N7823A

Part: ISOLATOR MOUNT — CRACKED (ZONE 800 SLIDE) · airframe 73,728 hrs · 38,890 cycles

PASSENGER CABIN ESCAPE SLIDE FWD UPPER ISOLATOR CRACKED. R & R PASSENGER CABIN ESCAPE SLIDE FWD UPPER ISOLATOR IAW SRM 51-40-02. INSPECTION C/W R&R PASSENGER CABIN ESCAPE SLIDE FWD UPPER ISOLATOR IAW SRM 51-40-02.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 72,279 hrs · 37,976 cycles

DURING EMERGENCY LIGHT OPERATIONAL TEST. FOUND AFT EMERGENCY LIGHT BULB IN R/H OVERWING EXIT WINDOW LIGHT ASSEMBLY INOP DURING EMERGENCY LIGHT OPERATIONAL TEST FOUND AFT EMERGENCY LIGHT BULB IN R/H OVERWING EXIT WINDOW LIGHT ASSEMBLY INOP. RELAMPED AND CHECKED GOOD PER AMM 33-51-00-720-801.

Part: BATTERY PACK — INOPERATIVE (ZONE 20) · airframe 72,279 hrs · 37,976 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK (M1672) DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK M1672 IAW AMM 33-51-06-960-805 AND PERFORMED GOOD EMERGENCY LIGHT TEST IAW AMM 33-51-06-960-805.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 72,279 hrs · 37,976 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK (M1670) DO NOT ILLUMINATE. REPLACED EMERGENCY BATTERY PACK (M1670); PERFORMED GOOD TEST PER AMM 33-51-06-960-805.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 72,279 hrs · 37,976 cycles

CRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208<[01] THIS IS DUPLICATED CARD... REMOVED AND REPLACED ON FAULT# TTG8Q010QNP2;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: PANEL — CRACKED (ZONE 300) · airframe 72,279 hrs · 37,976 cycles

VERTICAL STAB PANEL 323AL LOWER CLIP CRACKED.<[01] RECEIVED SERVICEABLE PANEL 323AL P/N:654A0004-711; BN 396992. PANEL WILL BE INSTALLED ON TASK CARD TTG8Q00Z3WDY;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 72,279 hrs · 37,976 cycles

CRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208. MARKED<[01] REMOVED AND REPLACED PANEL BREAK AT MID CABIN BS540 RBL1 WL208 IAW SRM 51-40-02 AND DWG# 143A5240 REV: B;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 72,279 hrs · 37,976 cycles

CRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208. MARKED<[01] REMOVED AND REPLACED BS540 LBL1 PANEL BREAK P/N#143A5240-63 IAW SRM 51-40-02 AND PER AIPC# 53-31-00-05;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: SKIN — CRACKED (ZONE 300) · airframe 72,279 hrs · 37,976 cycles

CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 23. 5' FROM FWD EDGE; .3' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON LH HORIZONTAL STABILIZER LOWER SKIN STA 193.90 23.5' FROM FWD EDGE; CUT OUT DIMENSIONS 1.7' X 1.0' AND INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-11.;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: ATTACH ANGLE — CRACKED (ZONE 500) · airframe 72,279 hrs · 37,976 cycles

LT WING DEFLECTION CONTROL RIB UPPER PANEL ATTACHMENT CRACKED.<[01] REPAIRED LT WING DEFLECTION CONTROL RIB UPPER PANEL ATTACHMENT IAW SRM 57-51-02-2R-3.;[02] CORRECTIVE ACTION COMPLETED.

Part: SEAL — MISSING (ZONE 300) · airframe 72,279 hrs · 37,976 cycles

R/H LOWER FWD SLIDE SEAL AND HARDWARE MISSING<[01] REPLACED R/H LOWER FWD SLIDE SEAL AND HARDWARE IAW AMM 53-31-31-400-803.;[02] CORRECTIVE ACTION COMPLETED.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 72,061 hrs · 37,842 cycles

EMERGENCY AREA LIGHTS AT SEAT ROW 12 LH & 13 RH INOP<[01] RELAMPED EMERGENCY AREA LIGHTS AT SEAT ROW 12 LH & 13 RH IAW AMM 33-51-03 OPS CHECK OK

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 70,507 hrs · 36,905 cycles

EMERGENCY LIGHT INOP AT SEAT ROW 4 LH<[01] RELAMPED EMERGENCY LIGHT AT SEAT ROW 4 LH IAW AMM 33-51-03 OPS CHECK OK

Part: SENSOR — FAULTY (ZONE 100) · airframe 69,791 hrs · 36,441 cycles

PER MOC/AHM DATA FLAP SENSOR LOCK OUT PENDING. PER QRH PERFORMED ZERO FLAPS LANDING WITH L/E ALT FLAP EXTENDED. NO ROLL OR ABNORMAL FLIGHT CHARACTERISTIC.<[01] REMOVED AND REPLACED #6 FLAP SKEW SENSOR. OP CHECK GOOD. REF AMM 27-59-01

Part: BALLAST — OVERHEATED (ZONE 200) · airframe 69,580 hrs · 36,313 cycles

DURING CLIMBOUT AT APPROXIMATLY 6000' WE ENCOUNTERED A STRONG ELECTRICAL BURNING SMELLTHAT DID NOT DISAPATEUNTILL AFTER LANDING<[01] PERFORMED SMOKE OR FUMES CONDITIONAL INSPECTION PER M.M. CH. 05-51-56. FOUND FWD ENTRY LIGHT BALLAST HOT/SMOLDERING WITH ODOR. REPLACED BALLAST AND LAMPS PER M.M. CH. 33-29-00. OPS CHECK GOOD. NO OTHER DEFECTS NOTED.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 69,580 hrs · 36,313 cycles

DURING CLIMBOUT AT APPROXIMATLY 6000' WE ENCOUNTERED A STRONG ELECTRICAL BURNING SMELLTHAT DID NOT DISAPATEUNTILL AFTER LANDING<[01] PERFORMED SMOKE OR FUMES CONDITIONAL INSPECTION PER M.M. CH. 05-51-56. FOUND FWD ENTRY LIGHT BALLAST HOT/SMOLDERING WITH ODOR. REPLACED BALLAST AND LAMPS PER M.M. CH. 33-29-00. OPS CHECK GOOD. NO OTHER DEFECTS NOTED.

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 69,087 hrs · 35,996 cycles

BATTERY PACK M1674 FAILED CAPACITY CHECK. BATTERY PACKS M1674 AND M1675 FAILED CAPACITY CHECK.<[01] R&R BATTERY PACKS M1674 AND M1675 IAW AMM 33-51-06.

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 69,087 hrs · 35,996 cycles

BATTERY PACK M1674 FAILED CAPACITY CHECK. BATTERY PACKS M1674 AND M1675 FAILED CAPACITY CHECK.<[01] R&R BATTERY PACKS M1674 AND M1675 IAW AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,571 hrs · 35,686 cycles

EMERGENCY LIGHTS INOP IN AFT GALLEY.<[01] R/R BATTERY PACK M1673 PER AMM 33-51-06.

Part: HANDLE — LOOSE (ZN 800 DOOR) · airframe 67,660 hrs · 35,134 cycles

FWD ENTRY DOOR INTERIOR HANDLE LOOSE. MOVES UP APPROX 1 DURING FLIGHT<[01] C/W GUIDE ARM ADJUSTMENT ON FWD ENTRY DOOR PER MT 752-11-01

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 67,655 hrs · 35,131 cycles

FWD ENTRY DOOR (L1) GIRT BAR WILL NOT SEAT<[01] REPACKED L1 SLIDE PER MT725-61-06. GIRT BAR STOWS PROPERLY

Part: MEGAPHONE — INOPERATIVE (ZN 200 FUS TOP) · airframe 67,153 hrs · 34,821 cycles

FWD L/H BULKHEAD MEGA PHONE INOP<[01] R/R FWD L/H BULKHEAD MEGA PHONE AMM 25-64-00

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 66,403 hrs · 34,323 cycles

CRACK ANGLE LOCATED ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT RT WING 2023-310574<[01] REPLACED ANGLE LOCATED ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 112A2004 SHEET 5 REV -. PERFORMED FUEL LEAK CHECK ON ANGLE LOCATED ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT RT WING IAW B737-700 AMM-28-11-00-790-801 STEP 4.G NO LEAKS FOUND.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED ANGLE LOCATED ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 112A2004 SHEET 5 REV -. PERFORMED FUEL LEAK CHECK ON ANGLE LOCATED ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT RT WING IAW B737-700 AMM-28-11-00-790-801 STEP 4.G NO LEAKS FOUND. RII <BR>SEE INDIVIDUAL SIGNOFF BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CRACK ANGLE LOCATED UPPER SIDE BS663 RBL42 AND WL168 AT AIR CONDITIONING BAY 2023-310571<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 25-JAN-24.;[02] REPLACED ANGLE LOCATED UPPER SIDE BS663 RBL42 AND WL168 AT AIR CONDITIONING BA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 111A1000 SHEET 130 REV A.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[03] REPLACED ANGLE LOCATED UPPER SIDE BS663 RBL42 AND WL168 AT AIR CONDITIONING BA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 111A1000 SHEET 130 REV A. RII ;SEE INDIVIDUAL SIGNOFF BELOW.

Part: BALANCE WEIGHT — CORRODED (ZN 500 LEFT WING) · airframe 66,403 hrs · 34,323 cycles

CORROSION AILERON BALANCE ADJUNTO WEINGHT LOC BALANCE BAY NO5 UPPER AND LOWER AT LT WING (6 EA) 2023-310556<[01] REPLACED AILERON BALANCE WEIGHT LOC. BALANCE BAY #5 UPPER AND LOWER LT WING IAW B737-700 SRM 51-60-01-0G-0 STEP 5.A (5)(D);[02] REPLACED AILERON BALANCE WEIGHT LOC. BALANCE BAY #5 UPPER AND LOWER LT WING IAW B737-700 SRM 51-60-01-0G-0 STEP 5.A (5)(D).<BR>ITEM RII.

Part: WEB — CRACKED (ZN 400 NACELLE/P) · airframe 66,403 hrs · 34,323 cycles

CRACK WEB INTERNAL STRUCTURE INBOARD FAN COWL ON ENGINE 1 2023-310525<[01] REPLACED WEB INTERNAL STRUCTURE INBOARD FAN COWL ON ENGINE 1 IAW GOODRICH AEROSTRUCTURES CMM 71-13-30 PAGE 10081;[02] TASK CARD COMPLETED

Part: BALANCE WEIGHT — CORRODED (ZN 600 RIGHT WIN) · airframe 66,403 hrs · 34,323 cycles

CORROSION AILERON BALANCE ADJUNTO WEINGHT LOC BALANCE BAY NO 5 UPPER AND LOWER AT RT WING (2 EA) 2023-310531<[01] REPLACED AILERON BALANCE WEIGHT LOC. BALANCE BAY #5 UPPER AND LOWER RT WING IAW B737-700 SRM 51-60-01-0G-0 STEP 5.A (5)(D);[02] REPLACED AILERON BALANCE WEIGHT LOC. BALANCE BAY #5 UPPER AND LOWER RT WING IAW B737-700 SRM 51-60-01-0G-0 STEP 5.A (5)(D) RII

Part: ROPE — MISSING (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

MISSING COMPARTMENT DOOR ESCAPE ROPE STRAP LT SIDE AT COCKPIT (1 EA) 2023-310520<[01] INSTALLED COMPARTMENT DOOR ESCAPE ROPE STRAP LT SIDE AT COCKPIT (1 EA) IAW B737-700 AMM 25-61-10-400-801;[02] COMPLETED

Part: BRACKET — ELONGATED (ZN 600 RIGHT WIN) · airframe 66,403 hrs · 34,323 cycles

ELONGATED HOLE INTERNAL CAVITY SUPPORT BRACKET INBOARD LEADING EDGE AT RT WING 2023-310566<[01] REPLACED BRACKET INBOARD LEADING-EDGE AT RT WING I.A.W. B737-700 SRM 51-40-02-0G-0;[02] TASK COMPLETED

Part: TIE CLIP — CRACKED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CRACK BILGE AREA TIE CLIP BS 500D LEVEL STRINGER 26L AT FWD CARGO COMPARTMENT 2023-310551<[01] REPLACED TIE CLIP LOC BILGE AREA BS 500D LEVEL STRINGER 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DWG 143A1225 SHEET 53 REV -.<BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[02] REPLACED TIE CLIP LOC BILGE AREA BS 500D LEVEL STRINGER 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DWG 143A1225 SHEET 53 REV -. ITEM RII <BR>SEE INDIVIDUAL SIGNSOFF BELOW

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

CRACK FLOOR STRUCTURE ANGLE ASSY LOCATED BS540 AND LBL1 WL208.1 AT PASSENGER CABIN 2023-310503<[01] REPLACED ANGLE ASSY AND FASTENERS LOCATED FLOOR STRUCTURE BS540 AND LBL1 WL208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DWG 143A0060 REV: A SHEET 36;[02] CORRECTED STEP 2.<BR>REPLACED ANGLE ASSY AND FASTENERS LOCATED FLOOR STRUCTURE BS540 AND LBL1 WL208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DWG 143A0060 REV: A SHEET 36. SEE INDIVIDUAL SIGNOFFS BELOW;[03] CERTIFIED STEP 2 COMPLETED <BR>RII

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

CRACK ANGLE LOCATED BS695 AND RBL24.75 WL203 AT PASSENGER CABIN 2023-310504<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[02] REPLACED REPAIR ANGLE LOCATED BS695 AND RBL24.75 WL203 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02 AND DWG #273A9110 SEE INDIVIDUAL SIGNOFFS BELOW;[03] CORRECTED STEP 1<BR>REPLACED REPAIR ANGLE LOCATED BS695 AND RBL24.75 WL203 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02 AND DWG #273A9110 SHEET 2 REV A SEE INDIVIDUAL SIGNOFFS BELOW;[04] CORRECTED STEP 2 AND 3<BR>REPLACED REPAIR ANGLE LOCATED BS695 AND RBL24.75 WL203 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02 AND DWG #273A9110 SHEET 2 REV A SEE INDIVIDUAL SIGNOFFS BELOW;[05] REPLACED REPAIR ANGLE LOCATED BS695 AND RBL24.75 WL203 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02 AND DWG #273A9110 SHEET 2 REV A SEE INDIVIDUAL SIGNOFFS BELOW<BR>CERTIFIED AS RII

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 66,403 hrs · 34,323 cycles

CRACK ANGLE LOCATE ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT LT WING 2023-310499<[01] REPLACED ANGLE LOCATE ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT LT WIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 112A2004 SHEET 5 REV - AND PERFORMED FUEL LEAK CHECK ON ANGLE LOCATE ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT LT WING IAW B737-700 AMM-28-11-00-790-801 STEP 4.G NO LEAKS FOUND.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED ANGLE LOCATE ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT LT WIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 112A2004 SHEET 5 REV - AND PERFORMED FUEL LEAK CHECK ON ANGLE LOCATE ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT LT WING IAW B737-700 AMM-28-11-00-790-801 STEP 4.G NO LEAKS FOUND. RII <BR>SEE INDIVIDUAL SIGNOFF BELOW.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

CRACK FLOOR STRUCTURE ANGLE ASSY LOCATED BS540 AND RBL1 WL208.1 AT PASSENGER CABIN 2023-310502<[01] REPLACED FLOOR STRUCTURE ANGLE ASSY LOCATED BS540 AND RBL1 WL208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CORRODED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CORROSION BILGE AREA PLATE BTW BS 767 TO BS 787 RBL 21 AT AFT CARGO COMPARTMENT 2023-310476<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45 MG; S/N: 130060401; DUE DATE: 20-MAR-24.;[02] REPLACED PLATE (SHIELD) AND FASTENERS LOCATED BILGE AREA BTW BS 767 TO BS 787 RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 146A0081 REV: A SHEET 25. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED PLATE (SHIELD) AND FASTENERS LOCATED BILGE AREA BTW BS 767 TO BS 787 RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 146A0081 REV: A SHEET 25. SEE INDIVIDUAL SIGN OFFS BELOW. RII.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CORROSION SUPPORT ZEE BTW STA 727 TO STA 767 RBL 21 AFT CARGO COMPARTMENT 2023-310488<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 45MG. S/N: 130064101. DUE DATE: 12-OCT-23.;[02] REMOVED CORROSION AND EVALUATED REWORK AREA ON SUPPORT ZEE LOCATED BTW STA 727 TO STA 767 RBL 21 AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 PAR. 4A (2) FIG. 103 DETAIL D. MEASURE OF REWORKED AREA IS: 0.037?. SEE INDIVIDUAL SIGNSOFF BELOW;[03] REMOVED CORROSION AND EVALUATED REWORK AREA ON SUPPORT ZEE LOCATED BTW STA 727 TO STA 767 RBL 21 AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 PAR. 4A (2) FIG. 103 DETAIL D. MEASURE OF REWORKED AREA IS: 0.037?. SEE INDIVIDUAL SIGNSOFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CRACK ANGLE - SUPPORT BS 727B TO BS 827 AT LEVEL STR18L AND WL202 AT AFT CARGO COMPARTMENT 2023-310473<[01] REPLACED ANGLE - SUPPORT BS 727B TO BS 827 AT LEVEL STR18L AND WL202 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 149A9490 SHEET 21 REV.-;[02] CORRECTED STEP 1: <BR>REPLACED ANGLE - SUPPORT BS 727B TO BS 827 AT LEVEL STR18L AND WL202 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 149A9490 SHEET 21 REV.-. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: GRIP — BROKEN (ZN 800 DOOR) · airframe 66,403 hrs · 34,323 cycles

BROKEN EMERGENCY DOOR GRIP ASSY LT SIDE AT PASSENGER CABIN (1 EA) 2023-310447<[01] REPLACED EMERGENCY DOOR GRIP ASSY LT SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 52-22-51-400-801 STEP 3.D ITEM (2) (D);[02] REPLACED EMERGENCY DOOR GRIP ASSY LT SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 52-22-51-400-801 STEP 3.D ITEM (2) (D).JOB COMPLETE.

Part: GRIP — BROKEN (ZN 800 DOOR) · airframe 66,403 hrs · 34,323 cycles

BROKEN EMERGENCY DOOR GRIP ASSY RT SIDE AT PASSENGER CABIN (1 EA) 2023-310448<[01] REPLACED EMERGENCY DOOR GRIP ASSY RT SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 52-22-51-400-801 STEP 3.D ITEM (2) (D);[02] REPLACED EMERGENCY DOOR GRIP ASSY RT SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 52-22-51-400-801 STEP 3.D ITEM (2) (D).JOB COMPLETE.

Part: LIGHT — DETERIORATED (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (6 EA) 2023-310454<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (6 EA) I.A.W B737-700 AMM 33-51-15-400-802;[02] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (6 EA) I.A.W B737-700 AMM 33-51-15-400-802

Part: FRAME — CRACKED (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

CRACK FRAME BS480 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2023-310471<[01] TOOL USED: EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272712; DUE DATE: 17-DEC-23;[02] PERFORMED HFEC INSPECTION ON FRAME BS480 AND STR8 TO STR9 AS PER NDT MANUAL PART 6; 51-00-00; PROCEDURE 23; CRACK INDICATION NOT FOUND. TOOL USED: EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272712; DUE DATE: 17-DEC-23 SEE SIGN OFF BELLOW;[03] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: TIE CLIP — CRACKED (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2023-310435<[01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 REV:- SHEET 18. SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 REV:- SHEET 18. SEE INDIVIDUAL SIGNOFFS BELOW RII CERTIFIED

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CRACK STRINGER 26L BS 540 FWD CARGO COMPARTMENT 2023-310422<[01] TOOL USED P/N: 35DL; S/N: 091419910; CAL DUE: 13-MAR-24.;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[04] REPAIRED STRINGER 26L BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW.;[05] REPAIRED STRINGER 26L BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW.<BR>CERTIFIED AS RII;[06] REPAIRED STRINGER 26L BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW.

Part: FRAME — CRACKED (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

CRACK FRAME LOCATED BS312 AND BETWEEN STR5L TO STR6L AT PASSENGER CABIN 2023-310438<[01] REPAIRED FRAME LOCATED BS312 AND BETWEEN STR5L TO STR6L AT PASSENGER CABIN IAW EA# M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPAIRED FRAME LOCATED BS312 AND BETWEEN STR5L TO STR6L AT PASSENGER CABIN IAW EA# M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CRACK STRINGER 23L BS 540 FWD CARGO COMPARTMENT 2023-310421<[01] TOOL USED P/N: 35DL; S/N: 091419910; CAL DUE: 13-MAR-24.;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[04] REPAIRED STRINGER 23L BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW;[05] REPAIRED STRINGER 23L BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW<BR>CERTIFIED AS RII

Part: PANEL — CRACKED (ZN 300 STABILIZE) · airframe 66,403 hrs · 34,323 cycles

CRACK SEAL PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB 2023-310433<[01] REPLACED SEAL PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STA I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9;[02] REPLACED SEAL PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STA I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9.JOB COMPLETE.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-310372<[01] TOOL USED DIGITAL CALIPER P/N:54-100-000-2;S/N:AE-32464;DUE DATE:04-MAR-24.;[02] TOOL USED: RADIOMETER PHOTOMETER KIT P/N: XRP-3000 S/N: 1753759;[03] TOOL USED: RADIOMETER PHOTOMETER KIT P/N: XRP-3000 S/N: 1753759 DUE DATE: 14-OCT-23;[04] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) (4) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) 2023-310382<[01] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM-33-51-01-960-801 STEP 2. C(4);[02] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM-33-51-01-960-801 STEP 2. C(4)

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2023-310371<[01] TOOL USED DIGITAL CALIPER P/N:54-100-000-2;S/N:AE-32464;DUE DATE:04-MAR-24.;[02] TOOL USED: RADIOMETER PHOTOMETER KIT P/N: XRP-3000 S/N: 1753759 DUE DATE: 14-OCT-23;[03] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2); (4) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 66,403 hrs · 34,323 cycles

CRACK LEADING EDGE RIB STA 105.26 ACCESS PANEL 341B RT HORIZONTAL STAB 2023-310361<[01] REPLACED LEADING EDGE RIB STA 105.26 ACCESS PANEL 341B RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02 AND DWG 186A1001; SHEET 10; REV. A. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CERTIFIED AS RII<BR>REPLACED LEADING EDGE RIB STA 105.26 ACCESS PANEL 341B RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02 AND DWG 186A1001; SHEET 10; REV. A. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (ZN 300 STABILIZE) · airframe 66,403 hrs · 34,323 cycles

CRACK LEADING EDGE ANGLE BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER 2023-310347<[01] REPLACED LEADING EDGE ANGLE LOC BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #176A3101 SHEET 4 REV -.<BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[02] REPLACED LEADING EDGE ANGLE LOC BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #176A3101 SHEET 4 REV -.RII SEE INDIVIDUAL SIGNSOFF BELOW.

Part: PRESSURE DECK — CRACKED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB LOC BS 664 AND RBL 42.5 . CRACK LENGTH 0.75 INCH 2023-310316<[01] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23;[02] PERFORMED REPAIR LOCATED HORIZONTAL PRESSURE DECK WEB BTW RBL 38 TO RBL 60 AND FASTENERS IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 PARAGRAPH 4 <BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[03] PERFORMED REPAIR LOCATED HORIZONTAL PRESSURE DECK WEB BTW RBL 38 TO RBL 60 AND FASTENERS IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 PARAGRAPH 4 <BR>SEE INDIVIDUAL SIGNSOFF BELOW.<BR>CERTIFIED AS RII

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CRACK GUSSET LOCATED STA 500D AND STR 19L FWD CARGO COMPARTMENT 2023-310302<[01] REPLACED GUSSET LOCATED STA 500D AND STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 143A7902 SHEET: 174 REV: - . SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED GUSSET LOCATED STA 500D AND STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 143A7902 SHEET: 174 REV: - . SEE INDIVIDUAL SIGNOFFS BELOW. RII CERTIFIED

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 66,403 hrs · 34,323 cycles

CRACK GUSSET LOCATED STA 500D AND STR 19R FWD CARGO COMPARTMENT 2023-310305<[01] REPLACED GUSSET LOCATED STA 500D AND STR 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV:- SHEET 174. SEE INDIVIDUAL SIGNOFFS BELOW;[02] CERTIFIED STEP 1 COMPLETE RII <BR>REPLACED GUSSET LOCATED STA 500D AND STR 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV:- SHEET 174. SEE INDIVIDUAL SIGNOFFS BELOW

Part: POWER SUPPLY — INOPERATIVE (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

INOP EMERGENCY LIGHT POWER SUPPLY AFT GALLEY AREA (2 EA) 2023-310185<[01] REPLACED EMERGENCY LIGHT POWER SUPPLY MODULES AND BATTERY PACKS (2 EA) AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06. TEST IS OK.<BR>PARTS REMOVED:<BR>P/N D717-01-100SWA S/N 54849<BR>P/N D717-01-100SWA S/N 11835<BR>P/N D717-02-030 S/N 2315<BR>P/N D717-02-030 S/N 22588<BR>PARTS INSTALLED:<BR>P/N D717-02-030 S/N 31458<BR>P/N D717-02-030 S/N 25457<BR>P/N D717-01-100SWA S/N 38068<BR>P/N D717-01-100SWA S/N 204178;[02] REPLACED EMERGENCY LIGHT POWER SUPPLY MODULES AND BATTERY PACKS (2 EA) AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06. TEST OK.<BR>PARTS REMOVED:<BR>P/N D717-01-100SWA S/N 54849<BR>P/N D717-01-100SWA S/N 11835<BR>P/N D717-02-030 S/N 2315<BR>P/N D717-02-030 S/N 22588<BR>PARTS INSTALLED:<BR>P/N D717-02-030 S/N 31458<BR>P/N D717-02-030 S/N 25457<BR>P/N D717-01-100SWA S/N 38068<BR>P/N D717-01-100SWA S/N 204178

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

INOP EMERGENCY LIGHT POWER SUPPLY AFT GALLEY AREA (2 EA) 2023-310185<[01] REPLACED EMERGENCY LIGHT POWER SUPPLY MODULES AND BATTERY PACKS (2 EA) AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06. TEST IS OK.<BR>PARTS REMOVED:<BR>P/N D717-01-100SWA S/N 54849<BR>P/N D717-01-100SWA S/N 11835<BR>P/N D717-02-030 S/N 2315<BR>P/N D717-02-030 S/N 22588<BR>PARTS INSTALLED:<BR>P/N D717-02-030 S/N 31458<BR>P/N D717-02-030 S/N 25457<BR>P/N D717-01-100SWA S/N 38068<BR>P/N D717-01-100SWA S/N 204178;[02] REPLACED EMERGENCY LIGHT POWER SUPPLY MODULES AND BATTERY PACKS (2 EA) AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06. TEST OK.<BR>PARTS REMOVED:<BR>P/N D717-01-100SWA S/N 54849<BR>P/N D717-01-100SWA S/N 11835<BR>P/N D717-02-030 S/N 2315<BR>P/N D717-02-030 S/N 22588<BR>PARTS INSTALLED:<BR>P/N D717-02-030 S/N 31458<BR>P/N D717-02-030 S/N 25457<BR>P/N D717-01-100SWA S/N 38068<BR>P/N D717-01-100SWA S/N 204178

Part: POWER SUPPLY — INOPERATIVE (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

INOP LOWER SIDEWALL PANEL BTW BS 727C TO BS 727D POWER SUPPLY EMERGENCY LIGHT LT SIDE AT PASSENGER CABIN (1 EA) 2023-310186<[01] REPLACED EMERGENCY LIGHT POWER SUPPLY <BR>S/N REMOVED:2315<BR>S/N INSTALLED:31458<BR>IAW B737-700 AMM 33-51-06-960-806<BR>PERFORMED TEST: TEST OK;[02] CORRECTED STEP 1: REPLACED EMERGENCY LIGHT POWER SUPPLY <BR>S/N REMOVED:22818<BR>S/N INSTALLED:186642<BR>IAW B737-700 AMM 33-51-06-960-806 <BR>PERFORMED TEST: TEST OK;[03] CORRECTED STEP 1: REPLACED EMERGENCY LIGHT POWER SUPPLY<BR>S/N REMOVED:22818<BR>S/N INSTALLED:186642<BR>IAW B737-700 AMM 33-51-06-960-806 AND PERFORMED TEST OK

Part: FITTING — CORRODED (ZN 200 FUS TOP) · airframe 66,403 hrs · 34,323 cycles

RUST WINDSCREEN LT SIDE LOWER FITTING ASSY AT FWD GALLEY AREA (2 EA) 2023-310206<[01] REPLACED WINDSCREEN LT SIDE LOWER FITTING ASSY AT FWD GALLEY AREA (2 EA) IAW SOPM 20-50-01 REV 38;[02] REPLACED WINDSCREEN LT SIDE LOWER FITTING ASSY AT FWD GALLEY AREA (2 EA) IAW SOPM 20-50-01 REV 38

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 66,400 hrs · 34,322 cycles

(CUSTOMER REQUEST) CRACK SUPPORT ANGLE LOC BS 663 LH SIDE AT CENTER WING BOX 2023-310172<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED SUPPORT ANGLE LOC BS 663 LH SIDE AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG DRAWING 111A1000 SHEET 130 REV. A<BR>SEE INDIVIDUAL SIGNOFF BELOW;[03] REPLACED SUPPORT ANGLE LOC BS 663 LH SIDE AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG DRAWING 111A1000 SHEET 130 REV. A. RII VERIFIED

Part: BATTERY PACK — POPPED (ZN 200 FUS TOP) · airframe 66,112 hrs · 34,150 cycles

PASSENGER CABIN EMERGENCY LIGHTING L AFT CHGR CIRCUIT BREAKER POPS WHEN MOVED TO ARM POSITION<[01] RESET L AFT CHGR CIRCUIT BREAKER PER AMM 20-60-01 OK TO CONTINUE ON MEL 33-14-01 SP1 AUTH# 126571;[02] TROUBLESHOT PER FIM 33-50 TASK 801; REMOVED AND REPLACED EMERGENCY LIGHTING POWER SUPPLIES M1670; M1669 AND BATTERY PACKS AT M1668;M1669; M1670 AND M1673 PER AMM 33-51-06. OPS CHECK GOOD

Part: POWER SUPPLY — POPPED (ZN 200 FUS TOP) · airframe 66,112 hrs · 34,150 cycles

PASSENGER CABIN EMERGENCY LIGHTING L AFT CHGR CIRCUIT BREAKER POPS WHEN MOVED TO ARM POSITION<[01] RESET L AFT CHGR CIRCUIT BREAKER PER AMM 20-60-01 OK TO CONTINUE ON MEL 33-14-01 SP1 AUTH# 126571;[02] TROUBLESHOT PER FIM 33-50 TASK 801; REMOVED AND REPLACED EMERGENCY LIGHTING POWER SUPPLIES M1670; M1669 AND BATTERY PACKS AT M1668;M1669; M1670 AND M1673 PER AMM 33-51-06. OPS CHECK GOOD

Part: HANDLE — CRACKED (GALLEY DOOR) · airframe 65,676 hrs · 33,864 cycles

FWD GALLEY DOOR HANDLE CRACKED.<[01] REMOVED AND REPLACED HANDLE AS PER AMM 20-50-11.

Part: ANGLE — CRACKED (L/H WING) · airframe 64,281 hrs · 32,938 cycles

L/H WING PANEL 511AT PANEL SUPPORT FWD ATTACH 'Z' ANGLE IS CRACKED / [01] R&R L/H WING PANEL 511AT PANEL SUPPORT FWD ATTACH 'Z' ANGLE IN REF TO SRM 51-40-02. NO FURTHER DEFECTS NOTED.

Part: PANEL — CRACKED (FUSELAGE) · airframe 62,940 hrs · 32,058 cycles

193D HAS ONE DIMPLED AND CRACKED FASTENER HOLE / [01] NEW PANELS INSTALLED IAW AMM 53-51-21. REF TSR TRACKING #2022001030

Part: PANEL — CRACKED (FUSELAGE) · airframe 62,940 hrs · 32,058 cycles

194E PNL HAS SIX DIMPLED; CRACKED AND ELONGATED HOLES. / [01] NEW PANELS INSTALLED IAW AMM 53-51-21. REF TSR TRACKING #2022001030

Part: BALLAST — INOPERATIVE (CABIN LIGHTS) · airframe 61,711 hrs · 31,292 cycles

SIDEWALL LIGHT ABOVE R/H OVERWING EXIT DOOR INOP / [01] R&R'D BALLAST PER AMM 33-21-00. THIS CLEARS MEL 33-2-03. MDDR# 26052

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,112 hrs · 30,940 cycles

LEFT OVERWING EMERGENCY EXIT DOOR FLOOR PROXIMITY LIGHT ASSEMBLY DOES NOT ILLUMINATE. / [01] REPLACED FUSE ON M1668 BATTERY CHARGER AND PERFORMED SATISFACTORY TEST OF LEFT OVERWING EMERGENCY EXIT SIGN INCANDESCENT LIGHTS PER AMM 33-51-06-960-804.; [02] VERIFIED FUSE ON M1668 BATTERY CHARGER REPLACED AND PERFORMED GOOD TEST PER AMM 33-51-06-960-804.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,112 hrs · 30,940 cycles

LEFT OVERWING EMERGENCY EXIT SIGN INCANDESCENT LIGHTS DO NOT ILLUMINATE. / [01] REPLACED FUSE ON M1668 BATTERY CHARGER AND PERFORMED SATISFACTORY TEST OF LEFT OVERWING EMERGENCY EXIT SIGN INCANDESCENT LIGHTS PER AMM 33-51-06-960-804.; [02] VERIFIED FUSE ON M1668 BATTERY CHARGER REPLACED AND PERFORMED GOOD TEST PER AMM 33-51-06-960-804.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,112 hrs · 30,940 cycles

AFT SERVICE EMERGENCY DOOR INDICATOR DOES NOT ILLUMINATE. / [01] RE-LAMPED LIGHT ASSY. AND PERFORMED GOOD OP CHECK AS PER AMM 33-51-01-960-801. NO FAULTS FOUND.; [02] VERIFIED AFT SERVICE DOOR EMERGENCY LIGHT OPS CHECKED IS GOOD PER AMM 33-51-01-960-860. NO FAULTS NOTED.

Part: FLOOR SUPPORT — CRACKED (BS 312-328 RBL31) · airframe 61,112 hrs · 30,940 cycles

INTERCOSTAL CRACKED BS 312-328 RBL 31 WL 208 ; / [01] REMOVED CRACKED INTERCOSTAL BS 312-328 RBL31 WL208 PER SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW INTERCOSTAL PER SRM 51-40-05-0G-0 AND DWG 141A5410. OK TO INSTALL.; [03] VERIFIED LOCATE AND DRILL OF NEW INTERCOSTAL PER SRM 51-40-05 AND DWG 141A5410; OK TO INSTALL NEW INTERCOSTAL; [04] INSTALLED NEW INTERCOSTAL BS 312-328 RBL31 WL208 PER SRM 51-40-02-0G-0 AND DWG 141A5400.; [05] VERIFIED INSTALLATION OF NEW INTERCOSTAL AT BS 312-328; RBL31; WL208; PER SRM 51-40-02 AND DWG 141A5400.; [06] VERIFIED ALL WORK COMPLETE THIS TASK

Part: FLOORBEAM — CRACKED (BS 294) · airframe 61,112 hrs · 30,940 cycles

CRACK AT FLOOR BEAM FASTENER HOLE BS 294.5 RBL 52.5 WL 208 ; / [01] REMOVED CRACK BY 1' X 1' TRIM OUT AT BS 294.5 RBL 52.5 WL208 PER SRM 51-10-02-0G-0; [02] VERIFIED REMOVED CRACK BY 1' X 1' TRIM OUT AT BS 294.5 RBL 52.5 WL208 PER SRM 51-10-02-0G-0; [03] REQUEST NDI TO PERFORM HFEC INSPECTION OF EDGE OF TRIM OUT TO VERIFY CRACK FREE CONDITION.; [04] HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. CAL ID N500D IS000450; [05] INSTALLED E.W.I.S PROTECTION ON REPAIR AREA I.A.W AMM 20-60-07; [06] REMOVED DAMAGE PART OF THE UPPER CHORD APPROXIMATELY RBL 23-RBL60 BS294 WL208 I.A.W SRM 51-10-02-0G-0; [07] VERIFIED DAMAGE REMOVAL PER SRM 51-10-02-0G-0 AND EA 21-153-01789-WIP1; [08] VERIFIED COMPLETION OF REPAIR PER EA 21-153-01789; [09] VERIFIED COMPLETION OF REPAIR PER EA 21-153-01789.; [10] VERIFIED ALL STEPS COMPLETE.

Part: PLATE — CORRODED (AFT CARGO) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON PLATE AFT CARGO BAY BS847 RBL23 WL156 ; / [01] CORROSION ON PLATE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] RECEIVED NEW PLATE ON BFG P.O #823171 /2. NEW PART WILL BE INSTALLED ON FAULT # TTG8Q004VHYV; [03] VERIFIED; RECEIVED NEW PLATE ON BFG P.O #823171 /2. NEW PART WILL BE INSTALLED ON FAULT # TTG8Q004VHYV

Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 61,112 hrs · 30,940 cycles

FOUND CRACKED INTERCOSTAL BELOW FLOOR PANEL 231AF; BS 380-400; BL0; WL 208 (MARKED) ; / [01] REMOVED CRACKED INTERCOSTAL BELOW FLOOR PANEL 231AF BS 380-400 BL 0 WL 208 PER SRM 51-40-02.; [02] CERTIFIED REMOVED CRACKED INTERCOSTAL BELOW FLOOR PANEL 231AF BS 380-400 BL 0 WL 208 PER SRM 51-40-02.; [03] LOCATED AND DRILLED NEW INTERCOSTAL PER DWG 143A5400 SHEET:38 REV:A AND SRM 51-40-05.; [04] LOCATED AND DRILLED NEW INTERCOSTAL PER DWG: 143A5410 SHEET:13 REV:B AND SRM 51-40-05; [05] CERTIFIED LOCATED AND DRILLED NEW INTERCOSTAL PER DWG: 143A5410 SHEET:13 REV:B AND SRM 51-40-05.; [06] VERIFIED LOCATE AND DRILL OF NEW INTERCOSTAL PER DWG 143A5410 AND SRM 51-40-05; OK TO INSTALL; [07] INSTALLED NEW INTERCOSTAL ANGLE BELOW FLOOR PANEL 231AF BS 380-400 BL 0 WL 208 IAW SRM 51-40-02 AND DWG 143A5400 ;SHEET 38; REV:A.; [08] VERIFIED: INSTALLED NEW INTERCOSTAL ANGLE BELOW FLOOR PANEL 231AF BS 380-400 BL 0 WL 208 IAW SRM 51-40-02 AND DWG 143A5400 ;SHEET 38; REV:A.; [09] INSTALLED NEW INTERCOSTAL ANGLE BELOW FLOOR PANEL 231AF BS 380-400 BL 0 WL 208 IAW SRM 51-40-02 AND DWG 143A5400; SHEET 66; REV:-.; [10] VERIFIED: INSTALLED NEW INTERCOSTAL ANGLE BELOW FLOOR PANEL 231AF BS 380-400 BL 0 WL 208 IAW SRM 51-40-02 AND DWG 143A5400; SHEET 66; REV:-.; [11] VERIFIED REPLACEMENT OF INTERCOSTAL ANGLE BELOW FLOOR PANEL 231AF; BS 380-400; BL 0; WL 208; PER SRM 51-40-02 AND DWG 143A5400; SHEET 66; [12] VERIFIED ALL WORK COMPLETED THIS TASK

Part: BAFFLE — CRACKED (BS 500B) · airframe 61,112 hrs · 30,940 cycles

BAFFLE CLIP IS CRACKED ON FWD SIDE OF BS 500B LBL25 WL 155 ; / [01] REMOVED BAFFLE CLIP BS 500B LBL 25 WL 155 PER SRM 51-40-02-0G-0; [02] UPDATED MEASUREMENT TABLE; [03] LOCATED AND DRILLED NEW CLIP AT BS 500B LBL 25 WL 155 PO# 827746/1 PER SRM 51-40-05-0G-0 AND DWG 143A7505. OK TO INSTALL; [04] VERIFIED STEPS 1-3. OK TO INSTALL.; [05] VERIFIED LOCATION AND DRILL UP OF CLIP PER DWG 143A7505. OK TO INSTALL; [06] INSTALLED CLIP PER SRM 51-40-02-0G-0 AND DWG 143A7505; [07] VERIFIED INSTALL; [08] VERIFIED INSTALLED CLIP PER SRM 51-40-02-0G-0 AND DWG 143A7505; [09] ASSIGNED PART TO TASK; [10] COMPLETE

Part: ANGLE — CORRODED (BS 777) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON INTERCOSTAL ANGLE BELOW SHIELD IN ACB BS 777 RBL 22 WL 156 ; / [01] EVALUATED CORROSION ON INTERCOSTAL ANGLE; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION ON INTERCOSTAL ANGLE; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED ACB INTERCOSTAL ANGLE BELOW SHIELD AT BS767 - BS787 PER SRM 51-40-02-OG-0; [04] LOCATED AND DRILLED ACB INTERCOSTAL ANGLE BELOW SHIELD AT BS767 - BS787; RBL22; WL156 PER SRM 51-40-05-OG-0 AND DWG 146A8123. OK TO INSTALL; [05] OK TO I INSTALL INTERCOSTAL ANGLE.; [06] INSTALLED ACB NEW ANGLE BELOW SHIELD AT BS767 - BS787; RBL22; WL156 PER SRM 51-40-02-0G-0 AND DWG 146A8123; [07] ASSIGNED PART TO TASK; [08] INSPECTED INSTALL; [09] INSPECTED INSTALL

Part: BAFFLE — CRACKED (BS 500C) · airframe 61,112 hrs · 30,940 cycles

FORWARD CARGO BAY BAFFLE CLIP ON THE FORWARD SIDE OF BS 500C FRAME IS CRACKED LBL 25 WL 156 ; / [01] REMOVED FCB BAFFLE CLIP ON FWD SIDE OF BS500C FRAME; LBL 25; WL 156. PER SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW FCB BAFFLE CLIP FWD SIDE OF FRAME BS500C; LBL25. PER DWG 143A7505 AND SRM 51-40-05-0G-0. OK TO INSTALL.; [03] COMPLETED MEASUREMENT FIELD; [04] VERIFIED LOCATED AND DRILLED NEW FCB BAFFLE CLIP FWD SIDE OF FRAME BS500C; LBL25. PER DWG 143A7505 AND SRM 51-40-05-0G-0. OK TO INSTALL.; [05] INSTALLED NEW FCB BAFFLE CLIP FWD SIDE OF FRAME BS500C; LBL 25; WL 156. PER DWG 143A7505 AND SRM 51-40-02-0G-0; [06] VERIFIED INSTALLED NEW FCB BAFFLE CLIP FWD SIDE OF FRAME BS500C; LBL 25; WL 156. PER DWG 143A7505 AND SRM 51-40-02-0G-0; [07] COMPLETED

Part: BAFFLE — CRACKED (BS 400-420) · airframe 61,112 hrs · 30,940 cycles

FORWARD CARGO BAY BAFFLE IS CRACKED AT FASTENER HOLE BS 400-420 RBL 25 WL 156 ; / [01] REMOVED FCB BAFFLE AT BS400-BS420; RBL 25; WL 156. PER SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW FCB BAFFLE BS400-BS420; RBL 25; WL 156. PER DWG 153A7505; AND SRM 51-40-05-0G-0. OK TO INSTALL.; [03] ADDED MEASUREMENT FIELD; [04] VERIFIED LOCATED AND DRILLED NEW FCB BAFFLE BS400-BS420; RBL 25; WL 156. PER DWG 153A7505; AND SRM 51-40-05-0G-0. OK TO INSTALL.; [05] INSTALLED NEW FCB BAFFLE BS400-BS420 ;RBL 25; WL 156. PER DWG 143A7505 AND SRM 51-40-02-0G-0; [06] CORRECTION TO STEP 2; DWG # SHOULD BE 143A7505; [07] COMPLETED INSTALLATION OF BAFFLE; [08] CORRECTION TO STEP 2; DWG # SHOULD BE 143A7505; [09] VERIFIED INSTALLED NEW FCB BAFFLE BS400-BS420 ;RBL 25; WL 156. PER DWG 143A7505 AND SRM 51-40-02-0G-0; [10] COMPLETED

Part: BAFFLE — CRACKED (BS 500A-500B) · airframe 61,112 hrs · 30,940 cycles

FORWARD CARGO BAY BAFFLE BS 500A-500B LBL 25 WL 156 IS CRACKED AT FASTENER HOLE ; / [01] LOCATED AND DRILLED NEW INTERCOSTAL PER SRM 51-40-05-0G-0 AND DWG 143A7505; [02] REMOVED INTERCOSTAL PER SRM 51-40-02-0G-0; [03] UPDATED MEASUREMENT; [04] UPDATED MEASUREMENT TABLE; [05] LOCATED AND DRILLED NEW INTERCOSTAL PER SRM 51-40-05-0G-0 AND DWG 143A7505; [06] VERIFIED LOCATE AND DRILL OF NEW INTERCOSTAL PER SRM 51-40-05 AND DWG 143A7505; [07] OK TO INSTALL NEW INTERCOSTAL BS 500A-500B LBL WL 156; [08] VERIFIED OK TO INSTALL; [09] OK TO INSTALL INTERCOSTAL/ BAFFLE; [10] INSTALLED INTERCOSTAL PER SRM 51-40-02-0G-0; AND DWG 143A7505; [11] VERIFIED INSTALL; [12] VERIFIED INSTALLED INTERCOSTAL PER SRM 51-40-02-0G-0; AND DWG 143A7505; [13] COMPLETED

Part: WEB — CRACKED (BS 296) · airframe 61,112 hrs · 30,940 cycles

CRACK IN LWR SUBTHRESHOLD WEB BS 296 RBL 56 WL 208 ; / [01] BEGAN TO REMOVED FASTENER FROM BS290-BS328 WL208 RBL53-RBL58 I.A.W SRM 51-40-02 FOR ACCESS.; [02] REMOVED LOWER SUBTHRESHOLD WEB BS290-BS331 RBL56 WL208 I.A.W SRM 51-40-02-06-0; [03] UPDATED MEASUREMENTS.; [04] REPAIRED LWR SUBTHRESHOLD WEB BS 296 RBL 56 WL 208 IAW EA 21-153-01756; [05] VERIFIED LWR SUBTHRESHOLD WEB BS 296 RBL 56 WL 208 WAS REPAIRED IAW EA 21-153-01756

Part: SKIN — CORRODED (BS 694) · airframe 61,112 hrs · 30,940 cycles

**CORROSION** ON FUSELAGE SKIN AT BODY STATION 694; RBL 1; WL 306. / [01] REMOVED CORROSION ON FUSELAGE SKIN BS694 RBL1 WL306;1'X1' AREA I.A.W SRM 51-10-02-0G-01 AND ARM90-7023-01 TABLE 3001 ZONE 1; [02] VERIFIED REMOVED CORROSION ON FUSELAGE SKIN BS694 RBL1 WL306;1'X1' AREA I.A.W SRM 51-10-02-0G-01 AND ARM90-7023-01 TABLE 3001 ZONE 1; [03] UT INSP BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.036' ADJACENT TO 0.040'. EQUIP ID#: ATS2031 S/N: 170515011; [04] HFEC INSP BLEND IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [05] DAMAGE ON FUSELAGE SKIN BS694;RBL1;WL306 FOUND TO BE OUT LIMITS I.A.W ARM90-7023-01 TABLE 3001 ZONE 1 ORIGINAL MATERIAL THICKNESS IS 0.040' REMAINING MATERIAL TICKNESS IS 0.036'; [06] VERIFIED DAMAGE ON FUSELAGE SKIN BS694;RBL1;WL306 FOUND TO BE OUT LIMITS I.A.W ARM90-7023-01 TABLE 3001 ZONE 1 ORIGINAL MATERIAL THICKNESS IS 0.040' REMAINING MATERIAL TICKNESS IS 0.036'; [07] UPDATING MEASUREMENTS FOR FAULT.; [08] AS PER EA 21-153-01632; THE DAMAGES ARE ALLOWABLE FOR CONTINUED SERVICE WITH REPETITIVE INSPECTIONS DEFINED ON 21-153-01632-INSP.; [09] VERIFIED STEPS COMPLETE.; [10] VERIFIED STEPS COMPLETE.

Part: SKIN — CORRODED (BS 696) · airframe 61,112 hrs · 30,940 cycles

**CORROSION** ON FUSELAGE SKIN AT BODY STATION 696; RBL 5; WL 305. / [01] REMOVED CORROSION ON FUSELAGE SKIN BS696 RBL5 WL305;1'X1' AREA I.A.W SRM 51-10-02-0G-01 AND ARM90-7023-01 TABLE 3001 ZONE 1; [02] VERIFIED REMOVED CORROSION ON FUSELAGE SKIN BS696 RBL5 WL305;1'X1' AREA I.A.W SRM 51-10-02-0G-01 AND ARM90-7023-01 TABLE 3001 ZONE 1; [03] HFEC INSP BLEND IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [04] UT INSP BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.036' ADJACENT TO 0.040'. EQUIP ID#: ATS2031 S/N: 170515011; [05] DAMAGE ON FUSELAGE SKIN BS696;RBL5;WL305 FOUND TO BE OUT LIMITS I.A.W ARM90-7023-01 TABLE 3001 ZONE 1 ORIGINAL MATERIAL THICKNESS IS 0.040' REMAINING MATERIAL TICKNESS IS 0.036'; [06] VERIFIED DAMAGE ON FUSELAGE SKIN BS696;RBL5;WL305 FOUND TO BE OUT LIMITS I.A.W ARM90-7023-01 TABLE 3001 ZONE 1 ORIGINAL MATERIAL THICKNESS IS 0.040' REMAINING MATERIAL TICKNESS IS 0.036'; [07] REFER TO FAULT TTG8Q005BHK5 FOR REPAIR RESOLUTION.; [08] REFER TO FAULT TTG8Q005BHK5 FOR REPAIR RESOLUTION; QC VERIFIED.; [09] VERIFIED NDI COMPLETE; [10] REFER TO FAULT TTG8Q005BHK5 FOR REPAIR RESOLUTION; QC VERIFIED; [11] REFER TO EA 21-153-01632 SUMMARY REQUIREMENT; BARCODE: TTG8Q005N4KF.

Part: SUPPORT — CORRODED (BS 727D-787) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727D - BS787 WL156. ; LBL 21 / [01] EVALUATED CORROSION FROM 727D-787 DEEPEST MEASUREMENT WAS AT BS 767 FOUND 0.020 REMOVED FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/N UNKOWN; [02] VERIFIED CORROSION FROM 727D-787 DEEPEST MEASUREMENT WAS AT BS 767 FOUND 0.020 REMOVED FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/N UNKOWN; [03] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS787 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED ACB LH FLOOR TO SIDEWALL SUPPORT BS 724-847 PER SRM 51-40-05; DWG #146A7500.; [05] VERIFIED LOCATED AND DRILLED ACB LH FLOOR TO SIDEWALL SUPPORT BS 724-847 PER SRM 51-40-05; DWG #146A7500.; [06] OK TO INSTALL FLOOR TO SIDE WALL SUPPORT; [07] CERTIFIED OK TO INSTALL; [08] OK TO INSTALL GIVEN.; [09] INSTALLED NEW FLOOR TO SIDE WALL SUPPORT AT BS727-787 LBL21 WL156 IAW SRM 51-40-02-0G-0 AND DWG 146A7500;1498102 AND 146A7502.; [10] INSTALLATION OF FLOOR TO SIDE WALL SUPPORT ANGLE IS BS727-847 LBL21 WL156.; [11] VERIFIED INSTALLATION OF L/H FLOOR TO SIDEWALL SUPPORT B 727-847 PER DWG 146A7500; 149A8102; 146A7502; AND SRM 51-40-02; [12] VERIFIED WORK IS COMPLETED; [13] COMPLETE

Part: SUPPORT FITTING — CRACKED (BS 918) · airframe 61,112 hrs · 30,940 cycles

CRACKED SUPPORT FITTING AT AFT CARGO BAY BEHIND WATER SERVICE PANEL BS918 RBL11 WL149. ; / [01] REPLACED SUPPORT FITTING PER SRM 51-40-02-0G-0 AND DRAWING 147A7221; [02] VERIFIED INSTALLATION PER SRM 51-40-02-0G-0 AND DRAWING 147A7221; [03] FIX PART CALL OUT; [04] COMPLETE; [05] REMOVED;LOCATED;DRILLED AND INSTALLED PART PER SRM 51-40-02 AND DWG.147A7221; [06] VERIFIED REMOVED; LOCATED; DRILLED AND INSTALLED PART PER SRM 51-40-02 AND DWG.147A7221

Part: FRAME — CORRODED (BS 947) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON FRAME AT AFT CARGO BAY BS947 LBL9 WL178. ; / [01] UPDATED MEASUREMENT TABLE; [02] REMOVED CORROSION ON BS 947 FRAME LBL 9 WL 178 3'X1' PER SRM 53-00-07-1A-1; [03] VERIFIED REMOVED CORROSION ON BS 947 FRAME LBL 9 WL 178 3'X1' PER SRM 53-00-07-1A-1; [04] HFEC INSP BLEND IAW 737 NDTM PT 6 51-00-00 PROC 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [05] HFEC INSP OPEN HOLE(S) IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; FOUND 1 (EA) CRACK AT I/B HOLE OF THE BLENDED AREA; REQUIRES OVERSIZE. EQUIP ID#: IS000450 S/N: N500D000M120071 EQUIP ID#: ATS2407 S/N: MM1591DD064104; [06] OVERSIZED INBOARD FRAME FASTENER HOLE COMMON TO WATER TANK SUPPORT ANGLE FASTENER HOLE TO .199 PER SRM 51-40-05-0G-0; 51-40-05-0G-0 AND DWG 147AA1047. OK TO INSTALL; [14] VERIFIED LOCATE AND DRILL OF NEW 947 BOTTOM FRAME PER SRM 51-40-05-0G-0 AND DWG 147AA1047. OK TO INSTALL; [15] BEGAN INSTALLING 947 FRAME STR 23R TO STR 23L PER SRM 51-40-02-0G-0 AND DWG 147A1047; [16] INSTALLED 947 FRAME STR 23L TO 23R PER SRM 51-40-02-0G-0 DWG 147A4710 DWG 147A1047; [17] VERIFIED INSTALLATION 947 BOTTOM FRAME STR 23L TO 23R PER DWG 147A1047; [18] APPLIED CORROSION INHIBITING COMPOUND TO BS947; STR 23L TO 23R FRAME AND REPAIR AREAS. PER AMM 51-21-91-620-802; [19] VERIFIED CIC APPLIED; [20] REMOVED AND REPLACED FRAME CHANGE BS 947 STR 23R TO 23L PER SRM 51-40-02-0G-0 AND DWG 147A1047;

Part: SKIN — CORRODED (BS 727D) · airframe 61,112 hrs · 30,940 cycles

CHAFING DAMAGE ON INTERNAL FUSELAGE SKIN AT AFT CARGO BAY BS727D+16 LBL11 WL149. ; / [01] BLENDED CHAFE DAMAGE ON SKIN 3.3'X1.1' PER SRM 53-00-01-1A-5; [02] VERIFIED BLENDING ON CHAFE DAMAGE AREA ON SKIN 3.3'X1.1' PER SRM 53-00-01-1A-5; [03] HFEC INSP BLENDED AREAS IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [04] UT INSP BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.056' ADJACENT TO 0.063'. SEE ATTACHED GRID ON COVER SHEET. EQUIP ID#: ATS2031 S/N: 170515011; [05] CORROSION ON BILGE SKIN MEASURES 3.3'X1.1'X.010 ORIGINAL THICKNESS .063 ; .056' REMAINING FOUND OUT OF LIMITS DUE ONLY .05T ALLOWED IN AREA FOR SECTION 46 [08] VERIFIED CORROSION ON BILGE SKIN MEASURES 3.3'X1.1'X.007'ORIGINAL THICKNESS .063; .056 REMAINING FOUND OUT OF LIMITS DUE TO ONLY .05T ALLOWED IN AREA FOR SECTION 46 REDUCED LOWER FUSELAGE SKIN ALLOWABLE SURFACE DAMAGE PER SRM 53-00-01-1A-5; [09] REFER TO EA 21-153-01627 SUMMARY REQUIREMENT; BARCODE: TTG8Q005ME8J.; [10] BLENDED CHAFE DAMAGE PER EA 21-153-01627; [11] VERIFIED BLENDED CHAFE DAMAGE PER EA 21-153-01627; [12] VERIFIED BLENDED CHAFE DAMAGE PER EA 21-153-01627

Part: WEB — CORRODED (CARGO THRESHOLD) · airframe 61,112 hrs · 30,940 cycles

CORROSION IN FWD CARGO COMPARTMENT ON SUB THRESHOLD WEB AT BS 467 RBL 28 WL 156 ; / [01] EVALUATED CORROSION BS 467 FOUND 0.020 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN. SUBTHRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q005B9AH; [02] VERIFIED CORROSION BS 467 FOUND 0.020 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN. SUBTHRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q005B9AH

Part: SUPPORT — CORRODED (BS 500B) · airframe 61,112 hrs · 30,940 cycles

CORROSION IN FWD CARGO COMPARTMENT ON AFT FLOOR TO SIDEWALL SUPPORT AT BS 500B+9.5 RBL 25 WL 156 ; / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT; FOUND 0.020 REMOVED FROM ORIG 0.040 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER 4566A S/N UNKNOWN. FLOOR TO SIDEWALL SUPPORT TO BE REPLACED ON CUST CARD #TTG8Q005BEU0; [02] VERIFIED - EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT; FOUND 0.020 REMOVED FROM ORIG 0.040 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] VERIFIED FLOOR TO SIDEWALL SUPPORT TO BE REPLACED ON CUST CARD #TTG8Q005BEU0 NO FURTHER ACTION REQUIRED

Part: SEAT TRACK — CORRODED (BS 727C) · airframe 61,112 hrs · 30,940 cycles

CORROSION IN WELL OF SEAT TRACK BS727C LBL45 WL 208 ; / [01] UPDATED MEASUREMENT TABLE.; [02] BLENDED AND REMOVED CORROSION DAMAGE FROM SEAT TRACK FROM BS 727B+17 TO BS 727C+3; LBL 45; WL 208 IAW SRM 53-00-52-1A-1 DETAIL A AND SRM 51-10-02-0G-0.; [03] VERIFIED CORROSION REMOVAL PER SRM.; [04] REMOVED .020 FROM AN ALLOWABLE OF .040 FROM SEAT TRACK BS 727B+17 TO BS 727C+3; LBL 45; WL 208 IAW SRM 53-00-52-1A-1 DETAIL A. USED DIAL DEPTH GAGE ATS ID: E96GG; S/N UNKNOWN.; [05] APPLIED CHEMICAL CONVERSION COATING PER SRM 51-20-01; AND APPLIED PRIMER PER SOPM 20-41-04.; [06] CORRECT ITEM 4; CORRECT DIAL DEPTH GAGE IS ATS ID: E9655; S/N UNKNOWN.; [07] CORRECTION ITEM 4.; [08] VERIFIED; REMOVED .020 FROM AN ALLOWABLE OF .040 FROM SEAT TRACK BS 727B+17 TO BS 727C+3; LBL 45; WL 208 IAW SRM 53-00-52-1A-1 DETAIL A. APPLIED CHEMICAL CONVERSION COATING PER SRM 51-20-01; AND APPLIED PRIMER PER SOPM 20-41-04.

Part: SEAT TRACK — CORRODED (BS 727A) · airframe 61,112 hrs · 30,940 cycles

CORROSION IN WELL OF SEAT TRACK BS727A+10 LBL45 WL 208 ; / [01] UPDATED MEASUREMENT TABLE.; [02] BLENDED AND REMOVED CORROSION DAMAGE FROM SEAT TRACK FROM BS 727A+7 TO BS 727A+13; LBL 45; WL 208 IAW SRM 53-00-52-1A-1 DETAIL A AND SRM 51-10-02-0G-0.; [03] VERIFIED CORROSION REMOVAL PER SRM.; [04] REMOVED .022 FROM AN ALLOWABLE OF .040 FROM SEAT TRACK BS 727A+7 TO BS 727A+13; LBL 45; WL 208 IAW SRM 53-00-52-1A-1 DETAIL A. USED DIAL DEPTH GAGE ATS ID: E96GG; S/N UNKNOWN.; [05] APPLIED CHEMICAL CONVERSION COATING PER SRM 51-20-01; AND APPLIED PRIMER PER SOPM 20-41-04.; [06] CORRECTION; CORRECT PART NUMBER IS 144A5350-3; AND CORRECT DIAL DEPTH GAGE IS ATS ID: E9655; S/N UNKNOWN.; [07] CORRECTION ITEM 4 AND MEASUREMENT TABLE ITEM 14.; [08] VERIFIED; REMOVED .022 FROM AN ALLOWABLE OF .040 FROM SEAT TRACK BS 727A+7 TO BS 727A+13; LBL 45; WL 208 IAW SRM 53-00-52-1A-1 DETAIL A. APPLIED CHEMICAL CONVERSION COATING PER SRM 51-20-01; AND APPLIED PRIMER PER SOPM 20-41-04.

Part: SUPPORT — CORRODED (BS 500A) · airframe 61,112 hrs · 30,940 cycles

CORROSION IN FWD CARGO COMPARTMENT ON AFT FLOOR TO SIDEWALL SUPPORT AT BS 500A+10 RBL 25 WL 156 ; / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT; FOUND 0.020 REMOVED FROM ORIG 0.040 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER 4566A S/N UNKNOWN; [02] VERIFIED - CORROSION ON FLOOR TO SIDEWALL SUPPORT; FOUND 0.020 REMOVED FROM ORIG 0.040 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] REMOVED FCB R/H FLOOR TO SIDEWALL SUPPORT BS500A-BS500D; RBL 25; WL 156. PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED FCB FLOOR TO SIDEWALL SUPPORT BS 500A-500D; RBL 25 PER SRM 51-40-05; DWG#143A7500.; [05] VERIFIED LOCATED AND DRILLED FCB FLOOR TO SIDEWALL SUPPORT BS 500A-500D; RBL 25 PER SRM 51-40-05; DWG#143A7500.; [06] OLD FLOOR TO SIDEWALL SUPPORT BS 500A-500D RBL25 WL 156 WAS REMOVED ON SWA CARD# 5330-E-16461-NG. OK TO INSTALL NEW FLOOR TO SIDEWALL SUPPORT; [07] OK TO INSTALL; [08] INSTALLED FLOOR TO SIDEWALL SUPPORT BS 500A-500D RBL 25 WL 156 PER SRM 51-40-02-0G-0; DWG 143A7500 AND DWG 143A7505; [09] INSTALLED FLOOR TO SIDEWALL SUPPORT BS 500A-500D RBL 25 WL 156 PER SRM 51-40-02-0G-0; DWG 143A7500 AND DWG 143A7505; [10] INSTALLED FLOOR TO SIDEWALL SUPPORT BS 500A-500D RBL 25 WL 156 PER SRM 51-40-02-0G-0; DWG 143A7500 AND DWG 143A7505; [11] COMPLETE; [12] VERIFIED INSTALLATION FLOOR TO SIDEWALL SUPPORT BS 500A-500D RBL 25 WL 156 PER SRM 51-40-02-0G-0; DWG 143A7500 AND DWG 143A7505; [13] COMPLETE

Part: WEB — CORRODED (BS 454-459) · airframe 61,112 hrs · 30,940 cycles

CORROSION IN FWD COMPARTMENT ON SUB THRESHOLD WEB AT BS 459-454 RBL 28-30 WL 156 ; / [01] EVALUATED CORROSION BS 454-459 FOUND 0.020 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN; [02] VERIFIED CORROSION BS 454-459 FOUND 0.020 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN; [03] REMOVED FCB SUB-THRESHOLD WEB BS440-BS494; RBL 28; WL 156. PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED AND COUNTERSINK NEW WEB PER SRM 51-40-02; [05] INSTALLED NUTPLATES PER DWG. 143A8330 AND SRM 51-40-02-0G-0; [06] VERIFIED INSTALLATION OF NUTPLATES ON FCB SUBTHRESHOLD WEB PER DWG 143A8330 AND SRM 51-40-02; [07] OLD THRESHOLD WEB AT BS 440 TO 480+12' RBL 28-30 WL 156 WAS REMOVED ON SWA CARD# 5330-E-16461-NG. OK TO INSTALL NEW THRESLHOLD WEB; [08] ADDED PART USE; [09] OK TO INSTALL NEW THRESLHOLD WEB; [10] VERIFIED LOCATION AND DRILL UP OF NEW SUB-THRESHOLD. OK TO INSTALL.; [11] INSTALLED THRELHOLD WEB AT BS 440 TO 480+12' RBL 28-30 WL 156 PER SRM 51-40-02-0G-0; AND DWG 143A8330; [12] VERIFIED INSTALL; [13] VERIFIED INSTALLATION OF SUBTHRESHOLD PER DWG 143A8330 AND SRM 51-40-02; [14] COMPLETE

Part: WEB — CORRODED (BS 813) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON WEB AT AFT CARGO BAY BS813 RBL19 WL159. ; / [01] REMOVED CORROSION UNDERNEATH 1IN. BY 1IN. AT B.S.813;RBL19;WL159 PER SRM 53-60-15-1A-1; [02] REMOVED N/P FOR ACCESS PER SRM 53-60-15-1A-1; [03] VERIFIED CORROSION REMOVED; [04] UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS 0.046'<BR><BR>CAL ID ATS2031 E650; [05] BLEND MEASURES 1'X1'X.010. ORIGINAL THICKNESS .056; .046 REMAINING FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-0L-1 AND SRM 53-60-15-1A-1; [06] VERIFIED BLEND MEASUREMENTS OUT OF LIMITS PER SRM 53-60-15-1A-1; [07] REMOVED ACB WEB AT BS795 - BS847 PER SRM 51-40-02-0G-0; [08] LOCATED AND DRILLED ACB VERTICAL WEB AT BS795 - BS847; RBL19; WL159 PER SRM 51-40-05-OG-0 AND DWG 146A8121. OK TO INSTALL; [09] VERIFIED LOCATED AND DRILLED ACB VERTICAL WEB AT BS795 - BS847; RBL19; WL159 PER SRM 51-40-05-OG-0 AND DWG 146A8121. OK TO INSTALL; [10] INSTALLED ACB VERTICAL WEB AT BS795 - BS847; RBL19; WL159 PER SRM 51-40-02-OG-0 AND DWG 146A8121; DWG 146A8120; [11] VERIFIED INSTALLED ACB VERTICAL WEB AT BS795 - BS847; RBL19; WL159 PER SRM 51-40-02-OG-0 AND DWG 146A8121; DWG 146A8120.; [12] VERIFIED INSTALLED ACB VERTICAL WEB AT BS795 - BS847; RBL19; WL159 PER SRM 51-40-02-OG-0 AND DWG 146A8121; DWG 146A8120.

Part: SUPPORT — CORRODED (BS 787) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON SIDEWALL SUPPORT AT AFT CARGO BAY BS787 2' BELOW S-24L WL160. ; / [01] EVALUATED CORROSION ON SIDEWALL SUPPORT; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED CORROSION ON SIDEWALL SUPPORT; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED ACB SIDEWALL SUPPORT AT BS787+ 2' BELOW S-24L WL160 PER SRM 51-40-02-OG-0; [04] LOCATED AND DRILLED NEW ACB SIDEWALL SUPPORT ANGLE BS787; WL 157 TO WL 190. PER DWG 146A1262 AND SRM 51-40-05-0G-0. OK TO INSTALL.; [05] VERIFIED CORRECTIVE ACTION #3 AND 4; OK TO INSTALL; [06] INSTALLED NEW ACB SIDEWALL SUPPORT ANGLE BS787 FWD SIDE OF FRAME; WL 157 TO WL 190. PER DWG 146A1262 AND SRM 51-40-02-0G-0; [07] VERIFIED INSTALLATION OF NEW ACB SIDEWALL SUPPORT ANGLE BS787 FWD SIDE OF FRAME; WL 157 TO WL 190. PER DWG 146A1262 AND SRM 51-40-02-0G-0; [08] VERIFIED COMPLETE; [09] INSTALLED PART PER DRAWING 146A1262 AND SRM 51-40-02-0G-0; [10] CONFIRMED PART ENTRY AND DOCUMENTATION OF REPAIR COMPLETE; JOB COMPLETE

Part: SUPPORT — CORRODED (BS 867) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS867 RBL20 WL165. ; / [01] EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.040 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/N UNKOWN; [02] VERIFIED EVALUATED CORROSION; FOUND 0.020 REMOVED FROM ORIG 0.040 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/N UNKOWN; [03] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS867 - BS887 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED ACB SIDEWALL SUPPORT BS 867-887; RBL 20 PER SRM 51-40-05; DWG# 146A7500; [05] VERIFIED LOCATED AND DRILLED ACB SIDEWALL SUPPORT BS 867-887; RBL 20 PER SRM 51-40-05; DWG# 146A7500; [06] OK TO INSTALL FLOOR TO SIDEWALL SUPPORT; [07] OK TO INSTALL; [08] INSTALLED ACB FLOOR TO SIDEWALL SUPPORT AT BS867- BS887; RBL20; WL 156 PER SRM 51-40-02-OG-O AND DGW 146A7500; [09] ADDED DWG 147A0060; [10] VERIFIED INSTALLATION OF ACB FLOOR-TO-SIDEWALL SUPPORT; BS 867-887; RBL20; WL 156; PER SRM 51-40-02-OG-O; DGW 146A7500; AND DWG 147A0060; [11] COMPLETED; [12] VERIFIED COMPLETION OF ALL WORK THIS TASK

Part: CARGO TRACK — CORRODED (BS 773) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON RAIL AT AFT CARGO BAY BS773 RBL8 WL157. ; / [01] UPDATED MESUREMENTS; [02] CORROSION ON RAIL PREVIOUSLY REPAIRED SECTION WAS FOUND TO OUT OF LIMITS DO TO NO LIMITS ARE LISTED IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] VERIFIED; CONFIRMED; [04] BEGAN INSTALLING REPAIR CHANNEL PER SRM 53-00-53-2R-2; [05] REPLACED CHANNEL PER SRM 53-00-53-2R-2; [06] VERIFIED INSTALLATION OF ACB REPAIR CHANNEL; BS 773; RBL 8; WL 157; PER SRM 53-00-53-2R-2; [07] UPDATED USED PART; [08] VERIFIED ALL WORK COMPLETE THIS TASK; [09] PRIOR TO INSTALLATION REMOVED PREVIOUS REPAIR PER SRM 51-40-02 AND FABRICATED REPAIR PART PER SRM 53-00-53-2R-2; [10] PRIOR TO INSTALLATION; VERIFIED DAMAGED CHANNEL WAS REMOVED AND REPLACEMENT CHANNEL WAS FABRICATED; LOCATED AND DRILLED; PER SRM 51-40-02 AND SRM 53-00-53-2R-2; VERIFIED ALL WORK COMPLETED THIS TASK; [11] CERTIFIED STEP

Part: CARGO TRACK — CORRODED (BS 773) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON RAIL AT AFT CARGO BAY BS773 LBL3 WL157. UPDATED MEASUREMENTS; [02] CORROSION ON RAIL PREVIOUSLY REPAIRED SECTION WAS FOUND TO OUT OF LIMITS DO TO NO LIMITS ARE LISTED IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] VERIFIED; CONFIRMED; [04] BEGAN INSTALLING REPAIR CHANNEL PER SRM 53-00-53-2R-2; [05] REPLACED CHANNEL PER SRM 53-00-53-2R-2; [06] ASSIGNED PART TO TASK; [07] REJECTION: INSPECTED INSTALLATION OF REPLACED CHANNEL PER SRM 53-00-53-24R-2. FOUND FORDWARD MOST HI LOK IN UPPER FLANGE MISSING COLLAR. ALL OTHER FASTENERS GOOD GENERATED FAULT TTG8Q005H958; [08] VERIFIED REPLACEMENT OF ACB REPAIR CHANNEL; BS 773; LBL 3; WL 157 PER SRM 53-00-53-2R-2; VERIFIED RESOLUTION OF FAULT # TTG8Q005H958 (MISSING HI-LOK COLLAR); [09] VERIFIED ALL WORK COMPLETE THIS TASK; [10] PRIOR TO INSTALLATION REMOVED PREVIOUS REPAIR PER SRM 51-40-02 AND FABRICATED REPAIR PART PER SRM 53-00-53-2R-2; [11] PRIOR TO INSTALLATION; VERIFIED REMOVAL OF DAMAGED CHANNEL AND FABRICATION OF NEW CHANNEL PER SRM 51-40-02 AND SRM 53-00-53-2R-2; VERIFIED ALL WORK COMPLETE THIS TASK

Part: CARGO TRACK — CORRODED (BS 773) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON RAIL AT AFT CARGO BAY BS773 LBL8 WL157. UPDATED MEASUREMENTS; CORROSION ON RAIL PREVIOUSLY REPAIRED SECTION WAS FOUND TO OUT OF LIMITS DO TO NO LIMITS ARE LISTED IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0, BEGAN INSTALLING REPAIR CHANNEL PER SRM 53-00-53-2R-2. REPLACED CHANNEL PER SRM 53-00-53-2R-2. VERIFIED INSTALLATION OF ACB REPAIR CHANNEL, BS 773, LBL 8, WL 157 PER SRM 53-00-53-2R-2. FABRICATED REPAIR PART PER SRM 53-00-53-2R-2. VERIFIED ALL WORK COMPLETE THIS TASK.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 61,112 hrs · 30,940 cycles

RT HORIZ. STAB RIB ASSY 4 (120.30) 4TH VERT. STIFFENER IS CRACKED. ; / [01] -SRM 55-10-09-2R-4 IS APPLICABLE. QC NEEDS TO VERIFY APPLICABILITY.<BR><BR>-REMOVED DAMAGED SECTION ON RIB 3RD STIFFENER IAW SRM 55-10-09-2R-4 STEP 4 B (1); (2). CUTOUT DIMENSIONS: WEB<BR>L=0.645''; W=0.335''; VERTICAL STIFFENER L=2.600''; W=0.450''. QC NEEDS TO VERIFY DAMAGE REMOVAL.; [02] VERIFIED DAMAGE REMOVAL.; [03] -HFEC CUT OUT EDGES ON RIB WEB AND VERTICAL STIFFENER. NDI QC NEEDS TO VERIFY CRACK FREE CONDITION.<BR><BR>-HFEC EXISTING HOLES WITHIN THE REPAIR AREA. NDI QC NEEDS TO VERIFY CRACK FREE CONDITION.; [04] HFEC INSPECTED DAMAGE CUTOUT AND OPEN HOLES IN THE REPAIR AREA PER 737NDT PART 6 51-00-00 PROCEDURES 23 AND 16. NO CRACKS FOUND. CAL ID IS000450 DUE 12/2021 AND ATS1411 DUE 05/2022.; [05] -PERFORMED A GENERAL VISUAL INSPECTION OF ALL AREAS WITHIN THE REPAIR AREA IAW SRM 55-10-09-2R-4 STEP 4 E. NO DISCREPANCIES FOUND. QC REQUIRED TO VERIFY.<BR><BR>-FABRICATED REPAIR PARTS IAW SRM 55-10-09-2R-4 STEP 4 F THRU 4 J. REPAIR PARTS MADE FROM: T-SECTION 60-5872#7075T76511 LOT# 1449876-1; ANGLE BAC1490-2793#7075T62 LOT# 1435997-1; SHIMS 7075T6#0.016'' LOT# 1439717-1. RII QC REQUIRED.<BR><BR>-CHEMICAL CONVERSION COATING APPLIED TO REPAIR PARTS AND RIB BARE SURFACES IAW SRM 55-10-09-2R-4 STEP 4 K.; [06] ACCOMPLISHED GVI INSP. NO DEFECTS NOTED. VERIFIED PARTS FABRICATION AND CHEMICAL CONVERSION PER SRM.;

Part: SHIELD — CORRODED (BS 505-514) · airframe 61,112 hrs · 30,940 cycles

CORROSION IN FWD CARGO COMPARTMENT ON AFT SHIELD AT BS 505-514 RBL 25 WL 156 ; / [01] EVALUATED CORROSION ON FCB SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES TO BE REPLACED PER SRM 51-10-02-0G-0; [02] VERIFIED - CORROSION ON FCB SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES TO BE REPLACED PER SRM 51-10-02-0G-0; [03] REMOVED FCB AFT SHIELD PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED FCB AFT SHIELD PER SRM 51-40-05; DWG# 143A0080; [05] VERIFIED LOCATED AND DRILLED FCB AFT SHIELD PER SRM 51-40-05; DWG# 143A0080; [06] OLD SHIELD ON FWD CARGO AFT SIDE WAS REMOVED ON SWA CARD #5330-E-16461-NG. OK TO INSTALL NEW SHIELD; [07] VERIFIED OK TO INSTALL NEW SHIELD BS 505-514 RBL 25 WL 156.; [08] OK TO INSTALL NEW SHIELD BS 505-514 RBL 25 WL 156.; [09] INSTALLED NEW SHIELD BS 493-500A RBL25 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A0080.; [10] INSTALLED NEW SHIELD BS 493-500A RBL25 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A0080; VERIFIED.; [11] INSTALLED NEW SHIELD BS 493-500A RBL25 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A0080; VERIFIED.

Part: WEB — CORRODED (THRESHOLD) · airframe 61,112 hrs · 30,940 cycles

CORROSION IN FWD CARGO COMPARTMENT ON SUB THRESHOLD WEB AT BS 468 RBL 27 WL 156 ; / [01] EVALUATED CORROSION BS 468 FOUND 0.020 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN. SUBTHRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q005B9AH; [02] CARD COMPLETE; [03] VERIFIED CORROSION BS 468 FOUND 0.020 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN. SUBTHRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q005B9AH

Part: SEAT TRACK — CORRODED (BS 945) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS945 RBL8 WL179. ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON RAIL WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] VERIFIED; CONFIRMED; [04] CUT OUT DAMAGE SECTION AT B.S.941;RBL8;WL179 PER SRM 53-00-53-2R-2; [05] VERIFIED DAMAGE REMOVAL; [06] HFEC INSP OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071 EQUIP ID#: ATS2407 S/N: MM1591DD064104; [07] FABRICATED RAIL END FROM B.S 941 TO 951-BAC1509-100146#7075-T6511 LOT #5040028;CHEMICAL CONVERSION AND PRIMED PER SRM 563-00-53-2R-2; [08] LOCATED AND DRILLED REPAIR PARTS; APPLIED CHEMICAL CONVERSION AND PRIMER PER SRM 53-00-53-2R-2. OK TO INSTALL; [09] FABRICATED RAIL END FROM B.S 941 TO 951-BAC1509-100146#7050-T76511 LOT #1459408;CHEMICAL CONVERSION AND PRIMED PER SRM 53-00-53-2R-2; [10] LOCATED AND DRILLED SPLICE SI #53100004-001 LOT #1461073-1 PER SRM 53-00-53-2R-2. OK TO INSTALL REPAIR PARTS; [11] VERIFIED FABRICATION OF SPLICE AND RAIL END MATERIAL; DRILL UP; LOCATION; CONVERSION COATING AND PRIMER PER SRM 53-00-53-2R-2. OK TO INSTALL; [12] INSTALLED REPAIR PARTS PER SRM 53-00-53-2R-2 AND DWG. 147A7500; [13] VERIFIED INSTALLED REPAIR PARTS PER SRM 53-00-53-2R-2 AND DWG. 147A7500; [14] COMPLETED

Part: SHIELD — CORRODED (BS 767-787) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767 - BS787 RBL22 WL157. ; / [01] EVALUATED CORROSION ON SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED - CORROSION ON SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED ACB AFT SHIELD AT BS847-BS867; RBL22; WL 157 PER SRM 51-40-02-OG-0; [04] CORRECTION FOR STEP 3 BS 767-787; [05] LOCATED AND DRILLED NEW SHIELD PO# 821453/1 PER SRM 51-40-05-0G-0 AND DWG 146A0081; [06] LOCATED AND DRILLED NEW SHIELD PO# 821453/1 PER SRM 51-40-05-0G-0 AND DWG 146A0081; [07] VERIFIED LOCATE AND DRILL OF NEW FWD SHIELD PER SRM 51-40-05 AND DWG 146A0081; [08] OK TO INSTALL ACB AFT SHIELD; [09] OK TO INSTALL ACB FORWARD SHIELD; [10] VERIFIED OK TO INSTALL ACB FORWARD SHIELD; [11] INSTALLED ACB FWD NEW SHIELD AT BS767 - BS787; RBL22; WL157 PER SRM 51-40-02-OG-0 AND DGW 146A0081; [12] ASSIGNED PART TO TASK; [13] VERIFIED INSTALLATION OF NEW ACB FWD SHIELD AT BS767 - BS787; RBL22; WL157 PER SRM 51-40-02-OG-0 AND DGW 146A0081; [14] VERIFIED ALL WORK COMPLETE THIS TASK

Part: FRAME — DENTED (BS 747) · airframe 61,112 hrs · 30,940 cycles

DENT ON FRAME AT AFT CARGO BAY BS747 3' BELOW S-23L WL163. ; / [01] UPDATED DAMAGE TABLE; [02] FRAME IS FOUND OUT OF LIMITS DUE TO NO DENT DAMAGE ALLOWED ON FRAMES PER SRM 51-00-07-1A-1; [03] CUT AND REMOVED DAMAGE FRAME BS 747 3' BELOW STR 23L MEASURING 1.1'X1.1' PER SRM 51-10-02-0G-0; [04] VERIFIED CUT AND REMOVED DAMAGE FRAME BS 747 3' BELOW STR 23L MEASURING 1.1'X1.1' PER SRM 51-10-02-0G-0; [05] HFEC INSP CUTOUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [06] FRAME IS FOUND OUT OF LIMITS DUE TO NO DENT DAMAGE ALLOWED ON FRAMES PER SRM 53-00-07-1A-1; [07] PERFORMED GVI PER TTG8Q005EJN3; NO DISCREPANCIES NOTED; [08] NDT COMPLETE IN STEP 5; CONFIRMED TECH STATES NO CRACKS; [09] OK TO INSTALL.; [10] OK TO INSTALL.; [11] REFER TO EA 21-153-01615 SUMMARY REQUIREMENT; BARCODE: TTG8Q005L49K.; [12] REPAIRED DENT ON FRAME PER EA 21-153-01615; [13] VERIFIED REPAIRED DENT ON FRAME PER EA 21-153-01615; [14] VERIFIED REPAIRED DENT ON FRAME PER EA 21-153-01615 STEPS ARE COMPLETE.

Part: FRAME SPLICE — CORRODED (BS 787) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON SPLICE AT AFT CARGO BAY BS787 RBL25 WL158. ; / [01] UPDATED DAMAGE TABLE; [02] REPLACEMENT OF PART DUED NO ALLOWABLE DAMAGE GIVEN IN SRM; [03] REMOVED FRAME 787 R.H. SPLICE PER SRM 51-40-02; [04] LOCATED AND DRILLED NEW FRAME SPLICE P/N 146A1300U3 AT BS 787 RBL25 WL158 IAW SRM 51-40-05-0G-0 AND DWG 146A1262. OK TO INSTALL.; [05] VERIFIED LOCATED AND DRILLED NEW FRAME SPLICE P/N 146A1300U3 AT BS 787 RBL25 WL158 IAW SRM 51-40-05-0G-0 AND DWG 146A1262. OK TO INSTALL.; [06] INSTALLED NEW FRAME SPLICE P/N 146A1300U3 AT BS 787 RBL25 WL158 IAW SRM 51-40-02-0G-0 AND DWG 146A1262 .; [07] VERIFIED INSTALLATION OF FRAME SPLICE BS 787 RBL 25 WL 158 PER DWG 146A1262; [08] VERIFIED JOB COMPLETE

Part: SHIELD — CORRODED (BS 436) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON FWD CARGO COMPARTMENT FWD SHIELD AT BS 436 RBL 25 WL 156 ; / [01] EVALUATED CORROSION ON FCB SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES TO BE REPLACED PER SRM 51-10-02-0G-0; [02] VERIFIED - CORROSION ON FCB SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES TO BE REPLACED PER SRM 51-10-02-0G-0; [03] REMOVED FCB FWD SHIELD PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED FCB FWD SHIELD PER SRM 51-40-05; DWG #143A0080; [05] VERIFIED LOCATED AND DRILLED FCB FWD SHIELD PER SRM 51-40-05; DWG #143A0080; [06] OLD SHIELD ON FWD CARGO FWD SIDE WAS REMOVED ON SWA CARD #5330-E-16461-NG. OK TO INSTALL NEW SHIELD; [07] VERIFIED OK TO INSTALL NEW SHIELD BS 420-440 RBL 25 WL 156.; [08] OK TO INSTALL NEW SHIELD BS 420-440 RBL 25 WL 156.; [09] INSTALLED NEW SHIELD BS 420-440 RBL25 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A0080; [10] INSTALLED NEW SHIELD BS 420-440 RBL25 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A0080; VERIFIED.; [11] INSTALLED NEW SHIELD BS 420-440 RBL25 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A0080; VERIFIED.

Part: SCUFF PLATE — CRACKED (CARGO THRESHOLD) · airframe 61,112 hrs · 30,940 cycles

FORWARD CARGO BAY FORWARD CORNER THRESHOLD IS CRACKED ; / [01] WELDED CRACK ON FCB;FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT #1131216 IAW SRM 53-30-15-2R-1 PARA 4.B.(2) AND (4).<BR>WELDING MACHINE CAL I.D. E10583; S/N KJ256554; [02] VERIFIED WELDED CRACK ON FCB;FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT #1131216 IAW SRM 53-30-15-2R-1 PARA 4.B.(2) AND (4). <BR>WELDING MACHINE CAL I.D. E10583; S/N KJ256554; [03] DYE PENETRANT INSPECTED WELD PER SOPM 20-20-02. NO DEFECTS NOTED. EQUIP ID# ATS2561-1;2;3; [04] SANDED THE WELD REPAIRED AREA IAW SRM 53-30-15-2R-1 PARA 4.B.(5); [05] VERIFIED SANDED THE WELD REPAIRED AREA IAW SRM 53-30-15-2R-1 PARA 4.B.(5); [06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON FWD CARGO FORWARD CORNER THRESHOLD IAW SRM 53-30-15-2R-1; [07] VERIFIED APPLICATION OF PRIMER AND SRM 53-30-15-2R-1 IS COMPLETE.

Part: SEAT TRACK — CORRODED (BS 727C) · airframe 61,112 hrs · 30,940 cycles

CORROSION IN WELL OF SEAT TRACK BS727C LBL25 WL 208 ; / [01] UPDATED MEASUREMENTS TABLE.; [02] BLENDED AND REMOVED CORROSION DAMAGE FROM SEAT TRACK FROM BS 727B+17 TO BS 727C+3; LBL25; WL 208 IAW SRM 53-00-52-1A-1 DETAIL A AND SRM 51-10-02-0G-0.; [03] VERIFIED CORROSION REMOVAL PER SRM.; [04] REMOVED .022 FROM AN ALLOWABLE OF .040 FROM SEAT TRACK BS 727B+17 TO BS 727C+3; LBL 25; WL 208 IAW SRM 53-00-52-1A-1 DETAIL A. USED DIAL DEPTH GAGE ATS ID: E96GG; S/N UNKNOWN.; [05] APPLIED CHEMICAL CONVERSION COATING PER SRM 51-20-01; AND APPLIED PRIMER PER SOPM 20-41-04.; [06] CORRECT ITEM 4; CORRECT DIAL DEPTH GAGE ATS ID: E9655; S/N UNKNOWN.; [07] CORRECTION ITEM 4.; [08] VERIFIED; REMOVED .022 FROM AN ALLOWABLE OF .040 FROM SEAT TRACK BS 727B+17 TO BS 727C+3; LBL 25; WL 208 IAW SRM 53-00-52-1A-1 DETAIL A. APPLIED CHEMICAL CONVERSION COATING PER SRM 51-20-01; AND APPLIED PRIMER PER SOPM 20-41-04.

Part: SHIELD — CORRODED (BS 857-864) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON AFT SHIELD AT AFT CARGO BAY BS857 - BS864 RBL21 WL165. ; / [01] EVALUATED CORROSION ON SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED - CORROSION ON SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [03] REMOVED ACB AFT SHIELD AT BS847-BS867; RBL22; WL 157 PER SRM 51-40-02-OG-0; [04] LOCATED AND DRILLED NEW SHIELD PO#821208/1 PER SRM 51-40-05-0G-0 AND DWG 146A0081; [05] LOCATED AND DRILLED NEW SHIELD PO#821208/1 PER SRM 51-40-05-0G-0 AND DWG 146A0081; [06] VERIFIED LOCATE AND DRILL OF NEW AFT SHIELD PER SRM 51-40-05 AND DWG 146A0081; [07] OK TO INSTALL NEW ACB AFT SHIELD BS847-BS867; RBL 22; [08] OK TO INSTALL GIVEN.; [09] SEALED AND INSTALLED NEW ACB AFT SHIELD BS847-BS867; RBL 22. PER DWG 146A0081; AMM 51-31-00-390-801; AND SRM 51-40-02-0G-0; [10] VERIFIED SEALED AND INSTALLED NEW ACB AFT SHIELD BS847-BS867; RBL 22. PER DWG 146A0081; AMM 51-31-00-390-801; AND SRM 51-40-02-0G-0; [11] ASSIGNED PART TO TASK; [12] COMPLETED

Part: SUPPORT — CORRODED (BS 259 LBL2) · airframe 61,112 hrs · 30,940 cycles

CORRSION OF INTERCOSTAL SUPPORT ; CORRSION AT INTERCOSTAL SUPPORT BS 259 +4 LBL 2 WL 208 / [01] REMOVED CORROSION ON SUPPORT CHANNEL AT BS 294+4; LBL 2; WL 208. DIMENSION OF DAMAGE REMOVAL AREA FOUND TO BE 1' X 1' WITH A MAX DEPTH OF 0.007' FROM ORIGINAL THICKNESS OF .040'. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1; FIG. 105; DETAIL E.; [02] VERIFIED REMOVED CORROSION ON SUPPORT CHANNEL AT BS 294+4; LBL 2; WL 208. DIMENSION OF DAMAGE REMOVAL AREA FOUND TO BE 1' X 1' WITH A MAX DEPTH OF 0.007' FROM ORIGINAL THICKNESS OF .040'. DAMAGE REMOVAL WAS MEASURED BY ATS PIN POINT DEPTH GAUGE ID: ATS400; S/N: UNKNOWN; CAL DUE DATE: 04/2022. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1; FIG. 105; DETAIL E.; [03] REMOVED DAMAGED SUPPORT CHANNEL BS 259-270; LBL 3 - RBL 3; WL 208 PER SRM 51-40-02-0G-0.; [04] LOCATED AND DRILLED NEW SUPPORT CHANNEL BS 259-270; LBL 3 - RBL 3; WL 208 PER SRM 51-40-05-0G-0. OK TO INSTALL; [05] VERIFIED LOCATED AND DRILLED NEW SUPPORT CHANNEL BS 259-270; LBL 3 - RBL 3; WL 208 PER SRM 51-40-05-0G-0. OK TO INSTALL; [06] INSTALLED INTERCOSTAL SUPPORT BS 259-270; LBL 3 - RBL 3; WL 208 PER SRM 51-40-02-0G-0; DWG #141A5210.; [07] INSTALLED INTERCOSTAL SUPPORT BS 259-270; LBL 3 - RBL 3; WL 208 PER SRM 51-40-02-0G-0; DWG #141A5210; [08] VERIFIED INSTALL OF INTERCOSTAL SUPPORT BS 259-270; LBL 3 - RBL 3; WL 208 PER SRM 51-40-02-0G-0; DWG #141A5210; [09] COMPLETED

Part: SUPPORT — CORRODED (BS 727C-767) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727C - BS767 RBL21 WL156. ; / [01] EVALUATED CORROSION BS 727C-767 FOUND DEEPEST MEASUREMENT AT BS 747 OF 0.020 FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/N UNKOWN; [02] VERIFIED EVALUATED CORROSION BS 727C-767 FOUND DEEPEST MEASUREMENT AT BS 747 OF 0.020 FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/N UNKOWN; [03] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS67 RBL21; WL156 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05; SRM 51-40-08 AND DWG 146A7500 REV:-; [05] VERIFIED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05; SRM 51-40-08 AND DWG 146A7500;

Part: WEB — CORRODED (BS 807-840) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS807 - BS840 RBL26 WL160. ; / [01] EVALUATED CORROSION; FROM BS 807-840; FOUND DEEPEST MEASUREMENT AT BS 827 TO BE 0.020 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN; [02] VERIFIED CORROSION; FROM BS 807-840; FOUND DEEPEST MEASUREMENT AT BS 827 TO BE 0.020 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN; [03] REMOVED ACB SUB THRESHOLD WEB AT BS807 - BS847 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED ACB SUBTHRESHOLD WEB AT BS807 - BS840; RBL26; WL160 PER SRM 51-40-05-0G-0 AND DWG 146A8340; [05] VERIFIED CORRECTIVE ACTION #3 AND #4; [06] OK TO INSTALL ACB SUBTHRESHOLD WEB; [07] OK TO INSTALL ACB SUBTHRESHOLD WEB; [08] VERIFIED CORRECTIVE ACTION #6 AND #7. OK TO INSTALL SUBTHRESHOLD WEB; [09] INSTALLED ACB SUBTHRESHOLD WEB AT BS807 - BS840; RBL26; WL160 PER SRM 51-40-020G-0 AND DWG 146A8340; [10] UPDATED PART USE VERIFIED INSTALL; [11] VERIFIED INSTALL; [12] ASSIGNED PART TO TASK; [13] VERIFIED INSTALLED ACB SUBTHRESHOLD WEB AT BS807 - BS840; RBL26; WL160 PER SRM 51-40-020G-0 AND DWG 146A8340; [14] COMPLETED

Part: WEB — CORRODED (THRESHOLD) · airframe 61,112 hrs · 30,940 cycles

CORROSION IN FWD CARGO COMPARTMENT ON SUB THRESHOLD WEB BS 472-475 RBL 29 WL 156 ; / [01] EVALUATED CORROSION BS 472-475 FOUND 0.020 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN. SUBTHRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q005B9AH; [02] VERIFIED CORROSION BS 472-475 FOUND 0.020 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN. SUBTHRESHOLD WEB TO BE REPLACED ON CUST CARD#TTG8Q005B9AH

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 61,112 hrs · 30,940 cycles

CRACKED FLOOR SUPPORT BS 344-360 BL 0 WL 208 ; / [01] REMOVED CRACKED FLOOR SUPPORT INTERCOSTAL AT IAW SRM 51-40-02 AND DWG 141A5400.; [02] LOCATED AND DRILLED NEW INTERCOSTAL PER SRM 51-40-05 AND DWG 141A5400 SHEET 32 AND 16.REQUEST OK TO INSTALL.; [03] VERIFIED WORK ON STEPS 1 AND 2.; [04] VERIFIED DRILL UP PER DWG 141A5400 SHEET 32. OK TO INSTALL; [05] INSTALLED INTERCOSTAL AT B.S. 344-360 BL 0 WL 208 IAW SRM 51-40-02 AND DWG 141A5400 SHEET 16 AND 32.; [06] VERIFIED STEP; [07] UPDATED MEASUREMENTS TABLE AND PARTS TABLE ALL WORK COMPLETE; [08] VERIFIED INSTALLATION OF INTERCOSTAL IAW SRM 51-40-02 AND DWG 141A5400 SHEET 16 AND 32; [09] COMPLETE

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 61,112 hrs · 30,940 cycles

FLOOR SUPPORT CRACKED AT BS 294.5-312 RBL16 WL208 ; / [01] REMOVED INTERCOSTAL FROM BS 294.5-312 RBL 16 WL208 PER SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW INTERCOSTAL FOR BS 294.5-312 RBL16 WL 208 PER SRM 51-40-05-0G-0. OK TO INSTALL; [03] VERIFIED LOCATED AND DRILLED NEW INTERCOSTAL FOR BS 294.5-312 RBL16 WL 208 PER SRM 51-40-05-0G-0. OK TO INSTALL; [04] INSTALLED NEW INTERCOSTAL AT BS 294.5-312 RBL 16 WL 208 IAW SRM 51-40-02AND DWG 141A5400 ID:0045 REV:A.; [05] INSTALLED NEW INTERCOSTAL AT BS 294.5-312 RBL 16 WL 208 IAW SRM 51-40-02AND DWG 141A5400 ID:0045 REV:A. VERIFIED; [06] VERIFIED STEP 4; [07] VERIFIED INSTALLATION OF NEW INTERCOSTAL AT BS 294.5-312 RBL 16 WL 208 IAW SRM 51-40-02AND DWG 141A5400 ID:0045 REV:A. VERIFIED; [08] COMPLETED

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 61,112 hrs · 30,940 cycles

CRACKED FLOOR SUPPORT BS 277-294.5 BL0 WL208 ; / [01] REMOVED CRACKED FLOOR SUPPORT BS 277-294.5 BL 0 WL 208 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT BS 277 - 294.5 PER SRM 51-40-02-0G-0; BOEING DWG 141A5400; SRM 51-40-05-0G-0; [03] OK TO INSTALL NEW FLOOR SUPPORT BS 277-294.5 BL 0 WL 208; [04] LOCATED AND DRILLED NEW FLOOR SUPPORT BS 277 - 294.5 BL 0 WL 208 PER SRM 51-40-02-0G-0; BOEING DWG 141A5400; SRM 51-40-05-0G-0; [05] REMOVED CRACKED FLOOR SUPPORT BS 277-294.5 BL 0 WL 208 SRM 51-40-02-0G-0; [06] LOCATED AND DRILLED NEW FLOOR SUPPORT BS 277 - 294.5 BL 0 WL 208 PER SRM 51-40-02-0G-0; BOEING DWG 141A5400; SRM 51-40-05-0G-0; [07] OK TO INSTALL NEW FLOOR SUPPORT BS 277-294.5 BL 0 WL 208; [08] VERIFIED LOCATED AND DRILLED NEW FLOOR SUPPORT BS 277 - 294.5 BL 0 WL 208 PER SRM 51-40-02-0G-0; BOEING DWG 141A5400; SRM 51-40-05-0G-0; [09] OK TO INSTALL NEW FLOOR SUPPORT BS 277-294.5 BL 0 WL 208; [10] INSTALLED NEW FLOOR SUPPORT AT BS 277-294.5 BL0 WL208 PER SRM 51-40-02 AND DWG#141A5400; [11] VERIFIED STEP 10; [12] VERIFIED INSTALLATION NEW FLOOR SUPPORT AT BS 277-294.5 BL0 WL208 PER SRM 51-40-02 AND DWG#141A5400; [13] COMPLETED

Part: RETAINER — CRACKED (RT WING) · airframe 61,112 hrs · 30,940 cycles

RT WING UPPER T/E PANEL JUST AFT OF #2 PYLON; HORIZ SEAL RETAINER IS CRACKED. ; / REMOVED AND REPLACED RIGHT WING UPPER T/E PANEL JUST AFT OF #2 PYLON HORIZ. SEAL RETAINER IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-25.; VERIFIED REMOVED AND REPLACED RIGHT WING UPPER T/E PANEL JUST AFT OF #2 PYLON HORIZ. SEAL RETAINER IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-25.

Part: CHANNEL — CRACKED (BS 303) · airframe 61,112 hrs · 30,940 cycles

CRACKED FWD ENTRY DOOR MOPSILL INNER CHORD BS 303.9 LBL50 WL 208 ; / [01] REMOVED CRACKED FWD ENTRY DOOR MOPSILL INNER CHORD IAW SRM 51-40-02; [02] LOCATED AND DRILLED NEW FWD ENTRY DOOR MOPSILL PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 141A8112.; [03] VERIFIED LOCATED AND DRILLED NEW FWD ENTRY DOOR MOPSILL PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 141A8112.; [04] OK TO INSTALL FWD ENTRY DOOR MOPSILL; [05] OK TO INSTALL; [06] INSTALLED NEW FWD ENTRY DOOR MOPSILL INNER CHORD PER SRM 51-40-02-0G-0 AND DWG 141A8110.; [07] UPDATED PARTS USAGE DATA.; [08] REJECTION DRAWING MISSING SHEET NUMBER AND REV.; [09] INSTALLED NEW FWD ENTRY DOOR MOPSILL INNER CHORD PER SRM 51-40-02-0G-0 AND DWG 141A8110 SHEET 6 REV:-.; [10] VERIFIED INSTALLATION FWD ENTRY DOOR MOPSILL PER SRM 51-40-02-0G-0 AND DWG 141A8110 SHEET 6 REV:-; [11] COMPLETE

Part: RETAINER — CRACKED (RT WING SEAL) · airframe 61,112 hrs · 30,940 cycles

RT WING UPPER T/E PANEL JUST AFT OF #2 PYLON; VERT SEAL RETAINER IS CRACKED. ; / [01] REMOVED AND REPLACED RIGHT WING UPPER T/E PANEL JUST AFT OF #2 PYLON VERT. SEAL RETAINER IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-25.; [02] VERIFIED REMOVED AND REPLACED RIGHT WING UPPER T/E PANEL JUST AFT OF #2 PYLON VERT. SEAL RETAINER IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-25.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,112 hrs · 30,940 cycles

CRACKED FLOOR SUPPORT BS 312-328 LBL45 WL208 ; / [01] REMOVED CRACKED FLOOR SUPPORT BS312-328 LBL45 WL208 PER SRM 51-40-02-OG-0.; [02] LOCATED AND DRILED NEW FLOOR SUPPORT AT BS312-328 LBL45 WL208 PER SRM51-40-05-0G-0. OK TO INSTALL; [03] VERIFIED LOCATED AND DRILED NEW FLOOR SUPPORT AT BS312-328 LBL45 WL208 PER SRM51-40-05-0G-0. OK TO INSTALL; [04] INSTALLED NEW FLOOR SUPPORT AT BS312-328 LBL45 WL208 PER SRM 51-40-02-0G-0 AND DWG#141A5400; [05] VERIFIED INSTALLATION OF NEW FLOOR SUPPORT AT BS312-328 LBL45 WL208 PER SRM 51-40-02-0G-0 AND DWG#141A5400; [06] COMPLETED

Part: ANGLE — CORRODED (BS 312 THRSHOLD) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON THRESHOLD SUPPORT ANGLE BS 312+10 LBL50 WL 209 ; / REPAIR ACCOMPLISHED PER SRM 53-10-15-1A-1; REINSTALLED ONE NUTPLATE ON THRESHOLD SUPPORT ANGLE BS 321 LBL 50 WL 209 PER SRM 51-40-02-0G-0.; VERIFIED COMPLETE

Part: FAIRING — CHAFED (FUSELAGE) · airframe 61,112 hrs · 30,940 cycles

CHAFE DAMAGE ON INNER SURFACE OF WING TO BODY FAIRING 193AL ; CHAFE DAMAGE ON INNER SURFACE OF WING TO BODY FAIRING 193AL / [01] IDENTIFIED PANEL 193AL IAW SRM 53-40-70-0I-1.FIG 2; ITEM[7]. FOUND DAMAGE ALONG EDGEBAND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-70-40-1A-1.PARA 4.B.(2). REQUIRES REPAIR PER SRM 51-70-05-2R-6 IAW SRM 53-40-70-2R-1.TABLE 202.<BR>VALIDATED APPLICABILITY OF SRM 51-70-05-2R-6 IAW SRM 53-40-70-2R-1.<BR>REMOVED DAMAGE FROM APPROX. 21'X13' DAMAGED AREA IAW SRM 51-70-05-2R-6.PARA 4.A-D.; [02] VALIDATED REPAIR PER SRM 51-70-05-2R-6; [03] CHANGED ALLOWABLE DAMAGE REFERENCE TO SRM 53-40-70-1A-1.PARA 4.B.(2).; [04] CERTIFIED CHANGE; [05] VERIFIED MATERIAL ID PER SRM 53-40-70-0I-1<BR>VERIFIED DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS PER SRM 53-40-70-1A-1<BR>VALIDATED REPAIR PER SRM 51-70-05-2R-6<BR>VERIFIED DAMAGE REMOVAL PER SRM 51-70-05-2R-6; [06] FABRICATED REPAIR PLIES FOR EDGE BAND USING BMS 8-139CL1ST120 LOT # 1454655-1 AND BMS 8-139CL1ST1581 LOT # 1457262-2 AND INSTALLED USING BMS 5-154TY2/3CL2GR05 ADHESIVE. VACUUM BAGGED; 5X5 OK AND SET TO CURE IAW SRM 51-70-05-2R-6 PAR 4.C.-E.; [07] CORRECTION ON LINE ITEM 6. SRM 51-70-05-2R-6 CORRECTION IS PARA 4. E.-G.; [08] FOR ITEM 6. ADHESIVE LOT # 1454850-1 AND 5X5 CHECKED WITH HOT BONDER ID: IS000678 S/N: 12071586.; [09] CURED PLIES USING HOT BONDER ID: IS000678 S/N: 12071586; UN-BAGGED; LIGHTLY SANDED AND CLEANED IAW SRM 51-70-05-2R-6 PARA 4.G.; [10] CERTIFIED WORK ACCOMPLISHED IAW SRM 51-70-05-2R-6.;

Part: FAIRING — CHAFED (FUSELAGE) · airframe 61,112 hrs · 30,940 cycles

CHAFE DAMAGE ON INNER SURFACE OF 192E FAIRING / [01] IDENTIFIED PANEL192E / MATERIAL IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM (3). FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PAR 4.B.(6)(A). REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 PARA 4.B.(2) TABLE 202.; [02] REMOVED APPROX. 16' X 2' DAMAGED PLIES AND CLEANED SURFACE. NO CONTAMINATION OR WATER NOTED IAW SRM 51-70-05-2R-6 PARA 4.B.;C. AND D.; [03] VALIDATED IDENTIFICATION; ALLOWABLE DAMAGE; REPAIR AND WORK ACCOMPLISHED IAW SRM 53-40-70 AND SRM 51-70-05-2R-6.; [04] VALIDATED REPAIR PER SRM 51-70-05-2R-6; [05] VERIFIED MATERIAL ID PER SRM 53-40-70-0I-1<BR>VERIFIED DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS PER SRM 53-40-70-1A-1 <BR>VALIDATED REPAIR PER SRM 51-70-05-2R-6 <BR>VERIFIED DAMAGE REMOVAL; SURFACE PREP; PER SRM 51-70-05-2R-6; [06] CORRECTION FOR LINE ITEM1. IS ITEM (14) NOT(3).; [07] VERIFIED CORRECTION FOR ITEM #1.; [08] FABRICATED REPAIR PLIES FOR EDGE BAND USING BMS 8-79CL3ST1581 LOT # 1456761-1 AND BMS 8-79CL3ST120 LOT # 1457269-3 IAW SRM 51-70-05-2R-6 PAR 4.D.; [09] VERIFIED STEP 5.; [10] FABRICATE ADHESIVE REPAIR PLY FROM BMS5-129GR5 LOT 1457261-2 AND INSTALLED ALL REPAIR PLIES; VACUUM BAGGED; LEAK CHECKED GOOD AND SET TO CURE IAW SRM 51-70-05-2R-6 PARA 4.F-G USING HOT BONDER ID#ATS532 S/N 15092117.;

Part: STRAP — CORRODED (BS 1023-1024) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON SHEAR WEB TENSION STRAP AT B.S. 1023-1024; L.B.L. 3; W.L. 208.1. ; / [01] REMOVED CORROSION ON STRAP BS1023-1024 LBL3 WL 208 IAW SRM 51-10-02. AREA OF REMOVAL 1'X6' REMOVED .020' MATERIAL. ORIGINAL THICKNESS .071'. NO ALLOWABLE LIMITS IN SRM. PART REQUIRES REPLACEMENT.; [02] UPDATED TABLE; [03] VERIFIED TABLE INPUT; [04] VERIFIED CORROSION OUT OF LIMITS IAW SRM 51-10-02.; [05] REMOVED OUT OF LIMITS SHEAR WEB TENSION STRAP AT B.S. 1023-1024 ;L.B.L. 3; W.L. 208.1 PER SRM 51-10-02-0G-0-A20048.; [06] VERIFIED STEP; [07] RECEIVED NEW SHEAR WEB TENSION STRAP P\N 147A5620-3; LOCATED AND DRILLED FASTENER HOLES IN NEW STRAP IAW SRM 51-40-05 AND DWG 147A5600 I.D.:0032; REV:B. REQUESTING OK TO INSTALL.; [08] VERIFIED; [09] INSTALLED NEW STRAP AT B.S. 1023-1024;L.B.L 3; W.L. 208.1; IAW SRM 51-40-02 AND DWG 147A5600.; [10] VERIFIED WORK ACCOMPLISHED; [11] REPLACEMENT OF STRAP ACCOMPLISHED PER SRM51-40-02 AND DWG 147A5600; [12] REJECTION - 3 RIVETS WITH STEPPED BUCKTAILS; APPROX BS 1020-1022; LBL 3; WL 208. GENERATED FAULT TTG8Q005DS73; [13] VERIFIED REPLACEMENT OF STRAP ACCOMPLISHED PER SRM51-40-02 AND DWG 147A5600.; [14] VERIFIED PROPER TRASFER OF REJECTED ITEM; ALL STEPS COMPLETE.

Part: CHANNEL — CORRODED (L2 DOORWAY) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON AFT ENTRY DOOR MOP SILL AT B.S. 950-986; L.B.L. 52; W.L. 208.1. ; / [01] REMOVED CORROSION ON AFT ENTRY DOOR MOPSILL AT B.S. 950-986 L.B.L. 52 W.L. 208.1 IN AREA OF 2.3' BY 36' BY 0.010' PER SRM 53-70-15-1A-1 AND SRM 51-10-02-0G-0. OUT OF LIMITS PER SRM 53-70-15-1A-1.; [02] VERIFIED OUT OF LIMITS PER SRM.; [03] REMOVED AFT ENTRY DOOR MOPSILL PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW MOPSILL PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 147A8540.; [05] OK TO INSTALL NEW MOPSILL.; [06] VERIFIED; LOCATED AND DRILLED NEW MOPSILL PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 147A8540.; [07] VERIFIED; OK TO INSTALL NEW MOPSILL.; [08] INSTALLED NEW AFT ENTRY DOOR MOPSILL PER SRM 51-40-02-0G-0 AND DWG 147A8501.; [09] VERIFIED INSTALLATION OF NEW AFT ENTRY DOOR MOPSILL PER SRM 51-40-02-0G-0 AND DWG 147A8501.; [10] UPDATED PARTS ROW; [11] VERIFIED ALL WORK AND INSPECTIONS ACCOMPLISHED IAW SRM 53-70-15; SRM 51-40-02; SRM 51-40-05; SRM 51-40-08; DWG 147A8501 AND DWG 147A8540

Part: FLOORBEAM — CORRODED (BS 947) · airframe 61,112 hrs · 30,940 cycles

CORROSION ON FLOOR BEAM; ON UPPER SURFACE; AT B.S. 947; R.B.L. 43-49; W.L. 208.1. ; / [01] REMOVED CORROSION ON FLOOR BEAM ON UPPER SURFACE AT B.S. 947 R.B.L. 43-49 W.L. 208.1 IN AREA OF 2.2' BY 6.0' PER SRM 53-70-51-1A-1 AND SRM 51-10-02-0G-0; [02] VERIFIED CORROSION REMOVED; [03] UT INSPECTED BLENDS IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.149'.<BR><BR>CAL ID ATS2031 E650; [04] OUT OF LIMITS PER SRM 53-70-51-1A-1; [05] VERIFIED OUT OF LIMITS PER SRM.; [06] VERIFIED REPAIR OF BS947 RBL43-48 WL 208 UPPER CHORD ACCOMPLISHED PER EA 21-153-01608 FAULT TTG8Q0059PHH; [07] VERIFIED REPAIR OF BS947 RBL43-48 WL 208 UPPER CHORD ACCOMPLISHED PER EA 21-153-01608 FAULT TTG8Q0059PHH; [08] UPDATED MEASUREMENTS TABLE; [09] VERIFIED ALL STEPS COMPLETE.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 61,112 hrs · 30,940 cycles

RT HORIZ. STAB RID ASSY. 4 (STAB STA 120.30) 2ND VERT STIFFENER IS CRACKED. ; / REMOVED RT HORIZONTAL STABILIZER INSPAR RIB LOCATED AT STAB STATION 120.30 IAW SRM 51-40-02-0G-0; [03] -SRM 55-10-09-2R-4 REMOVED DAMAGED SECTION ON RIB 3RD STIFFENER IAW SRM 55-10-09-2R-4 STEP 4 B (1); (2). CUTOUT DIMENSIONS: WEB<BR>L=0.575''; W=0.350''; VERTICAL STIFFENER L=2.600''; W=0.450''. [05] -HFEC CUT OUT EDGES ON RIB WEB AND VERTICAL STIFFENER.HFEC EXISTING HOLES WITHIN THE REPAIR AREA. [06] HFEC INSPECTED DAMAGE CUTOUT AND OPEN HOLES WITHIN THE REPAIR AREA PER 737NDT PART 6 51-00-00 PROCEDURES 23 AND 16. NO CRACKS FOUND. CAL ID IS000450 DUE 12/2021 AND ATS1411 DUE 05/2022; [07] -PERFORMED A GENERAL VISUAL INSPECTION OF ALL AREAS WITHIN THE REPAIR AREA IAW SRM 55-10-09-2R-4 STEP 4 E. NO DISCREPANCIES FOUND. QC REQUIRED TO VERIFY.<BR><BR>-FABRICATED REPAIR PARTS IAW SRM 55-10-09-2R-4 STEP 4 F THRU 4 J. . VERIFIED FABRICATION OF REPAIR PARTS AND CHEMICAL CONVERSION PER SRM.; [09] -APPLIED PRIMER TO REPAIR PARTS AND RIB BARE METAL IAW SRM 55-10-09-2R-4 STEP 4 L. OK TO INSTALL REPAIR PARTS.; [10] VERIFIED PRIMER AND OK TO INSTALL; [11] -INSTALLED REPAIR PARTS ON RIB 2ND STIFFENER AREA IAW SRM 55-10-09-2R-4 STEP 4 M THRU 4 R. QC REQUIRED TO VERIFY INSTALLATION.;

Part: FAIRING — CHAFED (WING-BODY) · airframe 61,112 hrs · 30,940 cycles

WING TO BODY FAIRING PANEL 194CL INNER SURFACE AREAS ARE CHAFED. CHAFING ALONG THE INNER EDGE BAND EXCEEDS THE ALLOWABLE LIMITS OF SRM 53-60-70-1A-1 PARA 4 B 3 A. REMOVED CHAFING DAMAGE FROM ALONG THE INNER EDGE BAND; CLEANED REPAIR AREA. FABRICATED REPAIR PLIES, INSTALLED PLIES, VACUUM BAGGED PLIES AND VERIFIED 5X5 AND SET PLIES TO CURE, UNBAGGED PLIES AND LIGHTLY SANDED IAW SRM 51-70-05-2R-6 PARA 4.A-G AND I. UT INSPECTED REPAIR PER NDTM PART 4; 51-00-02. NO DISBONDS NOTED. REFINISHED REPAIR AREA IAW SRM 51-70-05-2R-6 PARA 4 STEP I.

Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 61,112 hrs · 30,940 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD UPPER SUPPORT ANGLE IS CRACKED AT L.B.L. 8; W.L. 164. ; / [01] INSTALLED EWIS PROCTECTION AT REPAIR AREA PER AMM 20-60-07; AND REMOVED FASTENERS PER SRM 51-40-02-0G-0; [02] VERIFIED ITEM 1; [03] CONFORMED -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE PER SRM57-101-10-2R-5; -1 REPLACEMENT ANGLE FABRICATED IN ACCORDANCE WITH SRM57-10-10-2R REPAIR 5 REFER TO ATS BUILD RECORD ATSHFAB-101-353 JOB # 533544; -2 SPLICE ANGLE FABRICATED IN ACCORDANCE WITH SRM57-10-10-2R-5 REFER TO ATS BUILD RECORD ATSHFAB-101-355 JOB # 539866; [04] CORRECTED TYPO SHOULD READ SRM 57-10-10-2R-5 NOT 57-101; [05] VERIFIED; [06] REMOVED DAMAGED AREA IAW SRM 57-10-10-2R-5.; [07] CONFORMED -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE PER SRM 57-10-10-2R-5 [13] VERIFIED LOCATED AND DRILLED REPAIR PARTS (FILLER AND DOUBLER );APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REPAIR PARTS AND REPAIR AREA AT BS 663 LBL 6-18.IAW SRM 57-10-10-2R-5. OK TO INSTALL; [14] INSTALLED REPAIR PARTS FILLER AND DOUBLER AT BS 663 LBL 6-18 WL 164 IAW SRM 57-10-10-2R-5; [15] VERIFIED INSTALLED REPAIR PARTS FILLER AND DOUBLER AT BS 663 LBL 6-18 WL 164 IAW SRM 57-10-10-2R-5; R

Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 61,112 hrs · 30,940 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD UPPER SUPPORT ANGLE IS CRACKED AT R.B.L. 8; W.L. 164. ; / [01] INSTALLED EWIS PROCTECTION AT REPAIR AREA PER AMM 20-60-07; AND REMOVED FASTENERS PER SRM 51-40-02-0G-0; [02] VERIFIED ITEM 1.; [03] CONFORMED -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE PER SRM 57-10-10-2R -1 REPLACEMENT ANGLE FABRICATED IN ACCORDANCE WITH SRM 57-10-10-2R REPAIR 5 REFER TO ATS BUILD RECORD ATSHFAB-101-354 JOB # 539510; -2 SPLICE SPLICE ANGLE FABRICATED IN ACCORDANCE WITH SRM 57-10-10-2R R; [17] REMOVED EWIS PROTECTION OF REPAIR AREA BS 663 RBL 6-39 IAW AMM 20-60-07-913-801; [18] VERIFIED APPLIED SEALING AROUND AND CIC AT REPAIR AREA BS663 RBL 6-18 WL 164 IAW SRM 57-10-10-2R-5. AND REMOVED EWIS PROTECTION OF REPAIR AREA BS 663 RBL 6-39 IAW AMM 20-60-07-913-801; [19] FUEL TANK CAP SEALING OF FASTENERS COMMON TO REPAIR AND LEAK CHECK OF FASTENERS WILL BE ACCOMPLISHED ON FAULT # TTG8Q00588KK; [20] VERIFIED FUEL TANK CAP SEALING OF FASTENERS COMMON TO REPAIR AND LEAK CHECK OF FASTENERS WILL BE ACCOMPLISHED ON FAULT # TTG8Q00588KK.

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 61,112 hrs · 30,940 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. ; / [01] EVALUATED DENTS ON FLIGHT DECK FLOOR AT BS 255; RBL 4-LBL 14; WL 207.54. DENTS FOUND TO BE GOUGED THEREFORE DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1; FIGURE 105; DETAIL D.; [02] VERIFIED DENTS ON FLIGHT DECK FLOOR AT BS 255; RBL 4-LBL 14; WL 207.54. DENTS FOUND TO BE GOUGED THEREFORE DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1; FIGURE 105; DETAIL D.; [03] FLIGHT DECK FLOOR AT BS 255 RBL 4-LBL 14 REPAIRED PER EA M-21-153-00734; [04] ALL EA M-21-153-00734 RII STEPS COMPLETE; [05] FLIGHT DECK FLOOR AT BS 255 RBL 4-LBL 14 REPAIRED PER EA M-21-153-00734

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 60,453 hrs · 30,577 cycles

CAPTAINS I/B AFT SEAT TRACK FAILED CHECK / R&R CAPTAINS I/B AFT SEAT TRACK PER M/M 25-11-11

Part: SEAT TRACK — FAILED (COCKPIT) · airframe 60,453 hrs · 30,577 cycles

FIRST OFFICERS I/B AFT SEAT TRACK FAILED CHECK / R&R FO'S I/B AFT SEAT TRACK PER M/M 25-11-11

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 60,453 hrs · 30,577 cycles

R1 DOOR SLIDE GIRT NEEDS REINSTALLED; TOO LONG. REINSTALLED R1 DOOR SLIDE GIRT PER AMM.256601 AND MT 7256106.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,082 hrs · 30,358 cycles

FWD CEILING EMERGENCY LIGHT IS INOPERABLE. RE-LAMP FWD CEILING EMERGENCY LIGHT, REF AMM 33-51-21.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 59,120 hrs · 29,777 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1668; M1669; M1671; M1672; M1673; M1674 AND M1675 IN THE CABIN. / R&R EMERGENCY LIGHT BATTERIES AT LOCATIONS M1668; M1669; M1671; M1672; M1673; M1674 AND M1675 PER MM 33-51-06

Part: SLIDE — UNSAFETIED (R1 DOOR) · airframe 58,508 hrs · 29,382 cycles

R1 DOOR EMERGENCY SLIDE LOOSE WAS FALLING OUT. REPACKED SLIDE PER EA MT.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 58,111 hrs · 29,131 cycles

WING TO BODY FAIRING PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. / REMOVED AND REPLACED 193B PANEL REF AMM 53-51-21 .

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 56,624 hrs · 28,151 cycles

L/H HORIZONTAL STABILIZER #4 RIB AT STA. 120.3, FRONT LOWER STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 56,624 hrs · 28,151 cycles

L/H HORIZONTAL STABILIZER #4 RIB AT STA. 120.3, 3RD FROM FRONT LOWER STIFFENER CRACKED. / REPAIRED STIFFENER IAW SRM.

Part: FLOOR SUPPORT — DAMAGED (BS 420-440) · airframe 56,624 hrs · 28,151 cycles

FORWARD CARGO BAY INTERCOSTAL DAMAGED BETWEEN BS. 420 TO BS. 440, RBL 24. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 56,624 hrs · 28,151 cycles

FORWARD WINDSCREEN INBOARD EMERGENCY FLASHLIGHT INOPERATIVE. / R&R BATTERY PACK IAW CMM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 56,624 hrs · 28,151 cycles

R/H HORIZONTAL STABILIZER #4 RIB AT STA. 120.30, 3RD FROM FRONT LOWER STIFFENER CRACKED. / REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 56,624 hrs · 28,151 cycles

L/H HORIZONTAL STABILIZER #4 RIB AT STA. 120.3, 2ND FROM FRONT LOWER STIFFENER CRACKED. / REPAIRED STIFFENER IAW SRM.

Part: SCUFF PLATE — CRACKED (R2 DOORWAY) · airframe 56,624 hrs · 28,151 cycles

R2 DOOR SCUFF PLATE CRACKED. R&R SCUFF PLATE IAW EA.

Part: FLOOR SUPPORT — CRACKED (FWD CARGO BAY) · airframe 56,624 hrs · 28,151 cycles

FORWARD CARGO BAY FLOOR SUPPORTCRACKED BETWEEN BS. 500 TO BS. 500A, LBL 24. R & R FLOOR SUPPORT IAW SRM AND DWG.

Part: CHANNEL — CORRODED (R2 DOOR WAY) · airframe 56,624 hrs · 28,151 cycles

R2 DOOR MOPSILL CORRODED AT BS. 987, RBL 50. / R&R MOPSILL IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (BS 312) · airframe 56,624 hrs · 28,151 cycles

L1 DOOR JUST ABOVE UPPER SILL FRAME EDGE CRACKED AT BS. 312. / REPAIRED FRAME IAW ER & EA.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 56,624 hrs · 28,151 cycles

FWD CARGO BAY THRESHOLD FWD OF DOOR IS BROKEN / LOCATED; DRILLED; CONTERSUNK AND DEBURED NEW FWD CARGO BAY THRESHOLD FWD OF DOOR PER SRM 51-40-05 AND SRM 51-40-08 AND INSTALLED NEW FWD. CARGO BAY THRESHOLD FWD OF DOOR PER SRM 53-13-00-08. 59595U 13JUNE19.

Part: SCUFF PLATE — BROKEN (FWD CARGO THRESH) · airframe 56,624 hrs · 28,151 cycles

FWD CARGO BAY THRESHOLD AFT OF DOOR IS BROKEN / LOCATED; DRILLED; COUNTERSUNK AND DEBURED NEW FWD CARGO BAY THRESHOLD AFT OF DOOR PER SRM 51-40-05 AND SRM 51-40-08 AND INSTALLED THE NEW FWD CARGO BAY THRESHOLD AFT OF DOOR PER SRM 53-13-00-08. 59595U 13JUN19.

Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 56,624 hrs · 28,151 cycles

LEFT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. / REMOVED AND INSTALLED NEW SERVICEABLE LEFT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLAT IAW AMM 53-31-31-000-802; 53-31-31-400-802 STEPS 3A-D;E;F 59048U 3JUNE19

Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 56,624 hrs · 28,151 cycles

RIGHT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. / REMOVED RIGHT HAND HORIZONTAL 59048U 3JUN19 STABILIZER FORWARD UPPER SLIDE SEAL PLATE IAW AMM 53-31-31-000-802 59048U 3JUN19 3228C 03JUN19 INSTALLED NEW SERVICEABLE RIGH HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IAW AMM 53-31-31-400-802 59048U 4JUN19

Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 56,624 hrs · 28,151 cycles

LEFT HAND HORIZONTAL STABILIZER FORWARD LOWER SLIDE SEAL PLATE IS CRACKED. / REMOVED AND INSTALLED NEW/SERVICEABLE LEFT HAND HORIZONTAL STABILIZER FORWARD LOWER SLIDE SEAL PLATE IAW AMM 53-31-31-000-803; 53-31-31-400-803; ADJUSTMENT GOOD 10JUN19

Part: BAFFLE — CRACKED (BS 400-420) · airframe 56,624 hrs · 28,151 cycles

FORWARD CARGO BAY BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT CRACKED BETWEEN BS. 400 TO BS. 420, LBL 24. / R&R BAFFLE IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 56,624 hrs · 28,151 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET IAW SRM AND DWG.

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 56,624 hrs · 28,151 cycles

***CORROSION*** ON FLOOR PANEL SUPPORT SPLICE AT AFT CARGO BAY BS767+6 RBL16 WL157. / REMOVED AND REPLACED FLOOR PANEL SUPPORT SPLICE IAW AMM 23-52-10-000-801 59366U 06/15/19 AND SOPM 20-50-01 AND DWG 146A9401 IN AFT CARGO BAY BS 767+6 RBL 16 WL 157

Part: WEB — CORRODED (BS 807) · airframe 56,624 hrs · 28,151 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED AT BS 807, RBL 26. R&R WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (BS 500C) · airframe 56,624 hrs · 28,151 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS. 500C, RBL 24. / R&R ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 500D) · airframe 56,624 hrs · 28,151 cycles

FORWARD CARGO BAY ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE CORRODED AT BS. 500D, BETWEEN LBL 23 TO RBL 21. / R&R ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 540) · airframe 56,624 hrs · 28,151 cycles

FLOOR SUPPORT CORRODED AT BS. 540, BETWEEN LBL 25 TO LBL 45. R&R FLOOR SUPPORT IAW SRM, DWG AND AMM.

Part: CREASE BEAM — CORRODED (BS 616) · airframe 56,624 hrs · 28,151 cycles

CREASE BEAM WEB INNER CHORD CORRODED AT BS. 616, LBL 63. / REPAIRED CHORD IAW ER AND EA.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 56,624 hrs · 28,151 cycles

FLOORBEAM CRACKED AT BS. 540, BETWEEN BL 0 TO RBL 25. / R & R FLOORBEAM TEE IAW AMM & DWG.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 56,624 hrs · 28,151 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 21. / R&R SUPPORT PER DWG & SRM.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 56,624 hrs · 28,151 cycles

FLOORBEAM CRACKED AT BS 540, BETWEEN BL 0 TO LBL 25. R&R THE FLOORBEAM IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 56,624 hrs · 28,151 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 847, LBL 21. R&R SUPPORT PER DWG & SRM.

Part: SHIELD — CORRODED (BS 420) · airframe 56,624 hrs · 28,151 cycles

FORWARD CARGO BAY ON FORWARD SHIELD CORRODED AT BS. 420+9, RBL 24. / R&R SHIELD IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 794-827) · airframe 56,624 hrs · 28,151 cycles

AFT CARGO BAY, CARGO TRACK FOUND CORRODED BETWEEN BS 794 TO 827, RBL 14. R & R THE CARGO TRACK IAW SRM.

Part: CREASE BEAM — CORRODED (BS 673-730) · airframe 56,624 hrs · 28,151 cycles

CREASE BEAM WEB INNER CORD CORRODED BETWEEN BS. 673 TO BS. 730, RBL 64. / REPAIRED CHORD IAW ER AND EA.

Part: ANGLE — CRACKED (FWD CARGO LH) · airframe 56,624 hrs · 28,151 cycles

CRACKED INTERCOSTAL SUPPORT ANGLE AT FWD CARGO BAY BS400 LBL24 WL155. MARKED / REMOVED AND REPLACED INTERCOSTAL SUPPORT ANGLE AT FCB BS 400 LBL 24 WL 155 IAW SRM 51-40-05; SRM 51-40-02-0G-0 AND DWG # 143A7505. 59647U 04JUN19

Part: GUSSET — CRACKED (BS 500D) · airframe 56,624 hrs · 28,151 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM AND DWG.

Part: TRACK — CORRODED (CABIN) · airframe 56,624 hrs · 28,151 cycles

***CORROSION*** SEAT TRACK FLANGE AT STA564; LBL45; WL208.1 / CORROSION ON SEAT TRACK FLANGE AT BS 564; LBL 45 WAS REPAIRED IAW ATS ER 19-03353 REV IR DATED 18JUN19 AND EA 1-757-16301 REV IR

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 56,624 hrs · 28,151 cycles

***CORROSION*** ON FLOOR PANEL SUPPORT SPLICE AT AFT CARGO BAY BS727D+6 LBL20 TO RBL20 WL155. MARKED / REMOVED AND REPLACED FLOOR PANEL SUPPORT SPLICE IAW AMM 25-52-10-000-801 59366U 6/15/19 AND SOPM 20-50-01 AND DWG 146A9401 IN AFT CARGO BAY BS727D+6 LBL20 TO RBL 20 WL 155

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 56,624 hrs · 28,151 cycles

***CORROSION*** ON FLOOR PANEL SUPPORT SPLICE AT AFT CARGO BAY BS887 LBL8 TO RBL21 WL168. / NO ALLOWABLE DAMAGES LIMITS FOUND IN S.R.M. FOR FLOOR PANEL SPLICE AT BS 887. REMOVED AND REPLACED FLOOR PANEL SUPPORT I/A/W S.R.M. 51-40-02 AND DWG 146A9401

Part: SUPPORT — CRACKED (BS 727) · airframe 56,624 hrs · 28,151 cycles

AFT CARGO BAY BULKHEAD PANEL SUPPORT CRACKED AT BS. 727+2, RBL 4. / R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 767-787) · airframe 56,624 hrs · 28,151 cycles

AFT CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS 767 TO 787, RBL 21. R&R THE SHIELD IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 787-794) · airframe 56,624 hrs · 28,151 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS. 787 TO BS. 794, RBL 24. / R&R INTERCOSTAL PER SRM AND DWG.

Part: CREASE BEAM — CORRODED (BS 673-727) · airframe 56,624 hrs · 28,151 cycles

CREASE BEAM WEB INNER CHORD CORRODED BETWEEN BS. 673 TO BS. 727, LBL 63. / REPAIRED CHORD IAW ER AND EA.

Part: CREASE BEAM — CORRODED (BS 628-673) · airframe 56,624 hrs · 28,151 cycles

CREASE BEAM WEB INNER CHORD CORRODED BETWEEN BS. 628 TO BS. 673, LBL 63. / REPAIRED CHORD IAW ER AND EA.

Part: SUPPORT — CORRODED (BS 400-500D) · airframe 56,624 hrs · 28,151 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 400 TO BS. 500D, LBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 56,624 hrs · 28,151 cycles

***CORROSION*** ON TENSION STRAP AT AFT CARGO BAY BS 794 TO BS847 RBL19 WL157. / REMOVED DAMAGE FROM ACB TENSION STRAPE BS794-BS847 RBL19 IN DIFFERENT PLACES MATERIAL THICKNESS/ ORIGINAL 0.100' REMAINING MATERIAL THICKNESS 0.085' FOUND TO BE OUT OF LIMIT IAW SRM 53-60-15-1A-1 LOCATED AND DRILLED NEW TENSION STRAPE ITEM# 7530562 IAW SRM 51-40-05-0G-0 AND DWG# 146A0081 AND INSTALLED IAW SRM 51-40-02-0G-0 AND BOE.DWG# 146A8120

Part: SHIELD — CORRODED (BS 847-867) · airframe 56,624 hrs · 28,151 cycles

AFT CARGO BAY AFT SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 21. / R&R SHIELD PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 56,624 hrs · 28,151 cycles

FLOOR BEAM UPPER SURFACE CORRODED AT BS. 986, RBL 45. / REPAIRED FLOOR BEAM PER EA AN ER.

Part: BEAM — CORRODED (CABIN) · airframe 56,624 hrs · 28,151 cycles

***CORROSION*** 986 FLOOR BEAM UPPER SURFACE HAS CORROSION LBL 41-LBL 45 / CORROSION ON BS 986 FLOOR BEAM UPPER SURFACE AT LBL 41- LBL 45 WAS REPAIRED IAW EA 1-A53-8241 REV 3

Part: RETAINER — CRACKED (RIGHT WING) · airframe 56,624 hrs · 28,151 cycles

#6 AFT FLAP TRACK FAIRING O/B CENTER BULB SEAL RETAINER IS BROKEN / REMOVED #6 AFT FLAP TRACK FAIRING O/B BULB SEAL RETAINER IAW SRM 51-40-02 88928C 21MAY19 INSTALLED NEW/SERVICEABLE #6 AFT FLAP TRACK FAIRING O/B CENTER BULB SEAL RETAINER IAW SRM 51-40-02-0G-0; FASTENER IDENTEFICATION IAW IPC 27-51-18-03 59048CC 07JUN19

Part: BULKHEAD WEB — CRACKED (ZONE 100) · airframe 56,624 hrs · 28,151 cycles

HORIZONTAL PRESSURE WEB CRACKED AT BS. 665, LBL 32. REPAIRED WEB IAW ER AND EA.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 56,624 hrs · 28,151 cycles

L/H WING LEADING EDGE SLAT #5 NOSE SKIN CRACKED AROUND FASTENER AT LOWER SURFACE OF THE AT ACTUATOR RIBS. / REPAIRED #5 NOSE SKIN IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 55,277 hrs · 27,267 cycles

RT LOWER OVERWING EXIT LIGHT LENS COVER MISSING. INSTALLED LENS PER MM.

Part: LATCH — BROKEN (FLASHLIGHT) · airframe 54,837 hrs · 26,978 cycles

AFT GALLEY FLASHLIGHT COMPARTMENT LATCH BROKEN. SECURED LATCH PER SIP.

Part: BRACKET — MISALIGNED (R1 DOOR GIRT BAR) · airframe 52,943 hrs · 25,714 cycles

R1 DOOR SLIDE GIRT BAR BRACKET COVER MISALIGNED. REALIGNED SLIDE PER MT.

Part: SIGN — LOOSE (CABIN) · airframe 51,178 hrs · 24,587 cycles

FORWARD GALLEY EXIT SIGN LOOSE. SECURED SIGN PER AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 49,972 hrs · 23,843 cycles

LT WING NR 3 SLAT LOWER SKIN CRACKED AT FORWARD FITTING HOLES. R&R NR 3 SLAT PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,972 hrs · 23,843 cycles

NR 4 SEAT TRACK CORRODED BETWEEN BS 650 TO BS 704, RBL 45. R&R SEAT TRACK PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 49,901 hrs · 23,797 cycles

FORWARD ENTRY EXIT LIGHT LENS LOOSE. R&R LIGHT BASE ASSEMBLY PER MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 45,562 hrs · 21,243 cycles

L2 DOOR EMER SIGN LIGHT LENS MISSING. INSTALLED LENS ASSEMBLY IAW MM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

SEAT TRACK CRACKED AT STATION 727B, RBL 24.75. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

SEAT TRACK CRACKED AT STATION 727B, RBL 45.50. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

SEAT TRACK CRACKED AT STATION 727B, LBL 45.50. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

SEAT TRACK CRACKED AT STATION 727B, LBL 27.75. REPAIRED TRACK IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,516 hrs · 20,014 cycles

LEFT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70, CRACKED ON VERTICAL STIFFENER LOCATED SECOND STIFFENER BACK ON LOWER END. REPAIRED RIB IAW SRM.

Part: STRAP — CORRODED (BS 787-797) · airframe 43,516 hrs · 20,014 cycles

FOUND THE FUSELAGE STRAP CORRODED AT BS 787 - 797, RBL 19, WL 156. R & R THE STRAP IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

AFT CARGO BAY FLOOR TO SIDEWALL CORRODED BETWEEN BS 727 - 767, RBL 20. R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 - 847, LBL 20. R & R SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 360, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 907) · airframe 43,516 hrs · 20,014 cycles

FOUND THE FUSELAGE FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 727B, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 867) · airframe 43,516 hrs · 20,014 cycles

FOUND THE FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 43,516 hrs · 20,014 cycles

LEFT WING OTBD AFT FLAP INBD TE DELAMINATED. R & R AFT FLAP IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,516 hrs · 20,014 cycles

RIGHT WING NR 8 SLAT LOWER NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: POST — CRACKED (NR 3 WINDOW) · airframe 43,516 hrs · 20,014 cycles

FOUND THE NR 3 RT COCKPIT WINDOW POST CRACKED. REPAIRED THE POST IAW EA.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

GIRT BAR ATTACH FITTING CORRODED AT BS 344, LBL 60. R & R FITTING IAW SOPM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

LEFT CREASE BEAM CORRODED AT STATION 706 TO 727A. REPAIRED BEAM IAW EA.

Part: POST — CRACKED (NR 3 WINDOW) · airframe 43,516 hrs · 20,014 cycles

FOUND THE NR 3 LEFT COCKPIT WINDOW POST CRACKED. REPAIRED THE WINDOW POST IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,516 hrs · 20,014 cycles

RIGHT NR 3 WINDOW FRAME E - F POST THE 2ND & 3RD LOWER FASTENER HOLES CRACKED. REPAIRED FRAME IAW ER & EA.