N461WN

Part: UNKNOWN — ODOR (CABIN) · airframe 70,449 hrs · 42,250 cycles

FA SMELLED SOME ELECTRICAL ODOR CENTER CABIN ROW 7. C/W FUMES IN THE CABIN, NO DEFECTS NOTED IAW FIM 21-00 TASK 806. ACFT OK FOR SERVICE.

Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 70,393 hrs · 42,211 cycles

ELONGATED HOLE IN ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.

Part: TAIL CONE — DELAMINATED (ZONE 100) · airframe 70,393 hrs · 42,211 cycles

DELAMINATED TAIL CONE RIGHT SIDE ON EXTERNAL SKIN. REPAIRED TAIL CONE RIGHT SIDE ON EXTERNAL SKIN IAW SRM 51-70-04-2R-1, REPAIR 1.

Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 70,393 hrs · 42,211 cycles

CRACKED SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-O2, & SRM 51-10-02, ITEM 9. MEASUREMENT OF CRACK IS 0.200".

Part: PLATE — CRACKED (ZONE 600) · airframe 70,393 hrs · 42,211 cycles

CRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT RT WING. REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE ORSS 261 AT RT WING IAW SRM 51-10-02-0G-O, PARAGRAPH 9; DRAWING 115A2001 SHEET 29, REV- AND SRM 51-40-02-0G-0. MEASUREMENT OF CRACK, REMOVED: L: 0.44F INCH.

Part: SUPPORT ANGLE — CRACKED (ZONE 600) · airframe 70,393 hrs · 42,211 cycles

CRACK SUPPORT ANGLE, TRAILING EDGE ORSS 280 AT RT WING. EVALUATED SUPPORT ANGLE AND NOT FOUND ON ALLOWABLE DAMAGE ON SRM IAW SRM-57-51-02-1A-1 ALLOWABLE DAMAGE 1. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02 AND DWG 115A6200 SHEET 10 REV - MEASUREMENT OF CRACK: 0.300".

Part: PLATE — CRACKED (ZONE 600) · airframe 70,393 hrs · 42,211 cycles

CRACK CORRUGATED PLATE TRAILING EDGE IRSS 215 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 215 AT RT WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 30; REV A.

Part: PLATE — CRACKED (ZONE 500) · airframe 70,393 hrs · 42,211 cycles

CRACKED CORRUGATED PLATE TRAILING EDGE IRSS 215 AT LT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02-0G-0, PARAGRAPH 9, DRAWING 115A2001, SHEET 30, REV A, & SRM 51-40-02-0G-0. MEASUREMENT OF CRACK: REMOVED: L: 0.519 INCH.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 70,393 hrs · 42,211 cycles

CRACK ON AFT CORNER SCUFF PLATE IN FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS 2 TO 7, FIGURE 203.

Part: ANGLE — CRACKED (ZONE 500) · airframe 70,393 hrs · 42,211 cycles

CRACKED ANGLE, TRAILING EDGE ORSS 271 LT WING. REPLACED THE ANGLE IAW SRM 51-40-02, AND DRAWING 115A2930, SHEET 7, REV -.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 70,393 hrs · 42,211 cycles

CRACK SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND RBL 1 PASSENGER CABIN. INSTALLED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE BS 695 AND RBL 1 PASSENGER CABIN IAW SRM 51-40-0G AND DRAWING 273A9110 SHEET 6 REV A.

Part: ACCESS PANEL — DELAMINATED (ZONE 400) · airframe 70,393 hrs · 42,211 cycles

DELAMINATED ACCESS PANEL 431AT AT RT PYLON. PERFORMED VISUAL INSPECTION ON ACCESS PANEL 431AT AT RT PYLON AND NOT FOUND DAMAGE ON FIBER SKIN ONLY WAS FOUND SURFACE PROTECTION DETERIORATED IAW B737-700 NDT PART 1. 51-05-01 PARAGRAPH 3 AND RESTORED SURFACE PROTECTION IAW AMM 51-21-99-300-801.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 70,393 hrs · 42,211 cycles

CRACKED ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 70,393 hrs · 42,211 cycles

DELAMINATED FLOOR PANEL 241EF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN IAW SRM 53-00-50-2R-1 REPAIR 1.

Part: PRESSURE DECK — CRACKED (ZONE 100) · airframe 70,393 hrs · 42,211 cycles

CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 43 BETWEEN STA 663 TO STA 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.312 IN. APPROX. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK WEB AT RBL 43 BETWEEN BS 663 - 675 AT MAIN WHEEL WELL COMPARTMENT IAW SRM 53-40-51-2R-2 REPAIR 2.

Part: BRACKET — CORRODED (ZONE 600) · airframe 70,393 hrs · 42,211 cycles

CORROSION ON BRACKET FUEL BOOST PUMP REA LOCATED IRSS147 AT RT WING (2 E/A). REPLACED BRACKET FUEL BOOST PUMP AREA LOCATED IRSS147 AT RT WING IAW AMM 28-22-41-000-801 AND AMM 28-22-41-400-801.

Part: LIGHT — BROKEN (ZONE 200) · airframe 70,393 hrs · 42,211 cycles

BROKEN PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA). REPLACED PHOTOLUMINESCENT STRIPS IAW DWG 33500007, REV 2, & SOPM 20-50-12, REV 58.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 70,393 hrs · 42,211 cycles

CRACK HOLE ACCESS PANEL 561BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.

Part: LAMP — INOPERATIVE (ZONE 200 EXT) · airframe 69,803 hrs · 41,852 cycles

AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-03.

Part: HOOK — LOOSE (GIRT BAR) · airframe 69,722 hrs · 41,797 cycles

FWD SERVICE DOOR GIRT BAR HOOKS ARE REPORTED LOOSE. ADJUSTED FORWARD SERVICE DOOR GIRT BAR HOOKS IN REFERENCE TO AIRCRAFT MAINTENANCE MANUAL 25-66-00-201-NG

Part: FRAME — PULLED (ZONE 400) · airframe 68,684 hrs · 41,157 cycles

#1 ENG AFT STRUT FAIRING O/B SIDE FWD STIFFENER HAS PULLED THRU HILOCS <[01]. REPLACED FRAME SECTION AS REQUIRED REF SRM 51-40-05 AND DWG313A2700.

Part: SLIDE — DISLODGED (ZONE 800) · airframe 68,213 hrs · 40,865 cycles

LEFT AFT ENTRY DOOR SLIDE FELL OUT OF CONTAINER<[01] INSTALLED SLIDE PER M/M 25-66-01;AND MT#725-61-06-AE.NO DEFECTS NOTED.

Part: SKIN — DELAMINATED (ZONE 500 FLAP) · airframe 67,083 hrs · 40,188 cycles

L/H OUTBOARD AFT FLAP IS DELAMINATED ON INBD SIDE.<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.;[02] C/W INSP. REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.

Part: COVER — DISPLACED (ZONE 200) · airframe 66,791 hrs · 39,998 cycles

SEAT 12F EMERGENCY EXIT LIGHT COVER DISPLACED<[01] RE SECURED EMERGENCY EXIT LIGHT COVER AT SEAT 12F; REF STANDARD INDUSTRY PRACTICES.

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 66,756 hrs · 39,977 cycles

FORWARD CARGO BIN HAS A CRACK IN BIN FLOOR<[01] OK TO CONTINUE PER MEL 25-16-01 SP1<BR>FWD BAG PIT UNUSABLE;[02] R&R FWD CGO COMPARTMENT FLOOR PANEL PER AMM 25-52-10.

Part: BULB — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,738 hrs · 38,739 cycles

FSD UPPER EMERGENCY EXIT FWD BULB IS BURNT OUT 2023-652354<[01] REPLACED UPPER EMERGENCY EXIT FWD BULB IAW: B737-700 SWPM 20-84-13 AND PERFORMED OPERATIONAL TEST AMM 33-51-00-720-801 TEST IS OK.;[02] REPLACED UPPER EMERGENCY EXIT FWD BULB IAW: B737-700 SWPM 20-84-13 AND PERFORMED OPERATIONAL TEST AMM 33-51-00-720-801 TEST IS OK.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,738 hrs · 38,739 cycles

AFT SERVICE DOOR UPPER EMERGENCY EXIT LIGHT HAS BURNT OUT BULB 2023-652353<[01] REPLACED AFT SERVICE DOOR UPPER EMERGENCY EXIT LIGHT IAW: B737-700 SWPM 20-84-13 AND PERFORMED OPERATIONAL TEST AMM 33-51-00-720-801 TEST IS OK.;[02] REPLACED AFT SERVICE DOOR UPPER EMERGENCY EXIT LIGHT IAW: B737-700 SWPM 20-84-13 AND PERFORMED OPERATIONAL TEST AMM 33-51-00-720-801 TEST IS OK.

Part: NUT PLATE — CORRODED (ZN 600 RIGHT WIN) · airframe 64,738 hrs · 38,739 cycles

CORROSION RAIL NUT INTERNAL CAVITY LEADING EDGE OFSS 292 AT RT WING 2023-652286<[01] REPLACED RAIL NUT INTERNAL CAVITY LEADING EDGE OFSS 292 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 112A4402 SHEET 8 REV.B;[02] REPLACED RAIL NUT INTERNAL CAVITY LEADING EDGE OFSS 292 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 112A4402 SHEET 8 REV.B

Part: SLAT TRACK — CRACKED (ZN 500 LEFT WING) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE SLAT 1 INBOARD AUXILIARY SLAT TRACK AT LT WING 2023-652285<[01] REPLACED ANGLE SLAT 1 INBOARD AUXILIARY SLAT TRACK AT LT WING IAW B737-700 SRM 51-40-02;[02] REPLACED ANGLE SLAT 1 INBOARD AUXILIARY SLAT TRACK AT LT WING IAW B737-700 SRM 51-40-02

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ON STRINGER 15L LOCATED AT BS 294.5 MORE 4 INCH AT FWD GALLEY AREA 2023-652267<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE: 15-FEB-24 WAS USED.;[02] REPAIRED STRINGER 15L LOCATED AT BS 294.5 MORE 4 INCH AT FWD GALLEY AREA IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 STEP 4.K THROUGH L AND TABLE 201 FIGURE 206 SHEETS 1 AND 2;[03] CORRECTED STEP 2: REPAIRED STRINGER 15L LOCATED AT BS 294.5 MORE 4 INCH AT FWD GALLEY AREA IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 STEP 4.K THROUGH L AND TABLE 201 FIGURE 206 SHEETS 1 AND 2. SEE INDIVIDUAL SIGN-OFFS BELOW.;[04] REPAIRED STRINGER 15L LOCATED AT BS 294.5 MORE 4 INCH AT FWD GALLEY AREA IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 STEP 4.K THROUGH L AND TABLE 201 FIGURE 206 SHEETS 1 AND 2. SEE INDIVIDUAL SIGN-OFFS BELOW.

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK SUPPORT ANGLE LOCATED BS867 AND BETWEEN STR2R/STR3R AT PASSENGER CABIN 2023-652137<[01] REPLACED SUPPORT ANGLE LOCATED BS867 AND BETWEEN STR2R/STR3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND #DWG:146A7901 SHEET: 58 REV:-.;[02] TASK COMPLETED

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK STRINGER 26R BS 540 FWD CARGO COMPARTMENT 2023-652107<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[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 26R LOCATED BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED STRINGER 26R LOCATED BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK FRAME BS 259.5 AND STRINGER 8R AT PASSENGER CABIN 2023-652122<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC600D; S/N: 220273012; DUE DATE: 17-DEC-23.;[02] REPAIRED FRAME BS 259.5 AND BTW STR 8R TO STR 12R AT PASSENGER CABIN IAW EA 23-153-03257 AND 23-153-03257-WIP1. SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] REPAIRED FRAME BS 259.5 AND BTW STR 8R TO STR 12R AT PASSENGER CABIN IAW EA 23-153-03257 AND 23-153-03257-WIP1. RII. SEE INDIVIDUAL SIGN-OFFS BELOW.

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CORROSION WEB LOCATED BTW BS727A TO BS727B AND RBL3.0 WL148.5 AT AFT CARGO COMPARTMENT 2023-652092<[01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 221859911; DUE DATE: 07-NOV-23.;[02] EVALUATED REWORK AREA WEB LOCATED BTW BS727A TO BS727B AND RBL3.0 WL148.5 AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2; ITEM 4.C(B)(1); FIGURE 103 DETAIL E.. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] EVALUATED REWORK AREA WEB LOCATED BTW BS727A TO BS727B AND RBL3.0 WL148.5 AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2; ITEM 4.C(B)(1); FIGURE 103 DETAIL E.. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: STIFFENER — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED BS947.5 AND STR26L AT AFT CARGO COMPARTMENT 2023-652097<[01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS947.5 AND STR26L AT AFT CARGO IWA B737-700 #DWG:186A8103 SHEET: 9 REV:- AND SRM 51-40-02 AND 51-10-02 Ï¿½TEM 9.<BR>SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS947.5 AND STR26L AT AFT CARGO IWA B737-700 #DWG:149A8103 SHEET: 9 REV:- AND SRM 51-40-02 AND 51-10-02 Ï¿½TEM 9.<BR>SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS947.5 AND STR26L AT AFT CARGO IWA B737-700 #DWG:149A8103 SHEET: 9 REV:- AND SRM 51-40-02 AND 51-10-02 Ï¿½TEM 9.<BR>SEE INDIVIDUAL SIGNOFF BELOW

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK STRINGER 25R BS 540 FWD CARGO COMPARTMENT 2023-652106<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[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 25R BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[05] CORRECTED STEP 4<BR>REPAIRED STRINGER 25R 500C BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[06] REPAIRED STRINGER 25R BETWEEN STA 500C AND <BR> BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.<BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK STRINGER 26L BS 540 FWD CARGO COMPARTMENT 2023-652104<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[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 AND SRM 51-10-02 ITEM 9 . <BR>SEE INDIVIDUAL SIGN OFF BELOW;[05] CORRECTED STEP 4<BR>REPAIRED STRINGER 26L BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[06] CORRECTED STEP 4<BR>REPAIRED STRINGER 26L BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. RII SEE INDIVIDUAL SIGN OFF BELOW.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK STRINGER 23L BS 540 FWD CARGO COMPARTMENT 2023-652103<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[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 LOCATED BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED STRINGER 23L LOCATED BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK STRINGER 23R BS 540 FWD CARGO COMPARTMENT 2023-652105<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[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 23R LOCATED BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[05] CERTIFIED RII MAJOR REPAIR PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 7 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT 2023-652085<[01] REPLACED ANGLE LOCATED BS907 PLUS 7 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 17 REV D. PART USED: 147A7221Y32ATSMRO P.O: 2023 248205; SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED BS907 PLUS 7 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 17 REV D. PART USED: 147A7221Y32ATSMRO P.O: 2023 248205; SEE INDIVIDUAL SIGN OFF BELOW.

Part: CARGO TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ON TRACK LBL 17.24 LOCATED BS727E AT AFT CARGO COMPARTMENT 2023-652090<[01] REPAIRED CARGO TRACK LOCATED AT LBL 17.24 BETWEEN STA 727D TO STA 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPAIRED CARGO TRACK LOCATED AT LBL 17.24 BETWEEN STA 727D TO STA 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4. RII;SEE INDIVIDUAL SIGN OFF BELOW.

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK FRAME ON BS 907 BTW STR25R AND STR26R AFT CARGO COMPARTMENT 2023-652087<[01] REPLACED FRAME LOC. ON BS 907 BTW STR25R AND STR25L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A1007 SHEET 55 REV.-; 147A1007 SHEET 42 REV.D; 147A7500 SHEET 19 REV.-; 147A0002 SHEET 85 REV.-; 147A7500 SHEET 1 REV.B. SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED FRAME LOC. ON BS 907 BTW STR24R AND STR24L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A1007 SHEET 55 REV.-; 147A1007 SHEET 42 REV.D; 147A7500 SHEET 19 REV.-; 147A0002 SHEET 85 REV.-; 147A7500 SHEET 1 REV.B. SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED STEP 2 COMPLETED<BR>RII

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 11 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT 2023-652086<[01] REPLACED ANGLE LOCATED BS907 PLUS 11 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 17 REV D. PART USED: 147A7221Y32ATSMRO P.O: 2023 248209; SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED BS907 PLUS 11 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 17 REV D. PART USED: 147A7221Y32ATSMRO P.O: 2023 248209; SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK BS 294.5 ANGLE - SUPPORT AND STR13L FWD GALLEY AND LAV 2023-652068<[01] REPLACED ANGLE-SUPPORT LOC BS 294.5 STR 13L FWD GALLEY IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1311 REV C SHEET 1 <BR>SEE INDIVIDUAL SIGNS OFF BELOW;[02] CERTIFIED AS RII <BR>REPLACED ANGLE-SUPPORT LOC BS 294.5 STR 13L FWD GALLEY IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1311 REV C SHEET 1 <BR>SEE INDIVIDUAL SIGNS OFF BELOW

Part: FRAME — CRACKED (ZN 200 FUS TOP) · airframe 64,738 hrs · 38,739 cycles

CRACK FRAME LOCATED BS 727D BTW STRINGER 8L TO STRINGER 9L AT PASSENGER CABIN 2023-652063<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23.;[02] PERFORMED VISUAL INSPECTION ON AREA AND FOUND ONLY DIRTY AND PERFORMED CLEAN IAW SOPM 20-30-03 HFEC WAS DONE AND NOT FOUND CRACK INDICATION IAW B737-700 SRM 51-10-02.;[03] CORRECTED STEP 2: PERFORMED VISUAL INSPECTION ON AREA AND FOUND ONLY DIRTY AND PERFORMED CLEAN IAW SOPM 20-30-03 HFEC WAS DONE AND NOT FOUND CRACK INDICATION IAW B737-700 SRM 51-10-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[04] TASK CARD COMPLETE.

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE - SUPPORT LOCATED BS867 AND BTW STR26L / STR27L AFT CARGO COMPARTMENT 2023-652088<[01] REPLACED ANGLE - SUPPORT LOCATED BS867 AND BTW STR26L / STR27L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 <BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK WEB INTERCOSTAL LOCATED BTW 294.5 TO BS303.9 AND STR15L AT PASSENGER CABIN 2023-652065<[01] REPAIRED WEB INTERCOSTAL LOCATED BTW 294.5 TO BS303.9 AND STR15L AT PASSENGER CABIN IAW EA 23-153-03218-WIP1.;[02] REPAIRED WEB INTERCOSTAL LOCATED BTW 294.5 TO BS303.9 AND STR15L AT PASSENGER CABIN IAW EA 23-153-03218-WIP1.RII CERTIFIED

Part: CARGO TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK TRACK RBBL 13.84 LOCATED BS727E AFT CARGO COMPARTMENT 2023-652089<[01] REPAIRED CARGO TRACK RBBL 13.84 LOCATED BS727E AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4. SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED ACTION 1<BR> REPAIRED CARGO TRACK RBBL 13.84 LOCATED BS727D TO BS 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4. SEE INDIVIDUAL SIGN OFF BELOW;[03] JOB COMPLETED AND CERTIFIED RII.

Part: DOOR — CRACKED (ZN 800 DOOR) · airframe 64,738 hrs · 38,739 cycles

CRACK INNER CHORD LOCATED BS303.9 AT LEVEL STR 17L AT PASSENGER CABIN 2023-652071<[01] REPLACED NEW INNER CHORD LOCATED BS303.9 AT LEVEL STR 17L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 7 REV - SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1.<BR>REPLACED INNER CHORD LOCATED BS303.9 AT LEVEL STR 17L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 7 REV - SEE INDIVIDUAL SIGN-OFF BELOW;[03] CORRECTED STEP 1.<BR>REPLACED INNER CHORD LOCATED BS303.9 AT LEVEL STR 17L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 7 REV - RII SEE INDIVIDUAL SIGN-OFF BELOW

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK TIE CLIP LOCATED BS 277 STRINGER 10R CENTER SECTION 2023-652066<[01] REPLACED NEW TIE CLIP LOCATED BS 277 STRINGER 10R CENTER SECTION I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9 AND #DWG: 141A1110 SHEET: 17 REV:-.<BR>SEE INDIVIDUAL SIGNOFF BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFF BELOW.

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK STUB FRAME ON BS 294.5 UPPER POSITION RH SIDE AT FWD GALLEY AND LAV 2023-652064 CRACK STUB FRAME RH SIDE ON BS 294.5 UPPER POSITION FWD GALLEY AND LAV<[01] REPLACED STUB FRAME LOC BS 294.5 UPPER POSITION RH SIDE AT FWD GALLEY AND LAV. IAW B737-700 51-40-02 AND DWG 141A8370 SHEET 9 REV D .SEE INDIVIDUAL SING OFF BELOW;[02] REPLACED STUB FRAME LOC BS 294.5 UPPER POSITION RH SIDE AT FWD GALLEY AND LAV. IAW B737-700 51-40-02 AND DWG 141A8370 SHEET 9 REV D .SEE INDIVIDUAL SING OFF BELOW;[03] CORRECTED STEP 2 (MISSING RII)<BR>REPLACED STUB FRAME LOC BS 294.5 UPPER POSITION RH SIDE AT FWD GALLEY AND LAV. IAW B737-700 51-40-02 AND DWG 141A8370 SHEET 9 REV D .SEE INDIVIDUAL SING OFF BELOW<BR>RII

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,738 hrs · 38,739 cycles

INOP LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) 2023-651813<[01] REPLACED LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) IAW: B737-700 AMM 33-51-06-960-805 TEST IS OK;[02] REPLACED LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) IAW: B737-700 AMM 33-51-06-960-805 TEST IS OK

Part: BEAR STRAP — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ON BEAR STRAP LOCATED BTW BS291.5 TO 294.5 STR8R AND STR9R PASSENGER CABIN 2023-652067<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] REPAIRED BY 737-700 SRM 53-10-01-2R-6 AND EA M-21-153-03542. SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] REPAIRED BY 737-700 SRM 53-10-01-2R-6 AND EA M-21-153-03542. SEE INDIVIDUAL SIGN-OFFS BELOW.<BR>AS RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE LOCATED BTW BS291.5 TO BS294.5 AT LEVEL STR17R AT PASSENGER CABIN 2023-652072<[01] REPLACED ANGLE LOCATED BTW BS291.5 TO BS294.5 AT LEVEL STR17R AT PASSENGER CABIN I.A.W B737-700 #DWG: 141A8310 SHEET: 25 REV:- AND SRM 51-10-02 AND 51-10-02 ITEM 9.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FITTING — DETERIORATED (ZN 800 DOOR) · airframe 64,738 hrs · 38,739 cycles

DETERIORATED ENTRY DOOR COVER PLASTIC GIRTBAR FITTING AT FWD GALLEY AREA (2 EA) 2023-652058<[01] REPLACED ENTRY DOOR COVER PLASTIC GIRTBAR FITTING AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 25-66-02-400-801 STEP 3.A THRU 3.D ITEM (1) (H);[02] CERTIFIED WORK PERFORMED.

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CORROSION WEB LOCATED BTW BS727A TO BS727B AND LBL3.0 WL148.5 AT AFT CARGO COMPARTMENT 2023-652091<[01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 221859911; DUE DATE: 07-NOV-23.;[02] EVALUATED REWORK AREA WEB LOCATED BTW BS727A TO BS727B AND LBL3.0 WL148.5 AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2; ITEM 4.C(B)(1); FIGURE 103 DETAIL E.. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] EVALUATED REWORK AREA WEB LOCATED BTW BS727A TO BS727B AND LBL3.0 WL148.5 AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2; ITEM 4.C(B)(1); FIGURE 103 DETAIL E.. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FITTING — WORN (ZN 800 DOOR) · airframe 64,738 hrs · 38,739 cycles

WEAR ON ENTRY DOOR BASE GIRT BART FITTING AT FWD GALLEY AREA (2 EA) 2023-652057<[01] REPLACED ON ENTRY DOOR BASE GIRT BART FITTING AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 25-66-02-400-801 STEP 3A THRU 3.D ITEM (1) (G).;[02] CERTIFIED WORK PERFORMED.

Part: ACCESS PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

DELAMINATED ACCESS PANEL 193B WING TO BODY FAIRING EXTERNAL SKIN AFT LEFT CORNER AT LOWER FUSELAGE 2023-652045<[01] TOOL USED CALIPER P/N: 700-113-10; S/N 0033174; DUE DATE: 12-MAR-24.;[02] HOT BONDER P/N HCS9200B-AV; S/N 18196127; DUE DATE: 22-JAN-24.;[03] TOOL USED SCALE P/N 91847 S/N AE-409316 DUE DATE: 12-JUN-24.;[04] TOOL USED HOT BONDER P/N HCS9200B-AV; S/N 18196127; DUE DATE: 22-JAN-24.;[05] TOOL USED: UT EQUIPMENT P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 24-JAN-24;[06] REPAIRED ACCESS PANEL 193B WING TO BODY FAIRING EXTERNAL SKIN AFT LEFT CORNER AT LOWER FUSELAGE I.A.W. B737-700 SRM 53-40-70-2R-1 REPAIR 1 PARAGRAPH 4.B(2) TABLE 202. AND B737-700 SRM 51-70-04-2R-6 REPAIR 6 SEE INDIVIDUAL SIGN OFFS BELOW.;[07] JOB COMPLETED.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE LOCATED BS 695 RBL 24.75 AT CENTER WING BOX 2023-652025<[01] TOOL 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.;[02] REPLACED ANGLE LOCATED BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-05; SRM 51-10-02 IITEM 9 AND DWG 273A9110 REV A SHEET 6 <BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[03] REPLACED ANGLE LOCATED BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-05; SRM 51-10-02 IITEM 9 AND DWG 273A9110 REV A SHEET 6 <BR>SEE INDIVIDUAL SIGNSOFF BELOW.

Part: BEAM — CORRODED (ZN 200 FUS TOP) · airframe 64,738 hrs · 38,739 cycles

CORROSION CREASE BEAM LOCATED BS 639 LBL 64 WL 208.1 AT PASSENGER CABIN 2023-652027<[01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45 MG; S/N: 232017609; DUE DATE: 22-SEP-24.;[02] REPLACED CREASE BEAM SECTION LOC BTW BS616 + 12? TO BS 639 +9 ? LBL 64 WL 208.1 AT PASSENGER CABIN I.A.W. B737-700 DWG 144A5901 SHEET 36 REV '-' AND B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] REJECT STEP 8. TOOL MARK ON CREASE BEAM WEB RIVETS LOC BTW BS 639 LBL 64 WL 208.1 AT PASSENGER CABIN (3 EA. FAULT RAISED TTG8Q00PDDYL.;[04] CORRECTED STEP 2<BR>REPLACED CREASE BEAM SECTION LOC BTW BS616 + 12? TO BS 639 +9 ? LBL 64 WL 208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 144A5901 SHEET 36 REV '-'. SEE INDIVIDUAL SIGN-OFFS BELOW.;[05] TASK CARD COMPLETED <BR>REPLACED CREASE BEAM SECTION LOC BTW BS616 + 12? TO BS 639 +9 ? LBL 64 WL 208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 144A5901 SHEET 36 REV '-'. SEE INDIVIDUAL SIGN-OFFS BELOW.<BR>RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE LOCATED BS 695 BL0 LH SIDE AT CENTER WING BOX 2023-652024<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N: 38615K71; S/N: AE-40585; DUE DATE: 22-DEC-23.;[02] REPLACED ANGLE LOCATED BS 695 BLO LH SIDE AT CENTER<BR>WING BOX IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND<BR>DWG DWG 273A9110 SHEFT 6. REV. A;[03] CORRECTED STEP 2<BR>REPLACED ANGLE LOCATED BS 695 BL0 LH SIDE AT CENTER<BR>WING BOX IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND<BR>DWG DWG 273A9110 SHEFT 6. REV. A<BR>SEE INDIVIDUAL SIGNSOFF BELOW;[04] REPLACED ANGLE LOCATED BS 695 BL0 LH SIDE AT CENTER<BR>WING BOX IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND<BR>DWG DWG 273A9110 SHEFT 6. REV. A<BR>SEE INDIVIDUAL SIGNSOFF BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE LOCATED BS 695 LBL 24.75 AT CENTER WING BOX 2023-652022<[01] TOOL 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.;[02] REPLACED ANGLE LOCATED BS 695 LBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 273A9110 SHEET 6; REV. A<BR>SEE INDIVIDUAL SIGNSOFF BELOW;[03] REPLACED ANGLE LOCATED BS 695 LBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 273A9110 SHEET 6; REV. A<BR>SEE INDIVIDUAL SIGNSOFF BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ON ANGLE LOCATED BS727B AREA CEILING PANEL LH SIDE AFT CARGO COMPARTMENT 2023-652023<[01] REPLACED ANGLE LOCATED LOCATED AT CEILING UPPER POSITION LH SIDE BETWEEN BS727A TO BS747 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 149A9490 REV- .SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED ANGLE LOCATED LOCATED AT CEILING UPPER POSITION LH SIDE BETWEEN BS727A TO BS747 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 149A9490 REV- .FOR OVERHEAT SENSING ELEMENT INSTALATION AND OPERATIONAL SEE TTG8Q00PLF80.SEE INDIVIDUAL SIGNOFF BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE - CLIP LOCATED BS400 AND STR26R FWD CARGO COMPARTMENT 2023-652013<[01] REPLACED ANGLE - CLIP AND LOCATED BS400 AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 REV: B SHEET 2. SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED ANGLE - CLIP AND LOCATED BS400 AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 REV: B SHEET 2. <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE - CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT 2023-652014<[01] REPLACED ANGLE - CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 143A7505 SHEET 9 REV. A;[02] CORRECTED STEP 1<BR>REPLACED ANGLE - CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 143A7505 SHEET 9 REV. A SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED STEP 2 COMPLETED

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE - CLIP LOCATED BS500C AND STR26L FWD CARGO COMPARTMENT 2023-652016<[01] REPLACED ANGLE - CLIP LOCATED BS500C AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 207 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED STEP 1 COMPLETED

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE - CLIP LOCATED BS500A AND STR26L FWD CARGO COMPARTMENT 2023-652015<[01] REPLACED ANGLE - CLIP LOCATED BS500A AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 207 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED STEP 1 COMPLETED

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2023-651997<[01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG: 143A9481 SHEET 2 REV A;[02] CORRECTED STEP 1<BR>REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG: 143A9481 SHEET 2 REV A. SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 2<BR>REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG: 143A7902 SHEET 174 REV -SEE INDIVIDUAL SIGN OFF BELOW;[04] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG: 143A7902 SHEET 174 REV -SEE INDIVIDUAL SIGN OFF BELOW<BR>AS RII

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-651921<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:B22394220;DUE DATE:22-AUG-24.;[02] TOOL USED RADIOMETER PN. XRP-3000; SN. 1753759; DUE DATE. 12-APR-24;[03] REPAIRED THE AFT CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. STEPS ( 2 ) TO ( 7 ) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[04] TASK COMPLETED.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CRACK ANGLE LOCATED BS663.75 AND RBL6.14 WL 173.5 AT CENTER WING BOX 2023-651802<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24.;[02] REPLACED REPAIR ANGLE LOCATED BS663.75 AND RBL6.14 WL 173.5 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #111A1000 SHEET 139 REV - .SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED STEP 2 COMPLETED <BR>RII

Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 64,738 hrs · 38,739 cycles

CORROSION FLOOR STRAP LOC BS 787 PLUS 6 INCHES AND BTW STR 25R TO STR 26R AT AFT CARGO COMPARTMENT 2023-651778<[01] REPLACED STRAP LOC BS 787 PLUS 6 INCHES AND BTW STR 25R TO STR 26R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9.;[02] COMPLETE TASK CERTIFIED

Part: SKIN — CRACKED (RT SLAT) · airframe 64,738 hrs · 38,739 cycles

CRACK SLAT 8 LOWER SKIN LOCATED SLAT STATION 451.97 AT RT WING 2023-651791<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138003; DUE DATE: 27-MAR-24;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 12 MAR 24.;[03] PERFORMED PERMANENT REPAIR ON SLAT 8 LOWER SKIN LOCATED SLAT STATION 451.97 AT RT WING IAW B737-700 SRM 57-42-01-2R-8. REPAIR 8 AND SRM 51-40-02.SEE INDIVIDUAL SIGN OFF BELLOW.;[04] PERFORMED PERMANENT REPAIR ON SLAT 8 LOWER SKIN LOCATED SLAT STATION 451.97 AT RT WING IAW B737-700 SRM 57-42-01-2R-8. REPAIR 8 AND SRM 51-40-02.SEE INDIVIDUAL SIGN OFF BELLOW. COMPLETE TASK CERTIFIED

Part: GIRT BAR — LOOSE (ZN 200 FUS TOP) · airframe 64,498 hrs · 38,587 cycles

R1 DOOR SLIDE BRACKET LOOSE<[01] RESECURED R1 DOOR GIRT BAR BRACKET; OPERATES NORMAL PER AMM 25-66-01.

Part: FASTENER — INOPERATIVE (ZN 800 DOOR) · airframe 64,037 hrs · 38,280 cycles

FWD SERVICE DOOR GIRT BAR CLIP INOP.<[01] REPLACED DAMAGED FASTENER PER SRM 51-40-02.

Part: CONTACT — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,813 hrs · 38,114 cycles

AFT ENTRY DOOR (L2) EXTERIOR EMERGENCY LIGHT INOP<[01] DISCONNECTED WIRING FROM LIGHT ASSY ON AFT ENTRY DOOR EXTERIOR REF AMM 33-51-04.;[02] REPLACED L2 DOOR SLIDE EMERGENCY LIGHT SOCKET AND CONTACT PER AMM SIP. OPS CHECK GOOD AT THIS TIME.

Part: SOCKET — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,813 hrs · 38,114 cycles

AFT ENTRY DOOR (L2) EXTERIOR EMERGENCY LIGHT INOP<[01] DISCONNECTED WIRING FROM LIGHT ASSY ON AFT ENTRY DOOR EXTERIOR REF AMM 33-51-04.;[02] REPLACED L2 DOOR SLIDE EMERGENCY LIGHT SOCKET AND CONTACT PER AMM SIP. OPS CHECK GOOD AT THIS TIME.

Part: MEGAPHONE — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 61,982 hrs · 36,900 cycles

FORWARD MEGAPHONE INOP. / [01] R/R BATTERIES IAW AMM 25-64-00. MEGAPHONE OPS NORMAL. A/C OK FOR SERVICE.

Part: NONE — CRACKED (COCKPIT) · airframe 61,756 hrs · 36,750 cycles

#1 WINDSHIELD (FWD CAPT.) CRACKED / [01] R&R'D L1 WINDOW; C/W OP'S CKS; LEAK CK; NO DEFECTS NOTED IAW MM 56-11-11 REF LG #2048731 FOR HGS UPGRADE

Part: LENS — LOOSE (CABIN) · airframe 59,966 hrs · 35,582 cycles

ROW 12 R EXIT LT LENS FELL OFF / [01] RE INSTALLED LENS PER AMM 33-51-01

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. ; / [01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF. B737 AMM 33-51-04-960-801. TEST OK; [02] VERIFIED STEP 1.

Part: CONNECTOR — LOOSE (CABIN) · airframe 59,271 hrs · 35,159 cycles

L2 DOOR EMERGENCY EXIT SIGN LIGHT INOP. ; / [01] FOUND CONNECTORS LOOSED AND RECONNECTED AT L2 DOOR EMERGENCY EXIT SIGN LIGHT ; OPERATIONAL CHECK FOUND NORMAL AMM 33-51-01-960-802.; [02] C/W

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 59,271 hrs · 35,159 cycles

PANEL 242VF DELAMINATED ; / [01] CLEANED AND PREPARED FOR REPAIR FIBERGLASS AT ;FLOOR PANEL 242VF AS PER B737-700 SRM 53-00-50-2R-7; [02] VERIFIED CLEANING AND OK TO INSTALL REPAIR.; [03] REPAIRED DELAMINATION ; AT FLOOR PANEL 242VF AS PER B737-700 SRM 53-00-50-2R-7; [04] VERIFIED COMPLETED; [05] CLEANED; PREPARED FOR REPAIR THE FIBERGLASS; REPAIRED AT FLOOR PANEL 242VF AS PER B737-700 SRM 53-00-50-2R-7 MATERIAL USED PO;1711677PO;1150387 PO;1713932

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

CRACKED INTERCOSTAL AT STR 25R AND BETWEEN BS927 AND 947.5. AFT CARGO. ; CRACKED INTERCOSTAL AT STR 25R AND ETWEEN BS927 AND 947.5. AFT CARGO. / [01] REMOVED CRACKED INTERCOSTAL AT AFT CARGO STR 25-R BETWEEN STA 927 TO STA 947.5 IAW B 737-7 SRM 51-40-02-0G-0; [02] VERIFIED REMOVAL OF INTERCOSTAL.; [03] INSTALLED NEW INTERCOSTAL AT AFT CARGO R/H FROM STA 927 TO STA 947.5 STR 25R AS PER B737-700 SRM 51-40-02-0G-0; [04] REMOVED AND REPLACED AFT CARGO INTERCOSTAL FROM STA 927 TO STA 947.5 STR 25R AS PER B737-700 SRM 51-40-02-0G-0; [05] VERIFIED STEPS 3 AND 4...; [06] LATE ENTRY RII<BR>RII OK TO INSTALL.<BR>RII VERIFIED INSTALLATION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

CORROSION SPOTS ON AFT CARGO AFT LKHEAD LOWER ANGLE PNL SPPORT. CORROSION IS OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AFT CARGO AFT BULK HEAD SUPPORT ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW AFT CARGO AFT BULKHEAD LOWER ANGLE IAW SRM 51-40-05-0G-0. INSTALLED NEW AFT CARGO AFT BULKHEAD LOWER ANGLE IAW SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

CORROSION AT FWD CABIN WET AREA FLOOR SUPPORT BEAM = @ LBL14 AND STA 312 ; / [01] REMOVED CORROSION AT MAIN CABIN FWD WET AREA STA 312 & LBL 14 AS PER SRM 51-10-02-0G-0.; [02] PERFORMED UT THICKNESS ON REWORKED AREA IAW NDTM PART 4; 51-00-00 PROCEDURE 3. MINIMUM FOUND :0.067'.<BR>[27MG ; B/C 172139 ; CALIB.DUE-04/22]; [03] CHECK LIMITS ORIGINAL MATERIAL 0.125' MATERIAL LOST 0.058' MATERIAL REMAINING 0.067' FOUND OUT OF LIMITS AS PER SRM 53-10-51-1A-1 FIGURE 105 DETAIL B.; [04] LATE ENTRY INSTALLED PROTECTION OF EWIS AT MAIN CABIN FROM STA 294.5 TO 328 BETWEEN LBL 40 AND RBL 20 AS PER AMM 20-60-07-913-801.; [05] VERIFIED STEP 3; 4; [06] LATE ENTRY VERIFIED STEP 1; [07] VERIFIED ALL WORK ACCOMPLISHED ON REPLACEME

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

CORROSION ON AFT CABIN WET AREA FLOORBEAM UPPER FLANGE FASTENER HOLE, LBL43 BS 986.5 REMOVED CORROSION FROM AFT CABIN WET AREA FLOOR SUPPORT BEAM UPPER FLANGE FASTENERS HOLE IAW SRM 51-10-02-0G-0. PERFORMED SHOT PEENED PROCEDURE ALONG THE CUT EDGES OF THE REPAIR AREA PER SOPM 20-10-03. INSTALLED FASTENERS TEE ANGLE IAW SRM 53-70-51-2R-4, REPAIR 4,

Part: WEB — CORRODED (AFT CABIN) · airframe 59,271 hrs · 35,159 cycles

CORROSION AT AFT CABIN WET AREA GALLEY FLOOR SUPPORT WEB STA 1016 LBL 10. OUT OF LIMITS IAW SRM 53-70-51-1A-1. REMOVED AFT CABIN WET AREA GALLEY FLOOR SUPPORT WEB IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW AFT WET AREA FLOOR SUPPORT WEB IAW SRM=51-40-05-0G-0. PARTIALLY INSTALLED SHEAR WEB IAW SRM=51-40-05-0G-0. INSTALLED AFT CABIN WET AREA GALLEY FLOOR SUPPORT WEB IAW SRM 51-40-02-0G-0 AND DWG 147A5600 SHEET 32 REV B.

Part: DOOR SILL — CORRODED (R2 DOOR AREA) · airframe 59,271 hrs · 35,159 cycles

CORROSION. ** AFT CABIN R-2 DOOR FLOOR ENTRY LOWER SILL INNER CHORD FROM STA 947.5 TO STA 986.5 MKD ; / [01] REMOVED CORROSION AFT R-2 DOOR FLOOR ENTRY LOWER SILL CHORD FROM STA 947.5 TO STA 986.FOUND OUT LIMITS AREA [EXFOLIATED ] IAW SRM 51-10-02-0G-0. [20] ACCOMPLISHED REPLACED RT INNER CHORD AND INSTALLED RT AFT WEB REF B737-7 SRM 51-40-02-0G-0 AND DWG #147A8501; [21] REMOVED EWISN PROTECTION AT RT REPAIR AREAS REF 737-7 AMM 20-60-07-913-801; [22] CORRECTION STEP. 21 REMOVED EWIS; [23] CHANGED FROM MAJOR TO MINOR REPAIR TYPE; [24] VERIFIED R2 DOOR FLOOR ENTRY LOWER SILL INNER CHORD INSTALLATION & EWIS PROTECTION REMOVAL; [25] C/W; [26] VERIFIED REPLACED RT INNER CHORD STA 947 T0 STA 1007.<BR>VERIFIED INSTALLED RT AFT WEB FROM STA 986.5 TO STA 1016 BETWEEN RBL 45 TO RBL 60.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: CORROSION ** AT FWD WET AREA FLOOR SUPPORT ANGLE LBL12 BETWEEN STA 291.5 AND 312 ; / [01] PARTIALLY REMOVED FLOOR SUPPORT AT FWD CABIN WET AREA LBL 12 BETWEEN STA 294 AND STA 312 PER BOEING 737-700 SRM 51-40-02-0G-0.; [02] COMPLETED REMOVAL OF FLOOR SUPPORT ANGLE LBL 12 BETWEEN STA 291.5 AND 312 AS PER SRM 51-40-02-0G-0.; [03] LOCATED AND DRILLED FLOOR SUPPORT ANGLE REF B-737-700 SRM 51-40-05-0G-0; [04] VERIFIED REMOVAL OF FLOOR SUPPORT AND LOCATION AND DRILL OF NEW ONE.<BR>OK TO INSTALL; [05] INSTALLED FLOOR SUPPORT AT FWD WET ARE STA 291.5 TO STA 312 LBL 12 REFB-737-700-SRM 51-40-02; LATE ENTRY TREATED & PRIMER REF 51-20-01-0G-0; [06] VERIFIED INSTALLATION; [07] PARTS VERIFICATION; [08] LATE ENTRY TREATED & PRIMER VERIFIED

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: FWD CABIN WET AREA INTERCOSTAL SUPPORT CRACKED @ LBL45 BETWEEN STA 312 AND 328 MKD ; / [01] REMOVED DAMAGED INTERCOSTAL IN REFERENCE B-737 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED HOLES IN NEW INTERCOSTAL AT STA 312-328 LBL 45; IN REFERENCE B-737 SRM 51-40-02-0G-0; [03] VERIFIED NEW PART DRILL.<BR>OK TO INSTALL; [04] STAR INSTALLING HI LOCKS IN REFERENCE B-737 SRM 51-40-02-0G-0.; [05] INSTALLED NEW INTERCOSTAL AT FWD. WET AREA LBL 45 BETWEEN STA 312 AND STA 328 AS PER B737-700 SRM 51-40-02-0G-0 / 51-40-05-0G-0 AND DRWG # 141A5400.; [06] VERIFIED MEASUREMENTS; [07] VERIFIED INSTALLATION

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: FWD CABIN WET AREA FLOOR INTERCOSTAL CRACKED @ LBL 45 BETWEEN STA 328 AND 344 ; / [01] REMOVED INTERCOSTAL DAMAGED IN REFERENCE. B-737 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED HOLES IN THE NEW INTERCOSTAL IN REFERENCE B-737 SRM 51-40-02-0G-0 AT STA 328-344 LBL 45.; [03] VERIFIED NEW PART DRILL.<BR>OK TO INSTALL; [04] STAR INSTALLING HI LOCK IN REFERENCE. B737 SRM 51-40-02-0G-0.; [05] INSTALLED NEW INTERCOSTAL AT FWD WET AREA BETWEEN STA 328 AND STA 344 LBL 45 AS PER B737-700 SRM 51-40-02-0G-0 / 51-40-05-0G-0 AND DRWG # 141A5400 .; [06] VERIFIED PARTS AND MEASUREMENTS; [07] VERIFIED INSTALLATION

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: AFT CABIN WET AREA FLOOR PANEL # 242DF TOP SURFACE LAYERS DELAMINATED AND SEVERAL INERTS MISSING ; / [01] REMOVED CABIN FLOOR PANEL #242DF AS PER BOEING 737-700 AMM 53-21-00-000-801.; [02] OK TO INSTALL NEW FLOOR PANEL 242DF; [03] INSTALLED NEW PASSENGER CABIN FLOOR PANEL #242DF AS PER BOEING 737-700 AMM 53-21-00-400-801; [04] MEASURES; [05] VERIFIED FLOOR PANEL INSTALLATION 242DF

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: FWD CABIN FLOOR WET AREA INTERCOSTAL CRACKED AT BL-0 BETWEEN STA 270 AND 294.5 MKD DOT ; / [01] REMOVED INTERCOSTAL AT FWD CABIN WET AREA BL-0 BETWEEN STA 270 & 294.5 AS PER SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW INTERCOSTAL AS PER SRM 51-40-05-0G-0.; [03] VERIFIED STEPS 1; 2.<BR><BR>OK TO INSTALL NEW INTERCOSTAL; [04] INSTALLED NEW INTERCOSTAL AT MAIN CABIN FORWARD WET AREA BL-0 BETWEEN STA 270 AND 294.5 AS PER SRM 51-40-02-0G-0 AND DWG 141A5400.; [05] VERIFIED; [06] PART CERTIFICATION.; [07] C/W

Part: FLANGE — CRACKED · airframe 59,271 hrs · 35,159 cycles

FWD LT FUSELAGE FRAME SMALL CRACK AT FLANGE ABOVE L1 DOOR CUTOUT BS 312. REMOVED CRACK IAW SRM 53-10-07-2R-1 REPAIR 1. PERFORMED HFEC INSP. ALONG EDGE OF CUTOUT IAW NDT PART 6; 51-00-00, PROCEDURE 23. NO CRACKS NOTED. LOCATED & DRILLED NEW HOLES ON LAY OUT REPAIR AND FABRICATED NEW PART. HEAT TREATED ANGLE IAW BAC 5602 PAGES 22- 28. TRIM OUT REPAIR ANGLE IAW SRM 53-10-07-2R-1 REPAIR 1. LOCATED & DRILLED REPAIR PART IAW SRM 53-10-07-2R-1. PERFORMED ROTO INSP ON EXISTING HOLES IAW NDT P6 51-00-00 PROC.16; NO CRACKS. PERFORMED PENETRANT INSP ON ANGLE IAW SOPM 20-20-02, NO CRACKS NOTED. TREATED & PRIMED PART IAW AMM 51-21-41 -370-801 & AMM 5121-72-370-80. INSTALLED REPAIR IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ FWD FASTENER HOLE RBL 33 BETWEEN STA 312 AND 328 ; / [01] REMOVED FLOOR SUPPORT INTERCOSTAL RBL 33 BETWEEN STA 312 AND 328 INREF. B-737 700 SRM 51-40-02-0G; [02] LOCATED AND DRILLED NEW INTERCOSTAL P/N 141A5410U12 AS PER SRM 51-40-05-0G-0.; [03] VERIFIED. STEPS 1 AND 2; [04] RII OK TO INSTALL NEW INTERCOSTAL; [05] REMOVED AND REPLACED INTERCOSTAL P/N 141A5410U12 AT MAIN CABIN RBL 33 BETWEEN STA 312 AND 328 AS PER SRM 51-40-02-0G-0 AND DWG 141A5400; [06] VERIFIED STEP # 5.

Part: SUPPORT BEAM — CORRODED · airframe 59,271 hrs · 35,159 cycles

CORROSION AFT CABIN WET AREA FLOOR SUPPORT BEAM UPPER FWD FLANGE FASTENERS HOLES RBL 23 TO RBL45 STA 986.5. REMOVED CORROSION AFT WET AREA FLOOR SUPPORT BEAM UPPER FLANGE HOLES. FOUND OUT LIMITS. REPAIR PARTS TRIM AND DRILLED HOLES. TREAT AND PRIMED CUTOUT FLANGE, REPAIR PARTS AND ALL DRILLED HOLES IAW SRM 51-20-01-0G-0. PERFORMED DETAIL VISUAL INSPECTIONS OF CUTOUT FLANGE, ADJACENT STRUCTURE AND INTERCOSTAL, NO OTHER DAMAGE FOUND. TRIMMED OUT MACHINED INTERCOSTALS IAW SRM 53-70-51-2R-4 REPAIR 4 STEP 4.E 9(3). PERFORMED HFEC INSP ON CUTOUTS IAW NDT P6 51-00-00 PROC.23, NO CRACKS. ACCOMPLISHED FLAP PEENING ON CUT EDGES OF INTERCOSTALS AND CORNER FITTINGS IAW SRM 53-70-51-2R-4, SOPM 20-10-03.

Part: NONE — CORRODED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: CORROSION. ** AT L- 2 DOOR LOWER FLOOR ENTRY CUTOUT SILL INNER CHORD FROM STA 947.5 TO STA 986.5 MKD ; / [01] REMOVED CORROSION AT L-2 DOOR LOWER ENTRY CUT OUT SILL INNER CHORD FROM STA 947.5 TO STA 986.5 .FOUND OUT LIMITS AREA [EXFOLIATED]IAW B737 SRM 51-10-02-0G-0.; [31] REMOVED AND REPLACED L-2 DOOR LOWER FLOOR ENTRY SILL INNER CHORD BETWEEN STA 893 TO STA 1007 LBL-60 REF B737-7 SRM 51-40-02-0G-0 AND DWG#147A8501; [32] VERIFIED REMOVED AND REPLACED L-2 DOOR LOWER FLOOR ENTRY SILL INNER CHORD BETWEEN STA 893 TO STA 1007 LBL-60 REF B737-7 SRM 51-40-02-0G-0 AND DWG#147A8501; [33] VERIFIED LATE ENTRY: INSTALLED AND REMOVED EWIS PROTECTION AT L-2 DOOR LOWER FLOOR ENTRY SILL INNER CHORD AREA REF B7370-7 AMM 20-60-07-913-801

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

FWD WET AREA FLOOR PANEL 221CF EDGES DELAMINATED MKD ; / [01] RECEIVED AND REPLACED PANEL 221CF AS PER AMM 53-21-00-300-801.; [02] VERIFIED REPLACEMENT. CLOSING WILL BE ACCOMPLISHED ON CARD TTG8Q006Q1SK

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: AFT CABIN FLOOR PANEL # 241ZF TOP LAYERS DELAMINATED MKD ; / [01] MEASUARES; [02] RECEIVED AND REPLACED FLOOR PANEL 241ZF AS PER B737-700 AMM 53-21-00-300-801.; [03] PANEL WILL BE INSTALLED ON TTG8Q006Q134

Part: SUPPORT WEB — ELONGATED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

AFT CABIN WET AREA L/H GALLEY FLOOR SUPPORT WEB 2EA FASTENER HOLES ELONGATED AND MISSING NUT PLATES LBL 45 BETWEEN BS 986.5 AND 1016. REMOVED AFT WET AREA L/H FLOOR WEB AT STA 986.5 BETWEEN LBL 45 AND STA 986.5 IAW B 737-7 SRM 51-40-02-0G-01 LOCATED AND DRILLED NEW AFT WET AREA LT FLOOR SUPPORT WEB AT STA 986.5 IAW SRM 51-40-05-0G-0-A00745. START TO INSTALL FASTENERS AT AFT CABIN WET AREA LT GALLEY FLOOR SUPPORT WEB IAW SRM -40-05-0G-0-A00745. COMPLETED INSTALLED GALLEY FLOOR SUPPORT WEB AT MAIN CABIN AFT WET AREA IAW SRM 51-40-05-0G-01, AND 51-40-0G-0-A00745.

Part: FITTING — CORRODED (L1 DOOR) · airframe 59,271 hrs · 35,159 cycles

CORROSION ** AT L- 1-DOOR FWD GIRT BAR FITTING MKD ; / [01] REMOVED AND REPLACED GIRT BAR FITTING AT L-1 DOOR FWD REF B-737-700 SRM 51-40-02; [02] VERIFIED INSTALLATION PER B-737-700 SRM 51-40-02-0G-0; [03] ADDED REFERENCE MANUALLY

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

AFT CABIN WET AREA FLOOR PANEL # 241ABF EDGE DELAMINATED AND SEVERAL DAMAGED INSERTS MKD ; / [01] REPAIRED DELAMINATED AREA AND REMOVED & REPLACED DAMAGED INSERTS AT FLOOR PANEL 241ABF. REF B737-700 SRM 53-00-50-2R-0; SRM 53-00-50-2R-9 PARAGRAPH 4 AND SRM 53-00-50-2R-0 PARAGRAPH 5 S.; [02] VERIFIED REPAIR

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: CORROSION ** FWD CABIN WT AREA FLOOR SUPPORT ANGLE LBL 12 BETWEEN STA 312 AND 328 MKD DOT ; / [01] REMOVED FLOOR SUPPORT ANGLE AT FWD CABIN LBL 12 BETWEEN STA 312 AND STA 328 PER BOEING 737-700 SRM 51-40-02-0G-0.; [02] FLOOR SUPPORT ANGLE FOUND OUT OF LIMITS AS PER B737-700 SRM 53-10-51-1A-1; [03] INSTALLED NEW FLOOR SUPPORT ANGLE AT LBL 12 BETWEEN STA 312 AND STA 328 AS PER B737-700 SRM 51-40-02-0G-0 / DRWG # 141A5400 .; [04] VERIFIED INSTALLED NEW FLOOR SUPPORT ANGLE AT LBL 12 BETWEEN STA 312 AND STA 328 <BR>LATE ENTRY: OK TO INSTALL

Part: NONE — CORRODED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: CORROSION ** AT FWD CABIN WET AREA R-1 DOOR ENTRY LOWER SILL INNER CHORD BETWEEN STA312 AND 328 ; / [01] REMOVED 2 FASTENERS FOR ACCESS AT R-1 DOOR LOWER SILL INNER CHORD AT STA 312+9' PER BOEING 737-700 SRM 51-40-02-0G-0;[15] COMPLETED INSTALLATION OF NEW INNER CORD P/N 654A0004-134 AS PER SRM 51-40-02-0G-0 AND DWG 141A8310.; [16] REMOVED EWIS PROTECTION MENTIONED ON STEP 6 .; [17] VERIFIED INSTALLATION OF NEW R1 DOOR LOWER SILL INNER CHORD BETWEEN STA 277- STA 360; [18] RE-INSTALLED 2 FASTENERS REMOVED ON STEP 1.; [19] CORRECTION ADDED TO STEP 18: PER BOEING 737-700 SRM 51-40-02-0G-0.<BR>VERIFIED INSTALLATION OF FASTENERS

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

FWD CABIN WET AREA FLOORBEAM, LBL23 AND BS 312. REMOVED CORROSION IAW SRM 51-10-92-0G-0. COMPLETED FABRICATION OF REPAIR PARTS FOR THE FLOORBEAM IAW SRM 53-10-51-2R-17, REPAIR 17. TREATED AND PRIMED ALL REPAIR PARTS IAW AMM=51-00-58-201 AND AMM 51-21-72-370-802, STEP 29. INSTALLED REPAIR IAW SRM 51-40-02-0G-0, AND SRM 53-10-51-2R-17, REPAIR 17.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: AFT WET AREA CABIN FLOOR PANEL 241ADF TOP LAYERS DELAMINATED ; / [01] CLEANED AND PREPARED FOR REPAIR FIBERGLASS AT CABIN FLOOR PANEL 241 ADF AS PER B737- 700 SRM 53-00-50-2R-2; [02] VERIFIED STEP #1; [03] (RII) OK TO APPLY FIBERGLASS REPAIR.; [04] REPAIRED FIBERGLASS AT CABIN FLOOR PANEL 241ADF AS PER B737-700 SRM 53-00-50-2R-2; [05] (RII) VERIFIED STEP #4; [06] CLEANED ; PREPARED FOR REPAIR THE FIBERGLASS ;REPAIRED AT FLOOR PANEL 241ADF AS PER B737-700 SRM 53-00-50-2R-2 MATERIAL USED PO;1711677 PO;1150387 PO; 1713932; [07] (RII) FINAL INSPECTION; FIBERGLASS FLOOR REPAIRED.

Part: PANEL — CORRODED · airframe 59,271 hrs · 35,159 cycles

ACCESS PANEL 192F AT FWD AND AFT ANTENNA INTERFACE WITH CORROSION ; / [01] CLEANED AREA IN REFERENCE B-737 SRM 51-10-02- 0G-0AND FOUND OUT LIMITS IN REFENCES B-737 SRM 53-40-70-1A-1; [02] PAINTED ON ACCESS PANEL 192AT AS REQUURED REF B-737 AMM 51-21-73-370-803; [03] VERIFIED PAINT; [04] CORRECTION: PANEL 192F; [05] REPLACED PANEL 192F IN REFERENCE. B737 SRM 51-42-02-0G-0; [06] CORRECTION<BR>PANEL 192F WAS REPLACED AND PAINTED; [07] PANEL 192F WILL BE INSTALLED ON CARD TTG8Q006Q1F3

Part: SCUFF PLATE — CORRODED (FUSELAGE) · airframe 59,271 hrs · 35,159 cycles

L-2 DOOR INNER WEB STRUCTURE UNDER SCUFF PLATE CORRODED. REMOVED CORROSION UNDER SCUFF PLATE. FOUND OUT OF LIMITS IAW SRM 51-010-02-0G-0. REMOVED STRUCTURE UNDER SCUFF PLATE IAW SRM 51-40-02-0G-0. WEB STRUCTURE UNDER SCUFF PLATE INSTALLED WEB, INSTALLED FASTENERS IAW SRM 51-40-02-0G-0. ] FINALIZED INSTALLATION OF L-2 DOOR INNER WEB UNDER SCUFF PLATE IAW SRM 51-40-02-0G-0.

Part: SUPPORT BRACKET — CRACKED (RH WING) · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: RIGHT WING REAR SPAR UPPER PANEL SUPPORT BRACKET CRACKED ABOVE # 2 FUEL PUMP ; / [01] REMOVED AND REPLACED BRACKET AT RIGHT WING REAR SPAR UPPER PANEL SUPPORT;ABOVE # 2 FUEL PUMP PER SRM 51-40-02-0G-0.; [02] ACCOMPLISHED PARTS TRANSACTION.; [03] C/W

Part: PANEL SUPPORT — CRACKED (LH WING TO BODY) · airframe 59,271 hrs · 35,159 cycles

L/H FWD WING TO BODY FAIRING AFT SUPPORT FOR PANEL 191AL CRACKED. ; / [01] REMOVED WTB FAIRING PANEL 195 AL FOR ACCESS AS PER B737-700 AMM 53-51-21-000-802.; [02] REMOVED FRAME SUPPORT ANGLE FOR WTB FAIRING PANEL 191AL AS PER B737-700 SRM 51-40-02-0G-0.; [03] LOCATED AND DRILLED NEW SUPPORT ANGLE FOR WTB FAIRING PANEL 191AL AS PER B737-700 SRM 51-40-05-0G-0.; [04] VERIFIED REMOVED WTB FAIRING PANEL 195 AL AND REMOVED FRAME SUPPORT ANGLE FOR WTB FAIRING PANEL 191AL; [05] VERIFIED LOCATION AND DRILL OF NEW SUPPORT ANGLE.<BR>OK TO INSTALL; [06] INSTALLED NEW SUPPORT ANGLE FOR WTB FAIRING PANEL 191AL AS PER B737-700 SRM 51-40-02-0G-0 / DRWG # 116A3110; [07] VERIFIED STEP # 6; [08] OK TO INSTALL 195AL; [09] CLOSED P

Part: PANEL — CORRODED · airframe 59,271 hrs · 35,159 cycles

DME#1 BASE ON PANEL 192F CORRODED ; / [01] CLEANED AREA AND FOUND OUT LIMITS IN REFERENCE B-737 SRM 53-40-70-1-A-1; [02] ADD REFERENCE B-737 SRM 51-10-02-0G-0; [03] WILL BE ACCOMPLISHED IN ITEM #TTG8Q009DQ95; [04] VERIFIED ACCOMPLISHED IN ITEM #TTG8Q009DQ95

Part: PANEL — CORRODED · airframe 59,271 hrs · 35,159 cycles

SUPPLEMENTAL INFORMATION: DME#2 BASE ON PANEL 192F CORRODED ; / [01] CLEANED AREA AND FOUND OUT LIMITS IN REFERENCE B-737 SRM 53-40-70-1A-1; [02] ADD REFERENCE 51-10-02-0G-0; [03] ADD B-737 SRM; [04] WILL BE ACCOMPLISHED. IN ITEM # TTG8Q009DQ95; [05] VERIFIED ACCOMPLISHED. IN ITEM # TTG8Q009DQ95

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 59,273 hrs · 35,160 cycles

CRACK FOUND AT LT HORIZONTAL STAB HSS 184.70 LOWER SKIN, I/B OF DRAIN HOLE, 10' FROM AFT SPAR. REMOVED PAINT IAW AMM 51-21-11-150-801. PERFORMED HFEC INSP IAW NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED. CRACK LENGTH .625'. REMOVED PANEL 331BZ IAW SRM 55-10-01-2R REPAIR 8. INSTALLED PANEL #331BZ IAW SRM51-40-02-0G-0. RESTORED PAINT IAW AMM 51-21 -73-370-801.

Part: HANDLE — BROKEN (COCKPIT) · airframe 58,184 hrs · 34,511 cycles

F/O GLARESHIELD GRAB HANDLE BROKEN ; / [01] REMOVED AND REPLACED F/O GRAB ASSIST HANDLE PER AMM 20-00-00 S.I.P.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 58,053 hrs · 34,431 cycles

CABIN FLOOR PANEL 241CF UPPER SURFACE HAS PEELED FIBERS DOT A-21-19 ; / BONDED REPAIR IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3 J-M AND SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL. TAP TEST GOOD. CURED 3 HOURS AT 150 DEGREES OVEN--BO-O6 DUE 8-25-21;EVALUATED FLOOR BOARD AND FOUND PULLED FIBERS TO UPPER FACE SHEET AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REV. 73 TABLE 201 REPAIR 1.<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 REV. 73 REPAIR 1 STEPS 3 A;C;E;F AND SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL<BR>VERIFIED REPAIR MATERIALS AS GLASS (A94414); RESIN (A51765) IAW SRM 53-00-50-2R-1 REV. 73 REPAIR 1 TABLE 201;REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD 241CF IAW SRM 53-00-50-2R-1 REV. 73; SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL. TAP TEST GOOD.;STEP 1 OK. OK TO BOND;STEP 3 AND 4 OK. AUDITED

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 58,053 hrs · 34,431 cycles

CABIN FLOOR PANEL 231ZF UPPER SURFACE HAS 3 PUNCTURES INBD SIDE DOT A-21-13 ; / BONDED REPAIR . IAW B737-700 SRM 53-00-50-2R-2 PAR3J-L. AAR DIGITAL THERMOMETER 30347 D.D.4-29-22 150DEG 3HRS.;EVALUATED PANEL 231ZF. FOUND 3EA PUNCTURES TO UPPER FACE SKIN. FOUND TO BE REPAIRABLE IAW B737-700 SRM 53-00-50-2R-2 PAR 1A. CLEAN AND PREP AREA'S FOR REPAIR. B737-700 SRM 53-00-50-2R-2 PAR3A;C-E. APPLIED POTTING COMPOUND TO 3EA AREA'S. IAW B737-700 SRM 53-00-50-2R-2 PAR3 F-I. VERIFIED MATERIALS AS BMS 5-28 TY 19 (15911); BMS 9-3 (A72547); BMS 8-201 (A51765).;REPAIRED 3EA PUNCTURES TO UPPER FACE SKIN. IAW B737-700 SRM 53-00-50-2R-2; SRM 53-00-50-2R-O.;STEP 1 OK. OK TO BOND;STEP 3 AND 4 OK. AUDITED

Part: FLOORBOARD — PEELING (CABIN) · airframe 58,053 hrs · 34,431 cycles

CABIN FLOOR PANEL 242AF AFT UPPER SURFACE HAS PEELED FIBERS. EVALUATED FLOORBOARD 242AF AND FOUND PULLED FIBERS TO UPPER FACE SHEET, REPAIRABLE IAW SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL TABLE 201 REPAIR 1. CLEANED & PREPPED FLOORBOARD IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3 A C E F AND SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL. BONDED REPAIR PLIES IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3 J-M AND SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL. TAP TESTED GOOD. REPAIRED DAMAGE TO FLOORBOARD 242AF AFT UPPER SURFACE IAW SRM 53-00-50-2R-1 REV. 73 AND SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,053 hrs · 34,431 cycles

FUSELAGE SKIN BAS CORROSION AROUND WATER SERVIVE DOOR CUTOUT. BLENDED CORROSION. EVALUATED MATERIAL LOSS TO BE .004' ORIG .063' REMAINING .059' WITHIN LIMITS IAW SRM 53-00-01-1A-1. APPLIED ALODINE IAW AMM 51-21-41-370-803 & PRIMER IAW AMM 51-21-72-370-804. RESTORED TOP COAT AT WATER SERVICE DOOR CUTOUT IAW AMM 51-21-73-804.

Part: BATTERY — FAILED (CABIN) · airframe 55,268 hrs · 32,774 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675 IN CABIN. / REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT LOCATION M1675 IN CABIN PER AMM 33-51-06

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 54,144 hrs · 32,043 cycles

FLIGHT DECK #1 FIRST OFFICER WINDOW FRAME CRACKED AT C AND D POST UPPER CORNER. / REPAIRED FRAME IAW EA.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 54,144 hrs · 32,043 cycles

FWD CARGO BAY BS 500D STR 21 L/H GUSSET IS CRACKED / REMOVED & REPLACED GUSSET AT FCB BS 500D STR 21 L/H IAW SRM 51-40-02 & DWG 143A7902 REV.-E 59191U 14NOV19

Part: GUSSET — CRACKED (FWD CARGO) · airframe 54,144 hrs · 32,043 cycles

FWD CARGO BAY BS 500D STR 21 R/H GUSSET IS CRACKED / REMOVED & REPLACED GUSSET AT FCB BS 500D STR 21 R/H IAW SRM 51-40-02 & DWG 113A7902 REV.- E 59191U 14NOV19

Part: BAFFLE — DAMAGED · airframe 54,144 hrs · 32,043 cycles

WHILE WORKING CUSTOMER CARD T995135 FOUND BAFFLE AT BS 500A-500B; RBL 21; WL 156 IS DAMAGED. / REPAIRED BAFFLE AT BS 500A - 500B RBL 21; WL 156 IAW EA 1-753-36067 REV IR AND ATS REPAIR # 19-05640 REV IR.

Part: BAFFLE — CORRODED · airframe 54,144 hrs · 32,043 cycles

***CORROSION*** WHILE WORKING CUSTOMER CARD T995118/ FUSE 5044; FOUND CORROSION ON BAFFLE AT BS 747-767; RBL 21; WL 156 / CORRODED BAFFLE AT BS747-767; RBL21; WL156 REMOVED AND REPLACED IAW DWG 146A7500 AND B737 SRM 51-40-02

Part: ATTACH ANGLE — CRACKED (BS 767-787) · airframe 54,144 hrs · 32,043 cycles

AFT CARGO BAY SHIELD ATTACH ANGLE CRACKED BETWEEN BS. 767 TO BS. 787, RBL 22, AT FASTENER HOLE. / R&R ANGLE IAW SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 54,144 hrs · 32,043 cycles

***CORROSION*** IN MULTIPLE AREAS OF ACB FLOOR T STRAP STA 887 LBL 10 RBL 22 WL 159 / REMOVED AND REPLACED FLOOR STRAP LOCATED STA 887 LBL 10 - RBL 22 W.L 159 IAW SRM 51-40-02; 51-10-02 PARAGRAPH 9 AND DWG 146A9401.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 54,144 hrs · 32,043 cycles

***CORROSION*** IN MULTIPLE LOCATIONS IN ACB ON L/H FLOOR TO SIDEWALL SUPPORT STA 727-847 LBL 22 WL 175 / REMOVED & REPLACED L/H FLOOR TO SIDEWALL SUPPORT BS-727 - 847 LBL 22 WL 175 IAW SRM 51-40-02 & DWG 146A7500 59191U 11-13-19

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 54,144 hrs · 32,043 cycles

***CORROSION*** ON FORWARD CARGO BAY SHIELD FROM B.S. 420-440; R.B.L. 24; W.L. 155 / REMOVED AND INSTALLED NEW FCB SHIELD FROM BS420-440; RBL24; WL155 IAW SRM 51-40-02 AND DWG #143A8126. 59565U 09NOV19

Part: SUPPORT — CORRODED (BS 727-767) · airframe 54,144 hrs · 32,043 cycles

AFT CARGO BAY ON R/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 22. / R&R SUPPORT IAW DWG AND SRM.

Part: SHIELD — CORRODED (BS 767-787) · airframe 54,144 hrs · 32,043 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 767 TO BS. 787+7, RBL 22. / R&R SHIELD IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 759-867) · airframe 54,144 hrs · 32,043 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS. 759 TO BS. 867, BETWEEN RBL 13 TO RBL 15. / R&R TRACK IAW SRM.

Part: SUPPORT — CORRODED (BS 400-500D) · airframe 54,144 hrs · 32,043 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 400 TO BS. 500D, LBL 24. / R&R SUPPORT IAW SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 54,144 hrs · 32,043 cycles

***CORROSION*** IN MULTIPLE AREAS OF ACB FLOOR T STRAP STA 767 LBL 20 RBL 20 WL 159 / REMOVED AND INSTALLED NEW 'T' STRAP AT ACB BS 767 LBL 20 TO RBL 20 WL 159 IAW SRM 51-40-02. 59807U 11/16/19

Part: INTERCOSTAL — CORRODED (BS 787) · airframe 54,144 hrs · 32,043 cycles

AFT CARGO BAY BILGE INTERCOSTAL CORRODED AT BS. 787+8, RBL 7. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 494-500A) · airframe 54,144 hrs · 32,043 cycles

FORWARD CARGO BAY SHIELD CORRODED BETWEEN BS. 494 TO BS. 500A, RBL 24. / R&R SHIELD PER SRM AND DWG.

Part: SEAT TRACK — CORRODED · airframe 54,144 hrs · 32,043 cycles

CORROSION IN WELL AND TOP OF TRACK BS 480 - 520 LBL25 WL 208 / REMOVED CORROSION ON SEAT TRACK B.S 480-520 LBL 25; FOUND TO BE OUT OF LIMITS AT B.S 520; LBL 25 IN AN AREA OF 1.2' X 1' X .022' I.A.W SRM 53-00-52-1A-1 SETP 4A(2)(A) FIG 103. REMOVED AND REPLACED SEAT TRACK BS 480-520 LBL 25 I.A.W DWG 143A5300 SHT 42; SRM 51-40-02-0G-0 STEP 7D & 9B

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 54,144 hrs · 32,043 cycles

***CORROSION*** AROUND MAJORITY OF FASTENERS THROUGH FUSELAGE SKIN EXTERNALLY; COVERED BY DORSAL FIN FROM STA 867 TO STA 1006; APPROXIMATELY STR 2R TO STR 2L. / REPAIRED FUSELAGE SKIN B.S 867-1006 STR 2R-2L IAW EA 1-753-36041 REV IR AND ATS ER 19-05567 REV IR

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 54,144 hrs · 32,043 cycles

FWD SERVICE DOOR IS CRACKED AT #4 BEAM / REPAIRED FWD SERVICE DOOR #4 BEAM ON CUSTOMER R.O. #0520055-FWR; JOB #528263

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,144 hrs · 32,043 cycles

L/H HORIZONTAL STABILIZER #5 RIB CRACKED AT LOWER END OF #2 STIFFENER STAB. STA. 129.50. / REPAIRED #5 RIB PER SRM.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 54,144 hrs · 32,043 cycles

FWD SERVICE DOOR IS CRACKED AT #5 BEAM / REPAIRED FWD SERVICE DOOR #5 BEAM ON CUSTOMER R.O. #0520055-FWR; JOB #528263

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,144 hrs · 32,043 cycles

L/H HORIZONTAL STABILIZER #5 RIB CRACKED, LOWER END OF #3 STIFFENER STAB. STA. 129.50. / REPAIRED #5 RIB IAW SRM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 52,700 hrs · 31,086 cycles

R1 DOOR EVAC SLIDE GRIT BAR STOWAGE CLIP LOOSE. SECURED CLIP PER SIP.

Part: LIGHT — MISSING (CABIN) · airframe 52,600 hrs · 31,017 cycles

CENTER CABIN CEILING EMERGENCY EXIT LIGHT MISSING. R&R LIGHT HOUSING IAW AMM.

Part: SIGN — MISSING (CABIN) · airframe 52,600 hrs · 31,017 cycles

RT OVERWING EMERGENCY EXIT LOWER LIGHT MISSING DIRECTIONAL ARROW. R&R SIGN IAW MM.

Part: BRACKET — DIRTY (R1 DOOR) · airframe 51,845 hrs · 30,563 cycles

R1 DOOR EMERGENCY SLIDE BAR VERY HARD TO ARM. FOUND DEBRIS IN FORWARD DOOR BRACKET. CLEANED DEBRIS FROM BRACKET IAW AMM.

Part: SCREW — MISSING (FLOOR PLATE) · airframe 51,596 hrs · 30,424 cycles

R1 DOOR ESCAPE SLIDE ANCHOR (FLOOR) PLATE MISSING A SCREW. R&R PLATE SCREW PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,505 hrs · 30,357 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,505 hrs · 30,357 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,505 hrs · 30,357 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PACK PER AMM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 51,505 hrs · 30,357 cycles

RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM. 53-31-31

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,505 hrs · 30,357 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PACK PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,505 hrs · 30,357 cycles

LT EMERGENCY EXIT SIDEWALL LIGHT INOP. R&R LIGHT BALLAST PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,505 hrs · 30,357 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,505 hrs · 30,357 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PACK PER AMM.

Part: COVER — BROKEN (CABIN) · airframe 49,606 hrs · 29,113 cycles

AFT ATTENDANT PANEL EMERGENCY LIGHT SWITCH COVER BROKEN. R&R COVER IAW CMM.

Part: STIFFENER — CRACKED (LT WHEEL WELL) · airframe 49,606 hrs · 29,113 cycles

VERTICAL STIFFENER CRACKED IN LEFT WHEEL WELL AT LBL 27; LOWER WING TO BODY SUPPORT. / REMOVED AND REPLACED PER SRM 51-40-02.

Part: STRINGER — CRACKED (RT WING) · airframe 47,963 hrs · 28,065 cycles

R/H INBD FIXED LEADING EDGE AFT STRINGER AT WS 204.25 CRACKED AT FASTENER HOLE. 7TH HOLE FWD OF FWD SPAR / REMOVED AND REPLACED STRINGER I.A.W SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 47,963 hrs · 28,065 cycles

INBOARD FASTENER HOLE FOR DRAIN FITTING CRACKED AT APPROXIMATELY 7 O'CLOCK POSITION, RBL 33.5". REPAIRED FITTING PER EA.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 47,963 hrs · 28,065 cycles

FLOOR PANEL 232EF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / R&R'D FLOOR PANEL PER AMM 53-21-00

Part: FLOOR PANEL — PULLED (CABIN) · airframe 47,963 hrs · 28,065 cycles

FLOOR PANEL 231XF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / INSTALLED CABIN FLOOR PANEL 231XF PER AMM 53-21-00

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 47,963 hrs · 28,065 cycles

FLOOR PANEL 241AF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / R&R'D FLOOR PANEL PER AMM 53-21-00

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 47,963 hrs · 28,065 cycles

FLOOR PANEL 241DF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / R&R'D FLOOR PANEL PER AMM 53-21-00

Part: FLOOR PANEL — PULLED (CABIN) · airframe 47,963 hrs · 28,065 cycles

FLOOR PANEL 231KF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / R&R'D FLOOR PANEL PER AMM 53-21-00

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 47,963 hrs · 28,065 cycles

FLOOR PANEL 241CF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / R&R'D FLOOR PANEL PER AMM 53-21-00

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 47,963 hrs · 28,065 cycles

EXTERIOR LAV SERVICE DOOR HAS CORROSION ON INSIDE SURFACE / R&R LAV DOOR ASSY PER AMM 52-49-07

Part: BRACKET — CRACKED (RIGHT WING) · airframe 47,963 hrs · 28,065 cycles

RIGHT WING OBRSS 273;17 INCHES AFT R/S;1 INCH BELOW UPPER PNL SEAL RETAINER BRACKET IS CRACKED. / REPLACED SEAL RETAINER BRACKET PER SRM 51-40-02

Part: SKIN — DELAMINATED (TE FLAP) · airframe 46,963 hrs · 28,065 cycles

LT WING OUTBOARD AFT FLAP LOWER SKIN DELAMINATED AT INBOARD TRAILING EDGE. REPAIRED AFT FLAP PER SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 47,963 hrs · 28,065 cycles

AFT CARGO FWD CORNER THRESHOLD CRACKED IN 3 LOCATIONS (MARKED) / THRESHOLD PLATE REPAIRED ON REPAIR ORDER # 7530063-ANR. PLATE TO BE INSTALLED ON ROUTINE TASK CARD 753-721-00-01.

Part: SKIN — CRACKED (LE SLAT) · airframe 47,963 hrs · 28,065 cycles

LT WING NR 1 SLAT SKIN CRACKED AT SLAT ACTUATOR OUTBOARD ATTACH RIB 2ND FROM AFT FASTENER. R&R NR 1 SLAT PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 47,963 hrs · 28,065 cycles

RT WING NR 7 SLAT SKIN CRACKED AT LOWER NOSE ATTACH RIB ATTACHING FASTENER. R&R NR 7 SLAT PER SRM.

Part: FLOOR PANEL — CRACKED (AFT CARGO COMPT) · airframe 47,728 hrs · 27,914 cycles

AFT CARGO FWD CENTER FLOOR PANEL 140BF CRACKED/WORN / REMOVED AND REPAIRED PER AMM 25-52-10

Part: FLOOR PANEL — CRACKED (AFT CARGO COMPT) · airframe 47,728 hrs · 27,914 cycles

AFT CARGO FWD FLOOR PANEL 140AF CRACKED/WORN / REMOVED AND REPLACED PER AMM 25-52-10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,577 hrs · 27,817 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: GIRT BAR — LOOSE (R1 DOOR SLIDE) · airframe 46,882 hrs · 27,385 cycles

R1 DOOR SLIDE GIRT BAR LOOSE. SECURED THE GIRT BAR IAW MM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 45,466 hrs · 26,539 cycles

R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. (DID NOT DEPLOY) R&R SLIDE ASSY PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 43,483 hrs · 25,363 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R & R THE BATTERY PACK IAW AMM AND DWG.

Part: ENGINE — VIBRATION (NR 1) · airframe 43,372 hrs · 25,294 cycles

HIGH VIBRATION INDICATION ON NR 1 ENGINE. DECLARED EMERGENCY AND AIR TURNBACK. R & R THE NR 1 ENGINE IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 42,315 hrs · 24,670 cycles

FORWARD ENTRY DOOR EMER LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,058 hrs · 24,523 cycles

R1 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,979 hrs · 24,476 cycles

R1 DOOR EXTERIOR EMER LIGHT IN OPERATIVE. R & R LIGHT IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 41,979 hrs · 24,476 cycles

L2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

R1 DOOR CUTOUT UPPER HINGE RECESS CRACKED, AT BS 303, RBL 64. R & R HINGE BOX IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

R1 DOOR CUT OUT LOWER FWD CORNER ON THE INTERNAL SIDE CRACKED, AT BS 303, RBL 64. R & R CUT OUT IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,979 hrs · 24,476 cycles

RIGHT HORIZONTAL STABILIZER LE PANEL 341BZ, 5TH RIB OTBD FROM INBD END, RIB ATTACH ANGLE CRACKED AT UPPER AFT END. R & R RIB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

LEFT CREASE BEAM INNER CORD CORRODED, BETWEEN BS 695 - 711. REPAIRED INNER CHORD IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

RIGHT CREASE BEAM INNER CHORD CORRODED, BETWEEN BS 695 - 729. REPAIRED INNER CHORD IAW ER & EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

STRAP CORRODED AT BS 1016, BETWEEN LBL 6 - 10. R & R STRAP IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

FORWARD ENTRY DOOR INNER CHORD CORRODED, BETWEEN BS 313 - 348. R & R CHORD IAW SRM & DWG.

Part: STRUCTURE — CORRODED (R1 DOOR) · airframe 41,979 hrs · 24,476 cycles

R1 DOOR INNER CHORD CORRODED, BETWEEN BS 294 - 332. R & R INNER CHORD IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

RIGHT FLOOR TO SIDEWALL TRANSITION SUPPORT CORRODED, BETWEEN BS 767 - 727E. R & R SUPPORT IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 41,979 hrs · 24,476 cycles

AFT CARGO FLOORBEAM TRACK TOP SURFACE CORRODED, BETWEEN BS 793 - 807, RBL 14. R & R TRACK IAW SRM & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

LEFT CARGO FLOOR TO SIDEWALL TRANSITION SUPPORT CORRODED AT BS 770.5, LBL 24. R & R SUPPORT IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

STRINGER CLIP CORRODED, AT BS 967, STRINGER 23R. R & R CLIP IAW SRM & DWG.

Part: WEB — CORRODED (CARGO DOOR) · airframe 41,979 hrs · 24,476 cycles

FORWARD CARGO BIN DOOR WEB CORRODED, BETWEEN BS 460 - 490. R & R WEB IAW SRM.

Part: WEB — CORRODED (CARGO DOOR) · airframe 41,979 hrs · 24,476 cycles

CARGO DOOR WEB CORRODED, BETWEEN BS 795 - 830. REMOVED WEB IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 41,979 hrs · 24,476 cycles

STRINGER CLIP CORRODED AT BS 847, STRINGER 23L. R & R CLIP IAW SRM & DWG.

Part: CONTROL VALVE — FAULTY (BLEED AIR SYS) · airframe 41,305 hrs · 24,087 cycles

AIR RETURN, NR 1 BLEED TRIP OFF LIGHT ILLUMINATED DURING CLIMB & WOULD NOT RESET. R & R NR 1 ENG PRE-COOLER CONTROL VLV IAW MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 38,312 hrs · 22,355 cycles

FLOORBEAM SPLICE STRAP CRACKED AT BS 727B RBL 45.5. REPAIRED FLOORBEAM IAW EA.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 37,856 hrs · 22,081 cycles

L2 DOOR EMER EVAC SLIDE BOTTLE PRESS LOW. R & R SLIDE IAW MT.

Part: COVER — MISSING (EXIT SIGN) · airframe 36,304 hrs · 21,211 cycles

RIGHT OVERWING EMER EXIT SIGN COVER MISSING. INSTALLED COVER IAW AMM.

Part: STRAP — FRAYED (CABIN) · airframe 35,523 hrs · 20,745 cycles

RIGHT OVER WING DOOR ESCAPE STRAP FRAYED. R & R STRAP IAW MM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 35,523 hrs · 20,745 cycles

RIGHT HORIZONTAL STABILIZER STAB STATION 101.90 RIB FWD END OTBD SIDE CRACKED. REPAIRED RIB IAW EA.

Part: STRAP — FRAYED (EMERGENCY LIGHT) · airframe 35,523 hrs · 20,745 cycles

LEFT EMERGENCY EXIT HATCH ESCAPE STRAP FRAYED. R & R STRAP IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 34,984 hrs · 20,423 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT ROW 16. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 34,984 hrs · 20,423 cycles

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

Part: LENS — MISSING (CABIN) · airframe 34,984 hrs · 20,423 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,984 hrs · 20,423 cycles

AFT GALLEY EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 34,984 hrs · 20,423 cycles

LT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW MM.

Part: LENS — UNSECURE (CABIN) · airframe 32,854 hrs · 19,142 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER FELL OFF. R & R LENS ASSY IAW MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 32,708 hrs · 19,052 cycles

RIGHT STAB LOWER IN SPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 32,708 hrs · 19,052 cycles

LEFT HORIZ STAB LOWER IN SPAR SKIN CRACKED AT STA 138.70. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 32,708 hrs · 19,052 cycles

LEFT HORIZ STAB LOWER IN SPAR SKIN CRACKED AT STA 129.50. REPAIRED SKIN IAW SRM.

Part: ENGINE — FAILED (RIGHT) · airframe 30,330 hrs · 17,693 cycles

DIVERT/DECLARED EMERGENCY/ENGINE SHUT DOWN. ON CLIMBOUT NR 2 ENGINE LOUD BAND AND SHUTDOWN. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: SIGN — BROKEN (CABIN) · airframe 30,300 hrs · 17,669 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,956 hrs · 16,847 cycles

LT FRAME CRACKED AT BS 312, STR 4L. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,956 hrs · 16,847 cycles

AFT CARGO FLOOR SUPPORT CHANNEL CORRODED AT BS 770, LBL 12. REPAIRED CHANNEL PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,956 hrs · 16,847 cycles

AFT CARGO FLOOR SUPPORT CHANNEL CORRODED AT BS 770, LBL 3. REPAIRED CHANNEL PER EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 28,243 hrs · 16,439 cycles

FWD LT EMERGENCY BATTERIES FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 28,243 hrs · 16,439 cycles

FWD RT EMERGENCY BATTERIES FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: CONTROLLER — ARCED (COCKPIT) · airframe 27,025 hrs · 15,710 cycles

AIR TURNBACK, LEFT FORWARD WINDSHIELD ARCED AND THEN CRACKED. REMOVED AND REPLACED L1 WINDOW AND WINDOW HEAT CONTROLLER PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 26,841 hrs · 15,600 cycles

MID CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: CAP — MISSING (CABIN) · airframe 26,118 hrs · 15,205 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS END CAP MISSING. INSTALLED END CAP PER MM.

Part: TRACK — LOOSE (EVAC SLIDE) · airframe 26,118 hrs · 15,205 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE TRACK LOOSE. SECURED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 26,118 hrs · 15,205 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 19 TO ROW 23. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 25,508 hrs · 14,847 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: WIRE — DAMAGED (CABIN) · airframe 24,745 hrs · 14,420 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS WIRING INOP BETWEEN ROW 18 TO ROW 20. REPAIRED WIRE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 24,582 hrs · 14,311 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 24,122 hrs · 14,045 cycles

R1 DOOR EMERGENCY EXIT LIGHT BASE BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 21,684 hrs · 12,600 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,553 hrs · 12,522 cycles

DURING SCHEDULED MV2 CHECK FOUND EEPLS INOP AT ROW 1. RELAMPED PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 20,858 hrs · 12,097 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 807, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: COVER — MISSING (CABIN) · airframe 20,690 hrs · 11,997 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER MISSING AT ROW 7. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,113 hrs · 11,629 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,191 hrs · 9,853 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,191 hrs · 9,853 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,191 hrs · 9,853 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,191 hrs · 9,853 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,857 hrs · 9,654 cycles

FOUND RT OVERWING EMEGENCY EXIT DOOR SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.

Part: STRIP — CRACKED (CABIN) · airframe 16,745 hrs · 9,580 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS STRIP CRACKED. REMOVED AND REPLACED STRIP PER MM.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 12,138 hrs · 6,805 cycles

EEPLS LENS AFT COVER MISSING. INSTALLED COVER ASSY PER MM.

Part: SLIDE — UNWANTED DEPLOY (R2 DOOR) · airframe 11,146 hrs · 6,242 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 9,797 hrs · 5,474 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 7,728 hrs · 4,314 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (L1 DOOR) · airframe 2,971 hrs · 1,690 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.