N496WN

Part: LENS — LOOSE (ZN 200 FUS TOP) · airframe 63,012 hrs · 37,620 cycles

LOWER EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 12 DEF LOOSE; TAPED IN PLACE<[01] COMPLIED WITH EA M-21?133-00720. LENS TAPED IN PLACE

Part: LIGHT — INTERMITTENT (ZN 200 FUS TOP) · airframe 61,711 hrs · 36,805 cycles

EMERGENCY LIGHTS INTERMITTENT<[01] PERFORMED EMERGENCY LIGHTS OPS CK AS PER AMM 33-51-00; OPS CK NORMAL

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 61,711 hrs · 36,805 cycles

L/H OVERWING EXIT AFT EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-01

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 61,711 hrs · 36,805 cycles

R/H OVERWING EXIT SIDEWALL LIGHT INOP<[01] RELAMPED PER AMM 33-51-01

Part: ACTUATOR — INOPERATIVE (ZN 200 FUS TOP) · airframe 60,976 hrs · 36,321 cycles

ELEC STAB TRIM SWITCHES ON YOKE INOP<[01] FOUND CB P6-2 D10 STAB TRIM ACTUATOR OUT. REPLACED ACTUATOR IAW AMM 27-41-71. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 60,332 hrs · 35,901 cycles

RIGHT OVERWING EXIT WINDOW LIGHT INOP. REPLACED RIGHT OVER WING EXIT WINDOW LIGHT FUSE PER REF AMM 33-51-06. OPS CHECK GOOD.

Part: STARTER — SMOKE (#1 ENGINE) · airframe 60,020 hrs · 35,704 cycles

DURING #1 ENG START WITH 7 KNOT TAIL WIND; HAD NO N1 INDICATION. SMOKE & SPARKS OBSERVED FROM THE ENGINE WITH ENG OVERHEAT & FIRE INDICATION. DISCHARGED BOTH FIRE BOTTLES. / [01] REF LOG 1929122 FOR TS; REMOVED AND REPLACED #1 ENG STARTER PER M/M 80-11-01. REMOVED AND REPLACED FWD AND AFT ENG FIRE BOTTLES PER M/M 26-21-01. COMPLIED WITH CONDITIONAL INSP ENGINE FIRE PER M/M 05-51-49 NO DAMAGE FOUND

Part: FIRE BOTTLE — SMOKE (#1 ENGINE) · airframe 60,020 hrs · 35,704 cycles

DURING #1 ENG START WITH 7 KNOT TAIL WIND; HAD NO N1 INDICATION. SMOKE & SPARKS OBSERVED FROM THE ENGINE WITH ENG OVERHEAT & FIRE INDICATION. DISCHARGED BOTH FIRE BOTTLES. / [01] REF LOG 1929122 FOR TS; REMOVED AND REPLACED #1 ENG STARTER PER M/M 80-11-01. REMOVED AND REPLACED FWD AND AFT ENG FIRE BOTTLES PER M/M 26-21-01. COMPLIED WITH CONDITIONAL INSP ENGINE FIRE PER M/M 05-51-49 NO DAMAGE FOUND

Part: FIRE BOTTLE — SMOKE (#1 ENGINE) · airframe 60,020 hrs · 35,704 cycles

DURING #1 ENG START WITH 7 KNOT TAIL WIND; HAD NO N1 INDICATION. SMOKE & SPARKS OBSERVED FROM THE ENGINE WITH ENG OVERHEAT & FIRE INDICATION. DISCHARGED BOTH FIRE BOTTLES. / [01] REF LOG 1929122 FOR TS; REMOVED AND REPLACED #1 ENG STARTER PER M/M 80-11-01. REMOVED AND REPLACED FWD AND AFT ENG FIRE BOTTLES PER M/M 26-21-01. COMPLIED WITH CONDITIONAL INSP ENGINE FIRE PER M/M 05-51-49 NO DAMAGE FOUND

Part: LENS — MISINSTALLED (EMERGENCY LIGHT) · airframe 59,830 hrs · 35,588 cycles

FWD ENTRY DOOR LOWER EMERGENCY LIGHT LENS DIRECTIONAL ARROW IS POINTING THE WRONG DIRECTION / [01] REPLACED EMERGENCY LIGHT LENS AT FWD ENTRY DOOR REF AMM 33-51-01;[02] INSPECTED

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 59,830 hrs · 35,588 cycles

FWD SERVICE DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW / [01] REPLACED FORWARD SERVICE DOOR EMERGENCY LIGHT LENS REF AMM 33-51-01;[02] INSPECTED

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 59,825 hrs · 35,585 cycles

FWD SERVICE DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW / [01] REPLACED FORWARD SERVICE DOOR EMERGENCY LIGHT LENS REF AMM 33-51-01;[02] INSPECTED

Part: LENS — MISINSTALLED (EMERGENCY LIGHT) · airframe 59,825 hrs · 35,585 cycles

FWD ENTRY DOOR LOWER EMERGENCY LIGHT LENS DIRECTIONAL ARROW IS POINTING THE WRONG DIRECTION / [01] REPLACED EMERGENCY LIGHT LENS AT FWD ENTRY DOOR REF AMM 33-51-01;[02] INSPECTED

Part: NONE — INOPERATIVE (PAX CABIN) · airframe 59,797 hrs · 35,569 cycles

EMERGENCY LIGHTS INOP AT POSITIONS: L1 DOOR; R1 DOOR; OVERHEAD BINS 3R/H; 6R/H AND 13R/H. / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M1674 AND M1675 AS PER REF B737 AMM 33-51-06-960-805. EMERGENCY LIGHTS AT POSITIONS: L1 DOOR; R1 DOOR; OVERHEAD BINS 3R/H; 6R/H AND 13R/H TESTED OK.;[02] VERIFIED STEP 1

Part: NONE — INOPERATIVE · airframe 59,797 hrs · 35,569 cycles

EMERGENCY LIGHTS INOP AT POSITIONS: L1 DOOR; R1 DOOR; OVERHEAD BINS 3R/H; 6R/H AND 13R/H. / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M1674 AND M1675 AS PER REF B737 AMM 33-51-06-960-805. EMERGENCY LIGHTS AT POSITIONS: L1 DOOR; R1 DOOR; OVERHEAD BINS 3R/H; 6R/H AND 13R/H TESTED OK.;[02] VERIFIED STEP 1

Part: NONE — OUT OF POSITION (L2 DOOR) · airframe 59,797 hrs · 35,569 cycles

C/R L2 DOOR SLIDE SKIRT RIDES LOW/CATCHES ON DOOR SILL / [01] RE-POSITIONED L-2 DOOR SLIDE SKIRT AND ACCOMPLISHED DOOR OPC IN REF TO MT-725-61-06. SLIDE SKIRT NO LONGER HITS.;[02] VERIFIED STEP 1

Part: NONE — INOPERATIVE · airframe 59,797 hrs · 35,569 cycles

FWD ENTRY L/H LOWER EMERGENCY EXIT SIGN INOP. / [01] REMOVED LAVATORY A TOILET SHROUD FOR ACCESS IAW BOEING 737-7700 AMM 38-32-01-000-802-001.;[02] VERIFIED STEP 1 - REMOVED LAVATORY A TOILET SHROUD FOR ACCESS;[03] TERMINATED GROUND WIRE W4142-0152-20 AT GD3782; OPS CHECK PERFORMED; TEST PASSED PER REF B737 SWPM 20-20-12; AMM 33-51-14-960-801.;[04] VERIFIED STEP 3 TERMINATED GROUND WIRE W4142-0152-20 AT GD3782; OPS CHECK PERFORMED; TEST PASSED;[05] OK TO RE-INSTALL LAV A SHROUD

Part: PLATE — CRACKED (L1 DOOR) · airframe 59,797 hrs · 35,569 cycles

FOUND L-1 DOOR TRESHOLD PLATE CRACKED / [01] REMOVED L-1 DOOR THRESHOLD PLATE AS PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1 <BR>OK TO INSTALL ROBBER PART FROM SWA 205;[03] INSTALLED ROBBED L-1 DOOR THRESHOLD PLATE FROM A/C N205WN AT AIRCRAFT N496WN AS PER B737-700 SRM 51-40-02-0G-0;[04] VERIFIED STEP 3

Part: NONE — CRACKED (CABIN FLOOR) · airframe 59,797 hrs · 35,569 cycles

MAIN CABIN PHOTOLUMINESCENT-STRIP CRACKED AND SCRATCHED NEED TO REPLACE / [01] FAULT RAISED IN ERROR. TASK WILL BE ACCOMPLISHED ON TASK CARD: TTG8Q0039N4C.;[02] VERIFIED 1

Part: BRACKET — CRACKED (R/H MLG W/W) · airframe 59,797 hrs · 35,569 cycles

R/H MLG W/W UPPER CROSS BEAM AT THE ROOT OF THE WING; FWD ATTACH BRACKET CRACKED. DOT #208-40 / [01] REMOVED AND REPLACED BRACKET AT R/H MLG W/W UPPER CROSS BEAM AT THE ROOT OF WING IN REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1 REMOVED AND REPLACED BRACKET AT R/H MLG W/W UPPER CROSS BEAM AT THE ROOT OF WING

Part: FLOOR PANEL — BROKEN (CABIN FLOOR) · airframe 59,797 hrs · 35,569 cycles

FWD CABIN FLOOR PANEL 221GF; CORNER PIECE BROKEN OFF. / [01] PREPARED AREA FOR REPAIR CORNER AT FWD CABIN FLOOR PANEL # 221GF AS PER B737 SRM 53-00-50-2R-10;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED DAMAGED AREA AT FWD CABIN FLOOR PANEL#221GF AS PER B737 SRM 53-00-50-2R-10 MATERIAL USED RESIN PIO#1775480 FIBERGLASS PO#1690463;[04] VERIFIED STEP 3.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,797 hrs · 35,569 cycles

FOUND FWD WET AREA INTERCOSTAL -RBL 15 BETWEEN STA 294.5 AND STA 312 CRACKED AT UPPER FLANGE . / [01] LOCATED AND DRILLED NEW INTERCOSTAL PO#: 1765410 BETWEEN STA 294.5 AND STA 312 RBL 15 ASPER B737-700 SRM 51-40-05-0G-0.;[02] LATE ENTRY <BR>RECEIVED NEW INTERCOSTAL P/N: 141A5410U146TSMRO; PO# 1765410;[03] VERIFIED STEPS 1 AND 2.<BR>OK TO TREAT AND PRIME.;[04] TREATED AND PRIMED NEW HOLES AT NEW INTERCOSTAL ASPER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804.;[05] VERIFIED STEP 4.<BR>OK TO INSTALL NEW INTERCOSTAL.;[06] ADDING TO STEP #1: <BR>PENDING LOCATING AND DRILLING OF FLOOR PANEL FASTENER HOLES AT FWD WET AREA INTERCOSTAL BETWEEN STA 294.5 AND STA 312 RBL 15; AND NUT PLATE INSTALLATION.;[07] INSTALLED INTERCOSTAL BETWEEN STA 294.5 AND 312 RBL15 PER SRM 51-40-02;[08] VERIFIED STEP 7.;[09] LOCATED AND DRILLED OF FLOOR PANEL HOLES AT FDW WET NEW INTERCOSTAL BETWEEN STA 294.5 AND STA 312 RBL 15 AS PER B 737-700 SRM 51-40-05-0G-0;[10] VERIFIED STEP 9.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,797 hrs · 35,569 cycles

FOUND CABIN AREA STIFFENER AT LBL 20 BETWEEN STA 380 AND STA 400 SHOWS MULTIPLE CRACKS AROUND FASTENER HOLES / [01] REMOVED STIFFENER BETWEEN STA. 380 TO STA. 400 LBL. 20'AT MAIN CABIN. REF. SRM. 51-40-02-0G-0-A00729.;[02] VERIFIED REMOVAL OF STIFFENER BETWEEN STA. 380 TO STA. 400 LBL. 20'AT MAIN CABIN.;[03] RECEIVED NEW ANGLE PN #143A5410-170; PO#. 1784756; LOCATED AND DRILLED HOLES AT MAIN CABIN. REF. SRM.51-40-0G-0;[04] CORRECTION TO STEP 3: RECEIVED NEW ANGLE PN #143A5410-170; PO#. 1784756; LOCATED AND DRILLED HOLES AT MAIN CABIN STA 380 TO 400 LBL 20 REF. SRM.51-40-0G-0;[05] VERIFIED STEP 4 RECEIVED; LOCATED AND DRILLED HOLES AT MAIN CABIN STA 380 TO 400 LBL;[06] OK TO REPLACE STIFFENER AT LBL 20 BETWEEN STA 380 AND STA 400;[07] REPLACED STIFFENER AT MAIN CABIN LBL. 20' BETWEEN STA. 380 TO STA. 400. REF. SEM 51-40-02-0G-0.;[08] VERIFIED STEP 7 REPLACED STIFFENER AT MAIN CABIN LBL. 20' BETWEEN STA. 380 TO STA. 400.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,797 hrs · 35,569 cycles

FOUND CABIN AREA STIFFENER AT RBL 15 BETWEEN STA 380 AND STA 400 SHOWS MULTIPLE CRACKS AROUND FASTENER HOLES / [01] REMOVED STIFFENER AT MAIN CABIN BETWEEN STA. 380 TO STA. 400 RBL. 15'. REF. SRM. 51-40-02-0G-0-A00729.;[02] VERIFIED REMOVAL OF STIFFENER AT MAIN CABIN BETWEEN STA. 380 TO STA. 400 RBL. 15;[03] RECEIVED NEW ANGLE PART NUMBER 143A5410-170 PO# 1784756 AT CABIN AREA STIFFENER AT RBL 15 BETWEEN STA 380AND STA 400;[04] VERIFIED NEW REPLACMENT PART.;[05] LOCATED AND DRILLED NEW ANGLE AS PER SRM 51-40-05-OG-0;[06] CORRECTION FOR STEP 5:LOCATED AND DRILLED NEW CABIN AREA STIFFENER AT RBL 15 BETWEEN STA 380 AND STA 400 AS PER SRM 51-40-05-0G-0; PENDING FLOOR TO ANGLE HOLES;[07] VERIFIED STEP 6 LOCATED AND DRILLED NEW CABIN AREA STIFFENER AT RBL 15 BETWEEN STA 380 AND STA 400;[08] OK TO INSTALL NEW STIFFENER;[09] INSTALLED NEW STIFFENER AT MAIN CABIN AREA RBL. 15' BETWEEN STA. 380 TO STA. 400 REF.51-40-02-0G-0;[10] VERIFIED STEP 8 AND 9

Part: NONE — CORRODED (FUSELAGE) · airframe 59,797 hrs · 35,569 cycles

*CORROSION* FOUND AT AFT WET AREA LEFT INNER CHORD BETWEEN BSTA 947.5 AND BSTA 986.5 / [01] INSTALLED EWIS PROTECTION AT AFT WET AREA LEFT INNER CHORD BETWEEN BSTA.947.5 AND BSTA. 986.5 REFERENCE B737-700 AMM 20-60-07-913-801;[02] REMOVED INNER CHORD AT AFT WET AREA STA. 897 TO STA. 998 REFERENCE B 737-700 SRM 51-40-02-0G-0;[03] LATE ENTRY:PARTIALLY REMOVED CORROSION AT AFT WET AREA LEFT INNER CHORD BETWEEN STA 947.5 AND STA 986.5. CORROSION FOUND BEYOND LIMITS. REF 53-70-15-1A-1;[04] VERIFIED INSTALLED EWIS PROTECTION AT AFT WET AREA LEFT INNER CHORD BETWEEN BSTA.947.5 AND BSTA. 986.5;[05] VERIFIED STEP 3 PARTIALLY REMOVED CORROSION AT AFT WET AREA LEFT INNER CHORD BETWEEN STA 947.5 AND STA 986.5. CORROSION FOUND BEYOND LIMITS;[06] VERIFIED STEP 2 REMOVED INNER CHORD AT AFT WET AREA STA. 897 TO STA. 998;[07] LOCATED AND DRILL NEW INNER CHORD REFERENCE B737-700 SRM 51-40-020-0G-0;[08] VERIFIED STEP 7 LOCATED AND DRILL NEW INNER CHORD;[09] OK TO INSTALL NEW INNER CHORD AT AFT WET AREA FROM STA 897 TO STA. 998;[10] INSTALLED NEW INNER CHORD AT AFT WET AREA FROM STA. 897 TO STA. 998 REFERENCE B737-700 SRM 51-40-02-0G-0;[11] VERIFIED STEP 10 INSTALLED NEW INNER CHORD AT AFT WET AREA FROM STA. 897 TO STA. 998;[12] REMOVED EWIS PROTECTION AT AFT WET AREA BETWEEN BSTA 947.5 AND 986.5 REFERENCE AMM 20-60-07-913-801;[13] VERIFIED STEP 12 REMOVED EWIS PROTECTION AT AFT WET AREA BETWEEN BSTA 947.5 AND 986.5

Part: PANEL — CRACKED (AFT CARGO BAY) · airframe 59,797 hrs · 35,569 cycles

AFT CARGO COMP. PANEL 142NW CRACKED / [01] PREPARED FOR REPAIR PANEL 142 NW ;AS PER B737 AMM. 25-52-01-300-805;[02] VERIFIED STEP1. OK TO INSTALL REPAIR;[03] REPAIRED PANEI142 NWQ;AS PER B737 AAM 25-52-01-300-805 MATERIAL USED PO. 1783720 AND PO.1690463;[04] VERIFIED STEP 3.

Part: NONE — CORRODED (FUSELAGE) · airframe 59,797 hrs · 35,569 cycles

CABIN AFT WET AREA FLOOR BEAM AT STA 986 LBL 45 UPPER T CHORD SHOWS AREAS OF CORROSION / [01] REMOVED CORROSION AT CABIN FLOOR BEAM AT STA 986 LBL 45 AS PER B737-700 SRM 51-10-02-0G-0-A00248;[02] VERIFIED STEP 1;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED <BR>TOOL USED : OLYMPUS 27MG B/C 172139 04/22;[04] CORRECTION MIN THK NOTED 0.120';[05] REF TASK CARD: TTG8Q00EE591- M-21-153-00612 (MULTI 737-700- SWA- REPAIR- FUSELAGE- B.S 986.5 UPPER FLOOR BEAM CAP; CORROSION BLENDOUT EXTENDED ALLOWABLE LIMITS) FOR JOB COMPLETION.;[06] VERIFIED ABOVE STEP#5 AS STATED.;[07] CONCURR WITH STEP#5 & 6.<BR>REF TASK CARD: TTG8Q00EE591- M-21-153-00612 (MULTI 737-700- SWA- REPAIR- FUSELAGE- B.S 986.5 UPPER FLOOR BEAM CAP; CORROSION BLENDOUT EXTENDED ALLOWABLE LIMITS) FOR JOB COMPLETION.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,797 hrs · 35,569 cycles

FWD WET AREA INTERCOSTAL BETWEEN STA 294.5 TO STA 312 LBL 11 HAS CORROSION / [01] CLEANED CORROSION AS PER B737-700 SRM 51-10-02-0G-0;[02] VOID STEP 1.;[03] LOSE CABLE FROM THE ELEVATOR ( EA / SECTION) TO FACILITATE SHEET METAL WORK AS PER B737-700 AMM 20-10-91-000-801.;[04] FOUND EXFOLIATED CORROSION AND IS OUT OF LIMITS AS PER B737-700 SRM 53-00-04-1A-1. REMOVED INTER COSTAL AS PER B 737-700 SRM 51-40-02-0G;[05] VERIFIED STEP 3 AND 4;[06] LOCATED AND DRILLED NEW INTERCOSTAL AS PER B737-700 SRM 51-40-05-0G-0;[07] VERIFIED STEP 6;[08] OK TO TREAT AND PRIME.;[09] TREATED AND PRIMED AS PER B737-700 AMM 51-21-72-370-801;[10] VERIFIED STEP 9.;[11] OK TO INSTALL NEW INTERCOSTAL.;[12] (CORECTION TO STEPS 5 AND 7)<BR>(RII) VERIFIED STEPS 3; 4 AND 6.;[13] PARTIALLY INSTALLED NEW INTERCOSTAL AS PER B737-700 SRM 51-40-02-0G-0;[14] INSTALLED INTRCOSTAL BETWEEN STA 294.5 TO STA 312 AND LBL 11 AS PER B737-7 SRM 51-40-02-0G-0;[15] VERIFIED STEP 14;[16] REF STEP 3 ADJUSTED CABLE FROM THE ELEVATOR ( EA / SECTION) WORK ACCOMPLISHED ON TTG8Q0038ZYV;[17] VERIFIED 16

Part: NONE — CORRODED (FUSELAGE) · airframe 59,797 hrs · 35,569 cycles

FWD WET AREA FLOOR BEAM STA 312 LBL 12 HAS CORROSION / [01] INSTALLED PROTECTION EWIS AT FWD WET AREA BETWEEN STA 294.5 TO STA 328 AMM 20-60-07-913-801;[02] REMOVED CORROSION AT FWD WET AREA FLOOR BEAM STA 312 LBL 12 ;EXPLOITED CORROSION AREA FOUND OUT LIMITS SRM 51-10-02-G-0;[03] REMOVED CORROSION AT FWD WET AREA FLOOR BEAM STA 312 LBL 12 ;CORROSION IS ALL THE WAY THRU UPPER CHORD ; AREA FOUND OUT LIMITS. REF SRM 51-10-02-G-0;[04] VERIFIED REMOVAL OF CORROSION AT FWD WET AREA FLOOR BEAM STA 312 LBL 12 AND CORROSION OUT OF LIMITS;[05] VERIFIED INSTALLATION OF EWIS PROTECTION AT FWD WET AREA BETWEEN STA 294.5 TO STA 328;[06] FABRICATED SPLICE ANGLES 4 E/A MATERIAL USED 7075-0; .080' AS PER B737-7 SRM 53-10-51-2R-17 DETAIL G-G.;[07] VERIFIED FABRICATION OF SPLICE ANGLES 4 E/A MATERIAL USED 7075-0; .080';[08] CUT OUT THE DAMED SECTION FROM UPPER CHORD FROM FLOOR BEAM AT STA 312 RBL 27.250'AND LBL 21.500' AS PER B737-700 SRM 53-10-51-2R-17;[16] FABRICATED REPAIR ANGLE AT FLOOR BEAM STA 312 SRM 53-10-51-2R-17 REPAIR 17;[25] LOCATED AND OPENED NEW FASTENER HOLES AT REPAIR 'T' CHORD; SPLICE ANGLES AND SPLICE STRAPS AS PER B737-7 SRM 53-10-51-2R-17.;[32] PARTIAL ISNTALLED 'T' CHORD; SPLICE ANGLES AND SPLICE STRAPS AT FWD WET AREA FLOOR BEAM ;AT STA 312 AS PER B737-700 SRM 51-40-02-0G-0;[33] FABRICATED AND LOCATED NEW FASTENERS HOLES AT TAPER FILLERS ; STA 312 FLOOR BEAM REPAIR AS PER B737-7 SRM 53-10-51-2R-17.

Part: NONE — CORRODED (FUSELAGE) · airframe 59,797 hrs · 35,569 cycles

FWD WET AREA FLOOR BEAM STA 294.5 LBL 11 HAS CORROSION. / [01] INSTALLED EWIS PROTECTION AT FLOOR BEAM STA 294.5 LBL11 AREA . REF<BR>20-60-07-913-801;[02] REMOVED CORROSION AT FWD WET AREA FLOOR BEAM STA 294.5 LBL 11 SRM 51-10-02-0G-0; [14] FABRICATED SPLICE ANGLES 4 E/A MATERIAL USED 7075-0 .080' AS PER B737-7 SRM 53-51-2R-16.;;[26] FABRICATED AND LOCATED FASTENER HOLES AT TAPERED FILLERS MATERIAL USED 7075-T6; .O71'[28] VERIFIED STEPS 26 AND 27 FABRICATED AND LOCATED FASTENER HOLES AT TAPERED FILLERS MATERIAL USED 7075-T6; .O71;[29] OK TO TREAT AND PRIME TAPERED FILLERS;[30] TREATED AND PRIMED TAPERED FILLERS AS PER B737-7 SOPM 20-41-02.;[31] OK TO INSTALL TAPERED FILLERS;[32] INSTALLED TAPERED FILLERS AT FLOOR BEAM REPAIR STA 294.5 AS PER B737-7 SRM 53-10-51-2R-16.;[33] VERIFIED STEP 32 INSTALLED TAPERED FILLERS AT FLOOR BEAM REPAIR STA 294.5;[34] ACCOMPLISHED INSTALLATION AT FLOOR BEAM REPAIR BETWEEN LBL 21 TO RBL 25; STA 294.5 AS PER B737-7 SRM 53-10-51-2R-16.;[35] REINSTALLED INTERCOSTALS' BETWEEN STA 294.5 TO STA 277 RBL 12 STEPS #9 SRM51-40-02-0G-0

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,797 hrs · 35,569 cycles

CABIN AREA STIFFENER AT BL0 BETWEEN STA 380 AND STA 400 SHOWS MULTIPLE CRACKS AROUND FASTENER HOLES / [01] REMOVED STIFFENER AT BL0 BETWEEN STA 380 AND STA 400 AS PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STIFFENER REMOVED;[03] RECEIVED. NEW ANGLE PART NUMBER 143A5410-170 PO# 1784562 AT CABIN AREA STIFFENER AT BL 0 BETWEEN STA 380 AND STA 400;[04] VERIFIED NEW REPLACMENT PART.;[05] LOCATED AND DRILLED NEW ANGLE AS PER SRM 51-40-05-OG-0;[06] CORRECTION TO STEP 5 SHOULD STATE: LOCATED AND DRILLED NEW CABIN AREA STIFFENER AT BL0 BETWEEN STA 380 AND STA 400 AS PER SRM 51-40-05-0G-0; PENDING FLOOR TO ANGLE HOLES;[07] VERIFIED LOCATED AND DRILLED NEW CABIN AREA STIFFENER AT BL0 BETWEEN STA 380 AND STA 400;[08] OK TO INSTALL NEW ANGLE SUPPORT;[09] INSTALLED NEW ANGLE SUPPORT (STIFFENER) AT MAIN CABIN BL 0 BETWEEN STA; 380 TO STA. 400 . REF. SRM. 51-40-02-0G-0.;[10] VERIFIED STEP 9 INSTALLED NEW ANGLE SUPPORT (STIFFENER) AT MAIN CABIN BL 0 BETWEEN STA; 380 TO STA. 400

Part: FLANGE — CRACKED (L/H HORIZ. STAB.) · airframe 59,797 hrs · 35,569 cycles

AFTER REMOVAL OF LT HOR. STAB. RIB 5 FOUND LOWER FLANGE CRACKED BTW STIFENER 2 AND 3 / [01] CUTOUT DAMAGE AT LH HORIZONTAL STAB RIB #5 LOWER FLANGE BTW STIFFENER 2 AND 3 SRM 55-10-09-2R-5 REPAIR 5;[02] VERIFIED STEP 1;[03] PERFORMED A HFEC INSP. PER B737 NDT PART 6 50-00-00 PROC 23. NO CRACKS.<BR>TOOL USED OLYMPUS NORTEC 600 B/C 166317 CAL DUE DATE 10/22.;[04] PERFORMED HFEC ROTO INSP ON FASTENER OPEN HOLES AROUND OF CUTOUT OF LT HOR STA RIB 5 LOWER FLANGE BTW STIFENER 2 AND 3; IAW B 737 NDT PART 6 51-00-00 PROCE 16. TOOL NORTEC 600. BC 166316. CALIB DUE 10-8-22. NO CRACKS FOUND.;[05] ACCOMPLISHED INSURANCE CUT AT RIB 5 CUTOUT AREA IN REF SRM 55-10-09-2R-5;[06] VERIFIED INSURANCE CUT STEP 5.;[07] REF TASK CARDS: TTG8Q00ELGX8; AND TTG8Q00EJK10 FOR STIFFNER AND FLANGE REPAIRS. (22-155-02679 -WIP1); AND (22-155-02679-WIP2);[08] VERIFIED 7

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,797 hrs · 35,569 cycles

FWD WET AREA INTERCOSTAL BETWEEN STA 270 T0 STA 294.5;LBL 12 HAS CORROSION. / [01] CLEANED CORROSION AS PER B737-700 SRM 51-10-02-0G-0;[02] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.048'<BR>TOOL USED : OLYMPUS 27MG B/C 172139 04/22;[03] REMOVED INTERCOSTAL FOR REPLACEMENT AS PER B737-700 51-40-02-0G-0;[04] VERIFIED STEP#3;[05] LATE ENTRY <BR>PART VERIFIED OUT OF LIMITS AS PER DWG# 141A5650;[06] VERIFIED STEP#5 REF./ TO NDT./INSP RETURN INFO.& DRWING NOTES.;[07] RECEIVED NEW PART P/N: 141A5650U3; PO# 1772343; BN: 239959 AND LOCATED AND DRILLED AS PER B737-700 SRM 51-20-07-0G-0; 51-40-05-0G-0; AND DWG#141A5650.;[08] VERIFIED STEP# 7 / VERIFIED NEW PART AT ALL HOLES NO FAULTS EXIST AFTER DRILL PROCES VIA NDT.;[09] INSTALLED NEW NUT-PLATES AT FWD WET AREA INTERCOSTAL BETWEEN STA 270 TO STA 294.5; LBL 12 IN REF TO B737-700 SRM 51-40-10-2R-0.;[10] VERIFIED STEP 9;[11] OK TO INSTALL NEW INTERCOSTAL BETWEEN STA 270 T0 STA 294.5;LBL 12;[12] INSTALLED NEW INTERCOSTAL ;LBL BETWEEN STA 270 TO STA 294.5 LBL 12 REF SRM 51-40-02-0G-0;[13] VERIFIED STEP 12 INSTALLED NEW INTERCOSTAL ;LBL BETWEEN STA 270 TO STA 294.5 LBL 12

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 59,797 hrs · 35,569 cycles

LH HORIZONTAL STABILIZER RIB #5;STIFFENER 3 HAS CRACK. / [01] REMOVED CRACK AT LH HORIZONTAL STABILIZER RIB#5 STIFFENER 3 SRM51-10-02-G-0 AND 55-10-09-2R-4 REPAIR 4;[02] VERIFIED STEP 1;[03] PERFORMED HFEC INSP. ON CUTOUT IN WEB AREA OF THE L/H HORIZ. STAB. RIB #5 STIFF. #3 IAW B737 NDT PART 6 51-00-00 PROC. 23. NO CRACKS; EQUIP: NORTEC 600 B/C 166317 CAL DUE: 10/22;[04] RECEIVED NEW PARTS PO#1728471) LOCATED MEW PARTS AND DRILLER NEW HOLES AT LH HORIZONTAL STABILIZE RIB#5 STIFFENERS' #3 SRM 51-40-05-0ZG-0;[05] (CORRECTION STEP #1)CUT-OUT DAMAGE AT LH HORIZONTAL STABILIZER RIB#5 STIFFENER #3 SRM 51-10-02 AND 55)10-09-2R-4;[06] CORRECTION TO STEP # 1: CUTOUT CRACK AT LH HORIZONTAL STABILIZER RIB#5 STIFFENER 3. SRM 51-10-02-G-0 AND SRM 55-10-09-2R-4 REPAIR 4.;[07] VERIFIED STEPS 4 AND 6;[08] OK TO TREAT AND PRIME NEW HOLES;[09] TREATED AND PRIMED NEW HOLES AT L/H HORIZONTAL STAB RIB #5 STIFFENER 3. REF 51-20-01-0G-0 AND SRM 51-21-72-370-804;[10] OK TO INSTALL NEW REPAIR PARTS;[11] INSTALLED REPAIR PARTS AT LH HORIZONTAL STAB RIB 5 STIFFENER 3 SRM 55-10-09-2R-4 REPAIR 4;[12] VERIFIED STEP 11 -- INSTALLED REPAIR PARTS AT LH HORIZONTAL STAB RIB 5 STIFFENER 3 SRM 55-10-09-2R-4 REPAIR 4

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 59,797 hrs · 35,569 cycles

LH HORIZONTAL STABILIZER RIB #5;STIFFENER 2 HAS CRACK. / [01] CUTOUT DAMAGED AT LH HORIZONTAL STABILIZE RIB 5 STIFFENER 2 SRM 55-10-09-2R-4 REPAIR 4;[02] VERIFIED STEP 1;[03] PERFORMED A HFEC INSP. PER B737 NDT PART 6 50-00-00 PROC 23. NO CRACKS.<BR>TOOL USED OLYMPUS NORTEC 600 B/C 166317 CAL DUE DATE 10/22.;[04] PERFORMED A OPEN HOLE INSP. PER B737 NDT PART 6 50-00-00 PROC 16. NO CRACKS. TOOL USED OLYMPUS NORTEC 600 B/C 166317 CAL DUE DATE 10/22.;[05] REF TASK CARDS: TTG8Q00ELGX8; AND TTG8Q00EJK10 FOR STIFFNER AND FLANGE REPAIRS. (22-155-02679 -WIP1); AND (22-155-02679-WIP2);[06] VERIFIED 5

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 59,797 hrs · 35,569 cycles

HORIZONTAL STABILIZER RIB #5-STIFFINER 4 HAS CRACK AT LOWER POSITION. ADDING TO TITLE.LH HORIONTAL STABILIER RIB #5-STIFFINER 4 HAS CRACK AT LOWER POSITION. / [01] ITEM GENERATED IN ERROR. REFERENCE TTG8Q00EC9 FOR RIB #5 STIFFENER 3 CRACK;[02] CORRECTION FOR STEP 1 SHOULD READ: ITEM GENERATED IN ERROR. REFERENCE TTG8Q00EC9SW FOR RIB #5 STIFFENER 3 CRACK; AND TTG8Q00EC9H7 FOR RIB #5 STIFFENER # 2 CRACK;[03] VERIFIED STEP 1 AND 2

Part: LENS — BROKEN (PAX CABIN) · airframe 59,672 hrs · 35,494 cycles

FLOOR LEVEL EXIT LIGHT LENS BROKEN. / [01] REPLACED L1 DOOR EXIT SIGN PER AMM 33-51-01. OPS GOOD.

Part: SIGN — BROKEN · airframe 59,254 hrs · 35,222 cycles

F/A REPORTS THAT AFT LT EMERG EXIT SIGN BY AFT ENTRY DOOR IS BROKEN / [01] R&R AFT ENTRY-WALL MOUNTED EXIT LIGHT ASSY PER MM 33-51-01

Part: SLIDE — OUT OF ADJUST (AFT SERVICE DOOR) · airframe 59,181 hrs · 35,177 cycles

PROVISIONING REPORTS AFT SERVICE DOOR SLIDE HANGING / [01] REPLACED AFT SERVICE SLIDE IAW AMM 25-66-01.

Part: BRACKET — CRACKED (AFT SERVICE DOOR) · airframe 59,116 hrs · 35,136 cycles

AFT GALLEY SERVICE DOOR LOWER GATE BRACKET IS CRACKED. / [01] R&R AFT GALLEY SERVICE DOOR LOWER GATE BRACKET PER AMM 52-11-31

Part: STRINGER — CRACKED (R/H WING) · airframe 58,565 hrs · 34,791 cycles

RIGHT WING FUEL TANK BETWEEN RIB 19 AND RIB 20; UPPER AFT STRINGER END IS CRACKED. RIGHT WING FUEL TANK BETWEEN RIB 19 AND RIB 20 UPPER AFT STRINGER END IS CRACKED. / [01] REPAIRED DAMAGE IAW EA 22-157-00826;[02] VERIFIED ITEM 1;[03] AUDIT COMPLETE

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 58,565 hrs · 34,791 cycles

A22-08; PASSENGER CABIN FLOOR PANEL 241CF; UPPER SURFACE; PULLED FACE SHEET PLIES. / [01] EVALUATED AND FOUND DAMAGE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED FOR REPAIR IAW SRM 53-00-50-2R-1 PARAGRAPH 3A;C;E;F<BR>VERIFIED BOND MATERIALS AS GLASS-BMS9-3TYH3 (A10273); RESIN-EPOCAST50A1/9816 (A112601) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND;[02] VERIFIED AND OK TO BOND;[03] BONDED REPAIR; TAP TEST GOOD IAW SRM 53-00-50-2R-1 PARAGRAPH 3K;L;M. TOOLING-- OVEN-B0-06 DUE 5-15-22;[04] REPAIRED DAMAGE TO FLOOR BOARD UPPER SURFACE IAW SRM 53-00-50-2R-0 REPAIR GENERAL; SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 58,565 hrs · 34,791 cycles

A22-04; PASSENGER CABIN FLOOR PANEL 231XF; UPPER SURFACE; PULLED FACE SHEET PLIES. / [01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201.<BR>FABRIC (A10273); RESIN (A112601).<BR><BR>REQUESTING OK TO BOND;[02] VERIFIED AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (AAR 30347 EXP 5-15-22. TAP TEST GOOD.;[04] REPAIRED CABIN FLOOR PANEL 231XF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 58,565 hrs · 34,791 cycles

A22-05; PASSENGER CABIN FLOOR PANEL 241AF; UPPER SURFACE; PULLED FACE SHEET PLIES. / [01] EVALUATED DAMAGE; UPPER SURFACE DAMAGE REPAIRABLE IAW B737 SRM 53-00-50-2R-1; TAP TEST GOOD; NO DELAMINATION.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;E;F; AND J.<BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; FIBERGLASS CLOTH BMS9-3 (A10273); RESIN EPOCAST 50A(112601). <BR><BR>REQUIRES OKAY TO BOND REPAIR PLIES.;[02] VERIFIED AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS K; L; AND M. CURED AT 150 DEGREES FOR 4 HOURS; THERMOMETER AAR30347; CAL DUE 4/29/22. TAP TEST GOOD.;[04] REPAIRED PASSENGER CABIN FLOOR PANEL 241AF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 PAR 3.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 58,565 hrs · 34,791 cycles

A22-06; PASSENGER CABIN FLOOR PANEL 231ZF; UPPER SURFACE; PULLED FACE SHEET PLIES. / [01] EVALUATED AND FOUND MISSING FIBER ON UPPER SURFACE AS MARKED. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. RESIN (A112601); FABRIC (A10273).<BR><BR>REQUESTING OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (AAR 30347 EXP 4-29-22). TAP TEST GOOD.;[04] REPAIRED PASSENGER CABIN FLOOR PANEL 231ZF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 58,565 hrs · 34,791 cycles

A22-02; PASSENGER CABIN FLOOR PANEL 242BF; UPPER SURFACE; PULLED FACE SHEET PLIES. / [01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. FABRIC (A10273); RESIN (A112601).<BR><BR>REQUESTING OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (OVEN B0-06 EXP 5-15-22).;[04] REPAIRED PASSENGER CABIN FLOOR PANEL 242BF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 58,565 hrs · 34,791 cycles

EXTERNAL POWER DOOR CUT-OUT LOWER AFT SIDE CRACKED EXTERNAL POWER DOOR CUT OUT LOWER AFT SIDE CRACKED / [01] REMOVED 4EA INITIAL FASTENERS ON SKIN FOR ACCESS. CUT OUT DAMAGED POTION OF SURROUND DOUBLER; PREFORMED 10X INSP. OF TRIM OUT AREA. FOUND NO DAMAGE. WORK ACCOMPLISHED IAW SRM 53-10-15-2R.;[02] VERIFIED MATERIAL FOR -1 DOUBLER. 7075-T6; .050' IAW SRM 53-10-15-2R.;[03] HFEC TRIM OUT AND INTERIOR STRUCTURE IAW B737 NDT PART 6; 51-00-00 PROC 23. NO DEFECTS NOTED. TOOL#31823; DUE 23DEC22;[04] ADD TOO STEP 2 A-TAG #A12177 IAW SRM 53-10-15-2R.;[05] VERIFIED ITEMS 1; 2 AND 3;[06] FABRICATED -1 DOUBLER; LOCATED AND DRILLED REPAIR HOLES TO SIZE COUNTERSUNK AND DEBURRED AS NEEDED IAW SRM 53-10-15-2R.;[07] VERIFIED ITEM 6. OK TO TREAT AND PRIME DOUBLER AND CUTOUT;[08] RE-INSTALLED INITIAL FASTENERS REMOVED ON STEP 1 AND APPLIED ALODINE AND PRIMER TO -1 DOUBLER AND CUT EDGE OF SURROUND DOUBLER IAW SRM 53-10-15-2R.;[09] VERIFIED ITEM 8. OK TO INSTALL REPAIR DOUBLER;[10] INSTALLED -1 DOUBLER LESS RUB STRIP IAW SRM 53-10-15-2R.;[11] VERIFIED ITEM 10;[12] INSTALLED RUB STRIP IAW SRM 53-10-15-2R.;[13] VERIFIED ITEM 12;[14] C/W;[15] VERIFIED ITEM 14. AUDIT COMPLETE

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 58,565 hrs · 34,791 cycles

A22-07; PASSENGER CABIN FLOOR PANEL 241BF; UPPER SURFACE; PULLED FACE SHEET PLIES. / [01] EVALUATED AND FOUND DAMAGE TO UPPER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3A;C;E;F<BR>VERIFIED REPAIR MATERIALS AS GLASS-BMS9-3TYH3 (A10273); RESIN-EPOCAST 50A1/9816 (A112601) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEPS 3K;L;M. TAP TEST GOOD. TOOLING--- OVEN B0-06 DUE 5-15-22;[04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD.;[05] VERIFIED STEPS 3-4

Part: ANGLE — CRACKED (CENTER WING) · airframe 58,565 hrs · 34,791 cycles

CRACK FOUND ON UPPER ATTACH ANGLE IN A/C BAY AT STA 663 LBL 8 / [01] REMOVED ALL FASTENERS IN REPAIR AREA AND TRIMMED OUT DAMAGED SECTION OF UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5[10] INSTALLED REPAIR ANGLES AT STATION 663 CAP SEALED OUTER FASTENERS IAW B737 SRM 57-10-10-2R-5 INTERNAL FASTENERS REQUIRE CAP SEALED;[11] VERIFIED ITEM 10;[12] INTERNAL CENTER TANK FASTENER COLLARS REQUIRE CAP SEAL;[13] BOND TEST CHECK GOOD IAW B737 SRM 57-10-10-2R-5 TOOL 30318 DUE 10-27-22;[14] APPLIED PROTECTIVE FINISH (CIC) IAW B737 SRM 57-10-10-2R-5;[15] VERIFIED ITEMS 13 AND 14;[16] TRIMMED OUT DAMAGED SECTION OF UPPER ATTACH ANGLE IN A/C BAY AT STA 663 LBL 5-15 AND PERFORMED ANGLE REPAIR IAW SRM 57-10-10-2R-5;[17] APPLIED CAPSEAL TO INTERNAL FASTENERS IAW B737 SRM 57-10-10-2R-5;[18] VERIFIED STEP 16; 17 COMPLETE;[19] AUDIT COMPLETE;[20] REQUIRES LEAK CHECK

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 58,565 hrs · 34,791 cycles

A22-03; PASSENGER CABIN FLOOR PANEL 242F; UPPER SURFACE; PULLED FACE SHEET PLIES. / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1. PAR 3 STEPS A;C;E;F; AND J.<BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; FIBERGLASS CLOTH BMS9-3 (A10273); RESIN EPOCAST 50A (A112601). <BR><BR>REQUIRES OKAY TO BOND REPAIR PLIES.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1. PAR 3 STEPS K;L; AND M; CURED AT 150 DEGREES FOR 4 HOURS; OVEN BO-06 CAL DUE 5/15/22. TAP TEST GOOD.;[04] REPAIRED CABIN FLOOR PANEL 242AF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1. PAR 3.;[05] VERIFIED STEPS 3-4

Part: COVER — LOOSE (CABIN) · airframe 58,312 hrs · 34,632 cycles

EXIT ROW LIGHT COVER LOOSE ; / [01] RESECURED EXIT ROW LIGHT COVER REF SIP

Part: NONE — FAILED · airframe 57,868 hrs · 34,354 cycles

SUPPLEMENTAL INFORMATION: AFTER TAKEOFF WITH THE GEAR IN THE UP POSITION. ALL THREE LIGHTS REMAINED ILLUMINATED. ALL QRH CW GEAR AFTER NORMAL LANDING NORMAL WEIGHT LANDING AND NO LIMITATION SPEEDS EXCEEDED.32-62107 LEVER DN FAULT 32-62008 LEVER UP FAULT / 1. TOBIN MIKLAS (TECHNICIAN), 15-DEC-2021 16:39 UTC PERFORMED PSEU BITE PER FIM 32-09 TASK 801, F/C 32-62107 AND F/C 32-62008 CLEARED. OK TO CONTINUE PER MEL 32-16-01 SP32 AND SP 1 C/W. 2. DAVID MABRY (TECHNICIAN), 16-DEC-2021 01:16 UTC REMOVED AND INSTALLED NEW LANDING GEAR HANDLE MODULE REF AMM 32-31-11. ALL OP'S CHECKS GOOD AT THIS TIME

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,717 hrs · 34,270 cycles

RH EMERGENCY EXIT SIDEWALL LIGHT INOP ; / [01] RELAMPED RH OVER WING EXIT WINDOW LIGHT PER AMM 33-21-00 OPS CHECK GOOD

Part: PANEL — ELONGATED (FUSELAGE) · airframe 57,365 hrs · 34,041 cycles

SUPPLEMENTAL INFORMATION: 193D PANEL HOLES ; THE 193D PANEL HAS SEVERAL CRACKED AND ELONGATED HOLES. / [01] REMOVED AND REPLACED 193E IAW AMM 53-51-21

Part: PANEL — ELONGATED (FUSELAGE) · airframe 57,365 hrs · 34,041 cycles

SUPPLEMENTAL INFORMATION: 194E PANEL HOLES ; THE 194E PANEL HAS SEVERAL HOLES ELONGATED AND CRACKED. / [01] REMOVED AND REPLACED 194E PANEL IAW AMM 53-51-21

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 56,978 hrs · 33,796 cycles

RT OVER WING EXIT DOOR LIGHT INOP ; / [01] RELAMPED RH OVER WING EXIT LIGHT AS PER MM 33-22-00

Part: LIGHT — LOOSE (CABIN) · airframe 56,421 hrs · 33,473 cycles

FORWARD OVERHEAD CABIN EXIT INSERT FELL OFF ; / [01] R & R'D MID CABIN OVERWING EXIT LIGHT ASSY PER AMM 33-51-01 OP'S CHECK GOOD

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 54,479 hrs · 32,341 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE PER: SRM 53-60-15-2R-1

Part: FITTING — CRACKED (BS 947) · airframe 54,479 hrs · 32,341 cycles

AFT CARGO BAY FITTING IS CRACKED BS 947 LBL 10 WL 161 / REMOVED CRACKED FITTING AT BS 947 LBL 10 WL 161 IAW SRM 51-40-02-0G-0 DAMAGE LIMITS NOT GIVEN IN SRM PART IS REPLAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0. LOCATED AND DRILLED NEW FITTING IAW SRM 51-40-05-0G-0 OK TO INSTALL 13656R 26SEP2020 INSP 267 9-26-20 INSTALLED NEW FITTING AT BS 947 LBL 10 WL 161 IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A7410 13656R 26SEP2020

Part: FLOOR SUPPORT — CRACKED (BS 400-420) · airframe 54,479 hrs · 32,341 cycles

CRACKED INTERCOSTAL AT FWD CARGO BAY BS 400 TO BS 420 LBL 25 WL 155. REMOVED AND REPLACED INTERCOSTAL AT FWD CARGO BAY BS 400 TO BS 420 LBL 25 WL 155 PO 787275/2, PER SRM 51-40-02-0G-0 AND DWG 143A7505.

Part: FLOOR SUPPORT — CRACKED (BS 927-947) · airframe 54,479 hrs · 32,341 cycles

AFT CARGO BAY INTERCOSTAL CRACKED BS 927-947; RBL 21; WL 165. REMOVED DAMAGED INTERCOSTAL AT BS 927-947 RBL 21, IAW SRM CH 51-40-02. LOCATED AND DRILLED NEW INTERCOSTAL, IAW SRM CH 51-40-05 AND DRAWING 147A7500. 87696C 21SEP20, INSP 317 21SEP20. INSTALLED INTERCOSTAL AT BS 927-947 RBL 21 WL 165, IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A7500. 13656R 27SEP2020.

Part: FRAME — CORRODED (BS 947) · airframe 54,479 hrs · 32,341 cycles

CORROSION ON FUSELAGE FRAME AT BS 947; S-25R WL 162. CORROSION ON FRAME FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES, PER SRM 53-00-07-1A-1 FIG 102 DETAIL C. REMOVED FRAME STR 23R-23L. LOCATED, DRILLED, & INSTALLED NEW FRAME, PER SRM 51-40-02-0G-0; DWG 14700401; DWG 147A1047; DWG 147A0002.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 727-767; R.B.L. 21; W.L. 154. / REMOVED DAMAGE FLOOR TO SIDEWALL SUPPORT AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT BS727-767 RBL 21 WL 154 IAW SRM 51-40-02-0G-0 AND DWG 146A7500

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 875; R.B.L. 21; W.L. 154. / REMOVED CORROSION AND FOUND FLOOR TO SIDEWALL SUPPORT TO BE OUT OF LIMITS IAW SRM CH 53-00-53-1A-2 REMOVED AND REPLACED DAMAGED FLOOR TO SIDEWALL SUPPORT AT BS867-887 RBL21 WL154 IAW SRM CH 51-40-02 AND DRAWING# 146A7500; 146A1282 AND # 147A0060.

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 54,479 hrs · 32,341 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET BS500D S-19R WL193 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; AND DWG 143A7902

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 54,479 hrs · 32,341 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET BS500D STR19L WL193 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 143A7902 93046U 22SEP20

Part: CARGO TRACK — CORRODED (BS 794-812) · airframe 54,479 hrs · 32,341 cycles

CORROSION ON AFT CARGO BAY CARGO TRACK AT BS 794-812; RBL 14; WL 154. REMOVED CORROSION ON AFT CARGO BAY CARGO TRACK BS 794-812; RBL 14; WL 154; .012' DEEP FROM ORIGINAL THICKNESS .070', FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETAIL (D). REMOVED AND REPLACED AFT CARGO BAY CARGO TRACK BS 727-887; RBL 14; WL 154 IAW DWG 146A7500 AND DWG 146A0061 AND SRM 53-00-53-2R-3 FIG 203 DETAIL (A).

Part: SUPPORT — CORRODED (BS 947) · airframe 56,639 hrs · 33,610 cycles

***CORROSION*** ON AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT B.S. 947; L.B.L. 21 - R.B.L. 21; W.L. 154. / REMOVED CORROSION DAMAGED ACB AFT BULKHEAD CENTER SUPPORT LOWER AT BS 947 LBL21-RBL21 WL154 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW LOWER CENTER SUPPORT IAW SRM 51-40-05-0G-0 AND INSTALLED IAW SRM 51-40-02-0G-0 AND BOEING DWG 149A8118 13656R 27SEP2020

Part: CARGO TRACK — CORRODED (BS 400) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON TRACK TIEDOWN AT FWD CARGO BAY BS400 LBL18 WL156. / REMOVED CORROSION FROM FCB TRACK TIE DOWN BS 400; LBL 18; WL 156 IS .055' REMOVED FROM .040' ALLOWABLE AND FOUND OUT LIMITS PER SRM 53-00-53-1A-2 FIG 103; G. REMOVED FCB TRACK TIE DOWN BS 400; LBL 18; WL 156 PER SRM 51-40-02-0G-0; INSTALLED NEW FCB TRACK TIEDOWN; BS 400-500D; LBL 18; WL 156 PER SRM 51-40-02-0G-0; DWG 143A7500; DWG 143A7902 93114U 26SEP20

Part: SHIELD — CORRODED (BS 847-867) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY SHIELD AT B.S. 847-867; R.B.L. 21; W.L. 154. / REMOVED AFT CARGO BAY SHIELD AT B.S. 847-867; RBL 21; WL 154 I.A.W. SRM 51-40-02 DUE TO CORROSION BEING OUT OF LIMITS. LOCATED; DRILLED AND INSTALLED NEW SHIELD I.A.W. SRM 51-40-02-0G-0 SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND DWG 146A0081

Part: SHIELD — CORRODED (BS 767-794) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY SHIELD AT B.S. 767-794; R.B.L. 21; W.L. 154. / REMOVED CORROSION DAMAGED SHIELD IN ACB AT BS 767-794 RBL 21 WL 154 LOCATED NEW SHIELD DRILLED COUNTERSINK AND INSTALLED ALL IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 SRM 51-40-08-0G-0 AND BOEING DWG 146A0081 13656R 19SEP2020

Part: SHIELD — CORRODED (BS 500-500A) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL24 WL156. / CORROSION ON SHIELD P/N 143A8126-19 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; REMOVE SHIELD BS500-500A; RBL 24; WL 156 PER SRM 51-40-02-0G-0; INSTALLED NEW FCB SHIELD AT BS500-500A; RBL 24; WL156 PER SRM 51-40-02-0G-0; DWG 143A0080 93114U 22SEP20

Part: SUPPORT — CORRODED (BS 887-947) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 887-947; R.B.L. 21; W.L. 154. / REMOVED CORRODED FLOOR TO SIDEWALL SUPPORT AT BS887-947 RBL21 WL154 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0 INSTALLED IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A7500 13656R 27SEP2020

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 56,513 hrs · 33,533 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL156. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 P.O#793814-1 PER SRM 51-40-02-0G-0 AND DWG 143A7505

Part: SHIELD — CORRODED (BS 420-440) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL23 WL156. / REMOVED CORROSION DAMAGED SHIELD AT FCB BS 420-440 RBL 23 WL 156 LOCATED DRILLED AND INSTALLED NEW SHIELD ALL IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0 13656R 18SEP2020

Part: ATTACH ANGLE — CRACKED (BS 500B) · airframe 56,513 hrs · 33,533 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL25 WL156. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL25 PER SRM 51-40-02-0G-0 AND DWG 143A7505

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 56,513 hrs · 33,533 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C AFT SIDE LBL25 WL156. / REMOVED AND INSTALLED NEW ATTACH ANGLE AT FWD CARGO BAY BS500C AFT SIDE LBL25 PER SRM 51-40-02-0G-0 AND DWG143A7505

Part: ATTACH ANGLE — CRACKED (BS 400) · airframe 56,513 hrs · 33,533 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155 P.O#79781111 PER SRM 51-40-02-0G-0 AND DWG 143A7505

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156. / CORROSION ON FLOOR TO SIDEWALL SUPPORT P/N 143A7501-186 FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENERS HOLES PER SRM 53-00-53-1A-2 FIG 103; D. REMOVED FCB FLOOR TO SIDEWALL SUPPORT BS 500A-500D; RBL 23 PER SRM 51-40-02-0G-0; INSTALLED NEW FCB FLOOR TO SIDEWALL SUPORT AT BS 500A-500D; RBL 23; WL 156 PER SRM 51-40-02-0G-0; DWG 143A7500 93114U 26SEP20

Part: CARGO TRACK — CORRODED (BS 400) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON TRACK TIEDOWN AT FWD CARGO BAY BS400 RBL13 WL156. / REMOVED CARGO TRACK TIEDOWN BS396-BS500D RBL 13 WL 156; INSTALLED NEW CARGO TRACK TIEDOWN I.A.W BOEING DWG 143A7500; 143A7902; SRM 51-40-02-0G-0.

Part: GUSSET — CRACKED (BS 500D S21R) · airframe 54,479 hrs · 32,341 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-21R WL177. / REMOVED DAMAGED BKD SUPPORT GUSSET AND INSTALLED NEW BKD SUPPORT GUSSET AT BS 500D S-21R WL 177 IAW SRM 51-40-02-0G-0 AND DWG 143A7902.

Part: THRESHOLD WEB — CORRODED (FUSELAGE) · airframe 56,658 hrs · 33,620 cycles

***CORROSION*** ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS440 - BS492 RBL28 WL156. / DAMAGE EVALUATION ON FCB SUB-THRESHOLD WEB BS440-492; RBL28; WL156 WAS FOUND TO BE OUT OF LIMITS. DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-30-15. REMOVED AND INSTALLED NEW FCB SUB-THRESHOLD WEB BS440-492; RBL28; WL156 PER DWG 143A8330; AND SRM 51-40-02 87713U 22SEP20

Part: CARGO TRACK — CORRODED (BS 790 LBL 18) · airframe 54,479 hrs · 32,341 cycles

CORROSION ON AFT CARGO BAY CARGO TRACK TIE DOWN AT B.S. 790; L.B.L. 18; W.L. 154. / CORROSSION ON TIE DOWN TRACK MEASURED .040 DEEP IN .060 THCK ORIGINAL THICKNESS FOUND OUT OF LIMITS. REMOVED TRACK 727-807; REMOVED NEW TRACK LOCATED DRILLED & INSTALLED PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 53-00-53-1A-2; DWG 146A7500

Part: ATTACH ANGLE — CRACKED (BS 500A) · airframe 56,513 hrs · 33,533 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500A FWD SIDE LBL25 WL156. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS 500A FWD SIDE LBL 25 WL 156 P.O # 803728/1 PER SRM 51-40-02-0G-0; AND DWG 143A7505

Part: SUPPORT — CORRODED (BS 727-847) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 727-847; L.B.L. 21; W.L. 154. / DAMAGE EVALUATION ON ACB FLOOR TO SIDEWALL SUOPORT BS727-847; LBL 21; WL 154. WAS FOUND TO BE OUT OF LIMITS; DUE TO PROXIMITY TO HOLES. PER SRM 53-00-53. REMOVED AND INSTALLED NEW ACB FLOOR TO SIDEWALL SUOPORT BS727-847; LBL 21; WL 154. PER DWGS 146A7500; 146A0061; 140N4500; SRM 51-40-02. 87713U 25SEP20

Part: FLOORBEAM — CORRODED (BS 887) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 887; L.B.L. 21 - R.B.L. 21; W.L. 154. / REMOVED ACB FLOOR PANEL SUPPORT AT BS 887 RBL21-LBL21 WL 154 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-05-0G-0 COUNTERSUNK IAW SRM 51-40-08-0G-0 AND INSTALLED IAW SOPM 20-50-01 AND BOEING DWG 146A7500 AND 147A7500 13656R 27SEP2020

Part: WEB — CORRODED (BS 801-805) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY WEB AT B.S. 801-805; R.B.L. 20; W.L. 151. LOCATED UNDER TENSION STRAP. / REMOVED AND REPLACED WEB ASSY B.S.801-847 RBL20 WL151 PER SRM 51-40-02-0G-0 DWG 146A8120 DWG 146A8340

Part: NUT PLATE — CORRODED (BS 795) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY NUT PLATE STRAP UNDER TENSION STRAP AT B.S. 795; R.B.L. 20; W.L. 153. / REMOVED AND REPLACED NUT PLATE SCRAP B.S. 795 RBL 20 WL 153 PER SRM 51-40-02-0G-0 DWG 146A8120 DWG 146A8340

Part: WEB — CORRODED (CARGO THRESHOLD) · airframe 56,658 hrs · 33,620 cycles

***CORROSION*** ON AFT CARGO BAY DOOR THRESHOLD SUBWEB AT B.S. 794-847; R.B.L. 24; W.L. 154. / REMOVED CORROSION ON AFT BAY SUB THRESHOLD WEB AT BS 794-847; RBL 24 FOUND OUT OF LIMITS TO PROXIMITY TO HOLES PER SRM 53-00-53-A1-/1 FIG 103D AND REMOVED AND REPLACED AFT CARGO BAY DOOR THRESHOLD SUBWEB AT B.S. 794-847 IAW PER DWG 146A8340 92421U 09-26-20

Part: FLOORBEAM — CORRODED (BS 772) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 772; L.B.L 21 - R.B.L. 21; W.L. 154. / RECEIVED NEW SERVICEABLE SUPPORT ON SWA P.O.# 801448/1 NEW SUPPORT WILL BE INSTALLED ON SWA CARD# JPANEL-141-CLOSE

Part: SUPPORT — CORRODED (BS 500D) · airframe 56,639 hrs · 33,610 cycles

***CORROSION*** ON BULKHEAD TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500D LBL25 WL157. / REMOVED AND REPLACED BULKHEAD TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500D LBL25 WL157 P.O# 800572 /1 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 143A9481 AND DWG 143A7902 93046U 26SEP20

Part: FLOORBEAM — CORRODED (BS 727D) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 727D+4; L.B.L. 21 - R.B.L. 21; W.L. 154. / RECEIVED NEW SERVICEABLE SUPPORT ON SWA P.O.# 803241/1 NEW SUPPORT WILL BE INSTALLED ON SWA CARD# JPANEL-141-CLOSE

Part: STRAP — CORRODED (BS 798-809) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON AFT CARGO BAY TENSION STRAP AT B.S. 798-809; R.B.L. 21; W.L. 154. / REMOVED AND REPLACED TENSION B.S.798-809 RBL21 WL154 PER SRM 51-40-02-0G-0 DWG 146A8120 DWG 146A834

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS420 - BS500D LBL23 WL156. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS420-BS500D P.O# 80365511 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 143A7500; AND DWG 143A7505

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 54,479 hrs · 32,341 cycles

RT WING O/B AFT FLAP UPPER SURFACE IS DELAMINATED FROM I/B END TO 17' O/B FROM I/B END. / REMOVED & REPLACED RT OB AFT FLAP IAW MM 27-51-22-000-801 AND MM 27-51-22 400-801 ADJUSTMENT CHECK GOOD IAW MM 27-51-22-400-801 ALL TORQUES VERIFIED. (POS:RT O/B;TAG NO.:737643;P/N OFF/ON:113A3700-8;S/N OFF:000176;S/N ON:00432)

Part: STRINGER — CRACKED (BS 536) · airframe 54,479 hrs · 32,341 cycles

END OF STR 26L IN SNAKE PIT BS 536 WL 152 IS CRACKED AT FASTENER HOLES. REPAIRED S-26L AT BS 500D+11'-BS 540 INSTALLED NEW STRINGER SECTION, IAW SRM 53-00-03-2R-1 REP 1 AND REMOVED DAMAGED STRINGER SECTION, IAW SRM 53-00-03-2R-1 REP 1.

Part: SKIN — DENTED (BS 440) · airframe 54,479 hrs · 32,341 cycles

FUSELAGE SKIN HAS DENT BS 440+6' 1' ABOVE STR 18L. REPAIRED PER SRM 53-00-01-2R-36 (REPAIR 36). UPON FURTHER INVESTIGATION DENT WAS FOUND TO BE A PREVIOUS BLEND. BLEND MEASURED 1. X .9' X .007' ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS, PER SRM 53-00-01-1A-1. CUT OUT DAMAGE AND REPAIRED SKIN, PER SRM 53-00-01-2R-36 (REPAIR 36).

Part: STRAP — CORRODED (BS 270 LBL11-14) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** UPPER CHORD STRAP BS 270 FLOOR BEAM LBL 11-14 WL 207 / REMOVED UPPER CHORD STRAP BS270; FABRICATED AND INSTALLED I.A.W ALL REQUIREMENTS ON EA-1-A53-13812 DATED 31DEC14. REMAINIG FASTENER TO BE INSTALLED ON CARD U215694 COCKPIT 5001

Part: FLOORBEAM — CRACKED (BS 540) · airframe 54,479 hrs · 32,341 cycles

FLOOR SUPPORT CRACKED AT BS 540 BL0-LBL 25 WL 208. REPLACED CRACKED FLOOR SUPPORT AT BS 540 BL 0-LBL 25 WL 208, PER SRM 51-40-02-0G-0; DWG 143A0060. 57449U 17SEP20.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 54,479 hrs · 32,341 cycles

FLOOR SUPPORT CRACKED BS 540 BL 0-RBL 25 WL 208. REPLACED CRACKED FLOOR SUPPORT AT BS 540 BL 0-RBL 25 WL 208, PER SRM 51-40-02-0G-0; DWG 143A0060. 57449U 17SEP20

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 54,479 hrs · 32,341 cycles

MECHANICAL DAMAGE TO SEAT TRACK CROWN BS 520 LBL 25 WL 208. REMOVED MECHANICAL DAMAGE ON SEAT TRACK CROWN BS 520 LBL 25 WL 208, PER SRM 51-10-02-0G-0. MAX MATERIAL REMOVED WAS 1' X 2' X .023'. DAMAGE FOUND TO BE OUT OF LIMITS, PER SRM 53-00-52-1A-1. REMOVED AND REPLACED SEAT TRACK BS 480-520 LBL 25 WL 208, PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; BOEING DWG 143A5300; AND BOEING DWG 143A5310.

Part: FLOORBEAM — CORRODED (BS 259) · airframe 54,479 hrs · 32,341 cycles

CORROSION AFT CHORD BS 259 FLOOR BEAM LBL 9-RBL 8 WL 207. REPAIRED CHORD AT BS 259 LBL 9-RBL 8 WL 207, IAW ER 20-03288 REV IR AND ER 20-153-01899 REV IR.

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 54,479 hrs · 32,341 cycles

MECHANICAL DAMAGE TO SEAT TRACK CROWN BS 520 LBL 45 WL 208. REMOVED MECHANICAL DAMAGE ON SEAT TRACK CROWN BS 520 LBL 45 WL 208, PER SRM 51-10-02-0G-0. DAMAGE REMOVAL AREA WAS FOUND TO BE 1' X 3' X .030'. DAMAGE FOUND TO BE OUT OF LIMITS, PER SRM 53-00-52-1A-1. REMOVED AND REPLACED SEAT TRACK BS 480-520 LBL 45 WL 208, PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; BOEING DWG 143A5300; AND BOEING DWG 143A5310.

Part: SEAT TRACK — DAMAGED (BS 500A) · airframe 54,479 hrs · 32,341 cycles

TAB IS BROKEN OFF OF SEAT TRACK BS 500A+18 RBL45 WL208 / REMOVED SEAT TRACK BS480-520 RBL45 PER SRM 51-40-02-0G-0. INSTALLED NEW SEAT TRACK PER SRM 51-40-02-0G-0 AND DWG 143A5300 AND DWG 143A5400.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 54,479 hrs · 32,341 cycles

INTERCOSTAL CRACKED AT BS 344-360 LBL 11 WL 208. REMOVED AND REPLACED CRACKED INTERCOSTAL AT BS 344-360, LBL11, WL208, PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. AND BOEING DWG 141A5400.

Part: ANGLE — CRACKED (BS 663) · airframe 54,479 hrs · 32,341 cycles

BS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT RBL 8 WL 164. REPAIRED PER SRM 57-10-10-2R-5.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 54,479 hrs · 32,341 cycles

LT HORIZ STAB RIB AT STA 120.30 2ND VERT STIFFENER IS CRACKED. REPAIRED LT HORIZONTAL STABILIZER RIB AT STAB STA 120.30 2ND VERTICAL STIFFENER, IAW SRM 55-10-09-2R-4. 59796C 18SEP20.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 54,479 hrs · 32,341 cycles

LT HORIZ STAB RIB AT STA 120.30 4TH VERT STIFFENER IS CRACKED. REPAIRED LT HORIZONTAL STABILIZER RIB AT STAB STA 120.30 4TH VERTICAL STIFFENER, IAW SRM 55-10-09-2R-5. 59796C 18SEP20.

Part: SKIN — CORRODED (BS 887-967 S2L-R) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** ON FUSELAGE SKIN UNDER DORSAL FIN BS887 - BS967 S-2L TO S-2R WL306. / REPAIRED DAMAGE ON FUSELAGE SKIN UNDER DORSAL FIN BS 887-967 STR 2L TO 2R; WL 306 PER ER 20-03307 REV IR AND EA 20-153-01902 REV IR.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,479 hrs · 32,341 cycles

LT HORIZONTAL STAB RIB CRACKED STA 120.30 3RD RIB 28' AFT OF FRONT SPAR. REPAIRED LT HORIZ STAB RIB AT STAB STA 120.30 3RD VERT STIFFENER (RIB) 28' AFT OF FRONT SPAR, IAW SRM 55-10-09-2R5 AMM 51-31-00-390-805 AND BAC DRAWINGS 002A0001; 182A1500; 182A3001; 182A2401.

Part: SUPPORT BEAM — WORN (BS 536) · airframe 54,479 hrs · 32,341 cycles

WING CENTER SECTION LOWER SUPPORT BEAM LOWER CHORD BS 536.956+6' RBL 40.875 WL 156 IS WORN COMMON TO STRIKER PLATE. REPAIRED WING CENTER SECTION LOWER SUPPORT BEAM LOWER CHORD AT B/S 536.956+6' RBL 40.875, IAW SRM 57-10-13-2R-3 REPAIR 3. 59900U 24SEP20.

Part: DOOR SILL — CORRODED (LT OVRWNG EXIT) · airframe 54,479 hrs · 32,341 cycles

***CORROSION*** CORROSION ON L/H OVERWING EXIT LOWER SILL BS629 LBL59 WL221 / REMOVED L/H OVERWING EXIT LOWER SILL AND INSTALLED NEW PER SRM 51-40-02-0G-0 AND DWG 144A8201 AND DWG 144A8803. PRIOR TO REPLACEMENT. REMOVED CORROSION ON OVERWING EXIT LOWER SILL BS 629. LBL 59. WL 221 IN AN AREA OF 1' X 1' WITH A MAX DEPTH OF .016'. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-15-1A-1 AND SRM 51-10-02-0G-0. 53838C 23SEP20

Part: TRACK — DAMAGED (HORIZONTALS TAB) · airframe 54,479 hrs · 32,341 cycles

RIGHT HAND HORIZONTAL STAB PANEL 343AT SHARK FIN FWD SLIDE TRACK ON FUSELAGE IS DAMAGED / REMOVED AND REPLACED SHARK FIN FWD SLIDE TRACK ON FUSELAGE FOR RT HORIZONTAL STAB PANEL 343AT IAW MM 20-50-11-910-801.

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 54,479 hrs · 32,341 cycles

FLIGHT DECK FLOOR IS DENTED AT BS 255; RBL 4-LBL 14; WL 207.54. THE DAMAGE IS REPAIRED, PER EA 1-A53-33179 REV 1 WITH A CONCURRENT REPAIR NOTED IN EA 20-153-01899 REV IR NRC U251986 AND ER 20-03288 REV IR.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 52,465 hrs · 31,063 cycles

L/H OVER WING EXIT SIGN HAD LAMPS INOP/ RELAMPED SIGN IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 51,846 hrs · 30,650 cycles

EMERGENCY AISLE LIGHTS AT FUSELAGE STATION 727A AND 727E F/O'S SIDE INOP. REPAIRED SOCKET AT L1065 AND RELAMPED BOTH AISLE LIGHTS PER AMM, REPLACED FUSE AT BATTERY PACK M1672 PER CMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,603 hrs · 30,482 cycles

L/H AFT EXTERIOR EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LGIHTS) · airframe 50,960 hrs · 30,074 cycles

R/H EMERGENCY EXIT ROW SIDE WALL LIGHT NOP. R&R FUSE PER MM.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 50,385 hrs · 29,695 cycles

LH WING I/B AFT CORNER OF OUTBOARD FLAP IS DISBONDED. PERFORMED TEMP. REPAIR TO L/H INBOARD AFT CORNER PER SRM 57-53-01 1A-4. MAKE A DETAILED INSPECTION OF THE DAMAGED AND SPEED TAPE AT A DAILY INTERVAL. ALSO PERFORM A DAILY DETAILED ON THE SURROUNDING FASTNERS FOR ANY INDICATION OF PULLED FASTENERS OR CRACK INITIATION. REFER TO 51-00-06 FOR THE INSPECTION PROCEDURE COMPLIED WITH DAILY REINSPECT PER SRM 57-53-01 NO FURTHER DAMAGE NOTED REMAINS ON MX NOTE

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 50,385 hrs · 29,695 cycles

REF NON ROUTINE G646112 RIGHT WING I/B AFT CORNER OF OUTBOARD FLAP IS DISBONDED. PERFORMED TEMP REPAIR TO RIGHT WING I/B AFT CORNER PER SRM 57-53-01-1A-4 MAKE A DETAILED INSPECTION OF THE DAMAGED AND SPEED TAPE AT A DAILY INTERVAL. ALSO PERFORM A DAILY (DET) ON THE SURROUNDING FASTENERS FOR ANY INDICATION OF PULLED FASTENERS OR CRACK INITIATION. REFER TO 51-00-06 FOR THE INSPECTION REF DMA # 0761993 COMPLIED WITH DAILY REINSPECT PER SRM 57-53-01 NO FURTHER DAMAGE NOTED. CONTINUE PER MX NOTE TRACKING# 52927

Part: WEDGE — DEBONDED (LEFT WING) · airframe 50,385 hrs · 29,695 cycles

INBOARD AFT CORNER OF OUTBOARD AFT TRAILING EDGE FLAP DISBONDED. AREA MEASURES 1/2' WIDE FROM TRAILING EDGE AND 2 3/4' LONG FROM INBOARD EDGE / REPAIRED FLAP TE WEDGE PER SRM 51-70-10-2R-1 (PERMANENT) CL #56256

Part: FLAP — DEBONDED (R/H WING) · airframe 50,385 hrs · 29,695 cycles

RIGHT WING I/B AFT CORNER OF OUTBOARD FLAP IS DISBONDED .AREA MEASURES 1.343 ' LONG FROM I/B EDGE AND .718' WIDE FROM TRAILING EDGE. / RH OUTBD AFT FLAP WAS R&R'D ON ACTION LOG PG 0126212

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 49,922 hrs · 29,422 cycles

R1 DOOR GIRT BAR OUT OF ADJUSTMENT. SECURED GIRT BAR PER AMM.

Part: SENSOR — FAULTY (LE FLAP) · airframe 49,874 hrs · 29,396 cycles

AIR TURNBACK, LEADING EDGE FLAP TRANSIT LIGHT REMAINED ILLUMINATED AFTER FLAP RETRACTION. R&R FLAP NR 1 SENSOR 168 PER AMM.

Part: HANDLE — BROKEN (L1 DOOR) · airframe 49,137 hrs · 28,915 cycles

L1 DOOR ASSIST HANDLE BROKEN. R&R HANDLE PER SIP.

Part: FITTING — LOOSE (L2 DOOR) · airframe 49,037 hrs · 28,846 cycles

L2 DOOR AFT GIRT BAR FITTING LOOSE. SECURED FITTING IAW SOPM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 49,037 hrs · 28,846 cycles

AFT CARGO DOOR CUT OUT AFT LOWER CORNER SCUFF PLATE CRACKED. R&R SCUFF PLATE IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,037 hrs · 28,846 cycles

LT OVER THE WING EMERGENCY EXIT DOORS INTERNAL LIGHTS INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,037 hrs · 28,846 cycles

RT OVER THE WING EMERGENCY EXIT DOORS INTERNAL LIGHTS INOP. RELAMPED LIGHT PER AMM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,037 hrs · 28,846 cycles

RT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STA 129.5 3RD RIB. REPAIRED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,037 hrs · 28,846 cycles

RT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STA 129.5, 4TH RIB. REPAIRED STIFFENER PER SRM.

Part: SERVICE DOOR — CRACKED (MAIN CABIN) · airframe 49,037 hrs · 28,846 cycles

REMOVE AND REPLACE R1 DOOR DUE TO CRACKS IN #4 AND #5 BEAM / REMOVED FWD SVC DOOR IAW AMM 52-11-00-000-802 57229C 08NOV18 REPLACED FWD SERVICE DOOR PO 717092 IAW AMM 52-41-00-400-801; ADJUSTED DOOR IAW AMM 52-41-00-820-801 AND EA 1-752-2370 (POS:FSD; TAG NO:474696; P/N OFF:141A6516-18; S/N OFF:001630; P/N ON:141A6516-14; S/N ON:000905) (POS:FSD; TAG NO:454668; P/N OFF:141A6516-14; S/N OFF:000905; P/N ON:141A6516-18; S/N ON:001529)

Part: RETAINER — CRACKED (LT WING) · airframe 49,037 hrs · 28,846 cycles

L/H WING AFT BULB SEAL BRACKET ABOVE SAIL FAIRING AT ORSS 271 HAS A CRACK / REMOVED + REPLACED SEAL BRACKET FITTING + WEB IAW SRM 51-40-02-0G-0 PAR 4 + 9 ON L/H WING ABOVE SAIL FAIRING AT ORSS 271

Part: PANEL — CRACKED (LT WING) · airframe 49,037 hrs · 28,846 cycles

L/H TRAILING EDGE WING PANEL 561AB HAS CRACKS ON THE BACK SIDES OF FASTENER HOLES (MARKED) / REPAIRED LH TRAILING EDGE WING PANEL 561AB CRACKS ON BACKSIDES OF FASTENER HOLES I.A.W 737 SRM 57-51-01-2R-1 PARA 1;4C TABLE 202; 200Ï¿½F CURE PER SRM 51-70-04 REPAIR 9; DAMAGE PAST ALLOWABLE LIMITS I.A.W 737 SRM 57-51-01-1A-1 PARA 1;4B(1)(2); DAMAGE TO FIBERGLASS PLIES.

Part: BATTERY — FAILED (CABIN) · airframe 46,268 hrs · 27,056 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 46,268 hrs · 27,056 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER DWG AND AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 46,268 hrs · 27,056 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST M1675. R & R THE BATTERY IAW DWG AND AMM.

Part: BATTERY — FAILED (CABIN) · airframe 46,268 hrs · 27,056 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER DWG AND AMM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 46,268 hrs · 27,056 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 46,268 hrs · 27,056 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PER DWG AND AMM.

Part: BRACKET — PULLED (RT WING) · airframe 46,268 hrs · 27,056 cycles

RIGHT WING ATTACH BRACKET(WIGGLE PLATE) FOR LOWER AFT SHELF PANEL 651GB HAS PULLED FASTENERS. / R&R'D RIGHT WING ATTACH BRACKET(WIGGLE PLATE) FOR LOWER AFT SHELF PANEL 651GB REF SRM 51-40-02 AND AMM 20-50-11.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 46,268 hrs · 27,056 cycles

HORIZONTAL STABILIZER LEFT FORWARD UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED HORIZONTAL STABILIZER LEFT FORWARD UPPER SLIDING SEAL PER AMM. 53-31-31

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 46,268 hrs · 27,056 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M1668. R & R THE BATTERY IAW DWG AND AMM.

Part: RETAINER — CRACKED (LT WING) · airframe 46,268 hrs · 27,056 cycles

VERTICAL BULB SEAL RETAINER CRACKED ABOVE WIGGLE PLATE IN T/E SHELF AREA. / R/R VERTICAL BULB SEAL RETAINER ABOVE WIGGLE PLATE IN T/E SHELF AREA IAW SRM 51-40-02 AND M/M 20-50-11

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 46,268 hrs · 27,056 cycles

RIGHT HORIZONTAL STABILIZER AFT UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER AFT UPPER SLIDING SEAL PER SRM 51-40-02

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 46,268 hrs · 27,056 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M1669. R & R THE BATTERY IAW DWG AND AMM.

Part: SUPPORT BRACKET — CRACKED (LWR FUSELAGE) · airframe 46,268 hrs · 27,056 cycles

FUSELAGE WING TO BODY FAIRING SUPPORT BRACKET CRACKED BETWEEN FAIRINGS 191AR AND 195AR. / REMOVED AND REPLACED FUSELAGE WING TO BODY FAIRING SUPPORT BRACKET IAW SRM 51-10-02

Part: COVER — MISSING (CABIN) · airframe 45,227 hrs · 26,405 cycles

L2 DOOR EMERGENCY LIGHT COVER MISSING. REINSTALLED COVER PER AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 43,648 hrs · 25,454 cycles

RT WING OUTBD AFT FLAP LOWER SKIN DELAMINATED AT INBD END. REPAIRED FLAP PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,949 hrs · 25,054 cycles

RIGHT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

LT INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

LT INTERCOSTAL CRACKED AT BS 330 TO BS 348. R&R INTERCOSTAL PER SRM & DWG.

Part: STRINGER CLIP — CRACKED (BS 727D) · airframe 42,334 hrs · 24,683 cycles

STRINGER CLIP AT 8R CRACKED, BS 727D. R & R THE STRINGER CLIP IAW SRM AND DWG.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 42,334 hrs · 24,683 cycles

G-1 GALLEY EXIT LIGHT LENS CRACKED. R & R THE EMERGENCY LIGHT LENS IAW AMM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

AFT CARGO LT ZEE CHANNEL CORRODED BETWEEN BS 727E TO BS 767. REPAIRED ZEE CHANNEL IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

AFT CARGO RT ZEE CHANNEL CORRODED BETWEEN BS 727A TO BS 767. R&R ZEE CHANNEL IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

AFT CARGO AFT BULKHEAD SUPPORT CORRODED AT BS 947.5, STR 26R. R&R SUPPORT PER SRM & DWG.

Part: FRAME — CRACKED (BS 867) · airframe 42,334 hrs · 24,683 cycles

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

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

AFT CARGO FLOOR STRAP CORRODED AT BS 770. R&R STRAP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

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

Part: FRAME — CRACKED (BS 787) · airframe 42,334 hrs · 24,683 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

MAIN CABIN FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 867) · airframe 42,334 hrs · 24,683 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

MAIN CABIN FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME IAW EA.

Part: DOOR FRAME — CORRODED (BS 303) · airframe 42,334 hrs · 24,683 cycles

L1 DOOR FRAME CORRODED AT BS 303.9. REPAIRED THE DOOR FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

MAIN CABIN FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 500C) · airframe 42,334 hrs · 24,683 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

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

Part: FLOORBEAM — CORRODED (BS 986) · airframe 42,334 hrs · 24,683 cycles

CABIN FLOORBEAM CORRODED AT BS 986.5, LBL 40 TO 55. REPAIRED THE FLOORBEAM IAW EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

FORWARD CARGO BAY DOOR CUTOUT WEB SILL TOP SURFACE CORRODED. R&R WEB IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

AFT CARGO FLOOR STRAP CORRODED AT BS 727D+3. R&R STRAP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME AW ER AND EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 42,334 hrs · 24,683 cycles

LT MAIN WHEEL WELL SPAR VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 34. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

MAIN CABIN FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

MAIN CABIN FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,334 hrs · 24,683 cycles

MAIN CABIN FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 480) · airframe 42,334 hrs · 24,683 cycles

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

Part: FRAME — CRACKED (BS 827) · airframe 42,334 hrs · 24,683 cycles

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

Part: STRAP — BROKEN (FLASHLIGHT ASSY) · airframe 42,152 hrs · 24,579 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 41,086 hrs · 23,975 cycles

RIGHT LOWER EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 40,484 hrs · 23,615 cycles

RIGHT OVERWING EXIT DOOR LOWER EMER EXIT SIGN BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 39,455 hrs · 23,024 cycles

L1 DOOR EXIT LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 37,723 hrs · 21,981 cycles

LEFT PHOTO LUMINESCENT FLOOR STRIP DAMAGED AT ROW 7. R & R STRIP IAW MM & DWG.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 37,723 hrs · 21,981 cycles

LEFT PHOTO LUMINESCENT FLOOR STRIP DAMAGED AT ROW 1. R & R STRIP IAW MM & DWG.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 37,723 hrs · 21,981 cycles

RIGHT PHOTO LUMINESCENT FLOOR STRIP DAMAGED AT ROW 1. R & R STRIP IAW MM & DWG.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 37,723 hrs · 21,981 cycles

RIGHT PHOTO LUMINESCENT FLOOR STRIP DAMAGED. R & R STRIP IAW AMM.

Part: ATTACH BRACKET — LOOSE (R1 DOOR) · airframe 37,723 hrs · 21,981 cycles

R1 DOOR ESCAPE SLIDE UPPER AFT ATTACH BRACKET LOOSE. R & R BRACKET IAW SRM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 37,723 hrs · 21,981 cycles

LEFT PHOTO LUMINESCENT FLOOR STRIP DAMAGED AT ROW 8. R & R STRIP IAW MM & DWG.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 37,723 hrs · 21,981 cycles

LEFT PHOTO LUMINESCENT FLOOR STRIP DAMAGED. R & R STRIP IAW AMM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 37,723 hrs · 21,981 cycles

RIGHT PHOTO LUMINESCENT FLOOR STRIP DAMAGED AT ROW 9. R & R STRIP IAW MM & DWG.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 37,723 hrs · 21,981 cycles

RIGHT PHOTO LUMINESCENT FLOOR STRIP DAMAGED AT ROW 8. R & R STRIP IAW MM & DWG.

Part: LENS — LOOSE (EXIT SIGN) · airframe 35,984 hrs · 20,992 cycles

AFT GALLEY EMER EXIT SIGN LOOSE. R & R LENS IAW MM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

RIGHT SUPPORT BRACKET CRACKED AT BS 540 OTBD OF KEEL BEAM. R & R BRACKET IAW DWG & SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

FLOORBOARD SUPPORT STRUCTURE CRACKED AT BS 540, RBL 24.75. R & R SUPPORT IAW DWG & SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

LEFT SUPPORT BRACKET CRACKED AT BS 540 OTBD OF KEEL BEAM. R & R BRACKET IAW DWG & SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

FLIGHT COMPARTMENT FLOORBEAM FOR PANEL 211AF AFT ANGLE INTERCOSTAL CORRODED. REPAIRED INTERCOSTAL IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, RBL 24.75. REPAIR SEAT TRACK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

SKIN CRACKED AT BS 540, BETWEEN STRINGER 22L TO 23L. REPAIRED SKIN IAW EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

FLOOR SUPPORT SPLICE CRACKED AT BS 540 BETWEEN BL 0 TO RBL 24. R & R SPLICE IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

SKIN CRACKED AT BS 540, BETWEEN STRINGER 22R TO 23R. REPAIRED SKIN IAW EA.

Part: INTERCOSTAL — CRACKED (LT WING) · airframe 35,973 hrs · 20,985 cycles

LEFT WING OTBD OF THE INBD TE FLAP INTERCOSTAL WEB CRACKED. R & R WEB DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

FLOORBEAM SUPPORT BRACKET CRACKED AT BS 727B, LBL 45.5. REPAIRED BRACKET IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

FLOORBEAM SUPPORT BRACKET CRACKED AT BS 727B, LBL 24.75. REPAIRED BRACKET IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,973 hrs · 20,985 cycles

FORWARD SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: LIGHT — CRACKED (CABIN) · airframe 35,529 hrs · 20,725 cycles

FORWARD GALLEY EMER EEPLS CRACKED. R & R EEPLS IAW AMM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 33,135 hrs · 19,351 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD RETAINER CLIP LOOSE. R & R CLIP IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 32,728 hrs · 19,119 cycles

L1 DOOR EMERGENCY EGRESS LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,041 hrs · 18,721 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 30,979 hrs · 18,091 cycles

OVERHEAD EMERGENCY EXIT SIGN BETWEEN EMERGENCY EXIT ROW LOOSE. R&R SIGN IAW MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,584 hrs · 17,285 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED RIB AT STA 101.9, 38.25" AFT OF LEADING EDGE OF FWD SPAR. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,584 hrs · 17,285 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR RIB SKIN CRACKED AT STA 101.9, 29" AFT OF LEADING EDGE OF FWD SPAR. REPAIRED SKIN IAW EA.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 29,186 hrs · 17,018 cycles

PASSENGER CABIN, FLOOR PHOTO LUMINESCENT STRIPS APPROX STA 328 TO 953 BLUE FILM REMOVED. COMPLETED STEP 5.B.3.E OF MT 733-50-01 PASSENGER CABIN, FLOOR PHOTO LUMINESCENT STRIPS AT APPROX STA 328 TO STA 953 IAW MT 733-50-01 AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,186 hrs · 17,018 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL AT STA 500B TO 500C IS CRACKED AT STR 25L. REMOVED FWD CARGO COMPARTMENT INTERCOSTAL AT STA 500B TO 500C IAW SRM 51-40-02. INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,186 hrs · 17,018 cycles

FWD CARGO COMPARTMENT STA 500 T0 STA 500A APPROX STR 25L INTERCOSTAL FWD END IS CRACKED. REMOVED FWD CARGO COMPARTMENT INTERCOSTAL BETWEEN ST STA 500 TO STA 500A AT STR 25L. DRILLED UP NEW INTERCOSTAL AND INSTALLED IAW DWG

Part: FLAP — DELAMINATED (RT WING) · airframe 29,186 hrs · 17,018 cycles

RIGHT WING OUTBOARD AFT FLAP INBOARD AFT CORNER DELAMINATED. REPAIRED IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,186 hrs · 17,018 cycles

FWD CARGO COMPARTMENT, STA 500C + 10, LEFT HAND "Z" ANGLE HAS 1EA AREA OF CORROSION. BLENDED FWD CARGO COMPARTMENT, STA 500+10, LEFT 1 Z ANGLE AREA OF CORROSION/ INSTALLED REPAIR IAW SRM

Part: SILL — CORRODED (FUSELAGE) · airframe 29,186 hrs · 17,018 cycles

LEFT OVERWING EXIT DOOR CUTOUT-THRESHOLD SILL PLATE AND FASTENERS CORRODED ALONG OUTER ROW. REPAIRED AREA IAW 121449 IR AND EA 1-753-21369.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,254 hrs · 16,492 cycles

RIGHT HORIZONTAL STABILIZER RIB AT CRACKED AT STA 92.7. REPAIRED RIB IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,254 hrs · 16,492 cycles

RIGHT HORIZONTAL STABILZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,254 hrs · 16,492 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,254 hrs · 16,492 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,254 hrs · 16,492 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 157.1. REPAIRED SKIN IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 26,389 hrs · 15,473 cycles

LT EMERGENCY EXIT COVER LOOSE. SECURED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,338 hrs · 15,443 cycles

EGRESS LIGHT AT ROW 2 INOP. REPLACED LIGHT ASSY PER M/M.

Part: COVER — LOOSE (CABIN) · airframe 26,292 hrs · 15,413 cycles

LEFT EMERGENCY FLOOR TRACK LIGHT COVER AT ROW 1 LOOSE. SECURED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 25,847 hrs · 15,153 cycles

FWD EEPLS COVER LOOSE. REMOVED AND REPLACED EEPLS IAW MM.

Part: LIGHT — INSTALLED (CABIN) · airframe 25,672 hrs · 15,050 cycles

DURING SCHEDULED MV2 CHECK, FOUND THREE EMERGENCY EXIT EGRESS FLOOR LIGHTS INOP. REMOVED AND REPLACED LIGHT BULBS PER MM.

Part: CHECK VALVE — FAULTY (HYDRAULIC SYS) · airframe 24,623 hrs · 14,456 cycles

AIR TURNBACK/ DECLARED EMERGENCY. CAPTAIN SMELLED ODOR AT 10K GASPER TURNED OFF AT 10K. 20K FLIGHT ATTENDANT CALLED EYES BURNING WITH SMELL. REMOVED AND REPLACED "A" SYSTEM PNEUMATIC PRESSURE CHECK VALVE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,524 hrs · 14,391 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT EEPLS INOP. REPAIRED EEPLS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 24,247 hrs · 14,225 cycles

EEPLS LENS LOOSE AT ROW 1. SECURED LENS ASSY PER MM.

Part: CAP — LOOSE (CABIN) · airframe 24,247 hrs · 14,225 cycles

EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED END CAP PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 23,852 hrs · 13,981 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: COVER — LOOSE (CABIN) · airframe 23,077 hrs · 13,528 cycles

EEPLS COVER LOOSE AT ROW 2. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 22,636 hrs · 13,274 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 22,034 hrs · 12,930 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS LENS LOOSE. SECURED LENS PER MM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,973 hrs · 12,895 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 540, LBL 8. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,973 hrs · 12,895 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 540, LBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,973 hrs · 12,895 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,973 hrs · 12,895 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 540, RBL 42. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,973 hrs · 12,895 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 540, RBL 8. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,973 hrs · 12,895 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,973 hrs · 12,895 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED STIFFENER PER SRM.

Part: LENS — MISSING (CABIN) · airframe 21,800 hrs · 12,786 cycles

FWD EEPLS LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 21,772 hrs · 12,764 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT LOWER HORIZONTAL STABILIZER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 21,772 hrs · 12,764 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 20,446 hrs · 12,024 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 20,446 hrs · 12,024 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,300 hrs · 11,933 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,300 hrs · 11,933 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 5. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,762 hrs · 11,616 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,762 hrs · 11,616 cycles

DURING SCHEDULED HC2 CHECK, FWD ENTRY EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,762 hrs · 11,616 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,762 hrs · 11,616 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 19,443 hrs · 11,415 cycles

FWD LT EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,179 hrs · 11,252 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 7. RELAMPED PER MM.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 18,899 hrs · 11,083 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT LT EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED FUSE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,187 hrs · 10,653 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS INOP AT ROW 23. RELAMPED EEPLS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 17,727 hrs · 10,350 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS BROKEN BETWEEN ROW 1 TO ROW 2. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 17,520 hrs · 10,212 cycles

DURING SCHEDULED HC1 CHECK, EEPLS COVER OUT OF POSITION AT ROW 23. REMOVED AND REPLACED COVERS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,520 hrs · 10,212 cycles

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

Part: TRACK — LOOSE (CABIN) · airframe 16,696 hrs · 9,731 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK LOOSE AT FWD END OF CABIN, ROW 1. R&R TRACK PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 16,736 hrs · 9,750 cycles

EEPLS TRACK LOOSE AT FWD END OF CABIN. R&R EEPLS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 15,121 hrs · 8,787 cycles

DURING SCHEDULED HC2 CHECK, FOUND MID LT EMERGENCY EXIT BATTERY FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 15,121 hrs · 8,787 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD LT EMERGENCY EXIT BATTERY FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 15,121 hrs · 8,787 cycles

DURING SCHEDULED HC2 CHECK, FOUND AFT RT EMERGENCY EXIT BATTERY FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,947 hrs · 8,065 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 18 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 12,542 hrs · 7,200 cycles

DURING SCHEDULED HC1 CHECK, LEFT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — MISSING (CABIN) · airframe 11,452 hrs · 6,546 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT ROW 2. INSTALLED LENS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 11,398 hrs · 6,514 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM.

Part: CAP — CRACKED (CABIN) · airframe 10,411 hrs · 5,903 cycles

EEPLS END CAP CRACKED AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,075 hrs · 3,440 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,701 hrs · 2,633 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 4,639 hrs · 2,600 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,091 hrs · 1,742 cycles

DURING SCHEDULED RON CHECK, FOUND AFT CABIN EEPLS TRACK INOP. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: COVER — LOOSE (R2 DOOR SLIDE) · airframe 2,850 hrs · 1,603 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER PER MM.

Part: LIGHT — BROKEN (EMERGENCY EXIT) · airframe 2,181 hrs · 1,241 cycles

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