N744SW

Part: MEGAPHONE — NO TEST (AFT CABIN) · airframe 76,030 hrs · 45,380 cycles

AFT MEGAPHONE WILL NOT TEST ; / [01] REMOVED AND REPLACED AFT MEGAPHONE IAW AMM 25-64-00. OP CHECK GOOD

Part: SKIN — CRACKED (BS 520 S4R) · airframe 75,078 hrs · 44,816 cycles

FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; / C/W STEP3.DO A HIGH FREQUENCY EDDY CURRENT (HFEC) HOLE PROBE INSPECTION OF ANY ADDITIONAL EXISTING FASTENER HOLES COMMON TO THE REPAIR AREA PER 737 NDT PART 6; 51-00-00 PROCEDURE 16 USING A 0.030' NOTCH STANDARD. REFERENCE THIS EA FIGURE 2-1.ACCOMPLISHED NO DEFECTS.C/W STEP 4.DO A HIGH FREQUENCY EDDY CURRENT (HFEC) HOLE PROBE INSPECTION OF ALL EXISTING FASTENER COUNTERSINKS COMMON TO THE REPAIR AREA PER 737 NDT PART 6; 53-30-00; PROCEDURE 3 OR 4. REFERENCE THIS EA FIGURE 2-1.ACCOMPLISHED NO DEFECTS.; STEP 10 N/A; COMPLIED WITH EA

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,078 hrs · 44,816 cycles

FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R; ISSUED EA 2115301243WIP1 AS A SUBTASK TO THE FAULT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,078 hrs · 44,816 cycles

FUSELAGE CRACK INDICATION AT BS 500A +11 AND S4R

Part: SKIN — CRACKED (BS 500S S4R) · airframe 75,078 hrs · 44,816 cycles

FUSELAGE CRACK INDICATION AT BS 500A +11 AND S-4R ; /

Part: SKIN — CRACKED (BS 520 S4R) · airframe 75,078 hrs · 44,816 cycles

FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; / COMPLIED WITH EA

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,078 hrs · 44,816 cycles

FUSELAGE CRACK INDICATION AT BS 520 +13 AND S4R; REPAIRED PER EA 211531243

Part: SKIN — CRACKED (BS 520 S4R) · airframe 75,078 hrs · 44,816 cycles

FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; /

Part: SKIN — CRACKED (BS 500A S4R) · airframe 75,078 hrs · 44,816 cycles

FUSELAGE CRACK INDICATION AT BS 500A +11 AND S-4R ; /

Part: SKIN — CRACKED (BS 520 S4R) · airframe 75,078 hrs · 44,816 cycles

FUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; /

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 75,025 hrs · 44,785 cycles

AFT MEGAPHONE INOP / REPLACED AFT MEGAPHONE BATTERIES REF AMM 25-68-00. OPS CHECK GOOD.

Part: SLIDE — PULLED (L1 DOOR) · airframe 74,807 hrs · 44,668 cycles

CREW REPORTS:L1 DOOR SLIDE GIRL BAR MATERIAL PULLED OUT EXCESSIVE / REPOSITION SLIDE AND POSITIONS GIRL MATERIAL FOR L1 SLIDE ASSY ALL PER MT 7255-61-06 ALL C/W ALL NOW GOOD

Part: ENGINE — POWER LOSS (NR 1) · airframe 74,172 hrs · 44,326 cycles

NR 1 ENGINE N1 ROLLED BACK APPROX 15% AT CRUISE AND THEN RECOVERED AFTER 5-7 SECS AND HAD ASSOCIATED GRUMBLING NOISE FOR REMAINDER OF FLIGHT. NO EEC LIGHT AND NO HIGH VIBE IND.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 73,684 hrs · 44,016 cycles

INTERIOR: EMERGENCY LIGHT EXIT MISSING BULB AT LT OVERWING DOOR AT UPPER SIGN. RELAMPED AND PERFORMED GOOD TEST OF LT OVERWING UPPER EMERGENCY EXIT SIGN, PER AMM 33-51-01-960-801.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 73,684 hrs · 44,016 cycles

INTERIOR: EMERGENCY LIGHT EXIT MISSING BULB AT AFT SERVICE DOOR. RELAMPED AND PERFORMED GOOD TEST OF AFT SERVICE DOOR EMERGENCY EXIT SIGN, PER AMM 33-51-01-960-801.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 73,684 hrs · 44,016 cycles

INTERIOR: EMERGENCY LIGHT EXIT MISSING BULB AT L1 AND LT OVERWING. RELAMPED AND PERFORMED GOOD TEST OF LT OVERWING EMERGENCY EXIT SIGN. REPLACED AND PERFORMED GOOD TEST OF L1 EMERGENCY EXIT SIGN LIGHT ASSEMBLY, PER AMM 33-51-01-760-801 AND AMM 33-51-01-960-802.

Part: FLOOR SPLICE — CORRODED (BS 727D) · airframe 73,684 hrs · 44,016 cycles

***CORROSION*** AFT CARGO BAY FLOOR SPLICE CORRODED AT BS 727D. RBL14; WL156 / RECEIVED NEW/SERVICABLE AFT CARGO BAY FLOOR SPLICE AT BS 727D TO BE INSTALLED ON JPANEL-141-CLOSE. 57609U 15SEP20

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,684 hrs · 44,016 cycles

EMERGENCY LIGHT AFT OF RIGHT SIDE FLAP IS OUT. RELAMPED AND PERFORMED GOOD TEST OF RIGHT AFT SLIDE EMERGENCY LIGHT, PER AMM 33-51-04-960-801. 59019U 14SEP20.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 73,684 hrs · 44,016 cycles

EMERGENCY SLIDE LIGHT AT FWD SERVICE DOOR ONLY ILLUMINATES FOR A FEW SECONDS. REMOVED AND INSTALLED NEW. PERFORMED A GOOD INSTALLATION TEST OF THE M01674 BATTERY PACK, PER AMM 33-51-06-960-805.

Part: SPLICE PLATE — CORRODED (AFT CRGO FLR PNL) · airframe 73,684 hrs · 44,016 cycles

***CORROSION*** AFT CARGO BAY FLOOR SPLICE CORRODED AT BS 767+5. / RECEIVED SERVICEABLE REPLACEMENT PART; PO NUMBER 801448. REPLACEMENT SPLICE PLATE TO BE INSTALLED WITH FLOOR PANELS ON JPANEL-141-CLOSE. 57133U 14SEP20

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 73,684 hrs · 44,016 cycles

EXIT SIGN ABOVE AFT ENTRY DOOR IS INOP. PERFORMED CONTINUITY TEST FROM CONNECTOR D2982 TO D10744 AND GROUND, PER WDM 33-51-14 AND FOUND WIRE W3142-0474-20 DISCONNECTED FROM GD3814-DC. TERMINATED AND REINSERTED WIRE W3142-0474-20 INTO GD3814-DC AND PERFORMED GOOD CONTINUITY CHECK, PER SWPM 20-90-15 AND WDM 33-51-14. PERFORMED GOOD FUNCTIONAL TEST OF EMERGENCY EXIT LIGHTS ABOVE AFT LT DOOR, PER AMM 33-51-00-710-801 59019U 14SEP20.

Part: SKIN — DENTED (BS 578) · airframe 73,684 hrs · 44,016 cycles

FUSELAGE SKIN HAS A DENT AT BS 578+4.5'; 1.5' ABOVE S-4R. REPAIRED FUSELAGE SKIN DENT AT BS 578+4.5'; 1.5' ABOVE S-4R, PER EA 20-153-01719 REV IR AND ER 20-03260 REV IR.

Part: SKIN — DENTED (BS 203) · airframe 73,684 hrs · 44,016 cycles

FUSELAGE SKIN HAS A DENT AT BS 203.8+4.5'; 4' BELOW S-17L. FUSELAGE SKIN DENT AT BS 203.8+4.5'; 4' BELOW S-17L. REPAIRED IAW ATS ER 20-03255 REV IR DATED 23-SEP-2020 AND PER EA NO:20-153-01830 REV IR. 55981U 23SEP20.

Part: SKIN — DENTED (BS 827) · airframe 73,684 hrs · 44,016 cycles

FUSELAGE SKIN HAS A DENT AT BS 827+8.5; 3.8' ABOVE S-7L. REPAIRED FUSELAGE SKIN DENT AT BS 827+8.5; 3.8' ABOVE S-7L, PER 737-700 SRM 53-00-01-2R-3 (REPAIR 3).

Part: SUPPORT — CORRODED (BS 727-847) · airframe 73,684 hrs · 44,016 cycles

***CORROSION*** IN AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT B.S. 727-847; L.B.L. 21; W.L. 154. / REMOVED AND REPLACED FLOOR SIDEWALL SUPPORT AT ACB BS727-847 LBL27 WL154 AS PER SRM 51-40-02-0G-0 AND DRAWING #146A7502. EVALUATED FLOOR SIDEWALL SUPPORT AND AND FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 50% OF MATERIAL LOSS AS PER SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2. DRAWING #146A7500

Part: SHIELD — CORRODED (FWD CARGO) · airframe 73,684 hrs · 44,016 cycles

***CORROSION*** ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL24 WL157. / REMOVED AND REPLACED SHIELD AT FWD CARGO BAY LOCATED BS420-BS440 RBL24 WL157 ITEM 7530143 IAW SRM 51-40-02 ITEM 4.B AND DWG # 143A0080 59202U 10SEP20.

Part: ATTACH ANGLE — CRACKED (BS 500B) · airframe 73,684 hrs · 44,016 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL25 WL156. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS 500B FWD SIDE LBL25 IAW SRM 51-40-02-0G-0 AND DWG 143A7505

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 73,684 hrs · 44,016 cycles

***CORROSION*** ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FWD CARGO BAY BS500D RBL25 WL157. / REMOVED AND REPLACED ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FCB BS 500D S-19R - S-26R. ITEM 7530202 PO # 800475 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A7902 80641U 17SEPT20

Part: ATTACH ANGLE — CRACKED (BS 400) · airframe 73,684 hrs · 44,016 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 RBL25 WL156. / REMOVED AND REPLACED ON INTERCOSTAL ATTACH ANGLE AT FCB BS 400 RBL 25 NEW P/N 143A7502-156 PO# 802611. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 143A7505 80641U 14SEPT20

Part: SUPPORT — CORRODED (BS 727-767) · airframe 73,684 hrs · 44,016 cycles

***CORROSION*** IN AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT B.S. 727-767; R.B.L. 21; W.L. 154. / REMOVED AND REPLACED SIDEWALL SUPPORT AT ACB BS727-767 WL154 AS PER SRM 51-40-02-0G-0 AND DRAWING # 146A7502. EVALUATED SIDEWALL SUPPORT AND FOUND TO BE OUT OF LIMITS DUE TO 50% OF MATERIAL LOSS AS PER SRM.56-60-53-0I-2 AND SRM 53-00-53-1A-2

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 73,684 hrs · 44,016 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED AND REPLACED ON FCB AFT BULKHEAD SUPPORT GUSSET BS 500D S-19L P/N 143A9481-6 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A7902 80641U 15SEPT20

Part: ATTACH ANGLE — BENT (BS 500A) · airframe 73,684 hrs · 44,016 cycles

AFT SHIELD HAS BENT ATTACH ANGLE AT FWD CARGO BAY BS500A RBL25 WL157. / FABRICATED NEW FCB AFT SHIELD ATTACH ANGLE BS500A RBL-25 WL-157 MADE FROM BAC1503 - 100179 7075-T6511 LOT# 1442201-2 EXTRUSION IAW SRM 51-40-05 AND DWG # 143A8124 SENT TO OSS FOR HEAT TREATMENT AND RECIEVED FROM OSS IN THE FORM T73511 PER PO# 803068-SWA AND PO# 803067-SWA PRIMED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG # 143A7505 REV-D AND DWG # 143A0080

Part: CARGO TRACK — CORRODED (BS 500) · airframe 73,684 hrs · 44,016 cycles

***CORROSION*** ON TRACK TIEDOWN AT FWD CARGO BAY BS500 LBL18 WL157. / REMOVED AND INSTALLED NEW TRACK TIEDOWN AT FWD CARGO BAY AT BS396 TO BS500D LBL 18; WL 157 ITEM # 7535311 IAW SRM 53-30-53-01-2; SRM 53-00-53-1A-2 SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG # 143A7501; DWG # 143A7500 57319U 09-16-20

Part: BOOT — DAMAGED (RADOME) · airframe 73,684 hrs · 44,016 cycles

NOSE RADOME BOOT IS DAMAGED / REMOVED DAMAGED RADOME BOOT AND INSTALLED A NEW RADOME BOOT IAW. AMM 53-52-00-400-802. 6042U 14SEP20. AND AMM 53-52-00-000-802 6042U 14SEP20.

Part: STRINGER — CRACKED (BS 540) · airframe 73,684 hrs · 44,016 cycles

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 S-27L WL151. CRACKED STRINGER AT BS 540 S-27L WL151 WAS REPAIRED, IAW SRM 53-00-03-2R-1 REPAIR 1.

Part: STRINGER — CRACKED (BS 540) · airframe 73,684 hrs · 44,016 cycles

CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 S-23R WL 167. CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS 540 - S-23R. REPAIRED, IAW ATS ER 20-03242 REV IR DATED 21-SEP-2020 AND PER EA NO:20-153-01783 REV IR 55981U 22SEP20.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 73,684 hrs · 44,016 cycles

***CORROSION*** ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL22 TO RBL22 WL157. / REMOVED AND REPLACED ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FCB BS500D LBL22 TO RBL22 ITEM 7530142 PO # 798181 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02; DWG 143A7902 AND DWG 143A9481 80641U 17SEPT20

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 73,684 hrs · 44,016 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS 500C FWD SIDE RBL 25 WL 156. REMOVED AND REPLACED NEW ON INTERCOSTAL ATTACH ANGLE AT FCB BS 500C RBL 25 P/N 143A7502U160 PO NR 802622. LOCATED AND DRILLED, IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A7505. 80641U 14SEPT20.

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 73,684 hrs · 44,016 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / REMOVED AND REPLACED ON FCB AFT BULKHEAD SUPPORT GUSSET BS 500D S-19R P/N 143A948-5 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A7902 80641U 16SEPT20

Part: SKIN — BENT (FWD ENTRY DOOR) · airframe 73,684 hrs · 44,016 cycles

FORWARD ENTRY DOOR UPPER AFT DOOR SKIN IS BENT. REPAIRED FORWARD ENTRY DOOR UPPER AFT DOOR SKIN, PER SRM 52-00-01-2R-2.

Part: ATTACH BRACKET — BROKEN (WING) · airframe 73,684 hrs · 44,016 cycles

ATTACH BRACKET FOR PANEL 551FB AT IRSS 209 ALONG LOWER REAR SPAR CORD IS BROKEN / REMOVED ATTACH BRACKET FOR PANEL 551FB IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED HOLES IN NEW BRACKET IAW SRM 51-40-05-0G-0 FIGURE 4 SHEET 2. VERIFIED CORRECT FASTNER APPLICATION IAW AIPC 57-50-00-23 SHEET 004. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G-0 STEPS 7.D.(1);AND (4). 59799U 14SEP20

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 73,684 hrs · 44,016 cycles

FWD CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED FWD CARGO AFT CORNER SCUFF PLATE IAW SRM 51-40-05-0G-0 SCUFF PLATE TO BE INSTALLED ON CUSTOMER CARD # 753-140-00-01Y 56334U 17SEP20

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 73,684 hrs · 44,016 cycles

FWD CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED NEW FWD CARGO BAY FWD CORNER SCUFF PLATE IAW SRM 51-40-05-0G-0 SCUFF PLATE TO BE INSTALLED ON CUSTOMER CARD # 753-140-00-01Y 56334U 17SEP20

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 73,684 hrs · 44,016 cycles

MECHANICAL DAMAGE ON SEAT TRACK AT PASSENGER CABIN BS 520 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK AT PASSENGER CABIN FROM BS 480-520 LBL 45 WL 208, AS PER SRM 51-40-02-0G-0 AND DRAWING NR 143A5300. SEAT TRACK WAS EVALUATED AND FOUND TO BE OUT OF LIMITS L=1.2' D=0.045' ON TOP SURFACE OF THE CROWN AREA, AS PER SRM 53-00-52-1A-1 STEP 4 A FIG 103 DETAIL A.

Part: ATTACH FITTING — CRACKED (RT WING) · airframe 73,684 hrs · 44,016 cycles

UPPER ATTACH FITTING CRACKED ON RT WING DEFLECTION RIB ORSS281, MARKED. REMOVED THE DAMAGED PART AT UPPER ATTACH FITTING ON RT WING DEFLECTION RIB ORSS 281 AND INSTALLED REPAIR PARTS, IAW SRM 57-51-02-2R-3. 88920U 21SEP20.

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 73,684 hrs · 44,016 cycles

MECHANICAL DAMAGE ON SEAT TRACK AT PASSENGER CABIN BS 520 LBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK AT PASSENGER CABIN FROM BS 480-520 LBL 25 WL 208, AS PER SRM 51-40-02-0G-0 AND DRAWING NR 143A5300. SEAT TRACK WAS EVALUATED AND FOUND TO BE OUT OF LIMITS L=1.2' D=0.034' ON TOP SURFACE OF THE CROWN, AS PER SRM 53-00-52-1A-1 STEP 4A FIG 103 DETAIL A.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 73,684 hrs · 44,016 cycles

PASSENGER CABIN FLOOR 241AF IS DAMAGED. PASSENGER CABIN FLOOR PANEL 241AF WITH DAMAGE WAS REPLACED WITH A SERVICEABLE FLOOR PANEL, PER SRM 51-10-02-0G-0 PARA 9A(1), DUE TO AMOUNT OF ALL DAMAGE.

Part: SKIN — CORRODED (BS 678-707) · airframe 73,684 hrs · 44,016 cycles

CORROSION ON EXTERNAL FUSELAGE SKIN UNDER ADF NR 1 ANTENNA BS678-BS707 S-1 TO S-2R WL306. REPAIRED CORROSION ON FUSELAGE SKIN UNDER ADF NR 1 ANTENNA AT BS 678 - BS 707 S-1 TO S-2R WL 306, PER ER 20-03231 REV IR ON SWA EA 20-153-01795 REV IR.

Part: ATTACH ANGLE — CRACKED (RT WING TE) · airframe 73,684 hrs · 44,016 cycles

RIGHT WING FIXED T/E PANEL LOWER WEB ATTACH ANGLE CRACKED; JUST IB OF DEFLECTION RIB ORSS278. MARKED / REMOVED AND REPLACED RIGHT WING FIXED T/E PANEL LOWER WEB ATTACH ANGLE. JUST IB OF DEFLECTION RIB P/N 115A6260-2 IAW. AIPC 57-42-51-02 AND SRM 51-40-02 88920U 11SEP20

Part: SKIN — DENTED (FUSELAGE) · airframe 73,684 hrs · 44,016 cycles

TRANSFERRED FROM CARD V262886=FUSELAGE EXTERNAL SKIN DENT AT STA. 1006 + 3.5'; 2.5' BELOW STR. 16R HAS ADDITIONAL GOUGE DAMAGE NOTED IN DENTED AREA. / FUSELAGE EXTERNAL SKIN DENT AT BS 1006+3.5' BELOW STRINGER 16R REPAIRED IAW EA 20-153-01763 REV IR AND ATS ER 20-03235 REV IR

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 73,684 hrs · 44,016 cycles

BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 18 WL 154. REMOVED BS 663 LOWER COMPOSITE BULKHEAD, IAW SRM 51-40-02-0G-0. FABRICATED LT VAPOR BARRIER PR BOE DWG 111A1151-3, REFER TO ATS BUILD SHEET 752673. ATS LOCATED AND DRILLED, IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-07-0G-0 AND DWG 111A1000 REV-B DWG 111A1001 REV-F.

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 73,684 hrs · 44,016 cycles

FLIGHT DECK FLOOR IS DENTED AT BS 255 RBL 4-LBL 14 WL 207.54. DENT ON FLIGHT DECK FLOOR AT BS 255 RBL 4 TO LBL 14. REPAIRED IAW EA NO: 1-A53-33179 REV 1. 55981U 22SEP20.

Part: COUNTER — FAILED (FIRST OFFICER'S) · airframe 73,339 hrs · 43,800 cycles

SMOKE COMING FROM FIRST OFFICER`S MEMORY COUNTER. COMPLIED WITH CONDITIONAL INSPECTION FOR SMOKE IAW AMM 05-51-56. REPLACED MEMORY COUNTER ON F/O'S SIDE IAW AMM 33-11-00.

Part: SLIDER — CRACKED (HORIZONTAL STAB) · airframe 73,219 hrs · 43,735 cycles

LEFT HORIZONTAL STABILIZER FWD UPPER SLIDER IS CRACKED AT ATTACH POINT AREA / REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER UPPER FWD SLIDER PER AMM 53-31-31.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,917 hrs · 43,543 cycles

OVER WING EMERGENCY EXIT LIGHT INOP. / REMOVED AND REPLACED OVERWING EMERGENCY EXIT LIGHT PER AMM 33-51-04

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 72,670 hrs · 43,374 cycles

LOWER WTB PANEL 193B HAS MISSING MATERIAL AND WEAR ON UPPER SURFACE PERIMETER FROM CONTACT WITH STRUCTURE. L/H O/B FWD CORNER DELAMINATED APPROX. .2' DEEP AND .7' LONG. / REMOVED AND REPLACED LOWER WTB PANEL 193B PER AMM 53-51-21.

Part: SKIN — CRACKED (BS 500C) · airframe 72,235 hrs · 43,090 cycles

DURING INSPECTION OF CHEM-MILLED AT STRINGER 4R AN INDICATION OF POSSIBLE CRACKS AT BS 500C +7 AND +11. REPAIRED FUSELAGE SKIN CRACKS AT BS 500C+7 AND +11", STR 4R PER ER #20-01371 REV IR AND EA #1-753-36434 REV IR.

Part: DOOR SILL — CRACKED (FWD SERVICE DOOR) · airframe 72,047 hrs · 42,972 cycles

FWD SERVICE DOOR SCUFF PLATE DAMAGED AT TWO HOLES / OK TO INSTALL SCUFF PLATE. 56155R 28DEC19 INSP 387 SCUFF PLATE WAS REMOVED AND REPAIRED ON EA 1-A53-2076 R11 (U118157). INSTALLED REPAIRED SCUFF PLATE IAW EA 1-A53-2076 REV.11

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,156 hrs · 42,402 cycles

LT EMERGENCY LIGHT INOP AT ROW 14. FOUND CONNECT ON UNPLUG ABOVE CEILING AND LIGHT ASSEMBLY BROKEN. R&R LIGHT ASSEMBLY AND CONNECTED PLUG IAW MM.

Part: FUEL CONTROL — FAULTY (APU) · airframe 70,547 hrs · 42,004 cycles

DIVERSION, AUXILIARY POWER UNIT GEN OFF BUS LIGHT ILLUMINATED IN FLIGHT DURING / USE SHOWS 0 VOLTS. R&R AUXILIARY POWER UNIT FUEL CONTROL UNIT PER AMM.

Part: SCUFF PLATE — CRACKED (FWD SERVICE DOOR) · airframe 70,383 hrs · 41,894 cycles

FWD GALLEY DOOR SCUFF PLATE IS CRACKED IN TWO PLACES MOD / ACCOMPLISHED WA 1-753-35352 REF LOG PAGE 1028671 FOR LT TLD

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 69,744 hrs · 41,480 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT LOCATION M1674 PER AMM 33-51-06

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,744 hrs · 41,480 cycles

EMERGENCY LIGHT OUT AT 6ABC RELAMPED PER AMM33-51-03

Part: SIGN — UNSECURE (L1 DOOR) · airframe 69,320 hrs · 41,193 cycles

L1 DOOR EXIT SIGN AT WILL NOT STAY ATTACHED. REATTACHED SIGN PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 69,154 hrs · 41,078 cycles

L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER AMM.

Part: FRAME — NONE (AFT PRESS BULKHE) · airframe 69,094 hrs · 41,040 cycles

PER SI# 12107-53 PAGE 10 STEP F HOLE SIZE SHOULD READ .3745-.3755; THE ACTUAL HOLE SIZE READ .385; MAKING IT OUT OF LIMITS. / REAMED OUT OF LIMITS HOLE TO A .390' PER SI# 12107-53 STEP 5. C. STR 2L HOLE 6L STA 1016 REF. FIG 5; NO DEFECTS NOTED INSTALLATION TO BE COMPLETED ON CUSTOMER CARD # 12107-53 STEPS 10. M. THRU 10. P.

Part: FRAME — NONE (EMPENNAGE) · airframe 69,094 hrs · 41,040 cycles

PER SI# 12107-53 PAGE 9 STEP D HOLE SIZE SHOULD READ .3745-.3755; THE ACTUAL HOLE SIZE READ .385; MAKING IT OUT OF LIMITS. / REAMED OUT OF LIMITS HOLE TO A .390' PER SI# 12107-53 STEP 5. A. AT STR 2L HOLE 5L STA 1016 REF. FIG 5; NO DEFECTS NOTED INSTALLATION TO BE COMPLETED ON CUSTOMER CARD # 12107-53 STEPS J10. M. THRU 10.P. 92385U 1/15/19

Part: CONNECTOR — LOOSE (CABIN) · airframe 69,094 hrs · 41,040 cycles

FORWARD LAV LOWER LT EMERGENCY EXIT INDICATOR LIGHT CONNECTOR LOOSE. SECURED LIGHT CONNECTOR IAW WDM & AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

SKIN CORRODED BETWEEN BS 914 TO BS 917, STR 23L. REPAIRED SKIN PER SRM & EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

SKIN CORRODED BETWEEN BS 937 TO BS 943, STR 23L. REPAIRED SKIN PER EA & ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

SKIN CORRODED BETWEEN BS 928 TO BS 929, STR 23L. REPAIRED SKIN PER EA AND ER.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

RT INTERCOSTAL DAMAGED BETWEEN BS 867 TO BS 887. R&R INTERCOSTAL IAW SRM AND DWG.

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

***CORROSION*** INTERCOSTAL IN AFT CARGO COMPARTMENT AT STA. 927-947 R/H SIDE HAS CORROSION AROUND MULTIPLE FASTENER HOLES WL 156 / CORROSION ON RH INTERCOSTAL (BAFFLE) BS 927-947 RBL 20 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED DAMAGED BAFFLE AND INSTALLED NEW BAFFLE IAW SRM 51-40-02; SRM 51-40-05 AND BOEING DRAWINGS 147A7500 & 147A7580

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

INTERCOSTAL CORRODED BETWEEN BS 747 TO BS 767, RBL 21. R&R INTERCOSTAL IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

SUPPLEMENTAL INFORMATION: L/H DOUBLER BRACKET CRACKED STA.663 BETWEEN LBL.15.54 AND LBL.24.92 WL.145 PN# 111A1512-1 / LOCATED & DRILLED NEW PART# 7570583 PO# 723763 (111A1312-1) IAW SRM 51-40-03-0G-0; DWG 111A1000; PART TO BE INSTALLED ON DEFECT CARD# N168110; COPY ATTACHED. 81146U 12/31/18

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

FRAME SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM & EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT PRESSURE BULKHEAD VERTICAL STIFFENER CORRODED AT BS 1016, BL 0. REPAIRED STIFFENER PER SRM, ER, AND EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT PRESSURE BULKHEAD WEB CORRODED AT BS 1018, BETWEEN RBL 6 TO LBL 6. REPAIRED WEB PER SRM & EA.

Part: FRAME — CORRODED (AFT FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

***CORROSION*** ON BS 1006 FRAME BL0 TO RBL 3 WL 186 / REMOVED CORROSION ON FUSELAGE FRAME AT STA. 1006 BL0 TO RBL3 WL 186. FOUND TO BE OUT OF LIMITS DUE TO CORROSION AROUND FASTENER HOLES IAW SRM 53-00-07-1A-1. REMOVED FRAME AT STA 1006 IAW SRM 51-40-02-0G-0. FORMED NEW FRAME PART WITH 7075-0 .063' CLAD SHEET LOT# 5040389 IAW SRM 51-30-01-0G-0 AND BOEING DWG 147A1006. INSTALLED NEW FRAME AT STA. 1006 IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A0040

Part: SEAT TRACK — CRACKED (FLIGHT DECK) · airframe 69,094 hrs · 41,040 cycles

CAPTAINS SEAT I/B FWD TRACK IS CRACKED ON THE AFT EDGE. / INSTALLED CAPTAINS SEAT I/B FWD SERVICABLE TRACK IAW AMM 25-11-11-400-801. 92570U 17DEC18

Part: STIFFENER — CRACKED · airframe 69,094 hrs · 41,040 cycles

_CRACKED STIFFENER AT BS 663 LBL 29 WL 155 / LOCATED AND DRILLED NEW STIFFENER AT BS 663 LBL 15 - LBL 32 WL 155 PO# 684835; PN 111A1301U5 TO BE INSTALLED ON COSTUMER CARD# N168110 PER SRM 51-40-05-0G-0 AND BOEING DWG# 111A1001. 59156U 27DEC2018

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO BAY LT Z-ANGLE CORRODED BETWEEN BS 727D TO BS 797, LBL 21. R&R SPLICE IAW DWG AND SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO BAY RT AFT Z-ANGLE CORRODED BETWEEN BS 887 TO BS 947.5, RBL 21. R&R Z-ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 942.5, RBL 14. R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 69,094 hrs · 41,040 cycles

RROSION*** AFT CARGO BAY TRANSITION STRIP CORRODED AT STA 887 LBL 9 - RBL 21 / AFT CARGO COMPARTMENT TRANSITION STRIP AT STA 887 LBL 9 - RBL 21 HAS CORROSION AND IS OUT OF LIMITS DUE TO NO LIMITS IAW SRM 53-00-53-1A-2; REMOVED AND REPLACED TRANSITION STRIP P/N-146A9401U21; P.O.# 5078451 IN AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A9401. 59156U 17JAN2019

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 727D+5, LBL 3. REPAIRED SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

FLOOR SUPPORT BEAM CORRODED AT BS 706, RBL 6. R&R BEAM IAW SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO BAY FLOOR SUPPORT SPLICE CORRODED AT BS 753.5, LBL 8. R&R SPLICE PER SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO DOOR CUT OUT SURROUND STRUCTURE, LOWER SUB THRESHOLD WEB CORRODED. R&R WEB IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 727D+5, RBL 3. REPAIRED SUPPORT IAW SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO BAY FLOOR SUPPORT SPLICE CORRODED AT BS 753.5, RBL 3. R&R SPLICE FILLER IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 903, RBL 8. R&R SUPPORT IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO BAY RT FORWARD Z-ANGLE CORRODED BETWEEN BS 727D TO BS 767, RBL 21. R&R Z-ANGLE IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 727D+5, RBL 8. REPAIRED SUPPORT IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

BULKHEAD LOWER BOLT ANGLE CORRODED AT BS 1016, BL 0. R&R ANGLE IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 904, LBL 3. R&R TRACK IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO COMPARTMENT BULKHEAD SUPPORT BRACKET CRACKED AT BS 737, RBL 9. R&R BRACKET IAW SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

AFT CARGO COMPARTMENT FORWARD SHIELD CORRODED RT, BETWEEN BS 767 TO BS 787. R&R SHIELD IAW SRM & DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,094 hrs · 41,040 cycles

LT HORIZONTAL STABILIZER NR 4 RIB STIFFENERS CRACKED AT STAB STA 120.3. REPAIRED RIB PER SRM.

Part: STIFFENER — CORRODED (EMPENNAGE) · airframe 69,094 hrs · 41,040 cycles

***CORROSION*** ON EXTERNAL STIFFENER STA 1037; BETWEEN STR 2L-2R UNDER VERTICAL STAB / REMOVED CORROSION ON EXTERNAL STIFFENER AFTER EVALUATION FOUND 100% MATERIAL LOSS AND WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED STIFFENER IAW SRM 51-40-02-0G-0. FABRICATED NEW STIFFENER LOT# 5078820-1 PO# 725807 IAW SRM 51-30-01-0G-0 AND BOEING DWG 69-69859. INSTALLED NEW STIFFENER IAW SRM 51-40-02-0G-0 AND BOEING DWG 148A3110. ON EXTERNAL STIFFENER STA 1037 BETWEEN STR 2L-2R 57042C 23JAN19

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,094 hrs · 41,040 cycles

RT HORIZONTAL STABILIZER NR 2 RIB STIFFENER CRACKED AT STAB STA 129.50. R&R STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,094 hrs · 41,040 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STA 129.50, NR 3 RIB STIFFENERS CRACKED. REMOVED STIFFENER IAW SRM.

Part: PANEL — CRACKED (VERTICAL STABILI) · airframe 69,094 hrs · 41,040 cycles

VERT STAB PANEL 323AR HAS CRACKED RETAINER AND IS WORN / FABRICATED NEW VERT STAB PANEL 323AR FROM COMPONENT PARTS PER SRM 51-40-02-0G-0 AND DRAWING 172A6122 REV B. PAINTED NEW PANEL TO MATCH ORIGINAL PER AMM 51-21-72-370-801 AND AMM 51-21-73-370-803

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 69,094 hrs · 41,040 cycles

LT HORIZONTAL STABILIZER RIB AT STAB STA 120.3, NR 3 RIB STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,094 hrs · 41,040 cycles

RT HORIZONTAL STABILIZER RIB NR 2 STIFFENER CRACKED AT STAB STA 92.7. REPAIRED STIFFENER IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 69,094 hrs · 41,040 cycles

LT HORIZONTAL STABILIZER RIB AT STAB STA 120.3, NR 2 RIB STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: SHIELD — CORRODED (FWD CARGO RH) · airframe 69,094 hrs · 41,040 cycles

***CORROSION*** FWD CARGO BAY R/H SIDE AFT SHIELD HAS CORROSION AT FASTENER HOLES FROM STA 500-500D RBL 26 / NO LIMITS FOUND IN SRM. REMOVED AND REPLACED SHIELD I-A-W SRN 51-40-02-0G-0. AND BDWG# 143A0080 PO# 723763 AT FWD CARGO BAY R/H SIDE AFT SHIELD.

Part: BEAM — CRACKED (FSD) · airframe 69,094 hrs · 41,040 cycles

FOUND FWD SERVICE DOOR #4 BEAM CRACKED AT I/B SIDE OF RADIUS. / REMOVED AND REPLACED THE R1 SERVICE DOOR DUE TO CRACKS FOUND ON CUSTOMER CARD# 14079 INSPECTION CARD ON CUSTOMER CARD# N167661

Part: BEAM — CRACKED (FSD) · airframe 69,094 hrs · 41,040 cycles

FOUND FWD SERVICE DOOR #5 BEAM CRACKED AT I/B SIDE OF RADIUS. / REMOVED AND REPLACED THE R1 SERVICE DOOR DUE TO CRACKS FOUND ON CUSTOMER CARD # 14079 INSPECTION CARD ON CUSTOMER CARD# N167661

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

FORWARD CARGO BAY RT SIDE AFT SIDEWALL FLOOR SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, BETWEEN STR 25R TO STR 26R. R&R SUPPORT IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

GUSSET CRACKED AT BS 500D, STR 21L. R&R GUSSET PER SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.

Part: VAPOR BARRIER — DELAMINATED (LT MLG WW) · airframe 69,094 hrs · 41,040 cycles

LT MAIN LANDING GEAR VAPOR BARRIER PREVIOUS REPAIR DELAMINATED AT BS 663. REPAIRED BARRIER PER SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

GUSSET CRACKED AT BS 500D, STR 22R. R&R GUSSET IAW SRM AND DWG.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 69,094 hrs · 41,040 cycles

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

Part: PANEL — CRACKED (RIGHT WING) · airframe 69,094 hrs · 41,040 cycles

RIGHT WING PANEL 623DB CRACKED. / FABRICATED NEW RT WING PANEL 623DB PER DRAWING 114A8131 REV A. INSTALLED NEW PANEL PER SOPM 20-50-01

Part: SKIN — CRACKED (SLAT) · airframe 69,094 hrs · 41,040 cycles

#5 LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIBS HAS WORKING FASTENERS / REMOVED WORKING FASTENERS IAW SRM 51-40-02-0G-0 AT #5 L/E SLAT NOSE SKIN AT ACTUATOR. FOUND CRACK ON O/B FASTENER HOLE. REMOVED AND REPAIRED L/E SLAT SKIN DAMAGE IAW SRM 57-42-01-2R-8

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 69,094 hrs · 41,040 cycles

LT HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 663, LBL 36. REPAIRED WEB PER EA AND ER.

Part: FAIRING — CRACKED (LOWER EXT FUSELA) · airframe 69,094 hrs · 41,040 cycles

BODY FAIRING 194GL CRACKED / REPAIRED CRACK ON BODY FAIRING 194GL IAW SRM 53-60-70-22-1 TABLE 201 + SRM 51-70-04-2R-0 + 51-70-04-2R-2. DAMAGE WAS BEYOND ALLOWABE LIMITS IAW SRM 53-60-70-1A-1 PARA 4. A. (1) DAMAGE WAS WITHIN 3' OR A FASTENER. 80733U 27DEC18

Part: PANEL — DELAMINATED (LEFT WING) · airframe 69,094 hrs · 41,040 cycles

DELAMINATION; AND EROSION AT 3 FWD CORNERS ON L/H WING L/E PANEL 521KB / REPAIRED DELAMINATION; AND EROSION AT 3 FWD CORNERS ON L/H WING L/E PANEL 521KB I.A.W. 737 SRM 57-41-01-1A-1 PARA 1; 4E TABLE 202; 250 DEGREE FAHRENHEIR CURE PER 737 SRM 51-70-05 REPAIR 10.

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 69,094 hrs · 41,040 cycles

DELAMINATION AT CORNER; R/H WING; L/E PANEL 621QB / REPAIRED DELAMINATION AT CORNER; R/H WING; L/E PANEL 621QB I.A.W. 737 SRM 57-41-01-2R-1 PARA 1 4E TABLE 202; 250 DEGREE FAHRENHEIT CURE PER 737 SRM 51-70-05 REPAIRE 10

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 69,094 hrs · 41,040 cycles

DELAMINATION; AND DAMAGED SCREW HOLE; AT FWD O/B CORNER ON R/H WING; L/E PANEL 621HB / REPAIRED DELAMINATION; AND DAMAGED SCREW HOLE AT FWD O/B CORNER ON RH WING L/E PANEL 621HB; I.A.W 737 SRM 57-41-01-2R-1; I.A.W 737 SRM 51-70-05-2R-0 I.A.W 737 SRM 57-70-05-2R-10; DAMAGE WAS PAST ALLOWABLE LIMITS I.A.W 737 SRM 57-41-01-1A-1 PARA 4A(5)(9)

Part: PANEL — DELAMINATED (LEFT WING) · airframe 69,094 hrs · 41,040 cycles

PAINT MISSING; AND EROSION AROUND SEVERAL SCREW HOLES; ON L/H L/E WING PANEL 521HB + DELAMINATION AT CORNER / REPAIRED EROSION AROUND SEVERAL SCREW HOLES; ON L/H L/E WING PANEL 521HB I.A.W. SRM 737-700 57-41-01-2R-1 AND 51-70-05-2R-10; DAMAGE WAS PAST ALLOWABLE LIMITS I.A.W 737-700 SRM 57-41-01-1A-1 PARA 4 A 1 (A)

Part: PANEL — DELAMINATED (LEFT WING) · airframe 69,094 hrs · 41,040 cycles

DELAMINATION AT FWD O/B CORNER ON L/H WING L/E PANEL 521UB / REPAIRED DELAMINATION AT FWD O/B CORNER ON L/H WING L/E PANEL 521UB I.A.W 737 SRM 57-41-01-2R PARA 1; 4E TABLE 202; 250 DEGREE FAHRENHEIT CURE PER 737 SRM 51-70-05 REPAIR. 10.

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 69,094 hrs · 41,040 cycles

DELAMINATION AT 3 CORNERS OF R/H WING; L/E PANEL 621JB / REPAIRED DELAMINATION AT 3 CORNERS OF R/H WING; L/E PANEL 621JB I.A.W 737 SRM 57-41-01-2R-1; I.A.W 737 SRM 51-70-05-2R-R0; I.A.W 737 SRM 51-70-05-2R-0; DAMAGE WAS PAST ALLOWABLE LIMITS I.A.W 737 SRM 51-41-01-1A-1 PARA 4A(5)(9)

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 69,094 hrs · 41,040 cycles

DELAMINATION AT CORNER ON R/H WING; L/E PANEL 621TB / REPAIRED DELAMINATION AT CORNER ON R/H WING; L/E PANEL 621TB I.A.W 737 SRM 57-41-01-2R-1 PARA 1; 4E TABLE 202; 250 DEGREES FAHRENHEIT CURE PER 737 SRM 51-70-05- REPAIR 10.

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 69,094 hrs · 41,040 cycles

DELAMINATION AT 3 FWD CORNERS OF R/H WING; L/E PANEL 621DB / REPAIRED DELAMINATION AT 3 FWD CORNERS OF R/H WING L/E PANEL 621DB I.A.W 737 SRM 57-41-01-2R-1; I.A.W 737 SRM 51-70-05-2R-0; I.A.W 737 SRM 51-70-05-2R-10; DAMAGE WAS PAST ALLOWABLE LIMITS I.A.W 737 SRM 57-41-01-1A-1 PARA 4A(5)(9)-.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LE FLAP) · airframe 68,497 hrs · 40,662 cycles

DECLARED EMERGENCY, WHILE CONFIGURING FOR LANDING WHEN FLAPS 2 WAS SELECTED THE NUMBER 7 LEADING EDGE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED. ADJUSTED PROXIMITY SENSOR IAW AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 67,738 hrs · 40,172 cycles

REAR RT ENTRY FLASH LIGHTS INOP. R&R FLASHLIGHT PER AMM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,580 hrs · 40,074 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,580 hrs · 40,074 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 66,903 hrs · 39,652 cycles

RIGHT OVERWING ESCAPE HATCH THRESHOLD EMERGENCY EXIT LIGHT LENS BROKEN. R & R THE LENS IAW AMM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 66,892 hrs · 39,645 cycles

R1 DOOR THRESHOLD EMERGENCY EXIT LIGHT LENS CRACKED. R & R THE LENS IAW AMM.

Part: HOOK — OUT OF ADJUST (R1 GIRT BAR) · airframe 66,729 hrs · 39,548 cycles

R1 DOOR SLIDE GIRT BAR RETAINER HOOK OUT OF ADJUST. ADJUSTED THE HOOK IAW AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 66,397 hrs · 39,358 cycles

FWD CARGO CENTER SCUFF PLATE CRACKED ON FWD END / REPAIRED FWD. CARGO CENTER SCUFF PLATE IAW SWA EA 1-A53-2076 REV 11.

Part: PANEL — DELAMINATED (RH PYLON) · airframe 66,397 hrs · 39,358 cycles

(DOT 3) #2 ENGINE PYLON PANEL 441EL IS CHARD AND DELAMINATED ON LOWER FWD INSIDE CORNER / REPAIRED DELAMINATION AT LOWER FWD INSIDE CORNER OF #2 ENGINE PYLON PANEL 441EL IAW B737 SRM 51-70-04-2R-6 AND RESTORED TOP COAT PER AMM 51-21-99-300-801

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,415 hrs · 38,731 cycles

FUSELAGE SKIN CRACKED AT BS 500B+9, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,415 hrs · 38,731 cycles

SKIN CRACKED AT BS 500D+9, STR 4R. REPAIRED SKIN IAW EA.

Part: COVER — OUT OF POSITION (L1 DOOR SLIDE) · airframe 65,336 hrs · 38,683 cycles

L1 DOOR SLIDE MANUAL DEPLOY HANDLE COVER OUT OF POSITION. POSITIONED THE SLIDE COVER IAW MT.

Part: COVER — OUT OF POSITION (L2 DOOR) · airframe 65,336 hrs · 38,683 cycles

L2 DOOR EMERGENCY EVAC SLIDE MANUAL DEPLOY HANDLE COVER OUT OF POSITION. REPOSITIONED COVER IAW MT.

Part: LENS — UNSECURE (CABIN) · airframe 65,239 hrs · 38,615 cycles

LIGHT LENS FELL OFF. REINSTALLED LENS PER SIP.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,822 hrs · 37,731 cycles

AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 23R. REPAIRED BULKHEAD PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,822 hrs · 37,731 cycles

AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 23L. REPAIRED BULKHEAD PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,495 hrs · 36,936 cycles

LT EMERGENCY BULLNOSE LIGHT INOP BETWEEN ROWS 14 TO ROW 23. R&R LAMP IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,495 hrs · 36,936 cycles

RT EMERGENCY BULLNOSE LIGHT INOP AT ROW 22. R&R LAMP IAW MM.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 62,495 hrs · 36,936 cycles

FUSELAGE STRINGER CLIP CRACKED AT BS 360, STRINGER 10L. R & R THE STRINGER CLIP IAW SRM.

Part: CREASE BEAM — CRACKED (BS 294) · airframe 62,495 hrs · 36,936 cycles

CREASE BEAM CRACKED AT BS 294, STRINGER 17R. REPAIRED THE CREASE BEAM IAW EA.

Part: FRAME — CORRODED (BS 907) · airframe 62,495 hrs · 36,936 cycles

AFT CARGO BAY LOWER LOBE FRAME CORRODED AT BS 907, BETWEEN LBL 3 TO RBL 3, LOWER EDGE. REMOVED THE FRAME IAW EA.

Part: ANGLE — CORRODED (BS 303-326) · airframe 62,495 hrs · 36,936 cycles

R1 DOOR THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 303 TO 326, RBL 59. R&R THE ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

WEB CORRODED. R & R THE WEB IAW SRM & DWG.

Part: PLATE — CRACKED (LT WING) · airframe 62,495 hrs · 36,936 cycles

LT WING TRAILING EDGE WAFFLE PLATE CRACKED AT OUTBOARD REAR SPAR STATION 261. R&R WAFFLE PLATE IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 62,495 hrs · 36,936 cycles

RT WING TRAILING EDGE WAFFLE PLATE CRACKED AT OUTBOARD REAR SPAR STATION 261, LOWER PANEL FORWARD. R&R WAFFLE PLATE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 62,495 hrs · 36,936 cycles

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

Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 62,495 hrs · 36,936 cycles

FLOOR SUPPORT CORRODED AT BS 767+5, RBL 8. REPAIRED THE SUPPORT IAW SRM AND EA.

Part: SHIELD — CORRODED (BS 420-440) · airframe 62,495 hrs · 36,936 cycles

FORWARD CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS 440 TO 420. REPAIRED THE SHIELD IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 62,495 hrs · 36,936 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 294 TO 312, RBL 15. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

AFT PIT FLOOR SUPPORT WEB FORWARD CORRODED AT BS 927+4, RBL 3. R&R WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 62,495 hrs · 36,936 cycles

CABIN FLOORBEAM CORRODED AT BS 328, RBL 32 TO 56. REPAIRED THE FLOORBEAM IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

LT CREASE BEAM CORRODED AT L2 DOOR. R&R CREASE BEAM IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

FORWARD CARGO COMPARTMENT GUSSET BRACKET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW AMM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

AFT WET AREA BULKHEAD STRAP CORRODED AT BS 1016 LBL 3. R&R STRAP IAW DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

AFT PIT FLOOR SUPPORT WEB CORRODED AT BS 927+4, LBL 3. R&R WEB IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

AFT PIT FLOOR SUPPORT CORRODED AT BS 727D+6, RBL 13.8. R&R SUPPORT IAW SRM & DWG.

Part: FRAME — CRACKED (BS 500B) · airframe 62,495 hrs · 36,936 cycles

FORWARD CARGO BAY FRAME CRACKED AT BS 500B, STRINGER 28L. REPAIRED THE FRAME IAW EA.

Part: ANGLE — CORRODED (BS 440-488) · airframe 62,495 hrs · 36,936 cycles

FORWARD CARGO BAY LT ZEE ANGLE CORRODED BETWEEN BS 488 TO 440. R & R THE ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 62,495 hrs · 36,936 cycles

FLOOR SUPPORT CORRODED AT BS 767+5, LBL 8. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 62,495 hrs · 36,936 cycles

FLOOR SUPPORT CORRODED AT BS 767+5, LBL 12. REPAIRED THE FLOOR SUPPORT IAW SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 62,495 hrs · 36,936 cycles

FLOOR SUPPORT CORRODED AT BS 767+5, LBL 3. REPAIRED THE FLOOR SUPPORT IAW SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 62,495 hrs · 36,936 cycles

FLOOR SUPPORT CORRODED AT BS 767+5, RBL 3. REPAIRED THE FLOOR SUPPORT IAW SRM AND EA.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

FORWARD CARGO COMPARTMENT FRAME FORWARD SIDE GUSSET BRACKET CRACKED AT BS 500D, STR 21R. R&R GUSSET IAW DWG AND SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

AFT PIT Z ANGLE CORRODED BETWEEN BS 847 TO BS 867, RBL 20. R&R Z ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (BS 294) · airframe 62,495 hrs · 36,936 cycles

R1 DOOR FORWARD FRAME CUTOUT CRACKED AT BS 294, RBL 54. REPAIRED IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

CREASE BEAM INNER CHORD ANGLE CORRODED BETWEEN BS 303 TO BS 354, LBL 57. R&R CREASE BEAM IAW DWG & SRM.

Part: WEB — CORRODED (BS 986-1006) · airframe 62,495 hrs · 36,936 cycles

AFT WET AREA RT WEB CORRODED BETWEEN BS 986 TO 1006. R & R WEB IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

AFT PIT FLOOR SUPPORT TEE ANGLE CORRODED AT BS 847, RBL 16. R&R TEE ANGLE IAW DWG AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

FRAME CRACKED AT BS 312, STR 6L. REPAIRED FRAME IAW EA.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

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

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

AFT PIT FLOOR SUPPORT WEB STRAP CORRODED AT BS 847, RBL 18. R&R STRAP PER DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

R2 DOOR AFT WET AREA RT CREASE BEAM CORRODED. R & R CREASE BEAM IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 488-500D) · airframe 62,495 hrs · 36,936 cycles

FORWARD CARGO BAY LT ZEE ANGLE CORRODED BETWEEN BS 488 TO 500D. R & R THE ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 500A-500D) · airframe 62,495 hrs · 36,936 cycles

FORWARD CARGO BAY RT FLOOR SUPPORT CORRODED BETWEEN BS 500A TO 500D. R & R THE FLOOR SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

FLOORBEAM AT CORRODED AT BS 986.6, BETWEEN RBL 28 TO RBL 45. R&R FLOOR BEAM IAW EA & SRM.

Part: CREASE BEAM — CORRODED (BS 300-353) · airframe 62,495 hrs · 36,936 cycles

CREASE BEAM INNER ANGLE CORRODED BETWEEN BS 300 TO 353, RBL 57. R&R CREASE BEAM IAW DWG AND SRM.

Part: SHIELD — CORRODED (BS 492-500A) · airframe 62,495 hrs · 36,936 cycles

FORWARD CARGO COMPARTMENT SHIELD CORRODED BETWEEN BS 492 TO 500A AFT RT SIDE. R & R THE SHIELD IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS 294 TO BS 312, RBL 30. R&R INTERCOSTAL IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 727D-727E) · airframe 62,495 hrs · 36,936 cycles

FLOOR SHIELD ZEE ANGLE CORRODED BETWEEN BS 727D TO 727E, LBL 22. R & R THE ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

AFT PIT FLOOR SUPPORT CORRODED AT BS 787 TO BS 807, RBL 14. R&R TRACK IAW SRM.

Part: FLOORBEAM — CORRODED (BS 727E) · airframe 62,495 hrs · 36,936 cycles

FLOORBEAM CORRODED AT BS 727E+3, BETWEEN LBL 3 TO RBL 8. REPAIRED THE FLOORBEAM IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 747-767) · airframe 62,495 hrs · 36,936 cycles

AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 747 TO 767, LBL 17. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 62,495 hrs · 36,936 cycles

AFT GALLEY CENTER EMERGENCY EXIT LIGHT BROKEN AT MOUNT. R & R THE LIGHT IAW AMM.

Part: ANGLE — CRACKED (RT WING) · airframe 62,495 hrs · 36,936 cycles

RIGHT WING AFT TRAILING EDGE CAVITY WEB SUPPORT ANGLE CRACKED. R & R THE ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 727C) · airframe 62,495 hrs · 36,936 cycles

FLOORBEAM ANGLE CORRODED AT BS 727C+6, LBL 8. R & R THE ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

AFT PIT FLOOR SUPPORT CORRODED BETWEEN BS 727 TO BS 867, RBL 13.8. R&R SUPPORT IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

AFT PIT FLOOR Z ANGLE CORRODED BETWEEN BS 747 TO BS 767, RBL 22. REPAIRED Z ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 767-787) · airframe 62,495 hrs · 36,936 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 767 TO 787, LBL 22. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 747-767) · airframe 62,495 hrs · 36,936 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 747 TO 767, LBL 22. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 747-767) · airframe 62,495 hrs · 36,936 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 747 TO 767, LBL 8. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

AFT PIT FLOOR SUPPORT WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 7. REPAIRED WEB IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,495 hrs · 36,936 cycles

RT INBOARD SEAT TRACK CORRODED BETWEEN BS 500C+9 TO BS 520. REPAIRED SEAT TRACK IAW SRM.

Part: SKIN — CRACKED (RT WING LE SLAT) · airframe 62,495 hrs · 36,936 cycles

RIGHT WING NR 6 L/E SLAT LOWER SKIN CRACKED AT ACTUATOR CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,495 hrs · 36,936 cycles

LT WING NR 2 SLAT LOWER NOSE SKIN AT ACTUATOR CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,495 hrs · 36,936 cycles

LT WING NR 3 SLAT LOWER NOSE SKIN AT ACTUATOR CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING LE SLAT) · airframe 62,495 hrs · 36,936 cycles

RIGHT WING NR 8 L/E SLAT LOWER SKIN CRACKED AT ACTUATOR CUTOUT. REPAIRED THE SKIN IAW EA.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 62,015 hrs · 36,637 cycles

BULKHEAD WEB CRACKED AT BS 663, BETWEEN LBL 31.83 TO LBL 24.92. REPAIRED THE BULKHEAD IAW EA.

Part: INDICATOR — FAULTY (FUEL SYS) · airframe 61,454 hrs · 36,301 cycles

BOTH CENTER FUEL PUMP LOW PRESSURE LIGHTS ILLUMINATED, NO DRAW FROM CENTER TANK. PRIMED CENTER TANK BOOST PUMPS PER AMM. RESET CENTER TANK BOOST PUMP UFI'S PER AMM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 60,340 hrs · 35,648 cycles

L1 DOOR SLIDE PRESS INDICATION LOW. R & R SLIDE ASSEMBLY IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,875 hrs · 35,382 cycles

LEFT EMER LIGHTING BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,875 hrs · 35,382 cycles

RIGHT EMER LIGHTING BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 58,266 hrs · 34,402 cycles

R2 DOOR EMER EVAC SLIDE PRESS INDICATOR LOW. R & R SLIDE IAW MT.

Part: BATTERY — FAILED (CABIN) · airframe 57,808 hrs · 34,133 cycles

EMERGENCY LIGHT BATTERY M01675 FAILED CAPACITY CHECK. R & R BATTERY IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 56,446 hrs · 33,338 cycles

EMERGENCY EXIT LIGHT LENS CRACKED. R & R LENS IAW SIP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 500A, STRINGER 8L TO 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 360, STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 500A, STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 727B, STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 727D, STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 440, STRINGER 8L TO 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 747, STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 867, STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 827, STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 480, STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 787, STRINGER 8L TO 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 520, STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

FUSELAGE FRAME CRACKED AT STATION 440, STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,350 hrs · 33,289 cycles

MAIN LANDING GEAR WW UPPER PRESS WEB, BS 665, RBL 40.50, WL 203 CRACKED. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 56,350 hrs · 33,289 cycles

MLG WW BULKHEAD WEB CRACKED AT STATION 663, RBL 34, WL 199. REPAIRED WEB IAW SRM.

Part: LATCH — CORRODED (LAV SERVICE) · airframe 56,350 hrs · 33,289 cycles

LOWER FUSELAGE AFT LAVATORY SERVICE DOOR 146AR, FWD D LATCH INNER SURFACE CORRODED. R & R LATCH IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, RBL 24.75. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 24.75. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 45. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,350 hrs · 33,289 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: SUPPORT ANGLE — CORRODED (OVERWING EXIT) · airframe 56,350 hrs · 33,289 cycles

LEFT OVERWING EXIT DOORWAY BOTTOM SUPPORT ANGLE CORRODED. REPAIRED ANGLE IAW EA.

Part: PLATE — CRACKED (LT WING) · airframe 55,852 hrs · 33,005 cycles

LEFT WING AFT SPAR BEHIND NR 1 ENG WIGGLE PLATE CRACKED. REPAIRED WIGGLE PLATE IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 55,852 hrs · 33,005 cycles

LEFT WING AFT SPAR BEHIND NR 1 ENG T BRACKET CRACKED. REPAIRED BRACKET IAW SRM.

Part: FLAP — CRACKED (RT WING) · airframe 55,852 hrs · 33,005 cycles

RIGHT WING FLAP CRACKED AT SUPPORT ANGLE FOR FIXED TE PANEL. R & R FLAP IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 55,852 hrs · 33,005 cycles

LEFT WING AFT SPAR BEHIND NR 1 ENG LOWER BULB SEAL BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: SWITCH — FAULTY (COCKPIT) · airframe 55,732 hrs · 32,948 cycles

FLIGHT DECK EMER EXIT LIGHT SWITCH FAULTY. R & R SWITCH IAW WDM.

Part: LENS — MISSING (EXIT SIGN) · airframe 53,912 hrs · 31,906 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOWER LENS COVER MISSING. INSTALLED COVER IAW MM.

Part: SUPPORT — CRACKED (VERTICAL STAB) · airframe 53,547 hrs · 31,691 cycles

RT VERTICAL STABILIZER FIN PANEL 324CR LOWER SUPPORT STRIP CRACKED. R & R STRIP IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,547 hrs · 31,691 cycles

R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LAMP INOPERATIVE. RELAMPED LAMP IAW MM.

Part: SUPPORT — CRACKED (VERTICAL STAB) · airframe 53,547 hrs · 31,691 cycles

RT VERTICAL STABILIZER FIN PANEL 323CR LOWER SUPPORT STRIP CRACKED. R & R STRIP IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,469 hrs · 31,645 cycles

R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 52,948 hrs · 31,329 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R & R SLIDE IAW AMM & MT.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 52,948 hrs · 31,329 cycles

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

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 52,508 hrs · 31,072 cycles

REPORTED SMELL OF JET A IN CABIN FROM ROW 13 AFT. R & R NR 1 ENGINE MAIN FUEL PUMP ASSEMBLY & HMU ASSEMBLY IAW MT.

Part: LENS — BROKEN (CABIN) · airframe 52,098 hrs · 30,807 cycles

R2 DOOR EMERGENCY EXIT LENS BROKEN. R&R LENS ASSEMBLY IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,894 hrs · 30,083 cycles

CAPTAINS WINDOW FRAME POST CRACKED AT UPPER OUTBOARD CORNER. REMOVED AND REPLACED FRAME PER ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,894 hrs · 30,083 cycles

RIGHT NR 3 COCKPIT WINDOW, E-F POST 2ND HOLE FROM BOTTOM CRACKED. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,223 hrs · 29,687 cycles

LEFT LOWER AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED IAW AMM. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,830 hrs · 29,451 cycles

RIGHT OVERWING EMERGENCY EXIT EXTERNAL FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EMERGENCY LIGHT RIGHT OVERWING EXTERNAL FUSELAGE, OPS CHECK GOOD IAW SWA B737-NG AMM 33-51-04 -960-401.

Part: SIGN — MISSING (CABIN) · airframe 48,988 hrs · 28,905 cycles

EMERGENCY EXIT SIGN MISSING AT ROW 12. INSTALLED SIGN PER MM.

Part: LIGHT — DIRTY (CABIN) · airframe 46,105 hrs · 27,169 cycles

DURING SCHEDULED CV CHECK, FOUND RT EEPLS STAINED AT ROW 16. CLEANED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,083 hrs · 26,013 cycles

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

Part: LENS — MISSING (CABIN) · airframe 43,938 hrs · 25,919 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,596 hrs · 25,724 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT EXTERIOR EMERGENCY EXIT SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 43,596 hrs · 25,724 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP BETWEEN ROW 9 TO ROW 19. FOUND CONNECTOR LOOSE. SECURED CONNECTOR PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,596 hrs · 25,724 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 30 TO RBL 45. REPAIRED BEAM PER SRM.

Part: WIRE — BROKEN (CABIN) · airframe 43,596 hrs · 25,724 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT EMERGENCY EXIT LIGHT WIRE BROKEN AT STA 609. REPAIRED WIRE PER WDM.

Part: COVER — LOOSE (CABIN) · airframe 43,659 hrs · 25,763 cycles

LT OVERWING EXIT DOOR EMERGENCY EXIT LIGHT COVER LOOSE. RE-SECURED COVER PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,596 hrs · 25,724 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT SKIN CORRODED AT BS 791, RBL 19.5. REPAIRED SKIN PER SRM AND BAC DWG.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 43,596 hrs · 25,724 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 85. REPAIRED SKIN PER SRM.

Part: SKIN — DETERIORATED (ELEVATOR TAB) · airframe 43,596 hrs · 25,724 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT ELEVATOR TAB UPPER SURFACE DETERIORATED. REPAIRED TAB PER MM & SRM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 42,803 hrs · 25,258 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,803 hrs · 25,258 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,803 hrs · 25,258 cycles

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

Part: COVER — BROKEN (L1 DOOR) · airframe 40,501 hrs · 23,927 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 39,427 hrs · 23,273 cycles

DURING SCHEDULED CV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT SIGN LOOSE AT ROW 11. SECURED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,239 hrs · 21,929 cycles

DURING SCHEDULED 10Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,239 hrs · 21,929 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT MLG WHEEL WELL SKIN CRACKED AT BS 663, LBL 35. REPAIRED SKIN PER AAR EA.

Part: ATTACH FITTING — CRACKED (CENTER WING) · airframe 37,239 hrs · 21,929 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FWD UPPER ATTACH FITTING CRACKED AT BS 540, LBL 6. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CRACKED (CENTER WING) · airframe 37,239 hrs · 21,929 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FWD UPPER ATTACH FITTING CRACKED AT BS 540, LBL 14. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CRACKED (CENTER WING) · airframe 37,239 hrs · 21,929 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FWD UPPER ATTACH FITTING CRACKED AT BS 540, LBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CRACKED (CENTER WING) · airframe 37,239 hrs · 21,929 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FWD UPPER ATTACH FITTING CRACKED AT BS 540, RBL 6. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 37,239 hrs · 21,929 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING O/B AFT FLAP I/B UPPER SURFACE DELAMINATED. REPAIRED AFT FLAP PER AAR EA.

Part: ATTACH FITTING — CRACKED (CENTER WING) · airframe 37,239 hrs · 21,929 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FWD UPPER ATTACH FITTING CRACKED AT BS 540, RBL 42. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 37,239 hrs · 21,929 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FWD UPPER ATTACH FITTING CRACKED AT BS 540, RBL 14. REMOVED AND REPLACED FITTING PER SRM.

Part: ATTACH FITTING — CRACKED (CENTER WING) · airframe 37,239 hrs · 21,929 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING TANK FWD UPPER ATTACH FITTING CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 36,171 hrs · 21,289 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 36,171 hrs · 21,289 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 36,171 hrs · 21,289 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: TRUNNION — CORRODED (RT MLG) · airframe 35,308 hrs · 20,750 cycles

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

Part: TRUNNION — CORRODED (LT MLG) · airframe 35,308 hrs · 20,750 cycles

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

Part: HOOK — LOOSE (GIRT BAR) · airframe 34,548 hrs · 20,282 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 33,791 hrs · 19,805 cycles

FLIGHT DECK L1 WINDOW ARCED AND WINDOW CRACKED. REMOVED AND REPLACED L1 WINDOW AND HEAT CONTROLLER PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 31,355 hrs · 18,323 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,551 hrs · 17,833 cycles

DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,237 hrs · 17,656 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 19 TO RBL 47. REMOVED AND REPLACED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,237 hrs · 17,656 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 5. REPAIRED FLOORBEAM PER SWA EA.

Part: POSITION SENSOR — FAULTY (NLG) · airframe 27,702 hrs · 16,201 cycles

AFTER TAKEOFF FROM LAX, RETRACTED GEAR, NLG GEAR DISAGREEMENT LIGHT ILLUMINATED. CYCLED GEAR, LIGHT STAYED ON. REMOVED AND REPLACED NLG POSITION SENSOR PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,937 hrs · 15,773 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVEWRWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: HOOK — SHEARED (L1 DOOR SLIDE) · airframe 26,627 hrs · 15,581 cycles

DURING SCHEDULED HC1 CHECK, FOUND RIVETS SHEARED ON L1 DOOR EMERGENCY EXIT EVAC SLIDE AFT HOOK. REMOVED AND REPLACED EVAC SLIDE RIVETS PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,526 hrs · 13,759 cycles

DURING SCHEDULED MV3 CHECK, FOUND CABIN EMERGENCY LIGHT INOP AT ROW 18 DEF. RELAMPED LIGHT PER MM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 21,909 hrs · 12,845 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT VERTICAL STABILIZER FITTING ATTACH ANGLE AT STA 1007, CRACKED. REPAIRED STABILIZER PER EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,877 hrs · 12,235 cycles

DURING SPV, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 18,655 hrs · 10,968 cycles

DURING SCHEDULED 5Y CHECK, FOUND LT HORIZONTAL STAB WEB AFT OF UPPER LUG CRACKED. REPAIRED WEB PER EA.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 18,340 hrs · 10,801 cycles

DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS LIGHT COVERS CRACKED. REMOVED AND REPLACED EEPLS LIGHT COVERS PER MM.

Part: LIGHT — CRACKED (FWD CABIN) · airframe 15,933 hrs · 9,488 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS SECTION CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS SECTION AT ROW NR 1 PER MM.

Part: COVER — CRACKED (CABIN) · airframe 14,783 hrs · 8,824 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW NR 2 AND ROW NR 21. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: SLIDE — LOOSE (AFT SVC DOOR) · airframe 14,268 hrs · 8,540 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 12,591 hrs · 7,568 cycles

DIVERSION, F/O FWD WINDSHIELD ARCHED, DELAMINATED, AND THEN CRACKED. REMOVED AND REPLACED R1 WINDOW AND WINDOW HEAT CONTROLLER PER MM.

Part: FUSE — MALFUNCTIONED (HYD SYSTEM) · airframe 12,387 hrs · 7,427 cycles

AIR TURNBACK, AFTER TAKEOFF L/E FLAPS WOULD NOT RETRACT. RESET HYD FUSES PER MM.

Part: BUSHING — WORN (LT/RT ELEVATOR) · airframe 12,368 hrs · 7,414 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS ON ALL HINGE ATTACH POINTS PER MM.

Part: MOTOR — FAILED (HORIZ STAB) · airframe 12,328 hrs · 7,383 cycles

AIR TURNBACK, INFLIGHT FAILURE OF BOTH NORM AND AUTOPILOT ELECTRIC PITCH TRIM. REMOVED AND REPLACED STAB TRIM MOTOR PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 10,020 hrs · 6,037 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT PRESS BULKHEAD OIL CANNED BETWEEN STR 5R AND 6R. MX FERRY TO PAE, REPAIRED BULKHEAD PER BFG ER.

Part: BUSHING — WORN (LT/RT ELEVATOR) · airframe 7,870 hrs · 4,791 cycles

DURING SCHEDULED C4 CHECK (SWA SI 11038-55), LT & RT ELEVATOR TAB FAILED FREE PLAY CHECK. R&R BOTH ELEVATOR TAB ATTACH FITTING BOLTS AND BUSHINGS.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 7,830 hrs · 4,758 cycles

DURING SCHEDULED SERVICE CHECK (SWA SI 11038-55), FOUND RT ELEVATOR TAB BUSHING WORN AT NR 4 HINGE POINT. R&R BUSHING PER D&M ENTERPRISES SSR #015.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 7,830 hrs · 4,758 cycles

DURING SCHEDULED CHECK (SWA SI 11038-55), FOUND LT ELEVATOR TAB BUSHINGS WORN AT NR 2, NR 3 & NR 4 HINGE POINTS. R&R BUSHINGS PER D&M ENTERPRISES SSR NR 015.

Part: SWITCH — INTERMITTENT (COCKPIT) · airframe 7,609 hrs · 4,641 cycles

EMERGENCY EXIT NOT ARMED LIGHT ILLUMINATING INTERMITTENTLY ON P-5 PANEL. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH PER MM.

Part: COVER — CRACKED (CABIN FLOOR) · airframe 6,851 hrs · 4,198 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD SECTION. REMOVED AND REPLACED TRACK COVER PER MM.

Part: NUT — LOOSE (ESCAPE SLIDE) · airframe 5,829 hrs · 3,598 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE MOUNT BOLT LOOSE AND WORN. REMOVED AND REPLACED ANCHOR NUT PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 5,829 hrs · 3,598 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED GIRT ASSY PER MM.

Part: WINDOW — UNSECURED (COCKPIT)

ABORTED TAKEOFF, CAPT'S SLIDING WINDOW OPENED DURING TAKEOFF, SPEED LESS THAN 40 KNTS. INSPECTED AND OPERATED CAPT'S SLIDING WINDOW PER MM. OPS CK GOOD, NO DEFECT NOTED.