N430WN

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 65,600 hrs · 38,663 cycles

ALL 4 EMERGENCY FLASHLIGHTS INOP. ALL NOT BLINKING. / [01] REMOVED AND REPLACED 4 EACH BATTERIES REF AMM 25-64-00

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 65,600 hrs · 38,663 cycles

ALL 4 EMERGENCY FLASHLIGHTS INOP. ALL NOT BLINKING. / [01] REMOVED AND REPLACED 4 EACH BATTERIES REF AMM 25-64-00

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 64,634 hrs · 38,101 cycles

SUPPLEMENTAL INFORMATION: 444BR AFT STRUT FAIRING DELAM. ; / [01] REMOVED AND REPLACED AFT STRUT FAIRING PANEL 444BR PER SRM 51-40-02

Part: TRANSMITTER — FAILED (TE FLAP SYS) · airframe 64,354 hrs · 37,930 cycles

FLAPS WOULD NOT MOVE TO COMMANDED POSITION WITH THE LEVER. FLAPS WENT TO APPROX 13 DEGREES AND HAD TO EXTEND TO 15 WITH ALTERNATE EXTENSION ; / [01] REMOVED AND REPLACED RIGHT FLAP POSITION TRANSMITTER IAW AMM 27-58-01. OPS CHECK NORMAL.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 63,960 hrs · 37,685 cycles

AFT LEFT ESCAPE SLIDE CASE HAS LOOSE SCREW ; / [01] RESECURED SLIDE CASE REF AMM 25-66-01

Part: RIVET — SHEARED (L1 GIRT BAR) · airframe 63,418 hrs · 37,357 cycles

CABIN L1 FWD. ENTRY DOOR GIRT BAR AFT STOW BRACKET NOT SECURE.(MARKED) / [01] FOUND RIVET SHEARED ON BRACKET. R&R FASTENER PER SRM 51-40-02

Part: BULB — INOPERATIVE (AFT GALLEY LIGHT) · airframe 63,367 hrs · 37,330 cycles

FLT ATTDT REPORTS AFT GALLEY LIGHT BURNT OUT WITH SCORCH MARKS AND ELECTRICAL SMELL. ; / [01] REMOVED AND REPLACED RH AFT GALLEY WORK LIGHT BULB PER MM 33-26-01; OPS CHECK GOOD. INSPECTED SOCKET ASSY WITH NO DEFECTS NOTED. PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION PER MM 05-51-56 WITH NO FURTHER DEFECTS NOTED. A/C OK FOR SERVICE.

Part: FAIRING — DAMAGED (FUSELAGE) · airframe 62,167 hrs · 36,652 cycles

193 FAIRING PANEL HAS MULITPLE ELONGATED HOLES (LOCATIONS 30-38) / REMOVED AND REPLACED PNL 193B REF SRM 51-40-02; AMM 53-51-21

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,499 hrs · 36,261 cycles

RIGHT EMERGENCY SLIDE GROUND LIGHT. L548 DOES NOT ILLUMINATE. RELAMPED RIGHT EMERGENCY SLIDE GROUND LIGHT L548. PERFORMED A GOOD FUNCTIONAL CHECK, PER AMM 33-51-04-960-801. 59234U 23OCT20.

Part: BRACKET — CORRODED (L2 DOOR GIRT BAR) · airframe 61,499 hrs · 36,261 cycles

CORROSION, THREE AFT ENTRY AND GALLEY GRIT BAR FLOOR BRACKETS IS CORRODED. THREE AFT ENTRY AND GALLEY GIRT BAR FLOOR BRACKETS FOUND TO BE OUT OF LIMITS AND THEY WERE REPAIRABLE BY REPLACEMENT, IAW SRM 51-10-02-0G-0 STEP 9C. REMOVED AND RELACED BRACKETS, IAW AMM 25-66-02-000-801 AND AMM 25-66-02-400-801. P/N 65-65972-3. INSTALLATION TEST IS GOOD.

Part: BUSHING — CORRODED (RT TRUNNION) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** RMLG FWD TRUNNION SUPPORT FITTING BUSHING O/B FACES ALL FOUR LOCATION S / REPAIRED BUSHING O/B FACES 4EA PER CC# 1-A57-3246; WORKED ACCOMPLISHED BY OUTSIDE VENDOR FAA FORM 8130-3 TRACKING # 805315 SWA WO# 31165

Part: PLATE — BROKEN (LT WING) · airframe 61,499 hrs · 36,261 cycles

LEFT WING T/E WIGGLE PLATE AT ORSS 375 HAS BROKEN PHENOLIC / REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE AT ORSS 375 P/N.115A3760-49 IAW.SRM 51-40-02 AND DWG 115A3700 88920U 10OCT20

Part: PLATE — CRACKED (LT WING) · airframe 61,499 hrs · 36,261 cycles

LEFT WING WIGGLE PLATE AT ORSS 404.0 IS BENT AND PHENOLIC IS CRACKED / REMOVED AND REPLACED LEFT WING WIGGLE PLATE AT ORSS 404.0 P/N 115A3760-13 IAW SRM 51-40-02 AND DWG 115A3700 AND DWG 115A3711 88920U 13OCT20

Part: SHEAR WEB — CRACKED (CABIN) · airframe 61,499 hrs · 36,261 cycles

SHEAR WEB CRACKED BS 986.5, LBL 45, WL 208. REMOVED AND REPLACED SHEAR WEB FROM BS 986.5 TO BS 1016 LBL 45, WL 208, IAW SRM 51-40-02 AND DWG 147A5600.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 61,499 hrs · 36,261 cycles

LT HORIZONTAL STAB RIB 120.30 HAS A CRACK ON THE 2ND VERTICAL STIFFENER FROM FWD AT LOWER END. TRIMMED OUT THE DAMAGE PART AT LT HORIZONTAL STAB RIB 120.30 2ND VERTICAL STIFFENER LOWER END AND INSTALLED REPAIR PARTS, IAW SRM 55-10-09-2R-4 88920U 06OCT20.

Part: PLATE — CRACKED (RT WING) · airframe 61,499 hrs · 36,261 cycles

FOUND R/H WIGGLE PLATE AT ORSS261 LWR FLANGE TO BE CRACKED / REMVOED AND REPLACED R/H WIGGLE PLATE AT ORSS261 LWR FRAMES P/N 115A2781-14 IAW. SRM 51-40-02 AND AIPC 57-50-00-30. 88920U 10OCT20.

Part: WEB — CRACKED (LT WING) · airframe 61,499 hrs · 36,261 cycles

LEFT WING FIXED T/E PANEL AFT OF NO.1 PYLON LOWER WEB HAS A CRACK AROUND FASTENER ORSS277. MARKED / REMOVED AND REPLACED L/H FIXED T/E UPPER PANEL LOWER WEB ORSS 277 IAW SRM 51-40-02-0G-0 57083U 03OCT20

Part: PLATE — CRACKED (LT WING) · airframe 61,499 hrs · 36,261 cycles

LEFT WING T/E WIGGLE PLATE IS CRACKED ORSS261. / REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE @ ORSS 261 COMMON TO T/E ACCESS PANEL 551GB IAW SRM 51-40-02-0G-0 CHEMICAL CONVERSION COATING APPLIED TO BARE METAL AREAS IAW AMM 51-21-41-370-802 PRIMER & DECORATIVE FINISH APPLIED IAW AMM 51-21-72-370-804 & IAW AMM 51-21-99-300-801. 57053U 04OCT20

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 61,499 hrs · 36,261 cycles

DAMAGED FLOOR SUPPORT AT B.S. 312-328; L.B.L. 47; W.L. 208.1. / FLOOR SUPPORT IS ELONGATED HOLE AND CRACKED THEREFORE FOUND TO BE OUT OF LIMIT PER REF B737 SRM 53-10-51-1A-1 PARAGRAPH IB. REMOVED AND REPLACED INTERCOSTAL PER REF SRM 51-40-02-0G AND DWG NBR 141A5400

Part: GATE — CRACKED (R2 DOOR) · airframe 61,499 hrs · 36,261 cycles

ASD LOWER GATE SKIN HAS A CRACK AT THE AFT EDGE / REMOVED AND REPLACED ASD LOWER GATE PER AMM 52-41-31-000-802 AMM 52-41-31-400-802; AMM 52-09-12-000-801; AMM 52-09-12-400-801; AMM 52-41-61-400-801; AMM 52-41-61-000-801; AMM 52-41-00-820-801; AMM 52-09-00-700-801 57803U 22OCT20

Part: SUPPORT ANGLE — CORRODED (BS 794) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ACB AT FASTENER IN THRESHOLD INTERCOSTAL SUPPORT ANGLE; BS 794; RBL 19; WL 155 / REMOVED AND REPLACED ON ACB AT FASTENER IN THRESHOLD INTERCOSTAL SUPPORT ANGLE. BS794; RBL19 WL155 IAW SRM 51-40-02 AND DWG 146A0082. 05OCT20

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ACB FLOOR TO SIDEWALL SUPPORT BS 727- 767; RBL 20; WL 157 / EVALUATED DAMAGE ON FLOOR TO SIDEWALL SUPPORT BS 727 - 767 RBL 20 WL 157 MORE THAN 50% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT BS 727-767 RBL 20 WL 157 P/N 7530898 PO# 803976 IAW SRM 51-40-02 REF DWG 146A7500 89004U 07OCT20

Part: SKIN — DENTED (BS 887) · airframe 61,499 hrs · 36,261 cycles

FUSELAGE SKIN HAS A DENT AT BS 887+16.5; 2.5' ABOVE S-9R. REPAIRED FUSELAGE SKIN DENT AT BS 887+16.5; 2.5' ABOVE S-9R, PER ER 20-03388 REV IR DATED 10-14-20 AND EA 20-153-01938 REV IR.

Part: SUPPORT ANGLE — CORRODED (BS 767-787) · airframe 61,499 hrs · 36,261 cycles

CORROSION ACB ON INTERCOSTAL SUPPORT ANGLE BELOW SIDE SHIELD; BS 767- 787; RBL 21; WL 157 / REMOVED AND REPLACED ACB ON INTERCOSTAL SUPPORT ANGLE BELOW SIDE SHIELD BS 767-787 RBL 21 WL 157 IAW SRM 51-40-02 REF DWG 146A8123 89004U 06OCT20

Part: SUPPORT FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 61,499 hrs · 36,261 cycles

CORROSION, FORWARD ENTRY DOOR GIRT BAR FITTING SUPPORT AT BS 344 LBL 55 WL 208.1. THIS ITEM DOES NOT HAVE ALLOWABLE DAMAGE. THEREFORE, WILL BE REPAIRED BY REPLACEMENT, PER SRM 51-10-02-0G-0 PARAGRAPH 9. 92462R 02OCT20 INSP 46 02OCT20. REMOVED FWD ENTRY DOOR GIRT BAR FITTING SUPPORT, PER SRM 51-40-02 92462R 02OCT20. INSTALLED NEW FWD ENTRY DOOR GIRT BAR FITTING SUPPORT AT BS 349 LBL 55 WL 208.1, PER REF SRM 51-40-02-0G AND DWG 141A5220.

Part: ATTACH ANGLE — CORRODED (BS 328) · airframe 61,499 hrs · 36,261 cycles

CORROSION ON ATTACH ANGLE AT MAIN EBAY BS328 LBL53 WL182. / REMOVED AND INSTALLED NEW ON ATTACH ANGLE AT MAIN EBAY BS328 LBL53 FROM BAC 1490-2503 #7075T62C PO# 804408 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-20-01; AND DWG 141A8140

Part: STRAP — CORRODED (BS 708) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON STRAP AT PASSENGER CABIN BS708 RBL65 WL202. / PAX CABIN STRAP AT BS 708 RBL 65 WL 202 REPAIRED IAW ATS ER 20-03397; REV IR; DATED 10-OCT-2020 AND PER EA NO: 20-153-01986 REV IR. 55981U 14OCT20

Part: FLOORBEAM — CORRODED (BS 486.5) · airframe 61,499 hrs · 36,261 cycles

CORROSION, ON FLOOR BEAM AT BS 986.5, RBL 38-44, WL 208.1. FLOOR BEAM AT BS 986.5 RBL 38-44 WL 208.1. DAMAGED AREA FOUND TO BE OUT OF LIMIT, DUE TO THE LOCATION OF THE DAMAGE BEING ON PREVIOUS REPAIR. THEREFORE, REPAIRED FLOOR BEAM AT BS 986.5 RT WL 208.1, IAW SRM 53-70-51-2R-4 REPAIR 4.

Part: ATTACH ANGLE — CRACKED (BS 692) · airframe 61,499 hrs · 36,261 cycles

CRACKED ATTACH ANGLE AT PASSENGER CABIN BS692 RBL1 WL207. / REMOVED & REPLACED ATTACH ANGLE AT PASSANGER CABIN BS692 RBL1 WL207 PER SRM 51-40-02-0G-0 & DWG# 273A9112

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 61,499 hrs · 36,261 cycles

PASSENGER CABIN FLOOR SUPPORT CRACKED BS 540 RBL 1 WL 208, MARKED. REMOVED AND REPLACED PASSENGER CABIN FLOOR SUPPORT BS 540 RBL 0-RBL 24 WL 208, IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A0060.

Part: STRAP — CORRODED (BS 713) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON STRAP AT PASSENGER CABIN BS713 RBL65 WL202. / PAX CABIN STRAP BS 713 RBL 65 WL 202 REPAIRED IAW ATS ER 20-03397; REV IR; 10-OCT-2020 AND PER EA NO: 20-153-01986 REV IR. 55981U 14OCT20

Part: ATTACH ANGLE — CORRODED (BS 320) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON ATTACH ANGLE AT MAIN EBAY BS320 LBL53 WL182. / REMOVED AND INSTALLED NEW ATTACH ANGLE AT MAIN EBAY BS320 LBL53 FROM BAC1490-2503# 7075T62C PO# 804408 LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 141A8143. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01; SRM 51-40-02; DWG 141A8140. 80641U 12OCT20

Part: STRAP — CORRODED (BS 694) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON STRAP AT PASSENGER CABIN BS694 LBL65 WL202. MARKED / PAX CABIN STRAP AT BS 694 LBL 65 WL 202 REPAIRED IAW ATS ER 20-03397; REV IR; DATED 10-OCT-2020 AND PER EA NO: 20-153-01986 REV IR. 55981U 14OCT20

Part: SUPPORT FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 61,499 hrs · 36,261 cycles

CORROSION, FORWARD ENTRY DOOR GIRT BAR FITTING SUPPORT AT BS 312 LBL 53 WL 208.1. THIS ITEM DOES NOT HAVE ALLOWABLE DAMAGE. THEREFORE, WILL BE REPAIRED BY REPLACEMENT, PER SRM 51-10-02-0G-0 PARAGRAPH 9. 92462R 02OCT20 INSP 46 02OCT20. REMOVED FWD ENTRY DOOR GIRT BAR FITTING SUPPORT, PER REF SRM 51-40-02 92462R 02OCT20. INSTALLED NEW FWD ENTRY DOOR GIRT BAR FITTING SUPPORT AT BS 312 LBL 53 WL 208.1, PER REF SRM 51-40-02-0G AND DWG 141A5220.

Part: SUPPORT — CORRODED (BS 727-727E) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ACB FLOOR TO SIDEWALL SUPPORT BS 727- 727E; LBL 20; WL 157 REJECTED DUE TO FASTENER NOT INSTALLED AT BS. 727 AT FWD END; LOWER SIDE AND B.S 747 FWD OF FRAME. / REMOVED - ACB FLOOR TO SIDEWALL SUPPORT INSTALLED FASTENER AT BODY STATION 727 AT FWD END; LWR SIDE AND BS 747 FWD AT FRAME REF BOEING DRAWING 146A0061 & BOEING DRAWING: 146A7500. 89931R 08SEP20

Part: CHANNEL — CORRODED (BS 950-995) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON AFT SERVICE DOOR MOP SILL AT B.S. 950-995; R.B.L. 52; W.L. 208.1. / REMOVED AND INSTALLED NEW AFT SERVICE DOOR MOP SILL AT B.S. 907- BS 995; RBL 52 WL 208.1 ITEM #7530246 IAW SRM 51-40-02-0G-0; SRM 53-70-15-1A-1; SRM 53-70-15-01-1; SRM 51-40-05-0G-0; DWG# 147A8501 57319U 10-06-20

Part: FLOORBEAM — CORRODED (BS 896) · airframe 61,499 hrs · 36,261 cycles

CORROSION, ON FLOOR BEAM AT BS 986.5, LBL 44, WL 208.1. FLOOR BEAM AT BS 986.5, LBL 44, WL 208.1. DAMAGED AREA FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 50% OF MATERIAL LOSS IN AN AREA OF .5' X .5'. THEREFORE; REPAIRED FLOOR BEAM AT BS 986.5 LT WL 208, IAW SRM 53-70-51-2R-4 REPAIR 4.

Part: CHANNEL — CORRODED (BS 950-986) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON AFT ENTRY DOOR MOP SILL AT B.S. 950-986; L.B.L. 52; W.L. 208.1. / REMOVED CORROSION ON AED MOPSILL BS 950-986 LBL 52 ORIGINAL THICKNESS .080' MAT LOSS MORE THAN 30% IN AN AREA OF 30' X-2'.0 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1; REMOVED AND REPLACED AED MOP SILL IAW SRM 51-40-02 DWG # 147A8501

Part: SHEAR WEB — CORRODED (BS 1028 LBL4) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON SHEAR WEB AT B.S. 1028; L.B.L. 4; W.L. 208.1. / SHEAR WEB AT B.S. 1028 LBL 4 REPAIRED IAW ATS ER 20-03382; REV IR; DATED 09-OCT-2020 AND PER EA NO: 20-153-01983 REV IR 55981U 20OCT20

Part: SHIELD — CORRODED (BS 767-787) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ACB FLOOR SIDE SHIELD BS 767- 787; RBL 22; WL 157 / REMOVED AND REPLACED AT ACB FLOOR SIDE SHIELD BS 767-787 RBL 22 P/N 146A8127U12 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 146A0081 80641U 8OCT20

Part: SHIELD — CORRODED (BS 854) · airframe 61,499 hrs · 36,261 cycles

CORROSION ACB SIDE SHIELD AT FASTENER HOLE BS 854; RBL21; WL 167 / REMOVED AND REPLACED ACB AFT SHIELD PER SRM 51-40-02; SRM 51-40-05 AND DWG. 146A0081. 91195U 10-6-20 SHIELD REPLACED AT STA.847-867 R/H SIDE WL167. 91195U 10-6-20

Part: FLOORBEAM — CORRODED (BS 794) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ACB IN FLOOR SUPPORT 'T' ANGLE; AT FASTENER; BS 794; RBL 18; WL 157 / REMOVED AND REPLACED ON ACB IN FLOOR SUPPORT 'T' ANGLE AT FASTENER BS794; RBL18; WL157. IAW SRM 51-40-02 AND DWG 146A7500 80641U 05OCT20

Part: SKIN — DENTED (BS 500D) · airframe 61,499 hrs · 36,261 cycles

FUSELAGE SKIN HAS A DENT ON THE PREVIOUS REPAIR FASTENER AT BS 500D+10'; 2' BELOW S-R7. REPAIRED FUSELAGE SKIN DISCREPANCY AREA OF BS 500D+10'; 2' BELOW STR 7R, IAW SRM.53-00-01-2R-3 88302U 05OCT20.

Part: CHANNEL — CORRODED (BS 312-344) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON FORWARD ENTRY DOOR MOP SILL AT B.S. 312-344; L.B.L. 55; W.L. 208.1. / REMOVED CORROSION ON FWD ENTRY DOOR MOPSILL; THE LOST MATERIAL IS MORE THAN 10% REMAINING THICKNESS IS .050' ORIGINAL THICKNESS IS .080' THEREFORE FOUND TO BE OUT OF LIMITS PER REF SRM 53-10-15-1A-1. REMOVED AND REPLACED FWD ENTRY DOOR MOP SILL AT BS 312-344 LBL 55 WL 208.1 PER REF SRM 51-40-02-0G AND DWG NBR 141A8110.

Part: STRAP — CORRODED (BS 1017-1030) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON TENSION STRAP AT B.S. 1017-1030; L.B.L. 3; W.L. 208.1. / REMOVED AND REPLACED TENSION STRAP BS1006 TO 1030 LBL3; WL208.1 DUE TO NO ALLOWABLE LIMIT; FOUND ON SRM FOR THIS PART IAW SRM 51-40-02 & REF DWG 147A5600 REV H DATED 03/04/08

Part: CARGO TRACK — CRACKED (BS 767) · airframe 61,499 hrs · 36,261 cycles

ACB CARGO FLOOR TRACK IS CRACKED. BS 767; LBL 17; WL 156 / REMOVED AND REPLACED ON ACB CARGO FLOOR TRACK BS727 TO BS 867 LBL17 WL156. RECEIVED NEW TRACK ITEM 7531208 PO# 804224. LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02; DWG 146A7500 AND DWG 149A8102 80641U 07OCT20

Part: STRAP — CORRODED (BS 713) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON STRAP AT PASSENGER CABIN BS713 LBL65 WL202. MARKED / PAX CABIN STRAP AT BS 713 LBL 65 WL 202 REPAIRED IAW ATS ER 20-03397; REV IR; DATED 10-OCT-2020 AND PER EA NO: 20-153-01986 REV IR. 55981U 14OCT20

Part: SHEAR WEB — CORRODED (BS 1016) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON SHEAR WEB AT B.S. 1016; L.B.L. 5; W.L. 208.1. / SHEAR WEB AT B.S. 1016; LBL 5 REPAIRED IAW ATS ER 20-03382; REV IR; DATED 09-OCT-2020 AND PER EA NO: 20-153-01983 REV IR. 55981U 20OCT20

Part: FLOOR SUPPORT — CRACKED (PAX CABIN) · airframe 61,499 hrs · 36,261 cycles

PASSENGER CABIN FLOOR SUPPORT CRACKED BS 540 LBL 1 WL 208, MARKED. REMOVED AND REPLACED PASSENGER CABIN FLOOR SUPPORT BS 540 LBL 0-LBL 24 WL 208, IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A0060.

Part: STRAP — CORRODED (BS 719) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON STRAP AT PASSENGER CABIN BS719 RBL65 WL202. / PAX CABIN STRAP AT BS 719 RBL 65 WL 202 REPAIRED IAW ATS ER 20-03397; REV IR; DATED 10-OCT-2020 AND PER EA NO: 20-153-01986 REV IR 55981U 14OCT20

Part: ANGLE — CORRODED (SERVICE PANEL) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ACB WATER SERVICE PAN; FWD ANGLE HAS CORROSION AND AFT ANGLE IS CRACKED. BS 907- 927; RBL 8- 18; WL 170 / REMOVED AND REPLACED 2EA ANGLES AT ACB WATER SERVICE PAN PER SRM 51-40-02; SRM 51-40-05 AND DWG. 147A7221. 91195U 10-9-20

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL157. / REMOVED AND INSTALLED NEW ON FLOOR TO SIDEWALL SUPPORT AT FCB BS500A-BS500D ITEM 7535472 PO#804777 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A7500. 80641U 08OCT20

Part: BONDING STRAP — CORRODED (RT WING) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON RIGHT WING REAR SPAR AROUND IB BOOST PUMP LOWER BONDING STRAP. MARKED IRSS 146; WBL 94.24; NO.2 TANK AFT / REMOVED CORROSION ON RIGHT REAR SPAR AROUND I/B BOOST PUMP LOWER BONDING STRAP AT IRSS 146; WBL 94.24; NO 2 TANK AFT IAW SWA EA 20-157-01994 REV IR AND ATS ER 20-03391 REV IR

Part: FORMER — CRACKED (RT WING FAIRING) · airframe 61,499 hrs · 36,261 cycles

CRACKED FAIRING FORMER ON RIGHT WING FIXED LEADING EDGE AT INBOARD END. / REMOVED CRACKED FAIRING FORMER AT R/H WING FIXED L/E I/B END PER SRM 51-40-02 AND LOCATED AND DRILLED REPLACEMENT FAIRING FORMER PER SRM 51-40-05 AND DWG. 116A3118. OK TO INSTALL. LEAD 113 10/6/20 8924C 06OCT20 INSTALLED FAIRING FORMER AT R/H WING FIXED L/E AT I/B END PER SRM 51-40-02 AND DWG. 116A3118. 91195U 10.7.20

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 61,499 hrs · 36,261 cycles

FWD FLOOR PANEL 222BF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. FWD FLOOR PANEL 222BF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE, PER SRM 51-10-02-0G-0 PARA 9A (1).

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 61,499 hrs · 36,261 cycles

FWD FLOOR PANEL 221BF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF DAMAGE TO PANEL 221BF REPLACED WITH NEW PANEL, IAW SRM 51-10-02-0G-0 PAR 9 AND AIPC 53-21-00-50D ITEM 50.

Part: FLOOR PANEL — PULLED (AFT CABIN) · airframe 61,499 hrs · 36,261 cycles

AFT FLOOR PANEL 241XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241XF WITH UPPER SKIN HAVING MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL, DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9A (1).

Part: SKIN — DENTED (BS 360) · airframe 61,499 hrs · 36,261 cycles

FUSELAGE SKIN HAS A DENT AT BS 360+5.5', 1' BELOW S-15R. FUSELAGE SKIN DENT AT BS 360+5.5'; 1' BELOW S-15R REPAIRED, IAW ATS ER 20-03377 REV IR DATED 21-OCT-2020 AND PER EA NR 20-153-02028 REV IR 55981U 21OCT20.

Part: FRAME — DENTED (BS 420) · airframe 61,499 hrs · 36,261 cycles

DENT ON FRAME AT FWD CARGO BAY BS 420 S-25R WL 159, MARKED. REPAIRED DENT ON FRAME AT FWD CARGO BAY BS 420 S-25R WL159, IAW ER 20-03381 REV IR DATED 16OCT20 & EA 20-153-02022 REV IR.

Part: FLOOR PANEL — DENTED (AFT CABIN) · airframe 61,499 hrs · 36,261 cycles

AFT FLOOR PANEL 241AEF UPPER SKIN HAS LARGE DENT NEAR CUT-OUT. (MARKED) REPAIRED LARGE DENT NEAR CUT-OUT ON UPPER SKIN AND ADDITIONAL PUNCTURE DAMAGE FOUND ON LOWER SKIN ON AFT FLOOR PANEL 241AEF IAW SRM 53-00-50-2R-2 AND SRM 53-00-50-2R-4.

Part: SUPPORT ANGLE — CORRODED (BS 500D) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL25 WL157. / NO ALLOWABLE DAMAGE FOUND ON SRM; PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02. REMOVED AND REPLACED ACB AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE BS 500D L/H IAW SRM 51-40-02 REF DWG 143A7902 AND DWG 143A9481 89004U 14OCT20

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FWD CARGO BAY BS500D RBL25 WL157. / CORROSION ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FCB BS 500D RBL 25 WL 157 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM NEED TO REMOVE AND REPLACE IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE BS 500D RBL 25 WL 157 PN# 143A9485-34; PO # 803019 IAW DWG # 143A9481. AND IAW DWG # 143A7902

Part: FLOOR PANEL — PULLED (AFT CABIN) · airframe 61,499 hrs · 36,261 cycles

AFT FLOOR PANEL 241YF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF DAMAGE TO PANEL 241YF. REPLACED WITH NEW PANEL, IAW SRM 51-10-02-0G-0 PAR 9 AND AIPC 53-21-00-26 ITEM 66.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS500D LBL23 WL157. / REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS 400-BS 500D LBL 23 WL 157 IAW SRM 51-10-02. MAX MATERIAL REMOVED IN AREA OF 10LX2.5'W X 50% MATERIAL LOSS WICH IS OUT OF LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. REMOVED AND REPLACED NEW FLOOR TO SIDEWALL SUPPORT CHANNEL FROM BS 396 - BS 500D LBL 21.80. PN # 143A7501-80; PO# 805160 IAW SRM 51-40-02 AND IAW DWG # 143A7500

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 61,499 hrs · 36,261 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL155. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT STA. 500C LBL 25 FWD SIDE PER SRM 51-40-02; SRM 51-40-05 AND DWG. 143A7502. 91195U 10-9-20

Part: GUSSET — DAMAGED (FWD CARGO) · airframe 61,499 hrs · 36,261 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET HAS DAMAGE BS500D S-21R WL166. MARKED / REMOVED AND INSTALLED ON FCB AFT BULKHEAD SUPPORT GUSSET BS 500D S-21R WL 166 ITEM HFAB53-GU-011 PO # 804930 LOCATED AND DRILLED IAW SRM 51-40-05. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01; SRM 51-40-02 AND DWG 143A7902; DWG 143A9483 80641U 13OCT20

Part: GUSSET — CRACKED (FWD CARGO) · airframe 61,499 hrs · 36,261 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED AND REPLACED GUSSET AT STA. 500D STR 19L PER SRM 51-40-02; SRM 51-40-05 AND DWG. 143A7902. 91195U 10-10-20

Part: FLOORBEAM — CORRODED (FWD CARGO) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON DOUBLER AT FWD CARGO BAY BS500A+12 BL0 WL148.5. / REMOVED CORROSION ON DOUBLER AT FWD CARGO BAY BS500A+12' BL0 WL148.5 MORE 100% MATERIAL LOSS IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02. REMOVED AND REPLACED DOUBLER P/N 143A3233-4. PO# 786098/1 IAW SRM 51-40-02 AND DWG 143A3230.

Part: FRAME — DENTED (BS 460) · airframe 61,499 hrs · 36,261 cycles

DENT ON FRAME AT FWD CARGO BAY BS 460 LBL 28 WL 158, MARKED. REPAIRED FRAME AT FCB BS 460 LBL 28 WL 158, IAW SRM 53-30-07-2R-1 REPAIR 1.

Part: SHIELD — CORRODED (BS 420-440) · airframe 61,499 hrs · 36,261 cycles

CORROSION ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL23 WL157. / REMOVED AND REPLACED FWD SHIELD OF FWD CARGO BAY BS420-BS440 RBL23 PER SRM 51-40-02 AND DWG 143A0080

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL23 TO RBL23 WL157. / CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FCB BS 500D LBL 23 TO RBL 23 WL 157 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM USED TO REMOVE AND REPLACE IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS 500D LBL23. TO RBL 23 WL 157 PO # 803907 IAW DWG # 143A9481 AND IAW DWG # 143A7902.

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 61,499 hrs · 36,261 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE RBL25 WL155. / REMOVED & REPLACED INTERCOSTAL ATTACH ANGLE P/N 143A7502-14 AT FWD CARGO BAY BS 500C FWD SIDE RBL 25 WL 155 IAW SRM 51-40-02-06-0 & DRW 143A7505

Part: SHIELD — CORRODED (BS 500-500A) · airframe 61,499 hrs · 36,261 cycles

CORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL157. / REMOVED & REPLACED NEW SHIELD P/N 143A8126-19 AT FWD CARGO BAY BS 500-BS 500A RBL 23 WL 157 IAW SRM 51-40-02-0G-0 & DRW 143A0080

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 61,499 hrs · 36,261 cycles

FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 222CF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED, IAW SRM 53-00-50-2R-1.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 61,499 hrs · 36,261 cycles

LT HORIZONTAL STAB RIB ASSEMBLY 4 (STAB STA 120.30) 3RD STIFFENER FROM FWD CRACKED. TRIMMED OUT THE DAMAGE PART AT LT HORIZONTAL STAB RIB 120.30 3RD VERTICAL STIFFENER LOWER END AND INSTALLED REPAIR PARTS, IAW SRM 55-10-09-2R-4 88920U 06OCT20.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 61,499 hrs · 36,261 cycles

CRACK ON LOWER SURFACE OF THE LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIB ON #4 SLAT. / REMOVED; INSTALLED SERVICEABLE # 4 SLAT; ADJUSTED AND FUNCTIONAL TESTED IAW MM 27-81-21-000-801; MM 53-81-21-400-801 AND MM 27-81-00-820-803 ADJUSTMENT AND FUNCTIONAL CHECK GOOD (POS: 4; TAG/NO.: 749174; P/N OFF: 114A5040-3; S/N OFF: 001259; P/N ON: 114A5040-3; S/N ON: 001259)

Part: SKATE ANGLE — CHAFED (BS 1019) · airframe 61,499 hrs · 36,261 cycles

FUSELAGE UPPER EXTERIOR L/H AFT CLOSURE SKATE ANGLE IS CHAFED AT BS 1019; LBL 11. / REPAIRED FUSELAGE UPPER EXTERIOR L/H AFT CLOSURE SKATE ANGLE FROM BS 1016 TO BS 1019 IAW SRM 53-80-71-2R-6 REP 6

Part: SKIN — DEBONDED (TAILCONE) · airframe 61,499 hrs · 36,261 cycles

AFT TAIL CONE 544EB LOWER OUTER SKIN NEAR FWD EDGE IS DISBONDED, MARKED. REPAIRED DISBOND ON PANEL 544EB AFT TAIL CONE LOWER OUTER SKIN FWD EDGE, IAW SRM 57-53-01; SRM 51-70-05-2R-1; AMM 51-21-71; AMM 51-21-99.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 61,499 hrs · 36,261 cycles

LT HORIZONTAL STAB RIB ASSEMBLY 4 (STAB STA 120.30) 4TH STIFFENER FROM FWD CRACKED. TRIMMED OUT THE DAMAGE PART AT LT HORIZONTAL STAB RIB 120.30 4TH VERTICAL STIFFENER LOWER END AND INSTALLED REPAIR PARTS, IAW SRM 55-10-09-2R-4 88920U 06OCT20.

Part: RIB — CRACKED (HORIZONTAL STAB.) · airframe 61,499 hrs · 36,261 cycles

RT HORIZONTAL STAB NR 9 RIB IS CRACKED AT THE LOWER END OF NR 3 STIFFNER. REPAIRED RT HORIZONTAL STAB NR 9 RIB AT THE LOWER END OF NR 3 STIFFENER, IAW SRM 55-10-09-2R-4 89004U 03OCT20.

Part: SKATE ANGLE — CHAFED (BS 1125) · airframe 61,499 hrs · 36,261 cycles

FUSELAGE UPPER EXTERIOR R/H AFT CLOSURE SKATE ANGLE IS CHAFED AT BS 1125; RBL 11. / REPAIRED AT FUSELAGE UPPER EXTERIOR R/H AFT CLOSURE SKATE ANGLE FROM BS 1125 TO BS 1132.5 IAW SRM 53-80-71-2R-6 REP 6 HFEC AREA NO DEFECT NOTED PER 737 NDTM PART 6 51-00-00 PROC 23.

Part: SKATE ANGLE — CHAFED (BS 1008) · airframe 61,499 hrs · 36,261 cycles

FUSELAGE UPPER EXTERIOR R/H FWD CLOSURE SKATE ANGLE IS CHAFED AT BS 1008; RBL 11. / REMOVED & REPLACED FUSELAGE UPPER EXTERIOR RH FWD CLOSURE SKATE ANGLE BS 1006 TO BS 1016 IAW SRM 51-40-02-0G-0 & DRW 147A0030

Part: BONDING STRAP — CORRODED (RT WING) · airframe 61,499 hrs · 36,261 cycles

***CORROSION*** RH WING FWD BOOST PUMP AT UPPER BONDING STRAP APPROX LE STA 124 IFSS 120.00 WBL 94.24 / REPAIRED RH WING FWD BOOST PUMP AT UPPER BONDING STRAP APPROX LE STA 124 IFSS 120.00 WBL 94.24 IAW SWA EA 20-157-02051 REV IR AND ATS ER 20-03390 REV IR

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 61,499 hrs · 36,261 cycles

FLIGHT DECK FLOOR IS DENTED AT BS 255, LBL 14, WL 207.45. REPAIRED DENTED FLIGHT DECK FLOOR AT BS 255 LBL 14 WL 207.45, IAW EA 1-A53-33179 REV 1.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 61,456 hrs · 36,239 cycles

FOUND TWO CRACKS APPROXIMATELY 7 INCHES LONG ON FWD CARGO FLOOR PANEL 120 CF THAT EXCEED DAMAGE LIMITS PER AMM 53-00-53. DMAGE LOCATED AT APPROX. STATION 500. / PANEL 120CF REMOVED IAW MM 25-52-10 INSTALLED SERVICEABLE PANEL (FWD CARGO FLOOR PNL 120CF) IAW AMM 25-52-10

Part: RADOME — DAMAGED (NOSE) · airframe 61,016 hrs · 35,984 cycles

NOSE RADOME DAMAGED / R & R NOSE RADOME IAW PER AMM REF 53-52-00 POS P TAG 590176 P/N OFF/ON 1001002-7B S/N OFF C193859-07 S/N ON C156692-03

Part: SUPPORT ANGLE — CRACKED (NR 1 NACELLE) · airframe 60,946 hrs · 35,934 cycles

#1 ENGINE I/B COWL OIL SERVICE DOOR SUPPORT ANGLE CRACKED / REMOVED AND REPLACED PER FAN COWL AMM. 71-11-02 TAG NO: 715180 PN ON: 314-2200-17 SN ON: 8025001 PN OFF: SN OFF: 5053001

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,946 hrs · 35,934 cycles

EMERGENCY EXIT LIGHT FWD OF LT OVERWING EXIT HAS INOP BULBS. RELAMPED EMERGENCY EXIT LIGHTS PER AMM 33-51-04.

Part: COMPUTER — FAULTY (E&E BAY) · airframe 60,594 hrs · 35,712 cycles

ON DEPARTURE; AUTOTHROTTLE COMMANDO FULL THRUST@ 1000'ALL AIRSPEED WINDOW WOULD NOT OPEN. ON APPROACH A/C WENT INTO UNCOMMANDED TOGA / T/S FOUND NO FAULTS ON FML;DFCS;A/T TESTS. FOUND CAPTS TOGA SWITCH STICKING. REMOVED AND REPLACED REF AMM 22-11-39. REPLACED AUTOTHROTTLE COMPUTER REF AMM 22-31-00. ALT OPS NORMAL AT THIS TIME. POS ONLY P/N 760SUE2-5 S/N OFF AT00734 _______________________S/N AT01464

Part: ATTACH FITTING — CRACKED (SLAT ACTUATOR) · airframe 60,203 hrs · 35,450 cycles

#2 LEADING EDGE SLAT ACTUATOR ATTACHE POINT EVIDENCE OF CRACKS EMINATING FROM FASENER HOLES / REMOVED AND REPLACED #2 SLAT; RIG AND OPS CHECKED OK PER M/M 27-81-21 POS#2 PN; 114A5020-3 SN OFF; 00128 SN ON; 001506

Part: CARGO TRACK — CRACKED (AFT CARGO BAY) · airframe 61,499 hrs · 36,261 cycles

ACB CARGO FLOOR TRACK IS CRACKED BS 747, RBL 13, WL 156. REMOVED AND REPLACED ACB CARGO FLOOR TRACK BS 727- BS 887 SPLICE LOCATED AT BS 755 RBL 13 WL 156, IAW SRM 51-40-02-0G-0; SRM 53-00-53-2R-3 AND BOEING DWG 146A7500.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 59,620 hrs · 35,054 cycles

L2 DOOR SLIDE NEEDED REPACK DUE TO EXPOSED PULL TAB. / R&R SLIDE ASSEMBLY PER MT.

Part: COVER — INCORRECT (R1 DOOR SLIDE) · airframe 57,287 hrs · 33,554 cycles

R1 DOOR SLIDE COVER OVER MANUAL INFLATION HANDLE NOT INSTALLED CORRECTLY. CORRECTLY INSTALLED COVER PER CMM AND MT.

Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 57,287 hrs · 33,554 cycles

L2 DOOR SLIDE GIRT OUT OF POSITION. REPACKED GIRT ASSEMBLY PER MT AND CMM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 57,287 hrs · 33,554 cycles

RT HORIZONTAL STAB LOWER FORWARD SLIDING SEAL CRACKED AND DEFORMED AT UPPER FITTING. / R&R HORIZONTAL STAB LOWER FORWARD SLIDING SEAL IAW AMM 53-31-31.

Part: COVER — LOOSE (L1 DOOR) · airframe 56,563 hrs · 33,090 cycles

L1 DOOR SLIDE MANUAL HANDLE COVER LOOSE. SECURED COVER PER MT.

Part: COVER — CRACKED (AILERON RH) · airframe 56,053 hrs · 32,754 cycles

RIGHT HAND WING AILERON TAB HINGE COVERS CRACKED 2 EA / REMOVED & REPLACED RIGHT HAND WING AILERON TAB HINGE COVERS IAW AMM 27-11-21-000-801 & AMM 27-11-21-400-801. ADJUSTMENT CK AND OPS CK WILL BE ACCOMPLISHED ON CUSTOMER CARD #N166531

Part: FITTING — CRACKED (LE SLAT) · airframe 56,053 hrs · 32,754 cycles

RT WING NR 6 SLAT ACTUATOR FITTING CRACKED. R&R NR 6 SLAT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,053 hrs · 32,754 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOP. R&R LAMP PER AMM.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

A/C PACK BAY LOWER CHORD DAMAGED FROM DOOR LATCH AT BS 548, RBL 47. REPAIRED CHORD IAW ER AND EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

FT CARGO COMPARTMENT DOOR FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 787, STR 25R. R&R SHIELD IAW SRM AND DWG.

Part: SKIN — CRACKED (TE FLAP) · airframe 56,053 hrs · 32,754 cycles

RT WING INBOARD AFT FLAP CRACKED ON LOWER SURFACE. REPAIRED AFT FLAP IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

AFT CARGO RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767. R&R SUPPORT IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUEL TANK) · airframe 56,053 hrs · 32,754 cycles

RT CENTER WING FUEL TANK UPPER ATTACH ANGLE CRACKED AT BS 663, RBL 7. REPAIRED ANGLE PER EA & ER.

Part: ATTACH ANGLE — CRACKED (FUEL TANK) · airframe 56,053 hrs · 32,754 cycles

LT CENTER WING FUEL TANK UPPER ATTACH ANGLE CRACKED AT BS 663, LBL 7. REPAIRED ANGLE PER EA AND ER.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

AFT CARGO LT Z CHANNEL CORRODED BETWEEN BS 727 TO BS 807, LBL 20. R&R SUPPORT IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

AFT CARGO TOP OF FLOOR RAIL CORRODED AT BS 945, RBL 3. REPAIRED FLOOR RAIL IAW SRM.

Part: PANEL — CORRODED (AFT CARGO COMPT) · airframe 56,053 hrs · 32,754 cycles

***CORROSION*** AFT CARGO DOOR SURROUND AFT CLOSEOUT PANEL STA 847-867 / REMOVED AND REPLACED AFT CARGO DOOR SURROUND AFT CLOSEOUT PANEL IAW SRM 51-40-02-0G-0 SI# 7531255 MPN# 146A8127Y10 AND BOE DWG 146A0081 56844U 14NOV18

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

AFT CARGO RT Z CHANNEL CORRODED BETWEEN BS 947 TO BS 887, RBL 20. R&R SUPPORT IAW SRM DWG.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 56,053 hrs · 32,754 cycles

***CORROSION*** AFT CARGO BULKHEAD ATTACH ANGLE STA 947 LBL10-RBL20 / OUT OF LIMITS DUE TO NO LIMITS FOUND IN SRM REMOVED AND REPLACED NEW AFT CARGO BULKHEAD ATTACH ANGLE STA 947 LBL10-RBL20 I-A-W SRM 51-40-02-0G-0. PO#693895 AND BOEING DRAWING #149A8118

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

AFT CARGO T RAIL CORRODED AT BS 887, BETWEEN LBL 3 TO RBL 13. R&R TEE ASSEMBLY IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

AFT CARGO TOP OF TRACK CORRODED AT BS 945, RBL 13. R&R SUPPORT PER SRM & DWG.

Part: PANEL — CORRODED (AFT CARGO) · airframe 56,053 hrs · 32,754 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** AFT CARGO DOOR SURROUND FWD CLOSEOUT PANEL STA 784-794 / WORK ACCOMPLISHED ON CUSTOMER JOB CARD #N166958 WORK COPY ATTACHED

Part: RAIL — CORRODED (FWD CARGO COMPT) · airframe 56,053 hrs · 32,754 cycles

***CORROSION*** BS 500D AFT BULKHEAD LWR T CHORD CORRODED NUMEROUS FASTENERS / BLENDED OUT CORROSION AT STA 500D AFT I-A-W SRM 51-10-02-0G-0. L=1' W=1' NO LIMITS FOUND IN SRM REMOVED AND REPLACED NEW LWR RAIL SUPPORT I-A-W SOPM 20-50-01. PO# 708714

Part: SHIELD — CORRODED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

RT INTERCOSTAL SHIELD CORRODED BETWEEN BS 500+12 TO BS 500A. R&R SHIELD IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

AFT CARGO SILL WEB CORRODED ON UPPER SURFACE. R&R WEB PER SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

FORWARD CARGO DOOR SILL WEB CORRODED. R&R WEB IAW SRM AND DWG.

Part: STRAP — CRACKED (AFT CARGO COMPT) · airframe 56,053 hrs · 32,754 cycles

***CORROSION*** AFT CARGO AT STA 794+4' ABOVE S-25 R ON BOTTOM OF FLOOR SUPPORT STRAP HAS CORROSION AROUND NUT PLATES (MARKED) / NO LIMITS FOUND IN SRM REMOVED AND REPLACE W/NEW BOTTOM SUPPORT STRAP I-A-W SRM 51-40-02-0G-0 AT AFT CARGO STA 794+4 ABOVE STR 25R PO#715403 BOEING DRAWING #146A8128

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,053 hrs · 32,754 cycles

LT HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 663+2, LBL 32. REPAIRED DECK WEB PER EA AND ER.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

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

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,053 hrs · 32,754 cycles

LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,053 hrs · 32,754 cycles

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

Part: SKIN — CRACKED (SLAT) · airframe 56,053 hrs · 32,754 cycles

#8 LEADING EDGE SLAT NOSE SKIN LOWER SURFACE AT ACTUATOR ATTACH FITTING HAS CRACK AT FASTENER HOLE / REPAIRED #8 LEADING EDGE SLAT SKIN LOWER SURFACE AT ACTUATOR ATTACH FITTINGS IAW B737 SRM 57-42-01-2R-8 REPAIR 8.

Part: SKIN — ELONGATED (SLAT) · airframe 56,053 hrs · 32,754 cycles

#1 LEADING EDGE SLAT LOWER SURFACE NOSE SKIN AT ACTUATOR ATTACH FITTING HAS WORKING FASTENERS / #1 SLAT LOWER NOSE SKIN AT ACTUATOR ATTACH FITTING REPIRED IAW B737 SRM 51-42-01-2R-8 REPAIR 8.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 56,045 hrs · 32,749 cycles

FORWARD R1 WINDOW ARCED. R&R WINDSHIELD PER AMM.

Part: CONTROLLER — ARCED (COCKPIT) · airframe 56,045 hrs · 32,749 cycles

FORWARD R1 WINDOW ARCED. R&R WINDOW HEAT CONTROLLER PER MM.

Part: RIVET — LOOSE (L1 DOOR) · airframe 55,871 hrs · 32,641 cycles

L1 DOOR SLIDE CASE AFT GIRT BAR STOW HOOK LOOSE. R&R RIVETS PER SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,340 hrs · 32,295 cycles

LT OVERWING EMERGENCY EXIT SIGN INOP. RELAMPED SIGN IAW AMM.

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 54,965 hrs · 32,053 cycles

R2 DOOR EMERGENCY EVAC INADVERTENTLY CAME OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,704 hrs · 31,892 cycles

RT EMERGENCY BULLNOSE LIGHT INOP AT ROW 8. REPAIRED LIGHT IAW MM.

Part: PANEL — DELAMINATED (LT WING) · airframe 54,577 hrs · 31,807 cycles

UNDER LEFT WING THE SECOND PANEL OVER FROM THE FUEL SHUTOFF PANEL HAS A CRACK AND IS STARTING TO DELAMINATE / CLEARING # 73227 R&R PANEL 521DB PER SRM 51-40-02 PER DMA 0135329

Part: LENS — BROKEN (EXIT SIGN) · airframe 53,323 hrs · 31,049 cycles

LT OVER WING EXIT SIGN LENS COVER BROKEN. SECURED SIGN PER SIP.

Part: BATTERY — FAILED (CABIN) · airframe 49,835 hrs · 28,908 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 49,835 hrs · 28,908 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 49,835 hrs · 28,908 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PER AMM.

Part: PLATE — CRACKED (LT WING) · airframe 49,835 hrs · 28,908 cycles

LT WING AFT SPAR LOWER SHELF WIGGLE PLATE CRACKED OUTBOARD OF NR 3 FLAP TRACK. R&R WIGGLE PLATE PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 49,835 hrs · 28,908 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 49,835 hrs · 28,908 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 49,835 hrs · 28,908 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 49,835 hrs · 28,908 cycles

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

Part: BRACKET — LOOSE (R1 GIRT BAR) · airframe 48,786 hrs · 28,266 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR HOLDER BRACKET LOOSE. REPAIRED THE BRACKET IAW SRM & MT.

Part: LENS — LOOSE (R2 DOOR) · airframe 48,163 hrs · 27,903 cycles

R2 DOOR ESCAPE SLIDE LENS LOOSE. SECURED LENS IAW SIP.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 46,835 hrs · 27,156 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,463 hrs · 26,952 cycles

RIGHT OVERWING EMER EXIT EGRESS LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 45,891 hrs · 26,606 cycles

OVERHEAD EMER SIGN, LENS LOOSE. SECURED LENS IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,906 hrs · 26,019 cycles

EMERGENCY LIGHT INOPERATIVE BETWEEN ROW 3 & 6. R & R M1674 BATTERY PACK IAW MM.

Part: SIGN — MISSING (CABIN) · airframe 44,191 hrs · 25,615 cycles

RIGHT OVERWING EMER EXIT SIGN MISSING. INSTALLED SIGN IAW AMM.

Part: WEB — CRACKED (LT WING) · airframe 43,225 hrs · 25,059 cycles

LEFT WING UPPER TE SHELF PANEL VERTICAL WEB ON LOWER SURFACE CRACKED INBD OF FLAP DEFLECTION RIB. REPAIRED WEB IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 43,225 hrs · 25,059 cycles

RIGHT WING UPPER TE SHELF PANEL LOWER SUPPORT BRACKET CRACKED. R & R BRACKET IAW MM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 43,225 hrs · 25,059 cycles

LEFT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED ON RIB AT STATION 92.5, 18 INCHES AFT OF SPAR. REPAIRED STIFFENER IAW SRM.

Part: STRUCTURE — CRACKED (RT WING) · airframe 43,225 hrs · 25,059 cycles

RIGHT WING TE AUXILIARY STRUCTURE FOR SHELF PANEL BELOW DEFLECTION RIB CRACKED. REPAIRED STRUCTURE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

SEAT TRACK CRACKED BETWEEN BS 727A+17 TO 727A+18, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 227 TO 294, BL 0. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, LBL 32. R & R INTERCOSTAL IAW DRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

SEAT TRACK CRACKED BETWEEN BS 727A+17 TO 727A+18, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: FITTING — CORRODED (L1 DOOR) · airframe 43,225 hrs · 25,059 cycles

L1 DOOR EMER EVAC SLIDE FWD GIRT BAR ATTACH STRUCTURE FITTING CORRODED. R & R FITTING IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

SEAT TRACK CRACKED BETWEEN BS 727A+17 TO 727A+18, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 328 TO 344, LBL 32. R & R INTERCOSTAL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 312 TO 320, RBL 25. R & R INTERCOSTAL IAW SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 43,225 hrs · 25,059 cycles

L1 DOOR EMER EVAC SLIDE AFT GIRT BAR ATTACH STRUCTURE FITTING CORRODED. R & R FITTING IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 790 TO 867, RBL 14. REPAIRED SUPPORT IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

STRINGER CLIP CRACKED AT BS 277, STRINGER 10R. R & R CLIP IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

FORWARD SEAT TRACK HOLE OTBD SIDE CRACKED AT BS 727A+17, LBL 26.0. REPAIRED SEAT TRACK IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

FORWARD SEAT TRACK HOLE OTBD SIDE CRACKED AT BS 727A+18, LBL 26.0. REPAIRED SEAT TRACK IAW ACO.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

AFT CARGO FLOOR SUPPORT BRACKET CRACKED AT BS 947, LBL 10. R & R BRACKET IAW MM.

Part: POST — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

LEFT NR 3 WINDOW FRAME EF POST CRACKED. REPAIRED POST IAW ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

NUMBER 1 RT COCKPIT WINDOW SKIN CRACKED BETWEEN TWO FASTENER HOLES AT LOWER INBD CORNER. REPAIRED SKIN IAW ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

FUSELAGE SKIN THIRD ROW CRACKED AT BS 540, STRINGER 22L AFT HOLE. REPAIRED SKIN IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

FLIGHT DECK LT NR 1 WINDOW FRAME CRACKED. REPAIRED FRAME IAW ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

FUSELAGE SKIN SECOND ROW CRACKED AT BS 540, STRINGER 22L AFT HOLE. REPAIRED SKIN IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

RIGHT NR 3 WINDOW FRAME EF POST CRACKED. REPAIRED POST IAW ACO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,225 hrs · 25,059 cycles

COCKPIT FLOOR NUTPLATE HOLES CORRODED ON L ANGLE AT BS 270, BETWEEN LBL 10 TO RBL 10. REPAIRED L ANGLE IAW SRM,

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 43,225 hrs · 25,059 cycles

STIFFENER CRACKED JUST AFT & INBD OF RT VERTICAL FRONT SPAR TERMINAL FITTING. REPAIRED STIFFENER IAW SRM.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 42,816 hrs · 24,823 cycles

FUEL CROSS FEED CB FOUND TO BE POPPED INFLIGHT. R & R FUEL CROSS FEED VLV ACTUATOR IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 38,889 hrs · 22,525 cycles

RT EMERGENCY EXIT LIGHT LENS COVER FELL OFF AT ROW 3. SECURED COVER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,678 hrs · 21,823 cycles

AFT ENTRY DOOR OVERHEAD EMERGENCY LAMP INOP. RELAMPED IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,678 hrs · 21,823 cycles

RIGHT LOWER MID CABIN EMERGENCY EXIT LAMP INOP. RELAMPED IAW AMM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 37,055 hrs · 21,455 cycles

EMERGENCY EXIT SIGN BROKEN EMERGENCY EXIT ROW RIGHT. REMOVED AND REPLACED COVER PER M/M.

Part: BATTERY — FAILED (CABIN) · airframe 36,700 hrs · 21,248 cycles

ALL SEVEN EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST FWD LT, FWD RT, CTR LT, CTR RT, ROW 17 LT, AFT LT, AFT RT. REMOVED AND REPLACED ALL SEVEN EMERGENCY LIGHT BATTERIES PER MM. FWD LT, FWD RT, CTR LT, CTR RT, ROW 17 LT, AFT LT, AFT RT.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 36,700 hrs · 21,248 cycles

LEFT HORIZONTAL STABILIZER FORWARD LOWER SLIDING SEAL IS CRACKED. REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER FORWARD LOWER SLIDING SEAL REF MM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 36,700 hrs · 21,248 cycles

RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDING SEAL IS CRACKED. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDING SEAL REF MM

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 36,233 hrs · 20,982 cycles

CO-PILOT'S NR 1 WINDOW (C, D) POST CRACKED IN RADIUS. VERIFIED PER HFEC PART 6 51-00-00 FIG 23. REPAIRED CO-PILOTS NR 1 RIGHT SIDE WINDOW POST PER EA 1-753-21127.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,233 hrs · 20,982 cycles

EMERGENCY CABIN LIGHTS INOP. REMOVED AND REPLACED BATTERY & BATTERY OVERDOOR PANEL PER MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 36,227 hrs · 20,978 cycles

RIGHT STAB LOWER IN-SPAR SKIN CRACKED AT STAB STA 129.50 APPROX. 9.5" AFT OF STAB LEADING EDGE. REPAIRED PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 36,227 hrs · 20,978 cycles

LEFT STAB LOWER IN-SPAR SKIN CRACKED AT STAB STA 129.50 APPROX 14" AFT OF STAB LEADING EDGE. REPAIRED PER SRM.

Part: LENS — MISSING (CABIN) · airframe 35,873 hrs · 20,744 cycles

FORWARD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW M/M.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,716 hrs · 20,644 cycles

R1 DOOR EXTERIOR EMERGENY LIGHT INOP. RELAMPED LIGHT PER M/M.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 35,089 hrs · 20,247 cycles

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

Part: LIGHT — CRACKED (CABIN) · airframe 34,655 hrs · 20,000 cycles

EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER M/M.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,387 hrs · 19,843 cycles

LEFT EMERGENCY EGRESS LIGHT INOPERATIVE AT ROW 1. RELAMPED LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,387 hrs · 19,843 cycles

LEFT EMERGENCY LIGHTS INOPERATIVE AT ROW 19. RELAMPED EMERGENCY LIGHT PER MM.

Part: TRANSMISSION — FAULTY (LT WING TE FLAPS) · airframe 33,558 hrs · 19,357 cycles

DECLARED EMERGENCY - ALL FLAPS WOULD NOT EXTEND, BRAKE ENERGY 20.8 LEFT L/E FLAPS NEVER MOVED. RIGHT LE FLAPS EXTENDED 1/4 OF POSITIONS ONE. REMOVED AND REPLACED NR 4 T/E FLAP TRANSMISSION AND TORQUE TUBE PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 33,216 hrs · 19,148 cycles

LT EEPLS MISSING AT ROW 11. INSTALLED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,787 hrs · 18,884 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 32,746 hrs · 18,866 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 32,746 hrs · 18,866 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 32,416 hrs · 18,662 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 12 TO ROW 22. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 32,416 hrs · 18,662 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 4 TO ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 32,295 hrs · 18,561 cycles

FWD EEPLS BULB BROKEN. REMOVED AND REPLACED BULB IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 31,798 hrs · 18,294 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 30,645 hrs · 17,609 cycles

LT EEPLS COVER LOOSE AT ROW 10. SECURED COVER PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 30,122 hrs · 17,303 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS INOP. RECONNECTED WIRE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 30,122 hrs · 17,303 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,050 hrs · 17,258 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 147.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,050 hrs · 17,258 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,050 hrs · 17,258 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 129 50. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,050 hrs · 17,258 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 29,917 hrs · 17,178 cycles

EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 34. REPAIRED T-CAP PER SRM AND EA.

Part: LENS — CRACKED (CABIN) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 3.0. REPAIRED BEAM PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 300 TO BS 324, RBL 59. REPAIRED BEAM PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (GALLEY DOOR) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT GALLEY DOOR CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, RBL 8.1. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 8.1. REPAIRED BEAM PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 951 TO BS 986.5. REPAIRED BEAM PER SRM AND BAC DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR CUTOUT FORWARD FRAME WEB CRACKED AT BS 296.5, STR 17R. REPAIRED WEB PER SRM AND BAC DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT Z-ANGLE CORRODED BETWEEN BS 500C TO BS 500B. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 772, LBL 17.24. REPAIRED BEAM PER EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT Z-ANGLE CORRODED BETWEEN BS 500B TO BS 500A. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,303 hrs · 16,822 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT Z-ANGLE CORRODED BETWEEN BS 500D TO BS 500C. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 29,160 hrs · 16,733 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,891 hrs · 15,976 cycles

DURING SCHEDULED OTS CHECK, FOUND EXTERNAL LT FWD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: FLAP — WORN (RT WING) · airframe 27,061 hrs · 15,466 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING I/B MID FLAP WORN. REPAIRED MID FLAP PER SRM.

Part: TORQUE TUBE — WORN (TE FLAP) · airframe 25,716 hrs · 14,628 cycles

DURING SCHEDULED MV1 CHECK, RT WING FLAP INDICATION AT 30, LT WING FLAP INDICATION AT 40. REMOVED AND REPLACED TORQUE TUBE ASSY PER MM.

Part: TORQUE TUBE — WORN (TE FLAP) · airframe 25,716 hrs · 14,628 cycles

DURING SCHEDULED MV1 CHECK, RT WING FLAP INDICATION AT 30, LT WING FLAP INDICATION AT 40. REMOVED AND REPLACED TORQUE TUBE ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 25,629 hrs · 14,575 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 25,629 hrs · 14,575 cycles

LEFT EEPLS LENS LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: CAP — BROKEN (CABIN) · airframe 24,880 hrs · 14,119 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS END CAP BROKEN AT ROW 1. REMOVED AND REPLACED END CAP PER MM.

Part: COVER — CRACKED (CABIN) · airframe 24,880 hrs · 14,119 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED AT ROW 10. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,308 hrs · 13,764 cycles

LT OVERWING EMERGENCY EXIT ROW EEPLS LOOSE. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 23,150 hrs · 13,032 cycles

L1 DOOR EMERGENCY EVACUATION SLIDE LOOSE. SECURED SLIDE PER MT.

Part: LENS — MISSING (CABIN) · airframe 22,949 hrs · 12,919 cycles

FWD CABIN EEPLS STRIP LENS MISSING. INSTALLED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,264 hrs · 9,913 cycles

DURING SCHEDULED HC1 CHECK, AFT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,264 hrs · 9,913 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,370 hrs · 11,948 cycles

DURING SCHEDULED HC2 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,370 hrs · 11,948 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 21,370 hrs · 11,948 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,370 hrs · 11,948 cycles

DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,370 hrs · 11,948 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. R&R BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,118 hrs · 11,166 cycles

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

Part: COVER — MISSING (CABIN) · airframe 19,971 hrs · 11,081 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED EXIT SIGN ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 19,427 hrs · 10,762 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 15 ABC. INSTALLED LENS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 19,211 hrs · 10,634 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING AT ROW 13 ABC. INSTALLED LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 19,211 hrs · 10,634 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 18,890 hrs · 10,450 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZONAL STAB) · airframe 18,890 hrs · 10,450 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 18,634 hrs · 10,289 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,253 hrs · 10,085 cycles

EEPLS INOP AT ROW 8 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 18,077 hrs · 9,980 cycles

EEPLS COVER MISSING AT ROW 5 ABC. INSTALLED COVER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 16,338 hrs · 8,981 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 11. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 15,661 hrs · 8,601 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,012 hrs · 8,212 cycles

DURING SCHEDULED MV3 CHECK, FOUND RIGHT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 13,800 hrs · 7,551 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT COVER CRACKED AT ROW 2 ABC. REMOVED AND REPLACED EEPLS LIGHT COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,800 hrs · 7,551 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — BROKEN (ROW 17) · airframe 11,388 hrs · 6,184 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK COVER BROKEN AT ROW 17. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 10,464 hrs · 5,664 cycles

DURING SCHEDULED RON CHECK, R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 8,914 hrs · 4,830 cycles

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

Part: HOOK — DAMAGED (GIRT BAR) · airframe 8,214 hrs · 4,445 cycles

R1 DOOR EVAC SLIDE GIRT BAR FWD HOOK HAS SHEARED RIVET. REMOVED AND REPLACED RIVET PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 7,142 hrs · 3,822 cycles

L1 DOOR EVACS SLIDE FELL OUT. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 5,969 hrs · 3,196 cycles

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

Part: BALLAST — INOPERATIVE (CABIN) · airframe 4,557 hrs · 2,440 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED RT EMERGENCY EXIT LIGHT BALLAST.

Part: GIRT BAR — OUT OF ADJUST (AFT SERVICE DOOR) · airframe 2,411 hrs · 1,303 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 945 hrs · 532 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM.