N786SW

Part: DOOR — DELAMINATED (ZN 100 FUS LOWER) · airframe 74,617 hrs · 44,159 cycles

RT AC BAY DOOR; RT FWD O/B CORNER DELAM; MEASURES 4.25' X 4.25'<[01] REFERENCE EA 23-153-03744

Part: TAIL CONE — DELAMINATED (ZN 500 LEFT WING) · airframe 73,851 hrs · 43,709 cycles

LEFT WING #3 FLAP FAIRING TAIL CONE DELAMINATED.<[01] REMOVED AND REPLACED LH WING #3 FLAP FAIRING TAIL CONE PER SRM 51-40-02

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 73,636 hrs · 43,579 cycles

AFT SVC DOOR SLIDE HAS EXCESS MATERIAL OUT OF SLIDE COVER<[01] REPOSITIONED SLIDE ASSY REF AMM 25-66-01 / MT 725-61-06

Part: STUD — MISSING (ZN 100 FUS LOWER) · airframe 72,908 hrs · 43,121 cycles

AFT CARGO DOOR HANDLE TEFLON STUD MISSING<[01] INSTALLED AFT CARGO DOOR HANDLE TEFLON STUD PER AMM 52-31-14.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 72,675 hrs · 42,964 cycles

R1 DOOR ESCAPE SLIDE EMERGENCY LIGHT INOP.<[01] RELAMPED R1 EXTERNAL SLIDE EMERGENCY LIGHT.<BR>IAW B737 MM 33-51-04

Part: COVER — BROKEN (ZN 200 FUS TOP) · airframe 72,457 hrs · 42,818 cycles

RH LOWER EMERGENCY EXIT LIGHT COVER BROKEN<[01] REPLACED RH LOWER EMERGENCY EXIT LIGHT COVER PER AMM 33-51-01

Part: SIGN — INOPERATIVE (L1 DOOR) · airframe 70,923 hrs · 41,833 cycles

CUSTOMER WALK. L-1 DOOR EMERGENCY LIGHT TWO BULBS OUT NEED SIX WORKING. / [01] RELAMPED L-1 DOOR EMERGENCY EXIT SIGN 2EA AS PER REF B737 AMM 33-51-01-960-801. TEST OK.;[02] VERIFIED STEP 1.

Part: SIGN — BROKEN (R1 DOOR) · airframe 70,923 hrs · 41,833 cycles

R-1 DOOR LOWER EXIT SIGN LENS BROKEN / [01] REMOVED AND REPLACED R-1 DOOR LOWER EXIT SIGN. REF. BOEING 737-700 AMM 33-51-01-960-802.;[02] VERIFIED 1

Part: SIGN — BROKEN (R2 DOOR) · airframe 70,923 hrs · 41,833 cycles

R-2 DOOR LOWER EXIT SIGN BROKEN / [01] REMOVED AND REPLACED R2 LOWER EXIT SIGN AS PER AMM 33-51-01-960-802-NG.;[02] VERIFIED STEP 1

Part: SIGN — BROKEN (L1 DOOR) · airframe 70,923 hrs · 41,833 cycles

L-1 DOOR LOWER EXIT SIGN LENS BROKEN. / [01] REMOVED AND REPLACED L-1 DOOR LOWER EXIT SIGN. REF. BOEING 737-700 AMM 33-51-01-960-802.;[02] VERIFIED 1

Part: PANEL — DETERIORATED (FUSELAGE) · airframe 70,923 hrs · 41,833 cycles

PANEL 231XF (PANEL 231XF FLOOR PANEL) UPPER SURFACE RESIN DETERIORATED / [01] MEASUREMENTS;[02] PREPARED AND REPAIRED FLOOR PANEL #231XF AT DAMAGED AREA PER B737 SRM 53-00-50-2R-1 PARAGRAPH 3.M. MATERIALS USED RESIN P/O#1783720; CLOTH P/O#1690463;[03] VERIFIED STEPS 1 AND 2

Part: SKIN PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 70,923 hrs · 41,833 cycles

RT WING LOWER MID SPAN T/E PANEL 661BB - INNER SKIN HAS CRACKS AND BULGING AROUND NUMEROUS FASTENER HOLES AS MARKED. 124-023 / [01] CLEANED AND PREPARED DAMAGE FASTENER HOLES FOR REPAIR; PER FORMED DRY OUT FOUND NO WATER AS PER B737 SRM 51-70-04-2R-9;[02] REPAIRED DAMAGE FASTENER HOLES AS MARKED ON PANEL 661BB WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-9B MATERIALS USED PO#1690463 AND PO#1774613;[03] PERFORMED TAP TEST ON REPAIRED AREA; FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 5;[04] MEASUREMENTS;[05] VERIFIED 1 TO 4

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 70,923 hrs · 41,833 cycles

AFT CARGO AFT CORNER SCUFF PLATE CRACKED / [01] RECEIVED SCUFF PLATE PART # 146A8341-9 FROM JL WELDING TAG #011178 LOCATED AND DRILLED AS PER B 737-700 SRM 51-40-05-0G-0 SCUFF PLATE TO BE INSTALLED ON ITEM #TTG8Q00F4DRW;[02] [FINAL] VALIDATED STEP 1

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 70,923 hrs · 41,833 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #5 RIB CRACK NOTED AT RIVET EDGE HOLE (DOT-223 LHLE5). / [01] REMOVED L/H HORIZONTAL STAB #5 RIB AS PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW L/H HORIZONTAL STAB AS PER B737-700 SRM 51-40-05-0G-0;[03] REMOVED L/H HORIZONTAL STAB LEADING EDGE #5 RIB AS PER B737-700 SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW L/H HORIZONTAL STAB LEADING EDGE RIB AS PER B737-700 SRM 51-40-05-0G-0;[05] VALIDATED CORRECTED STATEMENTS 3 & 4<BR><BR>OK TO INSTALL NEW UNIT;[06] INSTALLED NEW L/H HORIZONTAL STAB LEADING EDGE #5 RIB AS PER B737-700 SRM 51-40-02-0G-0;[07] REMOVED L/H HORIZONTAL STAB LEADING EDGE #5 RIB AS PER B737-700 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW L/H HORIZONTAL STAB LEADING EDGE RIB AS PER B737-700 SRM 51-40-05-0G-0. INSTALLED NEW L/H HORIZONTAL STAB LEADING EDGE #5 RIB AS PER B737-700 SRM 51-40-02-0G-0.;[08] [FINAL] VALIDATED STEPS 6 & 7

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 70,923 hrs · 41,833 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #4 RIB CRACK NOTED AT RIVET EDGE HOLE (DOT-223 LHLE4). / [01] REMOVED #4 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED #4 NEW RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-0.;[03] VALIDATED STEPS 1 & 2<BR><BR><BR>OK TO INSTALL NEW UNIT;[04] INSTALLED #4 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[05] SUMMARY :REMOVED #4 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.LOCATED AND DRILLED #4 NEW RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-0.INSTALLED #4 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[06] [FINAL] VALIDATED STEPS 4 & 5

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 70,923 hrs · 41,833 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #3 RIB CRACK NOTED (DOT-223 LHLE3). / [01] REMOVED #3 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW #3 RIB AT L/H HORIZONTAL STAB AS PER REF SRM 51-40-05-0G-0.;[03] VALIDATED STEPS 1 & 2<BR><BR>OK TO INSTALL NEW UNIT;[04] INSTALLED #3 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[05] SUMMARY :<BR>REMOVED #3 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.LOCATED AND DRILLED NEW #3 RIB AT L/H HORIZONTAL STAB AS PER REF SRM 51-40-05-0G-0INSTALLED #3 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[06] [FINAL] VALIDATED STEPS 4 & 5

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 70,923 hrs · 41,833 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #2 RIB CRACK NOTED (DOT-223 LHLE2). / [01] REMOVED #2 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED # 3 NEW RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-0.;[03] CORRECTION STEP #2....LOCATED AND DRILLED # 2 NEW RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-;[04] VALIDATED STEPS 1; 2 & 3<BR><BR><BR>OK TO INSTALL NEW UNIT;[05] INSTALLED #2 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[06] SUMMARY :REMOVED #2 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED # 2 NEW RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-0.INSTALLED #2 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[07] [FINAL] VALIDATED STEPS 5 & 6

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 70,923 hrs · 41,833 cycles

PANEL 241AF HAS SURFACE DELAMINATION / [01] MEASUREMENTS;[02] CLEANED AND PREPARED DAMAGE AREAS AS MARKED FOR REPAIR ON TOP SURFACE OF MAIN CABIN FLOOR PANEL 241AF AS PER B737 SRM 53-00-50-2R-1;[03] VERIFIED STEPS 1 AND 2;[04] OK TO APPLY REPAIR;[05] REPAIRED DAMAGED AREAS AS MARKED WITH A PERMANENT REPAIR ON TOP SURFACE OF MAIN CABIN FLOOR PANEL 241AF AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO#1778544 AND PO#1690463;[06] PERFORMED TAP TEST ON REPAIRED AREAS; FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 5;[07] VERIFIED STEP 5;[08] VERIFIED STEP 6

Part: NONE — MISSING (OVERWING EXIT) · airframe 70,824 hrs · 41,768 cycles

EXIT SALINA SIGN MISSING FROM RH OVERWING EXIT / [01] INSTALL EXIT SALIDA COVER ON RH OVER WING EXIT DOOR PER SIP

Part: PANEL — SMOKE (AFT CABIN) · airframe 70,757 hrs · 41,724 cycles

AFT #1 COFFEE POT SMELLS OF ELECTRICAL SMOKE WHEN ON / [01] REMOVED AND REPLACED #1 COFFEE MAKER IAW AMM 25-30-01 OPS CK GOOD

Part: FLAP — DELAMINATED (L/H WING) · airframe 70,207 hrs · 41,359 cycles

LEFT WING OUTBOARD AFT FLAP HAS SEVERAL SPOTS OF DELAMINATION ON THE UNDER AND UPPER SIDE OF THE INBOARD 15 INCHES. (MARKED) / [01] REPAIRED AFT FLAP PER SRM 51-70-05.

Part: LENS — BROKEN (PAX CABIN) · airframe 70,196 hrs · 41,351 cycles

CREW REPORTS FWD ENTRY EMERGENCY EXIT SIGN LENS IS BROKEN / [01] C/W EA M-21-133-00720

Part: LENS — MISSING (R/H OVERWING) · airframe 69,275 hrs · 40,749 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS ( AFT SIDE) MISSING DIRECTIONAL ARROW / [01] R & R LENS IAW AMM 33-51-01;[02] INSPECTED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,535 hrs · 40,296 cycles

LH OUTER OVERWING EMERGENCY EXIT LIGHT INOP ; / [01] RELAMPED LH OUTER OVERWING EMER LIGHT IAW 33-51-04. OPS CHECKS GOOD.

Part: FITTING — CORRODED (L/H MLG W/W) · airframe 68,455 hrs · 40,247 cycles

SUPPLEMENTAL INFORMATION: LFT MLG FWD TRUNNION SUPPORT FITTING UPPER O/B (#1) BORE HAS EVIDENCE OF CORROSION ; LFT MLG FWD TRNNION SPPORT FITTING PPER O (#1) ORE HAS EVIDENCE OF CORROSION / [01] REPAIRED PER EA 1-A57-3246 REV 14

Part: FITTING — CORRODED (L/H MLG W/W) · airframe 68,455 hrs · 40,247 cycles

SUPPLEMENTAL INFORMATION: LFT MLG FWD TRUNNION SUPPORT FITTING; LOWER O/B LUG (#3) BORE HAS EVIDENCE OF CORROSION ; LFT MLG FWD TRNNION SPPORT FITTING; LOWER O LG (#3) ORE HAS EVIDENCE OF CORROSION / [01] REPAIRED PER EA 1-A57-3246 REV 14

Part: NONE — BROKEN (R/H WING) · airframe 68,454 hrs · 40,247 cycles

RT WING I/B FIXED T/E DEFLECTOR RIB LOWER SIDE ROD ATTACH LUG BROKEN. ; / [01] TRIMMED OUT AND REMOVED DMG TURNBUCKLE LUG AS PER B737-700 SRM 57-51-02-2R-2 REPAIR 2 AND SRM 51-10-02-0G-0; [02] VERIFIED STEP 1; [03] PERFORMED HFEC INSP. ON REWORKED AREA IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23.<BR>NO CRACKS NOTED<BR>TOOL: NORTEC 600 B/C: 166316 DUE: 10/08/22; [04] ACCOMPLISHED FLAP PEENING TO AFFECTED ARAEA REFERENCE B737-700 SRM 57-51-02-2R-2; SRM 51-20-06-OG-0 AND SOPM 20-10-03; [05] VERIFIED STEP 4; [06] VERIFIED SMOOTHNESS ON TRIMMED EDGES REF B737-700-SRM 57-51-02-2R-2 TOOL USED B/C 172332. FLAP PEENING TOOL USED B/C 19433; [07] VERIFIED STEP 6. OK TO TREAT AND PRIME; [08] FABRICATED NEW FILLERS REPAIRS 6 EA LOCATED AND DRILLED NEW FITTING PER SRM 57-51-02-2R-2; [09] VERIFIED STEP 8; OK TO INSTALL REPAIR PARTS; [10] ISNTALLED REPAIR PARTS AS PER B737-700 SRM 51-40-02-0G-0; SRM 57-51-02-2R-2 REPAIR 2 FIG 202 AND DWG #57200003 REV 2; [11] LATE ENTRY: TREATED AND PRIMED HOLES AS PER B737-700 AMM 51-21-41-370-804 AND AMM 51-21-72-370-803; [12] VERIFIED STEP 10 AND 11. TASK COMPLETE.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 68,454 hrs · 40,247 cycles

INTERNAL EMERGENCY EXIT SIGN INOP; AT LEFT OVERWING DOOR. DURING T/S FOUND BATTERY PACK INOPERATIVE. REMOVED AND REPLACED BATTERY AND PERFORMED TEST; TEST PASSED IAW AMM FIM 33-50 TASK 801 AND AMM 33-51-06-960-805.

Part: BATTERY PACK — OUT OF POSITION (CABIN) · airframe 68,454 hrs · 40,247 cycles

INTERNAL EMERGENCY EXIT SIGN INOP AT R/H OVERWING DOOR. REPOSITIONED BATTERY PACK ; PERFORMED OPERATIONAL TEST; TEST PASS IAW AMM 33-51-06=960-805.

Part: CAP — CORRODED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

AFT CARGO COMPARTMENT CAP STRIPS FWD AND AFT SIDE OF CARDO DOOR CUTOUT WITH CORROSION ; / [01] AFT CARGO COMPARTMENT CAP STRIPS FWD AND AFT SIDE OF CARGO DOOR CUTOUT WITH EXFOLIATION CORROSION PASSING THROUGH MATERIAL; [02] RECEIVED NEW CAP STRIPS P/N: 453A2411-3 AND 453A2411-1. REF TASK CARD TTG8Q004G35M FOR CAP STRIPS INSTALLATION; [03] VERIFIED STEPS 1 AND 2

Part: CAP — CORRODED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

AFT CARGO FLOOR L/H CAP STRIPS WITH CORROSION ; / [01] AFT CARGO FLOOR L/H CAP STRIPS WITH EXFOLIATION CORROSION PASSING THROUGH MATERIAL; [02] RECEIVED CAP STRIP P/N: 453A2611-8. REF. TASK CARD TTG8Q004G35M FOR CAP STRIP INSTALLATION.; [03] VERIFIED STEPS 1 AND 2

Part: CAP — CORRODED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

AFT CARGO FLOOR R/H CAP STRIPS WITH CORROSION ; / [01] AFT CARGO FLOOR R/H CAP STRIPS WITH EXFOLIATION CORROSION PASSING THROUGH MATERIAL; [02] RECEIVED CAP STRIP P/N: 453A2611-9 AND 453A2611Y3. REF. TASK CARD TTG8Q004G35M FOR CAP STRIP INSTALLATION.; [03] VERIFIED STEPS 1 AND 2

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

FWD CARGO COMPARTMENT FLOOR STRUCTURE INTERCOSTAL S25L BETWEEN STA 500B-500C CRACKED ; / [01] REMOVED DAMAGE INTERCOSTAL FROM FWD CARGO PER 737-700 SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT; [02] LOCATED AND DRILLED NEW INTERCOSTAL IAW B737-700 SRM 51-40-05; [03] VERIFIED 1 TO 3; [04] OK TO TREAT AND PRIME NEW HOLES; [05] TREATED AND PRIMER DRILL HOLE NEW INTERCOSTAL AS PER SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804; [06] VERIFIED 5. OK TO INSTALL INTERCOSTAL; [07] INSTALLED NEW INTERCOSTAL AS PER SRM 51-40-02-0G-0 AND DWG 143A7505.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

FWD CARGO COMPARTMENT FLOOR STRUCTURE INTERCOSTAL S25L BETWEEN STA 500-500A CRACKED ; / [01] REMOVED DAMAGE INTERCOSTAL FROM FWD CARGO PER 737-700 SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT; [02] REMOVED INTERCOSTAL AS PER SRM 51-40-02-0G-0; [03] LOCATED AND DRILL HOLE NEW INTERCOSTAL AS PER SRM 51-40-05; [04] VERIFIED STEPS 1 TO 3.; [05] OK TO TREAT AND PRIME; [06] TREATED AND PRIMER DRILL HOLE NEW INTERCOSTAL AS PER SRM 51-20-01-0G-0 AND AMM 51-21--72-370-804; [07] VERIFIED 6. OK TO INSTALL INTERCOSTAL; [08] INSTALLED NEW INTERCOSTAL AS PER SRM 51-40-02-0G-0 AND DWG 143A7505.

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 68,452 hrs · 40,246 cycles

RT HORIZONTAL STAB NR 4 INSPAR RIB HSS 120 FWD LOWER OTBD CORNER CRACKED. REMOVED CRACK IAW SRM 51-10-02-0G-0 & 55-10-09-2R-5 REPAIR 5. PERFORMED HFEC INSP OF CUT EDGES ON REPAIR AREA IAW NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS NOTED. PERFORMED HFEC ROTO INSP OF ALL EXISTING FASTENER HOLES WITHIN REPAIR AREA IAW NDT PART 6 51-00-00 PROCEDURE 16. NO CRACKS NOTED. ACCOMPLISHED GVI OF ALL AREAS WITHIN REPAIR AREA, NO DEFECTS NOTED IAW SRM 55-10-09-2R-5, STEP 4.F. FABRICATED ANGLE SHIM & FILLER IAW SRM 55-10-09-2R-5 REPAIR 5 & BAC 5602. LOCATED & DRILLED IAW SRM 51-40-05-0G-0. TREATED & PRIMED REPAIR PARTS IAW SRM 51-20-01 & SOPM 20-41-02. INSTALLED REPAIR IAW SRM 55-10-09-2R-5 REPAIR 5. STEP 12.

Part: RETAINER — CRACKED (R/H WING) · airframe 68,452 hrs · 40,246 cycles

RT WING T/E AT FLEX CONTROL RIB; TOP PANEL SEAL RETAINER CRACKED. REMOVED AND REPLACED R/H WING AT FLEX CONTROL RIB TOP PANEL SEAL RETAINER AS PER B737-700 SOPM 20-50-18.

Part: RUB STRIP — MISSING (BS 235.8) · airframe 68,452 hrs · 40,246 cycles

AT FRAME BS 235.8 MISSING SECTION WHERE INITIAL RUBBING STRIP ATTACH. TRIMMED DAMAGE AREA AT FRAME STA 235.8 PER SRM 51-10-02-0G-0 VERIFIED STEP 1. PERFORMED HFEC INSP ON CUTOUT AREA IAW B737 NDTP6 51-00-00 PROC.23 NO CRACKS. FABRICATED AND INSTALLED REPAIR AT FRAME IAW EA 21-153-03124 VERIFIED. STEPS 4 5& 6 RII VERIFIED STEPS 4, 5 & 6.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE SHIELD PANEL AT S-25R BETWEEN STA 847-867 WITH EXFOLIATION CORROSION ; / [01] REMOVED CORROSION FROM AFT CARGO SHIELF STA 847-867 RBL 25 AS PER B737-700 SRM 51-10-02-0G-0; [02] VERIFIED STEP 1; CORROSION WAS THRU METAL; [03] AFT CARGO SHIELD FOUND OUT OF LIMITS DUE TO EXFOLIATION CORROSION PASS THROUGH THE MATERIAL AS PER B737-700 SRM 53-00-53-1A-2; [04] LOCATED AND DRILLED NEW SHIELD P/N: 146A8127Y5 AS PER B737-700 SRM 51-40-02-0G-0; [05] REF TASK CARD TTG8Q004G35M FOR INSTALLATION OF THE SHIELD.

Part: PANEL — CRACKED (R/H WING) · airframe 68,452 hrs · 40,246 cycles

FLAP SUPPORT NO.8 PANEL 644EB LOWER SECTION CRACKED/DELAMINATED ; / [01] REMOVED DAMAGED PLIES AND PREPARED DAMAGED AREA FOR REPAIR AT PANEL 644EB AS PER B737-700 SRM 51-70-04-2R-0; [02] VERIFIED STEP 1; OK TO INSTALL REPAIR; [03] REPAIRED DAMAGED AREA AT PANEL 644EB AS PER B737-700 SRM 51-70-04-2R-0; [04] VERIFIED STEP 3; [05] APPLIED TOPCOAT TO FLAP SUPPORT NO.8 PANEL 644EB LOWER SECTION IN REF B737-7 AMM 51-21-73-370-803.; [06] REMOVED DAMAGE; REPAIRED AND APPLIED TOPCOAT TO FLAP SUPPORT #8 PANEL 644EB IN REF B737-7 SRM 51-70-04-2R-0; AND 51-21-73-370-803.; [07] STEPS 5/6

Part: NONE — CRACKED (CENTER WING) · airframe 68,452 hrs · 40,246 cycles

LOWER FUSELAGE CENTER WING L/H AIR CONDITIONING EXHAUST AIR EXIT SEAL RETAINER CRACKED @ INB. SIDE ;STA 663.75 MKD DOT ; / [01] REMOVED PREVIOUS REPAIR FOR ACCESS AT LOWER FUSELAGE CENTER WING L/H AIR CONDITIONING EXHAUST. PER SRM 51-40-02-0G-0; [02] REMOVED SEAL RETAINER AND DOUBLER PER B737-700 SRM 51-40-02-0G-0; [03] LOCATED AND DRILLED EXISTING FASTENERS HOLES TO DOUBLER PER B 737-700 SRM 51-40-05-0G-0; [04] VERIFIED 1 TO 3. OK TO INSTALL SEAL RETAINER; [05] OK TO INSTALL SEAL'S RETAINER DOBLER AND SEAL; [06] INSTALLED SEAL'S RETAINER DOUBLER; SEAL RETAINER AND SEAL PER B 737-700 SRM 51-40-02-0G-0; [07] VERIFIED 6; [08] REINSTALLED REPAIR PREVIOUSLY REMOVED ON STEP 1 PER SRM 57-10-10-2R-2 REPAIR 2 PARAGRAPH 6 TABLE 215; [09] REMOVED PREVIOUS REPAIR FOR ACCESS AT LOWER FUSELAGE CENTER WING L/H AIR CONDITIONING EXHAUST PER SRM 57-10-10-2R-2; [10] VERIFIED STEP 8. STEP 9 IS ONLY CORRECT REFERENCE FOR STEP 1

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

FWD CARGO FLOOR. SUPPORT RIGHT AT STRINGER 25 IS CORRODED.<REMOVED CORROSION ORIGINAL MATERIAL 0.032'; MATERIAL REMOVED 0.006' MATERIAL REMAINING 0.026' FOUND OUT OF LIMITS AS PER REF B737-700 SRM 53-30-52-0I-1 TOOL USED B/C 173805 CAL DUE 3/10/2022 CORRECTION STEP #1 REF: SRM 53-30-15-1A-1 REPLACED WITH NEW SHIELD P/N 143A8126-31 INSTALLATION WILL BE ACCOMPLISH ON TTG8Q004DPUJ VERIFIED 1 ; 2 & 3 ( SUPPORT REPLACED )

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

AFT CARGO FLOOR SUPPORT STRINGER HAS CORROSION AROUND NUT PLATES AND EDGES B/S 787-807 RIGHT. BL 13' ; / [01] REMOVED CORROSION AT AFT CARGO FLOOR RAIL STA 787-807 RBL 13 AS PER B737-700 SRM 51-10-02-0G-0; [02] VERIFIED STEP 1;[14] INSTALLED NEW TRACK AND REPAIR SPLICES AS PER B737-700 SRM 51-40-02-0G-0 AND SRM 53-00-53-02R-3 REPAIR 3 FIG 203; [15] VERIFIED STEP 14; DAMAGED TIE DOWN TRACK (FLOOR SUPPORT STRINGER) WAS REPLACED. TASK COMPLETE.

Part: FITTING — CRACKED (L/H WING) · airframe 68,452 hrs · 40,246 cycles

L/W T/E REAR SPAR DEFLECTION CONTROL RIB PANEL VERTICAL SEAL FITTING CRACKED AT FASTENER TAIL I/B SIDE MKD DOT<REMOVED FITTING L/W T/E REAR SPAR DEFLECTION CONTROL RIB REF. B737-700 SRM 51-40-02-OG-0 LOCATED N DRILLED FITTING REF. B737-700 SRM 51-40-05-OG-O VERIFIED 1 & 2. OK TO INSTALL NEW FITTING INSTALLED NEW FITTING REF B737-700 SRM 51-40-02-OG-0 VERIFIED 4

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 68,452 hrs · 40,246 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO FLOOR SUPPORT 'Z' CHANNEL RIGHT SIDE HAS CORROSION AROUND NUT PLATES STRINGER 25R 727C-767. / REMOVED CORROSION ON AFT CARGO FLOOR SUPPORT 'Z' CHANNEL RHS STA 727C-767 AS PER B737-700 SRM 51-10-02-0G-0 VERIFIED STEP 1 PERFORMED UT THICKNESS INSP. ON REWORKED AREA @ AFT CARGO RIGHT Z CHANNEL STRINGER 25R 727C-767 IAW B737 NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS .039'. EQUIP: OLYMPUS 27MG CAL DUE 4/22 B/C 172139 ORIGINAL MAT .04' MAT REMAINING .039' AND MAT REMOVED .001' FOUND WITHIN LIMITS AS PER B737-700 SRM 53-00-53-1A-2 VERIFIED STEP 4 OK TO TREAT AND PRIME AREA TREATED AND PRIMED REWORKED AREA AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804 VERIFIED STEP 6. TASK COMPLETE

Part: RIB — CRACKED (VERT. STAB.) · airframe 68,452 hrs · 40,246 cycles

VERTICAL DORSAL FIN 321A FORWARDMOST RIB CRACKED ; / [01] REMOVED DORSAL FIN FWD RIB AS PER B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED HOLES ON NEW RIB AS PER B737-7 SRM 51-40-05-0G-0.; [03] VERIFIED STEP 1-2 . OK TO INSTALL NEW RIB; [04] INSTALLED FWD RIB ON DORSAL FIN AS PER B737-700 SRM 51-40-02-0G-0; [05] VERIFIED STEP 4

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

FWD CARGO COMPARTMENT L/H UPPER GUSSET CRACKED ; / [01] REMOVED AND REPLACED GUSSET PER B 737-700 SRM 51-40-02-0G-0; [02] VERIFIED 1

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

FWD CARGO COMPARTMENT R/H UPPER GUSSET CRACKED ; / [01] REMOVED AND REPLACED GUSSET PER B 737-700 SRM 51-40-02-0G-0; [02] VERIFIED 1

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

SUPPLEMENTAL INFORMATION: **CORROSION** L/H MAIN CABIN SEATTRACK LBL 45.50 STA 827+18 SPOT OF LIGTH CORROSION / REMOVED CORROSION ON LH MAIN CABIN SEAT TRACK LBL 45.5 STA 827+18 AS PER B737-700 SRM 51-10-02-0G-0 VERIFIED STEP 1 MAXIMUM CLEANUP DEPTH .012' FOUND WITHIN LIMITS AS PER B737-700 SRM 53-00-52-1A-1. VERIFIED STEP 3 OK TO PRIME AREA APPLIED PRIMER TO REWORKED AREA AS REQUIRED AS PER B737-700 SRM 53-00-52-1A-1. VERIFIED STEP 5

Part: SKIN — CRACKED (R/H HORIZ. STAB.) · airframe 68,452 hrs · 40,246 cycles

RH HOR. STAB LE SKIN 341B RIB AT ABOUT LE STA 86 CRACKED ; / [01] REMOVED #2 RIB FROM RT HORIZONTAL STAB L/E PANEL AS PER B737-700 SRM 51-40-02-0G-0; [02] REMOVED RH HOR. STA LE SKIN 341B RIB AT ABOUT LE STA 86 AS PER B737-700 SRM 51-40-02-0G-0; [03] DRILLED NEW RIB AS PER B737-700 SRM 51-40-05-0G-0. FIG. 3; [04] VERIFIED STEPS 1. 2. AND 3. OK TO TREAT AND PRIME HOLES; [05] TREATED AND PRIMED HOLES AS PER B737-700 AMM 51-21-41-370-803 AND 51-21-72-370-804; [06] VERIFIED STEP 5; OK TO INSTALL NEW RIB; [07] INSTALLED RH HOR. STA LE SKIN 341B RIB AT ABOUT LE STA 86 AS PER B737-700 SRM 51-40-02-0G-0; [08] VERIFIED STEP 7. TASK COMPLETE.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

FWD CABIN FLOOR PANEL 221BF AFT O/B CORNER CRACKED ; / [01] PREPARED FOR REPAIR AT FWD CABIN FLOOR PANEL 221 BF AS PER B 737-700 SRM 53-00-50 2R- 10; [02] VERIFIED STEP 1; OK TO REPAIR; [03] REPAIRED AT PANEL FWD CABIN FLOOR PANEL 221 BF AS PER B737-700 SRM 53-00-50-2R-10 MATERIAL USED PO .1713932 ;PO. 1715777 AND PO. 1150387; [04] REPAIRED AT PANEL FWD CABIN FLOOR 221 BF AS PER B737-700 53-00-50-2R-10 MATERIAL USED PO.1713932 ;PO.1715777 AND PO.1150387; [05] VERIFIED STEP 3 AND 4. TASK COMPLETE

Part: SKIN — CRACKED (R/H HORIZ. STAB.) · airframe 68,452 hrs · 40,246 cycles

RH HOR STAB L/E SKIN 341B RIB AT ABOUT LE STA 110 CRACKED ; / [01] REMOVED #4 RIB FROM RT HORIZONTAL STAB L/E AS PER B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW PART AS PER B737-700 SRM 51-40-05-0G-0; [03] VERIFIED STEPS 1 AND 2; OK TO TREAT AND PRIME HOLES; [04] TREATED AND PRIMED HOLES AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804; [05] VERIFIED STEP 4; OK TO INSTALL NEW PART; [06] INSTALLED NEW RH HOR STAB L/E SKIN 341B RIB AT ABOUT LE STA 110 IN REF B737-7 SRM 51-40-02-0G-0.; [07] VERIFIED STEP 6. TASK COMPLETE

Part: SKIN — CRACKED (R/H HORIZ. STAB.) · airframe 68,452 hrs · 40,246 cycles

RH HOR STAB L/E SKIN 341B RIB AT ABOUT LE STA 96 CRACKED ; / [01] REMOVED RT HORIZONTAL STAB #3 RIB AS PER B737-700 SRM 51-40-02-0G-0; [02] DRILLED NEW RIB AT RH HOR STAB L/E SKIN 341B AT ABOUT LE STA 96 AS PER B737-700 SRM 51-40-05-0G-0; [03] VERIFIED STEP 1-2. OK TO TREAT AND PRIMER; [04] TREATED AND PRIMED HOLES AS PER B737-700 AMM 51-21-41-370-803 AND 51-21-72-370-804; [05] VERIFIED STEP 4. OK TO INSTALL NEW RIB.; [06] INSTALLED NEW RIB AT RH HOR STAB L/E SKIN 341B AT ABOUT LE STA 96 AS PER B737-700 SRM 51-40-02-0G-0; [07] VERIFIED STEP 6. TASK COMPLETE.

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 68,452 hrs · 40,246 cycles

R/H HORIZONTAL STABILIZER RIB 4 AT STAB. STA-120.30; STIFFENER 4 CRACKED. ; / [01] REMOVED DAMAGE AT RH H.S RIB #4 STIFFENER #4 AS PER B737-7 SRM 51-10-02-0G-0;[12] INSTALLED REPAIR PARTS AS PER B737-700 SRM 51-40-02-0G-0 AND SRM 55-10-09-2R-4 REPAIR 4.; [13] APPLIED FILLET SEAL AROUND REPAIR PARTS AS PER B737-700 SOPM 20-50-19; [14] LATE ENTRY: MIXED SEALANT BMS 5-95 AT 23:00 10/19/2021; SQUEEZE OUT AND FASTENER INSTALLATION VERIFICATION DUE BY 01:00 10/20/2021; [15] LATE ENTRY: SEALANT SQUEEZE OUT VERIFICATION AND 100% PERMANENT FASTENER INSTALLATION ACCOMPLISHED PRIOR TO SQUEEZE OUT LIFE PER SOPM 20-50-19; [16] VERIFIED STEPS 12; 13; 14 AND 15. TASK COMPLETE

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 68,452 hrs · 40,246 cycles

R/H HORIZONTAL STABILIZER RIB 4 AT STAB. STA-120.30; STIFFENER 3 CRACKED. ; / [01] REMOVED DAMAGE AT RH H.S. RIB #4 STIFFENER #3 AS PER B737-7 SRM 51-10-02-0G-0.; [02] VERIFIED STEP 1.REQUIRED NDT; [03] PERFORMED HFEC INSP. ON RIB#4 STIFFENER #3 ON THE WEB IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACK REMAINED AND MARK<BR>TOOL: NORTEC 600 B/C: 16316 DUE: 10/08/22; [04] REMOVED CRACK AT RH H.S RIB WEB (STIFFENER #3) AS PER B737-7 SRM 51-10-02-0G-0; [05] VERIFIED STEP 3-4; [06] PERFORMED HFEC INSP. OF THE CUT EDGES ON RIB#4; STIFFENER #3 AND WEB IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. NO CRACKS NOTED <BR>TOOL: NORTEC 600 B/C: 16316 DUE: 10/08/22; [07] PERFORMED HFEC ROTO INSP. OF ALL EXISTING FASTENER HOLES WITHIN THE REPAIR AREA ON RIB#4; STIFFENER #4 IAW B737 NDT PART 6; 51-00-00; PROCEDURE 16. NO CRACKS NOTED <BR>TOOL: NORTEC 600 B/C: 16316 DUE: 10/08/22<BR>TOOL: OLYMPUS MINIMITE B/C: 160006 DUE: 01/18/22; [08] LOCATED AND DRILLED RIB AND REPAIR PARTS AS PER B737-700 SRM 51-40-05-0G-0; [09] VERIFIED STEP 8; OK TO TREAT AND PRIME HOLES; [10] TREATED AND PRIMED HOLES AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804; [11] VERIFIED STEP 10. OK TO INSTALL REPAIR PARTS; [12] INSTALLED REPAIR PARTS AS PER B737-700 SRM 51-40-02-0G-0 AND SRM 55-10-09-2R-4 REPAIR 4.; [13] APPLIED FILLET SEAL AROUND REPAIR PARTS AS PER B737-700 SOPM 20-50-19

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 68,452 hrs · 40,246 cycles

R/H HORIZONTAL STABILIZER RIB 4 AT STAB. STA-120.30; STIFFENER 2 CRACKED. ; / [01] REMOVED DAMAGE AT RH H.S. RIB #4 STIFFENER #2 AS PER B737-7 SRM 51-10-02-0G-0; [02] VERIFIED STEP1 . REQUIRED NDT; [03] PERFORMED HFEC INSP. ON RIB#4 STIFFENER #2 ON THE WEB IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACK REMAINED AND MARK<BR>TOOL: NORTEC 600 B/C: 16316 DUE: 10/08/22; [04] REMOVED CRACK AT RH H.S RIB WEB (STIFFENER #2) AS PER B737-7 SRM 51-10-02-0G-0; [05] VERIFIED STEP 3-4; [06] PERFORMED HFEC INSP. OF THE CUT EDGES ON RIB#4; STIFFENER #2 AND WEB IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. NO CRACKS NOTED <BR>TOOL: NORTEC 600 B/C: 16316 DUE: 10/08/22; [07] PERFORMED HFEC ROTO INSP. OF ALL EXISTING FASTENER HOLES WITHIN THE REPAIR AREA ON RIB#4; STIFFENER #2 IAW B737 NDT PART 6; 51-00-00; PROCEDURE 16. NO CRACKS NOTED <BR>TOOL: NORTEC 600 B/C: 16316 DUE: 10/08/22<BR>TOOL: OLYMPUS MINIMITE B/C: 160006 DUE: 01/18/22; [08] LOCATED AND DRILLED RIB AND REPAIR PARTS AS PER B737-700 SRM 51-40-05-0G-0; [09] VERIFIED STEP 8; OK TO TREAT AND PRIME HOLES; [10] TREATED AND PRIMED HOLES AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804; [11] VERIFIED STEP 10. OK TO INSTALL REPAIR PARTS; [12] INSTALLED REPAIR PARTS AS PER B737-700 SRM 51-40-02-0G-0 AND SRM 55-10-09-2R-4 REPAIR 4.; [13] APPLIED FILLET SEAL AROUND REPAIR PARTS AS PER B737-700 SRM 55-10-09-2R-4 REPAIR 4 AND SOPM 20-50-19

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

FWD CABIN FLOOR PANEL 231AF TOP LAYER DELAMINATED ; / [01] RECEIVED FLOOR PANEL 231AF P/N: 144A5810-163. REF TASK CARD TTG8Q0065LEU; [02] VERIFIED STEP 1.

Part: STUB FRAME — CRACKED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

FORWARD GALLEY DOOR (R1) AT FWD UPPER STUB FRAME HAS A CRACK ; / [01] LOCATED AND DRILL HOLE NEW STUB FRAME AS PER SRM 51-40-05-0G-0; [02] LATE ENTRY REMOVED UPPER STUB FRAME AS PER SRM 51-40-02-0G-0; [03] VERIFIED STEP 1 AND 2.<BR>OK TO TOP TREAT AND PRIME NEW HOLES.; [04] APPLIED ALODINE AND PRIMER AS PER SRM 51-20-01 AND AMM 51-21-72; [05] OK TO PAINT.; [06] PAINTED UPPER STUB FRAME AS PER AMM 51-21-72-370-804; [07] VERIFIED STEP 6. OK TO INSTALL STUB FRAME; [08] INSTALLED UPPER STUB FRAME AS PER SRM 53-10-01-2R-6 REPAIR 6; [09] VERIFIED STEP 8; [10] COMPLETED INSTALLATION UPPER STUD FRAME AS PER SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

MULTIPLE CRACKS EMANATING FROM FASTENER HOLE OPPOSITE FITTING LATCH (2 CRACKS) AND ALSO FROM THE FWD ADJOINING FASTENER HOLE (3 CRACKS). ; / [01] INSTALLED EWIS PROTECTION AS PER AMM 20-60-07-913-801; [02] APLIED STRIPPING FOR REMOVE PAINT REMOVED PAINT AND STRIPPING AND CLEAN AREA AS PER AMM 51-21-11-150-810; [35] DAMAGE REPAIRED PER EA 21-153-02897 (737-700 SRM 53-10-01-2R-6);REPETITIVE INSPECTION PROGRAM DEFINED IN EA 21-153-02897-INSP; [36] VERIFIED 33;34 & 35

Part: ACCESS PANEL — CRACKED (R/H WING) · airframe 68,452 hrs · 40,246 cycles

RIGHT WING LOWER LEADING EDGE ACCESS PANEL # 621CB UPPER CORNER CRACKED AND DELAMINATED ; / [01] REMOVED PLIES DAMAGE AND PREPARED FOR REPAIR AT PANEL 621CB AS PER B737-700 SRM 51-70-06-2R-6; [02] VERIFIED STEP 1; OK TO INSTALL REPAIR; [03] REPAIRED AT PANEL 621 CB AS PER B737-700-SRM 51-70-06-2R-6 MATERIAL USED PO 1731939 PO 1694548 AND PO 1726512; [04] VERIFIED TABLE MEASUREMENT; [05] VERIFIED STEP 3 AND 4

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

GROUND POWER DOOR INNER DOUBLER CRACKED/PIECE MISSING ; / [01] APPLIED PAINT STREPPER AS PER AMM 51-21-11-150-801-NG (PAINT STRIPPING - PERMANENT; [19] REMOVED AND REPLACED DOUBLER EGPR P/N 141A3722-12 AS PER SRM 51-40-02-0G-0 AND DWG 141A3702; [20] VERIFIED 18; [21] VERIFIED 19; [22] OK TO RESTORE EXTERNAL AREA; [23] TREATED;PRIMER AND TOP COAT EXTERNAL AREA AROUND EXTERNAL POWER RECEPTACLE AREA PER SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804 AND 51-21-73-370-803; [24] LATE ENTRY : NOTE STEP 8 ; VERIFIED SQUEEZE OUT TIME BEFORE 10/25/21 6:00 PM AS PER REF. DRAWING # 141A3702.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 68,452 hrs · 40,246 cycles

ITEM GOUND POWER DOOR INNER DOUBLER CRACKED/PIECE MISSING ; / [01] APPLIED PAINT STRIPPER AS PER AMM 51-21-11-150-801-NG (PAINT STRIPPING - PERMANENT); [02] PARTIALLY REMOVED FASTENERS AT AFFECTED AREA PER SRM 51-40-02-0G-0;[19] REMOVED AND REPLACED DOUBLER EGPR P/N 141A3722-12 AS PER SRM 51-40-02-0G-0 AND DWG 141A3702; [20] VERIFIED 18; [21] VERIFIED 19; [22] OK TO RESTORE EXTERNAL AREA; [23] TREATED;PRIMER AND TOP COAT EXTERNAL AREA AROUND EXTERNAL POWER RECEPTACLE AREA PER SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804 AND 51-21-73-370-803; [24] LATE ENTRY:NOTE STEP 8;VERIFIED SQUEEZE OUT TIME BEFORE 10/25/21 6:00 PM AS PER REF DWG#141A3702; [25] VERIFIED STEP 23

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 67,527 hrs · 39,679 cycles

STARBOARD OVERWING EMERGENCY EXIT LIGHT LENS COVER MISSING. / R&R LENS COVER PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,866 hrs · 39,260 cycles

EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACKS IAW AMM.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 66,640 hrs · 39,124 cycles

RT DOOR EMERGENCY EXIT SIGN COVER FELL OFF. SECURED LIGHT COVER PER SIP.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 66,493 hrs · 39,019 cycles

R/H EMERGENCY EXIT SIGN SIDE OVERWING DETACHED FROM WALL. R&R EMERGENCY EXIT LENS IAW SIP.

Part: HOLDER — OUT OF ADJUST (R1 GIRT BAR) · airframe 66,430 hrs · 38,976 cycles

R1 DOOR GIRT BAR HOLDER LOOSE. ADJUSTED GIRT BAR HOLDER PER AMM.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 65,715 hrs · 38,511 cycles

R/H WING #10 SPOILER DELAMINATED AT UPPER SURFACE 7" FROM TRAILING EDGE AND 2" FROM OUTBOARD EDGE. / R&R #10 FLIGHT SPOILER PER MM.

Part: COVER — MISSING (CABIN) · airframe 65,692 hrs · 38,496 cycles

RT OVERWING EMERGENCY EXIT SIGN LIGHT COVER MISSING. R&R COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,923 hrs · 38,038 cycles

FUSELAGE EXTERIOR EMERGENCY LIGHT LOCATED AFT OF R2 DOOR INOP. RELAMPED LIGHT PER AMM.

Part: FITTING — LOOSE (R2 DOOR) · airframe 63,987 hrs · 37,451 cycles

R2 DOOR FORWARD GIRT BAR FITTING LOOSE. SECURED FITTING IAW SOPM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,987 hrs · 37,451 cycles

LT BOTH OVERWING EMERGENCY ESCAPE GROUND LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,987 hrs · 37,451 cycles

LT EMERGENCY AISLE LIGHT INOP AT BS 640. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,987 hrs · 37,451 cycles

LT EMERGENCY AISLE LIGHT INOP AT BS 560. R&R BATTERY PACK PER AMM.

Part: SUPPORT BRACKET — CRACKED (AFT CARGO BAY) · airframe 63,987 hrs · 37,451 cycles

DURING OK TO CLOSE IN ACB; FOUND FWD BULKHEAD SUPPORT BRACKET CRACKED AT BS 727; RBL 3; WL 163 (MARKED) / REMOVED AND REPLACED ACB FWD BULKHEAD SUPPORT BRACKET AT BS 727 RBL 3 WL 163 I.A.W SRM 51-40-02 AND BOEING DWG # 144A2600

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,987 hrs · 37,451 cycles

***CORROSION*** FCB R/H FLOOR TO SIDEWALL SUPPORT CORRODED IN MULTIPLE AREAS BETWEEN BS 500A AND 500D RBL 22 / REMOVED AND REPLACED FCB R/H FLOOR TO SIDEWALL SUPPORT FROM BS 500A TO BS 500D RBL22 IAW DWG 143A7500 AND SRM 51-40-02

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 63,987 hrs · 37,451 cycles

REAR SPAR HORIZONTAL STIFFENER CRACKED AT BS 663, RBL 20. R&R STIFFENER PER SRM AND DWG.

Part: FORMER — CRACKED (WHEEL WELL RH) · airframe 63,987 hrs · 37,451 cycles

BS 663 RH FAIRING FORMER IS CRACKED (P/N 111A1203-6) / REPAIRED BS 663 RH FAIRING FORMER CRACKED PER ER 18-05338 REV IR AND EA 1-753-33654 REV IR

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 63,987 hrs · 37,451 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** NET ANCHOR PLATES FOR ACB CARGO NETS FWD OF DOOR ARE CORRODED / NO ALLOWABLE LIMITS IN SRM; REMOVED AND REPLACED NET ANCHOR PLATE FOR ACB FWD OF DOOR IAW SOPM 20-50-01

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 63,987 hrs · 37,451 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** NET ANCHOR PLATES FOR ACB CARGO NETS AFT OF DOOR ARE CORRODED / NO ALLOWABLE LIMITS IN SRM; REMOVED AND REPLACED NET ANCHOR PLATE FOR ACB AFT OF DOOR IAW SOPM 20-50-01

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,987 hrs · 37,451 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** ACB FLOOR SPLICE STRAP CORRODED IN MULTIPLE AREAS AT BS 727D+6 / REMOVED ACB FLOOR SPLICE STRAP AT BS 727D+6 IAW 737 SRM 51-40-02; FABRICATED REPLACEMENT FLOOR SPLICE STRAP IAW 737 51-40-05 & DWG #146A9401; FLOOR SPLICE STRAP WILL BE INSTALLED ON JPANEL-141-CLOSE CARD; 724036 FUSE 325 80570U 13NOV18

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 737 TO BS 787. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

AFT CARGO BAY RT SHIELD CORRODED BETWEEN BS 767 TO BS 787+6. R&R SHIELD IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED. R&R WEB IAW DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 947. R&R SUPPORT IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

AFT CARGO BAY FLOOR STRUCTURE CORRODED AT BS 767+6, RBL 14. REPAIRED FLOOR STRUCTURE IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D TO BS 767. R&R SUPPORT IAW SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,987 hrs · 37,451 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** ACB FLOOR SPLICE STRAP CORRODED IN MULTIPLE AREAS AT BS 767+6 / REMOVED ACB FLOOR SPLICE STRAP AT BS 767+6 IAW 737 SRM 51-40-02; FABRICATED REPLACEMENT FLOOR SPLICE STRAP IAW 737 SRM 51-40-05 & DWG #146A9401; FLOOR SPLICE STRAP WILL BE INSTALLED ON JPANEL-141-CLOSE CARD; 724036 FUSE 325 80570U 13NOV18

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

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

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

FORWARD CARGO BAY BILGE ON FLOOR TO SIDEWALL SUPPORT AFT "SHIELD" CORRODED BETWEEN BS 500 TO BS 500A, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 TO BS 500D, LBL 25. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

FORWARD CARGO BAY BILGE ON FLOOR TO SIDEWALL SUPPORT FORWARD "SHIELD" CORRODED BETWEEN BS 420 TO BS 440, RBL 22. R&R SUPPORT IAW DWG AND SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

AIR PHONE ANTENNA DOUBLER SKIN CORRODED BETWEEN BS 500A+9 TO BS 500A+16, BETWEEN RBL 3 TO LBL 3. R&R DOUBLER IAW DWG AND SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

FORWARD CARGO BAY BILGE ON AIR PHONE ANTENNA DOUBLER CORRODED AT BS 500+7, BL 0. R&R DOUBLER IAW DWG AND SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

FORWARD CARGO BAY BILGE ON STRINGER TO FRAME CLIP CORRODED AT BS 500B, RBL 6. R&R STRINGER CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

FORWARD SERVICE WAY SCUFF PLATE SUPPORT ANGLE CORRODED AT BS 312+13, RBL 59. R&R ANGLE IAW DWG AND SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

FORWARD ENTRY WAY SCUFF PLATE SUPPORT ANGLE CORRODED BETWEEN BS 312 TO BS 328, LBL 63. R&R ANGLE IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

L2 DOOR MOP SILL WEB CORRODED BETWEEN BS 1006 TO BS 1016, LBL 39. R&R WEB IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

CABIN FLOOR SUPPORT CRACKED AT BS 269+3, LBL 30. R&R SUPPORT IAW DWG AND SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

L1 DOOR MOP SILL CORRODED BETWEEN BS 294 TO BS 360, LBL 60. R&R MOP SILL IAW SRM AND DWG.

Part: MOUNT — CORRODED (CABIN) · airframe 63,987 hrs · 37,451 cycles

***CORROSION*** ON HARD POINT MOUNT AT STA 344 LBL 59 WL 208 / REMOVED AND INSTALLED NEW HARD POINT MOUNT AT STA 344; LBL 59; WL 208 ITEM #141A5220-2 IAW AIPC 53-42-00-29; SRM 51-40-02-0G-0

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 63,987 hrs · 37,451 cycles

RT VERTICAL PRESSURE WEB CRACKED AT BS 663, EXTERIOR SIDE OUTBOARD OF DRAIN VALVE AREA. REPAIRED WEB PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

BEAM CORRODED AT BS 986, BETWEEN LBL 43 TO RBL 43. REPAIRED BEAM PER EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

FORWARD ENTRY WAY SCUFF PLATE SUPPORT ANGLE CORRODED BETWEEN BS 312 TO BS 328, LBL 60. R&R ANGLE IAW SRM AND DWG.

Part: DRAIN — CORRODED (ASD THRESHOLD) · airframe 63,987 hrs · 37,451 cycles

***CORROSION*** MULTIPLE AREAS AT AFT SERVICE DOOR MOP SILL / MULTIPLE CORROSION AREAS AT ASD MOPSILL FROM BS947 TO 987 FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS IAW SRM 53-70-15-1A-1. REMOVED AND REPLACED NEW ASD MOPSILL PN# 147A8540118: PO#703038 IAW SRM 51-40-02 AND IAW DWG# 147A8501

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 13. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 277+8, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

R2 DOOR MOP SILL WEB CORRODED AT BS 1006, RBL 40. R&R WEB IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,987 hrs · 37,451 cycles

CRACK ON CABIN FLOOR SUPPORT INTERCOSTAL AT STA 312+10 LBL 45 / REMOVED AND REPLACED CABIN FLOOR SUPPORT INTERCOSTAL FROM BS 312 TO BS 328 LBL45; P/N 141A5410-12. IAW SRM 51-20-01-0G-0 AND DWG 141A5400

Part: DOOR SILL — CORRODED (L2 DOOR) · airframe 63,987 hrs · 37,451 cycles

L2 DOOR MOP SILL CORRODED BETWEEN BS 947 TO BS 986, WL 208. REPAIRED MOP SILL PER SRM AND DWG.

Part: BRACKET — CORRODED (FED THRESHOLD) · airframe 63,987 hrs · 37,451 cycles

***CORROSION*** ON FWD ENTRY DOOR SURROUND JUST FORWARD OF THE LOWER FORWARD DOOR LATCH ON THE FORWARD EDGE OF A BRACKET AT STA 303.9+3 WL191 STR 15 (MARKED) / REMOVED; FABRICATED; & INSTALLED NEW FWD ENTRY DOOR BRACKET AT STATION 303. 9+3 WL 191. STR 15. PER SRM 51-40-02-0G-0; SRM 51-40-05; & DRAWING 141A8180 & PNG 141A8185.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 328+8, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

R1 DOOR MOP SILL CORRODED BETWEEN BS 291.5 TO BS 360. R&R MOP SILL IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 63,987 hrs · 37,451 cycles

ACB AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED ACB AFT CORNER SCUFF PLATE IAW EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 63,987 hrs · 37,451 cycles

FCB AFT SCUFF PLATE IS CRACKED / REPAIRED FCB AFT SCUFF PLATE IAW EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 63,987 hrs · 37,451 cycles

FCB FWD SCUFF PLATE IS CRACKED / REPAIRED FCB FWD SCUFT PLATE IAW EA 1-A53-2076 REV 11

Part: FLOOR PANEL — BROKEN (AFT CABIN) · airframe 63,987 hrs · 37,451 cycles

AFT CABIN FLOOR PANEL 242XF IS BROKEN / DUE TO THE EXTENT OF DAMAGE REPLACED AFT CABIN FLOOR PANEL 242XF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 220. 57066U 10/22/18

Part: FLOOR PANEL — BROKEN (AFT CABIN) · airframe 63,987 hrs · 37,451 cycles

AFT CABIN FLOOR PANEL 242SF AFT O/B CORNER BROKEN / DUE TO THE EXTENT OF DAMAGE TO THE AFT O/B CORNER; REPLACED AFT CABIN FLOOR PANEL 242SF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 17. 57066U 10/23/18

Part: FORMER — CRACKED (RT WING) · airframe 63,987 hrs · 37,451 cycles

RT WING FIXED LEADING EDGE INBOARD FAIRING SUPPORT FORMER CRACKED ON UPPER END. REPAIRED FORMER IAW SRM & DWG.

Part: WEB — CRACKED (LT WING) · airframe 63,987 hrs · 37,451 cycles

LT WING TRAILING EDGE UPPER PANEL ABOVE PYLON AFT TIP TRANSVERSE WEB CRACKED ON OUTBOARD UPPER FLANGE. R&R TRANSVERSE WEB IAW SRM & DWG.

Part: SUPPORT — CRACKED (LEFT WING) · airframe 63,987 hrs · 37,451 cycles

LT WING BULB SEAL SUPPORT ABOVE #1 PYLON AFT TIP IS CRACKED / REMOVED & REPLACED SEAL SUPPORT IAW SRM 51-40-02 & IPC 57-50-00-25

Part: WEB — CRACKED (RIGHT WING) · airframe 63,987 hrs · 37,451 cycles

RT WING UPPER T/E PANEL ABOVE PYLON AFT TIP LOWER BULB SEAL SUPPORT WEB IS CRACKED ON FWD FLANGE / REMOVED & REPLACED BULB SEAL SUPPORT WEB IAW SRM 51-40-02 & IPC 57-50-00-25; RH WING UPPER T/E PANEL ABOVE PYLON AFT TIP

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,987 hrs · 37,451 cycles

R1 DOOR NR 4 LOWER BEAM CRACKED ON THE INBOARD SIDE AT THE RADIUS COMMON TO THE FORWARD MOST ATTACH POINT FOR THE HANDLE BOX ASSEMBLY. R&R BEAM PER AMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,987 hrs · 37,451 cycles

UPPER SUPPORT ANGLE CRACKED AT BS 663, LBL 10. REPAIRED ANGLE PER EA AND ER.

Part: BEAM — CRACKED (FSD) · airframe 63,987 hrs · 37,451 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #5 (UPPER) BEAM TO BE CRACKED ON THE INBD SIDE AT THE RADIUS COMMON TO THE FORWARD MOST ATTACH POINT FOR THE HANDLE BOX ASSEMBLY. / FORWARD SERVICE DOOR #5 (UPPER) BEAM WAS REMOVED & REPLACED ON WORK ORDER: 510516. INSTALL WILL BE ACCOMPLISHED ON CUSTOMER CARD: 14079 (SF DOOR INSTALLATION.) 89931U 08NOV18

Part: SKIN — CRACKED (LE SLAT) · airframe 63,987 hrs · 37,451 cycles

LT WING NR 3 SLAT SKIN CRACKED AT LOWER SURFACE OF SLAT NOSE SKIN AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 62,238 hrs · 36,333 cycles

L1 DOOR EMERGENCY GROUND ILLUMINATION LIGHT INOP. R&R CHARGER PER AMM.

Part: RETAINER SEAL — CRACKED (LT WING) · airframe 62,238 hrs · 36,333 cycles

AFT FIXED T/E SEAL RETAINER ANGLE CRACKED JUST I/B OF FLAP PROGRAMING TRACK / R/R ANGLE IAW SRM 51-40-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,238 hrs · 36,333 cycles

L1 DOOR EMERGENCY GROUND ILLUMINATION LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: FAIRING — ELONGATED (RT WHEEL WELL) · airframe 62,229 hrs · 36,327 cycles

RIGHT MAIN WHEEL WELL LOWER FAIRING PANEL 193 AR HAS PULLED FASTENERS / E41398-BRADSHAW; GARY - 04/12/2018 04:31 WIP: REPAIRED FASTENER HOLES PER S.RM. 51-70-04 -2R-9. REINSTALLED THE PANEL PER THE SRM 51-40-02.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 61,287 hrs · 35,698 cycles

R2 DOOR ESCAPE SLIDE LOOSE. SECURED SLIDE PER MM.

Part: PANEL — DELAMINATED (RT WING) · airframe 61,177 hrs · 35,624 cycles

#2 ENGINE INBOARD PYLON HAS DELAMINATED AREA JUST AFT OF PANEL 444 AL; AT APPROX. NAC STA. 314. FOUND DELAM. AREA TO MEASURE 2.25' LONG BY 1.75' WIDE MOD / REMOVED #2 ENG. AFT I/B PYLON PANEL 444BL IAW SRM 51-40-02-0G-0 FIG 10 & 11 56586C 22OCT18 INSTALLED #2 ENG. AFT I/B PYLON PANEL 444BL IAW SRM 51-40-02-0G-0 STEP 7. IPC 54-52-06-02 ITEM 210

Part: SIGN — BROKEN (CABIN) · airframe 60,483 hrs · 35,185 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. R&R SIGN IAW AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 60,465 hrs · 35,173 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE LOOSE. SECURED SLIDE FLAPS IAW MT.

Part: DOOR — CRACKED (ASD) · airframe 60,268 hrs · 35,033 cycles

AFT GALLEY SERVICE DOOR; LOWER PAN AFT ATTACH ANGLE IS CRACKED. / REMOVED AND REPLACED PAN ASSY. PER M/M 20-50-11.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 60,262 hrs · 35,029 cycles

RIGHT OVERWING EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 60,262 hrs · 35,029 cycles

LEFT OVERWING EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,262 hrs · 35,029 cycles

RT FORWARD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,121 hrs · 34,940 cycles

LEFT PASSENGER CABIN STOW BIN EMERGENCY LIGHT INOPERATIVE AT ROW 20. R & R THE BULB IAW AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 58,383 hrs · 33,893 cycles

RT OVERWING LOWER EMERGENCY EXIT SIGN LENS BROKEN. R&R LENS IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 58,321 hrs · 33,854 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE FROM CONTAINER. SECURED SLIDE ASSEMBLY PER AMM AND MT.

Part: ADIRU — FAULTY (E&E BAY) · airframe 58,105 hrs · 33,736 cycles

IRS ON DC ILLUMINATED. ELECTRICAL ODOR IN COCKPIT AND CABIN. R & R THE NR 1 AIR DATA INERTIAL REFERENCE UNIT IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 57,457 hrs · 33,360 cycles

AFT CABIN EMERGENCY EXIT HATCH SIGN BULB INOP. R&R BULB IAW AMM.

Part: STRIP — CRACKED (FUSELAGE) · airframe 57,453 hrs · 33,359 cycles

AFT CARGO COMPARTMENT FORWARD BULKHEAD PLATE STRIP CRACKED AT BS 727. R&R STRIP IAW SRM.

Part: SKIN — BROKEN (FUSELAGE) · airframe 57,453 hrs · 33,359 cycles

RT EMERGENCY EXIT HATCH DOOR CUTOUT BROKEN. R&R CUTOUT IAW SRM AND DWG.

Part: PANEL — CRACKED (BS 663) · airframe 57,453 hrs · 33,359 cycles

LEFT WHEEL WELL FORWARD BULKHEAD FIBERGLASS PANEL CRACKED AT BS 663. REPAIRED THE PANEL IAW EA.

Part: PANEL — CRACKED (RT MLG WW) · airframe 57,453 hrs · 33,359 cycles

RIGHT WHEEL WELL FORWARD BULKHEAD FIBERGLASS PANEL CRACKED AT BS 663. REPAIRED PANEL IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,453 hrs · 33,359 cycles

AFT CARGO COMPARTMENT FRAME LOWER WEB CRACKED AT BS 727, WL 200 LT SIDE. REPAIRED WEB IAW EA.

Part: LIGHT — CRAZED (CABIN) · airframe 57,453 hrs · 33,359 cycles

FLOOR EMERGENCY LIGHT STRIP CRAZED. R & R THE LIGHT STRIP IAW DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 56,099 hrs · 32,581 cycles

AFT CARGO FWD CORNER THRESHOLD PLATE CRACKED. REPAIRED PLATE IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,099 hrs · 32,581 cycles

SKIN DAMAGED AT BS 802, STRINGER 25R. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,055 hrs · 31,977 cycles

RIGHT OVERWING EXIT SIDEWALL LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 53,984 hrs · 31,357 cycles

M1673 EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 53,984 hrs · 31,357 cycles

M1672 EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,938 hrs · 31,324 cycles

RIGHT HORIZONTAL STABILIZER STATION 92.70 RIB, 30" CRACKED AT LOWER CHORD, 20" AWAY FROM FRONT SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,938 hrs · 31,324 cycles

RIGHT HORIZONTAL STABILIZER STAB STATION 92.70, RIB 2.0", CRACKED ON THE WEB, 28.00" FROM LOWER FRONT SPAR. REPAIRED STABILIZER IAW SRM & EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,938 hrs · 31,324 cycles

FLIGHT DECK RT NR 3 WINDOW FRAME, CRACKED AT SECOND LOWER FASTENER HOLE. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,938 hrs · 31,324 cycles

FLIGHT DECK LT NR 3 WINDOW FRAME CRACKED AT SECOND LOWER FASTENER HOLE. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,938 hrs · 31,324 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME, CRACKED AT UPPER RT CORNER. REPAIRED FRAME IAW ACO.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 53,938 hrs · 31,324 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, LBL 40.75. REPAIRED WEB IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 53,899 hrs · 31,298 cycles

CENTER AISLE OVERWING EMER EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 52,842 hrs · 30,708 cycles

RIGHT EMER EXIT SIGN LENS MISSING AT ROW 12. R & R LENS IAW MM.

Part: COVER — MISSING (L2 DOOR) · airframe 52,601 hrs · 30,585 cycles

L2 DOOR EMER EVAC SLIDE MANUAL RELEASE HANDLE COVER MISSING. INSTALLED COVER IAW MT.

Part: LIGHT — WORN (CABIN) · airframe 49,442 hrs · 28,760 cycles

RIGHT FWD EEPLS WORN. R & R EEPLS IAW MM.

Part: LENS — DAMAGED (CABIN) · airframe 49,211 hrs · 28,615 cycles

RIGHT EMERGENCY EXIT LIGHT LENS DAMAGED. R & R LENS IAW MM.

Part: HMU — FAULTY (NR 2 ENGINE) · airframe 47,725 hrs · 27,782 cycles

AIR TURN BACK CLIMBING FROM 12000 TO 15000 NR 2 ENG STARTING SURGING FROM 62% N1 TO 79% N1 WITH AUTO THROTTLES ENGAGED INITIALLY. SURGE CONTINUED WITH AUTO THROTTLES OFF. R & R NR 2 ENG HMU & FUEL PUMP PACKAGE IAW MT.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 47,692 hrs · 27,758 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 47,150 hrs · 27,453 cycles

LT AFT NR 5 LED ON EMERGENCY EXIT DOOR SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: FSEU — FAULTY (TE FLAP) · airframe 45,159 hrs · 26,284 cycles

DECLARED EMERGENCY, FLAPS WOULD NOT MOVE WITH NORMAL METHOD. REMOVED AND REPLACED FSEU PER MM.

Part: LENS — BROKEN (CABIN) · airframe 44,692 hrs · 25,998 cycles

EMERGENCY EXIT LENSE COVER BROKEN IN AFT GALLEY. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY & COVER IAW AMM IN AFT GALLEY BY R2 DOOR OPS CHECKS GOOD.

Part: SIGN — BROKEN (CABIN) · airframe 44,280 hrs · 25,728 cycles

F/O'S SIDE AFT EMERGENCY EXIT LIGHT IN AFT GALLEY COVER BROKEN. REMOVED AND REPLACED AFT EMERGENCY EXIT SIGN NEXT TO AFT SERVICE COVER PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 44,022 hrs · 25,558 cycles

LEFT AFT WINDSCREEN AFT OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT IAW AMM.

Part: PANEL — CRACKED (LT MLG WW) · airframe 44,022 hrs · 25,558 cycles

LEFT WHEEL WELL FWD VAPOR BARRRIER FIBERGLASS PANEL CRACKED 7" LONG. VERIFIED REPAIR MATERIAL AS BMS 8-2R. FABRICATED REPAIR PATCH FOR FRONT & AFT OF 663 BULKHEAD IAW EA 1-53-3376. INSTALLED REPAIR PATCH IAW EA 1-A53-3376.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

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

Part: INTERCOSTAL — CRACKED (NR 1 FAN COWL) · airframe 44,022 hrs · 25,558 cycles

NR 1 ENGINE INBOARD FAN COWL ENGINE OIL ACCESS DOOR CUTOUT INTERNAL SHIELD INTERCOSTAL CRACKED. REPLACED INTERNAL SHIELD INTERCOSTAL ON NR 1 ENGINE INBOARD FAN COWL IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

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

Part: TERMINAL BLOCK — CORRODED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

CABIN STA 400 BELOW STR 6R, FRAME MOUNTED TERMINAL BLOCK, CORRODED. TERMINAL BLOCK NOT IN USE. REMOVED CORRODED TERMINAL BLOCK AND LOCATED, DRILLED AND INSTALLED NEW TERMINAL BLOCK AT STA 400 STR 6R IAW SRM 51-40-02-0G-0.

Part: TERMINAL BLOCK — CORRODED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

CABIN STA 559 ABOVE STR 7L, FRAME MOUNTED TERMINAL BLOCK CORROSION. REMOVED CORRODED TERMINAL BLOCK THEN LOCATED DRILLED AND INSTALLED NEW TERMINAL BLOCK AT STA 559 STR 7L IAW SRM 51-40-02-0G-0.

Part: FAIRING — CRACKED (FLAP TRACK) · airframe 44,022 hrs · 25,558 cycles

LEFT WING FLAP TRACK FAIRING 544AB FWD EDGE CRACKED. REPAIRED FAIRING IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

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

Part: STRAP — CORRODED (CARGO DOOR) · airframe 44,022 hrs · 25,558 cycles

AFT CARGO COMPARTMENT DOOR INBOARD REINFORCING STRAP CORRODED. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

FORWARD CARGO DOOR LOWER THRESHOLD CORRODED BETWEEN STA 455 TO STA 478. REMOVED AND REPLACED THRESHOLD IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

STRINGER CLIP CORRODED AT BS 727E, STR 6R. REMOVED AND REPLACED CLIP IAW SRM.

Part: FLAP — PUNCTURED (LT WING) · airframe 44,022 hrs · 25,558 cycles

LEFT WING INBOARD AFT FLAP PUNCTURED FWD OF T/E. REPAIRED OF AFT FLAP IAW SRM & MM.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 44,022 hrs · 25,558 cycles

LEFT HORIZONTAL STABILIZER, LOWER, LEADING EDGE, SLIDING SEAL CRACKED. REMOVED AND REPLACED SLIDING SEAL AT LEFT HORIZONTAL STABILIZER, LOWER, LEADING EDGE IAW AMM 53-31-31-400-801.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

LEFT CREASE BEAM INNER CHORD CORRODED AT BS 706 + 7. REMOVED AND REPLACED CREASE BEAM IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

FRAME CORRODED AT BS 360, STR 4L. REMOVED AND REPLACED FRAME IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

RIGHT CREASE BEAM INNER CHORD CORRODED BETWEEN BS 955 TO BS 982, RBL 48. REPAIRED BEAM IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 44,022 hrs · 25,558 cycles

L1 DOOR CREASE BEAM CORRODED BETWEEN BS 312 TO BS 344. REMOVED AND REPLACED ANGLE IAW AND DWG.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 44,022 hrs · 25,558 cycles

CRACK ON HORIZONTAL STIFFENER FWD SIDE OF WHEEL WELL BULKHEAD STA 663 AND LEFT OF AC BAY. REMOVED AND REPLACED STIFFENER IAW SRM AND BOEING DWG.

Part: FAIRING — CRACKED (RT WING) · airframe 44,022 hrs · 25,558 cycles

RIGHT WING NR 6 AFT FAIRING ATTACH HOLE NR 16, HAS A 2" LONG CRACK. RIGHT WING NR 6 AFT FAIRING ATTACH HOLE NR 16 HAS A 2" LONG CRACK. REPAIRED IAW EA 121187 IR AND EA 1-757-7611.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 42,529 hrs · 24,646 cycles

R2 DOOR EMERGENCY EXIT SIGN FELL OFF. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,642 hrs · 24,131 cycles

LEFT EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: COVER — BROKEN (CABIN) · airframe 41,202 hrs · 23,877 cycles

AFT SERVICE DOOR FLOOR LEVEL EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,567 hrs · 23,507 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 40,531 hrs · 23,486 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 40,531 hrs · 23,486 cycles

DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 40,034 hrs · 23,189 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,566 hrs · 22,917 cycles

LT EEPLS LOOSE AT ROW 7. SECURED EEPLS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 36,831 hrs · 21,383 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT GALLEY NR 4 EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,831 hrs · 21,383 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING NR 7 SLAT CRACKED. REPAIRED SLAT SKIN PER EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,831 hrs · 21,383 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 15.04. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,831 hrs · 21,383 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 6.14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,831 hrs · 21,383 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 32-40. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,831 hrs · 21,383 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, RBL 15.04. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,831 hrs · 21,383 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 40.87. REMOVED AND REPLACED FITTING PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 36,394 hrs · 21,128 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MT.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 36,394 hrs · 21,128 cycles

L1 DOOR EMERGENCY EVAC SLIDE DISLODGED. RE-INSTALLED SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,794 hrs · 20,759 cycles

DURING SCHEDULED MV1 CHECK, LT FWD EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,327 hrs · 20,488 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,327 hrs · 20,488 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: LIGHT — BURNED (CABIN) · airframe 34,265 hrs · 19,860 cycles

DECLARED EMERGENCY - INFLIGHT, SMELL OF SMOKE NOTED AT LT OVERWING. VISIBLE SMOKE ALSO NOTED BUT DISSIPATED AFTER A FEW MINUTES. FOUND READING LIGHT AT 11A VISIBLY BURNED. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 33,627 hrs · 19,461 cycles

EEPLS LOOSE AT ROW 8 ABC. SECURED EEPLS PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 33,607 hrs · 19,450 cycles

DURING SCHEDULED MV1 CK, FOUND R2 DOOR EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: SLAT — CRACKED (RT WING) · airframe 33,228 hrs · 19,219 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 SLAT CRACKED. REPAIRED SLAT PER ER.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 18,236 hrs · 31,555 cycles

IN FLT ENG SHUT DOWN / AIR TURNBACK. NR 1 ENG COMPRESSOR STALL WITH VIBRATION FELT. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 31,142 hrs · 17,982 cycles

DURING SCHEDULED HC2 CHECK, BOTH OVERWING EXIT LIGHTS BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,172 hrs · 17,411 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SUB FRAME CRACKED AT BS 294, STR 17R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,172 hrs · 17,411 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 38 TO RBL 5. REPAIRED BEAM PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 29,019 hrs · 16,704 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 29,019 hrs · 16,704 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: GASPER FAN — MALFUNCTIONED (CABIN) · airframe 28,219 hrs · 16,207 cycles

AT FL 330 A STRONG ELECTRICAL SMELL BEGAN IN CABIN AND THEN ODOR ENTERED FLIGHT DECK. TURNED OFF RT PACK, GASPER AND RECIRC SWITCHES, SMELL DISSIPATED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 27,796 hrs · 15,944 cycles

DURING SCHEDULED CV CHECK, FOUND AFT PRESSURE BULKHEAD OIL CANNED AT BS 1016, STR 2R TO STR 3R. REPAIRED BULKHEAD PER SWA EA.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 27,796 hrs · 15,944 cycles

DURING SCHEDULED CV CHECK, FOUND AFT PRESSURE BULKHEAD OIL CANNED AT BS 1016, STR 3L TO STR 4L. REPAIRED BULKHEAD PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,753 hrs · 15,308 cycles

DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 26,593 hrs · 15,198 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 24,192 hrs · 13,824 cycles

L1 DOOR EVACUATION SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 24,167 hrs · 13,808 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SEAL — TORN (RT ENGINE) · airframe 18,375 hrs · 10,463 cycles

AIR TURNBACK, INFLIGHT SHUTDOWN, DECLARED EMERGENCY. NR 2 ENGINE FLAMED OUT. FOUND TORN FUEL PUMP SEAL CAUSING FUEL LEAK. REMOVED AND REPLACED SEAL PER MM.

Part: FLOOR SUPPORT — CORRODED (BS 771-773) · airframe 18,374 hrs · 10,461 cycles

DURING SCHEDULED 5Y CHECK, FOUND FLOOR SUPPORT CORRODED BETWEEN BS 771 TO BS 773, LBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (BS 771-773) · airframe 18,374 hrs · 10,461 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED BETWEEN BS 771 TO BS 773, LBL 17. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (BS 771-773) · airframe 18,374 hrs · 10,461 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 771 TO BS 773, LBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: FITTING — CHAFED (LT WING) · airframe 18,374 hrs · 10,461 cycles

DURING SCHEDULED 5Y CHECK, FOUND LT WING WALKING BEAM AFT LOWER HANGER FITTING CHAFED. REPAIRED FITTING PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (BS 771-773) · airframe 18,374 hrs · 10,461 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 771 TO BS 773, RBL 8. REPAIRED FLOOR SUPPORT PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (BS 771-773) · airframe 18,374 hrs · 10,461 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 771 TO BS 773, RBL 14. REPAIRED FLOOR SUPPORT PER SWA EA.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 16,860 hrs · 9,640 cycles

DURING SCHEDULED RON CHECK, C/W BOROSCOPE INSPECTION OF NR 2 ENGINE AND FOUND 1 EA NR 3 HPC BLADE OUT OF LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,964 hrs · 7,986 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS LIGHTS INOP. REMOVED AND REPLACED LIGHT MODULE PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 10,384 hrs · 5,992 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS COVER MISSING AT ROW NR 20. REMOVED AND REPLACED EEPLS LIGHT ASSY AT ROW NR 20 PER MM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 10,310 hrs · 5,953 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 4,484 hrs · 2,675 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LENS MISSING. INSTALLED LENS PER MM.