N915WN

Part: SEAL — CRACKED (ZONE 300) · airframe 57,438 hrs · 34,808 cycles

RT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL HAS VERTICAL CRACKS PARALLEL TO BOTH THE FORWARD AND AFT EDGES. REMOVED AND REPLACED THE STABILIZER TO BODY UPPER FRONT R/H SLIDING SEAL PER AMM 53-31-31.

Part: SEAL — CRACKED (ZONE 300) · airframe 57,438 hrs · 34,808 cycles

L/H HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL HAS VERTICAL CRACKS PARALLEL TO BOTH THE FORWARD AND AFT EDGES. REMOVED AND REPLACED L/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL PER AMM 53-31-31.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 57,387 hrs · 34,772 cycles

FWD FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS TEST PASS.

Part: LIGHT — BURNED OUT (ZONE 200) · airframe 57,358 hrs · 34,752 cycles

LEFT EMERGENCY EXIT LATCH; EMERGENCY EXIT LIGHT BURNED OUT. REPLACED EMERGENCY EXIT LIGHT, LT EMERGENCY EXIT LATCH IAW AMM 33-51-04-960-801 STEP 2.F.(1)(2)(3)(A)(B)(D).

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 57,361 hrs · 34,753 cycles

INOPERATIVE EXTERNAL EMERGENCY LIGHT AFT SERVICE DOOR AT UPPER FUSELAGE. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-04-960-801, STEP 2.F. 1, 2, 3, A, B, D, 4. TESTED OK.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CRACK SUPPORT ZEE LOCATED BETWEEN BS 727D - 727E, S25L, WL 156. REPLACED SUPPORT ZEE IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 146A7500 SHEET 113 REV- DWG 146A7502 SHEET 27 REV-.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CRACKED SUPPORT BRACKET, BS 947.5, LBL 10 IN THE AFT CARGO COMPARTMENT. REPLACED SUPPORT BRACKET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 149A8103, SHEET 7, REV A.

Part: WEB — CRACKED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CRACK WEB CEILING AREA, BS 847 TO 867, LBL 19, AFT CARGO BAY. REPLACED WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 149A8100, SHEET 1 REV -.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CRACK CARGO TRACK RBBL 13.84 FRAME 747 AFT CARGO COMPARTMENT. REPAIRED CARGO TRACK RBL 13.84 BTW SECTION BS 727D - 787 IAW SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1, AND ALTERNATIVE 2.

Part: ANGLE — CRACKED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CRACK ANGLE LOCATED BS 867, LBL 10 IN THE AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS 867, LBL 10 IAW SRM 51-10-02, ITEM 9, AND INSTALLED FASTENERS IAW SRM 51-40-02, AND DRAWING 149A8102, SHEET 17, REV-. MEASUREMENT OF CRACK IS 0.550 INCH.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CRACK CARGO TRACK RBBL 13.84, BS 767 IN THE AFT CARGO COMPARTMENT. REPAIRED THE CARGO TRACK SECTION BS 727D - 787 IAW SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1 AND ALTERNATIVE 2.

Part: SHIELD — CORRODED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CORROSION SHIELD WEB FLOOR STRUCTURE BS 767 TO 794.5, S25R, WL156, AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-10-02, ITEM 9, AND INSTALLED FASTENERS IAW SRM 51-40-02, AND DRAWING 146A0081, SHEET 37, REV -.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CORROSION SUPPORT ZEE BETWEEN BS 727 - 767, S25R, WL 156. REPLACED SUPPORT ZEE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A7500, SHEET 113, REV-, AND DWG 146A7502, SHEET 49, REV-.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CRACK CARGO TRACK RBBL 13.84 BS 727 IN THE AFT CARGO COMPARTMENT. REPAIRED THE CARGO TRACK BTW BS 727D- 787 IAW SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1 AND 2.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CORROSION SUPPORT ZEE BETWEEN BS 727 - 767, S25R, WL 156. REPLACED THE SUPPORT ZEE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A7500, SHEET 113, REV-, AND DWG 146A7502, SHEET 49, REV-.

Part: WEB — CORRODED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CORRODED WEB, BS 492.4 - 500A, S26R, WL 156 IN THE FWD CARGO BAY. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A0080, SHEET 23, REV-.

Part: PLATE — CRACKED (ZONE 600) · airframe 57,361 hrs · 34,753 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING IAW SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 115A3712 SHEET 7REV A AND DWG 115A3700 SHEET 41 REV - .

Part: STRAP — CORRODED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CORROSION STRAP FLOOR STRUCTURE LOCATED BETWEEN STA1016 TO STA1040 AND RBL18 WL208.1. REPLACED STRAP FLOOR STRUCTURE IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A5730 SHEET 23 REV C.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CORROSION FLOOR BEAM, BS 986.5, LBL 42, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.

Part: STRAP — CORRODED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CORRODED STRAP, FLOOR STRUCTURE LOCATED BETWEEN BS 1016 TO 1040, LBL 4, WL 208.1. REPLACED THE STRAP IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 147A5600, SHEET 32, REV B.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CRACKED FLOOR SUPPORT LOCATED BETWEEN BS 312 - 328, LBL 46. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, AND DWG 141A5400, SHEET 26, REV-.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CRACKED FLOOR SUPPORT BS 328 - 344, LBL 46 REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02, DRAWING 141A5400, SHEET 44, REV-.

Part: TIE CLIP — CRACKED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CRACK TIE CLIP LOCATED BS 277, STR 10R. REPLACED THE TIE CLIP AND FASTENERS AT BS 277, S10R IAW SRM 51-40-02-0G-0 AND DWG 141A1110 SHEET 18 REV-.

Part: NUT PLATE — CRACKED (ZONE 500) · airframe 57,361 hrs · 34,753 cycles

CRACK ON RAIL NUT-PLATE LOCATED ORSS 286 INTERNAL CAVITY TRAILING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 286 INTERNAL CAVITY TRAILING EDGE AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.

Part: ANGLE — CRACKED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

CRACK ON ANGLE WING TO BODY FARING STRUCTURE BS 500D AT LEVEL STR19L AT LOWER FUSELAGE. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 116A3010, SHEET 39, REV-.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CORROED FLOORBEAM, BS 986.5, RBL 42, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CRACK WEB INTERCOSTAL LOCATED BETWEEN BS 294.5 - 303.9, S16L. PERFORMED A MAJOR REPAIR ON WEB INTERCOSTAL IAW EA 25-153-02714-WIP1, TTG8Q015JTW1 AND EA 25-153-02714, TTG8Q015TCU5.

Part: HANDLE — DETERIORATED (ZONE 800) · airframe 57,361 hrs · 34,753 cycles

DETERIORATED HANDLE ON FWD ENTRY DOOR AT FWD GALLEY AREA (2 E/A). REPLACED HANDLE ON FWD ENTRY DOOR AT FWD GALLEY AREA (2 E/A) IAW AMM 52-11-31-400-802 STEP 3.G.(2).

Part: ANGLE — CRACKED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CRACKED ANGLE, BS 695, BL 0. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 273A9110, SHEET 6, REV A.

Part: ANGLE — CRACKED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CRACKED ANGLE, FLOOR STRUCTURE, BS 695, BL 0. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0 SRM 51-10-02 ITEM 9 AND DWG 273A9110, SHEET 6, REV.A.

Part: ANGLE — CRACKED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CRACKED ANGLE FLOOR STRUCTURE LOCATED STA695 AND LBL24.75. REPLACED ANGLE LOCATED STA695 AND LBL24.75 CENTER SECTION IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 273A9110 REV A.

Part: ANGLE — CRACKED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CRACKED ANGLE, FLOOR STRUCTURE. BS 695, RBL 24.75. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 273A9110, REV A, & DWG 111A6000, SHEET 302, REV-.

Part: NUT PLATE — CRACKED (ZONE 600) · airframe 57,361 hrs · 34,753 cycles

CRACK ON RAIL NUT-PLATE LOCATED OFSS 469 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT PLATE LOCATED OFSS 469 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 112A4402, SHEET 13, REV -. CRACK MEASUREMENT IS: 0.257.

Part: NUT PLATE — CRACKED (ZONE 600) · airframe 57,361 hrs · 34,753 cycles

CRACK ON RAIL NUT-PLATE LOCATED OFSS 591 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 591 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02 ITEM 9 AND DWG: 112A4402 SHEET: 14 REV: -.

Part: NUT PLATE — CRACKED (ZONE 600) · airframe 57,361 hrs · 34,753 cycles

CRACK ON RAIL NUT-PLATE, OFSS 509 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 509 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02 ITEM 9 SRM 51-40-02, AND DWG 112A4402, REV -, SHEET 13. MEASUREMENT OF CRACK IS L: 0.240.

Part: ANGLE — CRACKED (ZONE 600 SLT TRK) · airframe 57,361 hrs · 34,753 cycles

CRACK ON ANGLE AUXILIARY TRACK SLAT 7 AT RT WING (TWO EACH). REPLACED ANGLE AUXILIARY TRACK LOCATED ON SLAT 7 AT RT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9. LENGTH OF CRACK 0.250 INCH.

Part: NUT PLATE — CRACKED (ZONE 500) · airframe 57,361 hrs · 34,753 cycles

CRACK ON RAIL NUT-PLATE LOCATED OFSS 369 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 369 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET:13 REV-.

Part: ANGLE — CRACKED (RT SLAT TRACK) · airframe 57,361 hrs · 34,753 cycles

CRACK ON ANGLE AUXILIARY TRACK SLAT 8 AT RT WING. REPLACED ANGLE AUXILIARY TRACK SLAT 8 AT RT WING IAW SRM 51-10-02 ITEM 9 & INSTALLED FASTENERS IAW SRM 51-40-02 AND DWG 114A5010; SHEET 16; REV A . AND MEASURE OF CRACK IS 0.750.

Part: NUT PLATE — CRACKED (ZONE 500) · airframe 57,361 hrs · 34,753 cycles

CRACK ON RAIL NUT-PLATE LOCATED OFSS 484 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 484 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 13, AND SHEET 14 REV-. MEASURE OF CRACK: L=0.410.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

INOPERATIVE BATTERY PACK BS 603 RT SIDE AT PASSENGER CABIN. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805, OPS CHECKED OK.

Part: ANGLE — CRACKED (ZONE 600) · airframe 57,361 hrs · 34,753 cycles

CRACKED ANGLE AUXILIARY TRACK SLAT 6, RT WING. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, AND SRM 51-40-02. DUE TO EVALUATED CRACK ON ANGLE AND NOT FOUND ALLOWABLE DAMAGE IAW SRM-57-42-02-1A-1, ALLOWABLE DAMAGE 1. MEASUREMENT OF CRACK IS L= 2.057.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

CRACK INDICATION ON STUB FRAME BETWEEN BS 294.5 - 296.5, S-8 & 9R AT FWD GALLEY DOOR AREA. CRACK LENGTH 1.375 IN. REPLACED STUB FRAME IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A8370, SHEET 9, REV -, SHEET 10, REV D.

Part: GIRT BAR — DETERIORATED (ZONE 800) · airframe 57,361 hrs · 34,753 cycles

DETERIORATED HARDWARE GALLEY GIRT BAR FLOOR BRACKETS. REPLACED HARDWARE GALLEY GIRT BAR BRACKETS IAW AMM 25-66-02-400-801.

Part: ACCESS PANEL — DELAMINATED (ZONE 100) · airframe 57,361 hrs · 34,753 cycles

DELAMINATED ACCESS PANEL 193AL AT FUSELAGE EXTERIOR, REPAIRED THE ACCESS PANEL 193AL IAW SRM 51-70-05-2R-6, REPAIR 6.

Part: GIRT BAR — DETERIORATED (ZONE 800) · airframe 57,361 hrs · 34,753 cycles

DETERIORATED HARDWARE AFT ENTRY GIRT BAR FLOOR BRACKETS. REPLACED HARDWARE AFT ENTRY GIRT BAR BRACKETS IAW AMM 25-66-02-400-801.

Part: LIGHT — BURNED (ZONE 200) · airframe 57,361 hrs · 34,753 cycles

BURNED EMERGENCY EXIT LIGHT LEFT SIDE IN PASSENGER CABIN. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01-960-801, STEP 2.C, 1, C THRU 2. TESTED OK.

Part: ACM — ODOR (ZONE 100) · airframe 57,266 hrs · 34,695 cycles

DURING F/O ROLL EXPERIENCED RANCID ODOR FOLLOWED BY EXTREMELY HOT AIR COMING THROUGH THE VENTS, COULD BARELY CONTROL TEMP IN CABIN ON LANDING AND TAXI IN WENT TO PACKS HIGH -CONTINE TO DESCRIPTION AND APU BLEED AND KEPT GETTING LEFT PACK TRIP OFF LIGHT. ACM REMOVED AND PARTIALLY ACM INSTALLED PER AMM 21-51-04; JOB STOPPED BECAUSE BUSHING IS NIS IN LAS. FINISHED INSTALLING LH ACM PER AMM 21-51-04. OPS AND LEACH CHECK GOOD.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 56,056 hrs · 33,974 cycles

AFT CARGO COMPARTMENT 2ND FLOOR BACK CRACKED THROUGH. R/R AFT CARGO FLOOR PANEL REF AMM 25-52-10.

Part: LENS — MISSING (ZONE 200) · airframe 55,764 hrs · 33,792 cycles

OVERHEAD PLACARD EMERGENCY EXIT SIGN MISSING FROM FRONT FWD ENTRY DOOR. INSTALLED LENS PER M/M 33-51-01 OK TO CONT SERVICE

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 55,120 hrs · 33,399 cycles

EMERGENCY LIGHTING BATTERY PACK AT L/H OVERWING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.

Part: ENGINE — POPPED (ZN 400 NACELLE/P) · airframe 54,505 hrs · 33,032 cycles

WHILE CLIMBING THROUGH FL210 EXPERIENCED A LOUD POP FROM ENGINE #2 ACCOMPANIED BY A MOMENTARY EGT EXCEEDANCE; OPERATED ENGINE AT REDUCED THRUST SETTING FR THE REMINDER OF THE FLIGHT WITH AIR RETURN TO SJC. OVERWEIGHT LANDING WAS NOT ACCOMPLISHED REFERENCE ORIGINAL WRITE-UP TTG8Q00X0QZX. SINCE ORIGINAL WRITE-UP WAS ASSIGNED TO ENGINE SN IN ERROR WHEN ENGINE WAS REMOVED IT UNASSIGNED THE CARD AND INITIATED A REPAIR ORDER TIED TO THE ENGINE. THAT CARD WAS CHANGED FROM LOG PAGE TO NON-ROUTINE SO THAT THIS CARD CAN REPRESENT THE ORIGINAL FAULT/LOG PAGE SIGN OFF.<[01] REMOVED AND REPLACED #2 ENGINE PER MT 771-00-01.<BR>C/W CONDITIONAL INSP 05-51-59 AMM.

Part: BATTERY PACK — INOPERATIVE (AFT FLASHLIGHT) · airframe 53,370 hrs · 32,320 cycles

AFT EMERGENCY FLASHLIGHTS BATTERIES NEED REPLACEMENT<[01] REMOVED AND REPLACED BOTH AFT EMERGENCY FLASHLIGHT BATTERIES IAW AMM 25-64-00.

Part: ACCESS DOOR — CORRODED (ZONE 100) · airframe 52,015 hrs · 31,485 cycles

ACCESS DOOR 311AL HAS CORROSION ON LEADING EDGE OF DOOR. ACCESS DOOR 311AL HAS CORROSION ON LEADING EDGE OF DOOR. PICTURES ATTACHED AND SUBMITTED TSR#2024001099.<[01] REPLACED THE ACCESS DOOR 311AL IAW AMM 52-49-11.

Part: GIRT BAR — LOOSE (ZN 800 DOOR) · airframe 51,616 hrs · 31,246 cycles

FWD SERVICE DOOR GIRT BAR LOOSE<[01] REPLACED RIVET ON GIRT BAR BRACKET ON THE FWD SERVICE DOOR REF SRM 51-40-02 AND MT 725-61-06 FOR REMOVAL AND INSTALLATION OF FWD SERVICE DOOR SLIDE.

Part: HANDLE — LOOSE (ZN 800 DOOR) · airframe 51,397 hrs · 31,116 cycles

FORWARD SERVICE DOOR ASSIST HANDLE LOOSE<[01] REPLACED HANDLE NUT REF AMM 52-41-00

Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 50,935 hrs · 30,834 cycles

R2 DOOR SLIDE SKIRT NEEDS REPOSITIONED CATCHES ON DOOR CUTOUT<[01] FAULT WILL BE ADDRESSED ON BARCODE TTG8Q00P25L7;[02] VERIFIED STEP 1

Part: LENS — LOOSE (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

FWD EMERGENCY WARNING LIGHT LENS BAR WON'T LOCK ON. FALLS OFF<[01] RESECURED R1 FWD EMERGENCY WARNING LIGHT IN REF AMM-33-51-01-960-802;[02] VERIFIED STEP 1

Part: FLAP — CRACKED (ZN 500 LEFT WING) · airframe 50,935 hrs · 30,834 cycles

FOUND DENT WITH A CRACK OUT OF LIMITS ON UPPER SURFACE L/H WING I/B AFT FLAP AT 21.5' I/B EDGE AND 12.5' T/E; LENGTH OF DENT CRACK = 1'.<[01] APPLIED REPAIR AT UPPER SURFACE L/H WING I/B AFT FLAP PER B737 SRM<BR> 57-53-01-2R-4; SRM 51-70-10-2R-4 AND SRM 51-70-10-2R-0 PARAGRAPH 20.B SIZE OF REPAIR IS 2.5'X3.5' MATERIAL USED FILM ADHES AF163-2K-06 PO#1798840 AND TOOLS USED TEMPERATURE CONTROL ID:160354 DUE DATE:02/23/24 AND VACUM GAGE ID:173239 DUE DATE:02-24-23 AND APPLIED TOP COAT AT UPPER SURFACE L/H WING I/B AFT FLA ON REPAIR AREA PER <BR>B737 AMM 51-21-99-300-802 MATERIAL USED PAINT PO#1750514.;[02] VERIFIED STEP 1

Part: FLAP — CRACKED (ZN 600 RIGHT WIN) · airframe 50,935 hrs · 30,834 cycles

FOUND DENT WITH A CRACK OUT OF LIMITS ON UPPER SURFACE R/H WING I/B AFT FLAP AT 32' FROM I/B EDGE AND 10.5' T/E; LENGTH OF DENT CRACK =1.5'.<[01] APPLIED REPAIR AT UPPER SURFACE R/H WING I/B AFT FLAP PER B737 SRM<BR> 57-53-01-2R-4; SRM 51-70-10-2R-4 AND SRM 51-70-10-2R-0 PARAGRAPH 20.B SIZE OF REPAIR IS 3.5'X4.5' MATERIAL USED FILM ADHES AF163-2K-06 PO#1798840 AND TOOLS USED TEMPERATURE CONTROL ID:160354 DUE DATE:02/23/24 AND VACUM GAGE ID:173239 DUE DATE:02-24-23 APPLIED TOP COAT AT UPPER SURFACE R/H WING I/B AFT FLA ON REPAIR AREA PER <BR>B737 AMM 51-21-99-300-802 MATERIAL USED PAINT PO#1750514.;[02] VERIFIED STEP 1

Part: FRAME — CRACKED (ZN 800 DOOR) · airframe 50,935 hrs · 30,834 cycles

FORWARD ENTRY DOOR CUTOUT STA 312 BETWEEN STR 5L-6L FRAME END CRACK<[01] FAULT WAS RESOLVED ON ANOTHER FAULT SEE EA M-22-153-01244 TASK CARD # TTG8Q00NPPLX FOR WORK ACCOMPLISHED;[02] VERIFIED STEP 1

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 50,935 hrs · 30,834 cycles

RIGHT HORIZONTAL STAB RIB # 4 HAS A CRACK AT FIRST HOLE FWD OF LOWER STIFFENER #4<[01] REMOVED CRACK AT FIRST HOLE FWD OF LOWER SECTION COMMON TO STIFFENER #4 REF SRM 51-10-02-0G-0 AND INSTALLED REPAIR PARTS AT RIGHT HORIZONTAL STAB RIB # 4 COMMON TO STIFFENER #4 REF SRM 55-10-09-2R-5.;[02] CORRECTION TO STEP 1. REMOVED CRACK AT FIRST HOLE FWD OF LOWER SECTION COMMON TO STIFFENER #4 REF SRM 51-10-02-0G-0 AND INSTALLED REPAIR PARTS AT RIGHT HORIZONTAL STAB RIB # 4 COMMON TO STIFFENER #4 REF SRM 55-10-09-2R-5. THIS WORK WAS ACCOMPLISHED IN CONJUCTION WITH TTG8Q00NJPDK;[03] RII /VERIFIED ENTRY #2 AS A CORRECT ENTRY FOR WORK ACCOMPLISHED AS A CORRECTIVE ACTION TAKEN & ALSO APPLYS TO ENTRY #1 AS A CORRECTION OF INFO. ENTERD. RII/VERIFIED TT# ENTERD WAS WORKED IN CONJUCTION WITH THIS N/R CARD.

Part: STRIP — CORRODED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

AFT CARGO COMP CAP STRIP BETWEEN STA 867-947.5 RBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 867 TO STA 947.5 RBL 21; PN: 453A2611Y3 PO:1728471. WILL BE INSTALLED PER TASK CARD TTG8Q00NKCXJ.;[02] VERIFIED STEP 1

Part: STRIP — CORRODED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

AFT CARGO COMP CAP STRIP BETWEEN STA 727-727D LBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 727 TO STA 727D LBL 21. PN: 453A2611-8 PO: 2012626. INSTALLATION WILL BE ACCOMPLISHED PER TASK CARD TTG8Q00NKCXJ.

Part: STRIP — CORRODED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

AFT CARGO COMP CAP STRIP BETWEEN STA 767-847 LBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 767 TO STA 847 LBL 21. PN: 453A2611-4 PO: 2012626. INSTALLATION WILL BE ACCOMPLISHED PER TASK CARD TTG8Q00NKCXJ.

Part: STRIP — CORRODED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

AFT CARGO COMP CAP STRIP BETWEEN STA 727-727D RBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 727 TO STA 727D RBL 21. PN: 453A2611-9 PO: 2012626. INSTALLATION WILL BE ACCOMPLISHED PER TASK CARD TTG8Q00NKCXJ.

Part: STRIP — CORRODED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

AFT CARGO COMP CAP STRIP BETWEEN STA 767-727D LBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 727D TO STA 767 LBL 21. PN: 453A2611-10 PO: 2012626. INSTALLATION WILL BE ACCOMPLISHED PER TASK CARD TTG8Q00NKCXJ.

Part: STRIP — CORRODED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

AFT CARGO COMP CAP STRIP BETWEEN STA 767-727D RBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 727D TO STA 767 RBL 21; PN: 453A2611-11 PO: 2028887. WILL BE INSTALLED PER TASK CARD TTG8Q00NKCXJ.;[02] VERIFIED STEP 1

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

AFT CARGO DOOR CUTOUT AFT SCUFF PLATE CRACKED<[01] RECEIVED REPAIRED PART FROM OUTSIDE VENDOR. PN: 146A8343-7 PO: 2028887. WILL BE INSTALLED PER TASK CARD TTG8Q002ED5A.;[02] VERIFIED STEP 1

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

AFT CARGO FWD BULKHEAD BRACKET CRACK AT RBL 6'<[01] REMOVED AND REPLACED BRACKET (PN: 144A9401-20) AT AFT CARGO COMPT FWD BULKHEAD STA 727 RBL 6 PER REF SRM 51-41-02-0G-0;[02] CORRECTION TO STEP #1: REMOVED AND REPLACED BRACKET (PN: 144A9401-20) AT AFT CARGO COMPT FWD BULKHEAD STA 727 RBL 6 PER REF SRM 51-41-02-0G-0 AND DWG #144A2600;[03] VERIFIED STEP 2

Part: FLOOR SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

AFT CARGO FLOOR SUPPORT AT B/S 771 22 INCHES RIGHT OF CENTER LINE IS CORRODED AT NUT PLATE HOLE<[01] WORK WAS ACCOMPLISHED PER TASK CARD TTG8Q00NM3MM;[02] VERIFIED STEP 1

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN INTERCOSTAL CRACK AT BL 0' BETWEEN STA 380-400<[01] REMOVED AND INSTALLED NEW INTERCOSTAL ANGLE AT MAIN CABIN BL 0' BETWEEN STA 380-400 AS PER SRM 51-40-02.;[02] CORRECTION: REMOVED AND INSTALLED NEW INTERCOSTAL ANGLE AT MAIN CABIN BL 0' BETWEEN STA 380-400 AS PER SRM 51-40-02. & DWG. 143A5400.;[03] VERIFIED STEP 2

Part: PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

ACCESS PANEL 241AF IS DAMAGED/ DELAMINATED<[01] RECEIVED MAIN CABIN FLOOR PANEL 241AF AND WILL BE INSTALLED ON T/C &NBSP;&NBSP;&NBSP;&NBSP;&NBSP;TTG8Q00MWWZR;[02] VERIFIED STEP 1

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN STA. 540 HORIZONTAL SPAR CHORD BETWEEN LBL 0.07 AND LBL 24.82 IS CRACKED NEAR EDGE<[01] REMOVED AND REPLACED PANEL BREAK AT MAIN CABIN STA 540 LBL 0.07 AND LBL 24.82 AS PER SRM 51-40-02-0G-0 AND DWG 143A5240.;[02] VERIFIED STEP 1

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN STA. 540 HORIZONTAL SPAR CHORD BETWEEN RBL 24.82 AND RBL 45.57 HAS CRACKS AROUND FASTENERS<[01] REMOVED AND REPLACED PANEL BREAK AT STA 540 RBL 24.82 AND RBL 45.57 AS PER SRM 51-40-02-0G-0 AND DWG-143A5240.;[02] VERIFIED STEP 1

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN INTERCOSTAL CRACK AT LBL 13' BETWEEN STA 380-400<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN LBL 13' BETWEEN STA 380-400 AS PER SRM 51-40-02-0G-0 AND DWG 143A5400.;[02] VERIFIED STEP 1

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN INTERCOSTAL CRACK AT RBL 10' BETWEEN STA 380-400<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN RBL 10' BETWEEN STA 380-400 AS PER SRM 51-40-02-0G-0 AND DWG 143A5400.;[02] VERIFIED INSTALLATION

Part: INTERCOSTAL — CORRODED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FWD WET AREA CORROSION AT INTERCOSTAL UPPER SURFACE STA 294.5+11' LBL 12'<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 294.5 TO STA 312 LBL 11.6 SRM 51-40-02-0G-0 AND DWG 141A5600;[02] VERIFIED STEP 1

Part: FLOOR PANEL — FRAYED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 241YF UPPER SURFACE FRAYING<[01] RECEIVED NEW FLOOR PANEL 241YF. ISSUE TAG #E199910 PO#2039038.;[02] VERIFIED STEP 1

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN INTERCOSTAL CRACK AT LBL 12' BETWEEN STA 344-360<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWWEEN STA 344 TO STA 360 AND LBL 12' IN REF B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING #141A5400.;[02] VERIFIED STEP 1

Part: FLOOR PANEL — FRAYED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 242VF UPPER SURFACE FRAYING<[01] RECEIVED FLOOR PANEL NEW 242 VF FLOOR.<BR>PANEL WILL BE INSTALLED ON TTGQ00MWX5H.;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 242VF AND WILL BE INSTALLED AND T/C TTG8Q00MWX5H;[03] VERIFIED STEP 2

Part: FLOOR PANEL — FRAYED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 242UF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 242UF AND WILL BE INSTALLED ON T/C TTG8Q00MWX5K;[02] VERIFIED STEP 1

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM FASTENER HOLE STA 986.5 RBL 45'<[01] REMOVED CORROSION AT MAIN CABIN AFT WET AREA STA 986.5 AND RBL 45' REF SRM 51-10-02-0G-0PERFORMED UT THICKNESS INSP AT REWORKED AREA; IAW B 737 NDT PART 4 51-00-00 PROC 3. MINI THICK 0.126'. TOOL 27MG. BC 172139. CALIB DUE 3-30-24.ORIGINAL MATERIAL 0.150'; REMOVED MATERIAL 0.024'; REMAINING MATERIAL 0.126'; REWORKED AREA IS OUT OF LIMITS REF 53-70-51-1A-1 AND IT WAS REPAIRED PER EA M-21-153-00612 INSTRUCTIONS ON TASK CARD #TTG8Q00NM8E2;[02] RII/VERIFIED ENTRY #1 AS WORK ACCOMPLISHED & FOUND OUT OF LIMITS ; AND REPAIRED AS STATED ON ( REPAIRED PER EA M-21-153-00612 INSTRUCTIONS ON TASK CARD #TTG8Q00NM8E2.

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

CRACK FOUND AT AREA AFT OF FWD. CARGO COMPARMENT; LOCATED AT STA. 540 WL 208 RBL 1; SEE DOT # 31<[01] REMOVED AND REPLACE PANEL BREAK AT STA 540 WL 208 RBL 1. AS PER; SRM 51-40-02-0G-0 AND DWG 143A5240.;[02] CORRECTION ON STEP # 1: REMOVED AND REPLACED PANEL BREAK AT STA 540 WL 208 RBL 1. AS PER; SRM 51-40-02-0G-0 AND DWG 143A5240.;[03] VERIFIED STEP 2

Part: FLOOR PANEL — CORRODED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 221EF ONE EACH INSERT CORRODED<[01] REMOVED AND REPLACED INSERT AT MAIN CABIN FLOOR PANEL 221EF IN REF SRM-53-00-50-SR-0;[02] VERIFIED STEP 1

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN INTERCOSTAL CRACK AT BL 0' BETWEEN STA 277-294.5<[01] REMOVED AND REINSTALLED NEW INTERCOSTAL AT MAIN CABIN BL 0' BETWEEN STA 277-294.5 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED STEP 1

Part: FLOOR SUPPORT — CORRODED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN AFT WET AREA CORROSION AT FLOOR SUPPORT STRAP BETWEEN STA 1016-1040 LBL 3'<[01] CLEAN AREA AT FLOOR SUPPORT STRAP BETWEEN STA 1016-1040 AND LBL 3' REF SOPM 20-30-03; TREAD AND PRIMER REF AMM 51-21-41-370-803 & AMM 51-21-72-370-804;[02] VERIFIED STEP # 1

Part: FLOOR PANEL — FRAYED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 242TF UPPER SURFACE FRAYING<[01] RECEIVED NEW FLOOR PANEL 242TF. ISSUE TAG #E199903 PO#2039032.;[02] VERIFIED STEP 1

Part: FLOOR PANEL — CORRODED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 221BF SEVERAL INSERT CORRODED<[01] RECEIVED NEW FLOOR PANEL 221BF. ISSUE TAG WN35867 PO#2028887;[02] VERIFIED STEP 1

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM FASTENER HOLE STA 986.5 LBL 45'<[01] REMOVED CORROSION AT MAIN CABIN AFT WET AREA STA 986.5 AND LBL 45' REF SRM 51-10-02-0G-0;PERFORMED UT THICKNESS INSP AT REWORKED AREA; IAW B 737 NDT PART 4 51-00-00 PROC 3. MINI THICK 0.122'. TOOL 27MG. BC 172139. CALIB DUE 3-30-24.ORIGINAL MATERIAL 0.150'; REMOVED MATERIAL 0.028'; REMAINING MATERIAL 0.122'; REWORKED AREA IS OUT OF LIMITS REF 53-70-51-1A-1<BR> AND IT WAS REPAIRED PER EA M-21-153-00612 INSTRUCTIONS ON TASK CARD TTG8Q00NMAE9;[02] RII/VERIFIED ENTRY #1 AS WORK ACCOMPLISHED & FOUND OUT OF LIMITS ; AND REPAIRED AS STATED ON ( REPAIRED PER EA M-21-153-00612 INSTRUCTIONS ON TASK CARD #TTG8Q00NMAE9.

Part: FLOOR PANEL — FRAYED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 241ZF UPPER SURFACE FRAYING<[01] RECEIVED FLOOR PANEL NEW 241ZF FLOOR.<BR>PANEL WIL BE INSTALLED ON TASK CARD TTGQOOMWX03.;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 241ZF AND WILL BE INSTALLED ON T/C TTG8Q00MWX03;[03] VERIFIED STEP 2

Part: FLOOR PANEL — FRAYED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 241XF UPPER SURFACE FRAYING<[01] RECEIVED FLOOR PANEL NEW 241XF FLOOR PANEL.<BR>PANEL WILL BE INSTALLED ON TASK CARD TTG8Q00MWX5D.;[02] RECEIVED MAIN CABIN FLOOR PANEL 241XF AND WILL BE INSTALLED ON T/C TTG8Q00MWWZ7;[03] VERIFIED STEP 2

Part: FLOOR PANEL — CORRODED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 241ACF SEVERAL INSERT CORRODED<[01] REMOVED AND REPLACED SEVERAL INSERTS AT MAIN CABIN FLOOR PANEL 241ACF IN REF SRM-53-00-50-2R-0-A00938;[02] VERIFIED STEP 1

Part: FLOOR PANEL — FRAYED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 241ABF UPPER SURFACE FRAYING<[01] RECEIVED FLOOR PANEL NEW 241 ABF FLOOR.<BR>PANEL WILL BE INSTALLED ON TASK CARD TTG8Q00MWWZZ.;[02] VERIFIED STEP 1

Part: FLOOR PANEL — CORRODED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 221CF SEVERAL INSERT CORRODED<[01] RECEIVED NEW FLOOR PANEL 221CF. ISSUE TAG E199911 PO#2039277;[02] VERIFIED STEP 1

Part: FLOOR PANEL — CORRODED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN FLOOR PANEL 241ADF SEVERAL INSERT CORRODED<[01] REMOVED AND REPLACED SEVERAL INSERTS AT MAIN CABIN FLOOR PANEL 241ADF IN REF SRM-53-00-50-2R-0-A00938;[02] VERIFIED STEP 1

Part: DEFLECTOR — DAMAGED (RT WING) · airframe 50,935 hrs · 30,834 cycles

RH WING DEFLECTOR PANEL ATTACH SERRATED PLATE HOLES ELONGATED<[01] ACCOMPLISHED REPAIR AT RIGHT WING DEFLECTION CONTRL RIB IN REF B737-700 SRM 57-51-02-2R-1; REPAIR 1.;[02] VERIFIED STEP 1

Part: SEAT TRACK — CORRODED (ZN 200 FUS TOP) · airframe 50,935 hrs · 30,834 cycles

MAIN CABIN CORROSION AT SEAT TRACK CROWN BOTTOM STA 663.75+12' RBL 24.75<[01] REMOVED DAMAGE FROM SEAT TRACK AT STA 663.75 RBL 24.75 FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1; FIG.103;DETAIL: 'A'. TOOL USED: BC: WN0012; DUE DATE: 4/18/24; PERFORMED SEAT TRACK REPAIR AS PER SRM 53-00-52-2R-3.;[02] VERIFIED STEP 1

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 50,935 hrs · 30,834 cycles

RT HORIZONTAL STABILIZER RIB #4 STIFFENER #4 CRACK AT LOWER SECTION<[01] REMOVED CRACK AT RT HORIZONTAL STABILIZER RIB #4 STIFFENER #4 AND FIRST HOLE FWD OF LOWER SECTION COMMON TO STIFFENER #4 REF SRM 51-10-02-0G-0 AND INSTALLED REPAIR PARTS AT RIGHT HORIZONTAL STAB RIB # 4 COMMON TO STIFFENER #4 REF SRM 55-10-09-2R-5.;[02] CORRECTION TO STEP 1. REMOVED CRACK AT RT HORIZONTAL STABILIZER RIB #4 STIFFENER #4 AND FIRST HOLE FWD OF LOWER SECTION COMMON TO STIFFENER #4 REF SRM 51-10-02-0G-0 AND INSTALLED REPAIR PARTS AT RIGHT HORIZONTAL STAB RIB # 4 COMMON TO STIFFENER #4 REF SRM 55-10-09-2R-5. THIS WORK WAS ACCOMPLIOSHED IN CONJUCTION WITH TTG8Q00NMWM0;[03] RII /VERIFIED ENTRY #2 AS A CORRECT ENTRY FOR WORK ACCOMPLISHED AS A CORRECTIVE ACTION TAKEN & ALSO APPLYS TO ENTRY #1 AS A CORRECTION OF INFO. ENTERD. RII/VERIFIED TT# ENTERD WAS WORKED IN CONJUCTION WITH THIS N/R CARD.

Part: DOUBLER — CRACKED (ZN 100 FUS LOWER) · airframe 50,935 hrs · 30,834 cycles

EXTERNAL GROUND POWER RECEPTACLE AFT CUTOUT LOWER AREA HAS MISSING SHIM OF PREVIOUS REPAIR & CRACKED SKIN DOUBLER.<[01] REMOVED AND REPLACED EXTERNAL GROUND POWER RECEPTACLE (EGPR) INNER DOUBLER AT STA 219.8 - STA 244 STR 19R - STR 24R REF SRM 51-40-02-0G-0 AND DWG 141A3702. TREATED; PRIMED ; AND TOP COAT AS REQUIRED REF AMM 51-21-73-370-803; AMM 51-21-72-370-801;[02] VERIFIED STEP 1

Part: RIB — CRACKED (ZN 600 RIGHT WIN) · airframe 50,935 hrs · 30,834 cycles

LEADING EDGE SLAT #5 STA 85.19 NOSE SKIN ACTUATOR RIB CRACK AT O/B SECOND FASTENER HOLE FROM AFT EDGE<[01] PERFORMED REPAIR ON LEADING EDGE SLAT #5 STA 85.19 NOSE SKIN ACTUATOR RIB IAW SRM 57-42-01-2R-8 REPAIR 8 FIG 202 SHEET 4.;[02] VERIFIED STEP 1

Part: MOUNT — CRACKED (DOOR SLIDE) · airframe 50,770 hrs · 30,730 cycles

FORWARD SERVICE CABIN DOOR (R1). AFT SLIDE MOUNT BRACKET UPPER ISOLATOR IS CRACKED.<[01] R&R FORWARD SERVICE CABIN DOOR (R1). AFT SLIDE MOUNT BRACKET UPPER ISOLATOR IAW SRM 51-40-02.;[02] C/W INSPECTION PER SRM 51-40-02.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 50,686 hrs · 30,675 cycles

RH AFT EMERGENCY BATTERY PACK IS INOP.<[01] R&RR/H AFT EMER BATTERY PER AMM 33-51-06; OPSC HECKK GOOD AT THIS TIME.

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 50,047 hrs · 30,277 cycles

RAMP REPORTS CRACK IN AFT CARGO COMP FLOOR<[01] MADE PERM REPAIR AFT CARGO COMP FLOOR AMM 25-52-01

Part: GIRT BAR — OUT OF POSITION (ZN 800 DOOR) · airframe 49,275 hrs · 29,755 cycles

SLIDE ON DOOR R1 STUCK IN THE DISARMED POSITION<[01] POSITIONED GRIT BAR INTO PROPER STOW POSITION PER S.I.P.

Part: TRACK — CRACKED (SLIDING SEAL) · airframe 48,999 hrs · 29,564 cycles

TAIL L/H UPPER AFT SLIDING SEAL TRACK IS CRACKED<[01] R+R UPPER AFT L/H STAB SLIDING SEAL TRACK IAW AMM 20-50-11.

Part: SUPPORT BRACKET — BROKEN (KEEL BEAM) · airframe 48,999 hrs · 29,564 cycles

FWD KEEL BEAM PANEL 192E FWD LEFT SUPPORT BRACKET BROKEN. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 48,999 hrs · 29,564 cycles

AFT ONE THIRD OF CABIN EMERGENCY LIGHTS FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK M01673 IAW AMM 33-51-06. ALL CHECKED GOOD.

Part: SEAL — LOOSE (HORIZONTAL STAB) · airframe 48,999 hrs · 29,564 cycles

TAIL LEFT UPPER AFT SLIDING SEAL HAS LOOSE RUB STRIP. REMOVED AND REPLACED 333AT SLIDING SEAL REF SRM 51-40-02.

Part: TRACK — CRACKED (SLIDING SEAL) · airframe 48,999 hrs · 29,564 cycles

TAIL R/H UPPER AFT SLIDING SEAL TRACK IS CRACKED<[01] R+R UPPER AFT R/H STAB SLIDING SEAL TRACK IAW AMM 20-50-11.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 48,092 hrs · 28,967 cycles

FWD SERVICE AND ENTRY DOOR EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW / [01] R&R LIGHT LENS COVERS WITH ARROW COVERS IAW AMM 33-51-01.;[02] INSPECTED

Part: LIGHT — INOPERATIVE (AFT SERVICE DOOR) · airframe 47,512 hrs · 28,551 cycles

AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP / [01] R&R AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT LAMP PER AMM 33-51-04. OPS CHECK GOOD

Part: EPSU — INOPERATIVE (PAX CABIN) · airframe 47,111 hrs · 28,271 cycles

EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST AT POSITIONS M1675; M1669; AND M1672 / [01] REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACKS AT POSITIONS M1675; M1669; AND M1672 PER ENG DWG 33500005 AND AMM 33-51-06

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 47,111 hrs · 28,271 cycles

EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST AT POSITIONS M1675; M1669; AND M1672 / [01] REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACKS AT POSITIONS M1675; M1669; AND M1672 PER ENG DWG 33500005 AND AMM 33-51-06

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 47,111 hrs · 28,271 cycles

EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST AT POSITIONS M1675; M1669; AND M1672 / [01] REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACKS AT POSITIONS M1675; M1669; AND M1672 PER ENG DWG 33500005 AND AMM 33-51-06

Part: NONE — OUT OF ADJUST (AFT SERVICE DOOR)

ASD ESCAPE SLIDE GIRT CATCHES ON THRESHOLD WHILE OPENING DOOR ; / [01] REPACKED ASD GIRT PER AMM 25-66-01-400-804 STEP 6.D(1(C-H); [02] CORRECTION FOR ITEM 1:<BR>REPACKED ASD ESCAPE SLIDE GIRT PER AMM 25-66-01-400-804 STEP 6.D(1(C-H); [03] VERIFIED CORRECTIVE ACTION 1-2.<BR><BR>VERIFIED GIRT NO LONGER CATCHES WHILE OPENING.

Part: NONE — INOPERATIVE (CABIN) · airframe 45,503 hrs · 27,299 cycles

FORWARD TWO FLASHLIGHT ARE DEAD. ; / [01] REMOVED AND REPLACED BATTERIES ON FORWARD ATTENDANT 2 EA. FLASHLIGHTS PER AMM 25-64-00-900-806.; [02] VERIFIED CORRECTIVE ACTION 1.

Part: ATTACH ANGLE — CRACKED (CENTER WING) · airframe 45,503 hrs · 27,299 cycles

B.S. 663 BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8; W.L. 164. ; / [01] TRIMED OUT ATTACH ANGLE AT VAPOR BARRIER BS 663 RBL 15 WL 164 PER SRM 57-10-10-2R-5 STEP 4 B<BR><BR>PERFORMED DETAIL INSPECTION OF THE REPAIR AREA AND UNDERLYING STRUCTURE TO MAKE SURE THAT THERE IS NO DAMAGE WITHIN THE REPAIR AREA; [02] PERFORM AN OPEN HOLE HFEC INSPECTION FOR ALL INITIAL FASTENERS HOLES IN THE REPAIR AREA TO MAKE SURE THERE IS NO DAMAGE; [13] REPAIRED CRACKED VAPOR BARRIER BULKHEAD UPPER ATTACH ANGLE BS 663 RBL 15 WL 164 PER SRM 57-10-10-2R-5; [14] VERIFIED CORRECTIVE ACTION 13

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

ACB FWD CORNER SCUFF PLATE CRACKED ; / [01] RECEIVED NEW AFT FWD SCUFF PLATE P/N 654A0004-97; LOCATED AND DRILLED SCUFF PLATE IAW SRM 51-40-05 AND DWG 143A8341 ID:007; REV:A<BR><BR>INSTALL SCUFF PLATE WILL BE ACCOMPLISHED ON C.C. TTG8Q002EGBV.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] CLARIFICATION TO STEP 1: RECEIVED NEW AFT CARGO BAY FORWARD SCUFF PLATE P/N 654A0004-97; LOCATED AND DRILLED SCUFF PLATE IAW SRM 51-40-05 AND DWG 143A8341 ID:007; REV:A

Part: GUSSET — CRACKED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

FCB GUSSET IS CRACKED AT BS500D S-19L WL190 ; / [01] REMOVED FCB GUSSET AT BS 500D STR 19L WL 190 IAW SRM 51-40-02; [02] LOCATED AND DRILLED NEW FCB GUSSET AT BS 500D STR 19L; PN#143A9481-6 IAW SRM 51-40-05 AND IAW DWG# 143A7902... OK TO INSTALL; [03] VERIFIED LOCATED AND DRILLED NEW GUSSET PER SRM 51-40-05 AND DWG 143A7902. OK TO INSTALL; [04] INSTALLED NEW FCB GUSSET AT BS500D S-19L WL 190; IAW SRM 51-40-02-0G-0 AND DWG#143A7902; [05] VERIFIED CORRECTIVE ACTION 4.; [06] VERIFIED ALL WORK ACCOMPLISHED.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

FCB GUSSET IS CRACKED AT BS500D S-19R WL190 ; / [01] REMOVED FCB GUSSET AT BS 500D STR19R WL 190 IAW SRM 51-40-02; [02] LOCATED AND DRILLED NEW FCB GUSSET AT BS 500D STR 19R; PN#143A9481-5 IAW SRM 51-40-05 AND IAW DWG# 143A7902... OK TO INSTALL; [03] VERIFIED LOCATED AND DRILLED NEW GUSSET PER SRM 51-40-05 AND DWG 143A7902. OK TO INSTALL; [04] INSTALLED NEW GUSSET AT BS500D S-19R WL190; IAW SRM 51-40-02-0G-0 AND DWG#143A7902; [05] VERIFIED CORRECTIVE ACTION 4.; [06] VERIFIED ALL WORK ACCOMPLISHED.

Part: PANEL — PULLED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

PANEL 561CB HAS SEVERAL PULLED FASTENER HOLES (MARKED) ; / [01] IDENTIFIED PANEL 561CB MATERIAL IAW SRM 57-51-01-0I-1 FIGURE 3. SHEET 1;ITEM [10] AND TABLE 3. ITEM [10].<BR><BR>CLEANED PANEL AND REMOVED FINISH AS NEEDED TO EVALUATE DAMAGE IAW AMM 51-21-11-150-815 PARA. 17. C. AND D<BR><BR>VISUAL INSPECTION FOUND DAMAGE TO GLASS FIBER PLIES TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4. B. (2)<BR><BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-05-2R-9 AS GIVEN IN SRM 57-51-01-2R-1 PARA 2.E.<BR><BR> REMOVED FULL DEPTH EDGEBAND PLY DAMAGE FROM 29 EA FASTENER HOLES ON THE AFT EDGE; WITH NO MOISTURE OR CONTAMINATION NOTED THEN CLEANED REPAIR AREA. AREA OF REMOVED DAMAGE IS LESS THAN 0.5' DIA. ALL IAW SRM 51-70-05-2R-9 PARA 4. A-C.;[10] FABRICATED REPAIR PLIES FROM BMS9-3 TYH2 LOT 1458851-1; INSTALLED PLIES WITH BMS8-301 CLASS 1 LOT JH1CAA0868.<BR><BR> ASSEMBLED VACUUM BAG AND LEAK CHECKED GOOD USING VACUUM GAGE ID: ATS2584 S/N: 5432766772.<BR><BR>SET PLIES TO CURE USING HOTBONDER I/D: NCX000523 S/N: 11051262. ALL IAW SRM 51-70-04-2R-9 PARA 4. J. - M.; [11] CURED REPAIR PLIES REMOVED BAGGING MATERIAL AND LIGHTLY SANDED IAW SRM 51-70-04-2R-9 PARA 4.M.REQUEST POST CURE NDI TO VERIFY NO DISBONDS IAW SRM 51-70-04-2R-9 PARA 4.O.; [12] VERIFIED CORRECTIVE ACTION ITEMS 10 AND 11.<BR><BR>UT INSPECTED REPAIR PER NDTM PART 4; 51-00-02. NO DISBONDS NOTED.<BR><BR>CAL ID: ATS2341 S/N: 190848104; [13] REFINISHED INNER AND OUTER SURFACE OF PANEL IAW SRM 51-70-04-2R-9 PARA 4 P.

Part: INTERCOSTAL — CORRODED (BS 767) · airframe 45,503 hrs · 27,299 cycles

CORROSION FOUND ON INTERCOSTAL AT RBL 20; WL153; STA767+5 AND STA767+6 ; / [01] REMOVED INTERCOSTAL FROM BS 767 TO BS 867; RBL 20; WL 153 IAW SRM 51-40-02-0G-0; [02] VERIFIED COMPLETE STEPS 1; 2.; [03] REMOVED CORROSION FROM INTERCOSTAL AFT CARGO BAY BS767+5'' RBL20 WL153; P/N 146A8123U19; IN AREA .7''X.3''X0.020'' DEEP; ORIGINAL THICKNESS 0.063''; REMAINING MAT. THICKNESS 0.043' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1 STEP 4.B. (2) FIGURE 102. TOOL USED: DEPTH GAGE ID:ATS2472; DUE DATE: 06/2022; [04] VERIFIED CORRECTIVE ACTION ENTRY 3.; [05] RECEIVED NEW INTERCOSTAL LOCATED AND DRILLED MAT. ITEM#146A8123U19; LOT#1470503-2 FROM BS767 TO BS787 RBL 20 WL 153 IAW.SRM 51-40-05-0G-0; DWG 146A8123; [06] VERIFIED DRILLED MAT. ITEM#146A8123U19; LOT#1470503-2 FROM BS767 TO BS787 RBL 20 WL 153 IAW.SRM 51-40-05-0G-0; DWG 146A8123.; [07] OK TO INSTALL NEW INTERCOSTAL.; [08] VERIFIED OK TO INSTALL.; [09] INSTALLED NEW INTERCOSTAL AFT CARGO BAY AT BS 767 TO BS 787 RBL 20 WL 153 IAW SRM 51-40-02-0G-0 DWG 146A0081; [10] VERIFIED INSTALLATION OF NEW INTERCOSTAL AFT CARGO BAY AT BS 767 TO BS 787 RBL 20 WL 153 IAW SRM 51-40-02-0G-0 DWG 146A0081; [11] TASK COMPLETE

Part: PANEL — PULLED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

PANEL 193B HAS SEVERAL PULLED THROUGH CRACKED FASTENER HOLES ; / [01] IDENTIFIED PANEL / MATERIAL 193B IAW SRM 53-40-70-0I-1 FIG. 2. TABLE 2. ITEM (13).<BR><BR>FOUND 3EA. CRACKED FASTENER HOLE DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4. B. (2) (A). <BR><BR>REPAIR WILL BE ACCOMPLISHED IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1.<BR><BR>REMOVED CRACKED DAMAGE AT 3EA. FASTENER HOLES ON L/E EDGE BAND & CLEANED REPAIR AREAS. NO CONTAMINATION OR WATER NOTED IAW SRM 51-70-05-2R-6. PARA 4. A. - D.; [02] VALIDATED APPLICABILITY OF REPAIR TO BE COMPLETED IAW SRM 51-70-05-2R-6 AS GIVEN IAW SRM 53-40-70-2R-1.; [11] PANEL 193B WITH SEVERAL PULLED THROUGH CRACKED FASTENER HOLES WERE REPAIRED IAW SRM 51-70-05-2R-6; [12] VERIFIED CORRECTIVE ACTIONS 10 AND 11

Part: ANGLE — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON ANGLE P/N 146A8125-53 ATTACHED TO INTERCOSTAL BS 767+5 WL 153 ; / [01] REMOVED DAMAGE ON ANGLE ATTACHED TO INTERCOSTAL AT BS 767 +5 WL 153; RBL 20 AREA .9' X 2' X .010' IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM ; IT'LL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.C.; [02] VERIFIED REMOVED DAMAGE ON ANGLE ATTACHED TO INTERCOSTAL AT BS 767 +5 WL 153; RBL 20 AREA .9' X 2' X .010' IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM ; IT'LL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.C.; [03] RECEIVED NEW ANGLE ITEM:146A8125-53 LOT:1463430-1. <BR>LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G-0 AND DRAWING:146A8123.<BR>OK TO INSTALL; [04] VERIFIED LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G-0 AND DRAWING:146A8123. <BR>VERIFIED OK TO INSTALL.; [05] INSTALLED NEW ANGLE ATTACHED TO INTERCOSTAL AFT CARGO BAY AT BS 767 TO BS 787 RBL 20 WL 153 IAW SRM 51-40-02-0G-0 DWG 146A8123; [06] VERIFIED INSTALLATION OF NEW ANGLE ATTACHED TO INTERCOSTAL AFT CARGO BAY AT BS 767 TO BS 787 RBL 20 WL 153 IAW SRM 51-40-02-0G-0 DWG 146A8123; [07] CORRECTED ON PART REQUIREMENT; [08] CORRECTED ON PART REQUIREMENT; [09] VERIFIED JOB IS COMPLETE

Part: STRAP — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON ACB FLOORBOARD SPLICE STRAP TOP SURFACE AT BS 767+5.5; WL 153; LBL 2.5; LBL 10; LBL 15; LBL 16; RBL 3; RBL 4.2; RBL 8; RBL 10.5 & RBL 14.3 ; / [01] VERIFIED COMPLETE STEPS 1 - 9.; [02] RECEIVED NEW ACB FLOORBOARD SPLICE STRAP BS 767 +5.5; WL 153 ; FROM RBL 21 TO LBL 21 P/N 146A9401-4 LOT# 1467541.<BR><BR>INSTALL PART WILL BE ACCOMPLISHED ON C.C. TTG8Q004E68F.; [03] VERIFIED RECEIVED NEW ACB FLOORBOARD SPLICE STRAP BS 767 +5.5; WL 153 ; FROM RBL 21 TO LBL 21 P/N 146A9401-4 LOT# 1467541.<BR>VERIFIED INSTALL PART WILL BE ACCOMPLISHED ON C.C. TTG8Q004E68F.

Part: PANEL — PULLED (R/H WING) · airframe 45,503 hrs · 27,299 cycles

RT WING T/E PANEL 661CB AFT ROW OF FASTENERS HOLES HAS MULTIPLE HOLES WHERE FASTENERS HAVE PULLED THROUGH ; / [01] IDENTIFIED PANEL 661CB IAW SRM 57-51-01-0I-1 FIGURE 3 ITEM [10] AND TABLE 3 ITEM [10]. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B.(2) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-9 PER SRM 57-51-01-2R-1 PARA 2.E. REMOVED FULL DEPTH EDGEBAND PLY DAMAGE FROM NUMEROUS FASTENER HOLES ON THE AFT EDGE; MAX AREA OF REMOVED DAMAGE IS 0.5' ALSO CLEANED REPAIR AREA. WORK ACCOMPLISHED IAW SRM 51-70-05-2R-9 PARA 4/A-C.; 05] APPLIED SLURRY MIXTURE OF BMS 8-301 CL1 LOT# JH1CAA0868 AND CHOPPED FIBERS TO FASTENER LOCATIONS. <BR>SET TO CURE WITH HEAT LAMP MONITORED WITH THERMOMETER ID: ATS2209 S/N: 43300739WS <BR>IAW SRM 51-70-05-2R-9 PARA 4D-F.; [06] CURED SLURRY; SANDED FLUSH; CLEANED REPAIR AREA; FABRICATED REPAIR PLIES FROM BMS9-3 TYH2 LOT 1458851-1; INSTALLED PLIES WITH BMS8-301 CLASS 1 LOT JH1CAA0868; VACUUM BAGGED; VERIFIED 5X5 AND SET PLIES TO CURE USING HOTBONDER I/D: NCX000526 S/N: 12051216. WORK ACCOMPLISHED IAW SRM 51-70-05-2R-9 PARA 4.F AND H-M. 11] REFINISHED PANEL IAW SRM 51-70-05-2R-9 PAR 4O AND AMM 51-21-99-300-802 PAR 3C(1)(D-E).; [12] VERIFIED CORRECTIVE ACTIONS 9 AND 10

Part: PANEL — PULLED (R/H WING) · airframe 45,503 hrs · 27,299 cycles

RT WING T/E PANEL 661AB AFT ROW OS FASTENER HOLES HAS MULTIPLE HOLE WHERE FASTENER HAS PULLED THROUGH ; / [01] IDENTIFIED PANEL 661CB IAW SRM 57-51-01-0I-1 FIGURE 3 ITEM [5] AND TABLE 3 ITEM [5]. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B.(2) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-9 PER SRM 57-51-01-2R-1 PARA 2.E. REMOVED FULL DEPTH EDGEBAND PLY DAMAGE FROM ALL THE FASTENER HOLES ON THE AFT EDGE; MAX AREA OF REMOVED DAMAGE IS 0.5' ALSO CLEANED REPAIR AREA. WORK ACCOMPLISHED IAW SRM 51-70-05-2R-9 PARA 4.A-C.; [02] CORRECTION TO ITEM 1: CORRECT PANEL IS 661AB NOT 661CB.VALIDATED APPLICABILITY OF SRM 51-70-05-2R-9.; [03] INSPECTED DAMAGE REMOVAL AND VERIFIED CORRECTIVE ACTIONS 1 AND 2. OKAY TO PROCEED PER SRM 51-70-05-2R-9.; [04] APPLIED SLURRY MIXTURE OF BMS 8-301 CL1 LOT# JH1CAA0868 AND CHOPPED FIBERS TO FASTENER LOCATIONS. <BR>SET TO CURE WITH HEAT LAMP MONITORED WITH THERMOMETER ID: ATS2209 S/N: 43300739WS <BR>IAW SRM 51-70-05-2R-9 PARA 4D-F.; [05] CURED SLURRY; SANDED FLUSH; CLEANED REPAIR AREA; FABRICATED REPAIR PLIES FROM BMS9-3 TYH2 LOT 1458851-1; INSTALLED PLIES WITH BMS8-301 CLASS 1 LOT JH1CAA0868; VACUUM BAGGED; VERIFIED 5X5 AND SET PLIES TO CURE USING HOTBONDER I/D: NCX000523 S/N: 11051262. WORK ACCOMPLISHED IAW SRM 51-70-05-2R-9 PARA 4.F AND H-M.;[10] REFINISHED PANEL IAW SRM 51-70-05-2R-9 PAR 4O AND AMM 51-21-99-300-802 PAR 3C(1)(D-E).

Part: PANEL — CRACKED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

PANEL 661BB HAS MULTIPLE PULLED THROUGH CRACKED FASTENER HOLES ON AFT EDGE ; / [01] IDENTIFIED PANEL 661CB IAW SRM 57-51-01-0I-1 FIGURE 3 ITEM [9] AND TABLE 3 ITEM [9]. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B.(2) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-9 PER SRM 57-51-01-2R-1 PARA 2.E. REMOVED FULL DEPTH EDGEBAND PLY DAMAGE FROM ALL THE FASTENER HOLES ON THE AFT EDGE; MAX AREA OF REMOVED DAMAGE IS 0.5' ALSO CLEANED REPAIR AREA. WORK ACCOMPLISHED IAW SRM 51-70-05-2R-9 PARA 4.A-C.; [02] CORRECTION TO ITEM 1: CORRECT PANEL IS 661BB NOT 661CB.VALIDATED APPLICABILITY OF SRM 51-70-05-2R-9.;

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON AFT CARGO R/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 RBL 22 STA 727+10; RBL 22 STA 727A+6; RBL 22 STA 727A+10; RBL 22 STA 727B+2; RBL 22 STA 727B+6; RBL 22 STA 727B+10; ; RBL 22 STA 727B+14; RBL 22 STA 727B+18; RBL 22 STA 727C+2; RBL 22 STA 727C+6. / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-6.; [02] DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727+10 TO BS 727B+10 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS; [03] VERIFIED DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727+10 TO BS 727B+10 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS.

Part: STRAP — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON AFT CARGO BAY AFT BULKHEAD SUPPORT STRAP AT STA 947; WL 153; RBL 4 & RBL 6. ; / [01] EVALUATED CORROSION DAMAGE ON AFT BULKHEAD SUPPORT STRAP AT ACB STA 947 WL 153 RBL 4 AND 6 FOUND TO BE OUT OF LIMITS DUE NO LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION 1; [11] INSTALLED NEW BULKHEAD SUPPORT STRAP AT AFT CARGO BAY; BS947; RBL4; WL153. IAW SRM 51-40-02-0G-0 AND DWG#149A8117; [12] VERIFIED CORRECTIVE ACTION 11; [13] VERIFIED JOB COMPLETE

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON AFT CARGO R/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 RBL 20 STA 747+8; RBL 22 STA 747+8; RBL 20 STA 747+10; RBL 20 STA 747+12; RBL 22 STA 747+14; RBL 22 STA 747+16. ; / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-6.; [02] DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 747+8 TO BS 747+14 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS; [03] VERIFIED DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 747+8 TO BS 747+14 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS.

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 45,503 hrs · 27,299 cycles

RIGHT HAND HORIZONTAL STAIBILIZER INSPAR RIB; 120.30; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] TRIMMED OUT THE DAMAGED PART OF THE RIB AT R/H HORIZ. STAB INSPAR RIB 120.3 3RD VERTICAL STIFFENER; CUT OUT DIMENSIONS 0.5' X 0.250' IAW SRM 55-10-09-2R-4.; [02] TRIMMED OUT THE DAMAGED PART OF THE RIB AT R/H HORIZ. STAB INSPAR RIB 120.3 3RD VERTICAL STIFFENER; CUT OUT DIMENSIONS 0.5' X 0.250' IAW SRM 55-10-09-2R-4. STEP 4B; [10] INSTALLED REPAIR PARTS AT RH HORIZONTAL STABILIZER STA 120.3 RIB 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4; [11] VERIFIED INSTALLATION OF REPAIR PARTS PER SRM 55-10-09-2R-4; [12] CHANGED REPAIR TYPE TO MAJOR; [13] TASK COMPLETE

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT STA 727E+18; LBL 20; STA 727E+18; LBL 22; STA 747+2; LBL 22; STA 747+5; LBL 20; STA 747+7; LBL 22; STA 747+9; LBL 20; STA 747+14; LBL 22; STA 747+18; ; LBL 22; STA 747+19; LBL 20; STA 767+3; LBL 22. / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-10.; [02] DAMAGE FOUND ON ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727E+18 TO BS 747+18 LBL 22 FOUND TO BE OUT OFF LIMIT AND WILL BE REPLACED WITH CUSTOMER CARD #TTG8Q00718NX; [03] VERIFIED DAMAGE FOUND ON ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727E+18 TO BS 747+18 LBL 22 FOUND TO BE OUT OFF LIMIT AND WILL BE REPLACED WITH CUSTOMER CARD #TTG8Q00718NX.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON AFT CARGO DOOR CUTOUT FWD SHIELD AT STA 767+3; RBL 22; AND STA 767+5; RBL 21. ; / [01] VERIFIED COMPLETE STEPS 1; 2.; [02] RECEIVED NEW SHIELD ITEM:146A8127U12ATSMRO LOT:1467562.<BR>LOCATED AND DRILLED NEW ACB FWD SHIELD IAW SRM 51-40-05-0G-0 AND DRAWING:146A8127.; [03] INSTALLATION OF ACB FWD SHIELD IS DOCUMENTED ON CUSTOMER CARD: CPCP/AD MOC 5360-E-16462-NG CUSTOMER SYSTEM ID:TTG8Q004E68F; [04] ADDED PART NUMBER; [05] VERIFIED LOCATED AND DRILLED NEW ACB FWD SHIELD IAW SRM 51-40-05-0G-0 AND DRAWING:146A8127. <BR>VERIFIED INSTALLATION OF ACB FWD SHIELD IS DOCUMENTED ON CUSTOMER CARD: CPCP/AD MOC 5360-E-16462-NG CUSTOMER SYSTEM ID:TTG8Q004E68F.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON AFT CARGO R/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 RBL 20 STA 727E+2; RBL 22 STA 727E+3; RBL 22 STA 727E+6; RBL 20 STA 727E+8; RBL 22 STA 727E+10; RBL 20 STA 727E+12; ; RBL 22 STA 727E+14; RBL 22 STA 727E+18; RBL 22 STA 747+5. / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-6.; [02] LOCATED AND DRILLED NEW ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 767; RBL 22; WL 153; MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5093799-1 IAW SRM 51-40-05-0G-0 AND DWG#146A7502 OK TO TREAT AND PRIME; [03] VERIFIED LOCATED AND DRILLED NEW ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 767; RBL 22; WL 153; MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5093799-1 IAW SRM 51-40-05-0G-0 AND DWG#146A7502.<BR>VERIFIED OK TO TREAT AND PRIME.; [04] APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 767 RBL 22 WL 153 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02; [05] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 767 RBL 22 WL 153 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02.; [06] INSTALLATION OF ACB FLOOR TO SIDE WALL SUPPORT BS 727 TO BS 767 RBL 22 WL 153 WILL BE ACCOMPLISHED WITH CUSTOMER MOC CARD# TTG8Q004E68F; [07] VERIFIED INSTALLATION OF ACB FLOOR TO SIDE WALL SUPPORT BS 727 TO BS 767 RBL 22 WL 153 WILL BE ACCOMPLISHED WITH CUSTOMER MOC CARD# TTG8Q004E68F.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 22; WL 153; STA 887+7; AND STA 907+2. ; / [01] VERIFIED COMPLETE STEPS 1; 2.; [02] CORRECTION : DAMAGE IS ON FLOOR TO SIDEWALL SUPPORT AT RBL 22; STA 887 +7 AND STA 907 +2; INSTEAD OF SHIELD.; [03] FABRICATED ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 867 TO BS 947 RBL 22 WL 153 MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5095753-1 IAW SRM 51-40-05-0G-0 ; DWG#147A7501 AND DWG#146A7502 OK TO TREAT AND PRIME; [04] VERIFIED FABRICATED ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 867 TO BS 947 RBL 22 WL 153 MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5095753-1 IAW SRM 51-40-05-0G-0 ; DWG#147A7501 AND DWG#146A7502.<BR>VERIFIED OK TO TREAT AND PRIME.; [05] APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 867 TO BS947 RBL 22 WL 153 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02 ; INSTALLATION WILL BE ACCOMPLISHED WITH CUSTOMER MOC CARD # TTG8Q004E68F; [06] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 867 TO BS947 RBL 22 WL 153 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02. <BR>VERIFIED INSTALLATION WILL BE ACCOMPLISHED WITH CUSTOMER MOC CARD # TTG8Q004E68F.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT WL 153; STA 767+10; LBL 22; STA 767+14; LBL 22; STA 787+10; LBL 22; STA 787+14; LBL 22. ; / [01] CORRECTED MEASUREMENTS; [02] VERIFIED ACCOMPLISHMENT OF STEPS 1-4.; [03] FABRICATED ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 847 LBL 22 WL 153 WITH SPLICER ANGLE AT BS 727E+10 MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5095753-1 IAW SRM 51-40-05-0G-0 AND DWG# 146A7502 OK TO TREAT AND PRIME; [04] VERIFIED FABRICATED ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 847 LBL 22 WL 153 WITH SPLICER ANGLE AT BS 727E+10 MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5095753-1 IAW SRM 51-40-05-0G-0 AND DWG# 146A7502.<BR>VERIFIED OK TO TREAT AND PRIME.; [05] APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB FLOOR TO SIDE WALL SUPPORT AND SPLICE ANGLE BS 727 TO BS 847 LBL 22 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02 AND WILL BE INSTALLED WITH CUSTOMER MOC CARD# TTG8Q004E68F; [06] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB FLOOR TO SIDE WALL SUPPORT AND SPLICE ANGLE BS 727 TO BS 847 LBL 22 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02. <BR>VERIFIED WILL BE INSTALLED WITH CUSTOMER MOC CARD# TTG8Q004E68F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 578 AND 663.75; L.B.L. 45.5; W.L. 208.1. ; / [01] COMPLETED STEPS 1;2; [02] VERIFIED COMPLETION OF ALL CORROSION REMOVAL STEPS; [03] APPLIED CHEMICAL CONVERSION COATING AND ONE LAYER OF ALUMINIZED EPOXY PRIMER TO REWORKED AREA IAW SRM 51-20-01 AND SOPM 20-41-04; [04] VERIFIED CORRECTIVE ACTIONS 3

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON ACB FLOOR SUPPORT AT WL 153; WL 7; STA 767+6 AND STA 767+14. ; CORROSION IS LOCATED AT LBL 7; NOT WL 7. / [01] VERIFIED PARTIAL UPDATES STEP 1; 2.; [02] VERIFIED UPDATED STEPS 1 AND 2 COMPLETE; [03] ALL ITEMS ARE COMPLETE; [04] CORRECTION FOR STEP 2 DAMAGE EVALUATION: LOCATION IS BS 767+14; WL 153; LBL 7; [05] ALL WORK STEPS COMPLETE; REQUESTING FINAL BUYOFF; [06] VERIFIED ALL WORK COMPLETE. VERIFIED CORRECTIVE ACTION 4.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON AFT CARGO R/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 RBL 22 STA 727C+10; RBL 22 STA 727C+14; RBL 22 STA 727C+18; RBL 22 STA 727D+3; RBL 22 STA 727D+5; RBL 22 STA 727D+6; ; RBL 22 STA 727D+7; RBL 22 STA 727D+10; RBL 20 STA 727D+10; RBL 22 STA 727D+14. / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-6.; [02] DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C+10 TO BS 727D+6 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS; [03] VERIFIED DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C+10 TO BS 727D+6 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 706+5 AND 727+16-727A+11; R.B.L. 24.75; W.L. 208.1 ; / [01] COMPLETED STEPS.; [02] VERIFIED COMPLETION OF ALL CORROSION REMOVAL STEPS; [03] APPLIED CHEMICAL CONVERSION COATING AND ONE LAYER OF ALUMINIZED EPOXY PRIMER TO REWORKED AREA IAW SRM 51-20-01 AND SOPM 20-41-04; [04] VERIFIED CORRECTIVE ACTIONS 3

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT STA 500C+13; RBL 24; WL 153. ; / [01] REMOVED CORROSION TO SIDEWALL SUPPORT BS 500C+13 RBL 24 REMOVED MATERIAL AREA L=1''XW=.05''XD=.012'' THICKNIE .040'' OUT OF LIMITS PER SRM 53-0053-1A-2 TOOL USED DEPTH GAUGE ID:ATS400 DUE08/2022; [02] REMOVED SIDEWALL SUPPORT PER REF SRM 51-40-02<BR><BR>FABRICATED NEW SIDEWALL SUPPORT RBL24 WL 153 PER REF DWG NBR 143A7501 AND SRM 51-40-05; [03] INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG; [04] VERIFIED INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 639+9; 663+16 AND 727A+2-727A+10; R.B.L. 45.5; W.L. 208.1 ; / [01] COMPLETED STEPS; [02] VERIFIED COMPLETION OF ALL CORROSION REMOVAL STEPS; [03] APPLIED CHEMICAL CONVERSION COATING AND ONE LAYER OF ALUMINIZED EPOXY PRIMER TO REWORKED AREA IAW SRM 51-20-01 AND SOPM 20-41-04; [04] VERIFIED CORRECTIVE ACTIONS 3

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 787+10-807; 827+3-827+15 AND 847+11-847+15; R.B.L. 45.5; W.L. 208.1. ; / [01] COMPLETED STEPS 1;2;3; [02] VERIFIED COMPLETION OF ALL CORROSION REMOVAL STEPS; [03] APPLIED CHEMICAL CONVERSION COATING AND ONE LAYER OF ALUMINIZED EPOXY PRIMER TO REWORKED AREA IAW SRM 51-20-01 AND SOPM 20-41-04; [04] VERIFIED CORRECTIVE ACTIONS 3

Part: SHIELD — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON FWD CARGO DOOR CUTOUT AFT SHIELD AT WL 153; STA 480+18; RBL 25; STA 500+2; RBL 24; STA 500+6; RBL 24; STA 500+6; RBL 25; STA 500+11; RBL 25; STA 500+12; RBL24; STA 500+14; RBL 24; ; STA 500+14; RBL 25; STA 500+18; RBL 25. / [01] REMOVED AFT; SHIELD ON FWD CARGO DOOR CUTOUT; WL153; RBL24;NO FOUND ALLOWABLE DAMAGE IN THE SRM. IAW. SRM 51-10-02-0G-0;STEP 9.; AND SRM 51-40-02-0G-0.; [02] CORRECTED MEASUREMENTS FIELD TABLE.; [03] VERIFIED CORRECTIVE ACTION 1; FOR REMOVAL OF FCB DOOR CUTOUT AFT SHIELD AND THAT DAMAGED SHIELD WILL BE REPAIRED BY REPLACEMENT DUE TO NO SRM LIMITS.; [04] LOCATED AND DRILLED NEW SHIELD P/N 143A8126U31; LOT 1472167-1 IAW SRM 51-40-05 AND DWG 143A0080; [05] VERIFIED CORRECTIVE ACTION ENTRY 4.; [06] INSTALLATION OF FCD CUTOUT AFT SHIELD WILL BE PERFORMED ON MOC 5330-E-16461-NG; [07] VERIFIED INSTALLATION OF FCD CUTOUT AFT SHIELD WILL BE PERFORMED ON MOC 5330-E-16461-NG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON FORWARD CARGO BAY AFT BULKHEAD SUPPORT STRAP AT STA 500D; WL 153; RBL 14; RBL 10; LBL 1; LBL 4; LBL 14; LBL 17; LBL 22; LBL 23. ; / [01] REMOVED CORROSION ON SUPPORT STRAP; FWD CARGO BAY AFT BULKHEAD AT STA 500D; WL 153; RBL 14;RBL10;LBL4;LBL14;LBL17;LBL22 AND LBL23. MEASURES RBL14: L=2.550'; W=1.100'; D=0.030'. ORIGINAL THICNESS 0.071'; MATERIAL REMOVED 0.030'; REMAINING MATERIAL THICKNESS 0.041'. THE SUPPORT STRAP IS OUT OF LIMITS. IAW. SRM 53-30-08-1A-1 ALLOWABLE DAMAGE 1; STEP 4.A(2)A. TOOL USED DEPTH GAGE ID: ATS1737; DUE DATE:07/2022.; [02] VERIFIED CORRECTIVE ACTION 1 (OUT OF LIMITS); [03] RECEIVED NEW SUPPORT STRAP; ITEM 143A9485Y35; LOT#1468693. LOCATED AND DRILLED NEW SUPPORT STRAP LOC AT STA 500D. IAW. SRM 51-40-05. OK TO INSTALL.; [04] VERIFIED CORRECTIVE ACTIONS 3; [05] INSTALLATION OF FCB AFT BULKHEAD SUPPORT STRAP STA 500D WL 153 WILL BE PERFORMED ON MOC 5330-E-16461-NG; [06] VERIFIED INSTALLATION OF FCB AFT BULKHEAD SUPPORT STRAP STA 500D WL 153 WILL BE PERFORMED ON MOC 5330-E-16461-NG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT WL 153; STA500A+2; RBL24; STA500A+6; RBL 25; STA500B+2; RBL 24; STA500B+2; RBL 24; STA500B+6; RBL 25; STA500B+18; RBL 25; STA500C+2; RBL 24; ; STA 500C+2; RBL25; STA500C+7; RBL 24; STA 500C+10; RBL 25. / [01] REMOVED CORROSION TO SIDEWALL SUPPORT BS 500A+2;RBL24; BS500A+6;RBL25; BS 500B+2; RBL24; BS 500+6; RBL25; BS 500B+18; RBL 25; 500C+2 RBL 24; . BS 500B+2 MATERIAL REMOVED L=1''XW=.05''XD.010'' TICKNIES IS .040'' IS OUT LIMITS IAW SRM 53-00-53-1A-2 STEP 4 (2); [02] CORRECTIVE #1 USED TOOL DEPH GAUGE ID: ATS400 DUE 08/2022; [03] VERIFIED CORRECTIVE ACTION ITEM 1 & 2.; [04] REMOVED SIDEWALL SUPPORT PER REF SRM 51-40-02<BR><BR>FABRICATED NEW SIDEWALL SUPPORT RBL24 WL 153 PER REF DWG NBR 143A7501 AND SRM 51-40-05; [05] FABRICATED FLOOR TO SIDEWALL SUPPORT AND SPLICE IAW REF DWG 143A7501 OK TO TREAT AND PRIME <BR>USING LOT NUMBER 5098100-1; [06] JUST SIDEWALL SUPPORT SPLICE WAS FABRICATED ON DIFFERENT NRC; [07] VERIFIED FABRICATED FLOOR TO SIDEWALL SUPPORT AND SPLICE IAW REF DWG 143A7501.<BR>VERIFIED OK TO TREAT AND PRIME.; [08] APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-21-72-370-801 AND SRM 51-21-41-370-802; [09] INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG; [10] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-21-72-370-801 AND SRM 51-21-41-370-802.<BR>VERIFIED INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON FWD CARGO L/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 LBL 25 STA 500C+10; LBL 25 STA 500C+14. ; / [01] REMOVED CORROSION AT FCB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-10-02-0G-0; MEASURES L=1.2'' X W=1.0'' X D=0.010 TOOL USED DIGITAL CALIPER ID:ATS2501 S/N:A19335647; MICROMETER ID:ATS1672 S/N:65092939; AND EVALUATED BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PART 4A;; [02] REMOVED FCB FLOOR TO SIDEWALL SUPPORT BS400-500D LBL25 WL153 IAW SRM 51-40-02-0G-0; [03] VERIFIED CORRECTIVE ACTION ITEM 1.; [04] VERIFIED ACCOMPLISHMENT OF STEPS 1 & 2.; [05] INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG; [06] VERIFIED INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON FWD CARGO DOOR CUTOUT FWD SHIELD AT W.L. 153; RBL 24; STA 420 + 6 & STA 420 + 17. ; / [01] REMOVED FWD SHIELD ON FWD CARGO DOOR CUTOUT; WL153; RBL24;DONT HAVE ALLOWABLE DAMAGE IN THE SRM. IAW. SRM 51-10-02-0G-0;STEP 9.; AND SRM 51-40-02-0G-0.; [02] UPDATED PART NUMBER IN MEASUREMENTS SECTION; [03] VERIFIED CORRECTIVE ACTION 1; FOR REMOVAL OF FCB DOOR CUTOUT FWD SHIELD AND THAT DAMAGED SHIELD WILL BE REPAIRED BY REPLACEMENT DUE TO NO SRM LIMITS.; [04] LOCATED AND DRILLED NEW SHIELD P/N 143A8126U21; LOT 1466561-1 IAW SRM 51-40-05 AND DWG 143A0080; [05] VERIFIED CORRECTIVE ACTION ENTRY 4.; [06] INSTALLATION OF FCD CUTOUT FWD SHIELD WILL BE PERFORMED ON MOC 5330-E-16461-NG; [07] VERIFIED INSTALLATION OF FCD CUTOUT FWD SHIELD WILL BE PERFORMED ON MOC 5330-E-16461-NG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT STA 727C+8; LBL 20; STA 727C+10; LBL 22; STA 727C+18; LBL 22; STA 727D+6; LBL 22; STA 727D+10; LBL 22; STA 727E+2; LBL 22; STA 727E+8; LBL 20; ; STA 727E+10; LBL 22; STA 727E+14; LBL 22. / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-9.; [02] DAMAGE FOUND ON ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C+8 TO BS 727E+8 LBL 22 FOUND TO BE OUT OFF LIMIT AND WILL BE REPLACED WITH CUSTOMER CARD # TTG8Q00718NX; [03] VERIFIED DAMAGE FOUND ON ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C+8 TO BS 727E+8 LBL 22 FOUND TO BE OUT OFF LIMIT AND WILL BE REPLACED WITH CUSTOMER CARD # TTG8Q00718NX.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 45,503 hrs · 27,299 cycles

CORROSION ON FWD CARGO L/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 LBL 24 STA 420+10; LBL 25 STA 500A+6; LBL 25 STA 500A+14; LBL 25 STA 500B+2;LBL 24 STA 500B+6; LBL 24 STA 500C+1; ; LBL 25 STA 500C+1; LBL 24 STA 500C+4; LBL 25 STA 500C+6; LBL 24 STA 500C+7. / [01] REMOVED CORROSION AT FCB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-10-02-0G-0; MEASURES L=1.1'' X W=1.0'' X D=0.014 TOOL USED DIGITAL CALIPER ID:ATS2501 S/N:A19335647; MICROMETER ID:ATS1672 S/N:65092939; AND EVALUATED BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PART 4A;; [02] REMOVED FLOOR TO SIDEWALL SUPPORT AT FCB BS400-500D LBL25 WL 153 IAW SRM 51-40-02-0G-0; [03] VERIFIED CORRECTIVE ACTION ITEM 1.; [04] VERIFIED ACCOMPLISHMENT OF STEPS 1-6.; [05] FABRICATED FLOOR TO SIDEWALL SUPPORT AND SPLICE IAW REF DWG 143A7501 AND SRM 53-00-53-2R-6 OK TO TREAT AND PRIME<BR>USING LOT NUMBER 5098100-1; [06] VERIFIED FABRICATED FLOOR TO SIDEWALL SUPPORT AND SPLICE IAW REF DWG 143A7501 AND SRM 53-00-53-2R-6.<BR>VERIFIED OK TO TREAT AND PRIME.; [07] APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-21-72-370-801 AND SRM 51-21-41-370-802; [08] INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG; [09] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-21-72-370-801 AND SRM 51-21-41-370-802. <BR>VERIFIED INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG.

Part: RETAINER — BROKEN (SLIDE BAR) · airframe 45,129 hrs · 27,073 cycles

LOCK OUT TAG OUT BOX RETAINING BAR BROKEN ; / [01] INSTALLED SLIDE BAR RETAINER PER SIP

Part: SCUFF PLATE — OUT OF LIMITS (AFT CARGO) · airframe 44,945 hrs · 26,952 cycles

AFT CARGO SCUFF PLATE CENTER THRESHOLD OUT OF LIMITS ; / [01] R/R AFTER CARGO DOOR SCUFF PLATE CENTER PER AMM 53-11-02

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 43,597 hrs · 26,187 cycles

PASSENGER CABIN ROW 24 ISLE PHOTO LUMINOUS STRIPS RIGHT AND LEFT HAS MOISTURE UNDER COVER / R&R PHOT LUMINOUS STRIPS PER AMM 33-51-15

Part: SLIDE — OUT OF TOLERANCE (L1 DOOR) · airframe 42,660 hrs · 25,626 cycles

EMERGENCY SLIDE FWD ENTRY DOOR PRESSURE IN RED. REPLACED FWD ENTRY DOOR SLIDE, PER MT 725-61-06. R & R 74893 P/N OFF/ON:5A3307-7 S/N OFF: BNG12262 S/N ON: BNG11742.

Part: LIGHT — MISSING (CABIN) · airframe 42,250 hrs · 25,359 cycles

PASSENGER CABIN EVACUATION STRIP MISSING AT AFT WHEEL CHAIR CLOSET AFT OF SEAT 24ABC. / INSTALLED STRIP PER AMM 33-51-15

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,788 hrs · 25,052 cycles

L/H O/W EMERGENCY LIGHTS INOP / R+R L/H O/W EMERGENCY LIGHTS BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,374 hrs · 24,791 cycles

EMERGENCY LIGHT WAS OUT FORWARD OF THE AFT CARGO DOOR. / RELAMPED LIGHT PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,306 hrs · 24,735 cycles

L/H OVERWING EMERGENCY LIGHT INOPERATIVE. / RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,299 hrs · 24,114 cycles

L/H EMERGENCY LIGHT TEST FAILED BETWEEN SEAT ROW 9 TO ROW 11. / R&R BATTERY PACK PER AMM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,299 hrs · 24,114 cycles

L/H HORIZONTAL STABILIZER RIB #4 CRACK INDICATION AT LOWER FLANGE #10 HOLE FROM AFT ON STIFFENER 4 SIDE. / REPAIRED #4 RIB IAW SRM.

Part: LENS — WORN (EMERGENCY LIGHT) · airframe 40,299 hrs · 24,114 cycles

GALLEY # 1 EMERGENCY EXIT LIGHT LENS WORN. / R&R LIGHT LENS PER AMM.

Part: CHANNEL — CORRODED (AFT CARGO) · airframe 40,299 hrs · 24,114 cycles

AFT CARGO COMPARTMENT R/H FLOOR SUPPORT ZEE CHANNEL CORRODED AND CRACKED AT FLANGE FROM STA 727C TO STA 767 / AT AFT CARGO COMPT R/H FLOOR SUPPORT ZEE CHANNEL CRACKED AT FLANGE REMOVED FROM STA 727 TO 767 IAW B737-700 SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW ZEE CHANNEL SECTION IAW B737-700 SRM 51-40-05-0G-0 MAT USED PO #1619098; TREATED AND APPLIED PRIMER PER REF B737-700 SRM 51-20-01-0G-0; INSTALLED NEW ZEE CHANNEL SECTION FROM STA 727 TO 767 IAW B737 SRM 51-40-02-0G-0

Part: STRAP — CORRODED (AFT CARGO) · airframe 40,299 hrs · 24,114 cycles

AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT STRAP HAS EXFOLIATING CORROSION AT STA 887 MKD DOT 60-009 / REMOVED AND REPLACED STRAP AT AFT CARGO COMPARTMENT PER REF 51-40-02-0G-0 AND 51-40-05-0G-0 AND DRAWING 146A9401 (STA 887).

Part: STRAP — CORRODED (BS 767) · airframe 40,299 hrs · 24,114 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT STRAP TOP SURFACE CORRODED AT FASTENER HOLES BS. 767. / R&R STRAP IAW SRM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 40,299 hrs · 24,114 cycles

COCKPIT SEAT TRACKS CORRODED PN 226-0202; & 226-0218. / RECEIVED NEW COCKPIT SEAT TRACK WITH PART #226-0204 AND 226-0218 WILL BE INSTALL WITH WORK ORDER #2015322 - 2000-0047 J753-330-00-01Y WITH REFERENCE AS PER AMM 25-11-11-400-801

Part: BEAM — CRACKED (R1 DOOR) · airframe 40,299 hrs · 24,114 cycles

R1 DOOR INTERNAL BEAM #4 CRACKED, AT INBOARD MOST HOLE AND BELOW FILLET RADIUS. / R&R #4 BEAM PER SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 40,299 hrs · 24,114 cycles

R2 LOWER SILL INNER CHORD CORRODED BETWEEN BS. 951 TO BS. 992.8. / R&R INNER CHORD PER SRM & DWG.

Part: WEB — CORRODED (BS 440-492) · airframe 40,299 hrs · 24,114 cycles

FORWARD CARGO COMPARTMENT LOWER SILL WEB EXPANDED CORRODED BETWEEN BS. 440 TO S. 492. R&R WEB PER SRM AND DWG.

Part: RIB — CRACKED (LH HOR STAB) · airframe 40,299 hrs · 24,114 cycles

LEFT HORIZ STAB RIB 4 STA 120.30 STIFFENER 3 APPEARS TO BE CRACKED AT LWR AREA. 8-46 / PERFORMED HFEC AT LEFT HORIZONTAL STAB RIB #4 STA 120.30 STIFFENER 3; FOUND CRACKED. CUT OUT DAMAGED AREA; PERFORMED HFEC AT CUT OUT (STIFFENER 3) NO CRACK NOTED. LOCATED AND DRILLED REPAIR PARTS (KIT PD:7551022). INSTALLED REPAIR PARTS AT LEFT HORIZONTAL STAB RIB #4 STA 120.30 STIFFENER 3 PER REF B737-700 SRM 55-10-09-2R-5; NDTM PART 6 51-00-00 PROCEDURE 23 AND PROCEDURE 16; B737-700 SRM 51-20-01-0G-0

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 40,299 hrs · 24,114 cycles

R/H SIDE VAPOR BARRIER WEB CRACKED AT BS. 663. / REPAIRED WEB PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 40,077 hrs · 23,968 cycles

OVERHEAD EXIT LIGHT WAS HANGING DOWN. R&R LIGHT ASSEMBLY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 38,082 hrs · 22,679 cycles

RT STOWBINS EMERGENCY LIGHTS INOP BETWEEN ROW 1 AND ROW 2. R&R BATTERY CHARGER IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 38,082 hrs · 22,679 cycles

L1 DOOR SURROUND EMERGENCY LIGHTS INOP. R&R BATTERY CHARGER IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,082 hrs · 22,679 cycles

RT STOWBINS EMERGENCY LIGHTS INOP BETWEEN ROW 1 AND ROW 2. R&R BATTERY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 38,082 hrs · 22,679 cycles

R1 DOOR SLIDE EMERGENCY LIGHTS INOP. R&R BATTERY CHARGER IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,082 hrs · 22,679 cycles

L1 DOOR SURROUND EMERGENCY LIGHTS INOP. R&R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,082 hrs · 22,679 cycles

R1 DOOR SLIDE EMERGENCY LIGHTS INOP. R&R BATTERY IAW AMM.

Part: VAPOR BARRIER — CRACKED (WHEEL WELL RH) · airframe 37,415 hrs · 22,273 cycles

COMTINUED FROM LOG 0763478 REF. LOG 0763478 RT. WHEEL WELL FWD BULK HEAD UPPER BARRIER HAS 7.5' CRACK BETWEEN RBL 31.83 & RBL 45.64. / CONTINUED FROM LOG 0763478; ALLOWABLE DAMAGE LIMIT. APPLY THE INTERIM SEAL OVER THE CRACK THAT IS LEFT AS GIVEN IN 737-700 SRM 57-10-10 PARAGRAPH 2.C.(4) ALLOWABLE DAMAGED; PERMANENT REPAIR TIME LIMIT 600 FLIGHT CYCLES.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 37,415 hrs · 22,273 cycles

RT WHEEL WELL FORWARD BULKHEAD VAPOR BARRIER CRACKED BETWEEN RBL 31.83 TO RBL 45.64. REPAIRED BARRIER IAW EA AND SRM.

Part: COVER — MISSING (CABIN) · airframe 36,882 hrs · 21,923 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER EA.

Part: LATCH — BROKEN (EVAC SLIDE) · airframe 36,700 hrs · 21,807 cycles

L2 DOOR ESCAPE SLIDE BLOCK ASSEMBLY LATCH BROKEN. R&R SLIDE PER MT.

Part: COVER — MISSING (EXIT SIGN) · airframe 36,060 hrs · 21,372 cycles

LT OVERHEAD OVERWING EXIT SIGN MISSING. INSTALLED COVER PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,502 hrs · 21,007 cycles

L2 DOOR EMERGENCY LIGHT SEGMENT INOP. R&R LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,502 hrs · 21,007 cycles

LT OVER WING EMERGENCY EXIT LIGHT SEGMENT INOP. R&R LIGHT PER AMM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,725 hrs · 20,520 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 34,725 hrs · 20,520 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 33,881 hrs · 19,996 cycles

RUDDER BALANCE ARM WEIGHT CORRODED / REPLACED RUDDER BALANCE WEIGHT IAW CMM 55-40-09 STEP 3A 1&2

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,881 hrs · 19,996 cycles

R1 DOOR EXTERIOR SLIDE LIGHT INOP. R&R LIGHT IAW AMM.

Part: SLIDE — LOOSE (CABIN) · airframe 33,881 hrs · 19,996 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 33,881 hrs · 19,996 cycles

LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663. REPAIRED WEB IAW SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 32,523 hrs · 19,151 cycles

MID CABIN EMERGENCY EXIT LIGHT LOOSE. SECURED THE LIGHT ASSY IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 32,397 hrs · 19,081 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER SIP.

Part: PUMP — OVERHEATED (NR 1 ENGINE) · airframe 31,347 hrs · 18,443 cycles

AIR TURNBACK, NR 1 ELECTRIC OVERHEAT LIGHT ILLUMINATED INFLIGHT. R&R NR 1 ELECTRIC HYDRAULIC PUMP IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 30,124 hrs · 17,692 cycles

FORWARD ENTRY LOWER EMERGENCY EXIT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 29,831 hrs · 17,522 cycles

LEFT MID CABIN BATTERY PACK FAILED THE TIME TEST FOR BATTERY PACK CAPACITY. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 29,831 hrs · 17,522 cycles

LEFT FORWARD CABIN BATTERY PACK FAILED THE TIME TEST FOR BATTERY PACK CAPACITY. R & R THE BATTERY PACK IAW AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 27,853 hrs · 16,395 cycles

SKIN CORRODED IN AFT CARGO THRESHOLD SCUFF PLATE DOME NUT HOLES. REPAIRED SKIN EA.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 27,853 hrs · 16,395 cycles

OVERWING EMER EXIT LIGHT CONNECTOR DAMAGED. R & R CONNECTOR IAW SWPM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 27,853 hrs · 16,395 cycles

LEFT HORIZONTAL STABILIZER THIRD VERTICAL RIB FRONT CRACKED AT STATION 92.70. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 27,853 hrs · 16,395 cycles

LEFT HORIZONTAL STABILIZER SECOND VERTICAL RIB FRONT CRACKED AT STATION 92.70. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 27,853 hrs · 16,395 cycles

LEFT HORIZONTAL STABILIZER CRACKED, BETWEEN SECOND & THIRD VERTICAL RIB FRONT SPAR AT STATION 92.70. REPAIRED RIB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,853 hrs · 16,395 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, LBL 45. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,853 hrs · 16,395 cycles

INTERCOSTAL CRACKED, BETWEEN BS 328 - 344, LBL 45. R & R INTERCOSTAL IAW SRM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 27,661 hrs · 16,281 cycles

CABIN RT AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 27,661 hrs · 16,281 cycles

CABIN LT AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,661 hrs · 16,281 cycles

LEFT FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 26,023 hrs · 15,335 cycles

MID CABIN OVERHEAD EMER EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: HOOK — BROKEN (R2 DOOR) · airframe 24,743 hrs · 14,595 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR HOOK BROKEN. REPAIRED HOOK IAW SRM & MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,071 hrs · 14,259 cycles

MOST FWD BULLNOSE EMER LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 21,250 hrs · 12,630 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,250 hrs · 12,630 cycles

AFT CARGO FLOOR SUPPORT ANGLE CORRODED AFT END OF AFT FLOOR BOARD AT STATION 947. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 21,250 hrs · 12,630 cycles

LT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 157.10, 10 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,250 hrs · 12,630 cycles

RT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 129.50, 27 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,250 hrs · 12,630 cycles

RT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 157.10, 10 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 21,250 hrs · 12,630 cycles

LT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 157.10, 16 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 21,250 hrs · 12,630 cycles

LT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 101.90, 20 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,250 hrs · 12,630 cycles

RT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 157.10, 17 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,250 hrs · 12,630 cycles

RT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 184.70, 10 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 21,250 hrs · 12,630 cycles

LT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 184.70, 10 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,020 hrs · 12,489 cycles

RT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,020 hrs · 12,489 cycles

LT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 18,912 hrs · 11,243 cycles

RT EMERGENCY EXIT LENS MISSING. R&R LENS IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 18,753 hrs · 11,143 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW SIP.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,702 hrs · 11,112 cycles

FLOOR PANEL SUPPORT CRACKED AT BS 540, BL0. R & R SUPPORT IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 18,702 hrs · 11,112 cycles

LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED 0.75" INBD OF RIB AT STAB STA 101.90. REPAIRED SKIN IAW SRM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 17,796 hrs · 10,594 cycles

LOWER RIGHT OVERWING EXIT SIGN BROKEN. REPLACED EXIT SIGN COVER IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 15,810 hrs · 9,452 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 15,706 hrs · 9,390 cycles

L2 DOOR EMERGENCY EXIT LIGHT WIRE OUT OF POSITION BEHIND L2 DOOR. REPOSITIONED WIRE IAW M/M.

Part: COVER — CRACKED (CABIN) · airframe 14,053 hrs · 8,431 cycles

LT EMERGENCY LIGHT COVER CRACKED BETWEEN ROW 4 TO ROW 7. REMOVED AND REPLACED COVER PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,053 hrs · 8,431 cycles

EMERGENCY LIGHT INOP AT ROW 1ABC. RELAMPED LIGHT PER M/M.

Part: COVER — CRACKED (CABIN) · airframe 14,053 hrs · 8,431 cycles

LT EMERGENCY LIGHT COVER CRACKED AT ROW 23. REMOVED AND REPLACED COVER PER M/M.

Part: COVER — LOOSE (CABIN) · airframe 13,969 hrs · 8,382 cycles

COVER LOOSE FROM ESCAPE LIGHT SYSTEM ON FLOOR STRIP AT ROW 1. REMOVED AND REPLACED COVER PER M/M.

Part: LENS — MISSING (CABIN) · airframe 13,372 hrs · 8,042 cycles

LT EEPLS COVER MISSING AT ROW 1. INSTALLED LENS IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 13,342 hrs · 8,023 cycles

EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 12,978 hrs · 7,804 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER BROKEN AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 11,781 hrs · 7,106 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EMERGENCY EXIT LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 11,781 hrs · 7,106 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY EXIT LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — MISSING (CABIN) · airframe 11,540 hrs · 6,953 cycles

LT EEPLS COVER MISSING AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 9,727 hrs · 5,901 cycles

EEPLS COVER MISSING AT ROW 2. INSTALLED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 9,562 hrs · 5,800 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 9,269 hrs · 5,612 cycles

LOOSE WIRE ON EEPLS. SECURED WIRE PER MM.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 8,968 hrs · 5,421 cycles

LT EEPLS OUT OF POSITION AT ROW 1. REPOSITIONED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,969 hrs · 4,823 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 7,103 hrs · 4,313 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 7,103 hrs · 4,313 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: COVER — BROKEN (CABIN) · airframe 6,523 hrs · 3,949 cycles

ROW 1 EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 6,417 hrs · 3,887 cycles

LT EEPLS COVER BROKEN AT ROW 12. REMOVED AND REPLACED COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 5,757 hrs · 3,492 cycles

LEFT EEPLS LENS LOOSE AT ROW 1. REMOVED AND REPLACED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 5,250 hrs · 3,173 cycles

FWD EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 4,467 hrs · 2,717 cycles

RT AFT GALLEY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 4,258 hrs · 2,592 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: FITTING — INOPERATIVE (EVAC SLIDE) · airframe 3,839 hrs · 2,337 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP INOP. REMOVED AND REPLACED SLIDE PER MT.

Part: ACM — SEIZED (AC BAY) · airframe 3,707 hrs · 2,260 cycles

THIRTY MINUTES PRIOR TO ARRIVAL IN FLL, FLT ATTENDANTS SMELLED OILY/RUBBER ODOR WITH VIBRATION CENTERED OVER ROW 9, RT SIDE. FOUND RT PACK ACM SEIZED. REMOVED AND REPLACED RT ACM PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,679 hrs · 2,245 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.