N791SW

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 73,279 hrs · 43,414 cycles

EXTERIOR EMERGENCY LIGHT AFT OF L2 DOOR INOP<[01] REMOVED AND REPLACED THE LAMP IN THE L2 DOOR AS PER AMM 33-51-01.TEST OK AT THIS MOMENT.

Part: SUPPORT PLATE — CRACKED (BS 178) · airframe 70,151 hrs · 41,389 cycles

LOWER FUSELAGE, NOSE COMPT AT WEATHER RADAR UNIT UPPER PLATE SUPPORT CRACKED. REPLACED THE SUPPORT PLATE IAW SRM 51-40-02, AND DWG 25510001, REV A.

Part: ANGLE — CRACKED (ZONE 500) · airframe 70,151 hrs · 41,389 cycles

CRACK ANGLE LOC. FRONT SPAR FUEL BOOST PUMP IFSS 120 APROX AT LT WING. REPLACED ANGLE LOC. FRONT SPAR FUEL BOOST PUMP IFSS 120 APROX AT LT WING. IAW SRM 51-40-02 AND SRM 51-10-02 STEP 9.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 70,151 hrs · 41,389 cycles

DONT PASS TEST CHARGER ASSY BATTERY PACK (M1670) AT PASSENGER CABIN. REPLACED CHARGER ASSY BATTERY PACK (M1670) AT PASSENGER CABIN IAW AMM 33-51-06-960-806; TEST IS OK.

Part: WEB — CORRODED (LT WING) · airframe 70,151 hrs · 41,389 cycles

CORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APROX AT LT WING 2022-649758. EVALUATED REWORKED AREA ON FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APROX AT LT WING AND FOUND WITHIN LIMITS IAW B737-700 SRM 57-20-10-1A-3 STEP 5.D FIGURE 105 TABLE 101 .SEE INDIVIDUAL SIGNOFF BELOW;[04] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: LIGHT — BROKEN (CABIN) · airframe 70,151 hrs · 41,389 cycles

BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (4 EA) 2022-649742. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN IAW AMM 33-51-15-400-802.

Part: STRINGER — CRACKED (BS 540 S26R) · airframe 70,151 hrs · 41,389 cycles

CRACKED STRINGER 26R, BS 540 IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1 REPAIR.

Part: SUPPORT ANGLE — CRACKED (RT WING TE) · airframe 70,151 hrs · 41,389 cycles

CRACK SUPPORT ANGLE, ORSS 275, FIXED TRAILING EDGE AREA, RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02 AND SRM 51-10-02, ITEM 9.

Part: STRINGER — CRACKED (BS 540 S23L) · airframe 70,151 hrs · 41,389 cycles

CRACKED STRINGER 23L, BS 540 IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1 REPAIR 1. THIS REPAIR IS CLASSIFIED AS CATEGORY A.

Part: STRINGER — CRACKED (BS 540 S27L) · airframe 70,151 hrs · 41,389 cycles

CRACKED STRINGER 27L, BS540 IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1 REPAIR 1.

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 70,151 hrs · 41,389 cycles

CRACKED STRINGER 26L, BS 540 IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1.

Part: RIB — NONE (HORIZONTAL STAB) · airframe 70,151 hrs · 41,389 cycles

CRACK INSPAR RIB LOCATED STAB STA 92.70 FRONT SPAR UPPER FLANGE AT RT HORIZONTAL STABILIZER. PERFORMED EDDY CURRENT INSPECTION ON DAMAGE AREA REPORT IAW NDT MANUAL 51-00-00, PART 6 PROCEDURE 23. CRACK INDICATION NOT FOUND LOCATED AT HSS 92.70 FRONT SPAR UPPER FLANGE.

Part: STRINGER — CRACKED (BS 540 S25R) · airframe 70,151 hrs · 41,389 cycles

CRACKED STRINGER 25R, BS 540 IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1.

Part: SUPPORT — CORRODED (LT WING) · airframe 70,151 hrs · 41,389 cycles

CORRODED SUPPORT STRUCTURE, ORSS 282 - ORSS 315, TRAILING EDGE AREA ON LT WING. REPLACED THE SUPPORT STRUCTURE IAW SRM 51-10-02 ITEM 9 AND DWG 115A3700 REV: B SHEET 3.

Part: SUPPORT — CRACKED (RT WING) · airframe 70,151 hrs · 41,389 cycles

CRACKED SUPPORT STRUCTURE, ORSS 282 TRAILING EDGE AREA, RT WING. REPLACED THE SUPPORT STRUCTURE IAW SRM 51-10-02 ITEM 9.

Part: SUPPORT — CRACKED (BS 1016) · airframe 70,151 hrs · 41,389 cycles

CRACK SUPPORT PLATE ASSY LOC. FRONT SPAR APPROX STA 1016 AT VERTICAL STABILIZER. REPLACED SUPPORT PLATE ASSY LOC. FRONT SPAR APPROX BS 1016 AT VERTICAL STABILIZER AND FASTENER IAW DWG 176A3101 SHEET 4 REV -, AND SRM 51-10-02 ITEM 9.

Part: WEB — CRACKED (NR 2 FAN COWL) · airframe 70,151 hrs · 41,389 cycles

CRACKED WEB OUTBOARD FAN COWL ON NR 2 ENGINE. REPLACED WEB IAW SRM 51-10-02, ITEM 9, AND CMM 71-13-30 FIGURE 3,

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 70,151 hrs · 41,389 cycles

ELONGATED HOLE ON ACCESS PANEL 544BB AT LT WING. REPLACED THE ACCESS PANEL 544BB AT LT WING IAW SRM B737-700 51-40-02-0G-0.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 70,151 hrs · 41,389 cycles

CRACKED ACCESS PANEL 661AB, RT WING TE. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 70,151 hrs · 41,389 cycles

CRACKED ACCESS PANEL 561AB, LT WING TE. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 70,151 hrs · 41,389 cycles

CRACKED FWD CORNER OF THE SCUFF PLATE IN THE AFT CARGO COMPARTMENT. REPAIRED BY WELDING FWD CORNER SCUFF PLATE IN THE AFT CARGO BAY IAW SRM 53-60-15-2R-1, REPAIR 1, AND 5975.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 70,151 hrs · 41,389 cycles

CRACK ACCESS PANEL 661BB TRAILING EDGE, RT WING. REPAIRED IAW SRM 51-70-04-2R-9, REPAIR 9, PARAGRAPH 4.N P, AND SRM 51-70-04-2R-0, REPAIR GENERAL, PARAGRAPH 4.P. AND SRM 51-30-10-0G-O GENERAL TABLE 1. [

Part: ANGLE — CRACKED (BS 695 RBL 24.5) · airframe 70,151 hrs · 41,389 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED AT BS 695 RBL 24.5 LOWER SURFACE WL 208.1 CENTER SECTION 2022-649534 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED AT BS 695 RBL 24.5 LOWER SURFACE WL 208.1 CENTER SECTION IAW B737-700 SRM 51-10-02 STEP 9 ; SRM 51-40-02 AND DWG 273A9112 SHEET 30 REV -. SEE INDIVIDUAL SIGN OFF BELOW;[03] COMPLETE TASK CERTIFIED RII

Part: PLATE — BROKEN (BS 847 S25R) · airframe 70,151 hrs · 41,389 cycles

BROKEN PLATE ON THE FLOOR PANEL 140CF, BS 847, S25R IN THE AFT CARGO COMPARTMENT. REPLACED THE PLATE IAW SRM 51-10-02.

Part: PLATE — BROKEN (FLOOR PANEL) · airframe 70,151 hrs · 41,389 cycles

BROKEN PLATE ON THE FLOOR PANEL 140CF AT BS 794.3, S25R IN THE AFT CARGO COMPARTMENT. REPLACED THE PLATE IAW SRM 51-10-02.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 70,151 hrs · 41,389 cycles

CRACK LEADING EDGE RIB ON THE L/E HSS 105.26, RT HORIZONTAL STAB. REJECTED RIB INSTALLATION ON RT HORIZONTAL STAB, DUE TO FOUND TOOL MARK LEADING EDGE SKIN. REPLACED THE RIB ON THE RT HORIZONTAL STAB IAW SRM 51-10-02, ITEM 9, AND DWG 186A1001, REV A, SHEET 10.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 70,151 hrs · 41,389 cycles

CRACK LEADING EDGE RIB ON L/E HSS 105.26 AT LT HORIZONTAL STABILIZER. REPLACED LEADING EDGE RIB LOC. ON L/E HSS 105.26 AT LT HORIZONTAL STABILIZER IAW SRM 51-10-02 ITEM 9 AND DWG 186A1001 SHEET 10 REV A.

Part: ANGLE — CRACKED (BS 695, BL 0) · airframe 70,151 hrs · 41,389 cycles

CRACKED ANGLE FLOOR STRUCTURE LOCATED AT BS 695 BL0 UPPER SURFACE WL 208.1. REPLACED THE ANGLE FLOOR STRUCTURE IAW SRM 51-40-02, AND DWG 273A9110, SHEET 5, REV A.

Part: STRINGER — CRACKED (L/H WING) · airframe 69,480 hrs · 40,936 cycles

WHILE REMOVING LH WING INBD LEADING EDGE FOUND STRINGER AT KRAS 206.32 TO KRAS 218 AT STRINGER ROW 2 CRACKED (116A4531-1) / [01] LOCATED AND DRILLED NEW STRINGER IAW SRM 51-40-05-0G-0 AND BOEING DWG# 116A4008 ID:0015 REV:F.;[02] LOCATED AND DRILLED NEW STRINGER; STRINGER ISNATALLED ON FAULT TTG8Q00E7XZX;[03] ALL WORK C/W<BR>AUDIT C/W

Part: RIB — BUCKLED (L/H HORIZ. STAB.) · airframe 69,480 hrs · 40,936 cycles

L/H HORIZ STAB L/E RIB AT STA 170.34 BUCKLED (186A1401-5) / [01] VERIFIED NEW L/H HORIZONTAL STAB RIB STA 170.34 P/N 186A1401U5; A TAGA141918 I/A/W BOEING DRAWING 186A1001 REV A;[02] VERIFIED STEP 1 C/W;[03] LOCATED AND DRILLED UP NEW RIB I/A/W B737 700 SRM 51-40-05 AND BOEING DRAWING 186A1001 REV A;[04] VERIFIED STEP 3<BR>OK TO INSTALL;[05] INSTALLED NEW RIB I/A/W B737 700 SRM 51-40-02 AND BOEING DRAWING 186A1001 REV A;[06] VERIFIED STEP 5;[07] RIB REPLACEMENT BEEN C/W;[08] AUDIT C/W

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 69,480 hrs · 40,936 cycles

POWER RECEPTACLE DOOR AFT FLANGE DOUBLER CRACKED REPAIR FILLER / [01] REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0;[02] VERIFIED MATERIAL ID FOR REPAIR DOUBLER IS 2024 T3 .050 TAG# A02062 IAW SRM 53-10-15-2R-4;[03] VERIFIED STEP 2 C/W;[04] FABRICATED REPAIR DOUBLER IAW B737 SRM 53-10-15-2R-4 REPAIR 4;[05] VERIFIED STEP 4 C/W;[06] OK GIVEN TO TREAT AND PRIME;[07] TREATED AND PRIMED REPAIR DOUBLER IAW B737 SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804;[08] VERIFIED STEP 7 C/W;[09] OK GIVEN TO INSTALL REPAIR PART;[10] STARTED INSTALLING REPAIR DOUBLER PER B737 SRM 53-10-15-2R-4;[11] VERIFIED STEP 10; STARTED REPAIR INSTALL;;[12] FINISHED INSTALLING REPAIR DOUBLER I.A.W SRM 53-10-15-2R-4;[13] VERIFIED STEP 12 C/W;[14] EDGE SEALED REPAIR AREA I.A.W SRM 53-10-15-2R-4;[15] APPLIED EXTERIOR PAINT TO REPAIR AREA I.A.W SRM 53-10-15-2R-4;[16] VERIFIED STEPS 14 &15 C/W;[17] JOB COMPLETED; AUDIT C/W

Part: RIB — BUCKLED (L/H HORIZ. STAB.) · airframe 69,480 hrs · 40,936 cycles

L/H HORIZ STAB L/E RIB AT STA 123.85 BUCKLED (186A1306-1) / [01] VERIFIED NEW L/H HORIZONTAL RIB STA 123.85 P/N 186A1352-11 ; A TAG A141919 I/A/W BOEING DRAWING 186A1306 REV -;[02] VERIFIED STEP 1 C/W;[03] LOCATED AND DRILLED UP NEW RIB I/A/W B737 700 SRM 51-40-05 AND BOEING DRAWING 186A1306 REV -;[04] VERIFIED STEP 3<BR>OK TO INSTALL;[05] INSTALLED NEW RIB I/A/W B737 700 SRM 51-40-02 AND BOEING DRAWING 186A1306 REV -;[06] VERIFIED STEP 5;[07] AUDIT C/W

Part: STRINGER CLIP — BUCKLED (FUSELAGE) · airframe 69,480 hrs · 40,936 cycles

STATION 500C S-15L STRINGER CLIP IS BUCKLED / [01] MATERIAL FOR STRINGER CLIP VERIFIED AS BAC1493-852 7075T62 A TAG# A13147 IAW BOEING DRAWING #143A1010 REV. BE;[02] VERIFIED STEP 1 C/W;[03] LOCATED AND DRILLED STRINGER CLIP IAW B737 SRM 51-40-05-0G-0.;[04] VERIFIED STEP 3 C/W<BR><BR>OK TO TREAT AND PRIME;[05] TREATED AND PRIMED CLIP IAW B737 AMM 51-21-41-370-803; AND 51-21-72-370-804.;[06] VERIFIED STEP 5 C/W<BR><BR>OK TO INSTALL NEW STRINGER CLIP;[07] INSTALLED STRINGER CLIP IAW B737 SRM 51-40-02-0G-0.;[08] ALL WORK C/W<BR>AUDIT C/W;[09] REF ORIGINAL FAULT TTG8Q00E5QS0

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,480 hrs · 40,936 cycles

STATION 500C S-14L TO S-15L SHEAR TIE HAS 3 CRACK / [01] RECIEVED NEW MACHINED 143A3010-31 SHEAR TIE PO NUMBER 413605 MACHINED PER BOEING DWG 143A3010 PL REV BD;[02] A TAG A142444;[03] VERIFIED ITEM 1 AND 2;[04] VERIFIED NEW PART CRACK FREE IAW SOPM 20-20-02 FPI TYPE 1; METHOD A; LEVEL 3;[05] LOCATED AND DRILLED SHEAR TIE IAW B737 SRM 51-40-05-0G-0.;[06] VERIFIED STEP 5 C/W<BR><BR>OK TO TREAT AND PRIME;[07] TREATED AND PRIMED SHEAR TIE IAW B737 AMM 51-21-41-370-803; AND 51-21-72-370-804.;[08] VERIFIED STEP 7 C/W;[09] REMOVED AND REPLACED DAMAGED SHEAR TIE IAW SRM 51-40-02-0G-0 AND DWG 143A3010 PL REV. BD (REMOVE/INSTALL DOCUMENTED ON WORK CARD TTG8Q00E7WKS AND TTG8Q00EC1RB);[10] VERIFIED JOB IS COMPLETE;[11] VERIFIED ITEM 9 AND 10;[12] AUDIT C/W;[13] REF ORIGINAL FAULT TTG8Q00E5QRD

Part: BRACKET — CRACKED (FUSELAGE) · airframe 69,479 hrs · 40,935 cycles

BS 500 C STR 14 L TO STR 15 L; FRAME TO FUSELAGE BRACKET HAS 3 CRACK / [01] REFERENCE TTG8Q00E6C2Q

Part: STRINGER CLIP — BUCKLED (FUSELAGE) · airframe 69,479 hrs · 40,935 cycles

BS 500 C STR 15 L STRINGER CLIP BUCKLED / [01] REFERENCE TTG8Q00E6C2Q

Part: LIGHT — LOOSE (R/H CABIN) · airframe 68,617 hrs · 40,382 cycles

EMERGENCY EXIT LIGHT FLOOR STRIP COMING LOOSE ROW 9 FO SIDE; 2-3 FEET / [01] SECURED STRIP DOWN. <BR>MM 33-51-15

Part: LIGHT — INOPERATIVE · airframe 68,361 hrs · 40,213 cycles

22DEF OVERHEAD BIN EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED 22DEF OVERHEAD BIN EMERGENCY LIGHT AND OPS CHECK GOOD REF AMM 33-51-03

Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 67,919 hrs · 39,948 cycles

L-2 DOOR SLIDE GIRT BAR GIRT TOO LONG; NEEDS REINSTALLED. ; / [01] REINSTALLED L-2 DOOR SLIDE GIRT BAR PER MT 725-61-06

Part: PLATE — CRACKED (L/H WING) · airframe 67,919 hrs · 39,948 cycles

LEFT WING LOWER TRAILING EDGE WIGGLE PLATE CRACKED JUST AFT OF #1 ENGINE ; / [01] R+R LEFT WING LOWER TRAILING EDGE WIGGLE PLATE JUST AFT OF #1 ENGINE PER SRM 51-40-02.

Part: LIGHT — INOPERATIVE · airframe 67,914 hrs · 39,947 cycles

EMERGENCY EXIT LIGHTS BATTERY PACK M1670 INOP. ; / [01] REMOVED & REPLACED POWER SUPPLY AT POS. M1670 AS PER B737 AMM 33-51-06-960-806. PENDING TEST; [02] REMOVED & REPLACED BATTERY PACK AT 1670 AS PER B737<BR>AMM 33-51-06-960-805 PENDING TEST; [03] PERFORMED POWER SUPPLY AND BATTERY PACK OPS CHECK; FOUND NORMAL AS PER B737 AMM 33-51-06-960-806 & 33-51-06-960-805.; [04] VERIFIED STEP 1;2;3

Part: LIGHT — INOPERATIVE · airframe 67,914 hrs · 39,947 cycles

EMERGENCY EXIT LIGHTS BATTERY PACK M1672 INOP. ; / [01] REMOVED & REPLACED POWER SUPPLY AT POS. M1672 AS PER B737 AMM 33-51-06-960-806. PENDING TEST; [02] REMOVED AND REPLACED BATTERY PACK AT POS. M1672 AS PER B737 AMM 33-51-06-960-805.; [03] PERFORMED POWER SUPPLY AND BATTERY PACK OPS CHECK; FOUND NORMAL AS PER B737 AMM 33-51-06-960-806 & 33-51-06-960-805.; [04] VERIFIED STEP 1;2;3

Part: LIGHT — INOPERATIVE · airframe 67,914 hrs · 39,947 cycles

EMERGENCY EXIT LIGHTS BATTERY PACK M1668 INOP. ; / [01] REMOVED & REPLACED POWER SUPPLY AT POS. M1668 AS PER B737 AMM 33-51-06-960-806. PENDING TEST; [02] REMOVED & REPLACED BATTERY PACK AT M1668 AS PER B737 AMM 33-51-06-960-805. PENDING TEST; [03] PERFORMED POWER SUPPLY AND BATTERY PACK OPS CHECK; FOUND NORMAL AS PER B737 AMM 33-51-06-960-806 & 33-51-06-960-805.; [04] VERIFIED STEP 1;2;3

Part: LIGHT — INOPERATIVE · airframe 67,914 hrs · 39,947 cycles

EMERGENCY EXIT LIGHTS BATTERY PACK M1674 INOP. ; / [01] REMOVED & REPLACED POWER SUPPLY AT POS. M1674 AS PER B737 AMM 33-51-06-960-806. PENDING TEST; [02] REMOVED AND REPLACED BATTERY PACK AT POS. M1674 AS PER B737 AMM 33-51-06-960-805.; [03] PERFORMED POWER SUPPLY AND BATTERY PACK OPS CHECK; FOUND NORMAL AS PER B737 AMM 33-51-06-960-806 & 33-51-06-960-805.; [04] VERIFIED STEP 1;2;3

Part: LIGHT — DAMAGED · airframe 67,914 hrs · 39,947 cycles

AFT LOWER CEILING EXIT SIGN DAMANGED. ; / [01] REMOVED AND REPLACED AFT LOWER CEILING EXIT SIGN ASPER B737-700 AMM 33-51-01-960-801; [02] VERIFIED STEP 1

Part: BRACKET — CRACKED (AFT CARGO BULKHE) · airframe 67,914 hrs · 39,947 cycles

AFT CARGO FWD BULKHEAD BRACKET SUPPORT CRACK; STA 727 RBL 5 ; / [01] REMOVED SUPPORT BRACKET ON AFT CARGO FWD BULKHEAD STA 727 PER REF 737 SRM 51-4-02-0G-0; [02] CORRECTION REMOVED AFT CARGO SUPPORT BRACKET; FWD BULKHEAD STA 727 PER REF. 737 SRM 51-40-02-0G-0; [03] VERIFIED STEP 2. OK TO INSTALL NEW BRACKET.; [04] REMOVED DAMAGE BRACKET ON AFT CARGO COMPARTMENT STA 727 RBL5 AND INSTALLED NEW BRACKET PER REF.737. SRM 51-40-02-0G-0 AND DRAWING #144A9401; [05] VERIFIED STEP 4.

Part: SPLICE STRAP — ELONGATED (AFT CARGO) · airframe 67,914 hrs · 39,947 cycles

AFT CARGO COMPARTMENT FLOOR SPLICE STRAP AT STA 767+5 WITH HOLES ELONGATED ; / [01] RECEIVED NEW FLOOR SPLICE STRAP P/N 146A9401-4; NEW STRAP TO BE INSTALLED ON T/C 5360-E-16462-NG; BAR CODE TTG8QOO4FW0P; [02] VERIFIED STEP 1.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 67,914 hrs · 39,947 cycles

L/H HORIZONTAL RIB # 4 AT STIFFENER #4 LOWER AREA CRACK ; / [01] CUT OUT AND REMOVE DAMAGE ON VERTICAL STIFFENER ON RIB # 4 AT STIFFENER #4 PER REF 737 SRM 55-10-09-2R-4; [ FABRICATED LOWER ANGLE.063 BAC1480-2793 7075 T6PER REF 737 SRM 55-10-09-2R05 AND LOCATED AND DRILLED REPAIR PARTS INSTALLED REPAIR AT RIB # 4 ; STIFFENER #4 PER REF.737 SRM 55-10-09-2R-5 FIG 204 ON L/H HORIZONTAL STABILIZER; [21] CUTOUT AREA AT LOWER CHORD AT L/H HOR RIB #4 AT STIFFENER #4 AND INSTALLED REPAIR AS PER B737-7 SRN 55-10-09-2R-5 FIG 204.; [22] HORIZONTAL RIB #4 WILL BE INSTALL ON N/R TASK # TTG8Q009Z8XP.; [23] HORIZONTAL RIB #4 WAS REMOVED ON N/R #TTG8Q009Z8XP.; [24] VERIFIED STEP 21; [25] VERIFIED STEPS 22 AND 23; [26] C/W

Part: RIB — CRACKED (LH HOR STAB) · airframe 67,914 hrs · 39,947 cycles

RIB # 4 STIFFENER # 1 CRACK UPPER AREA ; / [01] ENTER IN ERROR THE CORRECT STIFFENER CRACK IS# 4 INSTEAD OF #1; [02] VERIFIED STEP 1.

Part: FITTING — CORRODED (L1 DOOR) · airframe 67,914 hrs · 39,947 cycles

L-1 DOOR AFT GIRT BAR FITTING WITH SURFACE CORROSION ; / [01] REMOVED CORROSION ON L1 DOOR AFT GIRT BAR FITTING REF. B737-7 SRM 51-10-02-0G-0; [02] AFTER CORROSION REMOVAL; ORIGINAL MAT. 0.075'; MATERIAL REMOVED 0.043'; MATERIAL REMAINING 0.032'; FOUND OUT OF LIMITS REF. B737-7 SRM 53-10-51-1A-1; [03] REMOVED AFT FITTING REF. B737-7 SRM 51-40-02-0G-0; [04] VERIFIED STEPS 1; 2 AND 3; [05] OK TO INSTALL GIRT BAR FITTING; [06] INSTALLED NNEW AFT FITTING REF B737-7 SRM 51-40-02-0G-0; [07] REMOVED AND REPLACED L1 DOOR AFT GIRT BAR FITTING REF. USED B737-7 SRM 51-40-02-0G-0; [08] VERIFIED STEP 7

Part: SPLICE STRAP — ELONGATED (AFT CARGO) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO FLOOR STRAP AT STA 727D +5 O/B HOLES ELONGATED ; / [01] RECEIVED NEW FLOOR SPLICE STRAP P/N 146A9401-8; NEW SPLICE STRAP TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004FW0P; [02] VERIFIED STEP 1.

Part: MEGAPHONE — INOPERATIVE · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: FWD WINDSCREEN MEGAPHONE BATTERY INOP ; / [01] REMOVED AND REPLACED BATTERY IN REF WITH AMM 25-64-00-900-804; [02] VERIFIED WORK PERFORMED

Part: FLASHLIGHT — INOPERATIVE · airframe 67,914 hrs · 39,947 cycles

FWD WINDSCREEN FLASHLIGHT BATTERY INOP ; / [01] REMOVE AND REPLACE FLASHLIGHT BATTERY IN REF WITH AMM 25-64-00-900-806; [02] VERIFIED WORK PERFORMED

Part: MEGAPHONE — INOPERATIVE · airframe 67,914 hrs · 39,947 cycles

AFT WINDSCREEN MEGAPHONE BATTERY INOP ; / [01] REMOVE AND REPLACE BATTERY IN REF WITH AMM 25-64-00-900-804; [02] VERIFIED STEP 1

Part: FLASHLIGHT — INOPERATIVE · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: AFT WIDSCREEN FLISHLIGHT BATTERY INOP ; / [01] REMOVED AND INSTALL FLASHLIGHT BATTERY IN AFT WINDSCREEN IN REF WITH AMM 25-64-00-900-806; [02] VERIFIED STEP 1

Part: NONE — CRACKED (COCKPIT) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: FLIGHT COMPARTMENT UPPER CEILING DRIP SHIELD RIGHT SIDE CORNER COMPOSITE AREA CRACK ; / [01] REPAIRED DAMAGE AREA ON FLIGHT COMPARTMENT UPPER CEILING DRIP SHIELD RIGHT SIDE CORNER FLANGE AS PER B737 AMM 25-00-00-300-801 MATERIALS USED PO#1714421 AND PO#1690463; [02] VERIFIED WORK PERFORMED

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: **CORROSION** AFT CARGO COMPARTMENT BILGE AREA; RIB AT STA-827 BETWEEN S-25L AND S-26L; FWD FACE AREA AROUND RIVET SPOT OF SURFACE CORROSION. DOT#208-161 ; / [01] REMOVED FASTENERS ON AFT CARGO COMP. BILGE AREA SHIELD TIE OF FRAME; AT STA: 827; BETWEEN S-25L AND S-26L FOR ACCESS; PER REF. B737 SRM 51-40-02-0G-0; [02] REMOVED CORROSION ON AFT CARGO COMP. BILGE AREA SHIELD TIE OF FRAME; AT STA: 827; BETWEEN S-25L AND S-26L ; CORROSION PASS THRU; PER REF. B737 SRM 51-10-02-0G-0; [03] VERIFIED STEPS 1 AND 2.; [04] REMOVED DAMAGE SHEAR TIE PER REF. 737 SRM 51-40-02-0G-0; AT STA 827 BETWEEN STRINGER 25 AND 26 L; [05] VERIFIED STEP 4.; [06] LOCATED AND DRILLED NEW SHEAR TIE PER REF 737 SRM 51-40-05-0G-0; [07] (RII) VERIFIED STEP 6.; [08] OK TO TREAT AND PRIME REPAIR AREA AND PART.; [09] TREATED AND PRIMER REPAIR AREA PER REF 737 AMM 51-21-41-370-802 AND 51-21-72-370-804; [10] VERIFIED STEP 9.; [11] (RII) OK TO INSTALL NEW SHEAR TIE.; [12] INSTALLED NEW SHEAR TIE AT STA. 827 BETWEEN STRINGER 25 AND 26 L PER REF. 737 SRM 51-40-02-0G-0 AND DRAWING 146A3010 AND 146A3200; [13] (RII) VERIFIED STEP 12.; [14] INSTALLED NEW SHEAR TIE AT STA. 827 BETWEEN STRINGER 25 AND 26 L PER REF. 737 SRM 51-40-02-0G-0 AND DRAWING 146A3010 AND 146A3200; [15] (RII) VERIFIED STEP 14.

Part: WEB — CORRODED (AFT CARGO) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: **CORROSION** AFT CARGO COMPARTMENT BILGE AREA; FLOOR SUPPORT STRUCTURE AT RBL-14 BETWEEN STA-727A AND STA-727B; SPOTS OF CORROSION AND RIVETS (2 EACH) MISSING. DOT#208-171 ; / [01] REMOVED FASTENERS ON AFT CARGO COMP. BILGE AREA; FLOOR SUPPORT STRUCTURE WEB; AT RBL-14; BETWEEN STA: 727A AND 727B; PER REF. B737 SRM 51-40-02-0G-0; [15] INSTALLED NEW INTERCOSTAL WEB ;AFT CARGO BETWEEN STA. 727A; AND 727B; RBL 14 PER REF. 737 SRM 51-40-02-0G-0 AND DRAWING 146A7505; [16] REMOVED AND REPLACED DAMAGE INTERCOSTAL WEB ;AFT CARGO BETWEEN STA 727A AND 727B ; RBL 14 PER REF. 737 SRM 51-40-02-0G-0 AND DRAWING 146A7505; [17] VERIFIED STEP 15 AND 16.

Part: NONE — CORRODED (FWD CARGO) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPARTMENT FWD BULKHEAD LOWER CENTER CAPSTRIP HAS CORROSION AROUND FASTENER HOLE AT R/H EDGE ; / [01] AFTER INSPECTION ;FWD CARGO COMPARTMENT FWD BUILKHEAD LOWER CENTER CAPS-TRIP FOUND OUT OF LIMITS IN REF B737-700 SRM 53-00-53-1A-2;PARRAGRAF 4.A(2)(A) FIGURE 103 DETAIL D; [02] RECEIVED NEW CAP-STRIP AT FWD CARGO COMPARTMENT FWD BULKHEAD LOWER AREA;AAR ISSUE TAG KD1723 P.O 1746221;WILL BE INSTALL ON A.D 5330-E-16461-NG YASK CARD TTG8Q004FHQD; [03] VERIFIED STEPS 1 AND 2

Part: NONE — CORRODED (FWD CARGO) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPARTMENT L/H AFT ZEE CHANNEL UPPER SURFACE BETWEEN STA 480 TO 500C STR 26L HAS CORROSION AROUND FASTENERS HOLES ; / [01] REMOVAL AND INSTALLATION OF ZEE CHANNEL BEING ACCOMPLISHED ON CARD #TTG8Q00A0VS7; [02] CORROSION AROUND FASTENER HOLES FOUND OUT OF LIMITS REF. B737-7 SRM 53-00-53-1A-2; [03] REMOVED DAMAGED SECTION OF ZEE CHANNEL AT PREVIOUS SPLICE AREA AT STA. 490 TO 500D; REF. B737-7 SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW ZEE CHANNEL SECTION REF. B737-7 SRM 51-40-05-0G-0; AND DRW. #143A7500; [05] VERIFIED STEP 4; [06] OK TO TREAT AND PRIME ZEE CHANNEL; [07] TREATED AND PRIMED ZEE CHANNEL REF. B737-7 SRM 51-20-01-0G-0; [08] INSTALLED ANCHOR NUTS ON ZEE CHANNEL AND INSTALLED REPAIR REF. USED B737-7 SRM 51-40-02-0G-0; 53-0053-2R-6; AND DRW #143A7500; [09] REMOVED DAMAGED SECTION OF ZEE CHANNEL AT PREVIOUS SPLICE AREA AT STA. 490 TO 500D; FABRICATED AND REPLACE ZEE CHANNEL REF. USED B737-7 SRM 51-40-02-0G-0; 51-40-05-0G-0; 51-20-01-0G-0; 53-00-53-2R-6 AND DRW #143A7500; [10] VERIFIED STEP 9

Part: FITTING — CORRODED (L1 DOOR) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: **CORROSION** L-1 DOOR FWD AND AFT GIRT BAR FITTINGS WITH SURFACE CORROSION. DOT#208-101 ; / [01] REMOVED CORROSION AT L-1 DOOR FWD AND AFT GIRT BAR FITTINGS IN REF B737-700 SRM 51-10-02-0G-0; [02] AFTER REMOVE CORROSION AT MAIN CABIN GIRT-BAR FITTINGS L-1 DOOR ;FOUND OUT OF ;ORIGINAL MATERIAL 0.075';MATERIAL REMAINING 0.045';IN REF B737-700 SRM 53-10-51-1A-1; [03] VERIFIED STEP #1 AND # 2.; [04] OK TO INSTALL NEW FWD AND AFT GIRT BAR FITTINGS; [05] INSTALLED MAIN CABIN GIRT BAR FITTINGS AT L-1 DOOR IN REF B737-700 SRM 51-40-02-0G-0; [06] VERIFIED STEP # 5; [07] JOB IS COMPLETE; [08] JOB IS COMPLETE; [09] FWD FITTING ONLY; AFT WORKED ON TTG8Q00AAD61

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: PASSENGER CABIN FWD WET AREA BETWEEN STA-312 AND STA-328 AT LBL-45; INTERCOSTAL WITH CRACK. DOT#208-104 ; / [01] REMOVED INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN FS 312-328 LBL 45 IN REF B737-700 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1<BR>OK TO DRILL HOLES; [03] LOCATED AND DRILLED NEW INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN FS 312-328 LBL 45;IN REF B737-700 SRM 51-40-02-0G-0; [04] ENTER IN ERROR STEP #3;LOCATED AND DRILLED REF B737-700 SRM 51-40-05-0G-0; [05] VERIFIED STEP 4<BR>OK TO TREAT AND PRIME HOLES; [06] TREATED AND PRIME HOLES ;IN REF B737-700 SRM 51-20-01-0G-0; [07] VERIFIED STEP 6<BR>OK TO INSTALL I TERCOSTAL; [08] INSTALLED INTERCOSTAL AT CABIN FWD WET AREA BETWEEN STA 312 TO STA 328 LBL-45 REF B737-7 SRM 51-40-02-0G-0 AND DWG #141A5400; [09] REMOVED AND REPLACED INTERCOSTAL AT CABIN FWD AREA FROM STA 312 TO STA 328 LBL -45 REF B737 -7 SRM 51-40-02-0G-0 AND DWG #141A5400; [10] VERIFIED STEP 8 AND 9; [11] JOB IS COMPLETE

Part: NONE — CORRODED (FWD CARGO) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPARTMENT R/H SIDE ZEE CHANNEL BETWEEN STA 490 TO 500C STR 26R HAS CORROSION AROUND FASTENERS HOLES ; ACTAL LOCATION IS FWD CARGO RH SIDE STA 490 TO STA 500 STR 26R / [01] REMOVED ZEE-CHANNEL ACCOMPLISSHED ON TTG8Q004FHQD; [02] REMOVED CORROSION AT FWD CARGO COMPARTMENT R/H SIDE ZEE CHANNEL BETWEEN FS 490 TO 500C STRINGER 26R IN REF B737-700 SRM 51-10-02-0G-0; [03] AFTER REWORK AREA ;FOUND OUT OF LIMITS ZEE-CHANNEL IN REF B737-700 SRM 53-00-53-1A-2 PARRAGRAFH 4.A(2)(A);FIGURE 103 ;DETAIL D; [04] LOCATED AND DRILLED NEW HOLES AT ZEE-CHANNEL IN REF B737-700 SRM 51-40-05-0G-0; [05] VERIFIED STEP 4<BR>OK TO TREAT AND PRIME; [06] TREATED AND APPLY PRIMER AT NEW HOLES AT ZEE-CHANNEL IN REF VB737-700 SRM 51-20-01-0G-0; [07] VERIFIED STEP 6; [08] INSTALLATION ZEE-CHANNEL WILL BE ACCOMPLISHED ON TTG8Q004FHQD; [09] REMOVED CORROSION AT FWD CARGO COMPARTMENT R/H SIDE ZEE CHANNEL BETWEEN FS 490 TO 500C STRINGER 26R IN REF B737-700 SRM 51-10-02-0G-0;AFTER REWORK AREA ;FOUND OUT OF LIMITS ZEE-CHANNEL IN REF B737-700 SRM 53-00-53-1A-2 PARRAGRAFH 4.A(2)(A);FIGURE 103 ;DETAIL D.LOCATED AND DRILLED NEW HOLES AT ZEE-CHANNEL IN REF B737-700 SRM 51-40-05-0G-0.TREATED AND APPLY PRIMER AT NEW HOLES AT ZEE-CHANNEL IN REF VB737-700 SRM 51-20-01-0G-0; [10] VERIFIED STEP 9

Part: NONE — CORRODED (FWD CARGO) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPARTMENT R/H AFT ZEE CHANNEL UPPER SURFACE BETWEEN STA 500A TO 500D STR 26R HAS CORROSION AROUND FASTENERS HOLES ; / [01] REMOVAL AND INSTALLATION OF ZEE CHANNEL BEING ACOOMPLISHED ON CARD #TTG8Q004FHQD; [02] LOCATED AND DRILLED NEW ZEE CHANNEL REF. B737-7 SRM 51-40-05-0G-0; [03] VERIFIED STEP 2; [04] OK TO TREAT AND PRIME; [05] TREATED AND PRIMED ZEE CHANNEL REF. B737-7 SRM 51-20-01-0G-0; [06] VERIFIED STEP 5; [07] INSTALLED ANCHOR NUTS ON ZEE CHANNEL REF. B737-7 SRM 51-40-02-0G-0 AND DRW.#143A7500; [08] FABRICATED FWD CARGO COMPARTMENT R/H ZEE CHANNEL STA500A TO 500D; STR26; WL 156; REF. USED B737-7 SRM 51-40-05-0G-0; 51-20-01-0G-0; 51-40-02-0G--0; AND DRW.#143A7500; [09] VERIFIED STEP 8

Part: ANGLE — CRACKED (L1 DOOR) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: CABIN PASSENGER UPPER SECTION OF L1 DOOR INTERNAL AREA STA312 HAS CRACK ; / [01] REMOVED FASTENERS AND MADE CUT OUT OF CRACKED AREA AS PER B737-700 SRM 53-10-07-2R-1.; [02] VERIFIED STEP 1; [03] PERFORMED HFEC INSP ON REWORKED AREA. IAW B 737 NDT PART 6 51-00-00 PROCE 23. TOOL NORTEC 600. BC 172389. CALIB DUE 7-2-22. NO CRACKS FOUND.; [04] PERFORMED HFEC ROTOR INSSP ON FASTENER OPEN HOLES. IAW B 737 NDT PART 6 51-00-00 PROCE 16. TOOL NORTEC 600. BC 172389. CALIB DUE 7-2-22. NO CRACKS FOUND.; [05] FABRICATED REPAIR ANGLE FROM 7075-O; .063' AS PER B737-700 SRM 53-10-07-2R-1.; [06] VERIFIED STEP # 5; [07] DVI OF UNDERLYING STRUCTURE NO DEFECTS FOUND.; [08] HEAT TREATED REPAIR ANGLE TO T6 CONDITION REF. BAC 5602 AND B737-7 SRM 53-10-07-2R-1 REPAIR 1. TAG #399089; [09] VERIFIED HEAT TREATMENT DOCUMENTATION<BR>OK TO TREAT AND PRIME; [10] PERFORMED PENETRANT INSP. ON FABRICATE ANGLE PART IAW BOEING SOPM 20-20-02. NO CRACKS NOTED; [11] APPLIED ALODINE AND PRIMER AS PER B737-700 SRM 51-20-01-0G-0.; [12] VERIFIED STEP 11<BR>OKTO INSTALL PART; [13] INSTALLED REPAIR PART AS PER B737-700 SRM 53-10-07-2R-1.; [14] REPAIRED CRACK AT CABIN PASSENGER UPPER SECTION OF L1 DOOR INTERNAL AREA STA 312 AS PER B737-700 SRM 53-10-07-2R-1.; [15] VERIFIED STEP 13 AND 14

Part: NONE — CORRODED (FUSELAGE) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: MAIN CABIN AFT WET AREA AFT LOWER PRESSURE SEAL; UPPER SEAL RETAINER HAS CORROSION STA 1016+16' LBL 13' ; / [01] REMOVED CORRODED SEAL RETAINER AT STA. 1016+16; LBL 13' ; PER REF 737 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1; [03] NEW SEAL RETAINER P/N 65-46823U21; TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00A0KZQ; [04] VERIFIED STEP 3

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 67,914 hrs · 39,947 cycles

LEFT HORIZONTAL STABILIZER STA. 120.30 RIB 4 STIFFENER # 3 CRACKED AT LOWER RADIUS. ; / [01] CUT OUT AND REMOVED DAMAGE FROM VERTICAL STIFFENER ON RIB #4 STIFFENER #3 PER REF.737 SRM 55-10-09-2R-4; [02] (RII) VERIFIED STEP 1. REMOVED DAMAGE ON WEB BELOW STIFFENER #3; PER REF. 737 SRM 55-10-09-2R-4; [06] VERIFIED STEP 5.; [07] PERFORMED HFEC INSP. ON RERPAIR AREA CUTOUT ON L/H STAB STA 120.30 RIB #4 STIFF. #3 @ LWR RADIUS IAW B737 NDT PART 6 51-00-00 PROC. 23. NO CRACKS; EQYUIP: NORTEC 600 CAL DUE: 10/22 B/C 166316; [08] PERFORMED ROTO INSP. ON RERPAIR AREA EXISTING HOLES ON L/H STAB STA 120.30 RIB #4 STIFF. #3 IAW B737 NDT PART 6 51-00-00 PROC. 16. NO CRACKS; EQYUIP: NORTEC 600 CAL DUE: 10/22 B/C 166316 ROUGHNESS ID 171854; [14] LOCATED AND DRILLED REPAIR PARTS PER REF B737 SRM 51-40-05-0G-0 TO STIFF # 3.; [15] VERIFIED STEP 12 AND 13.; [16] (RII) VERIFIED STEP 14.; [17] OK TO TREAT AND PRIME PARTS.; [18] TREATED AND PRIMER TRIMMED AREAS PER REF 737 AMM 51-21-41-370-802 AND 51-21-72-370-804; [19] VERIFIED STEP 18.; [20] (RII) OK TO INSTALL PARTS.; [21] INSTALLED REPAIR ON L/H HORIZONTAL STAB. AT RIB #4 ;STIFFENER #3; PER REF737 SRM 55-10-09-2R-4 FIG. 202; [22] (RII) VERIFIED STEP 21.; [23] INSTALLED REPAIR ON L/H HORIZONTAL STAB. AT RIB #4 ;STIFFENER #3; PER REF737 SRM 55-10-09-2R-4 FIG. 202; [24] (RII) VERIFIED STEP 23.

Part: SUPPORT — CRACKED (CABIN FLOOR) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: MAIN CABIN FLOOR SUPPORT STA 540 BETWEEN BL 0' AND RBL 24' HAS A CRACK AT FWD LOWER SURFACE I/B EDGE. ; / [01] REMOVED DAMAGED FLOOR SUPPORT; STA540; BL 0 - RBL24; LOCATED AND DRILLED NEW FLOOR SUPPORT REF USED B737-7 SRM 51-40-02-0G-0 AND 51-40-05-0G-0; [02] VERIFIED STEP.<BR> OK TO INSTALL SERVICEABLE PART; [03] INSTALLED NEW FLOOR SUPPORT; STA540; BL 0 - RBL24; LOCATED AND DRILLED NEW FLOOR SUPPORT REF USED B737-7 SRM 51-40-02-0G-0 AND DRW #143A5240; [04] VERIFIED STEP 3; [05] REMOVED AND REPLACED FLOOR SUPPORT; STA540; BL 0 - RBL24; WL208 REF. USED B737-7 SRM 51-40-02-0G-0; 51-40-05-0G-0 AND DRW 143A5240

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 67,914 hrs · 39,947 cycles

LEFT HORIZONTAL STABILIZER STA. 120.30 RIB 4 STIFFENER # 2 CRACKED AT LOWER RADIUS. ; / [01] CUT OUT AN REMOVED DAMAGE FROM VERTICAL STIFFENER OF RIB # 4 AT STIFFENER # 2 PER REF. 737 SRM 55-10-09-2R-4; [02] (RII) VERIFIED STEP 1 REMOVED DAMAGE ON WEB BELOW STIFFENER #2 PER REF. 737 SRM 55-10-09-2R-4; [10] VERIFIED SURFACE ROUGHNESS 63 PER REF 737 SRM 55-10-09-2R-4; ROUGHNESS ID 171854; [11] VERIFIED ROUGHNESS SURFACE 125 ON REPAIR PARTS CUT EDGES PER REF. 737 SRM 55-10-09-2R-4; ROUGHNESS ID 171854; [12] LOCATED AND DRILLED REPAIR PARTS PER REF B737 SRM 51-40-05-0G-0 TO STIFF # 2.; [13] VERIFIED STEPS 10 AND 11.; [14] (RII) VERIFIED STEP 12.; [15] OK TO TREAT AND PRIME PARTS.; [16] TREATED AND PRIMER TRIMMED AREAS PER REF 737 AMM 51-21-41-370-802 AND 51-21-72-370-804; [17] VERIFIED STEP 16.; [18] (RII) OK TO INSTALL REPAIR PARTS.; [19] INSTALLED REPAIR ON L/H HORIZONTAL STAB. AT RIB # 4; STIFFENER # 2; PER REF. 737 SRM 55-10-09-2R-4 FIG.202; [20] (RII) VERIFIED STEP 19.; [21] INSTALLED REPAIR ON L/H HORIZONTAL STAB. AT RIB # 4; STIFFENER # 2; PER REF. 737 SRM 55-10-09-2R-4 FIG.202; [22] (RII) VERIFIED STEP 21.

Part: SUPPORT — CRACKED (CABIN FLOOR) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: MAIN CABIN FLOOR SUPPORT STA 540 BETWEEN BL 0' AND LBL 24' HAS A CRACK AT AFT LOWER FACE I/B END. ; / [01] REMOVED DAMAGED FLOOR SUPPORT; STA540; BL 0 - LBL24; LOCATED AND DRILLED NEW FLOOR SUPPORT REF USED B737-7 SRM 51-40-02-0G-0 AND 51-40-05-0G-0; [02] VERIFIED STEP.<BR>OK TO INSTALL SERVICEABLE PART; [03] LATE ENTRY; REMOVED FLOOR 231UF FOR ACCESS REF. B737-7 AMM 53-21-00-000-801; [04] VERIFIED STEP 3; [05] INSTALLED NEW FLOOR SUPPORT; STA540; BL 0 - LBL24; LOCATED AND DRILLED NEW FLOOR SUPPORT REF USED B737-7 SRM 51-40-02-0G-0 AND DRW# 143A5240; [06] VERIFIED STEP 5; [07] OK TO REINSTALL FLOOR PANEL 231UF; [08] INSTALLED FLOOR PANEL #231UF REF. B737-7 AMM 53-21-00-400-801; [09] VERIFIED STEP 8; [10] REMOVED AND REPLACED CABIN FLOOR SUPPORT; STA540; BL 0 - LBL24; WL 208; REF. USED B737-7 SRM 51-40-02-0G-0 AND 51-40-05-0G-0; AND DRW# 143A5240; [11] VERIFIED STEP 10

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: AFT CABIN FLOOR PANEL 242TF UPPER SURFACE PEELING. ; DELAMINATION / [01] MEASUREMENTS; [02] CLEANED AND PREPARED AFT CABIN FLOOR PANEL 242TF UPPER SURFACE FOR REPAIR AS PER B737 SRM 53-00-50-2R-1; [03] REPAIRED DAMAGE TOP SURFACE AREA AS MARKED ON AFT CABIN FLOOR PANEL 242TF AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO# 1714421 AND PO#1690463; [04] VERIFIED STEP # 1; 2; AND 3; [05] VERIFIED STEP # 1 2 AND 3

Part: ACCESS PANEL — DELAMINATED (FUSELAGE) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: INNER LINER MATERIAL SHOWS EVIDENCE OF DELAMINATION AND OVER 90% MATERIAL DETERIORATION ; ACCESS PANEL 431DR / [01] REMOVED AND REPLACED ALUMINIUM FOIL DAMAGE AT PANEL 431DR IN REF B737-700 SRM 51-70-14-2R-3; [02] VERIFIED WORK PERFORMED

Part: NONE — LOW (L2 DOOR) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: L2 DOOR SLIDE ASSY AT THE INFLATION CYLINDER;THE PRESSURE INDICATOR NEEDLE AT PRESSURE GAGE IS OUT THE ' GO ' BAND (GREEN) ; / [01] L2 DOOR SLIDE ASSY TO BE REPLACED ON CUSTOMER CARD 721-61-06-AE (TTG8Q0064MUJ); [02] VERIFIED STEP 1

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: INNER LIMNER MATERIAL SHOWS EVIDENCE OF DELAMINATION & OVER (0% OF MATERIAL DETERIORATION ; INNER LIMNER MATERIAL SHOWS EVIDENCE OF DELAMINATION & OVER 90% OF MATERIAL DETERIORATION PANEL 441DR / [01] REMOVED AND REPLACED ALUMINIUM FOIL DAMAGE AT PANEL 441DR IN REF B737-700 SRM 51-70-14-2R-3; [02] VERIFIED WORK PERFORMED

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: MAIN CABIN SEAT TRACK FROM STA 500B TO 520 LBL 45.5' HAS CORROSION AND SCRATCHES AT CROWN UPPER AND CENTER SECTION (MKD 107-007). ; / [01] REMOVED CORROSION AND SCRATCHES AT MAIN CABIN SEAT TRACK FROM FS 500B-520 LBL 45.5 AT CROWN UPPER AND CENTER SECTION IN REF B737-700 SRM 53-00-52-1A-1; [08] INSTALLED EWIS PROTECTION AT MAIN CABIN PASSENGER SEAT TRACK REPAIR AREA STA 460 TO STA 540 BETWEEN LBL-24 TO LBL-46 REF B737-7 AMM 20-60-07-913-801; 13] LOCATED AND DRILLED NEW SEAT TRACK AND SPLICE SECTION REPAIR BETWEEN STA 460 TO 521 LBL-45.5 REF B737-7 SRM 53-00-52-2R-4 STEP 4.D THRU H; [17] CORRECTON STEP 13. LOCATED AND DRILLED NEW SEAT TRACK SECTION BETWEEN STA 500C+10' TO STA 521 LBL-45.5; [23] INSTALLED SEAT TRACK AND SPLICE REPAIR AT CABIN PASSENGER FROM STA 500C+10' TO STA 521 LBL-45.5 REF B737-7 SRM 53-00-52-2R-4 STEP 4.L THRU N; [27] INSTALLED CABIN FLOOR PANELS #231PF; 231QF; 231VF; 231WF; REF. B737-7 AMM 53-21-00-400-801; [28] REMOVED CORROSION AND SCRATCHES AT MAIN CABIN SEAT TRACK FROM STA. 500B-520 LBL 45.5; AT CROWN UPPER & CENTER SECTION; CUT OUT DAMAGE SECTION AND INSTALLED REPAIR FROM STA500C+10 TO 521.45; REF. USED B737-700 SRM 53-10-02-0G-0; 53-00-52-1A-1; 51-20-01-0G-0; 53-00-52-2R-4; 51-40-08-G-0; & AMM 53-42-11-100-801;

Part: PANEL — ELONGATED (FUSELAGE) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: LOWER FUSELAGE PANEL 193D HAS 2 HOLE ELONGATED. (WORK WITH N/R TTG8Q009W5HD) ; / [01] PREPARED THE DAMAGED FASTENERS HOLES AND FILLED THE HOLE WITH RESIN AND CHOPPED FIBERS; MADE THE SURFACE CONTOUR OF THE REPAIR EQUAL TO INITIAL SURFACE. REF B737-700 SRM 53-40-70-2R-1; SRM 51-70-04-2R-9 PARAGRAPH 4 AND SRM 51-70-04-2R-0 PARAGRAPH 4.; [02] VERIFIED STEP 1.<BR>OK TO INSTALL REPAIR.; [03] APPLIED THE FABRIC REPAIR PLIES AT FASTENERS HOLES DAMAGED. REF B737-700 SRM 53-40-70-2R-1; SRM 51-70-04-2R-9 PARAGRAPH 4; FIGURE 201 REPAIR 9 PAGE 3 AND SRM 51-70-04-2R-0 PARAGRAPH 4.; [04] VERIFIED STEP #3.; [05] OK TO APPLY PROTECTIVE COAT.; [06] APPLIED PROTECTIVE COAT AT REPAIR AREA ACCESS PANEL 193D. REF B737-700 AMM 51-21-99-300-802.; [07] VERIFIED STEP #6; [08] MATERIAL USED RESIN EY 3804 PO#: 1753536 AND BMS9-3-120TYD CL7 PO#: 1690463.; [09] FINAL INSPECTION; PANEL HOLES REPAIRED.

Part: SUPPORT ANGLE — CRACKED · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: L/H RAM AIR INLET DUCT I/B INTERNAL SUPPORT ANGLE STA 540 HAS EVIDENCE OF CRACK ; / [01] REMOVED ANGLE AT LT RAM AIR INLET DUCT I/B INTERNAL SUPPORT STA 540 REF B737-7 SRM 51-40-02-0G-0; [02] VIRIFIED STEP 1; [03] LOCATED AND DRILLED NEW ANGLE SUPPORT REF B737-7 SRM 51-40-05-0G-0; [04] VERIFIED STEP 3<BR>OK TO TREAT AND PRIME; [05] TREATED AND PRIME HOLES AT NEW ANGLE SUPPORT REF B373-7 SRM 51-20-01-0G-0; [06] VERIFIED STEP 5; [07] OK TO INSTALL ALGLE SUPPORT; [08] INSTALLED NEW SUPPORT ANGLE AT LT RAM AIR INLET DUCT STA 540 REF B737-7 SRM 51-40-02-0G-0 AND DWG#143A0060; [09] REMOVED AND REPLACED NEW SUPPORT ANGLE AT LT RAM AIR INLET DUCT I/B STA 540 REF B737-7 SRM 51-40-02-0G-0 AND DWG#143A0060; [10] VERIFIED STEPS 8 & 9.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: LOWER FUS. CENTER WING R/H W/W FWD STA 663.75 STIFFENER CRACKED AT LOWER END O/B OF A/C AIR EXIT DUCT MKD DOT ; / [01] REMOVED LOWER FUSELAGE CENTER WING R/W/W STA 663.75 STIFFENER O/B OF A/C AIR DUCT REF B737-7 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1; [03] LOCATED AND DRILLED NEW STIFFENER ANGLE REF B737-7 SRM 51-40-05-0G-0; [04] VERIFIED STEP 3<BR>OK TO TREAT AND PRIME HOLES; [05] TREATED AND PRIME HOLES AT NWE STIFFENER ANGLE REF B737-7 SRM 51-20-01-0G-0; [06] VERIFIED STEP 5; [07] OK TO INSTALL STIFFENER; [08] PARTIALLY INSTALLED FASTENERS AT STIFFENER ANGLE LOWER FUSELAGE CENTER WING R/W/W STA 663.75 O/B A/C AIR EXIT DUCT REF B737-7 SRM 51-40-02-0G-0; [09] VERIFIED STEP 8; [10] INSTALLED 100% FASTENERS AT LOWER FUSELAGE CENTER WING R/W/W FWD STA 663.75 STIFFENER ANGLE O/B OF A/C AIR EXIT DUCT REF B737-7 SRM 51-40-02-0G-0 AND DWG#111A1000; [11] OK TO CAPSEAL FASTENERS; [12] APPLIED CAP SEALANT AT FASTENERS STIFFENER ANGLE REF B737-7 SOPM 20-50-19; [13] REMOVED AND REPLACED NEW STIFFENER ANGLE AT LOWER FUSELAGE CENTER WING R/W/W FWD STA 663.75 O/B OF A/C AIR EXIT DUCT REF B737-7 SRM 51-40-02-0G-0 AND DWG#111A1000; [14] VERIFIED WORK PERFORMED STEPS 12 AND 13

Part: NONE — LOOSE (R1 DOOR) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: R1 DOOR BOTH UPPER PLATES LOOSE ; / [01] REMOVED R1 DOOR FUSELAGE HINGE TORQUE TUBE AS PER B737-700 AMM 52-41-41-000-801; [02] REMOVED AT R1 DOOR FUSELAGE BODY HINGE TORQUE TUBE UPPER AND LOWER BEARING PLATES AS PER B737-700 SRM 51-40-02-0G-0; [03] VERIFIED STEPS 1 AND 2; [04] OK TO INSTALL; [05] INSTALLED NEW UPPER AND LOWER BEARING PLATES I.A.W B737 SRM 51-40-02-0G-0; [06] VERIFIED STEP 5; [07] OK TO INSTALL TORQUE TUBE; [08] INSTALLED R1 DOOR FUSELAGE HINGE TORQUE TUBE I.A.W B737-700 AMM 52-41-41-400-801.; [09] VERIFIED STEP 8; [10] REMOVED AND REPLACED AT R1 DOOR BOTH UPPER PLATES AND BEARINGS AS PER B737-700 AMM 52-41-41/401 AND SOPM 20-50-03; [11] R1 SERVICE DOOR WILL BE INSTALLED ON CARD TTG8Q009WGSS; [12] VERIFIED STEPS 10 & 11

Part: LIFE LINE — OUT OF ADJUST · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: RIGHT EMERGENCY DOOR LIFE LINE IS NOT STOWED CORRECTLY AND ALUMINUM TAPE IS TORN. ; / [01] INSTALLED RIGHT EMERGENCY EXIT DOOR LIFE LINE CORRECTLY AND ALUMINUM TAPE I.A.W. B737-700 AMM 25-61-10-400-802; [02] VERIFIED 1

Part: PANEL — DELAMINATED (LH WING) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: L/WING L/E ACCESS PANEL 521DB FWD I/B CORNER DELAMINATED ; / [01] PREPARED FOR REPAIR AT PANEL 521 DB AS PER B737-700 SRM 51-70-06-2R-6; [02] VERIFIED STEP 1. OK TO INSTALL REPAIR.; [03] REPAIRED AT PANEL 521 DB AS PER B737-700 SRM 51-70-06-2R-6 PO.1731995; PO.1150387;PO.1713932; [04] VERIFIED STEP 3. OK TO PAINT PANEL.; [05] PREPARED FOR REPAIR AND REPAIRED AT PANEL 521 DB AS PER B737-700 SRM. 51-70-06-2R-6 PO.1731995; PO 1150387 ;PO.1713932 .PAINTED AT PANEL 521 DB AS PER B737-700 AMM 51-21-99-300-802 MATERIAL USED PO.1750464; [06] VERIFIED STEP 5.

Part: SKIN — CRACKED (L/H WING) · airframe 67,914 hrs · 39,947 cycles

SUPPLEMENTAL INFORMATION: L/WING #2 SLAT NOSE SKIN LOWER SURFACE AT ACTUATOR RIB AREA HAS EVIDENCE OF CRACK AROUND 1 EA FASTENER. SLAT STATION 322.71 ; / [01] REMOVED ACCESS PANEL 524DB AS PER B737-700 SRM 51-40-02-0G-0.;[11] FABRICATED FILLER RAPAIR MATERIAL USED 7075-T6 0.071' PO#1746529; DOUBLER REPAIR MATERIAL USED 7075-T6 0.063 PO#1741903 REF B737-7 SRM 57-42-01-2R-8 STEP 4.E TABLE 202 FIG.202 [23] INSTALLED 100% FASTENERS AT LT WING #2 SLAT NOSE SKIN LOWER SURFACE ACTUATOR RIB REPAIR REF B737-7 SRM 57-42-01-2R-8 STEP 4.L; [24] REINSTALLED FLEX SEAL AT LT WING #2 SLAT REF B737-7 SRM 57-42-01-2R-8 STEP 4.M; [25] VERIFIED STEP 23 AND 24; [26] OK TO RE-INSTALL ACCESS PANELS 524CB & 524EB; [27] OK TO RE INSTALL ACCESS PANEL 524DB; [28] REINSTALLED ACCESS PANELS # 524CB;524EB & 524DB AT LT WING SLAT #2 REF B737-7 SRM 51-40-02-0G-0 AND 57-42-01-2R-8 STEP 4.R; [29] VERIFIED STEP 28; [30] PERFORMED AERODINAMIC SMOOTHNESS FILLER SEAL AT LT WING #2 SLAT LOWER SKIN REPAIR REF B737-7 SRM 57-42-01-02R-8 STEP 4.O; [31] ACCOMPLISHED LT WING #2 SLAT NOSE SKIN LOWER SURFACE ACTUATOR RIB REPAIR MATERIAL USED (FILLER). 7075-T6 0.063'( DOUBLER REPAIR) 7075-T6 0.071' REF B737-7 SRM 57-42-01-2R-8 STEP 4. TABLE 202 FIG 202; [32] VERIFIED STEPS 30 AND 31

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 67,822 hrs · 39,887 cycles

AFT ENTRY DOOR SLIDE Z FOLD EXPOSED REPACKED AFT ENTRY DOOR SLIDE PER MT 725-61-06

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 66,301 hrs · 38,921 cycles

R/H EMERGENCY EXIT SIGN LENS MISSING AT OVERWING EXIT DOOR. INSTALLED LENS IAW AMM.

Part: BATTERY PACK — LOW (CABIN) · airframe 64,996 hrs · 38,062 cycles

LT BATTERY PACK M01669 HAD LOW OUTPUT. R&R BATTERY PACK PER AMM.

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 63,732 hrs · 37,241 cycles

***CORROSION*** AFT CARGO BAY INTERCOSTAL AT R/H STA 747-767 HAS CORROSION AT FASTENER HOLES / CORROSION ON THE BAFFLE (INTERCOSTAL) @ THE R/H SIDE STA 747-767 AFT CARGO FOUND TO BE OUT OF LIMITS DUE TO CORROSION AROUND FASTENER HOLES IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED INTERCOSTAL @ THE AFT CARGO R/H SIDE STA 747-767 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; DWG 146A7505 AND 146A7502.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO LT INTERCOSTAL CORRODED BETWEEN BS 500 TO BS 500A, LBL 22. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO RT INTERCOSTAL CORRODED BETWEEN BS 500B TO BS 500C, RBL 22. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FUSELAGE INTERCOSTAL CORRODED AT STA 500B TO STA 500C, LBL 22. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO INTERCOSTAL CORRODED BETWEEN BS 400 TO BS 420, LBL 22. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO INTERCOSTAL CORRODED BETWEEN BS 440 TO BS 460, LBL 22. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO RT INTERCOSTAL CORRODED BETWEEN BS 500A TO BS 500B, RBL 22. R&R INTERCOSTAL PER SRM, ER, AND EA.

Part: INTERCOSTAL — CORRODED (FWD CARGO) · airframe 63,732 hrs · 37,241 cycles

***CORROSION*** FOUND AT THE FWD CARGO L/H INTERCOSTAL FROM STA 460-480 LBL 22 / EVALUATED CORROSION ON L/H FWD CARGO INTERCOSTAL FROM STA 460-480 LBL 22 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED L/H FWD CARGO INTERCOSTAL FROM STA 460-480 LBL 22 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7505 57305U 12/16/18

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO INTERCOSTAL CORRODED BETWEEN BS 500C TO BS 500D, RBL 22. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO INTERCOSTAL CORRODED BETWEEN BS 500C TO BS 500D, LBL 22. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO LT INTERCOSTAL CORRODED BETWEEN BS 500A TO BS 500B, LBL 22. REPAIRED INTERCOSTAL IAW SRM, ER, AND EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO BAY RT FORWARD SHIELD CORRODED AT MULTIPLE FASTENER HOLES. R&R SHIELD IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO BAY CARGO DOOR CUTOUT SUB THRESHOLD WEB CORRODED. R&R WEB IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

AFT CARGO BAY RT AFT Z-ANGLE CORRODED BETWEEN BS 867 TO BS 947.5. R&R SUPPORT IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,732 hrs · 37,241 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS 787 TO BS 887, RBL 14. R&R FLOOR TRACK IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

AFT CARGO BAY DOOR CUTOUT THRESHOLD WEB CORRODED IN MULTIPLE AREAS. R&R WEB IAW SRM AND DWG.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO BAY GUSSET CORRODED AT BS 480, STR 19L. R&R CLIP PER SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 727A TO BS 727B, LBL 17. R&R SUPPORT IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

AFT CARGO BAY LT Z-ANGLE CORRODED BETWEEN BS 727 TO BS 847. REPAIRED Z ANGLE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO BAY RT AFT Z-CHANNEL CORRODED AT MULTIPLE FASTENER HOLES. R&R Z CHANNEL IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO BAY LT GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 63,732 hrs · 37,241 cycles

***CORROSION*** AFT CARGO BAY TRANSITIONING STRIP CORRODED AT STA 887 LBL 9 TO RBL 21 / TRANISTIONING STRIP CORROSION OUT OF LIMITS DUE TO NO LIMITS FOUND IN SRM. REMOVED AND REPLACED NEW TRANISTION STRIP I-A-W AMM 25-52-10-400-801 PO# 711664.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO BAY RT AFT SHIELD CORRODED AT MULTIPLE FASTENER HOLES. R&R SHIELD IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 63,732 hrs · 37,241 cycles

AFT CARGO DOOR AFT CORNER SCUFF PLATE CRACKED / LOCATED AND DRILLED NEW AFT CARGO AFT CORNER SCUFF PLATE IAW B737 SRM 51-40-05-0G-0 TO BE INSTALLED ON CUSTOMER CARD# 753-140-00-02Y

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

AFT CARGO BAY RT FORWARD Z-ANGLE CORRODED BETWEEN BS 727 TO BS 767. R&R Z ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

AFT CARGO BAY DOOR AFT SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 21. REMOVED AFT SHIELD IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

AFT CARGO BAY FLOOR STRAP CORRODED AT BS 794.5, RBL 21.5. R&R STRAP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD CARGO BAY LT Z-CHANNEL CORRODED AT MULTIPLE FASTENER HOLES ACROSS ENTIRE LENGTH. R&R Z CHANNEL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 44. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD PASSENGER COMPARTMENT FLOOR STRUCTURE FORWARD ENTRY DOOR CUTOUT INNER CHORD SUPPORT ANGLE CORRODED AT STR 17L. R&R ANGLE IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD PASSENGER COMPARTMENT FLOOR STRUCTURE STRAP CORRODED AT BS 320, RBL 32. R&R STRAP PER SRM ND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,732 hrs · 37,241 cycles

R1 DOOR NR 5 BEAM CRACKED AT INBOARD SIDE OF RADIUS. R&R R1 DOOR IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

STRINGER CLIP CRACKED AT BS 270, STR 10R. R&R CLIP PER DWG AND SRM.

Part: PANEL — DELAMINATED (LEFT WING) · airframe 63,732 hrs · 37,241 cycles

PANEL 511AB HAS DELAMINATION ON FORWARD INBOARD CORNER. / REPAIRED DELAMINATION ON FORWARD INBOARD CORNER OF PANEL 511AB IAW SRM 57-41-01-2R-1 PARA 4. E. TABLE 202 + SRM 51-70-05-2R-6

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 63,732 hrs · 37,241 cycles

VERTICAL STIFFENER CRACKED ATTACH TO VAPOR BARRIER AT BS 663, LBL 27. R&R STIFFENER IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD PASSENGER COMPARTMENT FLOOR STRUCTURE SERVICE DOOR CUTOUT INNER CHORD CORRODED BETWEEN BS 293 TO BS 342, STR 17L. R&R CHORD IAW SRM & DWG.

Part: STRINGER CLIP — GOUGED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

STRINGER CLIP GOUGED AT BS 360, STR 10L. R&R STRINGER CLIP PER DWG & SRM.

Part: ANGLE — CORRODED (FED THRESHOLD) · airframe 63,732 hrs · 37,241 cycles

FORWARD PASSENGER COMPARTMENT FLOOR STRUCTURE; S17L AT FWD. ENTRY DOOR CUT OUT ANGLE ATTACHED TO SKIN HAS CORROSION. / REMOVED CORROSION I-A-W SRM 51-10-02-0G-0. L=2'; W=1'; D=.009' OUT OF LIMITS PER SRM 53-10-15-1A-1 PG 4.C.(2)(A). REMOVED FWD ENTRY DOOR CUT OUT ANGLE PER SRM 51-40-02-0G-0. FORMED NEW ANGLE PER B DWG# 141A8234 SRM 51-30-01; MATERIAL USED 2024 'O'.063' LOT# 5019863; HEAT TREATED 2024T3 PO# 721212; LOCATED AND DRILLED FASTENER HOLES PER SRM 51-40-05-0G-0. TREATED AND PRIMED PER AMM 51-21-41-370; AMM 51-21-72-370. INSTALLED ANGLE PER BDWG# 141A8230 AND SRM 51-40-02-0G-0. AT FWD PASSENGER COMPT FLOOR STRUCTURE S17L FWD ENTRY DOOR CUTOUT.

Part: FLOORBEAM — SCRATCHED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FORWARD PASSENGER COMPARTMENT FLOOR STRUCTURE FLOORBEAM UPPER SURFACE SCRATCHED AT BS 328, BETWEEN RBL 21 TO RBL 43. R&R CHORD PER EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

L1 DOOR CUTOUT CENTER SCUFF PLATE SUPPORT ANGLE CORRODED, STR 17L. R&R "Z" ANGLE PER SRM & DWG.

Part: STRUCTURE — CORRODED (R1 DOOR) · airframe 63,732 hrs · 37,241 cycles

R1 DOOR INNER CHORD CORRODED BETWEEN BS 294.5 TO BS 328. R&R CHORD IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

AFT WET AREA FLOOR STRUCTURE STRAP CORRODED AT BS 1020, LBL 2. R&R STRAP IAW SRM & DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

AFT WET AREA FLOOR STRUCTURE CORRODED AT BS 1015, LBL 42.5. R&R SHEAR WEB IAW SRM AND DWG.

Part: BEAM — CORRODED (CABIN) · airframe 63,732 hrs · 37,241 cycles

***CORROSION*** FLOOR BEAN IN THE FWD WET AREA AT STA 294.5 RBL 13.5 HAS CORROSION / FLOOR BEAM IN WET AREA AT STA 294.5 RBL 13.5 HAD CORROSION AREA WAS REPAIRED IAW ER 18-05975 REV. P1 AND EA 1-753-33815 REV IR

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FLOOR PANEL 221GF BROKEN AT O/B FWD CORNER / REPAIRED BROKEN EDGE AT O/B FWD CORNER OF FLOOR PANEL 221GF PER SRM 53-00-50-2R-6. DAMAGE WAS BEYOND ALLOWABLE LIMITS PER SRM 53-00-50-1A-1 PARA 4E(1)

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FLOOR PANEL 242TF O/B AFT CORNER IS DISBONDED / REPAIRED FLOOR BOARD PANEL 242TF O/B AFT CORNER IAW 737-700 SRM 53-00-50-2R-9 PARA 3 A-I

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FLOOR PANEL 221BF DELAMINATED AT I/B CORNER / REPAIRED DELAMINATION AT I/B CORNER OF FLOOR PANEL 221BF PER SRM 53-00-50-2R-1. DAMAGE WAS BEYOND ALLOWABLE LIMITS PER SRM 53-00-50-1A-1 PARA 4F

Part: WEB — CORRODED (CABIN) · airframe 63,732 hrs · 37,241 cycles

***CORROSION*** AFT WET AREA FLOOR STRUCTURE HAS CORROSION AT STA 1016 LBL 4. (MARKED) / AFT WET AREA FLOOR STRUCTURE CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS IN SRM. REPAIRED FLOOR STRUCTURE SHEAR WEB IAW ER 18-05892 REV IR AND EA 1-753-33831 REV IR

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

R2 DOOR LOWER CUTOUT INNER CHORD CORRODED BETWEEN BS 956 TO BS 990, RBL 45. R&R CHORD PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 297, BL 0. R&R INTERCOSTAL IAW SRM AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,732 hrs · 37,241 cycles

FLOORBEAM CORRODED AT BS 986, RBL 30. REPAIRED T-CHORD IAW SRM AND EA.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 63,732 hrs · 37,241 cycles

LT MAIN LANDING GEAR VAPOR BARRIER CRACKED. REPAIRED BARRIER IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,732 hrs · 37,241 cycles

LT WING NR 3 SLAT NOSE SKIN CRACKED AT ACTUATOR ATTACHMENT. R&R NR 3 SLAT ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,732 hrs · 37,241 cycles

LT WING NR 1 SLAT NOSE SKIN CRACKED AT ACTUATOR ATTACHMENT. REPAIRED NR 1 SLAT NOSE SKIN IAW SRM.

Part: VAPOR BARRIER — DEBONDED (RT MLG WW) · airframe 63,732 hrs · 37,241 cycles

RT MAIN LANDING GEAR VAPOR BARRIER DEBONDED. REPAIRED BARRIER PER SRM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 62,770 hrs · 36,611 cycles

L1 DOOR SLIDE LOOSE FROM HOUSING. REINSTALLED SLIDE PER MT.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 62,418 hrs · 36,379 cycles

FORWARD GALLEY LOWER EMERGENCY FLASHLIGHT STRAPS BROKEN. R&R STRAPS PER SIP.

Part: SIGN — UNSECURE (CABIN) · airframe 62,407 hrs · 36,373 cycles

RT EXIT ROW SIGN CAME OFF. INSTALLED LIGHT PER AMM.

Part: SIGN — DISLODGED (CABIN) · airframe 60,894 hrs · 35,438 cycles

AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN DISLODGED. INSTALLED SIGN PER MM.

Part: COVER — MISSING (R2 DOOR SLIDE) · airframe 59,555 hrs · 34,596 cycles

R2 DOOR SLIDE MANUAL EXTENSION HANDLE COVER MISSING. INSTALLED THE COVER IAW MT.

Part: COVER — MISSING (L2 DOOR SLIDE) · airframe 59,555 hrs · 34,596 cycles

L2 DOOR SLIDE MANUAL EXTENSION HANDLE COVER MISSING. INSTALLED THE COVER IAW MT.

Part: BATTERY — FAILED (CABIN) · airframe 59,311 hrs · 34,439 cycles

FORWARD RT BATTERY FAILED TIME TEST. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,311 hrs · 34,439 cycles

AFT RT BATTERY FAILED TIME TEST. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,311 hrs · 34,439 cycles

AFT LT BATTERY FAILED TIME TEST. R&R BATTERY PER AMM.

Part: FITTING — LOOSE (L1 DOOR) · airframe 58,658 hrs · 34,039 cycles

L1 DOOR EVAC SLIDE FWD GIRT BAR CLIP LOOSE. SECURED & ADJUSTED CLIP PER MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 58,559 hrs · 33,972 cycles

FORWARD GALLEY FLASHLIGHT STRAP BROKEN. R & R THE STRAP IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 57,141 hrs · 33,144 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS IAW AMM.

Part: FLAP — DAMAGED (LT WING) · airframe 57,141 hrs · 33,144 cycles

LT WING TRAILING EDGE INBOARD AFT FLAP DAMAGED. R&R AFT FLAP IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,141 hrs · 33,144 cycles

FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (BS 663) · airframe 57,141 hrs · 33,144 cycles

RIGHT AIR CONDITIONING BAY AFT BULKHEAD CRACKED AT BS 663. REPAIRED THE BULKHEAD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,141 hrs · 33,144 cycles

RT AIR CONDITION PACK BAY AFT BULKHEAD UPPER ATTACH ANGLE CRACKED AT STA 663. REPAIRED ANGLE IAW EA.

Part: SIGN — BROKEN (CABIN) · airframe 57,141 hrs · 33,144 cycles

AFT LAV EMERGENCY EXIT SIGN BROKEN. R&R SIGN IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,141 hrs · 33,144 cycles

LT BULKHEAD AND FRAME CRACKED AT BS 727, WL 200. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,141 hrs · 33,144 cycles

RT BULKHEAD AND FRAME CRACKED AT BS 727, WL 200. REPAIRED FRAME IAW EA.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,670 hrs · 32,868 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 56,110 hrs · 32,541 cycles

AFT GALLEY EMERGENCY EXIT SIGN LENS LOOSE AT FLOOR LEVEL. SECURED THE SIGN LENS PER SIP.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 55,557 hrs · 32,189 cycles

AFT GALLEY INBD EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 55,548 hrs · 32,184 cycles

CENTER AISLE OVER WING EMER EXIT SIGN LOOSE. SECURED SIGN AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 54,608 hrs · 31,674 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. R&R SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 54,164 hrs · 31,418 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

LONGITUDINAL FLOORBEAM UPPER AFT END CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM IAW ACO & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75, FASTENER HOLE NR 9. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75, FASTENER HOLE NR 10. REPAIRED SEAT TRACK IAW EA.

Part: TIE DOWN — CORRODED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

L1 DOOR EMER EVAC SLIDE AFT GIRT BAR TIE DOWN, CORRODED AT NUTPLATE HOLES. R & R TIE DOWN IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75, FASTENER HOLE NR 8. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5, FASTENER HOLE NR 8. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5, FASTENER HOLE NR 10. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75, FASTENER HOLE NR 8. REPAIRED SEAT TRACK IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

FLOORBEAM FASTENER HOLE NR 3 CRACKED AT BS 727B, LBL 24. REPAIRED BEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

AFT SEAT TRACK CRACKED AT BS 727B, LBL 45.5 IN FWD HOLE. REPAIRED SEAT TRACK IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

STRINGER CLIP CORRODED AT BS 727A, STRINGER 3R. R & R CLIP IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 53,817 hrs · 31,227 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, RBL 41.5. REPAIRED WEB IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,817 hrs · 31,227 cycles

RIGHT STOW BIN EMER ESCAPE LIGHT INOPERATIVE AT ROW 3. RELAMPED LIGHT IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75, IN FASTENER HOLE NR 5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5, IN FASTENER HOLE NR 7. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.4, IN FASTENER HOLE NR 8. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5, IN FASTENER HOLE NR 9. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75, IN FASTENER HOLE NR 7. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5, IN FASTENER HOLE NR 9. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75, IN FASTENER HOLE NR 9. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75, IN FASTENER HOLE NR 2. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,817 hrs · 31,227 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75, IN FASTENER HOLE NR 10. REPAIRED SEAT TRACK IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 53,741 hrs · 31,182 cycles

FORWARD ENTRY EXIT LIGHT, LENS LOOSE. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,705 hrs · 31,160 cycles

L1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,647 hrs · 31,127 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,468 hrs · 31,025 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,129 hrs · 30,811 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,064 hrs · 30,778 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,030 hrs · 30,759 cycles

LEFT EMERGENCY EXIT STOW BIN LIGHT INOPERATIVE AT ROW 20. RELAMPED LIGHT IAW AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 52,307 hrs · 30,348 cycles

L1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: SLIDE — TORN (R2 DOOR) · airframe 52,236 hrs · 30,309 cycles

R2 DOOR EMER EVAC SLIDE TORN. R & R SLIDE IAW MT.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,163 hrs · 29,701 cycles

AFT CARGO BULKHEAD PANEL SUPPORT ANGLE CRACKED AT BS 947. R & R ANGLE IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 50,192 hrs · 29,151 cycles

LEFT OVERWING LOWER EMER LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 49,700 hrs · 28,872 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 49,693 hrs · 28,867 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 49,174 hrs · 28,586 cycles

L1 DOOR SLIDE OUT OF ADJUSTMENT. REPOSITIONED SLIDE IAW MM.

Part: HANDLE — LOOSE (L2 DOOR) · airframe 49,005 hrs · 28,484 cycles

L2 DOOR EMER EVAC SLIDE MANUAL HANDLE LOOSE. SECURED HANDLE IAW SIP.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,271 hrs · 28,062 cycles

LEFT NR 1 WINDOW FRAME NR 4 FASTENER HOLE CRACKED. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (NR 3 WINDOW) · airframe 48,271 hrs · 28,062 cycles

RIGHT NR 3 WINDOW FRAME E F POST CRACKED AT 2ND FASTENER HOLE FROM BOTTOM. REPAIRED POST IAW ACO.

Part: WINDOW FRAME — CRACKED (NR 3 WINDOW) · airframe 48,271 hrs · 28,062 cycles

LEFT NR 3 WINDOW FRAME E F POST CRACKED AT 1ST & 2ND FASTENER HOLES FROM BOTTOM. REPAIRED POST IAW ACO.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 47,983 hrs · 27,887 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW SIP.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,363 hrs · 25,700 cycles

FORWARD CARGO AFT CEILING AT AFT BULKHEAD HAS SEVERAL CRACKS. REPAIRED PER AMM.

Part: GUIDE — MISSING (EVAC SLIDE) · airframe 43,765 hrs · 25,339 cycles

FWD SERVICE DOOR GIRT BAR MISSING PLASTIC GUIDE. REMOVED AND REPLACED FWD RIGHT SLIDE REF M/M ICT 633802 P/N OFF/ON 63550-101 S/N OFF 0337F S/N ON 0214F

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

WIRE BUNDLE ATTACH CLIP AT BS 867 BETWEEN STR 2-3 R CRACKED. REMOVED AND REPLACED WIRE BUNDLE ATTACH CLIP AT BS 867 BETWEEN STR 2-3R PER SRM 51-40-02-0G-0 56173U, 24NOV12.

Part: PIN — DEFORMED (RT HORIZ STAB) · airframe 43,718 hrs · 25,310 cycles

RIGHT HORIZ STAB REAR SPAR LOWER ATTACHMENT PIN HAS DEFORMED PLATING. REMOVED AND REPLACED PIN IAW AMM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FWD CARGO BAY INTERCOSTAL ATTACH ANGLE IS CRACKED ON FWD SIDE OF BS 500C FRAME RBL 24. REMOVED AND REPLACED FWD CARGO BAY ATTACH ANGLE PER SRM.

Part: PANEL — CRACKED (RT HORIZ STAB) · airframe 43,718 hrs · 25,310 cycles

RIGHT HORIZONTAL STAB PANEL 341B, NR 2 RIB UP FROM BOTTOM IS CRACKED. REPAIRED RIGHT HORIZONTAL, STAB PANEL 341B, NR 2 RIB UP FROM BOTTOM IAW EA1-755-1751 AND ATS ER 12-03550.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,718 hrs · 25,310 cycles

LEFT HORIZONTAL STAB PANEL 331B NR 2 RIB UP FROM BOTTOM IS CRACKED. REMOVED AND REPLACED; LOCATED HOLES, DRILLED, DEBURRED NEW RIB PO #419604 & INSTALLED AT LT HORIZONTAL STAB PANEL 331B NR 2 RIB IAW SRM 51-40-05 & SRM 51-40-02.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,718 hrs · 25,310 cycles

LEFT HORIZONTAL STAB PANEL 331B NR 3 RIB UP FROM BOTTOM IS CRACKED. REMOVED AND REPLACED; LOCATED HOLES DRILLED, DEBURRED NEW RIB PO 419604 & INSTALLED AT LT HORIZONTAL STAB PANEL 331B NR 3 RIB IAW SRM 51-40-05 & SRM 51-40-02.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FLOOR PANEL 231AF HAS A BROKEN INSERT. FLOOR PANEL 231AF BROKEN INSERT WAS REPAIRED PER SWA EA 1-A53-13206 DATED 8/16/2010, EA 1-753-21061 DATED 14-NOV-2012, AND ATS ER 12-13536 DATED 14NOV2012.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,718 hrs · 25,310 cycles

LT HORIZONTAL STAB, INSPAR RIB AT STA 92.7 IS CRACKED AT 2ND VERTICAL STIFFENER ON THE LOWER END. REMOVED, REPAIRED, REINSTALLED LT HORIZ STAB INSPAR RIB, 2ND VERTICAL STIFFENER AT STAB STA 92.7 IAW SRM 55-10-09-2R-4, SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

BS 335 STR 5R PREVIOUS REPAIR DOUBLER IS CRACKED. REMOVED AND REPLACED NEW INTERCOSTAL PO 418553 P/N 141A8330-62 IAW SRM 51-40-02 AT BS 328-344 STR 5R.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION ON I/B ANGLE FOR CREASE BEAM WEB BS 638 STR 17L. REPAIRED CORROSION ON I/B ANGLE CREASE BEAM WEB BS 638 STR 17C IAW ER 12-03523 & EA 1-753-21137.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION ON FLOOR SUPPORT BS 727D +5" RBL 3 WL 155. REPAIRED FLOOR SUPPORT AT BS 727D+5" RBL 3 WL 155 PER EA 1-A53-4982.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 907 STR 8-9R. REPAIRED FRAME CRACKED A/C BRACKET ATTACHMENT BS 907 STR 8-9R IAW ER 12-03470 & EA 1-753-21111.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 480, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FUSELAGE BELLY SKIN ADF PANEL CORRODED BETWEEN BS 241 TO BS 242. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 727D, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION ON FLOOR TO SIDE WALL SUPPORT BS 727 - 767 RBL 22 WL 155. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS 727-767 RBL 22 WL 155 PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION ON FLOORBOARD ATTACH STRAP AROUND FASTENER HOLES BS 887 RBL 15 - LBL 15 WL 168. FABRICATED FLOORBOARD STRAP SPLICE BS 887 RBL 15 - LBL 15 WL 168 IAW DRW 146A9401 & INSTALLED PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION ON FLOOR SUPPORT BS 772 RBL 3 WL 155. REPAIRED FLOOR SUPPORT BS 772 RBL 3 WL 155 IAW EA 1-A53-4982 REV 3 89004U 10NOV12.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,718 hrs · 25,310 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STA 92.70. REPAIRED RIB IAW SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION AFT SIDE SHEAR TIE ATTACH ANGLE BS 727B RBL 6 WL 148. REMOVED AND REPLACED ANGLE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION AT AFT CARGO BAY SUB THRESHOLD WEB HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED AFT CARGO BAY SUB THRESHOLD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 360 STR 8-9R. REPAIRED FUSELAGE FRAME CRACKED AT AIR CONDTIONING BRACKET ATTACHMENT BS 360 STR 8-9R IAW ER 12-03469 & EA 1-753-21001.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 907 STR 8-9R. REPAIRED FRAME CRACKED A/C BRACKET ATTACHMENT BS 907 STR 8-9R IAW ER 12-03470 & EA 1-753-21111 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS500C STR8-9L. WORK ACCOMPLISHED PER EA# 1-A53-12114 REV 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION AT ON FLOOR SUPPORT BS 727D +5" LBL 12 WL 155. REPAIRED FLOOR SUPPORT AT BS727+5" LBL 17 WL 155 PER EA NR 1-A53-4982.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION ON FLOOR SUPPORT BS 772 RBL 8 WL 155. REPAIRED FLOOR SUPPORT BS 772 RBL 8 WL 155 IAW EA 1-A53-4982 REV 3 89004U 10NOV12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FLOOR SUPPORT CORRODED AT BS 951, RBL 31, WL 208. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION ON FLOOR SUPPORT BS 793 - 853 RBL 15 WL 155. REPAIRED FLOOR SUPPORT FROM BS 747+8.5" TO BS 887 RBL 15 WL 155 PER SRM 53-00-53-2R-3 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION ON FLOOR SUPPORT BS 727D +5" RBL 8 WL 155. REPAIRED FLOOR SUPPORT AT BS 727D+5" RBL 8 WL 155 PER EA 1-A53-4982.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 867 STR 8-9R. REPAIRED FRAME AT BS 867 STR 8-9R IAW EA 1-A53-12114.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 747, STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 727D, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 440, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 500A, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 480, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 500A, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT I/B FASTENER HOLE AT PSU RAIL SUPPORT BS 827 STR 8R - 9R. REPAIRED FRAME CRACKED AT I/B FASTENER HOLE OF PSU RAIL SUPPORT BS 827 STR 8R - 9R IAW ER 12-03535 & EA 1-753-21112 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 747, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT I/B FASTENER HOLE AT PSU RAIL SUPPORT BS 787 STR 8R - 9R. REPAIRED CRACKED FRAME BS 787 STR 8-9 RT IAW EA 1-A53-12114.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 787, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT BS 827, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FRAME CRACKED AT I/B FASTENER HOLE AT PSU RAIL SUPPORT BS 827 STR 8R - 9R. REPAIRED FRAME CRACKED AT I/B FASTENER HOLE OF PSU RAIL SUPPORT BS 827 STR 8R - 9R IAW ER 12-03535 & EA 1-753-21112.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

BS 294 WL 208 RBL 53 FWD SERVICE DOOR FWD FRAME IS CRACKED AT FASTENER HOLE. REPAIRED FWD SERVICE DOOR FWD FRAME AT BS 294 WL 208 RBL 53 PER EA 1-753-21082.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

BS 294 - 312 WL 208 RBL 15 INTERCOSTAL CRACKED AT FASTENER HOLES. BS 294 - 312 ML208, RBL 15. REMOVED AND REPLACED NEW INTERCOSAL ITEM 7530291. PO 418937 IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION CARGO BAY RIGHT SIDE FLOOR-TO-SIDEWALL BS 500B - 500D RBL 24. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

BS 312-324 WL 208 RBL 30 INTERCOSTAL CRACKED AT FASTENER HOLES. BS 312-324 WL 208, RBL 30 REMOVED AND REPLACED INTERCOSTAL P/N 141A5410V12 PO 418939 IAW SRM 51-40-05 AND SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED AFT SIDE BS 500C FRAME LBL 24, WL 153. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FLOOR SUPPORT CORRODED AT BS 956, RBL 27. REMOVED AADN REPLACED SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

BS 324 - 344 WL 208 LBL 45 INTERCOSTAL CRACKED AT FASTENER HOLE. BS 324-344 WL 208 LBL 45 REMOVED AND REPLACED NEW INTERCOSTAL P/N 141A5410U16 REG NUMBER 532790 IAW SRM 51-40-02 AND SRM 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CORROSION ON FLOOR SUPPORT AT BS 951, RBL 31-44, WL 208. REMOVED AND REPLACED FLOOR SUPPORT AT BS 951 RBL 31-44 WL 208 IAW SRM 51-40-02 P/N 147A5765U26.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED ON SIDE BS 500C FRAME LBL 24, WL 153. REMOVED AND REPLACED ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FWD CARGO BAY STR 19R TIE ANGLE (CLIP) IS CRACKED AT I/B FLANGE COMMON TO BS 500D BULKHEAD ANGLE. REMOVED & REPLACED FWD CARGO BAY STR 19R TIE ANGLE (CLIP) BS 500D IAW SRM 51-40-02-0G-0.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FWD CARGO BAY STR 19L TIE ANGLE (CLIP) IS CRACKED AT I/B FLANGE COMMON TO BS 500D BULKHEAD ANGLE. REMOVED AND REPLACED FWD CARGO BAY STR 19L TIE ANGLE (CLIP) BS 500 D SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

BS 312-324 WL 208 LBL 45 INTERCOSTAL CRACKED AT FASTENER HOLE. REMOVED AND REPLACED NEW INTERCOSTAL P/N 141A5410V12 PO 418915 BETWEEN BS 312 - 324 WL 208 LBL 45 IAW SRM 51-40-02 AND SRM 51-40-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,718 hrs · 25,310 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986. REPAIRED CHORD IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 43,718 hrs · 25,310 cycles

LEFT WING T/E, AFT SUPPORT ANGLE CRACKED FORM UPPER T/E PANEL ABOVE NR 1 ENGINE STRUT. REMOVED AND REPLACED ANGLE IAW SOPM AND SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 43,718 hrs · 25,310 cycles

LEFT WING T/E, BULB SEAL SUPPORT ANGLE CRACKED ABOVE NR 1 ENGINE STRUT. REMOVED AND REPLACED CRACKED BULB SEAL SUPPORT ANGLE ON LEFT WING T/E ABOVE NR 1 ENGINE STRUT IAW SOPM 20-50-01 AND SRM 51-40-02-0G-0 STEPS 4. A, B, C AND E 7438U 08NOV12.

Part: SUPPORT — BROKEN (RT WING) · airframe 43,718 hrs · 25,310 cycles

RT WING, LOWER T/E SUPPORT ROD ATTACH POINT ON I/B - O/B FLAP DEFLECTION RIB IS BROKEN. REPAIRED LOWER T/E SUPPORT ROD ATTACH POINT ON THE I/B-O/B RT/WING DEFLECTION R/B PER EA 1-A57-1997 REV 1, EA 1-757-07693 AND ER 12-03549.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,718 hrs · 25,310 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,718 hrs · 25,310 cycles

THE LEFT HORIZ STAB LWR SKIN HAS A 3.2' CRACK 3.2" FROM STAB STA 92.70. REPAIRED LEFT HORIZ STAB LWR SKIN 3.2" FROM STAB STA 92.70 IAW SRM 55-10-01-2R-11 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,914 hrs · 24,820 cycles

R1 WINDOW FRAME POST CRACKED. REPAIRED FRAME PER EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,914 hrs · 24,820 cycles

L1 WINDOW FRAME POST CRACKED. REPAIRED FRAME PER EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,912 hrs · 24,819 cycles

R1 WINDOW FRAME POST CRACKED. REPAIRED FRAME PER EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,912 hrs · 24,819 cycles

L1 WINDOW FRAME CRACKED. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,518 hrs · 24,588 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 42,518 hrs · 24,588 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 38,948 hrs · 22,545 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. R&R LIGHT ASSY. PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 37,700 hrs · 21,817 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,393 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, LBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,393 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, RBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,393 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, LBL 54. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,393 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,393 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,393 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 540, LBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,435 hrs · 20,513 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,435 hrs · 20,513 cycles

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

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 35,004 hrs · 20,254 cycles

FWD LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,490 hrs · 19,953 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 11. RELAMPED PER MM.

Part: LIGHT — BROKEN (R1 DOOR) · airframe 31,920 hrs · 18,416 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 31,137 hrs · 17,933 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 6 SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 31,137 hrs · 17,933 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,647 hrs · 17,658 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,360 hrs · 17,478 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 7 TO RBL 20. REMOVED AND REPLACED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,360 hrs · 17,478 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 41 TO LBL 43. REPAIRED BEAM PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 29,162 hrs · 16,765 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 29,162 hrs · 16,765 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,725 hrs · 16,498 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 23,713 hrs · 13,507 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,765 hrs · 12,963 cycles

DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 21,469 hrs · 12,226 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED FUNCTIONAL TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 21,469 hrs · 12,226 cycles

DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY EXIT BATTERY PACK FAILED FUNCTIONAL TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 21,469 hrs · 12,226 cycles

DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY EXIT BATTERY PACK FAILED FUNCTIONAL TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — MALFUNCTIONED (R1 DOOR) · airframe 17,409 hrs · 9,874 cycles

R1 DOOR EMERGENCY EVAC SLIDE MALFUNCTIONED DURING EMERGENCY DEPLOYMENT. REMOVED AND REPLACED SLIDE PER MM.

Part: STRAP — BROKEN (L1 DOOR SLIDE) · airframe 17,409 hrs · 9,874 cycles

DURING SCHEDULED RON CHECK, L1 DOOR EMERGENCY EVAC SLIDE CASE BONDING STRAPS BROKEN. REMOVED AND REPLACED BONDING STRAPS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 16,679 hrs · 9,476 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. INSTALLED SLIDE PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 15,362 hrs · 8,725 cycles

DURING SCHEDULED MV2 CHECK, FOUND 2 EACH LENSES MISSING FROM EEPLS AT ROWS 12C AND 10C. REMOVED AND REPLACED LIGHT LENSES PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 14,747 hrs · 8,365 cycles

L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 13,588 hrs · 7,694 cycles

DURING SCHEDULED RON, FOUND EEPLS LIGHT LENSES AT RT ROW 3, RT ROW 11, BROKEN. REMOVED AND REPLACED EEPLS LENSES PER MM.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 13,426 hrs · 7,599 cycles

L1 DOOR EVAC SLIDE DEPLOYED AT GATE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — LOW (L2 DOOR) · airframe 12,901 hrs · 7,324 cycles

L2 DOOR EVAC SLIDE PRESSURE LOW PRESSURE INDICATION. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 12,596 hrs · 7,153 cycles

EEPLS COVER LOOSE AT OVERWING EXIT ROW. SECURED EEPLS COVER PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 12,585 hrs · 7,148 cycles

EEPLS COVER AT OVERWING EMERGENCY EXIT BROKEN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,574 hrs · 7,144 cycles

OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 12,248 hrs · 6,974 cycles

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

Part: LENS — MISSING (CABIN) · airframe 11,909 hrs · 6,802 cycles

RED LENS MISSING FROM EEPLS AT OVERWING. INSTALLED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 10,677 hrs · 6,122 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 1, 3, 5, 12, 15, 20 AND 23. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 7,981 hrs · 4,603 cycles

EEPLS COVER DAMAGED AT ROW NR 16. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 7,981 hrs · 4,603 cycles

EEPLS COVER DAMAGED AT ROW NR 16. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 8,027 hrs · 4,787 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.