N717SA

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 77,953 hrs · 46,354 cycles

THE ESCAPE SLIDES ON BOTH FWD ENTRY DOOR AND FWD SERVICE DOOR ARE HANGING UNUSUALLY LOW BELOW THEIR CONTAINERS ; / [01] READJUSTED BOTH FWD ENTRY AND FWD SVC DOOR EMERGENCY ESCAPE SLIDES PER 25-66-00

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 77,953 hrs · 46,354 cycles

THE ESCAPE SLIDES ON BOTH FWD ENTRY DOOR AND FWD SERVICE DOOR ARE HANGING UNUSUALLY LOW BELOW THEIR CONTAINERS ; / [01] READJUSTED BOTH FWD ENTRY AND FWD SVC DOOR EMERGENCY ESCAPE SLIDES PER 25-66-00

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 76,640 hrs · 45,600 cycles

AFT SERVICE DOOR SLIDE ' PULL TO INFLATE TAB' IS OUT OF THE CASE. FOUND VELCRO COVER DESLODGED; REPOSITION PER S.I.P

Part: SKIN — CRACKED (BS 639) · airframe 76,395 hrs · 45,467 cycles

REF LP 0990749 WHILE PERFORMING EA 1-A53-36784 AND MT 5331-I-11783-NG PART 6; 53-30-25 FOUND CRACK INDICATION AT BS 639 + 9' S4R AT CHEM MILLED EDGE. CRACK WAS LOCATED WITH PART 6; 53-30-18 AND VERIFIED WITH PART 4; 53-30-07. / ACCOMPLISHED ALL EA 1-A53-10228 REV 1; INSP REPEAT REQUIRED; THRESHOLD 50;000 CYCLES AND REPEAT INSP. 4;500 CYCLES. ACCOMPLISHED ALL EA 1-A53-14845.LATEST REV. ACCOMPLISH ALL EA 1-A53-14846 LATEST REV. THRESHOLD 50;000 CYCLES AND 8;000 CYCLES. REPEAT SEE SA-M 326 ATTACHED #A1308452

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 75,125 hrs · 44,712 cycles

LEFT HORIZONTAL STAB L/E ;LOW SLIDE CRACKED. / REMOVED AND REPLACED PER AMM 53-31-31

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 75,121 hrs · 44,711 cycles

EXTERNAL EXIT LIGHT RIGHT SIDE AFT OF WING FLAP IS OUT / REPLACED FUSE FOR RIGHT GROUND ILLUMINATION EXIT LIGHT STA757 PER AMM 33-51-06-960-804 AND REPLACED LAMP FOR RIGHT STA757 GROUND ILLUMINATION EXIT LIGHT PER AMM 33-51-04-960-801. OPS CHECKED RIGHT GROUND ILLUMINATION EXIT LIGHT STA 757 PER AMM 33-51-04-960-801 CHECKED GOOD

Part: FLOOR SUPPORT — CRACKED (BS 277-294.5) · airframe 75,121 hrs · 44,711 cycles

PASSENGER CABIN FLOOR INTERCOSTAL BS 277-BS 294.5; RBL 1; WL 208 IS CRACKED. / REMOVED INTERCOSTAL BS277-294 RBL1; LOCATED AND DRILLED NEW INTERCOSTAL; ALL I.A.W BOEING DWG 141A5400; SRM 51-40-05-0G-0; 51-40-02-0G-0. OK TO INSTALL 80512R 23JUL20. INSP 357 JUL232020 INSTALLED NEW INTERCOSTAL (BS277-BS294.5 RBL1 WL208 I.A.W BOEING DWG 141A5400 AND SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (BS 259) · airframe 75,121 hrs · 44,711 cycles

CORROSION ON BS 259 FLOOR BEAM UPPER FWD CHORD AT BL 0 -LBL 4 WL208 / REPAIRED DAMAGE ON BS 259 FLOOR BEAM UPPER FWD CHORD AT BL0-LBL4. WL208 PER ER 20-02921 REV IR AND EA 20-153-01297 REV IR

Part: FLOORBEAM — CORRODED (BS 259) · airframe 75,121 hrs · 44,711 cycles

CORROSION ON BS 259 FLOOR BEAM UPPER AFT CHORD AT LBL 12. DAMAGED REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01297 REV IR (ATS ER 20-02921 REV IR).

Part: FLOOR SUPPORT — CORRODED (BS 259-270) · airframe 75,121 hrs · 44,711 cycles

CORROSION ON FLOOR SUPPORT BS 259 - 270; LBL 12 / REMOVED AND REPLACED FLOOR SUPPORT BS 259-270 LBL12 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; BOEING DWG# 141A5210; AND BOEING DWG# 140A9810.

Part: SKIN — DENTED (BS 360) · airframe 75,121 hrs · 44,711 cycles

DENT ON FUSELAGE SKIN BS360+2' 5' BELOW STR 4L REF NRC V474386 / DAMAGE REPAIRED PER EA 20-153-01291 REV IR AND ATS ER 20-02933 REV IR. REFER TO NRC U188571 FOR TRACKING

Part: SKIN — CORRODED (BS 679-701) · airframe 75,121 hrs · 44,711 cycles

ADF NO. 1 ANTENNA FASTENER HOLES HAVE CORRROSION - BS679-BS701; RBL1-RBL9; WL308.5 / REPAIRED SKIN UNDER ADF ANTENNA BS679-701 RBL1-RBL9 IAW EA 20-153-01236 REV IR AND ER 20-02930 REV IR.

Part: HOUSING — DAMAGED (LT OVRWG DOOR) · airframe 75,121 hrs · 44,711 cycles

L/H OVERWING EXIT LIFT HANDLE HOUSING DAMAGED / REMOVED LH OVERWING EXIT LIFT HANDLE HOUSING AND INSTALLED NEW LH OVERWING EXIT LIFT HANDLE HOUSING IAW AMM 52-22-51-400-801 STEPS 3C-2D 57045U 7-29-2020

Part: SKIN — DENTED (BS 259) · airframe 75,121 hrs · 44,711 cycles

DENT ON FUSELAGE SKIN BS259+6' 2' ABOVE STR 17L REF L110399 AND C029806 / REPAIRED PER EA 20-153-01179 REV IR AND ATS ER 20-02868 REV IR

Part: SKIN — DENTED (BS 328) · airframe 75,121 hrs · 44,711 cycles

DENT ON FUSELAGE SKIN BS 328+8.5' 1' ABOVE STR 26R REF 9667278 / REPAIRED PER: EA 20-153-01183 REV IR AND ATS ER 20-02869 REV IR

Part: SKIN — DENTED (BS 1006) · airframe 75,121 hrs · 44,711 cycles

FUSELAGE SKIN HAS DENT BS 1006+2' 2.5' BELOW 15R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01276 REV IR AND ATS ER 20-02937 REV IR. REFER TO NRC U188806 FOR TRACKING

Part: FORMER — CHAFED (FAIRING) · airframe 75,121 hrs · 44,711 cycles

FAIRING FORMER HAS CHAFF DAMAGE BS 657-667 RBL 27 WL 140 / REMOVED AND REPLACED FAIRING FORMER B.S.757-667 RBL27 WL140 PER IPC 53-42-00-91 SRM 51-40-05-0G-0

Part: SKIN — DENTED (BS 1006) · airframe 75,121 hrs · 44,711 cycles

DENT ON FUSELAGE SKIN BS1006+3.3' .7' BELOW STR 15R / REPAIRED PER EA 20-153-01276 REV IR AND ATS ER 20-02937 REV IR

Part: STIFFENER — CHAFED (BS 663) · airframe 75,121 hrs · 44,711 cycles

STIFFENER HAS CHAFF DAMAGE BS 663 RBL 14 WL 140 / REMOVED AND REPLACED STIFFENER B.S.663 RBL14 WL140 797822-SWA PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AMM 51-21-72-730-804 AND DWG 111A1000

Part: FORMER — CHAFED (FAIRING) · airframe 75,121 hrs · 44,711 cycles

FAIRING FORMER HAS CHAFF DAMAGE BS 657-667 RBL 14 WL 140 / REMOVED AND REPLACED FAIRING FORMER B.S.657-667 RBL14 WL140 P.O# 797802/1 PER SRM 51-40-02-0G-0 SRM 53-40-71-1A-1 SRM 51-40-05-0G-0 DWG PL149A7214 AMM 51-21-72-370-804 AND IPC 53-42-00-91

Part: SKIN — CORRODED (BS 1088) · airframe 75,121 hrs · 44,711 cycles

CORROSION ON FUSELAGE LOWER SKIN BS 1088 RBL 5 TO LBL5 JUST FORWARD WL 210 OF APU DOOR. REMOVED CORROSION IN TWO AREA'S 4'X7' AND 0.50'X7 MAX BLEND OF .005' IN BOTH AREA'S ORIGINAL THICKNESS 0.080'. AS PER EA 20-153-01244 REV IR AND ATS ER. 20-02917 REV IR THE DAMAGE IS ALLOWABLE FOR CONTINUED SERVICE WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.

Part: SUPPORT — CORRODED (BS 400) · airframe 75,121 hrs · 44,711 cycles

CORROSION AT FCB ON FWD BULKHEAD PANEL LOWER SUPPORT BS400 RBL13 WL157. MARKED / REMOVED FCB FWD BULKHEAD PANEL LOWER SUPPORT BS400 RECEIVED NEW BULKHEAD PANEL LOWER SUPPORT LOCATED; DRILLED; COUNTERSUNK BULKHEAD PANEL LOWER SUPPORT INSTALLED FCB FWD BULKHEAD PANEL LOWER SUPPORT BS400 IAW SRM 51-40-02; SRM 51-40-05 SRM 51-40-08 DWG #284A0603 CORROSION ON FCB FWD BULKHEAD PANEL LOWER SUPPORT BS400 WAS FOUND OUT OF LIMITS DUE TO NO SRM ALLOWABLE LIMITS PART REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9(C) 7191U 22JUL20

Part: SUPPORT — CORRODED (BS 500-500C) · airframe 75,121 hrs · 44,711 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS500 - BS500C LBL23 WL157. MARKED / REMOVED FLOOR TO SIDEWALL SUPPORT AT FCB BS400-500D LBL23 RECEIVED NEW SIDEWALL SUPPORT LOCATED; DRILLED; COUNTERSUNK SIDEWALL SUPPORT INSTALLED NEW FCB SIDEWALL SUPPORT BS400-500D LBL23 IAW SRM 51-40-02; SRM 51-40-08; SRM 51-40-05; DWG# 143A7500; DWG# 143A7505 DWG# 143A7902 CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT AT BS400-500D LBL27 WAS FOUND OUT OF LIMITS DUE TO PROXIMITY TO HOLES IAW SRM 53-00-53-1A-2 FIG 103(D) 7191U 20JUL20

Part: SUPPORT — BENT (BS 500D-520) · airframe 75,121 hrs · 44,711 cycles

BENT INTERCOSTAL AT FWD CARGO BAY BS 500D - 520 LBL 6 WL 156. MARKED / REMOVED DAMAGED INTERCOSTAL; BS500D-520; LBL-6; LOCATED; DRILLED; AND INSTALLED; NEW INTERCOSTAL; BS500D-520; LBL-6; IAW SRM 51-40-02-0G-0; DWG 143A7902.

Part: WEB — CORRODED (BS 727A) · airframe 75,121 hrs · 44,711 cycles

CORROSION ON CREASE BEAM WEB BS 727A+2 LBL65 WL 208 / REMOVED AND REPLACED WEB AT BS727A+2 LBL65 WL208 DUE TO CORROSION BEING OUT OF LIMITS PER SRM 53-60-13-1A-1 WEB REPLACEMENT AND REPAIR ACCOMPLISHED PER ATS ER 20-02894 REV IR AND EA 20-153-01212 REV IR SRM 51-40-02 DWG 146A5900.

Part: STRINGER — BENT (BS 520-540) · airframe 75,121 hrs · 44,711 cycles

BENT STRINGER AT FCB SNAKE PIT AREA S-20L BS520 - BS540 WL188. MARKED / REPAIRED PER:EA 20-153-01307 REV IR AND ATS ER 20-02902 REV IR

Part: CARGO TRACK — CORRODED (BS 500) · airframe 75,121 hrs · 44,711 cycles

CORROSION ON RAIL AT FCB BS500+6 LBL9 WL157. CORROSION ON RAIL AT FWD CARGO BAY BS500+6; LBL9; WL157 FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG 103 DETAIL D DUE TO PROXIMITY TO HOLES. ACCOMPLISHED REPAIR TO RAIL AT BS500+6; LBL9; WL157 PER SRM 53-00-53-2R-2; FIG 203/REPAIR 2 ALTERNATIVE 5.

Part: RAIL — CORRODED (BS 500A) · airframe 75,121 hrs · 44,711 cycles

CORROSION ON RAIL AT FCB BS500+6 LBL13 WL157. MARKED / CORROSION ON RAIL AT FWD CARGO BS500+6; LBL13; WL157 FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG 103 DETAIL DUE TO PROXIMITY TO HOLES. ACCOMPLISHED REPAIR TO RAIL AT BS500+6; LBL13; WL157 PER SRM 53-00-53-2R-2 FIG 203/REPAIR 2 ALTERNATIVE 5.

Part: RAIL — CORRODED (BS 500) · airframe 75,121 hrs · 44,711 cycles

CORROSION ON RAIL AT FCB BS 500+6 RBL 3 WL 157. REMOVED AND REPLACED FCB RAIL IAW SRM 53-00-53-2R-2.

Part: SUPPORT — BENT (BS 500D-520) · airframe 75,121 hrs · 44,711 cycles

BENT INTERCOSTAL AT FWD CARGO BAY SNAKE PIT AREA BS500D - BS520 RBL6 WL156. MARKED / REMOVED DAMAGED INTERCOSTAL; RECIEVED FABRICATED INTERCOSTAL LOCATED; DRILLED; APPLIED CHEMICAL CONVERSION COATING; PRIMED AND INSTALLED; ALL IAW SRM 51-40-02-0G-0; SRM 51-20-01-0G-0; AMM 51-21-72-370-804; SRM 51-40-05-0G-0; DWG 143A7902.

Part: SUPPORT — CORRODED (BS 402) · airframe 75,121 hrs · 44,711 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS402 LBL23 WL157. MARKED / CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS402; LBL23; WL157 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG 103 DETAIL D DUE TO PROXIMITY TO HOLES. FLOOR TO SIDEWALL SUPPORT TO BE REPLACED FROM BS400 TO BS500D; LBL23; WL157 ON CARD U188730.

Part: STRAP — CORRODED (FWD CARGO) · airframe 75,121 hrs · 44,711 cycles

***CORROSION*** ON STRAP AT FCB BS440 - BS493 RBL21 WL157. / REMOVED AND REPLACED FCB STRAP B.S. 440-493 RBL21 WL 157 IAW SRM 51-40-02-0G-0 AND DWG 143A0080

Part: SKIN — DENTED (BS 360) · airframe 75,121 hrs · 44,711 cycles

DENT ON FUSELAGE SKIN BS360+14' ABOVE STR 17L REF C029807; V474383; V474384 AND V474416 / REPAIRED AS PER EA 20-153-01105 REV IR AND ATS ER 20-02866 REV IR

Part: WEB — CORRODED (BS 440-493) · airframe 75,121 hrs · 44,711 cycles

***CORROSION*** ON SUBTHRESHOLD WEB AT FCB BS440 - BS493 RBL25 WL157. MARKED / REMOVED AND REPLACED FCB SUB THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG 143A8330

Part: SHIELD — CORRODED (FWD CARGO) · airframe 75,121 hrs · 44,711 cycles

***CORROSION*** ON FWD SHIELD AT FCB BS420 - BS440 RBL23 WL157. / REMOVED AND REPLACED FWD SHIELD ASSY FCB B.S. 420-440 RBL23 WL157 PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND DWG 143A0080

Part: SUPPORT — CORRODED (BS 727D) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN AFT CARGO BAY ON FLOOR PANEL SUPPORT AT B.S. 727D+6; L.B.L. 21-R.B.L. 21; W.L. 154. / CORROSION ON AFT CARGO BAY FLOOR PANEL SUPPORT AT BS727D+6; LBL21-RBL21; WL154 FOUND OUT OF LIMITS DUE TO NO SRM ALLOWABLE LIMITS. REMOVED SUPPORT AND INSTALLED NEW SUPPORT PER SRM 51-40-02-0G-0 AND DWG 146A7500.

Part: STRAP — CORRODED (BS 774-800) · airframe 75,121 hrs · 44,711 cycles

***CORROSION*** IN AFT CARGO BAY ON TENSION STRAP AT B.S. 774-800; R.B.L. 20; W.L. 154. / CORROSION ON ACB TENSION STRAP AT B.S.774-800; RBL20 WL154 FOUND OUT OF LIMITS DUE TO PROXIMITY TO HOLES PER SRM 53-60-15-1A-1 FIG 103 DETAIL D. REMOVED ACB TENSION STRAP AT 774-862; RBL20 WL154 PER SRM 51-40-02-0G-0; INSTALLED NEW TENSION STRAP AT BS774-862; RBL20; WL154 PER SRM 51-40-02-0G-0; DWG 146A8120; DWG 146A0081 93114U 21JUL20

Part: SUPPORT — CORRODED (BS 773) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN AFT CARGO BAY ON FLOOR PANEL SUPPORT AT BS 773; L.B.L. 21-R.B.L. 21; W.L. 154. / CORROSION ON AFT CARGO BAY FLOOR PANEL SUPPORT AT BS773; LBL21-RBL21; WL154 WAS FOUND OUT OF LIMITS DUE TO NO SRM LIMITS. REMOVED SUPPORT AND INSTALLED NEW SUPPORT PER SRM 51-40-02-0G-0 AND DWG 146A7500.

Part: SUPPORT — CORRODED (BS 867-887) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 867-887; R.B.L. 21; W.L. 154. / REMOVED CORROSION DAMAGED FLOOR TO SIDEWALL SUPPORT AT BS867-887 RBL21 WL154 LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AND INSTALLED ALL IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND BOEING DWG 146A7500 13656R 19JUL2020

Part: SUPPORT — CORRODED (BS 727-767) · airframe 75,121 hrs · 44,711 cycles

***CORROSION*** IN AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT B.S. 727-767; R.B.L. 21; W.L. 154. / REMOVED ACB SIDEWALL SUPPORT BS727-767 RBL21 RECEIVED NEW SIDEWALL SUPPORT LOCATED; DRILLED; COUNTERSUNK SIDEWALL SUPPORT INSTALLED NEW ACB SIDEWALL SUPPORT BS727-762 RBL21 IAW SRM 51-40-02; SRM 51-40-08; SRM 51-40-05; DWG# 146A0061; DWG# 146A7500 7191U 15JUL20 CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS727-767; RBL21; WL154 WAS FOUND OUT OF LIMITS DUE TO PROXIMITY TO HOLES PER SRM 53-00-53-1A-2 FIG 103; DETAIL D.

Part: STRAP — CORRODED (BS 775) · airframe 75,121 hrs · 44,711 cycles

***CORROSION*** IN AFT CARGO BAY ON TENSION STRAP SUPPORT AT B.S. 775; R.B.L. 20; W.L. 154. / CORROSION ON ACB TENSION STRAP SUPPORT AT BS775; RBL20; WL154 FOUND OUT OF LIMITS DUE TO PROXIMITY TO HOLE PER SRM 53-60-15-1A-1 FIG 103; DETAIL D. REMOVED ACB TENSION STRAP SUPPORT AT BS767-787; RBL20; WL154 PER SRM 51-40-02-0G-0; INSTALLED ACB NEW SUPPORT AT BS767-787; RBL20; WL154 PER SRM 51-40-02-0G-0; DWG 146A0081 93114U 20JUL20

Part: SKIN — DENTED (BS 360) · airframe 75,121 hrs · 44,711 cycles

DENT ON FUSELAGE SKIN BS360+12' 3' BELOW STR 5L / REPAIRED PER EA 20-153-01291 REV IR AND ATS ER 20-02933 REV IR

Part: SHIELD — CORRODED (AFT CARGO) · airframe 75,121 hrs · 44,711 cycles

***CORROSION*** IN AFT CARGO BAY ON SHIELD AT B.S. 767-794; R.B.L. 21; W.L. 154. / CORROSION ON ACB SHIELD AT BS767-794; RBL21; WL154 FOUND OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM PART REPLACEMENT PER SRM 51-10-02-0G-0; 9.C. REMOVED ACB SHIELD AT BS767-794; RBL21; WL154 PER SRM 51-40-02-0G-0; INSTALLED NEW SHIELD AT BS767-794; RBL21; WL154 PER SRM 51-40-02-0G-0; DWG 146A0081 93114U 20JUL20

Part: SUPPORT — CORRODED (BS 727-847) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT B.S. 727-847; L.B.L. 21; W.L. 154. / REMOVED ACB SIDEWALL SUPPORT BS727-847 LBL21 RECEIVED NEW SIDEWALL SUPPORT LOCATED; DRILLED; COUNTERSUNK SIDEWALL SUPPORT INSTALLED NEW ACB SIDEWALL SUPPORT BS727-847 LBL21 CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS727-847 LBL21 WL154 WAS FOUND OUT OF LIMITS DUE TO PROXIMITY TO HOLES IAW SRM 53-00-53-1A-2; SRM 51-40-02; SRM 51-40-08; SRM 51-40-05 DWG# 146A7500 7191U 20JUL20

Part: FLOORBEAM — CRACKED (BS 540) · airframe 75,121 hrs · 44,711 cycles

CRACKED FLOOR PANEL SUPPORT AT B.S. 540; B.L. 0 - L.B.L. 24.5; W.L. 208.1. / REPLACED CRACKED FLOOR SUPPORT AT BS540 BL0-LBL24.5 WL208.1 PER SRM 51-40-02-0G-0 AND AIPC 53-31-00-05. 57449U 8JUL20

Part: GUSSET — CORRODED (AFT CARGO) · airframe 75,121 hrs · 44,711 cycles

***CORROSION*** IN AFT CARGO BAY ON SHIELD TO FRAME GUSSET AT B.S. 768; R.B.L. 23; W.L. 154. / CORROSION ON ACB SHIELD TO FRAME GUSSET AT BS768; RBL23; WL154 FOUND OUT LIMITS DUE TO NO SRM LIMITS PART REPLACEMENT PER SRM 51-10-02-0G-0 9.C. REMOVED ACB SHIELD TO FRAME GUSSET AT BS768; RBL23; WL154 PER SRM 51-40-02-0G-0; INSTALLED NEW ACB SHIELD TO FRAME GUSSET AT B.S768; RBL23; WL154 PER SRM 51-40-02-0G-0; DWG 146A0081 93114U 20JUL20

Part: SUPPORT — CORRODED (BS 887-947) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 887-947; R.B.L. 21; W.L. 154. / REMOVED CORROSION DAMAGED FLOOR TO SIDEWALL SUPPORT AT BS887-947 RBL21 WL154 ACB LOCATED DRILLED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT ALL IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 BOEING DWG 147A7500 AND 147A9409 13656R 19JUL2020

Part: WEB — CORRODED (BS 794-847) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN AFT CARGO BAY THRESHOLD SUBWEB A AT B.S. 794-847; R.B.L. 24; W.L. 154. / CORROSION ON ACB THRESHOLD WEB AT BS794-847; RBL24; WL154 FOUND OUT OF LIMITS DUE TO PROXIMITY TO HOLES PER SRM 53-60-15-1A-1 FIG 103 DETAIL D. REMOVED ACB THRESHOLD WEB BS794-847; WL154 PER SRM 51-40-02-0G-0 INSTALL NEW THRESHOLD WEB; RBL20; WL154 BS794-847 PER SRM 51-40-02-0G-0; DWG 146A8340 93114U 24JUL20

Part: FLOOR SUPPORT — CORRODED (BS 847-867) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN AFT CARGO BAY INTERCOSTAL AT B.S. 847-867; R.B.L. 6; W.L. 152. / DAMAGE EVALUATION ON ACB INTERCOSTAL BS847-867; RBL6; WL152. WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO HOLE. PER SRM 53-60-15. REMOVED AND INSTALLED NEW INTERCOSTAL PER DWG 146A8130; SRM 51-40-02 87713U 23JUL20

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEATTRACK BS 390; BS352; RBL 45 WL 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEATTRACK BS 476 LBL25 WL 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEATTRACK BS 750; BS876; LBL 45 WL 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEATTRACK BS 415; BS447; RBL25 WL 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEAT TRACK BS 727B+13;BS 870; LBL25 WL 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEAT TRACK BS 540-727B LBL45 WL 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEAT TRACK BS 610; BS647; BS670; BS980; BS698; BS712 RBL 45 WL 208.

Part: BULKHEAD — CRACKED (BS 663) · airframe 75,121 hrs · 44,711 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT R.B.L. 54; W.L. 150 IN RIGHT HAND WHEEL WELL. / REMOVED AND REPLACED R/H 663 VAPOR BARRIER PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AMM 53-51-21-400-802 AMM 51-31-00-390-805 DWG 111A1000 DWG 111A1001 DWG 111A1151 DWG 11A7000 DWG 144A7100

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEAT TRACK BS 727C+5; BS727E; BS760; BS790; BS824; BS855 RBL45 WL 208.

Part: SKIN — CORRODED (BS 947-1006) · airframe 75,121 hrs · 44,711 cycles

MULTIPLE AREAS OF CORROSION FOUND ON CROWN SKIN; BS 947-1006; STR-2L TO STR-2R (UNDER DORSAL FIN) / REPAIRED CORROSION DAMAGE ON CROWN SKIN; BS947-1006 STR 2L TO 2R (UNDER DORSAL FIN) PER ER 20-02856 REV IR AND EA 20-153-01127 REV IR

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEATTRACK BS 500B+8; BS 500D; RBL 45 WL 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEATTRACK BS 727E+7; BS727D+18; BS787; BS820; BS855; BS884; RBL25 WL 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEAT TRACK BS 404; BS 430; BS 465 LBL45 WL 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEAT TRACK BS 657 LBL25 WL 208.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,121 hrs · 44,711 cycles

CORROSION IN WELL OF SEATTRACK BS 495; BS500A+7; BS500C LBL25 WL 208.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 75,121 hrs · 44,711 cycles

FLOOR SUPPORT CRACKED BS 344-360-BL 0 WL 208 / REPLACED CRACKED FLOOR SUPPORT AT BS344-360 BL0 WL208 PER SRM 51-40-02-0G-0 AND DWG# 141A5400. 57449U 7JUL20

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 75,036 hrs · 44,658 cycles

FWD GALLEY FLASH LIGHT INOP REMOVED AND REPLACED FLASHLIGHT BATTERY PER M/M 25-64-00

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 73,750 hrs · 43,853 cycles

L2 DOOR SLIDE MANUAL INFLATION HANDLE COVER MISSING. / REPOSITIONED SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,481 hrs · 43,679 cycles

RT AFT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,481 hrs · 43,679 cycles

RT OVERWING EMERGENCY EXIT LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,481 hrs · 43,679 cycles

LT FORWARD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER MM.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 72,970 hrs · 43,329 cycles

PANEL # 192BL HAS EROSSION AND DELAMANTION AT FWD LEADING EDGE / REMOVED & INSTALLED NEW PANEL # 192BL IN REF TO SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,865 hrs · 43,264 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 72,534 hrs · 43,041 cycles

R/H OVERWING EXIT SIDEWALL LIGHT INOPERATIVE. R&R EXIT LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,242 hrs · 42,861 cycles

LT EMERGENCY LIGHT AT STOW BIN INOP AT ROW 1. R&R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,242 hrs · 42,861 cycles

RT EMERGENCY LIGHT AT STOW BIN INOP AT ROW 3. R&R LIGHT IAW AMM.

Part: SKIN — BUCKLED (FUSELAGE) · airframe 72,242 hrs · 42,861 cycles

FUSELAGE SKIN BUCKLED BETWEEN BS. 500B TO BS. 500C, STR. 4R. REPAIRED SKIN IAW SRM AND EA.

Part: SKIN — BUCKLED (FUSELAGE) · airframe 72,242 hrs · 42,861 cycles

FUSELAGE UPPER SKIN BUCKLED BETWEEN BS. 500B TO BS. 500C, BETWEEN STR. 3R TO STR. 4R. REPAIRED SKIN PER EA.

Part: SKIN — BUCKLED (FUSELAGE) · airframe 72,242 hrs · 42,861 cycles

FUSELAGE LOWER SKIN BUCKLED BETWEEN BS. 500B TO BS. 500C, BETWEEN STR. 4R TO STR. 5R. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 71,721 hrs · 42,533 cycles

R2 EVAC SLIDE GIRT BAR STRAP MANUAL INFLATE HANDLE COVER OUT OF POSITION. REPOSITIONED SLIDE PACKS PER SIP.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 71,721 hrs · 42,533 cycles

L2 EVAC SLIDE GIRT BAR STRAP MANUAL INFLATE HANDLE COVER OUT OF POSITION. REPOSITIONED SLIDE PACKS PER SIP.

Part: LENS — MISSING (L2 DOOR) · airframe 71,013 hrs · 42,089 cycles

L2 DOOR EXIT LENS MISSING DIRECTIONAL ARROWS. INSTALLED LENS PER AMM.

Part: LENS — MISSING (R2 DOOR) · airframe 71,013 hrs · 42,089 cycles

R2 DOOR EXIT LENS MISSING DIRECTIONAL ARROWS. INSTALLED LENS PER AMM.

Part: LENS — UNSECURE (CABIN) · airframe 70,720 hrs · 41,901 cycles

CENTER AISLE EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED LENS PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,992 hrs · 41,449 cycles

RT OVERWING EMERGENCY LIGHT AT AFT FLAP INOP. R&R LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,992 hrs · 41,449 cycles

LT SIDE EMERGENCY LIGHTING FAULTY BETWEEN AT BS 952 TO BS 727C. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 69,992 hrs · 41,449 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY TEST AT LOCATION M1672, BS 952, WL 290. R&R BATTERY PACK IAW AMM.

Part: WIRE — DAMAGED (COCKPIT) · airframe 69,992 hrs · 41,449 cycles

FLIGHT DECK EMERGENCY FLOOD LIGHT INOP. TERMINATED WIRE TO GROUND BLOCK IAW WDM & AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,992 hrs · 41,449 cycles

LT EMERGENCY AISLE LIGHT INOP AT ROW 20. R&R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,992 hrs · 41,449 cycles

FLIGHT COMPARTMENT EMERGENCY DOME LIGHT INOP. R&R LIGHT IAW AMM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 69,992 hrs · 41,449 cycles

L2 DOOR EMERGENCY EXIT LIGHT ABOVE THE DOOR FAILED OPERATIONS CHECK. CONNECTED WIRE IAW WDM AND AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 69,992 hrs · 41,449 cycles

FORWARD SECTION EMERGENCY LIGHTS FAILED OPS CHECK. R&R BATTERY PACK IAW AMM.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 69,992 hrs · 41,449 cycles

AFT PIT FLOOR PANEL 140CF UPPER AND LOWER SURFACES HAVE WIDESPREAD CORROSION REMAINING PRIMARILY ALONG SIDES AFTER INITIAL REWORK ON NRC X756433. / EVALUATED AFT CARGO PIT FLOOR PANEL 140CF UPPER AND LOWER SURFACE FOUND CORROSION EXCEED A MAXIMUM OF 3' OUT OF LIMITS IAW SRM 53-00-53-1A-1 FLOOR PANEL REMOVED AND REPLACED ON N/R X757716

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

E&E BAY CEILING CABIN FLOORBEAM INTERCOSTAL UPPER CHORD CRACKED AT BS 390, RBL 43. R&R INTERCOSTAL IAW EA & DWG.

Part: BRACKET — CRACKED (E & E COMPT) · airframe 69,992 hrs · 41,449 cycles

E&E COMPARTMENT FLOOR SUPPORT BRACKET AT STA 351 LBL 15 IS CRACKED / REMVOED AND REPLACED FLOOR SUPPORT AT STA 351 LBL15 WITH FABRICATED BRACKET IAW EA 1-753-32951 REV IR AND EA 180364 IR; BRACKET INSTALLED IAW SRM 51-40-02 AND DWG 284A 0839

Part: BRACKET — ELONGATED (E & E COMPT) · airframe 69,992 hrs · 41,449 cycles

E&E COMPARTMENT FLOOR SUPPORT BRACKET AT STA 351 TO 370 LBL 19 HAS ELONGATED HOLES / REMOVED AND REPLACED FLOOR SUPPORT BRACKET ('T') AT STA 351-370 LBL19 WITH FABRICATED BRACKET IAW EA 1-753-32951 REV IR AND EA 180364 IR; SUPPORT BRACKET INSTALLED IAW SRM 51-40-02 AND DWG 284A0839

Part: BRACKET — ELONGATED (E & E COMPT) · airframe 69,992 hrs · 41,449 cycles

E&E COMPARTMENT FLOOR SUPPORT BRACKET AT STA 370 RBL 1 TO LBL19 HAS ELONGATED HOLES / REMOVED DAMAGED FLOOR SUPPORT BRACKET AT STA 370 RBL1 TO LBL19 IN E & E COMPARTMENT; FABRICATED AND INSTALLED NEW P/N 284A3839-19 CHANNEL BRACKET IAW AAR EA 180344 IR AND SWA EA 1-753-32906 REV IR

Part: BAFFLE — CRACKED (FWD CARGO LH) · airframe 69,992 hrs · 41,449 cycles

FWD CARGO BAY BAFFLE IS CRACKED AT STA 460 TO 480 L/H / REPLACED NEW BAFFLE AT FWD CARGO STA 460-480 L/H SIDE I.A.W. B737-700 SRM 51-40-02-0G & BOEING 143A7505 AREV: AY: DWG; ID: 0004.

Part: BAFFLE — CRACKED (FWD CARGO LH) · airframe 69,992 hrs · 41,449 cycles

FWD CARGO BAY BAFFLE FOUND CRACKED AT STA 440 TO 460 L/H / REMOVED AND REPLACED BAFFLE PN 143A7510-9 AT CARGO LH STA 440 TO 460 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV A ATAG WN9485

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT FLOOR STRUCTURE BAFFLE CLIP CRACKED AT BS 500C, RBL 24. R&R CLIP IAW DWG & SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

CORROSION ON INTERNAL DOUBLER STA 360 +3' AT STR 28L / BLENDED CORROSION AT STA 360 + 3' STR 28R INTERNAL DOUBLER; ORIGINAL THICKNESS .050'; REMAINING .044'; LOSS OF .006' FOUND OUT OF LIMITS IAW SRM 53-00-01-1A-5. REMOVED CORRODED DOUBLER AND LOCATED; DRILLED AND INSTALLED NEW DOUBLER IAW SRM 51-40-02-0G-0 AND DWG 143A3230 REV. B APPLIED CIC TO NEW DOUBLER IAW AMM 51-21-91-620-802

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FUSELAGE SKIN CORRODED AT BS 400+3, STR 25L. REPAIRED SKIN IAW EA.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

EXHAUST DUCT INTERNAL DOUBLER CORRODED AT BS 360+ 6, BETWEEN STR 28L TO STR 28R. R&R DOUBLER IAW DWG.

Part: SHEAR TIE — CORRODED (E&E BAY) · airframe 69,992 hrs · 41,449 cycles

SHEAR TIE AT STA 380 STR 25L- 26L IS CORRODED / SHEAR TIE AT STA 380 STR 25L-26L WAS CORRODED 100% THROUGH MATERIAL; FABRICATED NEW SHEAR TIE IAW EA 180333 IR AND EA 1-753-32874 REV IR; SHEAR TIE REMOVED AND INSTALLED ON N/R X757536 SA-M 326 E2333986 ITEM 5

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FUSELAGE SKIN CORRODED AT BS 360+2, STR 25L. REPAIRED SKIN IAW EA.

Part: INTERCOSTAL — CORRODED (E&E BAY) · airframe 69,992 hrs · 41,449 cycles

INTERCOSTAL STA 351-360 STR 28L IS CORRODED THROUGH / REMOVED CORRODED THROUGH INTERCOSTAL ST STA 351-360 STR 28L AND REPLACED WITH NEW FABRICATED INTERCOSTAL IAW BOEING DWG 141A8512 INTERCOSTAL INSTALLED ON N/R X757538 SA-M 326 E233987 ITEM 2.

Part: LENS — CRACKED (CABIN) · airframe 69,992 hrs · 41,449 cycles

AFT LAV EMERGENCY EXIT LIGHT LENS CRACKED. R&R LENS IAW AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FUSELAGE SKIN CORRODED AT BS 360+10, STR 23L. REPAIRED SKIN IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

LOWER ATC ANTENNA SUPPORT CORRODED AT BS 360, BL 0. R&R SUPPORT IAW SRM AND DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 69,992 hrs · 41,449 cycles

PASSENGER CABIN SIDEWALL EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R&R LIGHT IAW AMM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE IAW EA.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

SUPPORT BRACKET AT STA 380 STR 24L ON ASSY 284A3837-2 IS CORRODED / REMOVED 'OUT OF LIMITS' -34 BRACKET AND INSTALLED NEW BRACKET ON T -2 ASSY AS REQ D REF:B737 SRM 51-40-02-0G-0 STEP 4B AND BAC DWG 143A9173 REV. - MATERIAL TAG A22465.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FRAME CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

STRINGER CORRODED BETWEEN BS 344+7 TO BS 380, STR 27L. REPAIRED STRINGER IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

STRINGER CLIP CORRODED AT BS 380 STR 24L. R&R STRINGER CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

SHEAR TIE CORRODED AT BS 380, BETWEEN STR 23L TO STR 24L. R&R SHEAR TIE PER SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

STRINGER CORRODED BETWEEN BS 360+9 TO BS 360+12, STR 28R. REPAIRED STRINGER IAW EA.

Part: ATTACH BRACKET — CRACKED (E&E BAY) · airframe 69,992 hrs · 41,449 cycles

E&E COMPARTMENT ATTACH BRACKET AT STA 360 IS CRACKED AT 24L / REMOVED CRACKED -9 BRACKET AND INSTALLED NEW -9 BRACKET ONTO -2 ASSY AS REQ D. REF:B737 SRM 51-40-02-0G-0 STEP 4B AND BAC DWG 284A0837 REV. A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FUSELAGE SKIN CORRODED AT BS 360+2, STR 26L. REPAIRED SKIN IAW SRM AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

ELECTRONICS AND EQUIPMENT COMPARTMENT STRINGER CORRODED AT BS 380, STR 23L. R&R STRINGER IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

E&E COMPARTMENT STRINGER SPLICE CORRODED AT BS 360+10, STR 25L. R&R SPLICE IAW EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FUSELAGE STRINGER SPLICE CORRODED AT STA 370, STR 26L. REPAIRED SPLICE PER SWA EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FUSELAGE STRINGER SPLICE CORRODED AT STA 370, STR 24L. REPAIRED SPLICE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

E&E COMPARTMENT STRINGER SPLICE CORRODED AT BS 360+10, STR 28L. REPAIRED SPLICE IAW EA & DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

LT HORSE SHOE DOUBLER CRACKED AT BS 663 FASTENER HOLE. R&R WEB IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, STR 25R. R&R INTERCOSTAL IAW DWG & SRM.

Part: GIRT BAR — DAMAGED (L1 DOOR) · airframe 69,992 hrs · 41,449 cycles

L1 DOOR GIRT BAR ATTACHMENT HARDWARE DAMAGED. R&R GIRT BAR ASSEMBLY IAW AMM.

Part: FASTENER — STRIPPED (R2 DOOR) · airframe 69,992 hrs · 41,449 cycles

R2 DOOR BOTH LOWER GIRT BAR ADAPTER MOUNT STRIPPED. R&R HARDWARE IAW AMM.

Part: FASTENER — STRIPPED (R2 DOOR) · airframe 69,992 hrs · 41,449 cycles

R2 DOOR GIRT BAR ATTACHING HARDWARE STRIPPED. R&R HARDWARE ASSEMBLY IAW AMM.

Part: FASTENER — STRIPPED (L2 DOOR) · airframe 69,992 hrs · 41,449 cycles

L2 DOOR GIRT BAR ATTACHMENT HARDWARE STRIPPED. R&R HARDWARE IAW AMM.

Part: VAPOR BARRIER — CRACKED (LWR FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

STA 663 LOWER VAPOR BARRIER WEB U DOUBLER FOR PACK EXHAUST IS CRACKED / REMOVED CRACKED DOUBLER AND INSTALED NEW DOUBLER AS PER B737 SRM 51-40-02-0G-0 AND BAC DWG 111A1515 REV -

Part: FASTENER — STRIPPED (L2 DOOR) · airframe 69,992 hrs · 41,449 cycles

L2 DOOR LOWER GIRT BAR ADAPTER MOUNT ATTACHMENT FITTING STRIPPED. R&R HARDWARE IAW AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 69,992 hrs · 41,449 cycles

FWD CARGO PIT AFT CORNER SCUFF PLATE CRACKED / FWD CARGO PIT AFT CORNER SCUFF PLATE WELDED ON SOUTHWEST EA # 1-A53-2076 REV 11

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

PRESSURE WEB CRACKED AT BS 663.5, STR 48L. R&R WEB IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,992 hrs · 41,449 cycles

RT HORIZONTAL STAB FWD SPAR RIB CRACKED AT STA 129.5. REPAIRED RIB PER SWA EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,992 hrs · 41,449 cycles

RT HORIZONTAL STAB FWD SPAR RIB STIFFENER CRACKED AT STA 101.9. REPAIRED RIB STIFFENER PER SWA EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,992 hrs · 41,449 cycles

RT HORIZONTAL STAB FWD SPAR RIB STIFFENER CRACKED AT STA 129.5. REPAIRED RIB STIFFENER PER EA.

Part: BEAM — ELONGATED (FSD) · airframe 69,992 hrs · 41,449 cycles

SUPPLEMENTAL INFORMATION: R1 DOOR UPPER BEAM HAS MULTIPLE FASTNER HOLES ELONGATED HOLES. / REMOVED AND INSTALLED NEW R-1 DOOR UPPER BEAM I/A/W SRM 51-40-02-0G-0 AND BOEING DWG # 141A6535 REC:C REPAIRED IAW AAR EA 180346 IR AND SWA EA 1-752-2282 REV IR

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT CENTER TANK VERTICAL STIFFENER CRACKED AT BS 540, RBL 25. R&R STIFFENER IAW DWG AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

INTERCOSTAL CORRODED BETWEEN BS 907 TO BS 927, BETWEEN STR 23L TO STR 24L. R&R INTERCOSTAL IAW DWG & SRM.

Part: DOUBLER — CORRODED (LOWER EXT FUSELA) · airframe 69,992 hrs · 41,449 cycles

SUPPLEMENTAL INFORMATION: WING TO BODY FAIRING PANEL 191CR; TOP DOUBLER FOR DRAIN MAST IS CORRODED. / EVALUATED DAMAGE TO PNL191CR TOP DOUBLER DRAIN MAST. FOUND NO SRM LIMITS. PART OUT OF LIMITS. REMOVED & REPLACED DRAIN MAST DOUBLER IAW EA180297 REV P1 & IR & SWA EA 1-753-32811

Part: BEAM — ELONGATED (FSD) · airframe 69,992 hrs · 41,449 cycles

SUPPLEMENTAL INFORMATION: R1 DOOR #5 BEAM ABOVE HANDLE BOX ASSY; FWD MOUNT HOLES ARE ELONGATED FROM FASTENER MOVEMENT / REAMED UP HOLES TO FIRST OVER SIZE .266 'NO FURTHER DAMAGE NOTED' AT R-1 DOOR #5 BEAM ABOVE HANDLE BOX ASSY. FWD MOUNT HOLES I/A/W SRM 51-40-05-0G-0 AND BOEING DWG #65C36625 REV -

Part: BEAM — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

R1 DOOR BEAM CRACKED. R&R BEAM IAW SRM AND DWG.

Part: FLOOR PANEL — CORRODED (FLIGHT DECK FLOO) · airframe 69,992 hrs · 41,449 cycles

SUPPLEMENTAL INFORMATION: FLIGHT COMPARTMENT FLOOR PANEL HAS CORROSION ON LOWER SURFACE. / BLENDED AND REMOVED CORROSION ON FLIGHT DECK FLOOR PANEL LOWER SURFACE. ORG 'T' .040' REMOVAL .008' MATERIAL WITH .032' REMAINING OUT OF LIMITS IAW SRM 53-10-51-18. LOCATED AND DRILLED NEW PANEL IAW SRM 51-40-05 APPLIED TOP COAT IAW MM 51-21-73. PANEL INSTALLED ON JPANEL-211-CLOSE ATAG A69910

Part: FLOOR PANEL — FRAYED (CABIN) · airframe 69,992 hrs · 41,449 cycles

SUPPLEMENTAL INFORMATION: MAIN CABIN FLOOR BOARD 232 RF UPPER SUFACE FIBER FRAYED. / REPAIRED MAIN CABIN FLOORBOARD #232 RF UPPER SURFACE IAW B737 SRM 53-00-50-50-2R-1STEP 3 K THROUGH O

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,992 hrs · 41,449 cycles

R1 DOOR CRACKED INNER BEAM BELOW DOOR HANDLE BOX AT LOWER FORWARD. R&R INNER BEAM IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 69,992 hrs · 41,449 cycles

SUPPLEMENTAL INFORMATION: MAIN CABIN FLOOR BOARD 231 XF UPPER SUFACE FIBER FRAYED. / REPAIR MAIN CABIN FLOOR BOARD #231 XF IAW B737 SRM 53-00-50-2R-1 PAR. 3 STEPS K THROUGH O

Part: ISOLATOR — CRACKED (R1 DOOR) · airframe 69,992 hrs · 41,449 cycles

R1 DOOR LOWER AFT SLIDE MOUNT CRACKED ISOLATOR. R&R ISOLATOR IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 69,992 hrs · 41,449 cycles

MAIN CABIN FLOOR BOARD 231 ZF UPPER SUFACE FIBER FRAYED. / REPAIRED MAIN CABIN FLOOR BOARD # 231ZF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 STEP 3 K THROUGH O

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 69,992 hrs · 41,449 cycles

SUPPLEMENTAL INFORMATION: MAIN CABIN FLOOR BOARD 241 AF UPPER SUFACE FIBER FRAYED. / FABRICATED NEW FLOORBOARD 241AF AS REQUIRED IAW B737 SRM 53-00-50-2R-2; PAR (1A) REV 64; AND BAC5085 PER DWG #144A5810; REV B. REMOVED AND INSTALLED PASS CABIN FLOOR BOARD PANEL 241AF IAW AMM 53-21-00-000-801 STEP 2A;2;3;4;A AND AMM 53-21-00-400-801 STEP 3A;F;6;3-7

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 69,992 hrs · 41,449 cycles

SUPPLEMENTAL INFORMATION: MAIN CABIN FLOOR BOARD 241 DF UPPER SUFACE FIBER FRAYED. / FABRICATED NEW FLOORBOARD 241DF AS REQUIRED IAW B737 SRM 53-00-50-2R-2; PAR (1A) REV 64; AND BAC5085 PER DWG #144A5810; REV B. REMOVED AND INSTALLED PASS CABIN FLOOR BOARD PANEL 241DF IAW AMM 53-21-00-000-801 STEP 2A;2;3;4;A AND AMM 53-21-00-400-801 STEP 3A;F;B;3-7 A52923

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,992 hrs · 41,449 cycles

RT HORIZONTAL STAB FWD SPAR RIB CRACKED AT STA 101.9. REPAIRED RIB PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 69,992 hrs · 41,449 cycles

G4 GALLEY EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R&R LIGHT IAW AMM.

Part: PANEL — DELAMINATED (HORIZONTAL STAB) · airframe 69,992 hrs · 41,449 cycles

RH HORIZ STAB UPPER TE SURFACE; FROM ELEVATOR COUNTERWEIGHT CUTOUT TO LOGO LT; FILLET STRIP PANEL FRAYED AND DELAMINATED. / REPLACED 2 EA R/H HORIZ STAB UPPER TE FILLET STRIP PNL IAW B 737 SRM 51-40-02-0G-0 STEP 10 D 3 A70340 A70327

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,992 hrs · 41,449 cycles

LH HORIZONTAL STABILIZER LEADING EDGE PANEL; LE STA 151.75 (9TH RIB FROM INBOARD EDGE) RIB CRACKED AT LOWER AFT FASTENER HOLE; MARKED. / REPLACED NEW RIB ON L/H HORIZONTAL STAB LE ACCESS PANEL ( #9 FROM INBD SIDE) I.A.W B737-700 SRM 51-40-02-0G.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,992 hrs · 41,449 cycles

RT HORIZONTAL STAB FWD SPAR RIB CRACKED AT STA 129.5. REPAIRED RIB PER SWA EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,992 hrs · 41,449 cycles

LH HORIZONTAL STABILIZER LEADING EDGE PANEL; LE STA 86.66 (2ND RIB FROM INBOARD EDGE) RIB INNER CHORD ANGLE CRACKED AT UPPER AFT FASTENER HOLE; MARKED. / REPLACED NEW RIB ON L/H HORIZONTAL STAB LE ACCESS PANEL ( #2 FROM INBD SIDE ) I.A.W B737-700 SRM 51-40-02-0G.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

R1 DOOR CUTOUT FORWARD UPPER CORNER STUB FRAME CRACKED. R&R STUB FRAME IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,992 hrs · 41,449 cycles

LH HORIZONTAL STABILIZER LEADING EDGE PANEL; LE STA 95.96 (3RD RIB FROM INBOARD EDGE) RIB INNER CHORD ANGLE CRACKED AT UPPER AFT FASTENER HOLE; MARKED. / REPLACED NEW RIB ON L/H HORIZONTAL STAB LE ACCESS PANEL (#3 FROM INBOARD SIDE) I.A.W B737-700 SRM 51-40-02-0G.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,992 hrs · 41,449 cycles

LH HORIZONTAL STABILIZER LEADING EDGE PANEL; LE STA 105.26 (4TH RIB FROM INBOARD EDGE) RIB INNER CHORD ANGLE CRACKED AT UPPER AFT FASTENER HOLE; MARKED. / REPLACED NEW RIB ON L/H HORIZONTAL STAB LE PANEL (#4 FROM INBOARD SIDE) I.A.W SRM B737-700 51-40-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL CORRODED AT BS 767+5, RBL 3. R&R ANGLE IAW SRM AND EA.

Part: TRACK — CORRODED (AFT CARGO COMPT) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT STA 767 + 5 LBL 17; FLOOR LONGITUDINAL CORROSION AND NUTPLATES CORRODED. / REMOVED AND REPLACED AFT CARGO PIT FLOOR TRACK ASSY FROM STA 727 TO STA 867 LBL17 I/A/W BOEING DWG 146A7500 REV-; 737-700 SRM 51-40-02-0G-0; 737-700 SRM 51-40-05-0G-0 APPLIED C.I.C TO NEW SEAT TRACK I/A/W 737 AMM 51-21-91-620-802

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO COMPARTMENT AT STA 947; RBL 10; FLOOR SUPPORT L-ANGLE IS CORRODED / EVALUATED FLOOR SUPPORT AT BS 947 RBL 10 FOR CORROSION NO ALLOWABLE SRM LIMITS FOUND REMOVED AND REPLACED CORRODED L-ANGLE FLOOR SUPPORT IAW BOEING DWG 149A8117 REV- AND SRM 51-40-02-0G-0

Part: WEB — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL WEB UPPER AND LOWER SURFACE CORRODED BETWEEN BS 767 TO BS 787, RBL 21. R&R WEB IAW SRM & DWG.

Part: SPAR — CORRODED (LEFT WING) · airframe 69,992 hrs · 41,449 cycles

LH WING TRAILING EDGE; AFT SPAR HAS INTERGRAULAR CORROSION AT AFT BOOST PUMP LOWER BONDING WIRE ATTACH POINT IRSS 142 - 150; MARKED. / REMOVED CORROSION AT L/H WING T/E SPAR AT AFT BOOST PUMP LOWER BONDING WIRE ATTACH POINT IRSS 142-150 I/A/W 737-700 SRM 51-10-02-0G-0 ORIGINAL THICKNESS .678 MATERIAL REMOVED .137 REMAINING .541 OUT OF LIMITS REPAIRED DAMAGE I/A/W SOUTHWEST EA. 1-757-15214 REV IR AND AAR EA.180290 REV IR. RESTORED FINISH AND REPLACED BONDING JUMPER I/A/W EA 180290 P1 STEP 16 AND EA 180290 IR STEP 12

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL LOWER SURFACE CORRODED AT BS 727D+5, RBL 8. REPAIRED CHANNEL IAW SRM AND EA.

Part: SPAR — CORRODED (RIGHT WING) · airframe 69,992 hrs · 41,449 cycles

RH WING TRAILING EDGE; AFT SPAR HAS CORROSION AT AFT BOOST PUMP LOWER BONDING WIRE ATTACH POINT IRSS 142 - 146; MARKED. / REMOVED CORROSION ON R/H REAR SPAR AT LOWER BOOST PUMP BONDING WIRE ATTACH POINT IRSS 142-146. VERIFIED MATERIAL LOSS. ORIGINAL MATERIAL IS .680 REMAINING .0575; LOSS OF .105; OUT OF LIMITS IAW SRM 57-20-10-1A-3. REPAIRED IAW AAR EA 180287 IR AND SWA EA 1-757-15213 REV IR

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO COMPARTMENT AT STA 887; FLOOR PANEL SPLICE IS CORRODED. / AFT CARGO COMPARTMENT AT STA 887; REMOVED AND REPLACED FLOOR PANEL SPLICE (TEE) P/N 146A9401V39 SI 7530863 A TAG WN 6232; IAW: BOEING DWG. 146A7500 AND B737 SRM. 51-40-0 0G 0 APPLIED CORROSION INHIBITING COMPOUND; IAW AMM. 51-21-91-620-802.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 69,992 hrs · 41,449 cycles

RH WING TRAILING EDGE; 17' AFT OF REAR SPAR STA ORSS 273; SEAL RETAINER ATTACH BRACKETCRACKED; MARKED. / REMOVED CRACKED SEAL RETAINER ATTACH BRACKET AND INSTALLED NEW ATTACH BRACKET RH WING STA ORSS273 IAW SRM 57-40-02-0G-0 AND DWG #115A2930 REV-. ATAG#60789

Part: CARGO TRACK — CORRODED (CARGO TRACK) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL CORRODED AT BS 767+5, RBL 14. R&R CARGO TRACK IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE FITTING CRACKED BS 947, LBL 11. R&R FITTING IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL CORRODED AT BS 767+5, RBL 8. R&R ANGLE IAW SRM & EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 69,992 hrs · 41,449 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL NUTPLATE CORRODED AT BS 727D+5, LBL 8. R&R CHANNEL PER EA & SRM.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO COMPARTMENT AT L/H STA. 865; LBL 10; FLOOR SUPPORT STRUCTURE L-ANGLE HAVE CORROSION. / REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT AFT CARGO COMPARTMENT AT L/H STA 847 TO STA 867 LBL 10 I/A/W BOEING DWG 149A8102 REV.B; 737-700 SRM 51-40-02-0G-0; AND 737 AMM 51-21-91-620-802. CORROSION WAS REMOVED ORIGINAL THICKNESS .090 REMOVED .025 REMAINING .065 OUT OF LIMITS I/A/W 737-700 SRM 53-00-53-1A-2 FIG 103

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL CORRODED AT BS 767+5, LBL 3. R&R ANGLE IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL NUTPLATE CORRODED AT BS 727D+5, LBL 12.5. R&R CHANNEL IAW SRM & EA.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT STA 767 + 5 LBL 8; FLOOR LONGITUDINAL CORROSION AND NUTPLATES CORRODED. / REMOVED EXISTING CORRODED REPAIR ANGLE AND INSTALLED NEW LONGITUDINAL ANGLE W/ NUTPLATES I/A/W SWA EA# 1-A53-4982 REV. 3

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL CORRODED AT BS 767+5, LBL 12. REPAIRED ANGLE IAW EA.

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO COMPARTMENT AT R/H STA 857 - 867; RBL 22; AFT OF DOOR; SHIELD HAVE 3 EACH FASTNER HOLES THAT ARE CORRODED. / REMOVED ADN REPLACED AFT CARGO COMPARTMENT R/H SHIELD AFT OF DOOR; RBL 22 STA 847 TO 86. CORROSION WAS REMOVED ORIGINAL THICKNESS .050; REMOVED .018 REMAINING .032 OUT OF LIMITS I/A/W 737-700 SRM 53-00-53-1A-2 FIG 103. APPLIED C.I.C TO NEW SHIELD I/A/W BOEING DWG 146A0081 REV C; 737-700 SRM 51-40-02-0G-0 AND 737 AMM 51-21-91-60-802 ATAG-WN5522

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT GUSSET CRACKED AT BS 500D, STR 21L. R&R GUSSET IAW SRM & DWG.

Part: RAIL — CORRODED (FWD CARGO LH) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT AFT BULKHEAD LEFT SIDE CURVED ANGLE STA 500D LBL 27-52 HAS CORROSION AROUND FASTENER HOLES / REMOVED FWD PIT AFT BULKHEAD LEFT SIDE CURVED ANGLE STA 500D LBL 27-52 IAW B737-700 WSRM 51-40-02 FECIEVED AND VERIFIED NEW RAIL ASSY AS P/N 143A9485-30 ATAG # WN5180 IAW B737-700 IPC 53-11-01-43 ITEM 155. LOCATED DRILLED AND INSTALLED NEW RAIL ASSY IAW B737-700 SRM 51-40-05 AND 51-40-02 APPLIED CIC IAW B737-700 51-21-91-620-802 ATAG # WN 5180

Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT STA 500D AFT BULKHEAD RIGHT SIDE CURVED ANGLE RBL 27-44 HAS CORROSION AROUND FASTENER HOLES / REMOVED CORROSION ON AFT BULKHEAD RIGHT SIDE CURVE ANGLE RBL 27.44 MATERIAL WAS FOUND TO BE 100% OUT OF LIMITS IAW SRM 51-10-02-0G-0 REMOVED AND REPLACAED RIGHTSIDE CURVED AFT BULKHEAD ANGLE RBL 27.44 IAW BOEING DWG 143A9481 REV A AT BS500D ATG#KD1565

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL LOWER SURFACE CORRODED AT BS 727D+5, LBL 3. REPAIRED CHANNEL IAW SRM AND EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT Z ANGLE CORRODED AT BS 727D, RBL 25. R&R Z ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FWD CARGO LH) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT FLOOR STRUCTURE Z-ANGLE STA 460+5 TO 500C+7 LBL 24 HAS CORROSION AROUND FASTENER HOLES / REMOVED 'OUT OF LIMITS' SECTION OF '2' ANGLE STA. 390-440 L/H AND INSTALLED NEW SECTION OF '2' ANGLE AS PER B737 SRM 53-00-53-2R-5 AND BAC DWG #143A7500 REV.- ATAGS A46933; A46935

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT FLOOR STRUCTURE Z-ANGLE CORRODED BETWEEN BS 500A TO BS 500D, RBL 24. R&R ANGLE IAW DWG AND SRM.

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT DOOR SURROUND LOWER SILL WEB STA 440-492 RBL 28 HAS CORROSION ON UPPER SURFACES / REMOVED AND REPLACED 1 EA WEB SILL @ STA. 440-492 RBL 28 REMOVED CORROSION @ SILL WEB IAW SRM 51-10-02-0G; VERIFIED W/DX MAG. ORIG 'T' 056 LOSS .008 REMAINING .048 FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1 FIG 103 SHEET 1 INSTALLED NEW WEB SILL IAW DWG# 143A8330 SHEET 12 REV C

Part: SHIELD — CORRODED (FWD CARGO RH) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT DOOR SURROUND AFT SHIELD STA 492-500A RBL 23 HAS CORROSION ON UPPER AND LOWER SURFACES / EVALUATED CORROSION ON FWD CARGO PIT DOOR SURROUND AFT SHEILD STA 492-500A RBL 23 FOUND MORE THAN 50% MATERIAL LOSS OUT OF LIMITS IAW SRM 53-30-15-1A-1. REMOVED AND REPLACED SHEILD SI#7531855 MPN 143A8126U31 ATAG# WN4897 IAW BOEING DWG# 143A0080 REV- AND SRM 51-40-02-0G-0.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL LOWER SURFACE CORRODED AT BS 727D+5, RBL 3. R&R CHANNEL IAW SRM & EA.

Part: WINDOW — CRACKED (COCKPIT) · airframe 69,992 hrs · 41,449 cycles

FIRST OFFICERS NR 2 WINDOW CRACKED IN SUPPORT FRAME. R&R NR 2 WINDOW PER TC.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT FLOOR STRUCTURE BAFFLE UNDER Z-ANGLE CRACKED BETWEEN BS 500A TO BS 500B, RBL 24. REPAIRED Z-ANGLE IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT FLOOR STRUCTURE BAFFLE CLIP CRACKED AT BS 500B, LBL 24. R&R CLIP IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGITUDINAL FASTENER HOLE CORRODED AT BS 727B+2, LBL 3. REPAIRED CHANNEL IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT FLOOR LONGERON CORRODED AT BS 727B, RBL 14. R&R TRACK IAW SRM. R&R TRACK IAW DWG 146A7500REV-.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO PIT LT Z ANGLE CORRODED BETWEEN BS 727C+10 TO BS 727E+10. R&R SPLICE PLATE IAW SRM.

Part: GUSSET — CORRODED (FWD CARGO LH) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT CARGO NET TIEDOWN STRUCTURE STA 420+18 STR 22L TIEDOWN MATING SURFACE HAS CORROSION / REMOVED CORROSION 1EA FASTNER HOLE BLOWN OUT 100% MATERIAL LOSS IAW SRM 51-10-02-06. RECIEVED SMAL FOR P/N 143A9403-33 GUSSET ON BOEING CONTROL NUMBER 0270191769 FABRICATED NEW- 33 GUSSET PER BOEING DRAWING 143A9403 -SHEET 26 REV- OUT OF MATERIAL 7075-T6-063 ATAG #A62595

Part: INTERCOSTAL — BROKEN (FWD CARGO LH) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT FLOOR STRUCTURE BAFFLE UNDER Z-ANGLE STA 500B-500C LBL 24 CORNER IS BROKEN OFF AT AFT END / REMOVED AND REPLACED RAFFLE AT STA 500B-500C LBL 24 PN 143A7510-11 IAW SRM 51-40-02-0G-0 51-40-050-0G-0 ATA A67631

Part: ANGLE — CORRODED (FWD CARGO LH) · airframe 69,992 hrs · 41,449 cycles

FORWARD CARGO PIT AFT BULKHEAD STA 500D LBL 24 - RBL 24 LOWER ANGLE HAS CORROSION AROUND FASTENER HOLES / REMOVED CORROSION FROM BS 500D LBL 24-RBL24 LWR ANGLE; MORE THAN 50% LOSS; OUT OF LIMITS IAW SRM 51-10-02. LOCATED AND DRILLED NEW ANGLE P/N 143A9485Y35 ATAG #WW2836 IAW SRM 51-40-05 AND BOEING DWG. 143A9485 REV. B. INSTALLED NEW BS500D LBL24 - RBL24 LWR ANGLE IAW 51-40-03 AND BOEING DWG 143A9485 REV B. APPLIED CIC IAW B737-700 AMM 51-21-91-620-802

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO COMPARTMENT CARGO DOOR CUTOUT CENTER SCUFF PLATE HAS A WEAR MARK AND CRACK 6.5' FROM FWD EDGE ON UPPER SURFACE. / AFT CARGO CENTER SCUFF PLATE REPLACED ON W/O 37445 8300 0013 W2605857 DIS # 0232641

Part: SKIN — CRACKED (LE SLAT) · airframe 69,992 hrs · 41,449 cycles

LT WING LEADING EDGE NR 3 SLAT NOSE SKIN AT ACTUATOR CRACKED AT 3 FASTENER HOLES. REPAIRED SKIN IAW SRM & DWG.

Part: NONE — CORRODED (AFT CARGO THRESH) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO BAY DOOR SILL PLATE HAS CORROSION AT 10 EACH SCREW HOLES (MARKED) / REMOVED CORROSION IAW B737 SRM 53-60-15-1A-1; FOUND TO BE OUT OF LIMITS IAW SRM53-60-15-1A-1. REMOVED DAMAGED SILL WEB IAW B737 SRM51-40-02. IDENTIFIED NEW WEB AS P/N 146A8123-25 PER BOEING ENG. DWG146A8120 REV:E. LOCATED AND DRILLED IAW B737 SRM 51-40-05; COUNTER SANK HOLES IAW B737 SRM 51-40-08. TREATED AND PRIMED HOLES IAW 737 AMM51-21-41 AND AMM 51-21-72. INSTALLED LOWER SILL WEB IAW B737-SRM51-40-02 AND BOEING ENG DWG NO 146A8340 REV:A. APPLIED CIC IAW B737 AMM 51-21-91-620-802.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,992 hrs · 41,449 cycles

RT WING LEADING EDGE NR 6 SLAT NOSE SKIN AT ACTUATOR CRACKED. R&R NR 6 SLAT SKIN IAW SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO COMPARTMENT CARGO DOOR CUTOUT CENTER SCUFF PLATE HAS A WEAR MARK AND POSSIBLE CRACK INDICATION 9.5' FROM AFT UPPER SURFACE. / AFT CARGO CENTER SCUFF PLATE REPLACED ON W/O 7445 8300 0013 W260587 DIS # 0232641

Part: STRAP — CORRODED (CARGO BAY) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO COMPARTMENT FORWARD AND AFT FLOOR STRAPS CORRODED. R&R STRAPS PER DWG.

Part: STRIP — CORRODED (FWD CARGO RH) · airframe 69,992 hrs · 41,449 cycles

FWD PIT R/H SIDEWALL TO FLOOR CAP STRIP HAS SEVERAL AREA'S OF CORROSION ( MARKED) / VERIFIED CAP STRIPFOR FWD PIT R/H SIDEWALL 1008 OUT OF LIMITS IAW B737-700 SRM 53-30-53-01-2. INSTALLED IN JPANEL-121-CLOSE (REPLACED WITH NEW CAP STRIP) A-TAG: WN2820

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO COMPARTMENT AFT CORNER SCUFF PLATE IS CRACKED / REPLACED AFT CARGO AFT CORNER SCUFF PLATE PN 654A0004-169 SI 7530337 IAW IPC 53-13-00-05 REPLACED ON PARTS RACK PART TO BE INSTALLED ON W/O 37443-8300-0002

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 69,992 hrs · 41,449 cycles

AFT CARGO COMPARTMENT CARGO DOOR CUTOUT CENTER SCUFF PLATE HAS A CRACK AT THE FWD EDGE ON BENT SURFACE. / AFT CARGO CENTER SCUFF PLATE REPLACED ON W/O 37445 8300 0013 W2605857 DIS # 0232641

Part: LIGHT — ODOR (CABIN) · airframe 69,062 hrs · 40,873 cycles

ACRID ODOR RT SIDE IN MID-CABIN ROW 14. R&R SIDEWALL LIGHT BULB PER AMM.

Part: SKIN — DELAMINATED (RUDDER) · airframe 68,459 hrs · 40,465 cycles

RIGHT RUDDER SKIN DELAMINATED ON TRAILING EDGE 24.5 INCHES IN FROM THE TOP. R & R THE RUDDER ASSEMBLY IAW AMM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 67,896 hrs · 40,114 cycles

LEFT HORIZONTAL FORWARD LOWER SLIDING SEAL CRACKED AND BENT AT UPPER ATTACHMENT. / INSTALLED ASSEMBLED SLIDER SEAL PER MM 53-31-31.

Part: NONE — CRACKED (LOWER EXT FUSELA) · airframe 67,896 hrs · 40,114 cycles

KEEL BEAM 192E PANEL FORWARD LEFT AND RIGHT CLIPS CRACKED. / REMOVED AND REPLACED CLIPS PER 51-40-02 SRM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 67,056 hrs · 39,589 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. R & R THE SIGN ASSEMBLY IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 66,937 hrs · 39,518 cycles

RT OVERWING EXIT LIGHT COVER LOOSE. SECURED COVER ASSEMBLY IAW AMM.

Part: BRACKET — CRACKED (LT WING) · airframe 65,760 hrs · 38,836 cycles

LT WING INBOARD OF LEADING EDGE BRACKET CRACKED ON LOWER FORWARD FIXED LEADING EDGE AT APPROXIMATE WS 200. R&R BRACKET PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FRAME CORRODED AT BS 303.9, STRINGER 22L. REPAIRED FRAME IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

STRINGER CORRODED BETWEEN BS 294.5 - 312, STRINGER 23L. R & R STRINGER IAW SRM & DWG.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

EQUIPMENT ELECTRONIC COMPARTMENT TEE CORRODED AT BS 303.9, STRINGER 23L. R & R TEE IAW SRM & DWG.

Part: FAIRING — BROKEN (TE FLAP) · airframe 63,528 hrs · 37,477 cycles

LEFT WING FLAP TRACK FAIRING 543BB PHONOLITE BROKEN. R & R PHONOLITE IAW SRM & DWG.

Part: WEB — CRACKED (RT WING) · airframe 63,528 hrs · 37,477 cycles

RIGHT WING TE WEB ASSEMBLY CRACKED AT WBL 201.90. R & R WEB ASSEMBLY IAW SRM.

Part: FAIRING — BROKEN (TE FLAP) · airframe 63,528 hrs · 37,477 cycles

LEFT WING FLAP TRACK FAIRING 544BB PHONOLITE BROKEN. R & R PHONOLITE IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 63,528 hrs · 37,477 cycles

LEFT WING TE UPPER CHORD ANGLE CRACKED AT LEVEL IRSS 140. R & R ANGLE IAW SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 63,528 hrs · 37,477 cycles

LEFT WING FLAP TRACK FAIRING 542BB CRACKED. REPAIRED FAIRING IAW EA & SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 63,528 hrs · 37,477 cycles

RIGHT WING TE UPPER CHORD ANGLE CRACKED AT LEVEL IRSS 140. R & R ANGLE IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,528 hrs · 37,477 cycles

PRESSURE DECK WEB CRACKED AT BS 663.75, RBL 40. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,528 hrs · 37,477 cycles

PRESSURE DECK WEB CRACKED AT BS 663.75, LBL 36. REPAIRED WEB IAW EA.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 63,528 hrs · 37,477 cycles

FORWARD CARGO COMPARTMENT TRACK CRACKED AT BS 460, RBL 14. REPAIRED TRACK IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

AFT CARGO COMPARTMENT SUPPORT ZEE CORRODED BETWEEN BS 727D - 787, STRINGER 25L. REPAIRED SUPPORT ZEE IAW SRM.

Part: COVER — CRACKED (R1 DOOR) · airframe 63,528 hrs · 37,477 cycles

COVER CRACKED AT BS 332, STRINGER 9R. R & R COVER IAW AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FLOORBEAM CRACKED AT BS 328, RBL 19. REPAIRED FLOORBEAM IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

AFT CARGO COMPARTMENT SUPPORT ZEE CORRODED, BETWEEN BS 727C+9 - 767, STRINGER 25R. REPAIRED SUPPORT ZEE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN LBL 11 - RBL 43. REPAIR FLOORBEAM IAW EA.

Part: FLASHLIGHT — CRACKED (CABIN) · airframe 63,528 hrs · 37,477 cycles

LEFT FWD GALLEY EMER FLASHLIGHT BASE CRACKED. R & R FLASHLIGHT IAW CMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

INTERCOSTAL CRACKED, BETWEEN BS 277 - 294.5, BL 0. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

INTERCOSTAL CRACKED AT BETWEEN BS 344 - 360, LBL 11. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

INTERCOSTAL CRACKED BETWEEN BS 294.5 - 312, RBL 15. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

INTERCOSTAL CRACKED, BETWEEN BS 328 - 344, LBL 46. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 - 328, LBL 46. R & R INTERCOSTAL IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FLOOR STRUCTURE INNER CHORD CRACKED BS 294.5, LBL 56. R & R CHORD IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FORWARD BULKHEAD WEB CRACKED AT BS 663.75, LBL 15. REPAIRED WEB IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FORWARD CARGO COMPARTMENT BRACKET CRACKED AT BS 500C, STRINGER 26R. R & R BRACKET IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FORWARD BULKHEAD WEB CRACKED AT BS 663.75, LBL 8. REPAIRED WEB IAW EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

AFT CARGO COMPARTMENT CHANNEL SUPPORT CRACKED AT BS 727, RBL 3. R & R SUPPORT IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R GUSSET IAW SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FORWARD CARGO COMPARTMENT BRACKET CRACKED AT BS 500A, STRINGER 26L. R & R BRACKET IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FORWARD BULKHEAD STIFFENER CRACKED BS 663.75, BETWEEN RBL 5 - 34. R & R STIFFENER IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FORWARD CARGO COMPARTMENT, GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R GUSSET IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,528 hrs · 37,477 cycles

AFT CARGO COMPARTMENT TRACK CORRODED, BETWEEN BS 887 - 947.5, LBL 8.1. R & R TRACK IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

AFT CARGO COMPARTMENT INTERCOSTAL WEB CRACKED, BETWEEN BS 927 - 947.5, STRINGER 25R. R & R WEB IAW SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

FORWARD CARGO COMPARTMENT, BRACKET CRACKED AT BS 400, STRINGER 26R. R & R BRACKET IAW SRM & DWG.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 63,528 hrs · 37,477 cycles

AFT CARGO COMPARTMENT TRACK CRACKED AT BS 727E, RBL 13.84. REPAIRED TRACK IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,528 hrs · 37,477 cycles

HORIZONTAL STIFFENER CRACKED AT BS 663.75, BETWEEN RBL 5 - 65. R & R STIFFENER IAW SRM & DWG.

Part: MOUNT — CORRODED (GIRT BAR) · airframe 63,528 hrs · 37,477 cycles

R1 DOOR GIRT BAR MOUNT HARDWARE RUTTED. R & R MOUNT ASSEMBLY IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 62,640 hrs · 36,951 cycles

R1 DOOR LOWER FWD CORNER, EMER EXIT SIGN COVER LOOSE. R & R SIGN ASSEMBLY IAW AMM.

Part: WINDOW — ARCED (COCKPIT) · airframe 62,327 hrs · 36,770 cycles

R1 COCKPIT WINDOW ARCING. R & R R1 WINDOW ASSEMBLY IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 61,779 hrs · 36,458 cycles

R1 DOOR EMER EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 61,083 hrs · 36,025 cycles

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

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,362 hrs · 35,068 cycles

SEAT TRACK CORRODED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 59,003 hrs · 34,873 cycles

LEFT LOWER EMER EXIT LIGHT COVER MISSING. INSTALLED COVER IAW MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 58,498 hrs · 34,592 cycles

R1 DOOR EXIT SALIDA LIGHT COVER LOOSE. R & R SIGN ASSEMBLY IAW AMM.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 57,272 hrs · 3,882 cycles

B ELEC HYD PUMP LOW PRESS LIGHT ON SWITCH FAILED. R & R PUMP IAW MM.

Part: CASTING — CRACKED (KRUEGER FLAP) · airframe 56,944 hrs · 33,705 cycles

RIGHT WING NR 4 KRUEGER FLAP CASTING CRACKED AT RADIUS JUST OTBD OF ACTUATOR FITTING. R & R KRUEGER FLAP IAW MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, LBL 8. R & R INTERCOSTAL IAW DWG & SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 56,925 hrs · 33,696 cycles

LEFT HORIZONTAL STABILIZER LOWER FLANGE AT RIB CRACKED AT BS 92.70, ZONE 13. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 56,925 hrs · 33,696 cycles

RIGHT HORIZONTAL STABILIZER STATION 101.9 29 INCHES AFT OF FWD SPAR 1 INCH FROM LOWER EDGE RIB CRACKED. REPAIRED RIB IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 56,925 hrs · 33,696 cycles

LEFT WING OTBD AFT FLAP DELAMINATED AT INBD END ON UPPER & LOWER SURFACES. R & R AFT FLAP IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

COCKPIT LT NR 3 WINDOW FRAME E - F WINDOW POST CRACKED AT UPPER FASTENER, COMMON TO NR 2 WINDOW FRAME. R & R FRAME IAW DWG & SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

COCKPIT RT NR 3 WINDOW FRAME E - F POST CRACKED AT UPPER FASTENER COMMON TO NR 2 WINDOW FRAME. R & R FRAME IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

FUSELAGE FRAME CRACKED AT STATION 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 56,925 hrs · 33,696 cycles

RIGHT WING NR 3 FLAP FAIRING CRACKED FASTENER HOLE AT AFT TAIL CONE CONNECTION. REPAIRED FAIRING IAW WO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

FUSELAGE FRAME CRACKED AT STATION 727B, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

FUSELAGE FRAME CRACKED AT STATION 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

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

Part: FAIRING — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

LEFT OVERWING BODY FAIRING 195CL AFT EXTERIOR AFT CORNER CRACKED. REPAIRED FAIRING IAW WO.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,925 hrs · 33,696 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT STATION 663, RBL 34.5. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,925 hrs · 33,696 cycles

RIGHT WING NR 8 SLAT LE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 56,925 hrs · 33,696 cycles

RIGHT WING NR 7 SLAT ACCESS PANEL 624DB CRACKED AT INBD LOWER FASTENER HOLE. R & R PANEL IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,925 hrs · 33,696 cycles

FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: FITTING — OUT OF ADJUST (L2 DOOR) · airframe 55,992 hrs · 33,163 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW CLIPS OUT OF ADJUSTMENT. ADJUSTED CLIPS IAW SIP.

Part: FITTING — OUT OF ADJUST (R2 DOOR) · airframe 55,992 hrs · 33,163 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW CLIPS OUT OF ADJUSTMENT. ADJUSTED CLIPS IAW SIP.

Part: FITTING — OUT OF ADJUST (R1 DOOR) · airframe 55,992 hrs · 33,163 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW CLIPS OUT OF ADJUSTMENT. ADJUSTED CLIPS IAW SIP.

Part: FITTING — OUT OF ADJUST (L1 DOOR) · airframe 55,992 hrs · 33,163 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW CLIPS OUT OF ADJUSTMENT. ADJUSTED CLIPS IAW SIP.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 55,409 hrs · 32,813 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. R & R SLIDE IAW TC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,259 hrs · 32,720 cycles

RT EMERGENCY LIGHTS INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: PLATE — CRACKED (LT WING) · airframe 52,761 hrs · 31,265 cycles

LEFT WING, WIGGLE PLATE BEHIND NR 1 ENGINE PYLON IS CRACKED. REMOVED AND REPLACED WIGGLE PLATE PER MM AND SRM 51-40-02.

Part: RETAINER — CRACKED (LT WING) · airframe 52,761 hrs · 31,265 cycles

LEFT WING UPPER T/E SHELF PANEL, O/B OF NR 6 GROUND SPOILER, SEAL RETAINER IS CRACKED. REMOVED AND REPLACED SEAL RETAINER PER SRM 51-10-02.

Part: BATTERY — FAILED (CABIN) · airframe 52,761 hrs · 31,265 cycles

AFT EMERGENCY BATTERY M1675 FAILED CAPACITY CHECK. REMOVED AND REPLACED AFT EMERGENCY BATTERY AT LOCATION M01675 PER MM AND SWPM.

Part: BATTERY — FAILED (CABIN) · airframe 52,761 hrs · 31,265 cycles

AFT EMERGENCY BATTERY M1673 FAILED CAPACITY CHECK. REMOVED AND REPLACED AFT EMERGENCY BATTERY AT LOCATION MO1673 PER MM AND SWPM.

Part: BATTERY — FAILED (CABIN) · airframe 52,761 hrs · 31,265 cycles

AFT EMERGENCY BATTERY FAILED CAPACITY CHECK AT M1672. REMOVED AND REPLACED AFT EMERGENCY BATTERY AT LOCATION M1672 PER MM AND SWPM.

Part: BATTERY — FAILED (CABIN) · airframe 52,761 hrs · 31,265 cycles

AFT EMERGENCY BATTERY M1669 FAILED CAPACITY CHECK. REMOVED AND REPLACED AFT EMERGENCY BATTERY AT LOCATION M01669 PER MM AND SWPM.

Part: COVER — BROKEN (CABIN) · airframe 52,727 hrs · 31,245 cycles

RIGHT AFT SERVICE DOOR EMERGENCY LIGHT COVER BROKEN. INSTALLED NEW LIGHT ASSEMBLY ON RIGHT AFT SERVICE DOOR EMERGENCY LIGHT PER M/M.

Part: SIGN — BROKEN (CABIN) · airframe 51,675 hrs · 30,574 cycles

R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED SIGN PER M/M.

Part: LIGHT — BROKEN (CABIN) · airframe 50,630 hrs · 29,925 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 50,188 hrs · 29,682 cycles

FORWARD CABIN GALLEY EMERGENCY EXIT SIGN LIGHT LENS CRACKED. REMOVED AND REPLACED LENS IAW AMM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 50,188 hrs · 29,682 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147.90. REPAIRED SKIN IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 49,442 hrs · 29,266 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS BRACKET LOOSE. SECURED LENS IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 47,907 hrs · 28,365 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BASE BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,915 hrs · 27,784 cycles

DURING SCHEDULED MV1 CHECK FOUND, L1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 5. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (TE FLAP) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING I/B AFT FLAP LOWER SKIN I/B END CRACKED. REPAIRED AFT FLAP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR CREASE BEAM CORRODED FROM BS 947.5 TO BS 992.8. REMOVED AND REPLACED BEAM PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP I/B UPPER AND LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CAP CORRODED AT BS 986.5, BETWEEN RBL 28 TO RBL 46. REMOVED AND REPLACED T-CAP PER MM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED ON I/B LOWER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME SECTION PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME SECTION PER EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 31. REMOVED AND REPLACED FITTING PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME ANGLE CORRODED AT BS 787, RBL 20. REMOVED AND REPLACED ANGLE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME SECTION PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME SECTION PER EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 41. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME SECTION PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED CHANNEL PER MM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, RBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, RBL 14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, RBL 41. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, RBL 31. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,795 hrs · 25,982 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 43,233 hrs · 25,652 cycles

AFT GALLEY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 42,690 hrs · 25,369 cycles

L1 COCKPIT WINDOW ARCED INFLIGHT. REMOVED AND REPLACED L1 WINDOW AND HEAT CONTROLLER PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 41,893 hrs · 24,858 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT LOWER IN-SPAR SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 41,593 hrs · 24,858 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT LOWER IN-SPAR SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,893 hrs · 24,858 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 40,967 hrs · 24,284 cycles

EEPLS LOOSE AT ROW 7. SECURED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 40,944 hrs · 24,270 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 37,588 hrs · 22,177 cycles

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

Part: BATTERY PACK — FAILED (EMEGENCY LIGHT) · airframe 37,588 hrs · 22,177 cycles

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

Part: FAN — FAULTY (E&E BAY) · airframe 36,841 hrs · 21,719 cycles

FLIGHT CREW REPORTED A BURNING ELECTRICAL ODOR. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,321 hrs · 21,392 cycles

DURING SCHEDULED CV CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 21 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 35,001 hrs · 20,603 cycles

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

Part: TRUNNION — CORRODED (RT MLG) · airframe 34,748 hrs · 20,445 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 34,410 hrs · 20,257 cycles

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

Part: ACTUATOR — FAULTY (NLG) · airframe 32,882 hrs · 19,329 cycles

NOSE GEAR WOULD NOT RETRACT. CYCLED GEAR HANDLE NOSE GEAR RETRACTED. R&R NLG LOCK ACTUATOR PER MM.

Part: MANIFOLD — FAULTY (NLG W/W) · airframe 32,869 hrs · 19,323 cycles

AIRTURN BACK - NOSE GEAR WOULD NOT RETRACT, CYCLED GEAR LEVER TWICE NO HELP. RED AND GREEN LIGHTS ILLUMINATED. R&R NOSE GEAR HYD LOCKING ACTUATOR MANIFOLD ASSY PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 30,088 hrs · 17,773 cycles

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

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 30,029 hrs · 17,732 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 7 TO RBL 11. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,029 hrs · 17,732 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 10 TO BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,029 hrs · 17,732 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 40 TO RBL 40. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,029 hrs · 17,732 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOOR SUPPORT BEAM CORRODED AT BS 772 , RBL 8 TO LBL 13. REPAIRED FLOOR SUPPORT BEAM IAW SWA EA.

Part: BULB — INOPERATIVE (FUSELAGE) · airframe 28,722 hrs · 16,940 cycles

DURING SCHEDULED RON CHECK, FOUND R2 DOOR AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,304 hrs · 14,980 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,558 hrs · 14,580 cycles

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

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 23,839 hrs · 14,150 cycles

EMERGENCY EXIT SIGN AT AFT SERVICE DOOR BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 21,810 hrs · 13,031 cycles

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

Part: CONTROLLER — ARCED (COCKPIT) · airframe 20,876 hrs · 12,492 cycles

R1 WINDOW ARC WHEN WINDOW HEAT SELECTED. REMOVED AND REPLACED WINDOW HEAT CONTROLLER PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,216 hrs · 11,026 cycles

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

Part: SLIDE — OUT OF ADJUST (ALL CABIN DOORS) · airframe 16,531 hrs · 10,104 cycles

DURING SCHEDULED C4 CHECK, FOUND ALL FOUR CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: LENS — MISSING (CABIN) · airframe 15,989 hrs · 9,798 cycles

EEPLS LENSES MISSING (4 EA) IN CABIN. INSTALLED LENSES PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 15,272 hrs · 9,395 cycles

DURING SCHEDULED RON, FOUND AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,224 hrs · 8,848 cycles

DURING SCHEDULED RON, FOUND AFT ENTRY DOOR RT SIDE SLIDE LIGHT INOP. REMOVED AND REPLACED DOOR SLIDE LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,206 hrs · 8,834 cycles

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT LIGHTS INOP AT ROW'S 13 ABC, 23 DEF AND 21 DEF. REPAIRED OVERHEAD EXIT LIGHTS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,206 hrs · 8,834 cycles

DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,206 hrs · 8,834 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP BETWEEN ROW'S 21 AND 23. REPAIRED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 14,206 hrs · 8,834 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S 12 AND 21. REMOVED AND REPLACED COVERS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 13,719 hrs · 8,557 cycles

EEPLS LOOSE. SECURED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 11,858 hrs · 7,464 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW 1 & ROW 23. R&R COVERS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 11,306 hrs · 7,150 cycles

EEPLS LOOSE AT ROW 1. SECURED EEPLS PER MM.

Part: CONTROL ARM — WORN (ELEVATOR) · airframe 10,405 hrs · 6,615 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, FOUND LT ELEVATOR TAB CONTROL MECHANISM HAS EXCESSIVE PLAY AT ROD CONNECTIONS. REMOVED AND REPLACED ELEVATOR TAB CONTROL MECH PER MM.

Part: BEARING — WORN (ELEVATOR TAB) · airframe 9,901 hrs · 6,342 cycles

DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND NR 2 & 4 LT ELEVATOR TAB BEARINGS WORN. REMOVED AND REPLACED BEARINGS PER D&M ENTERPRISES WORK ORDER SSR:011.

Part: BEARING — WORN (ELEVATOR TAB) · airframe 9,901 hrs · 6,342 cycles

DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND NR 1, 2 & 4 RT ELEVATOR TAB BEARINGS WORN. REMOVED AND REPLACED BEARINGS PER D&M ENTERPRISES WORK ORDER SSR:011.

Part: LAMP — INOPERATIVE (ROW 20) · airframe 8,290 hrs · 5,372 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT INOP AT LT OVERHEAD BIN, ROW 20. REMOVED AND REPLACED LAMP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,736 hrs · 4,404 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 8. RELAMPED PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP NEAR OVERWING EXIT. REMOVED AND REPLACED LIGHT ASSY PER MM.