353 cycles

A22-005; VERT STAB STA1016; LBL11; 5' ABOVE VERT STAB L/H ATTACH FTG; LATERAL SUPPORT CHANNEL CRACKED AT STRAIN RELIEF CUTOUT. ; / [01] REMOVED VERTICAL STAB LATERAL SUPPORT CHANNEL STA 1016 IAW SRM 51-40-02; [02] VERIFIED NEW PART TO BE MPN: 176A3101U26 ATAG: WN8100 IAW AIPC 55-33-11-02A ITEM 45.; [03] LOCATED AND DRILLED NEW PART IAW SRM 51-10-05; [04] VERIFIED STEPS 1;2 AND3<BR>OK TO INSTALL; [05] INSTALLED VERTICAL STAB LATERAL SUPPORT CHANNEL STA 1016 LBL11 IAW SRM 51-40-02; [06] APPLIED CIC TO NEW PART IAW 51-21-91-620-802; [07] REMOVED AND REPLACED VERTICAL STAB LATERAL SUPPORT CHANNEL STA 1016 LBL11 IAW SRM 51-40-02 AND AIPC 55-33-11-02A; [08] VERIFIED STEP 7<BR>AUDIT CW

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

A125-20 - AFT CARGO BAY - FLOOR PANEL - 140BF - PERIMETER CORRODED ; / [01] MEASURED TOTAL ACCUMULATED LENGTH OF CORROSION DAMAGE TO BE = 27 ' LIMIT = 20'. PANEL 140BF IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102; [02] VERIFIED MATERIAL FOR NEW FLOOR PANEL TO BE MPN: 2024-T3-071 ATAG: A106982 IAW AMM 25-52-01-201-801 TABLE 1C1; [03] VERIFIED STEPS 1& 2; [04] FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201 AND SRM 51-40-05; [05] VERIFIED STEP 4<BR>OK TO TREAT/PRIME; [06] TREATED AND PRIMED LOWER SIDE OF NEW FLOOR PANEL IAW AMM 51-21-41-370-803 AND AMM 51-21-72-370-804; [07] MEASURED TOTAL ACCUMULATED LENGTH OF CORROSION DAMAGE TO BE = 27 ' LIMIT = 20'. PANEL 140BF IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102. FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201 AND SRM 51-40-05. TREATED AND PRIMED LOWER SIDE OF NEW FLOOR PANEL IAW AMM 51-21-41-370-803 AND AMM 51-21-72-370-804; [08] VERIFIED STEPS 6&7<BR>AUDIT CW

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 27,330 hrs · 12,353 cycles

A22-008; CABIN FLOOR PANEL 231FF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3A;C;E;F<BR>VERIFIED REPAIR MATERIALS AS REPAIR PLIES-- BMS9-3TYH3 (A10273); RESIN-- EPOCAST 50A1/9816 (A100514) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND; [02] STEP 1 OK. OK TO BOND; [03] BONDED REPAIR PLIES; CURED IN OVEN B0-06 DUE 2-19-22; TAP TEST GOOD IAW SRM 53-00-50-2R-1 STEPS 3K;L;M; [04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD; [05] VERIFIED STEPS 3-4; [06] AUDITED

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 27,330 hrs · 12,353 cycles

A22-010; CABIN FLOOR PANEL 231DF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED DAMAGE; UPPER FACE SHEET IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION NOTED.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;E;F; AND J. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; FIBERGLASS CLOTH BMS9-3 (A10273); RESIN EPOCAST 50A (A102321).<BR><BR>OKAY TO BOND REQUIRED.; [02] STEP 1 OK. OK TO BOND; [03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS K;L; AND M; AND B737 SRM 53-00-50-2R-0 REPAIR GENERAL. CURED AT 150 DEGREES FOR 4 HOURS; OVEN BO-06 CAL DUE 2/19/22. TAP TEST GOOD.; [04] REPAIRED CABIN FLOOR PANEL 231DF UPPER FACE SHEET IAW B737 SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.

Part: CREASE BEAM — CORRODED (AFT GALLEY) · airframe 27,330 hrs · 12,353 cycles

AFT GALLEY DOOR R-2 CREASE BEAM IS CORRODED. BS 975; WL208; RBL64. DOT 23 ; / [01] REMOVED CORROSION ON CREASE BEAM ANGLE IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS : ORIGINAL 'T' .080 REMAINING.060 LOSS .020 FOUND OUT OF LIMITS IAW SRM 53-70-15-1A-1 TOOL USED AAR UT # 36649 DUE 12/08/22; [03] VERIFIED STEPS 1 AND 2; [04] VERIFIED ITEMS 1;2; AND 3.<BR>BLEND OUT OF LIMITS; [05] REMOVED DAMAGE CREASE BEAM IAW SRM 51-40-02; [06] REMOVED ' L' ANGLE AT STA 992 RBL 64-48 TO FOM IAW SRM 51-40-02; [07] VERIFIED STEPS 5 AND 6; [08] VERIFIED NEW CREASE BEAM ANGLE P/N147A8540-8 TAG #WN3366 IAW DWG 147A8501 REV.-; [09] VERIFIED STEP 6 IS COMPLETE; [10] VERIFIED STEP 8; [11] LOCATED AND DRILL HOLES ON NEW CREASE BEAM IAW SRM 51-40-05-0G-0; [12] VERIFIED STEP 11; [13] VERIFIED STEP 11; [14] OK TO INSTALL; [15] INSTALLED CREASE BEAM IAW SRM 51-40-02 DWG 147A8501; [16] VERIFIED STEP 15; [17] VERIFIED STEP 15. OK TO INSTALL L ANGLE STEP 6.; [18] INSTALLED 'L' ANGLE IAW SRM 51-40-02 DWG 147A8501 REV .-; [19] APPLIED CORROSION INHIBITING COMPOUND CREASE BEAM IAW AMM 51-21-91-620-802; [20] VERIFIED STEPS 18 AND 19 ARE COMPLETE; [21] CORRECTED THICKNESS; [22] VERIRIFED CORRECTION; [23] UPDATED PARTS INFO; [24] VERIFIED STEPS 18 AND 19. AUDIT COMPLETE; [25] ADJUSTED PART NUMBER PN MEASURMENT TABLE; [26] VERIFIED P/N CORRECT ON MEASUREMENT TABLE

Part: LENS — CRACKED (CABIN) · airframe 27,330 hrs · 12,353 cycles

A-061 DOT 002. R/H AFT EMERGENCY EXIT AFT HEADER PNL (232ZLW) LIGHT LENS CRACKED ; / [01] INSTALLED WINDOW LIGHT LED LENS IAW AMM 33-21-00-960-804 <BR><BR>STEP 9. C. (4)-(5)(C); [02] UPDATED PARTS INSTALLED INFO; [03] VERIFIED STEP 1; AUDIT C/W

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 27,330 hrs · 12,353 cycles

A22-012; CABIN FLOOR PANEL 241UF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED PANEL 241UF AND FOUND AREA'S OF PULLED FIBER'S ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B 737-800 SRM 53-00-50 2R -1 PAR 1A REV74. CLEAN AND PREP FOR REPAIR. IAW B737-800 SRM 53-00-50-2R-1 PAR 3 A;C;E&F. TAP TEST GOOD VERIFY MATERIALS: BMS 8-201 RESIN (A102321); BMS 9-3 CLOTH (A10273). IAW B 737-800 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.; [02] STEP 1 OK. OK TO BOND; [03] BONDED REPAIR. IAW B737-800 SRM 53-00-50-2R-1 PAR 3K-M. AAR OVEN BO-06 2/19/22. 150DEG 3HRS; [04] REPAIRED AREA'S OF PULLED FIBER'S ON UPPER SURFACE OF PANEL 241 UF. IAW B737-800 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 27,330 hrs · 12,353 cycles

A22-013; CABIN FLOOR PANEL 241VF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. TAP TEST GOOD.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. FABRIC (A10273); RESIN (E82891)<BR><BR>REQUESTING OK TO BOND; [02] STEP 1 OK. OK TO BOND; [03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (OVEN B0-06 EXP 2-19-22). TAP TEST GOOD.; [04] REPAIRED CABIN FLOOR PANEL 241VF UPPER SURFACE AS MARKED IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

A125-21 - AFT CARGO BAY - FLOOR PANEL - 140CF - PERIMETER CORRODED ; / [01] VERIFIED LIMITS; FOUND OUT OF LIMITS ( MORE THAN 20' LENGTH ) IAW 25-52-01-201-801.; [02] IDENTIFIED MATERIAL FOR PNL # 140CF AS: 2024 - T3-071 A TAG # A84104. IAW AMM 25-52-01-201-801.; [03] VERIFIED STEPS 1 AND 2; [04] FABRICATED NEW PNL # 140 CF IAW AMM 25-52-01-201-801.; [05] VERIFIED STEP #4; OK GIVEN TO TREAT AND PRIME FLOOR PANEL; [06] ALODINED AND PRIMED THE LWR SURFACE OF PNL # 140 CF IAW AMM 51-21-72.; [07] VERIFIED ITEM 6<BR>CORROSION PARAMETERS NOT FILLED OUT.; [08] FINISHED FAB.; [09] AUDIT C/W

Part: PANEL — CRACKED (AFT CARGO) · airframe 27,330 hrs · 12,353 cycles

A-125-02 - AFT CARGO BAY - BULKHEAD PANEL - 142 NWB - CRACKED/TEMPORARY REPAIR INSTALLED ; / [01] REPLACED ON SHELF NEW BULKHEAD PANEL 142NWB. VERIFIED PART AS 453A2510-1; IAW AIPC 25-52-19-01B. ITEM # 35. A-TAG # WN12334.; [02] ALL WORK C/W<BR>AUDIT C/W

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

A-125-06 - FORWARD CARGO BAY - FLOOR PANEL - 120DF - PERIMITER CORRODE ; / [01] EVALUATED DAMAGE FOUND DAMAGE TO BE LONGER THEN 20' FOUND FLOOR PANEL TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1; [02] VERIFIED NEW FLOOR PANEL MATERIALS AS P/N <BR>2024-T3-071 ATAG A105081 IAW AMM 25-52-01-201-801; [03] VERIFIED STEPS 1 AND 2 C/W; [04] BEGAN FABRICATING FWD CARGO FLOOR PANEL 120DF IAW SRM 51-40-05-OG-O.; [05] VERIFIED STEP 4 C/W; [06] FINISHED FABRICATING NEW FLOOR PANEL 120DF IAW SRM 51-40-05-OG-0; [07] VERIFIED STEP 6 C/W<BR><BR>OK TO TREAT AND PRIME; [08] TREATED AND PRIMED LOWER SURFACE OF NEW FLOOR PANEL 120DF IAW AMM 51-21-41-370-803/ 51-21-72-370-801; [09] FABRICATED NEW FWD CARGO FLOOR PANEL 120DF IAW SRM 51-40-05-OG-O.; [10] CORRECTING REF FOR STEP 9. SHOULD BE AMM 25-52-01-201-801; [11] ALL WORK C/W<BR>AUDIT C/W

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

A-125-09 - FORWARD CARGO BAY - FLOOR PANEL - 120AF - PERIMETER CORRODED ; / [01] VERIFIED LIMITS ON FWD PIT FLOOR PANEL 120AF. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. FIG 102.; [02] VERIFIED MATERIAL FOR REPLACEMENT PANEL AS .071; 2024-T3; IAW AMM 25-52-01-201-801. A-TAG # A105083.; [03] VERIFIED STEPS 1 AND 2 C/W; [04] NEED OK TO TREAT AND PRIME BACKSIDE OF PANEL 120AF TO COMPLETE FABRICATION OF PANEL.; [05] OK TO TREAT AND PRIME; [06] FABRICATED FWD PIT REPLACEMENT FLOOR PANEL 120AF; IAW AMM 25-52-01-201-801. TREATED BACKSIDE OF PANEL IAW AMM 51-21-41-370-803. PRIMED BACKSIDE OF PANEL IAW AMM 51-21-72-370-804; [07] ALL WORK C/W<BR>AUDIT C/W

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

A-125-08 - FORWARD CARGO BAY - FLOOR PANEL - 120CF - PERIMETER CORRODED ; / [01] EVALUATED DAMAGE : CORROSION IS MORE 20 INCH FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1; [02] VERIFIED MATERIAL ID : IS 2024 T3 .071 TAG #A105083 IAW AMM 25-52-01-201-801; [03] VERIFIED STEPS 1 & 2 ARE COMPLETE; [04] VERIFIED STEPS 1 AND 2; [05] FABRICATED 120 CF FLOOR PANEL IAW AMM 25-52-01-201-801; [06] VERIFIED STEP5 IS COMPLETE; [07] VERIFIED ITEM 5. OK TO TREAT AND PRIME; [08] APPLIED ALODINE AND PRIMER ON NEW PANEL IAW SRM 51-20-01 AMM 51-21-72-370-804; [09] VERIFIED STEP 8 IS COMPLETE; [10] VERIFIED ITEM 9. AUDIT COMPLETE

Part: PANEL — CRACKED (FUSELAGE) · airframe 27,330 hrs · 12,353 cycles

PANEL 194BL CORNER IS CRACKED AND BROKEN ; / [01] EVALUATED DAMAGE; PANEL CORNER IS REPAIRABLE IAW B737 SRM 53-60-70-2R-1 TABLE 203.<BR><BR>REMOVED DAMAGE; CLEANED AND PREPPED REPAIR AREA. BONDED REPAIR PLIES IAW B737 SRM 51-70-05-2R-10 REPAIR 10 PAR 4 STEPS A THRU G AND IAW B737 SRM 51-70-05-2R-0; CURED FOR 120 MINUTES AT 250 DEGREES; OVEN BO-06; CAL DUE 2/19/22. TAP TEST GOOD. FIBERGLASS CLOTH BMS8-79 (A109669); FILM ADHESIVE BMS5-101(A68274).<BR><BR>REQUIRES OKAY TO PAINT.; [02] OK TO PAINT; [03] RESTORED FINISH IAW B737 AMM 51-21-99-300-801 TABLE 701 PAINT ECL-G-357SC-RED (A103442); [04] REPAIRED PANEL 194BL CORNER IAW B737 SRM 53-60-70-2R-1 REPAIR 1 AND B737 SRM 51-70-05-2R-10 REPAIR 10.

Part: BRACKET — DENTED (L1 DOOR GIRT BAR) · airframe 11,402 hrs · 25,580 cycles

GIRT BAR ON FORWARD ENTRY DOOR DIFFICULT TO STOW. / FOUND PARTIALLY DENT BRACKET. ADJUSTED BRACKET ON FWD ENTRY DOOR SLIDE CASE PER AMM 26-66-01.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 24,512 hrs · 10,855 cycles

RAMP REPORTS L1 GIRT BAR FIGHTING RETAINING CLIP / REPOSITIONED AND SECURED GIRT BAR PER AMM 25-66-01

Part: GROMMET — LOOSE (L1 GIRT BAR) · airframe 24,205 hrs · 10,693 cycles

GROMMET ON FOWARD ENTRY GIRT BAR FELL OFF. INSTALLED GROMMET PER SIP.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 22,130 hrs · 9,640 cycles

PHOTO LUMINESCENT STRIP @ 12D IS LOOSE CAUSES A TRIPPING HAZZARD SECURED PHOTO LUMINESCENT STRIP AT 12D USING SIP

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 21,022 hrs · 9,149 cycles

EMERGENCY LIGHT BATTERY PACK IN POSITION (M2816) WOULD NOT HOLD A CHARGE. / R&R BATTERY PACK PER AMM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 21,022 hrs · 9,149 cycles

R/H WING #8 SLAT UPPER SURFACE DELAMINATED AT 39" OUTBOARD AND 1.5" TRAILING EDGE. / REPAIRED SLAT IAW SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 21,573 hrs · 9,400 cycles

RIGHT HAND WING #8 SLAT UPPER SURFACE IS DELAMINATED AT 39' O/B AND 1.5' T/E / RIGHT HAND WING #8 SLAT UPPER SURFACE DELAMINATED AT 39' O/B AND 1.5' T/E REPAIRED IAW SRM 57-42-01-2R-4 AND IAW SRM 51-70-10-2R-2. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-42-01-1A-1 PARA 4B(5)(D). DAMAGE WOULD REQUIRE REPAIR IN LESS THAN 24 MO. APPLIED PERMANENT REPAIR.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 21,022 hrs · 9,149 cycles

FORWARD CARGO COMPARTMENT AFT BULKHEAD RH SUPPORT CORRODED AT BS. 500I, RBL 25. / R&R SUPPORT PER DWG AND SRM.

Part: SUPPORT — CORRODED (BS 500I) · airframe 21,573 hrs · 9,400 cycles

***CORROSION*** FWD CARGO COMPARTMENT AFT BULKHEAD RH SUPPORT BS 500I RBL25 WL 156 / REMOVED AND REPLACED FWD CARGO AFT BULKHEAD R/H SUPPORT PART # 143A9485-34 PER BOEING DWG # 143A9481 AND SRM 51-40-02-0G-0 57903U 06JAN20

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 21,022 hrs · 9,149 cycles

FORWARD CARGO COMPARTMENT AFT BULKHEAD LOWER CENTER SUPPORT CORRODED AT BS. 500I, BETWEEN RBL 20 TO RBL 25. / R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (BS 500I) · airframe 21,573 hrs · 9,400 cycles

***CORROSION*** FWD CARGO COMPARTMENT AFT BULKHEAD LOWER CENTER SUPPORT BS 500I RBL20-RBL 25 WL 156 / REMOVED + REPLACED FWD CARGO COMPARTMENT AFT BULKHEAD LOWER CENTER SUPPORT BS 500I RBL20 - RBL25 WL 156 IAW SRM 51-40-02-0G-0 + DWG 143A9481. 56379U 05JAN20

Part: FLAP — DELAMINATED (L/H WING) · airframe 21,573 hrs · 9,400 cycles

LEFT HAND WING INBOARD MAIN FLAP LOWER O/B SURFACE DELAMINATED / REMOVED $ REPLACED L/H I/B MAIN FLAP IAW B737 AMM 27-51-11-000-801 & AMM 27-51-11-400-801. ADJUSTMENT CHECK IS GOOD IAW B737 AMM 27-51-11-820-801. (POS:LH; TAG NO:547763; P/N OFF:113A2100-71; S/N OFF:000267; P/N ON:113A2100-71; S/N ON:V1210)

Part: SKIN — CRACKED (LT WING) · airframe 21,022 hrs · 9,149 cycles

L/H LEADING EDGE SKIN INBOARD AFT EDGE HAD 4EA CRACKS AT SKIN COUNTERSINKS WING STA. 218. / REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (L/H WING) · airframe 21,573 hrs · 9,400 cycles

LEFT HAND LE SKIN I/B AFT EDGE HAS 4EA CRACKS AT SKIN COUNTERSINKS WING STA 218 / CUT AND REMOVED DAMAGED SECTION OF SKIN AT WS 218 L/H L/E SKIN. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 57-41-01-2R-3

Part: SKIN — DELAMINATED (TE FLAP) · airframe 21,022 hrs · 9,149 cycles

L/H WING INBOARD MAIN FLAP LOWER OUTBOARD SURFACE DELAMINATED. / R&R MAIN FLAP IAW AMM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 21,022 hrs · 9,149 cycles

FORWARD CARGO COMPARTMENT RH ZEE CHANNEL CORRODED BETWEEN BS. 406 TO BS. 420, RBL 25. / R&R ZEE CHANNEL IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 21,573 hrs · 9,400 cycles

***CORROSION*** FWD CARGO COMPARTMENT RH ZEE CHANNEL BS 406 - 420; RBL 25; WL 156 / REMOVED DAMAGED FWD CARGO R/H ZEE CHANNEL FROM STA 406-420; RBL 25; WL156 IAW SRM 51-40-02-0G-0. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. INSTALLED REPLACEMENT FWD CARGO R/H ZEE CHANNEL PO #733837/1 IAW SRM 51-40-02-0G-0 AND DWG #143A7500 ID:75 57403U 01/04/2020

Part: CHANNEL — CORRODED (FWD CARGO BAY) · airframe 21,573 hrs · 9,400 cycles

***CORROSION*** FWD CARGO COMPARTMENT LH ZEE CHANNEL BS 406 - 500I LBL 25 WL 156 / CORROSION DAMAGE ON FWD CARGO LH ZEE CHANNEL BS 406-500I LBL25 WL156 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 PARAGRAPH 4 DETAIL D. REMOVED AND REPLACED LH ZEE CHANNEL FROM BS 406-500I WITH SPLICES AT BS 480-500 AND 500E-500F. ALL PER SRM 53-00-53-2R-5; SRM 51-40-02 SRM 51-40-05; BOEING DRAWING 143A7501 & BOEING DRAWING 143A7500

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 21,022 hrs · 9,149 cycles

FORWARD CARGO COMPARTMENT ZEE CHANNEL CORRODED BETWEEN BS. 500 TO BS. 500I, RBL 25. / R&R R/H ZEE CHANNEL IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 21,022 hrs · 9,149 cycles

AFT CARGO COMPARTMENT SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 25. / R&R SHIELD IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FWD CARGO BAY) · airframe 21,573 hrs · 9,400 cycles

***CORROSION*** FWD CARGO COMPARTMENT RH ZEE CHANNEL BS 500 - 500I RBL25 WL 156 / REMOVED AND REPLACED R/H ZEE CHANNEL IN FWD CARGO BS 500A-500I RBL 25 WL 156 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 SRM 53-00-53-1A-2; AMM 51-21-41-370-801; AMM 51-21-73-370-803 AND INSTALLED REPAIR SPLICE AT BS 500D+10 IAW 53-00-53-2R-5

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 21,022 hrs · 9,149 cycles

AFT CARGO COMPARTMENT ZEE CHANNEL CORRODED BETWEEN BS. 727 TO BS. 847, LBL 25. / R&R ZEE CHANNEL PER SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 21,022 hrs · 9,149 cycles

FORWARD CARGO COMPARTMENT ZEE CHANNEL CORRODED BETWEEN BS. 406 TO BS. 500I, LBL 25. / R&R ZEE CHANNEL PER SRM & DWG.

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 21,573 hrs · 9,400 cycles

***CORROSION*** AFT CARGO COMPARTMENT RH ZEE CHANNEL BS 727 - 787 RBL 25 WL 156 / REMOVED + REPLACED AFT CARGO COMPARTMENT R/H ZEE CHANNEL BS 727-787 RBL 25 WL 156 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-10-2R-0; & DWG 146A7500. 56379U 04JAN20 PARTS FABRICATED USING 7075T62 CLAD EXTRUSION LOT# 5090803-1.1. ORIGINAL CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPAIR SPLICE INSTALLED AT BS 727F+10. 56379U 04JAN20

Part: ANGLE — CRACKED (R/H WING) · airframe 21,573 hrs · 9,400 cycles

RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB OUTBOARD ATTACH ANGLE CRACKED (MARKED) / REMOVED AND REPLACED RIGHT WING TE DEFLECTION CONTROL RIB OB ATTACH ANGLE PER SRM 51-40-02 AND DRAWING 115A6200

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 21,022 hrs · 9,149 cycles

AFT CARGO COMPARTMENT RH ZEE CHANNEL CORRODED BETWEEN BS. 727 TO BS. 787, RBL 25. / R&R ZEE CHANNEL IAW SRM & DWG.

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 21,573 hrs · 9,400 cycles

***CORROSION*** AFT CARGO COMPARTMENT LH ZEE CHANNEL BS 727 - 847 LBL 25 WL 156 / CORROSION ON AFT CARGO COMPARTMENT LH ZEE CHANNEL BS 727-847 LBL25 WL156 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG 103; E. REMOVED AND REPLACED ZEE CHANNEL WITH REPAIR SPLICE LOCATIONS 727D+14 LBL25 AND 727J+10 LBL25 PER SRM 51-40-02; SRM 53-00-53-2R-5 AND BOEING DRAWING 146A7500

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 21,022 hrs · 9,149 cycles

AFT CARGO COMPARTMENT RH ZEE CHANNEL CORRODED BETWEEN BS. 867 TO BS. 887, RBL 25. / R&R ZEE CHANNEL PER SRM AND DWG.

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 21,573 hrs · 9,400 cycles

***CORROSION*** AFT CARGO COMPARTMENT RH ZEE CHANNEL BS 867 - 887 RBL 25 WL 156 / AFT CARGO R/H ZEE CHANNEL BS 867-887 RBL25 WL156 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED WITH NEW ITEM #BAC1496-377 #707T62; LOT #5067496-1 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DRAWING 146A7500 REV. B. 92679U 1-4-2020

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 21,573 hrs · 9,400 cycles

***CORROSION*** AFT CARGO COMPARTMENT RH SHIELD BS 847 - 867 RBL 25 WL 156 / REMOVED CORROSION ON AFT CARGO COMPARTMEN SHEILD R/H BS 847-867 RBL 25 WL 156 IN AN AREA OF L1.20' X W1.20' X D.028 I.A.W. SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS I.A.W. SRM 53-00-53-1A-2. LOCATED AND DRILLED NEW SHEILD I.A.W. SRM 51-40-05-0G-0 AND BOEING DWG 146A0081 REV:A. INSTALLED NEW SHEIL P/O # 765476 I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 146A0081 REV:A

Part: SUPPORT BRACKET — CRACKED (AFT CARGO BAY) · airframe 21,573 hrs · 9,400 cycles

AFT CARGO COMPARTMENT LH BULKHEAD SUPPORT BRACKET CRACKED BS 867 RBL 10 WL 156 / REMOVED CRACKED SUPPORT BRACKET BS 867 RBL 10 WL 156 I.A.W. SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW SUPPORT BRACKET P/O# 774596 I.A.W. SRM 51-40-05-0G-0. INSTALLED NEW BRACKET I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 149A8102 REV: A.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 21,022 hrs · 9,149 cycles

R/H WING TRAILING EDGE DEFLECTION CONTROL RIB OUTBOARD ATTACH ANGLE CRACKED. / R&R ANGLE PER SRM AND DWG.

Part: SUPPORT — CRACKED (FWD CARGO RH) · airframe 21,573 hrs · 9,400 cycles

FLOOR SUPPORT AT STA 540 FROM RBL 3-23 IS CRACKED / REMOVED AND REPLACED FLOOR SUPPORT AT STA 540 RBL 3-23 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG #143A5240

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,022 hrs · 9,149 cycles

FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN LBL 3 TO LBL 23. / R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CRACKED (FWD CARGO LH) · airframe 21,573 hrs · 9,400 cycles

FLOOR SUPPORT AT STA 540 FROM LBL 3-23 IS CRACKED / REMOVED AND REPLACED FLOOR SUPPORT AT STA 540 LBL 3-23 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG #143A5240

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,022 hrs · 9,149 cycles

FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN RBL 3 TO RBL 23. / R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: PANEL — DELAMINATED (BELLY) · airframe 21,398 hrs · 9,327 cycles

BELLY PANEL 192K (149A7753-3) IS DELAMINATED (OUTER LAYER OF FIBERGLASS PEELED OFF).INSTALLED PANEL 149A7753-2 PER EA OTHER-53EA-07525 PANEL MUST BE REMOVED AND INSTALL SERVICEABLE 149A7753-3 PANEL WITHIN 7 DAYSPERMANENT ACTION REQUIRED:REMOVE THE 149A7753-2 PANEL AND INSTALL A SERVICEABLE 149A7753-3 PANEL / REMOVED - 2 PANEL & INSTALLED 3 PANEL; REF SA-M #0157988 FOR FULL RESOULTION

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 21,345 hrs · 9,305 cycles

BELLY PANEL 192K (149A7753-3) IS DELAMINATED (OUTER LAYER OF FIBERGLASS PEELED OFF). / INSTALLED PANEL 149A7753-2 PER EA OTHER-53EA-07525 PANEL MUST BE REMOVED AND INSTALL SERVICEABLE 149A7753-3 PANEL WITHIN 7 DAYS

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 19,910 hrs · 8,645 cycles

PHOTO LUMINESCENT LIGHT TRACK DAMAGED. R&R STRIPS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 19,001 hrs · 8,251 cycles

RT EGRESS LIGHT LENS COVER MISSING AT ROW 17. R&R EMERGENCY LIGHT ASSEMBLY IAW AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 19,001 hrs · 8,251 cycles

RIGHT EGRESS LIGHT LENS MISSING AT ROW 17. R&R LIGHT ASSEMBLY PER MM.

Part: LENS — MISSING (CABIN) · airframe 17,572 hrs · 7,627 cycles

LT OVERHEAD BIN EMERGENCY LIGHT LENS COVER MISSING AT ROW 8. INSTALLED COVER PER SIP.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 16,549 hrs · 7,188 cycles

LEFT WING UPPER TRAILING EDGE PANEL BETWEEN #5 AND #6 SPOILERS AFT SUPPORT BRACKET IS CRACKED AT ON / REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02AMT 444447INSP 56505

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 16,549 hrs · 7,188 cycles

LH HORIZONTAL UPPER FWD SLIDER IS CRACKED / R&R SLIDER PER MM REF 53-31-31AMT 21524INSP 49016

Part: BATTERY — FAILED (CABIN) · airframe 16,323 hrs · 7,096 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER DWG AND AMM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 16,549 hrs · 7,188 cycles

RH HORIZONTAL STAB; UPPER FWD SLIDER IS CRACKED / R&R R/H HORIZONTAL STAB UPPER FWD SLIDING SEAL REF AMM 53-31-31. AMT 67662INSP 49016

Part: SIGN — UNSECURE (CABIN) · airframe 13,870 hrs · 6,012 cycles

R1 DOOR EMERGENCY EXIT SIGN CAME OFF. R&R SIGN PER MM.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 13,300 hrs · 5,764 cycles

LH HORIZONTAL STAB; UPPER FWD SLIDER IS CRACKED / R&R LH HORIZONTAL STAB UPPER FWD SLIDER PER M/M 53-31-31

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 13,300 hrs · 5,764 cycles

RH HORIZONTAL STAB UPPER FWD SLIDER IS CRACKED / R&R RH HORIZONTAL STAB UPPER FWD SLIDER PER M/M 53-31-31

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 12,244 hrs · 5,332 cycles

R2 DOOR SLIDE GIRT BAR FLAP OUT OF ADJUST. ADJUSTED THE SLIDE IAW MT.

Part: LIGHT — CRACKED (ROW 18) · airframe 11,211 hrs · 4,891 cycles

RIGHT EMERGENCY LIGHT BEZEL CRACKED AT ROW 18. R & R THE LIGHT IAW AMM.

Part: HANGER ASSY — UNSECURE (L1 DOOR GIRT BAR) · airframe 11,211 hrs · 4,891 cycles

L1 DOOR SLIDE COVER AFT GIRT BAR HANGER RIVETS SHEARED. R & R THE HANGER ASSEMBLY IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,625 hrs · 4,173 cycles

LEFT FORWARD ENTRY EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 8,873 hrs · 3,857 cycles

R1 DOOR EMER LIGHT EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: LENS — MISSING (CABIN) · airframe 7,146 hrs · 3,102 cycles

LEFT OVERHEAD BIN, EMER EXIT LIGHT LENS COVER MISSING AT ROW 4. INSTALLED LENS IAW SIP.

Part: LENS — MISSING (CABIN) · airframe 3,915 hrs · 1,754 cycles

LEFT OVERHEAD BIN EMER EXIT LIGHT LENS COVER MISSING AT ROW 12. INSTALLED COVER IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 2,612 hrs · 1,158 cycles

FORWARD GALLEY EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.