N969WN

Part: HANDLE — LOOSE (ZONE 800) · airframe 44,610 hrs · 27,481 cycles

FWD GALLEY RIGHT HAND SIDE DOOR ASSIST GRAB HANDLE LOOSE<[01] SECURED FWD GALLEY R/H SIDE ASSIST HANDLE REF AMM 25-21-35

Part: PLATE — CRACKED (ZONE 500) · airframe 44,193 hrs · 27,201 cycles

LEFT WING AFT SPAR AREA WAFFLE PLATE JUST OTBD OF PANEL 551DB, CRACKED AT FASTENER. DRILLED AND REMOVED CRACKED WAFFLE PLATE IAW SRM 51-40-02-0G-0. INSTALLED NEW WAFFLE PLATE IAW SRM 51-40-02-0G-0, PART 115A2781-3.

Part: PLATE — CRACKED (ZONE 600) · airframe 44,193 hrs · 27,201 cycles

RIGHT WING AFT SPAR AREA WAFFLE PLATE JUST OTBD OF PANEL 651DB, CRACKED AT FASTENER. DRILLED AND REMOVED CRACKED WAFFLE PLATE AT RT WING OTBD OF 651BB IAW SRM 51-40-02-0G-0, LOCATED AND DRILLED ALL FASTENER HOLES INTO NEW RT WAFFLE PLATE IAW SRM51-40-02-0G-0. INSTALLED NEW WAFFLE PLATE IAW SRM 51-40-02-0G-0.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 44,193 hrs · 27,201 cycles

BS 295; ABOVE STR 8R; STUB FRAME ABOVE R1 DOOR SEAL DEPRESSOR CRACKED. REMOVED DAMAGE PART; LOCATED; DRILL AND INSTALLED NEW PART I.A.W. SRM 51-40-02-0G-0 AND IAW AMM 51-21-73-701 DWG 141A8370 REV D, SRM 51-40-05-0G-0,

Part: SEAT TRACK — WORN (ZONE 200) · airframe 44,193 hrs · 27,201 cycles

CABIN SEAT TRACK WORN ON UPPER CROWN AT STA 520 LBL 45 WL 208. REMOVED THE SEAT TRACK AT BS 500C+10.5' TO 520 IAW. SRM 51-40-02-0G-0, LOCATED AN DRILLED NEW SEAT TRACK IAW SRM 53-00-52-2R-4 REPAIR 4; INSTALLED NEW SEAT TRACK IAW SRM 53-00-52-2R-4, REPAIR 4, AND DWG 53210001 REV C. APPLIED CIC TO AREA IAW 53-00-52-2R-4, REPAIR 4, STEP 4.

Part: SEAL — CRACKED (ZONE 300) · airframe 44,193 hrs · 27,201 cycles

LEFT LOWER HORIZONTAL STAB PANEL 333AB SEAL PLATE CRACKED. REPLACED LT LOWER HORIZONTAL STAB PANEL 333AB SEAL PLATE IAW AMM 51-40-02-0G-0, STEP 4.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 44,193 hrs · 27,201 cycles

FLOOR PANEL 241BF HAS UPPER SURFACE DENTS AND PULLED FIBERS. REPAIRED FLOOR PANEL 241BF UPPER SURFACE IAW SRM 53-00-50-2R-2, SRM 53-00-50-2R-0, REPAIR GENERAL AND EA M-25-153-02385.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 44,193 hrs · 27,201 cycles

FLOOR PANEL 242AF HAS UPPER SURFACE DENTED AND PULLED FIBERS. REPAIRED THE FLOOR PANEL 242AF UPPER SURFACE IAW SRM 53-00-50-2R-2; SRM 53-00-50-2R-0, REPAIR GENERAL, AND EA M 25-153-02385.

Part: FLOOR PANEL — DENTED (ZONE 100) · airframe 44,193 hrs · 27,201 cycles

FLOOR PANEL 241AF HAS UPPER SURFACE DENTS AND PULLED FIBERS. REPAIRED FLOOR PANEL 241AF UPPER SURFACE IAW SRM 53-00-50-2R-2; SRM 53-00-50-2R-0 REPAIR GENERAL AND EA M-25-153-02385.

Part: FLOOR PANEL — PULLED (ZN 200 FUS TOP) · airframe 44,193 hrs · 27,201 cycles

FLOOR PANEL 242BF HAS UPPER SURFACE DENTED AND PULLED FIBERS. REPAIRED FLOOR PANEL 242BF UPPER SURFACE IAW SRM 53-00-50-2R-2, SRM 53-00-50-2R-0, REPAIR GENERAL, AND EA M 25-153-02385.

Part: SKIN — DELAMINATED (ZONE 500 FLAP) · airframe 43,688 hrs · 26,880 cycles

LEFT WING OB AFT FLAP LOWER FACE SHEET DELAMINATED AT IB TE 19.5' X 10'(PICS ATTACHED)<[01] R/R LEFT WING OUT BOARD AFT FLAP PER AMM 27-51-22

Part: SEAT BACK — OUT OF ADJUST (ZONE 200) · airframe 43,688 hrs · 26,880 cycles

PASSENGER SEAT 11D RECLINES INTO EMERGENCY EXIT ROW. ADJUSTED PASSENGER SEAT 11D RECLINE CABLE PER CMM 25-21-42.

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 43,688 hrs · 26,880 cycles

AFT CARGO FLOOR PANEL 140BF WORN,CRACKED AND PREVIOUSLY REPAIRED. REMOVED AND REPLACED PER AMM 25-52-10-401-NG (CARGO FLOOR PANEL - REMOVAL/INSTALLATION - PERMANENT). AFT CARGO FLOOR PANEL 140BF.

Part: NUT — STRIPPED (FIRE LOOP) · airframe 40,885 hrs · 25,185 cycles

WHEEL WELL FIRE LIGHT ON DURING CLIMB PART NUMBER 35460-3 NEEDED. PAR APP SUBMITTED DCN-042441<[01] OK TO CONT PER MEL 26-4-01 SP1 SP3;[02] UPON INSPECTION FOUND LH SIDE OF THE WHEEL WELL FIRE DETECTOR LOOP NOT SECURED AND THE NUT STRIPPED OUT. FIRE LOOP DETECTOR WILL NEED A NEW NUT AND LOOP TO SECURE PROPERLY. REF AMM 26-18-02. WHEEL WELL FIRE REMAINS ON MEL 26-4-01.

Part: FIRE LOOP — LOOSE (ZONE 100) · airframe 40,885 hrs · 25,185 cycles

WHEEL WELL FIRE LIGHT ON DURING CLIMB PART NUMBER 35460-3 NEEDED. PAR APP SUBMITTED DCN-042441. OK TO CONT PER MEL 26-4-01 SP1 SP3. UPON INSPECTION FOUND LH SIDE OF THE WHEEL WELL FIRE DETECTOR LOOP NOT SECURED AND THE NUT STRIPPED OUT. FIRE LOOP DETECTOR WILL NEED A NEW NUT AND LOOP TO SECURE PROPERLY. REF AMM 26-18-02. WHEEL WELL FIRE REMAINS ON MEL 26-4-01. TROUBLESHOT WHEEL WELL FIRE LIGHT ON. REF FIM 26-18 TASK 801. OPS NORMAL. NO DEFECTS NOTED.

Part: GIRT BAR — UNKNOWN (DOOR) · airframe 38,929 hrs · 23,923 cycles

L1 AND L2 GIRT BARS VERY HARD FOR FAS TO INSERT.<[01] INSPECTED BOTH L1 AND L2 GIRT BARS. ALL CHECKS GOOD. GIRT BARS OPERATE NORMALLY IAW AMM 25-66-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,759 hrs · 23,805 cycles

AFT ENTRY DOOR SLIDE LIGHT INOP<[01] RELAMPED AFT ENTRY DOOR SLIDE LIGHT REF AMM 33-51-04 OPS CHECK GOOD.

Part: SIGN — LOOSE (ZN 200 FUS TOP) · airframe 37,911 hrs · 23,305 cycles

OVERHEAD EXIT ROW EXIT SIGN HANGING BY WIRE<[01] SECURED O/H EXIT SIGN PER MM 33-51-01

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 37,838 hrs · 23,258 cycles

EXIT SIGN CENTER ISLE BROKEN<[01] RELAMPED EE LIGHT PER AMM 33-51-28

Part: LIGHT — LOOSE (ZN 200 FUS TOP) · airframe 37,821 hrs · 23,246 cycles

AFT ENTRY DOORWAY; EMERGENCY EXIT LIGHT COVER LOOSE<[01] REMOVED AND REPLACED DAMAGED AFT ENTRY DOORWAY; EMERGENCY EXIT LIGHT ASSY I.A.W. AMM 3-51-01-960-802 STEPS 3. C. (1) THRU (6) (A) THRU (E) TEST IS REQUIRE;[02] REMOVED; REPLACED AND PERFORMED GOOD TEST OF AFT ENTRY DOOR EMERGENCY LIGHT PER AMM 33-51-01-960-802;[03] VERIFIED CORRECTIVE ACTIONS AND MEASUREMENTS TABLE. CARD COMPLETE.

Part: COVER — LOOSE (ZN 200 FUS TOP) · airframe 37,821 hrs · 23,246 cycles

LH EMERGENCY EXIT DOOR EXIT LIGHT COVER LOOSE.<[01] UPON FURTHER INVESTIGATION; FOUND LIGHT LENS COVER TO HAVE LOWER RETAINING SCREW LOOSE. TIGHTENED LOWER RETAINING SCREW ON L/H EMERGENCY EXIT DOOR EXIT LIGHT LENS COVER IAW SOPM 20-50-01.;[02] COMPLETED MEASUREMENTS SECTION;[03] VERIFIED COMPLETE

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

CABIN FLOOR INTERCOSTAL CRACKED; BS 277 + 5; RBL 1; WL 208<[01] REMOVED AND REPLACED INTERCOSTAL BS277+5; RBL1; WL208<BR>IAW SRM 51-40-02 AND DWG 141A5400;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.

Part: SUPPORT ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLE AT STATIONS: 767; 767+6; 767+10; WL 156; LBL 22.<[01] THIS CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD NBR: TTG8Q00NPGFW;[02] VERIFIED APPLICABILITY PER SRM 53-60-53-0I-1 AND ALLOWABLE DAMAGE SRM 53-00-53-1A-2.<BR>REMOVED CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLE REWORKED AREAS FOUND MULTIPLES AREAS WITH MORE 50% OF LOSS MATERIAL BS 767+10 L=1.3' ; W=1.5' ; D= 0.032'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP A(2)(A) FIG 103<BR>TOOL USED:ATS2472<BR>DUE:12/31/23;[03] VERIFIED STEPS 1 AND 2; MEASUREMENT TABLE; CARD COMPLETE.

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

CORROSION ON AFT CARGO COMPARTMENT DOOR CUT-OUT SUB-THRESHOLD WEB FROM STA787+7 TO STA 787+14; RBL 20 TO RBL 28; WL 156; STA 787+15.5; RBL 26; STA 827+18; RBL 20; WL 156.<[01] REMOVED AND REPLACED SUB-THRESHOLD WEB <BR>BS794-BS847 RBL20 WL156 <BR>IAW SRM 51-40-02 & DWG146A8120;[02] VERIFIED. <BR>VERIFIED MEASUREMENTS.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLE AT: STA 727A+10; 727A+14; 727B; 727B+2; 727B+10; 727B+14; 727B+18; 727C; 727C+10; 727C+14; WL 156; RBL 22.<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00NPEX4;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

AFT CARGO BAY DOOR CUT-OUT FWD SHIELD IS CORRODED FROM STA 767+1 TO STA 767+19; RBL 20 TO 22; WL 156.<[01] REMOVED AND REPLACED ACB FWD SHIELD IAW SRM 51-40-02;[02] REMOVED AND REPLACED ACB FWD SHIELD IAW SRM 51-40-02 AND DWG # 146A0081;[03] VERIFIED MEASUREMENTS FIELDS AND CORRECTIVE ACTION 2. CARD COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT AT: STA727C+18; FROM STA727D+3 TO 727D+11; STA727D+14; STA727D+18; STA727E+2; STA727E+6; STA727E+ 18; STA747+5; STA747+10 WL156; RBL 22<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00NPEX4;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLE AT: STATIONS 727A+6; 727D+3; 727D+6; 727D+7.5; 727D+13; 727D+16; 727E; 727E+10; 727E+12;747+18; LBL 20-22; WL 156.<[01] REMOVED AND INSTALLED NEW AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT WL156 STA 727 -STA 847 LBL22 I.A.W SRM 51-40-0A-0G-0 AND DWG 146A7500;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT ANGLE AT: STA 747+14 AND STA 747+14; RBL 22; WL 156.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT RBL 22 WL156 STA 727 -STA 767 I.A.W SRM 51-40-0A-0G-0 AND DWG 146A7500.;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

FCB AFT CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED FCB AFT CORNER SCUFF PLATE. IAW SRM 53-30-15-2R-1<BR>THIS PART WILL BE INSTALLED ON TASK CARD NBR: TTG8Q00NFN78.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE

Part: CARGO TRACK — CORRODED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

FWD CARGO BAY HAS CORROSION ON RAIL AT BS 480+19; LBL 2; WL 156<[01] FWD CARGO BAY RAIL WAS REPAIRED PER REF SRM 53-00-53-1A-2;[02] VERIFIED COMPLETE

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

FWD CARGO BAY UPPER GUSSET IS CRACKED AT BS 500C+19; LBL 61; WL 194<[01] INSTALLED NEW FCB UPPER GUSSET BS 500C+19; LBL 61; WL 194 IAW SRM 51-40-02 AND DWG #143A7902;[02] REMOVED AND REPLACED FCB UPPER GUSSET BS 500C+19; LBL 61; WL 194 IAW SRM 51-40-02 AND DWG #143A7902;[03] VERIFIED COMPLETE RII STEP 3.;[04] VERIFIED COMPLETE STEP 4 AND MEASUREMENT TABLE; CARD COMPLETE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

FWD CABIN FLOOR PANEL 222DF HAS PULLED STRANDS ON UPPER SURFACE.<[01] FWD CABIN FLOOR PANEL 222DF HAD PULLED STRANDS ON UPPER SURFACE REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETE AND CURE SHEETS

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

FWD CARGO BAY UPPER GUSSET IS CRACKED AT BS 500C+19; RBL 61; WL 194<[01] REMOVED AND REPLACED FCB UPPER GUSSET BS 500C+19; RBL 61; WL 194 IAW SRM 51-40-02 AND DWG #143A7902;[02] VERIFIED COMPLETE RII STEP 3.;[03] VERIFIED COMPLETE STEP 4; CARD COMPLETE.

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 37,821 hrs · 23,246 cycles

LT HORIZ STAB GAP COVER 333AT BLADE SEAL IS CRACKED<[01] REMOVED AND REPLACED LT HORIZ STAB PANEL 333AT BLADE SEAL IAW SRM 51-40-02; STEP 4. AND MM 20-50-11.<BR><BR>SCREWGUN<BR>ATS1482<BR>CAL DUE 10/23;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 37,821 hrs · 23,246 cycles

AREA AFT OF FWD CARGO BAY HAS A CRACKED STR; STR R25; BS 520+19<[01] REMOVED AND REINSTALLED AND PERFORMED GOOD OPERATIONAL TEST OF RETRACTABLE LANDING LIGHT ASSEMBLY. IAW AMM 33-42-02-960-802.;[02] CERTIFIED ACTION 1.;[03] COMPLETED STEPS 6 AND 10;[04] CERTIFIED ACTION 3.;[05] DAMAGE REPAIRED PER 23-153-02888-WIP1.;[06] DAMAGE REPAIRED PER EA 23-153-02888.;[07] VERIFIED TASK COMPLETE

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 37,821 hrs · 23,246 cycles

CORROSION ON 986 FLOOR BEAM AT AFT WET AREA RBL43 WL208.<[01] REPAIRED IAW SRM 53-70-51-2R-6; REPAIR 6; FIG 205;<BR>FLOOR BEAM BS986; RBL43; WL208;[02] VERIFIED CORRECTIVE ACTION COMPLETE

Part: SKIN — CORRODED (ZN 200 FUS TOP) · airframe 37,821 hrs · 23,246 cycles

EXTERNAL RADOME AND ADAPTER RING - ROW 44 WI-FI - AIRCRAFT SKIN HAS SPOTS CORROSION ON SURROUND RIVETS BS 727B+15 TO BS 727C+14 BETWEEN LBL 10 TO RBL 10 APPROX. 53 EA (MARKED)<[01] 'REFER TO FAULT TTG8Q00NJ6Y7 WHERE EA 23-153-02981 WAS ADDED AS A SUBTASK.';[02] CORRECTED MEASUREMENTS.;[03] VERIFIED CORRECTIVE ACTION 1;2.<BR>VERIFIED MEASUREMENTS TABLE.<BR>JOB COMPLETED.

Part: SKIN — CORRODED (ZN 200 FUS TOP) · airframe 37,821 hrs · 23,246 cycles

EXTERNAL RADOME AND ADAPTER RING - ROW 44 WI-FI - AIRCRAFT SKIN HAS SPOTS CORROSION ON SURROUND RIVETS BS 727E+10 TO BS 747+17 BETWEEN LBL 13 TO RBL (MARKED) STC LARGE EXTERNAL DOUBLER ROW 44 WI-FI -HAS SPOTS CORROSION ON SURROUND RIVETS BS 727E+4 TO BS 747+10<[01] AS PER EA 23-153-02981; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.;[02] CORRECTED MEASUREMENTS.;[03] VERIFIED CORRECTIVE ACTION 1;2.<BR>VERIFIED MEASUREMENTS TABLE.<BR>JOB COMPLETED.

Part: TAIL CONE — DEBONDED (ZN 200 FUS TOP) · airframe 37,821 hrs · 23,246 cycles

TAILCONE FAIRING DISBONDED SKIN AT LOWER RH SIDE 9' FROM FWD EDGE<[01] TAILCONE FAIRING DISBONDED SKIN AT LOWER RH SIDE 9' FROM FWD EDGE WAS REPAIRED IAW SRM 51-70-04-2R-2.;[02] VERIFIED THE REPAIR OF THE TAILCONE FAIRING DISBONDED SKIN AT LOWER RH SIDE 9' FROM FWD EDGE WAS REPAIRED IAW SRM 51-70-04-2R-2

Part: FLOOR PANEL — DAMAGED (ZN 100 FUS LOWER) · airframe 37,157 hrs · 22,813 cycles

FWD CARGO COMPARTMENT AFT FLOORBOARD IS WTL.<[01] REMOVED AND REPLACED FWD CARGO AFT FLOORBOARD REF. AMM 25-52-10

Part: FLOOR PANEL — DAMAGED (ZN 100 FUS LOWER) · airframe 37,157 hrs · 22,813 cycles

AFT CARGO CARGO COMPARTMENT FLOORBOARD 140BF IS WTL<[01] REMOVED FLOOR BOARD REF AMM 20-50-11. FABRICATED AND INSTALLED FLOORBOARD PANEL PER M/M 25-52-01 & 25-52-10.;[03] VERIFIED FABRICATION AND INSTALLATION OF FLOORBOARD PANEL PER M/M 25-52-01 & 25-52-10.

Part: COVER — MISSING (ZN 200 FUS TOP) · airframe 36,419 hrs · 22,356 cycles

CAPT SIDE O/W EXIT LIGHTED EXIT/SALIDA SIGN COVER MISSING<[01] INSTALLED LH EMERG EXIT LIGHTED SIGN COVER PER AMM 33-51-01. A/C OK FOR SERVICE.

Part: CONTAINER — LOOSE (R2 DOOR SLIDE) · airframe 35,753 hrs · 21,901 cycles

CREW REPORTS R2 DOOR SLIDE CONTAINER LOOSE. SECURED DOOR SLIDE CONTAINER MOUNTING HARDWARE PER AMM 25-66-01

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 35,368 hrs · 21,655 cycles

L/H OVERWING EXIT EMERGENCY EXIT SIGN; FWD LIGHT INOP / [01] R&R EMERGENCY EXIT LIGHT PER AMM 33-51-00

Part: NONE — MISSING (FUSELAGE) · airframe 35,191 hrs · 21,540 cycles

EXTERNAL POWER DOOR CUTOUT LOWER FLANGE HAS AREA MISSING / [01] REMOVED THE INITIAL RUBBING BLOCK AND TRIMMED OUT DAMAGED AREA OF EGPR SURROUND DOUBLER IAW SRM 53-10-15-2R-4 ZONE 2 ALT. 2;[02] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 23. NO DEFECTS NOTED. TOOL#31823; DUE 23DEC22;[03] ENLARGED TRIM OUT BY .040' AS INSURANCE CUT IAW SRM 53-10-15-2R-4;[04] PERFORMED 10X VISUAL INSPECTION OF TRIM OUT AREA; NO DEFECTS NOTED IAW SRM 53-10-15-2R-4;[05] VERIFIED PN: 2024-T3-050 A-TAG: A83990 FOR -2 DOUBLER AND PN: 2024-T3-040 A-TAG: A84491 FOR -3 FILLER IAW SRM 53-10-15-2R-4;[06] VERIFIED STEPS 1 AND 3-4;[07] VERIFIED STEPS 3; 4; 5 & 6 C/W;[08] COMPLETED FABRICATION OF REPAIR PARTS IAW SRM 53-10-15-2R-4 ZONE 2 ALT. 2;[09] VERIFIED STEP 8;[10] VERIFIED STEP 8 & 9;[11] OK GIVEN TO TREAT AND PRIME.;[12] TREATED AND PRIMED REPAIR PARTS AND BARE SURFACES IN REPAIR AREA IAW SRM 53-10-15-2R-4;[13] VERIFIED STEP 12;[14] VERIFIED ITEM 12<BR>OK TO INSTALL REPAIR;[15] COMPLETED INSTALLATION OF REPAIR IAW SRM 53-10-15-2R-4 ZONE 2 ALT. 2;[16] VERIFIED JOB IS COMPLETE;[17] VERIFIED STEPS 15 & 16 C/W; JOB COMPLETE; AUDIT C/W

Part: HOOK — LOOSE (L1 DOOR) · airframe 34,561 hrs · 21,116 cycles

L1 DOOR SLIDE COVER BOTH GIRT BART HOOKS HARDWARE LOOSE. / [01] SECURED L1 DOOR SLIDE COVER GIRT BART HOOKS PER SRM 51-40-02;[02] SECURED L1 DOOR SLIDE GIRT BART HOOK PER SRM 51-40-02

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,404 hrs · 19,718 cycles

R/H GROUND ILLUMINATION EMERGENCY LIGHT IS INOP ; RH GROND ILLMINATION EMERGENCY LIGHT IS INOP / [07] REPLACED FUSE FOR R/H GROUND ILLUMINATION EMERGENCY LIGHT PER AMM 33-51-06-960-804 STEPS 3.D.(1) THRU (4). PERFORMED GOOD EMERGENCY LIGHTS OPERATIONAL TEST PER AMM 33-51-00-710-801; [08] OK TO REINSTALL AIR GRILLE AT STA727C+7; LBL68; [09] VERIFIED CORRECTIVE ACTIONS 6; 7.<BR><BR>COMPLETED STEPS 1 AND 2.; [10] INSTALLED AIR GRILLE AT STA 727C +7; LBL 68 IAW CMM 25-23-01.; [11] VERIFIED CORRECTIVE ACTION ITEM 10.; [12] VERIFIED TASK IS COMPLETE.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED ; / [01] WELDED CRACK ON RADIUS OF ACB; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4).<BR>WELDING MACHINE CAL I.D. E10583; S/N; KJ256554 12/2021; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.<BR><BR>OK TO ACCOMPLISH PENETRANT INSPECTION PER SRM 53-60-15-2R-1 4.B.(4); [03] FLUORESCENT DYE PENETRANT INSPECTED REPAIR AREA IN ACCORDANCE WITH SOPM 20-20-02 METHOD C. <BR>VOID NOTED OPEN TO THE SURFACE ON INNER SURFACE OF SCUFF PLATE. (MARKED)<BR><BR>TOOL I.D. ATS2504 (DLM-1000 RADIOMETER)<BR>S.N. 191348; [04] WELDED DEFECT AS NOTED BY NDT ON ACB; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(4). <BR>WELDING MACHINE CAL I.D. E10583; S/N; KJ256554 12/2021;07] SANDED REPAIR WELD AREA SMOOTH PER SRM 53-60-15-2R-1 PARA 4.B.(5); [08] VERIFIED CORRECTIVE ACTION ENTRY 7.<BR><BR>OK TO TREAT AND PRIME; [09] APPLIED TREAT AND PRIMER; AND PARTING AGENT TO THE INNER SURFACE AFT CORNER SCUFF PLATE ACB IAW SRM 53-60-15-2R-1 REPAIR 1 4.B ( [11] INSTALLED ACB AFT CORNER SCUFF PLATE; APPLIED FILLET SEAL AROUND ALL CORNER SCUFF PLATE AND APPLIED FILLET COMPOUND IN THE UPPER CORNER TO THE DOORWAY IAW SRM 53-60-15-2R-1 REPAIR 1; [12] VERIFIED INSTALLATION OF ACB AFT CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 REPAIR 1; [13] TASK CARD COMPLETE.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

CORROSION ON AFT SHIELD AT AFT CARGO BAY BS847 - BS867 RBL21 WL164 LOWER SURFACE. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0 PAR. 9C. LOCATED AND DRILLED A NEW SHILD IAW SRM 51-40-05-OG-0 AND DWG 146A8127. INSTALLED NEW SHIELD ON ACB AFT BS 847- BS 867 RBL 21 WL164 IAW SRM 51-40-02-0G-0 AND DWG 1468127.

Part: SEAT TRACK — ELONGATED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

FLIGHT DECK; F/O SEAT TRACK AFT OUTBOARD LOCK PIN HOLES ENLARGED. F/O SEAT TRACK AFT INBOARD LOCK PIN HOLES ENLARGED AND TOP SURFACE GROOVED. ; / [01] REMOVED AND REPLACED FLIGHT DECK FO'S AFT I/B AND O/B SEAT TRACKS IAW AMM 25-11-11-400-801.; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: SEAT TRACK — ELONGATED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

FLIGHT DECK CAPT. SEAT TRACK AFT OUTBOARD; LOCK PIN HOLES ENLARGED. SEAT TRACK AFT INBOARD; LOCK PIN HOLES ENLARGED AND TOP SURFACE GROOVED. ; / [01] REMOVED AND REPLACED FLIGHT DECK CAPT'S AFT I/B SEAT TRACK IAW AMM 25-11-11-400-801.; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.; [03] REMOVED AND REPLACED FLIGHT DECK CAPT'S AFT O/B SEAT TRACK IAW AMM 25-11-11-400-801.; [04] UPDATED PARTS REQUIREMENT; [05] VERIFIED INSTALLATION OF CAPTAIN'S O/B SEAT TRACK PER AMM 25-11-11-400-801. ALIGNMENT GOOD

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED AT WL 153; STA727D+18; RBL 22; STA727E+1.5; RBL 20; STA727E+2; RBL 22; STA727E+5; RBL 20; STA727E+6; RBL 22; STA727E+8; RBL 22; STA727E+10; RBL 22; STA727E+14 RBL 22; STA727E+18 RBL 22; STA 727E+19 RBL 20. / REMOVED CORROSION AFT CARGO FLOOR TO SIDEWALL SUPPORT BTW 727D+18 TO 727E+10 WL 153 RBL 20 TO RBL 22 IAW SRM 51-10-02 PARA#15 EVALUATED ALL REWORKED AREA THE DEPPEST AREA STA 727E+10 RBL22 DIMENSION L=1.5' X W=1' DEPTH=.012 ORIGINAL THICKNESS .040' REMAINING THICKNESS .028' FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 FIGURE 103 DEATIL E DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT B/S 767 TO B/S 727D +12' RBL22 MATERIAL USED BAC1496-777 7075T6 IAW SRM 51-40-05 AND DWG 146A7502 REV:-. AND 146A7500 REV: VERIFIED APPLICABILITY FOR SIDEPLATE REPAIR IAW 53-00-53-2R-6 REPAIR 6 DRILLED NEW SPLICE SIDEPLATE BTW B/S 727C TO B/S 727D RBL22 MATERIAL USED BAC1496-777 7075T62 IAW SRM 53-00-53-2R-6 REPAIR 6 SRM 51-40-05 AND DWG 146A7502 REV:- AND. 146A7500 VERIFIED APPLICABILITY FOR SIDEPLATE REPAIR IAW SRM 53-00-53-2R-6 REPAIR 6 APPLIED CHEMICAL CONVERSION AND PRIMER ON REPAIR PARTS (1EA) SPLICE [1EA] ZEE CHANNEL IAW SRM 53-00-53-2R-6 REPAIR 6 SRM 51-20-01SOPM 20-41-02. INSTALLED FLOOR TO SIDEWALL SUPPORT AT ACB BS727 TO BS767 RBL22 WL153 PER SRM 51-40-02-0G AND DWG 146A7500 AND 146A7502. . VERIFIED INPECTION ITEMS ARE COMPLETE

Part: SHIELD — CORRODED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

CORROSION ON FORWARD CARGO BAY SHIELD, BS 500+13, RBL 24, WL 154. REMOVED FWD CARGO BAY AFT SHIELD IAW SRM 51-40-02. NO ALLOWABLE DAMAGE IN SRM. LOCATED & DRILLED A NEW SHIELD IAW SRM 51-40-05-OG-0 & DWG143A0080. INSTALLED NEW AFT SHIELD IAW SRM 51-40-02-0G-0 & DWG 143A0080.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 45.5. WL 208.1, BS 540+18 - 559, 639+8, 663 - 663+11, 685 - 706, 716 - 727+8, AND 727A - 727B. COMPLETED ALL STEPS VERIFIED PARTIAL STEPS 1-6. APPLIED A CHEMICAL CONVERSION COATING AND ONE LAYER OF EPOXY PRIMER TO REWORKED AREAS IAW SRM 51-20-01 AND SOPM 20-41-04 VERIFIED STEPS 1-6 AND CORRECTIVE ACTION 3

Part: SHIELD — CORRODED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

AFT CARGO BAY DOOR CUTOUT FWD SHIELD IS CORRODED AT WL 153; BS 767+1; RBL 20; 767+2.5; RBL 22; 767+4; RBL 20; 767+7; RBL 22; 767+8; RBL 20; 767+11; RBL 22; 767+15; RBL 22. DAMANGE FOUND ON FWD SHIELD, FOUND TO BE OUT OF LIMIT IAW SRM 51-10-02-0G-0 PAR. 9C. LOCATED AND DRILLED NEW SHILD IAW SRM 51-40-05-OG-0 & DWG 146A8127. INSTALLED NEW SHIELD IAW SRM 51-40-02-0G-0 &DWG 146A8127.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT IS CORRODED AT WL 153; STA747+2; RBL 22; STA747+6; RBL22; STA747+10; RBL 22; STA747+14; RBL 22; STA747+15; RBL 20; STA 747+18; RBL22. ; / [01] REMOVED CORROSION AFT CARGO FLOOR TO SIDEWALL SUPPORT (BTW B/S 747 +2' TO B/S 747+18')WL 153 RBL 20 TO 22 IAW SRM 51-10-02 PARAGRAPH 15 EVALUATED ALL REWORKED AREAS; THE DEPPEST AREA : STA 747+18 RBL 22; DIMENSION L=1.' X W=.8'X DEPTH= 0.013' ORIGINAL TICKNESS 0.040' REMAINING THICKNESS 0.027' FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 FIGURE 103 DEATIL'E'.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED AT WL 153; STA767+2; LBL 21; STA767+7; LBL 20 TO 22; STA767+10; LBL 22; STA767+13; LBL 20; STA767+14; LBL22; STA767+18; LBL 22; STA767+18.5; LBL20; STA787+6 LBL 22. / REMOVED CORROSION AT AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT WL 153 STA767+2 LBL21; L:0.800' W: 0.700' DEPTH: 0.002'; STA767+7 LBL 20 TO 22; L:2' W:1' DEPTH: 0.003' STA767+10 LBL 22; L: 1' W: 0.800' DEPTH: 0.003' STA767+13 LBL 20; L:1' W:0.850' DEPTH: 0.002' STA767+14 LBL22; L:0.950' W: 0.890' DEPTH:0.003' STA767+18 LBL 22; L:0.950' W:0.850' DEPTH 0.002' STA767+18.5 LBL20; L:950' W:860' DEPTH:0.001' IAW SRM 51-10-02 PARAGRAPH 15 . EVALUATED ALL REWORKED AREAS ; THE DEEPEST AREA IS 0.003' ORIGINAL TICKNESS 0.040' REMAINING THICKNESS: 0.037' ALL THE REWORKED AREAS WITHIN ALLOWABLE DAMAGE FOUND IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 FIGURE 103 DETAIL 'E ' TOOL USED MICROMETER ID:ATS601 S/N:87172291 DATE DUE:05/2022 VERIFIED ITEM 1 CORRECTIVE ACTIONS. APPLIED CHEMICAL CONVERSION AND PRIMER COATING ON REWORKED AREAS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 STEP 2E(1-2) ACCOMPLISHED WORK ON CUSTOMER CARD# TTG8Q006WFXZ VERIFIED CORRECTIVE ACTION ENTRY 4. OK TO TOPCOAT THE GLOSS WHITE (TOPCOAT) IS DOCUMENTED IN THE CUSTOMER CARD# TTG8Q004BJWH STEP# 20. AND ALL MAINTENANCE ACTION ARE COMPLETED IN THE TASK CARD TTG8Q006WFXZ REQUEST FINAL BUYOFF. VERIFIED CORRECTIVE ACTION 6. RII FUNCTION NOT REQUIRED FOR THIS FAULT.

Part: WEB — CORRODED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

AFT CARGO DOOR CUTOUT WEB CORRODED AT WL 153, BS 787+8, RBL 20, BS 787+10; RBL 22, BS 787+11.5, RBL 24, BS 787+3, RBL 24, BS 787+14, RBL 26, AND BS 787+16, RBL 26. DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-60-15-1A-1, PAR 4G. LOCATED AND DRILLED NEW WEB IAW SRM 51-40-05-OG-0 DWG 146A8123. INSTALLED THE NEW CUTOUT WEB IAW DWG 146A8340 REV-, AND SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT IS CORRODED AT WL 153, BS 727C+11, RBL 20, BS 727C+18.5, RBL 20, BS 727D+3, RBL 22, BS 727D+4.5, RBL 20, BS 727D+5.5, RBL 20, BS 727D+7.5, RBL 20, BS 727D+10, RBL 20, BS 727D+10, RBL 22, BS 727D+13, RBL 20, & BS 727D+14, RBL 22. FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. LOCATED & DRILLED NEW SPLICE SIDEPLATE IAW SRM 53-00-53-2R-6 REPAIR 6, SRM 51-40-05, & DWG 146A7502 REV:- AND. 146A7500 REV. MAINTENANCE ACTIONS ARE COMPLETED ON THE CARD TTG8Q006WDL9.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

CRACKED FLOOR SUPPORT AT STA 541; LBL 1; WL 207. ; / [01] REMOVED FLOOR SUPPORT AT STA 541 LBL 1 WL 207 IAW SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT P/N 143A5240-35; LOT 1465980-10 AT STA 541; LBL1; WL207. IAW.SRM 51-40-05 AND DWG#143A0060. OK TO INSTALL.; [03] STEP 2; ADD REV B.; [04] CORRECTION TO ITEM 2 AND 3 CORRECTIVE ACTIONS; LOCATED AND DRILLED NEW FLOOR SUPPORT P/N 143A5240-35; LOT 1465980-10 AT STA 541; LBL1; WL207. IAW.SRM 51-40-05 AND DWG#143A0060; REV B. OK TO INSTALL.; [05] VERIFIED ITEM 4 CORRECTIVE ACTIONS. <BR>OK TO INSTALL.; [06] INSTALLED NEW FLOOR SUPPORT AT STA 541; LBL 1; WL 207 IAW. SRM 51-40-02 AND DWG#143A0060; REV B.; [07] VERIFIED ITEM 6.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 32,404 hrs · 19,718 cycles

CRACKED FLOOR SUPPORT AT BS 541, RBL 1, WL 207. REMOVED FLOOR SUPPORT IAW SRM 51-40-02-0G-0. LOCATED & DRILLED A NEW FLOOR SUPPORT IAW SRM 51-40-05 & DWG 143A0060. INSTALLED THE NEW FLOOR SUPPORT IAW SRM 51-40-02 & DWG 143A0060, REV B.

Part: BULKHEAD — CRACKED (BS 663) · airframe 32,404 hrs · 19,718 cycles

CRACKED LOWER LT COMPOSITE BULKHEAD AT BS 663, LBL 35, WL 152. UPON INSPECTION OF PANEL FOUND ONE ADDITIONAL CRACK ALL FOUND OUT OF LIMITS IAW SRM 57-10-10-1A-2 PAR 4D(1). REPAIRED ACCOMPLISHED IAW SRM 51-70-04-2R-10.

Part: BULKHEAD — CRACKED (BS 663) · airframe 32,035 hrs · 19,489 cycles

LT MLG W/W ;FWD BULK HEAD HAVE VAPOR BARRIER CRACK APPOX 4 INCH LONG . CRACK LOCATED AT BETWEEN LBL 31 AND LBL 45;BEHING A HYD RETURN FILTER. ; / [01] PERFORMED INTERIM SEAL ON WHEEL WELL SIDE OF VAPOR WEB PER SRM 57-10-10-1A-2 STEP 2.C.4(A). VISUAL REINSPECTION OF THE REPAIR AREA DUE AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY. IF ADDITIONAL DAMAGE IS FOUND; REFER TO SRM<BR>57-10-10-1A-2 FOR DAMAGE LIMITS AND REPAIRS

Part: LIGHT — BROKEN (CABIN) · airframe 31,318 hrs · 19,084 cycles

LOWER EMERGENCY EXIT SIGN AT EMERGENCY EXIT ROW FIRST OFFICER SIDE BROKEN. REMOMVED AND REPLACED RIGHT OVERWING EXIT LOWER LIGHT REF AMM 33-51-01. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 30,224 hrs · 18,438 cycles

EMERGENCY LIGHTING BATTERY PACK AT RT OVER WING EXIT FAILED CAPACITY CHECK. REMOVED AND REPLACED, PER AMM.33-51-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 30,224 hrs · 18,438 cycles

RT AFT EMERGENCY LIGHTING BATTERY PACK FAIL CAPACITY CHECK. REMOVED AND REPLACED, PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,676 hrs · 17,457 cycles

EMERGENCY BULLNOSE LIGHTS AT 9 ABC AND 11 ABC INOP / DMA # 0254376 R&R BATTERY PACK (M1670) PER MM 33-51-06 & WDM 33-51-13. ALL ASSOCIATED EMER LTS OPS CHECK GOOD. CL # 38461

Part: BATTERY PACK — FAILED (CABIN) · airframe 28,654 hrs · 17,441 cycles

1 EA EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. / REMOVED AND REPLACED 1 EA EMERGENCY LIGHT BATTERY PACK AT POSITION M01668 PER AMM 33-51-06

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 28,654 hrs · 17,441 cycles

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

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 28,032 hrs · 17,044 cycles

FORWARD ENTRY DOOR, LOWER EMERGENCY EXT LIGHT LENS MISSING DIRECTIONAL ARROW. / R&R EXIT SIGN AMM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 28,032 hrs · 17,044 cycles

RIGHT WING EMERGENCY EXIT LOWER LIGHT LENS MISSING DIRECTIONAL ARROW. / R&R LENS PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 27,432 hrs · 16,652 cycles

CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN AT MID CABIN LOOSE. / R&R LIGHT HOUSING ASSEMBLY IAW AMM.

Part: CHANNEL — CORRODED (WHEEL WELL LH) · airframe 27,175 hrs · 16,491 cycles

LH MWW BS 663 VAPOR BARRIER WEB UPPER CHANNEL P/N 111A1306-1 IS EXFOLIATED AT UPPER FASTENER HOLE LBL 58. / REMOVED AND REPLACED L/H 663 VAPOR BARRIER UPPER CHANNEL IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG# 111A1000 REV F

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 27,175 hrs · 16,491 cycles

VAPOR BARRIER CRACKED IN UPPER CHORD AT BS. 663, LBL 30. / REPAIRED ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (AFT CARGO BAY) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO STA 927 TO 947 RBL 18 INTERCOSTAL CRACKED. / REMOVED AND REPLACED INTERCOSTAL AT STA 927 TO 947 RBL 18 IAW SRM 51-40-02-0G-0 PAR 4 PART# 147A7500 Y22; ATAG WN0664 IAW DWG 147A7500 REV-

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO PIT AFT CORNER SCUFF PLATE CRACKED / RECEIVED RH CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE ON BACKSHOP W/O 40014-1000-0002. INSTALLED AFT CARGO; FWD CUFF PLATE IAW EA 1-A53-2076 REV 11 AND 737-700 AMM 53-11-02-420-801. P/N- 146A8341-5.

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 27,175 hrs · 16,491 cycles

PASSENGER CABIN FWD WET AREA BETWEEN STA 344 AND 360 BL 0 WL 208.1 INTERCOSTAL HAS 2 EA CRACKS IN FASTENER HOLES FWD AND AFT AS MARKED / REMOVED AND REPLACED PASSENGER CABIN FWD WET AREA BETWEEN STA 344 AND 360 BL 0 WL 208.1 INTERCOSTAL IAW B-737 SRM 51-40-02-0G-0 STEP 7.D AND DWG 141A5400 REV- A TAG WN 5803

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 27,175 hrs · 16,491 cycles

G1 GALLEY EMERGENCY EXIT LIGHT ASSEMBLY CONNECTORS MISSING. / R&R LIGHT ASSEMBLY IAW AMM.

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 27,175 hrs · 16,491 cycles

PASSENGER CABIN FWD WET AREA BETWEEN STA 312 AND 328 LBL 45 INTERCOSTAL IS CRACKED AS MARKED / REMOVED INTERCOSTAL FROM BS 310 TO 328 LBL 45' IAW SRM 51-40-02. IDENTIFIED NEW INTERCOSTAL P/N 141A5410-12 IAW DWG 141A5400 REV - LOCATED AND DRILLED NEW PART AT BS 312 TO 328 LBL 45' IAW DWG 141A5400 REV - AND SRM 51-40-05-0G-0. APPLIE CIC AREA REWORK IAW AMM 51-21-91-620-802; TESTED NUT PLATE BOND TOOL AAR #41801 (CB602-3) DUE 2/20 IAW SRM 51-40-10-2R-0 ATAG #A14442

Part: ANGLE — CORRODED (BS 328) · airframe 27,175 hrs · 16,491 cycles

PASSENGER CABIN FORWARD WET AREA BETWEEN BS. 294 TO BS. 328, RBL 58 AREA, CENTER LOWER THRESHOLD L ANGLE BRACKET ATTACHED TO OUTBOARD SIDE OF THE CREASE BEAM CHORD CORRODED. / R&R "Z" ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 27,175 hrs · 16,491 cycles

PASSENGER CABIN AFT WET AREA TOP FLANGE OF FLOOR BEAM CORRODED AT BS. 986, RBL 44. / REPAIRED FLOOR BEAM PER EA.

Part: FRAME — CRACKED (BS 312) · airframe 27,175 hrs · 16,491 cycles

L1 DOOR CUTOUT JUST ABOVE UPPER DOOR SILL FRAME CRACKED IN INBOARD RADIUS AT BS. 312, STR. 6L. / REPAIRED FRAME IAW EA.

Part: STRAP — CORRODED (AFT CARGO THRESH) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO STA 794+9 TO 807+14; RBL 23; WL 154; LOWER SILL STRAP HAS CORROSION ON UPPER SURFACE. / REMOVED CORROSION AT AFT CARGO LOWE SILL STRAP IAW 737-700 SRM 51-10-02-06-0 VEIFIED LIMTS AS ORG 'T' .100';LOSS OF .015'; REMAINING .085' IS OUT OF LIMITS IAW 737-700 SRM 53-00-53-1A-2 VERIFIED NEW AFT CARGO LOWER SILL AS P/N:146A8128-14 IAW A-TAG WN6459 AND BOEING DWG 146A8120 REV A. INSTALLED AFT CARGO LOWER SILL IAW B737-700 SRM 51-40-02-0G-0 AND BOEING DWG 146A8120 REV A. A TAG WN6459 PN 146A8128-14.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO DOOR CUTOUT; FWD CORNER SCUFF PLATE IS CRACKED. / RECEIVED AFT CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE ON BACKSHOP W/O 40064-1600-0001. INSTALLED AFT CARGO FWD SCUFF PLATE IAW EA 1-A53-2076 REV 11 AND 737-700 AMM 53-11-02-420-801. P/N - 143A8341-7

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO STA 947; RBL 18 TO LBL 11; WL 166; BULKHEAD TO FLOOR SUPPORT ANGLE HAS CORROSION ON UPPER SURFACE / AFT CARGO STA 947 RBL 18 TO LBL 11 WL 166 BULKHEAD TO FLOOR SUPPORT ANGLE HAS CORROSIEN FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA SRM 53-00-53-111-2 REMOVED FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND IAW BOEING DWG # 149A8118 REV- ATAG#WN4812

Part: TRACK — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO STA 927+16; RBL 15; WL 166; FLOOR SUPPORT TRACK HAS CORROSION ON LOWER SURFACE AROUND NUT PLATES. / REMOVED AND REPLACED FLOOR SUPPORT TRACK AFT CARGO BAY STA 887-947.5+2' RBL13 P/N 147A7501U14 A-TAG# WN7682 I/A/W DWG 147A7500 REV- AND SRM 51-40-02-0G-0. REMOVED CORROSION I/A/W SRM 51-10-02-0G-0 ORIG 'T' .070' .059' REM .013' LOSS OUT OF LIMITS I/A/W SRM 53-00-53-1A-2. APPLIED CIC TO NEW FLOOR SUPPORT TRACK I/A/W AMM 51-21-91-620-802. P/N 147A7501014 A-TAG# WN7682

Part: ANGLE — CORRODED (BS 727C-787) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO Z-ANGLE CORRODED ON UPPER AND LOWER SURFACE BETWEEN BS. 727C8 TO BS. 787+12, LBL 23. / R&R Z ANGLE IAW SRM.

Part: ATTACH ANGLE — CORRODED (BS 927) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO ATTACH ANGLE COMMON TO LONGITUDINAL WEB CORRODED AT BS. 927+16, RBL 16, ON FORWARD FACE OF FLANGE. / R&R ATTACH ANGLE IAW DWG.

Part: CAP — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO COMPARTMENT FLOOR CAPSTRIP MARKED L/H FWD IS CORRODED. / REMOVED CORROSION FROM CAP STRIP IAW B737-700 SRM 51-10-020-0G-0 VERFIED WITH 10X GLASS. EVALUATED DAMAGE REMOVED FOUND CAPSTRIP TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA IAW B737-700 SRM 51-10-02-0G-0. 51-10-02-0G-0. VERFIED NEW CAPSTRIP AS P/N 453A2611-8 ATAG# WN2954. REPLACED ON BENCH P/N 453A2611-8 ATAG WN2454

Part: ANGLE — CORRODED (BS 727C-767) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO Z-ANGLE CORRODED ON UPPER AND LOWER SURFACE BETWEEN BS. 727C+10 TO BS. 767, RBL 23. / REPAIRED Z-ANGLE PER SRM.

Part: CAP — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO COMPARTMENT FLOOR CAPSTRIP MARKED R/H IS CORRODED. / EVALUATED DAMAGE REMOVED FOUND TO BE OUT OF LIMITS DUE TO PUBLISHED DATA IAW B737-700 52-10-02-0G-0. REMOVED CORROSION FROM FLOOR CAPSTRIP IAW B737-700 51-10-02-0G-0. VERFIED NEW CAPSTRIP AS P/N 453A2611-1 ATAG# A32125 IAW B737-700 AIPC 82-52-10-02 PREPLACED ON BENCH. P/N 453A2611-1 ATAG A32125

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO COMPARTMENT AFT DOORWAY TIEDOWN PLATE IS CORRODED. / REMOVED CORROSION FROM AFT CARGO COMPARTMENT AFT DOORWAY TIEDOWN PLATE. NO SRM LIMITS GIVEN. REPLACED PART ON SHELF IAW B737 SRM 51-10-02-0G-0 STEP 9 P/N 453A2611-2 'A' TAG A20769

Part: CAP — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO COMPARTMENT FLOOR CAPSTRIP MARKED R/H FWD IS CORRODED. / REMOVED CORROSION FROM CAPSTRIP IAW B737-700 SRM 51-10-02-0G-0 VERFIED WITH 10X GLASS VERFIED LIMITS FOUND TO BE OUT OF LIMITS DUE TO O PUBLISHED DATA IAW B737-700 SRM 51-10-02-0G-0 VERFIED NEW CAPSTRIP AS P/N 453A2611-9 ATAG# A48890. PREPLACED ON BENCH P/N 453A2611-9 ATAG A48890

Part: CAP — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT FLOOR CAPSTRIP MARKED L/H IS CORRODED. / REMOVED CORRSION FROM CAPSTRIP IAW B737-700 SRM 51-10-02-0G-0 VERFIED WITH 10X GLASS EVALUATED DAMAGE REMOVED FOUND CAPSTRIP TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA IAW B737-700 51-10-02-0G-0. VERFIED NEW CAPSTRIP AS P/N 453A2611-4 ATAG# WN8957 REPLACED ON BENCH P/N 453A2611-4 ATAG WN8957

Part: CAP — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO COMPARTMENT FLOOR CAPSTRIP MARKED L/H IS CORRODED. / REMOVED CORROSION FROM CAPSTRIP IAW B737-700 SRM 51-10-02-0G-0 VERFIED WITH 10X GLASS. EVALUATED DAMAGE REMOVED FOUND CAPSTRIP TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA IAW B737-700 SRM 51-10-02-0G-0 VERFIED NEW PART AS P/N 453A2611-10 ATAG WN8865 IAW B737-700 AIPC 25-52-10-02. P/N 453A2611-10 ATAG WN8865

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO COMPARTMENT FWD DOORWAY TIEDOWN PLATE IS CORRODED. / VERIFIED NEW TIE DOWN PLATE P/N 453A2611-1 ATAG 247402 IAW B737-700 AIPC 25-52-10-02. REPLACED ON BENCH. P/N: 453A2611-1 ATAG A47402

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO COMPARTMENT FLOOR PANEL SPLICE ON 140CF IS CORRODED. / AFT CARGO COMPARTMENT FLOOR PANEL SPLICE ON 140CF IS CORRODED BLEND CORROSION AND FOUND NO PUBLISHED LIMITS IAW SRM 51-10-02-0G-0 REMOVED CORRODED PANEL SPLICE IAW SRM 51-40-02-0G-0 AND INSTALLED NEW PANEL SPLICE IAW AIPC 53-42-11-30 AND IAW SRM 51-40-02-0G-0 ATAG BO4223

Part: INTERCOSTAL — CORRODED (FWD CARGO RH) · airframe 27,175 hrs · 16,491 cycles

FWD CARGO COMPARTMENT R/H Z ANGLE BETWEEN STA 500A AND 500D ABOVE STR 25 R AREA; WL 156.4 TOP SKIN SURFACE HAS 5 EA AREAS OF CORROSION AS MARKED. REMOVED CORROSION ON RIGHT HAND Z-ANGLE STA 500A TO 500D UPPER SURFACE 5 EACH AREAS; USEING 10X MAG NO FURTHER CORROSION FOUND IAW B737 SRM 51-10-02-0G-0; STEP 15; ORIGINAL THICKNESS .040; LOSS OF .003; AT DEEPEST BLEND REMAINING .037 WITHIN LIMITS IAW B737 SRM 53-00-53-1A-2 FIG 103; PG 9 DETIAL A-A USING AAR REMOVED INTERCOSTAL FROM BS 310 TO 328 LBL 45' IAW SRM 51-40-02. NEW INTERCOSTAL P/N PRIMER 141A5410-12 IAW DWG 141A5400 REV - LOCATED AND 4 DRILLED NEW PART AT BS 312 TO 328 LBL 45' IAW DWG 141A5400 REV - AND SRM 51-40-05-0G-0. APPLIE CIC AREA REWORK IAW AMM 51-21-91-620-802.

Part: INTERCOSTAL — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO STA 747+10 TO 767; RBL 23; WL 154; BAFFLE ANGLE HAS CORROSION ON LOWER SURFACE AROUND NUTPLATE HOLES / REMOVED AND EVALUATED CORROSION ON -8 INTERCOSTAL. ORIGINAL THICKNESS .030' LOSS OF .013' WITH .027' REMAINING BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02-0G-0 AND DWG 146A7502 REV A

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO. STA 947; RBL 23; WL166; CURVED BULKHEAD TO SIDEWALL SUPPORT ANGLE HAS CORROSION ON UPPER SURFACE. / REMOVED CORROSION FORM CURVED SIDEWALL SUPPORT IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED DATA. REMOVED DAMAGED BULKHEAD SIDEWALL SUPPORT AT AFT CARGO COMPARTMENT STA 947' ; RBL 23'; & WL 166' IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW PART IAW SRM 51-40-05-0G-0 & BOEING DRAWING 149A8118 REV: B. INSTALLED NEW SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0. RESTORED FINISHES. P/N 149A8118-27

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO STA 767+2 TO 787; RBL 27; WL 154; SPLASH SHIELD HAS CORROSION ON UPPER AND LOWER SURFACE / REMOVED SPLASH SHIELD @ AFT CARGO F.S. 767+2 TO 787; RBL 27 FOUND TO BE 'OUT OF LIMITS' ORIGINAL 'T' =.050. REMAINING 'T' =.042; LOSS=.008. RECIEVED NEW SHIELD P/N 146A8127U2 SI # 7531132 LOCATED & DRILLED NEW SHIELD. INSTALLED NEW SHIELD. APPLIED CIC TO NEW INSTALLED SHIELD. ALL ACTIONS ARE IAW B737 SRM 51-10-02-0G-0; 51-40-02-0G-0; 51-40-05-0G-0; 51-40-06-0G-0; AMM 51-21-91-620-802; BOEING DWG'S 146A8127 REV - & DWG # 146A0081 REV A. P/N 146A3127U12 SI # 7531132 A-TAG # WN 7041 AAR TOOL # 36644 DUE 09 SEP 20.

Part: WEB — CORRODED (BS 794-847) · airframe 27,175 hrs · 16,491 cycles

AFT CARGO LOWER SILL WEB CORRODED BETWEEN BS. 794 TO BS. 847, RBL 27, ON UPPER SURFACE. / R&R WEB IAW SRM & DWG.

Part: WEB — CORRODED (CARGO THRESHOLD) · airframe 27,175 hrs · 16,491 cycles

FORWARD CARGO BAY BETWEEN CENTER CARGO LOWER DOOR THRESHOLD WEB CORRODED BETWEEN BS. 480+5 TO BS. 460+8, AREAS TOP SKIN. / R&R THRESHOLD WEB IAW DWG & SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 27,175 hrs · 16,491 cycles

FWD CARGO DOOR; FWD CORNER SCUFF PLATE IS CRACKED INTO 2 PIECES / ACCOMPLISHED WELD REPAIR ON FWD CARGO FWD CORNER SCUFF PLATE I.A.W E.A 1-A53-2016 REV IR II

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 27,175 hrs · 16,491 cycles

FWD CARGO DOOR; AFT CORNER SCUFF PLATE IS CRACKED INTO 2 PIECES / ACCOMPLISHED WELD REPAIR ON FWD CARGO AFT CORNER SCUFF PLATE I.A.W EA. 1-A53-2076 REV II.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 27,175 hrs · 16,491 cycles

L/H WHEEL WELL VAPOR WEB CRACKED AT BS. 663, LBL 49. / REPAIRED BARRIER WEB IAW SRM & DWG.

Part: LENS — CRACKED (CABIN) · airframe 27,175 hrs · 16,491 cycles

AFT WET AREA R2 DOOR EMERGENCY EXIT LENS CRACKED. / R&R LENS IAW AMM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 27,175 hrs · 16,491 cycles

R/H WHEEL WELL VAPOR BARRIER WEB CRACKED AT BS. 663, RBL 48. / R&R VAPOR BARRIER IAW SRM AND DWG.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 27,175 hrs · 16,491 cycles

R/H VAPOR BARRIER CRACKED AT BS. 663. / R&R VAPOR BARRIER BULKHEAD IAW DWG AND SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 27,175 hrs · 16,491 cycles

L/H VAPOR BARRIER PANEL CRACKED AT BS. 663. / REPAIRED VAPOR BARRIER IAW SRM.

Part: ANGLE — CRACKED (VERTICAL STABILI) · airframe 27,175 hrs · 16,491 cycles

VERTICALSTAB.INTERNALSIDE. STA 1016; LATTERAL EXPANTION JOINT ANGLE IS CRACKED IN RADIUS 3' O/B OF STR 2R; 8' ABOVE FUSELAGE SKIN / REMOVED AND REPLACED VERTICAL LATERAL EXPANSION JOINT ANGLE STA 1016 IAW SRM 51-40-02-0G-0 AND BOEING DWG 176A 3101 REV-.

Part: CAP — CORRODED (FWD CARGO RH) · airframe 27,175 hrs · 16,491 cycles

FWD CARGO RH SIDEWAL TO FLOOR PANEL CAP STRIP HAS CORROSION ON LOWER SURFACE / REMOVED CORROSION FROM FWD CARGO RH SIDEWALL TO FLOOR PANEL CAP STRIP. NO SRM LIMITS GIVEN REPLACED PART ON SHELF IAW B737 SRM 51-10-02-0G-0 STEP 9 P/N 453A1611-5 'A' TAG A18452

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,919 hrs · 15,050 cycles

RT EXTERIOR EMERGENCY EXIT DOOR LIGHT INOP. R&R BATTERY PACK CHARGER PER AMM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 24,646 hrs · 14,881 cycles

SUPPLEMENTAL INFORMATION: L/H FWD UPPER SLIDING SEAL CRACKED / R&R L/H FWD UPPER SLIDING SEAL REF AMM 53-31-31.

Part: BATTERY — FAILED (CABIN) · airframe 24,646 hrs · 14,881 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 24,646 hrs · 14,881 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PER AMM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 24,646 hrs · 14,881 cycles

SUPPLEMENTAL INFORMATION: R/H FWD UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED R/H FWD UPPER SLIDER PER AMM 53-31-31

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 22,385 hrs · 13,443 cycles

FORWARD GALLEY FLASHLIGHT STRAP BROKEN. R&R STRAP IAW AMM.

Part: NONE — CRACKED (CABIN) · airframe 22,385 hrs · 13,443 cycles

SUPPLEMENTAL INFORMATION: CABIN FLOOR BOARD SUPPORT PANEL BREAKS BETWEEN PNL 231XF; AND 231UF ARE CRACKED. L\H AND R\H. / REMOVED AND REPLACED CABIN FLOOR BOARD SUPPORTS BETWEEN PNL 231XF; AND 231UF; LH AND RH IAW SRM 51-40-02

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 20,347 hrs · 12,124 cycles

AFT CARGO; R/H TRANSITION ANGLE HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES FROM STA. 847 TO 867 / AFT CARGO; R/H TRANSITION ANGLE FROM STA. 847 TO 867 REMOVED AND REPLACED AS PER SRM 51-10-02 AND 51-40-02.

Part: CAP — CORRODED (FWD CARGO BAY) · airframe 20,347 hrs · 12,124 cycles

R/H TRANSITION ANGLE AT STA 336 AND RBL 21 HAS CORROSION AT FASTENER HOLE. / REMOVED AND INSTALLED NEW R/H TRANSITION ANGLE PER SRM 51-40-02.

Part: CAP — CORRODED (FWD CARGO BAY) · airframe 20,347 hrs · 12,124 cycles

L/H TRANSITION ANGLE STA 500 TO 500D AT LBL 21 HAS SEVERAL SPOTS OF CORROSION. (MARKED) / REPAIR TRANSITION ANGLE PER SRM 53-00-53-2R-5.

Part: CAP — CORRODED (FWD CARGO BAY) · airframe 20,347 hrs · 12,124 cycles

R/H TRANSITION ANGLE STA 500 TO 500A AT RBL 21 HAS SEVERAL SPOTS OF CORROSION. (MARKED) / REMOVED AND INSTALLED NEW R/H TRANSITION ANGLE @ STA500 -500A RBL @ PER SRM 51-40-02.

Part: CAP — CORRODED (FWD CARGO BAY) · airframe 20,347 hrs · 12,124 cycles

R/H TRANSITION ANGLE STA 500A TO 500C AT RBL 21 HAS SEVERAL SPOTS OF CORROSION. (MARKED) / REPLACED R/H TRANSITION ANGLE PER SRM 51-40-02.

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 20,347 hrs · 12,124 cycles

CARGO FLOOR ANGLE WHERE THE LOWER EDGE OF PANEL 121HW ATTACHES AT AFT WALL OF FWD CARGO STA 500D FROM LBL 21 TO RBL 21 HAS SEVERAL SPOTS OF CORROSION. (MARKED) / REMOVED AND REPLACED ANGLE ASSY. PER SRM 51-10-02 AND SRM 51-40-02.

Part: TRACK — ELONGATED (FWD CARGO BAY) · airframe 20,347 hrs · 12,124 cycles

ELONGATED FASTENER HOLE ON UPPER SURFACE OF INTERCOSTAL INCHES FWD OF STA 500D AT LBL 17.24. (MARKED) / REPAIRED CARGO TRACK PER SRM 53-00-53-2R-3 AND EA 1-753-31804.

Part: BRACKET — CRACKED (LT WING) · airframe 20,347 hrs · 12,124 cycles

LEFT WING UPR. SHELF PANEL O/B ATTACH BRACKET IS CRACKED ON FWD. SIDE AT RADIUS. / REMOVED & REPLACED BRACKET PER SRM 51-10-02.

Part: VAPOR BARRIER — CRACKED (WHEEL WELL LH) · airframe 19,921 hrs · 11,858 cycles

BS663; BAY 8L VAPOR BARRIER CRACKED / ACCOMPLISHED INTERIM REPAIR PER SRM 57-10-10-2R-2 REPAIR 2

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,311 hrs · 10,294 cycles

BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01669. R&R BATTERY PACK PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,311 hrs · 10,294 cycles

BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01675. R&R BATTERY PACK PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,311 hrs · 10,294 cycles

BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01673. R&R BATTERY PACK PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,311 hrs · 10,294 cycles

BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01672. R&R BATTERY PACK PER MT.

Part: LENS — BROKEN (CABIN) · airframe 14,466 hrs · 8,617 cycles

R2 DOOR EGRESS LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: COVER — UNSECURE (CABIN) · airframe 12,618 hrs · 7,525 cycles

RIGHT WING DOOR EXIT LIGHT COVER FELL OFF. SECURED COVER IAW SIP.

Part: COVER — UNSECURE (CABIN) · airframe 12,618 hrs · 7,525 cycles

R1 DOOR EXIT LIGHT COVER FELL OFF. SECURED COVER IAW SIP.

Part: COVER — UNSECURE (CABIN) · airframe 12,618 hrs · 7,525 cycles

L2 DOOR EXIT LIGHT COVER FELL OFF. SECURED COVER IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 11,437 hrs · 6,836 cycles

RIGHT OVERWING EXIT EMER BATTERY PACK FAILED CAPACITY CHECK. R & R EMER BATTERY PACK IAW MM.

Part: HYDRAULIC LINE — BROKEN (NR 1 ENGINE) · airframe 5,749 hrs · 3,497 cycles

AIR TURNBACK DECLARED EMERGENCY, NR 1 ENGINE HYDRAULIC FAILURE ON TAKEOFF. BOTH A HYDRAULIC PUMPS ELECTRICAL & ENG CAME ON. NO FLUID LOSS, FOUND NR 1 ENG EDP RETURN LINE BROKEN. R&R NR 1 ENG RETURN LINE & R&R NR 1 ENG EDF IAW AMM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 4,977 hrs · 3,053 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. R & R SIGN IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 4,568 hrs · 2,796 cycles

R2 DOOR EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED SIGN ASSY IAW M/M.

Part: COVER — BROKEN (CABIN) · airframe 4,509 hrs · 2,755 cycles

FLOOR EMERGENCY EXIT LIGHT COVER BROKEN AT ROW 1. REMOVED ADN REPLACED COVER PER AMM.

Part: COVER — MISSING (CABIN) · airframe 4,346 hrs · 2,658 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 3,893 hrs · 2,388 cycles

EMERGENCY EXIT SIGN AT OVERWING EXITS BROKEN. REMOVED, REPLACED AND OPERATIONAL CHECKED OVERWING AISLE EXIT IAW AMM 33-51-01-960-802. OPS CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 3,000 hrs · 1,818 cycles

EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER M/M.

Part: SIGN — BROKEN (CABIN) · airframe 2,965 hrs · 1,792 cycles

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

Part: LATCH — OUT OF ADJUST (COCKPIT) · airframe 2,419 hrs · 1,447 cycles

GEAR DID NOT RETRACT ON TAKEOFF. CYCLED 3 TIMES, OPENED AND STOWED MANUAL GEAR EXTENSION ACCESS DOOR TWICE, GEAR RETRACTED AFTER CYCLING DOOR TWICE. ADJUSTED LATCHES ON MANUAL GEAR EXT ACCESS DOOR PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,346 hrs · 1,391 cycles

FORWARD EEPLS INOP. RELAMPED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 1,146 hrs · 673 cycles

FWD EMERGENCY TRACK LIGHTING LENS MISSING. INSTALLED LENS PER M/M.

Part: COVER — MISSING (CABIN) · airframe 1,052 hrs · 615 cycles

R2 DOOR EMERGENY EXIT SIGN COVER MISSING. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 244 hrs · 139 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.