N727SW

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 75,107 hrs · 44,523 cycles

FWD ENTRY DOOR SLIDE FELL OUT. RE-POSITIONED AND SECURED SLIDE REF AMM 25-66-01

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 74,500 hrs · 44,185 cycles

ROW 6DEF EMERGENCY LIGHT COVER MISSING. LIGHT WORKS NORMALLY / CLOSING DMA 0154430 INSTALLED LENS COVER @ ROW 6DEF EMERGENCY LIGHT AS PER AMM 33-51-03. CL# 71277

Part: BATTERY PACK — FAILED (CABIN) · airframe 74,280 hrs · 44,042 cycles

BATTERY PACKS FAILED CAPACITY TEST AT FOLLOWING POSITIONS; FRONT LEFT; ROW 16 LEFT; LEFT OVERWING; RIGHT OVERWING; AFT LEFT; AND AFT RIGHT. REMOVED AND REPLACED PER AMM.33-51-06.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,855 hrs · 43,794 cycles

EMERGENCY LIGHT ABOVE THE FORWARD ENTRY DOOR THRESHOLD PORTION HAS LIGHTS OUT. REPLACED LAMPS FOR EMERGENCY LIGHT AT THE FWD ENTRY DOOR THRESHOLD AND PERFORMED GOOD TEST, PER AMM 33-51-01-960-801.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,855 hrs · 43,794 cycles

DURING EMERGENCY LIGHTING TEST L1067, L730,ND L1065 ARE INOPERABLE AT STA 429. REPLACED AND PERFORMED GOOD TEST OF BATTERY PACK M1674, PER AMM 33-51-06-960-805.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,855 hrs · 43,794 cycles

CORROSION, ON CREASE BEAM INNER CORD BS 639 LBL 55 WL 208. REMOVED AND INSTALLED NEW CREASE BEAM INNER CHORD BS 532-675 LBL 55 WL 208, IAW BOEING DWGS 144A5910, 144A5901, 143A5240 AND SRM 51-40-02-0G-0 BS 639 LBL 55 WL 208 CREASE BEAM INNER CHORD CORROSION WAS FOUND TO BE OUT OF LIMITS, PER SRM 53-40-13-1A-1 56040C 07NOV20.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,855 hrs · 43,794 cycles

CORROSION, EXTERNAL FUSELAGE SKIN NUTPLATE HOLES AT ADF ANTENNAE LOCATION BS 678-702 STR 1-2RT. REPAIRED DAMAGE ON EXTERNAL FUSELAGE SKIN NUTPLATE HOLES AT ADF ANTENNA LOCATIONS BS 678-702 STR 1-2RT, PER ER 20-03489 REV IR AND EA 20-153-02201 REV IR.

Part: SUPPORT PLATE — CORRODED (AFT CARGO) · airframe 73,855 hrs · 43,794 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION AROUND NUT PLATE HOLES BS727 TO BS847 LBL23 WL156 / EVALUATED CORROSION ON ACB LH FLOOR TO SIDEWALL SUPPORT; BS727-847; REMOVED .015' FROM ORIG .040'; FOUND TO BE OUT OF LIMITS; LOCATED; DRILLED AND INSTALLED; IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 146A7500

Part: SUPPORT PLATE — CORRODED (AFT CARGO) · airframe 73,855 hrs · 43,794 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION AROUND NUT PLATE HOLES BS727 TO BS767 RBL23 WL156 / EVALUATED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT. REMOVED 0.015'; FROM ORIG .040'; FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-1A-2. LOCATED; PRIMED AND INSTALLED NEW ACB RH FLOOR TO SIDEWALL SUPPORT; BS727-767; IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 146A7500.

Part: SKIN — DENTED (FUSELAGE) · airframe 73,855 hrs · 43,794 cycles

DENT ON FUSELAGE SKIN BS 927+3, COMMON TO STR 18L. DENT ON FUSELAGE SKIN BS 927+3, COMMON TO STR 18L WAS FOUND TO BE OUT OF LIMITS, DUE TO LOCATION AT STRINGER 18L. REPAIRED PER ATS ER 20-03499 REV IR AND EA 20-153-02206 REV IR.

Part: SKIN — DENTED (FUSELAGE) · airframe 73,855 hrs · 43,794 cycles

DENT ON FUSELAGE SKIN BS 907 +10; 2' BELOW STR 18L. DENT MEASURES L=2.6' W=2' Y= .024 W/Y=83 IS WITHIN LIMITS, PER SRM 53-00-01-1A-1 & EA 20-153-02206 REV IR & ER 20-03499 REV IR. APPLIED DAMAGE IDENTIFICATION, AS PER MPM 52.03.01.02 & PER EA 20-153-02206 REV IR. DAMAGE IS ALLOWABLE FOR CONTINUED SERVICE WITHOUT REPETITIVE INSPECTIONS & NO TERMINATING ACTION REQUIREMENTS.

Part: STRINGER — CORRODED (BS 536) · airframe 73,855 hrs · 43,794 cycles

CORROSION COMMON TO END OF STR 26L IN SNAKE PIT BS 536 WL 152. CORROSION COMMON TO END OF STR 26L BS 536 WL152 FOUND TO BE OUT OF LIMITS, PER SRM 53-00-03-1A-1. CUTOUT DAMAGED SECTION BS 500D+11'-BS 536 STR 26L. REPAIRED SECTION, PER SRM 53-00-03-2R-1 SRM 51-40-02-0G-0.

Part: STRINGER — CRACKED (BS 536) · airframe 73,855 hrs · 43,794 cycles

CRACK COMMON TO END OF STR 23L IN SNAKE PIT BS 536 WL 163. STRINGER WAS REPAIRED, PER ATS ER 20-03457 REV IR AND SWA EA 20-153-02126 REV IR.

Part: STRINGER — CORRODED (BS 536) · airframe 73,855 hrs · 43,794 cycles

CORROSION COMMON TO END OF STR 27L IN SNAKE PIT BS 536 WL 150. CORROSION COMMON TO END OF STR 27L BS 536 WL 150 FOUND TO BE OUT OF LIMITS, PER SRM 53-00-03-1A-1. CUTOUT DAMAGED SECTION BS 500D+11'-BS 536 STR 27L. REPAIRED SECTION, PER SRM 53-00-03-2R-1 SRM 51-40-02-0G-0.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 73,855 hrs · 43,794 cycles

CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 693 LBL 1 WL 204-207, MARKED. REPLACED CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 693 LBL 1 WL 204-207, PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 273A9112 REV B DWG 273A9110 REV A.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 73,855 hrs · 43,794 cycles

CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 RBL 24 WL 204, MARKED. REPLACED CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 RBL 24 WL 204, IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 273A9112 REV A DWG 111A6000 REV A.

Part: STRINGER — CRACKED (BS 536) · airframe 73,855 hrs · 43,794 cycles

CRACK COMMON TO END OF STR 26R IN SNAKE PIT BS 536 WL 152. REMOVED DAMAGE AND REPAIRED STR 26R IN SNAKE PIT BS 536 WL 152, IAW SRM 53-00-03-2R-1.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 73,855 hrs · 43,794 cycles

CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 RBL 1 WL 207, MARKED. REPLACED CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 RBL 1 WL 207, PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 273A9112 REV B DWG 273A9110 REV A.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,855 hrs · 43,794 cycles

CORROSION, ON CREASEBEAM WEB ATTACH ANGLE STA 664 RBL 67 WL 208 UPPER SURFACE, MARKED. REMOVED CORROSION ON CREASEBEAM WEB ATTACH ANGLE STA 664 RBL 67 WL 208 UPPER SURFACE. MAX MATERIAL REMOVED FROM .056' 7075T6 LOT NR 1331117-2. REMOVED OLD AND LOCATED & DRILLED, TREATED, & PRIMED AND INSTALLED NEW ANGLE, PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 SRM 51-30-01-0G-0 SRM 53-40-13-1A-1 SRM 51-10-02-0G-0 SRM 51-20-01-0G-0 SOPM 20-43-03 DWG 144A5930 DWG 144A5920 DWG 144A5900.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 73,855 hrs · 43,794 cycles

CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 LBL 24 WL 204, MARKED. REPLACED CRACKED ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 LBL 24 WL 204, PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 273A9112 REV A 273A9110 REV A.

Part: DOOR — CORRODED (LAV SERVICE) · airframe 73,855 hrs · 43,794 cycles

EXTERIOR LAV SERVICE DOOR HAS CORROSION ON THE INTERNAL SIDE OF DOOR AROUND THE BONDING JUMPER STUD / FOUND CORROSION ON INTERNAL SIDE OF THE EXTERIOR LAV SERVICE DOOR TO BE OUT OF LIMITS; ORIGINAL THICKNESS 0.100; REMOVED 0.040 MATERIAL PER SRM 52-40-01-0I-4; SRM 52-40-01-1A-4; REMOVED DAMAGED LAV SERVICE DOOR PER SRM 52-49-07-000-801. INSTALLED NEW LAV SERVICE DOOR; AND PERFORMED A GOOD BONDING RESISTANCE CHECK PER SRM 52-49-07-400-801.

Part: PLATE — MISSING (AFT BAY DOOR) · airframe 73,855 hrs · 43,794 cycles

STRIKER PLATES ON BOOMERANG ANGLE LOCATED ON R/H AC BAY DOOR #192CR ARE MISSING OR DAMAGED / REMOVED AND REPLACED BOOMERANG ANGLE ON R/H AC BAY DOOR IAW AIPC 52-48-11-03 AND SOPM 20-50-01.

Part: ANGLE — CRACKED (RT WING) · airframe 73,855 hrs · 43,794 cycles

RIGHT WING TRAILING EDGE TRANSVERSE WEB ABOVE #2 PYLON FAIRING AFT TIP THE O/B ATTACH ANGLE CRACKED / REMOVED AND REPLACED R/W T/E TRANSVERSE WEB O/B ATTACH ANGLE (CLIP) ABOVE #2 PYLON FAIRING AFT TIP IAW SRM 51-40-02-0G-0 PARA 4; AIPC 57-42-51-02; AND BAC DRAWING 115A6200.

Part: PRESSURE DECK — CRACKED (BS 663) · airframe 73,855 hrs · 43,794 cycles

DURING COMPLETION OF CCN 753-201-00-02 FOUND HORIZONTAL PRESSURE DECK CRACKED ON LEFT SIDE AT BS 663 WL 201 LBL 30 AND 32. ALSO AT BS 673 WL201 LBL 30 AND 38, AREAS MARKED. REMOVED DAMAGE PART OF THE HORIZONTAL PRESSURE DECK BS 663-674 LBL 30-LBL 60 WL 201 AND REPAIRED IAW SRM 53-40-51-2R-2 REPAIR 2.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 73,855 hrs · 43,794 cycles

LEFT HORIZONTAL STAB RIB ASSEMBLY 4 (STAB STA 120.30) HAS CRACK AT 4TH STIFFENER. REPAIRED LT HORIZONTAL STABILIZER RIB ASSEMBLY 4 AT STAB STA 120.30 4TH STIFFENER, IAW SRM 55-10-09-2R-5. 59796C 20 OCT '20.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 73,855 hrs · 43,794 cycles

LT HORIZONTAL STABILIZER RIB ASSEMBLY 4 (STAB STA 120.30) STIFFENER 3 IS CRACKED AT LOWER END. REPAIRED LT HORIZONTAL STABILIZER RIB ASSEMBLY 4 AT STAB STA 120.30 3RD STIFFENER, IAW SRM 55-10-09-2R-5 59796C 20 OCT '20.

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 73,855 hrs · 43,794 cycles

FLIGHT DECK FLOOR IS DENTED AT BS 255 RBL 4-LBL 14 WL 207.54. REPAIRED FLIGHT DECK FLOOR DAMAGE AT BS 255 RBL 4-LBL 14 WL 207.54, PER ER 20-03451 REV IR AND EA NR 20-153-02181 REV IR.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 73,855 hrs · 43,794 cycles

LT HORIZONTAL STABILIZER RIB ASSEMBLY 4 (STAB STA 120.30) STIFFENER 2 IS CRACKED AT LOWER END. REPAIRED LT HORIZONTAL STAB RIB ASSEMBLY 4 (STAB STA 120.30) 2ND STIFFENER AT LOWER END, IAW SRM 55-10-09-2R-5.

Part: HANDLE — LOOSE (L2 DOOR ASSIST) · airframe 73,855 hrs · 43,794 cycles

FWD ENTRY DOOR ASSIST HANDLES ARE LOOSE. TIGHTENED FED ASSIST HANDLE, PER SOPM 20-50-01.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 73,822 hrs · 43,776 cycles

FWD SERVICE DOOR SLIDE LOOSE IN COVER / ADJUSTED FWD SERVICE DOOR SLIDE PER S.I.P.

Part: LIGHT — UNSECURE (CABIN) · airframe 73,822 hrs · 43,776 cycles

EXIT FLOOR LIGHT STRIPS LOOSE NEW FORWARD ENTRY DOOR / SECURED EXIT FLOOR LIGHT STRIP PER S.I.P.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 73,791 hrs · 43,755 cycles

AFT SERVICE DOOR SLIDE PARTIALLY DEPLOYED. AFT SLIDE NOTE DEPLOYED, PARTIALLY FELL OUT OF CONTAINER. REINSTALLED SLIDE, PER MT 725-61-06. A/C OK FOR SERVICE STS LINE MX Q6TR841X.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 72,668 hrs · 43,056 cycles

FWD CARGO COMPARTMENT AFT FLOOR PANEL CRACKED / REMOVED & REPLACED FWD CARGO COMPARTMENT AFT FLOOR PANEL PER AMM 25-52-1

Part: SUPPORT — ELONGATED (WHEEL WELL RH) · airframe 71,276 hrs · 42,203 cycles

REF LP: 1213458 LOWER AFT FAIRING FOR RH WHEEL WELL CUT OUT (PN: 149A7603-120) HAS SEVERAL ATTACHING HOLES THAT ARE ELONGATED / 'REFERENCE DMA 0156733' REMOVED AND REPLACED WHEEL WELL FAIRING SUPPORT PER SRM 51-40-02 CL #27301

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 70,354 hrs · 41,597 cycles

RT WING OVER WING EMERGENCY EXIT HANDLE MOLDING LOOSE. SECURED HANDLE REF MM.

Part: PANEL — ELONGATED (LOWER EXT FUSELA) · airframe 70,346 hrs · 41,594 cycles

193 B PANEL HOLES FOR SCREWS ARE ENLARGED / R&R 193B PANEL PER BOEING DOCUMENT NUMBER 149A7652-13 PL AND EO 14108 SA-M 326: A1073171

Part: BRACKET — LOOSE (L1 DOOR) · airframe 70,339 hrs · 41,589 cycles

L1 DOOR SLIDE GIRT BAR ATTACHMENT HANGING LOOSE. TIGHTEN GIRT BAR BRACKETS PER MT.

Part: SKIN — DEBONDED (GROUND SPOILER) · airframe 69,908 hrs · 41,308 cycles

R/H WING #12 SPOILER DEBONDED AT 14.5" FROM INBOARD EDGE AND 9" FROM LEADING EDGE. / R&R #12 OUTBOARD GROUND SPOILER PER AMM.

Part: SKIN — DEBONDED (LT WING SPOILER) · airframe 69,908 hrs · 41,308 cycles

L/H WING #6 SPOILER DEBONDED. R&R #6 INBOARD GROUND SPOILER PER AMM.

Part: SKIN — DEBONDED (RT WING SPOILER) · airframe 69,908 hrs · 41,308 cycles

R/H WING #9 SPOILER DEBONDED AT 3" FROM OUTBOARD EDGE AND 10" FROM TAILING EDGE. / R&R #9 SPOILER PANEL IAW MM.

Part: SPOILER — DEBONDED (RIGHT WING) · airframe 69,908 hrs · 41,308 cycles

DURING COMPLETION OF CCN: EA 1-A57-15168 FOUND #7 SPOILER TO BE DISBONDED AT 4 EA LOCATIONS. 1 = 14' FROM O/B EDGE AND 10' FROM L/E. 2 = 9' FROM L/E AND 29.5' FROM O/B EDGE. 3 = 5' FROM T/E AND 20' FROM I/B EDGE. 4 = 8' FROM L/E AND 19' FROM I/B EDGE. / REMOVED & REPLACED #7 I/B GROUND SPOILER IAW AMM 27-62-12-000-801 AND 27-62-12-400-801 FUNCTIONAL TEST GOOD (POS#7;P/N OFF/ON:113A4600-2;S/N ON:001325)

Part: SKIN — DEBONDED (LT WING SPOILER) · airframe 69,908 hrs · 41,308 cycles

L/H WING #1 SPOILER DEBONDED AT 3.5" FROM LEADING EDGE AND 5" FROM OUTBOARD EDGE. / R&R #1 OUTBOARD GROUND SPOILER PER AMM.

Part: SKIN — DEBONDED (RT WING SPOILER) · airframe 69,908 hrs · 41,308 cycles

R/H WING #10 SPOILER DEBONDED AT 12" FROM OUTBOARD EDGE AND 9" FROM LEADING EDGE. / R&R #10 SPOILER PANEL IAW AMM.

Part: SKIN — DEBONDED (LT WING SPOILER) · airframe 69,908 hrs · 41,308 cycles

L/H WING #3 SPOILER PANEL DEBONDED AT 4" FROM OUTBOARD EDGE AND 4" FROM LEADING EDGE. / R&R #3 SPOILER PANEL IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 69,631 hrs · 41,125 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 69,631 hrs · 41,125 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,465 hrs · 41,019 cycles

L/H OVERWING EMERGENCY LIGHT INOP. R&R BULB PER AMM.

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 69,253 hrs · 40,870 cycles

RT WHEEL WELL STA. 663 RBL 26; STIFFENER CRACKED. / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 69,253 hrs · 40,870 cycles

L1 DOOR EXTERNAL EMERGENCY LIGHT INOP AT BS 371. CONNECTED CONNECTOR PLUG PER AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

FLOOR SUPPORT FORMED WEB CRACKED AT BS 360, LBL 12. R&R WEB IAW SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

INTERNAL BUTT SPLICE CORRODED FOUND UNDER BS 360, STR 25L. REPAIRED BUTT SPLICE PER SRM AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

ELECTRONICS AND EQUIPMENT BAY AIRCRAFT SKIN AT CHEMILL EDGE CORRODED BETWEEN BS 362 TO BS 366, STR 26L. REPAIRED SKIN IAW SRM AND EA.

Part: PLATE — CORRODED (AFT CARGO THRESH) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO FWD SCUFF PLATE NET ANCHOR CORRODED P/N 453A2611-1 / REPLACED NET ANCHOR PLATE PART# 453A2611-1 ISSUE TAG # A94946 PER HIPC 25-52-10-02

Part: WEB — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

FLOOR WEB AFT OF R2 DOOR CUTOUT CRACKED. R&R FLOOR WEB PER DWG AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

FLOORBEAM UPPER T CAP CORRODED AT BS. 986, RBL 45. R&R "T" CAP PER SRM.

Part: STRINGER — CORRODED (FWD FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

CORROSION FOUND ON STR 27L AFT OF SPLICE AT STA 360+10' / EVALUATED DAMAGE ON STR 27L AFT OF SPLICE @ STA 360+10' IAW B737 SRM 53-30-03-1A-1. FOUND 100% MATERIAL LOSS OUT OF LIMITS REPAIRED IAW B737 SRM 53-00-03-2R-1 & EA 190055 REV P1 & IR & SWA EA 1-753-34071 REV IR

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

AFT OF SPLICE CORRODED AT BS 360+10, STR 25L. R&R STRINGER SECTION IAW EA.

Part: SPLICE STRAP — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

INTERNAL SKIN BUTT SPLICE STRAP UNDER CORRODED AT BS 360, BETWEEN STR 25L TO STR 28L. REPAIRED SPLICE STRAP IAW EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

STRINGER SPLICE CORRODED AT BS 360+5, STR 25L. R&R STRINGER SPLICE IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

INTERNAL SKIN BUTT SPLICE STRAP UNDER CORRODED AT BS 360, BETWEEN STR 25L TO STR 28L. REPAIRED SKIN IAW EA.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

SPLICE CORRODED AT BS 360+5, STR 27L. R&R SPLICE IAW SRM & DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

STRINGER END FITTING CORRODED AT BS 1016, STR 27L. R&R FITTING IAW DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

CORROSION FOUND ON INTERCOSTAL JUST I/B OF STR 27L AT STA 360+5' P/N 143A9173-12 / REMOVED CORROSION AN INTERCOSTAL @STA 36+5' O/B STR 27L FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-04-1A-1 ORIG. .080 REMAIN .067 LOSS .013 MORE THAN 10% REMOVED. RECIEVED NEW INTERCOSTAL ON BACKSHOP W/O 38832/1300/0003 LOCATED AND DRILLED NEW INTERCOSTAL IAW BOEING DWG 143A173 REV E; TREATED & PRIMED IAW B737 AMM 51-21-41-370-802 & 51-21-72-370-804 INTERCOSTAL REMOVED & REPLACED ON CARD X882611 SAM 326 E356036 ITEM 1

Part: FITTING — CRACKED (AFT CARGO COMPT) · airframe 69,068 hrs · 40,761 cycles

AREA AFT OF AFT CARGO COMPARTMENT STA 948 LBL 10 FITTING JUST FWD OF WATER TANK SUPPORT BRACKET IS CRACKED / REMOVED AND REPLACED -6 FITTING AT STA 948 LBL 10 PER SRM 51-40-02-0G-0 AND DWG 149A8103 REV-

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

FORWARD OF R1 DOOR, UPPER STUB FRAME CRACKED AT BS 295. R&R FRAME IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO EQUIPMENT BAY CHORD CORRODED AT BS 1016, BETWEEN STR 27L TO STR 27R. R&R ANGLE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

ELECTRONIC AND EQUIPMENT COMPARTMENT STRINGER CORRODED AT BS 360+15, STR 25L. REPAIRED STRINGER IAW SRM AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

EXTERIOR FUSELAGE SKIN CORRODED AT BS 360, BETWEEN STR 24L TO STR 28L. R&R SKIN IAW SRM.

Part: SPLICE STRAP — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

EQUIPMENT AND ELECTRONICS COMPARTMENT INTERIOR SPLICE STRAP CORRODED AT BS 360, STR 26L. R&R SPLICE STRAP IAW SRM AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

STRINGER CORRODED AT BS 360+2, STR 27L. REPAIRED STRINGER IAW SRM & EA.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,068 hrs · 40,761 cycles

IN AFT CARGO PIT; 4 EA. CAP STRIPS CORRODED ON L/H SIDE OF FLOOR PNL'S / RECEIVIED 4EA NEW CAP STRIPS FOR AFT CARGO L/H SIDE; P/N -453A2611-8 ON ATAG# WN2510 P/N -453A2611-10 ON ATAG# A90113; P/N -453A2611-4 ON ATAG# WN2988; AND P/N- 453A2611-13 ON ATAG# A90199; REPLACED ON BENCH IAW IPC 25-52-10-02.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,068 hrs · 40,761 cycles

LT WING OUTBOARD AFT FLAP BOTTOM SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

R1 SERVICE DOOR FUSELAGE SURROUND STRUCTURE BEAR STRAP CRACKED AT BS 295, BETWEEN STR 8R TO STR 9R. REPAIRED BEAR STRAP IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

FLOOR SUPPORT CORRODED AT BS 270, BETWEEN LBL 7 TO LBL 9. R&R FLOOR SUPPORT IAW SRM AND EA.

Part: ANGLE — CORRODED (APU COMPARTMENT) · airframe 69,068 hrs · 40,761 cycles

APU COMPARTMENT; AFT BULKHEAD; LOWER L-ANGLE. LBL 18 TO RBL 18 HAS CORROSION ON UPPER AND FWD SURFACE. / REMOVED CORROSION ORIGINAL 'T' .050' REMOVED .011' REMAINING .039' OUT OF LIMITS REMOVED DAMAGED ANGLE. TREATED; PRIMED & INSTALLED NEW ANGLE AS REQUIRED I.A.W BOEING 148A2601 REV- 148A2680 REV:A SRM 51-40-02-0G-0; 51-10-02-0G-0; 53-80-08-1A-1; 51-40-05-0G-0; 51-21-01-0G-0

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

R2 DOOR CREASE BEAM WEB CORRODED BETWEEN BS 953 TO BS 992. R&R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

L1 CREASE BEAM CORRODED ON UPPER SURFACE. R&R L1 CREASE BEAM IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

ELECTRONIC AND EQUIPMENT COMPARTMENT STRINGER CORRODED AT BS 360+9, STR 26L. REPAIRED STRINGER IAW SRM AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

ELECTRONIC AND EQUIPMENT COMPARTMENT STRINGER CORRODED AT BS 360+2, STR 26L. REPAIRED STRINGER IAW SRM AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

FORWARD CARGO COMPARTMENT, FRAME INTERCOSTAL CRACKED BETWEEN BS 480 TO BS 500, STR 19L. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,068 hrs · 40,761 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB STIFFENER CRACKED AT STA 133.15, 2ND FROM FORWARD SPAR AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,068 hrs · 40,761 cycles

RT HORIZONTAL STABILIZER, LEADING EDGE STA 133.15, RIB STIFFENER 4TH FROM FORWARD SPAR CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 69,068 hrs · 40,761 cycles

RT HORIZONTAL STABILIZER LEADING EDGE STA 133.15, RIB STIFFENER 3RD FROM FORWARD SPAR IS CRACKED AT LOWER END. REPAIRED RIB STIFFENER IAW SRM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,068 hrs · 40,761 cycles

R1 DOOR NR 4 BEAMS CRACKED. R&R BEAM IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

E&E COMPARTMENT STRINGER SPLICE CORRODED AT BS 367, STR 26L. R&R STRINGER SPLICE IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,068 hrs · 40,761 cycles

RT HORIZONTAL STABILIZER PANEL 341B, STAB LEADING EDGE STA 95.96 RIB CHORD ANGLE CRACKED AT LOWER AFT EDGE. R&R RIB IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

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

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,068 hrs · 40,761 cycles

LT HORIZONTAL STABILIZER LEADING EDGE PANEL 331B, STAB LEADING EDGE STA 113 RIB CHORD ANGLE CRACKED. R&R RIB IAW DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,068 hrs · 40,761 cycles

RT HORIZONTAL STABILIZER PANEL 341B, STAB LEADING EDGE STA 122.5, RIB CHORD ANGLE CRACKED AT LOWER AFT EDGE. R&R RIB IAW SRM & DWG.

Part: NONE — CORRODED (AFT CARGO) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO 727 CHORD CORRODED AT BS 727 LBL 5' TO RBL 2' / BLENDED & REMOVED CORROSION @ STA 727 CHORD FROM LBL 5' TO RBL 2' IN BELLY OF A/C IAW B737 SRM 51-10-02-0G-0. NO LIMITS FOR AREA. REPAIRED AREA AW EA 190011 REV P1 & IR AND SWA EA 1-753-33960 REV IR.

Part: RETAINER — CRACKED (LT WING) · airframe 69,068 hrs · 40,761 cycles

LH WING LOWER TRAILING EDGE PANEL 561CB HAS NUMEROUS BULB SEAL FASTENER HOLES WITH CRACKS; MARKED. / REPAIRED L/H WING LOWER T/E PANEL 561 CB BULB SEAL FASTENER HOLES IAW B 737-700 SRM 57-51-01-2R-1 REPAIR 1 REV 66

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO INTERCOSTAL CORRODED BETWEEN BS 727A TO BS 727B, RBL 3. R&R INTERCOSTAL PER SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

STRINGER CLIP CRACKED AT BS 259.3+2, STR 8L. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

STRINGER CLIP CRACKED AT BS 259.3+2, STR 12L. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

STRINGER CLIP CRACKED AT BS 259.3+2, STR 16L. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

STRINGER CLIP CRACKED AT BS 259.3+2, STR 10L. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

STRINGER CLIP CRACKED AT BS 259.3+2, STR 6L. R&R CLIP IAW SRM AND DWG.

Part: FAIRING — CORRODED (LWR FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

WING TO BODY FAIRING PANEL 192F HAS CORROSION ON EXTERNAL SKIN UNDER MARKER BEACON ANTENNA; #1; AND #2 DME ANTENNA / WING TO BODY FAIRING 192F REPAIRED WITH BACK SHOP REQUEST WORK ORDER 38832/1700/0001 SERIAL NO: 6851700 SHOP

Part: VAPOR BARRIER — DETERIORATED (LT MLG WW) · airframe 69,068 hrs · 40,761 cycles

VAPOR BARRIER EXISTING REPAIR DETERIORATED AT BS 663, LBL 10. REPAIRED BARRIER IAW SRM & DWG.

Part: VAPOR BARRIER — DETERIORATED (RT MLG WW) · airframe 69,068 hrs · 40,761 cycles

VAPOR BARRIER DETERIORATED AT BS 663, RBL 10. REPAIRED VAPOR BARRIER IAW SRM.

Part: PAN — CORRODED (WATER SERVICE PN) · airframe 69,068 hrs · 40,761 cycles

WATER SERVICE PAN IS CORRODED ON EXTERIOR SIDE IN VARIOUS AREAS / REMOVED CORROSION FROM THE WATER SERVICE PAN IAW SRM 51-10-02; 100% MAT LOSS FOUND TO BE OUT OF LIMITS IAW SRM 51-00-01-1A-5. REMOVED & REPLACED WATER SERVICED PAN IAW SRM 51-40-02 & DWG #147A7221 REV D. AMM 52-49-09-400-801; AMM 38-11-03-400-801; AMM 38-11-09-400-801. BOND CHECK GOOD; AAR TOOL #34005 CAL DUE 09/27/19. ATAG WN3824 & A83753

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

FORWARD CARGO COMPARTMENT DOOR CUTOUT FORWARD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE PER EA.

Part: SERVICE DOOR — CORRODED (LWR FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

WATER SRVICE DOOR PANEL HAS CORROSION AT FWD HINGE (INTERNAL SURFACE) / ORIGINAL WATER SERVICE DOOR PANEL HAS 100% MATERIAL LOSS AT FWD HINGE POINT. VERIFIED NEW DOOR; 147A7221-43; IAW BOEING DWG #147A7221 REV. D APPLIED FINISHES TO NEW DOOR IAW AMM 51-21-41; AMM 51-21-72; AND AMM 51-21-73. A TAG # RI0141

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

FORWARD CARGO COMPARTMENT DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE PER EA.

Part: DOUBLER — CORRODED (WATER SERVICE PN) · airframe 69,068 hrs · 40,761 cycles

WATER SERVICE DOOR CUTOUT; FROM EXTERIOR SIDE; INNER SURFACE OF BEAR STRAP IS CORRODED AROUND DOOR HINGE / REMOVED CORROSION FROM WATER SERVICE DOOR CUTOUT BEAR STRAP DOUBLER IAW SRM 51-10-02. ORIG. MATERIAL 'T' IS .090' WITH A LOSS OF .026' REMAINING 'T' OF .064' IS OUT OF LIMITS IAW SRM 53-00-01-1A-1. REMOVED DAMAGED BEARSTRAP DOUBLER IAW SRM 51-40-02 AND INSTALLED NEW DOUBLER; 147A7221026; IAW SRM 51-40-02 AND BOEING DWG # 147A7221 REV. D. A TAG # A83802

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 400+3 TO BS 400+16, LBL 24. REPAIRED SEAT TRACK IAW SRM.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT FLOORBOARD SUPPORT STRAP STA 727D+5 LBL20 TO RBL 20 HAS CORROSION. / REPLACED PART ON TABLE. TEE STRAP # 146A9401-8 IAW AIPC 53-42-11-30 STA 727D+5 LBL20 TO RBL20 TO BE INSTALLED ON CUSTOMER ORDER JPANEL-141-CLOSE

Part: WEB — CORRODED (AFT CARGO) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO FLOOR STRUCTURE STA 907 TO BS 927, STR 23L AND 24L INTERCOSTAL HAS CORROSION. REMOVED CORROSION ON INTERCOSTAL WEB. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1. AAR TOOL 38289 DUE DATE 04/03/18. REMOVED INTERCOSTAL WEB IAW SRM 51-40-02-0G-0. RECEIVED NEW INTERCOSTAL WEB FROM BACKSHOP ON WORK ORDER # 38832 1600 0002. TRIMMED TO SIZE; LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-41-05 AND BOEING DRAWING # 147A3401 REV C. TREATED AND PRIMED NEW INTERCOSTAL WEB IAW AMM 51-21-72-370-804 AND AMM 51-21-41-370-803. PERFORMED CONFORMITY INSPECTIONS ON NEW INTERCOSTAL WEB P/N 147A7401-11 AND DWG # 147A7401 REV C.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE BULKHEAD POST SUPPORT BRACKET CRACKED AT BS 867, LBL 10. R&R BRACKET IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT LT Z-ANGLE CORRODED BETWEEN BS 727 TO BS 847. R&R Z ANGLE PER SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT SHIELD STA 847 TO STA 867 RBL 20 UPPER AND LOWER SURFACE HAS CORROSION. / REMOVED AND EVALUATED CORROSION. BLENDED DEPTH .008' FROM ORIGINAL .051' REMAINING .043'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. AAR TOOL 38289 DUE DATE 04/13/19. REMOVED FLOOR SHIELD IAW SRM 51-40-02. VERIFIED NEW FLLOR SHIELD P/N 146A812745 / 7530336 ON ATAG # WN9057 IAW BOEING DRAWING # 146A0081 REV C. LOCATED AND DRILLED NEW FLOOR SHILED IAW SRM 51-40-05 AND BOEING DRAWING # 146A0081 REV C. INSTALLED NEW FLOOR SHIELD IAW SRM 51-40-02 AND BOEING DRAWING # 146A0081 REV C. ATAG # WN9087

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 807+1 TO BS 827, LBL 45. R&R SEAT TRACK. IAW SRM.

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO FLOOR STRUCTURE BS 927 - 947 INBD OF STR 27L INTERCOSTAL HAS CORROSION. REMOVED, EVALUATED DAMAGE. BLENDED CORROSION .046' ORIGINAL THICKNESS; REMOVED .010'; REMAINING .036' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1. REMOVED INTERCOSTAL WEB FROM AFT CARGO IAW SRM 51-40-02. TRIMMED TO SIZE; LOCATED &DRILLED NEW INTERCOSTAL WEB IAW SRM 51-40-05 & DWG# 147A7580 REV E. TREATED AND PRIMED NEW INTERCOSTAL IAW AMM 51-21-72-370-804 AND AMM 51-21-41-370-803. INSTALLED NEW INTERCOSTAL WEB AFT CARGO STA 927-947 STR 27L IAW SRM 51-40-02 AND BOEING DWG 147A7580 REV B.

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 69,068 hrs · 40,761 cycles

PASSANGER CABIN; STA 540; BL0 TO LBL 24; LATERAL FLOOR SUPPORT IS CRACKED ON INBOARD END. / REMOVED AND REPLACED LATERAL FLOOR SUPPOR P/N 143A5240-3 ON PASSENGER CABIN STA 540; BL '0' TO LB 24' IAW B737-700 SRM 51-40-05-0G-0 SRM 51-40-02-0G-0; AMM 51-21-91-620-802 AND DWG # 143A0060 RE: B.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT FLOORBOARD SUPPORT STRAP STA 771 LBL20 TO RBL 20 HAS CORROSION. / REPLACED TEE STRAP ASSY ON TABLE; PART# 146A9401-4 PER AIPC 53-42-11-30 STA 771 LBL20 TO RBL20 TO BE INSTALLED ON CUSTOMER ORDER JPANEL-141-CLOSE.

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE STA 727A TO STA 727B LBL3 INTERCOSTAL HAS CORROSION. / REMOVED AND EVALUATED CORROSION. BLEND DEPTH .008' FROM ORIGINAL .036' WITH .028' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-04-1A-1. REMOVED NAD REPLACED INTERCOSTAL WEB STA 727A TO STA 727B LBL3 PER SRM 51-40-02-0G-0 AND DWG 146A7505 REV - APPLIED CIC PAE AMM 51-21-91-620-802

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT DOOR CUTOUT SILL WEB HAS CORROSION. / REMOVED AND EVALUATED CORROSION; BLENDED CORROSION ON AFT SILL WEB ORIGINAL THICKNESS .050'; REMOVED .020'; REMAINING .030'. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1. AAR TOOL 38288 DUE DATE 04/03/19. REMOVED SILL WEB AFT CARGO DOOR CUTOUT IAW SRM 51-40-02. VERIFIED NEW SILL WEB P/N - 146A8123U6 ON ATAG # WN9626 IAW BOEING DWG # 146A8123 REV C. LOCATED AND DRILLED NEW SILL WEB AFT CARGO DOOR CUTOUT IAW SRM 51-40-05 AND BOEING DWG # 146A8123 REV C. INSTALLED NEW SILL WEB AFT CARGO DOOR CUTOUT IAW SRM 51-40-02 AND BOEING DWG # 146A8123 REV C. ATAG # WN9626 P/N - 146A8123U6

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 727A TO BS 727B, LBL 45. REPAIRED SEAT TRACK CROWN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT SIDEWALL SUPPORT ANGLE CRACKED AT BS 727D, BETWEEN STR 19L TO STR 25L. R&R SUPPORT ANGLE PER SRM AND DWG.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT R\H Z-ANGLE STA 727 TO STA 767 HAS CORROSION ON UPPER AND LOWER SURFACE. / REMOVED AND EVALUARED CORROSION. BLEND DEPTH .030' FROM ORIGINAL .040' WITH .010' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED Z-ANGLE STA 727 - 767 RH PER SRM 51-40-02-0G-0 AND DWG 146A7500 REV A

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT FLOORBOARD SUPPORT SHIELD STA 767 TO STA 792 RBL 22 UPPER AND LOWER SURFACE AT NUTPLATE HOLES HAS CORROSION. / REMOVED AND EVALUATED CORROSION. BLEND DEPTH .020' ORIGINAL .051' REMAINING .031'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. AAR TOOL 38289 DUE DATE 04/13/19. REMOVED SUPPORT SHIELD IAW SRM 51-40-02. VERIFIED NEW SUPPORT SHIELD P/N 146A8127U1 / 7530271 ON ATAG # WN5340 IAW BOEING DRAWING # 145A8127 REV C. LOCATED AND DRILLED NEW FLOOR SHIELD IAW SRM 51-40-05. AND BOEING DRAWING # 146A8127 REV C. INSTALLED NEW FLOOR SHIELD IAW SRM 51-40-02 AND BOEING DRAWING # 146A8127 REV C. ATAG # WN5340

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT BULKHEAD LOWER SUPPORT STA 847 TO STA 867 LBL 20 HAS CORROSION. / REMOVED AND EVALUATED CORROSION ON LOWER SUPPORT. BLENDED CORROSION ORIGINAL THICKKNESS .124' REMOVED .024'; REMAINING .094'. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-2. AAR TOOL 38289 CAL DUE 04/03/19. REMOVED LOWER SUPPORT AFT CARGO IAW SRM 51-4-02. VERIFIED NEW AFT CARGO LOWER SUPPORT STA 847 - 867 LBL 20 P/N - 146A8109UR4 ON ATAG # ZJ0251 IAW BOEING DWG # 148A8102. LOCATED AND DRILLED NEW LOWER SUPPORT IAW SRM 51-40-05 AND BOEING DWG # 149A8102. INSTALLED NEW LOWER SUPPORT AFT CARGO STA 847 - 867 LBL 20 IAW SRM 51-40-02 AND BOEING DWG # A1498102. ATAG # ZJ0251 P/N - 149A819U124

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 69,068 hrs · 40,761 cycles

PASSENGER CABIN;RH INBD SEAT TRACK LOWER CENTER CORRODED STA 827-832 / SEAT TRACK SEGMENT WAS REMOVED AND REPLACED FROM STA 807+10 TO STA 887; RBL 24. SEE NRC X881996 SAM 326 E356241 ITEM 3.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE FLOORBOARD SUPPORT STRAP STA 887 LBL 10 TO RBL 20 HAS CORROSION. / REPLACED TEE STRAP ASSY ON TABLE PER AIPC 53-42-11-30. STRAP PART #146A9401-39 STA887 LBL10 TO RBL20 TO BE INSTALLED ON CUSTOMER ORDER JPANEL-141-CLOSE.

Part: SUPPORT STRAP — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE; LOWER SILL SUPPORT STRAP STA 780 TO STA 800 RBL 19 HAS CORROSION. / REMOVED CORROSION PER SRM 51-10-02-0G-0. BLEND DIMENSIONS 1' X 3' WITH MAX DEPTH OF .025' FROM ORIGINAL .162 WITH .142' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A. REMOVED AND REPLACDED LOWER SILL SUPPORT STRAP STA 790 TO STA 775 PER DWG 146A8920 REV A AND SRM 51-40-02-0G-0 ATAG # R10122

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT FLOOR TRACK STA 927 TO 947 LBL 3 HAS CORROSION AT NUTPLATE HOLES. / EVALUATED TRACK ASSY AFT CARGO STA 887 - 947. 100% MATERIAL LOSS ON TRACK ASSY. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. ORIGINAL THICKNESS .071'; REMAINING .000'. REMOVED TRACK ASSY AFT CARGO STA 887 - 947 LBL 3 IAW SRM 51-40-02. VERIFIED NEW TRACK ASSY AFT CARGO STA 887 - 947 LBL 3 P/N - 147A7501U13 ON ATAG # WN8780 IAW BOEING DWG # 147A7801 REV B. LOCATED AND DRILLED NEW TRACK ASSY AFT CARGO STA 887 - 947 LBL 3 IAW SRM 51-40-05 AND BOEING DWG # 147A7501 REV B. INSTALLED NEW TRACK ASSY AFT CARGO STA 887 - 947 LBL 3 IAW SRM 51-40-02 AND BOEING DWG # 147A7501 REV B.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT R\H Z-ANGLE STA 927 TO STA 947 UPPER AND LOWER SURFACE HAS CORROSION. / REMOVED AND EVALUATED CORROSION. BLEND DEPTH .010' FROM ORIGINA; .040' WITH .030' REMAINING BLEND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED Z-ANGLE STA 887 TO 947 PER SRM 51-40-02-0G-0 AND DWG 146A500 REV A

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS 500D+8 TO BS 520, LBL 24. R&R SEAT TRACK IAW SRM & EA.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT R\H Z-ANGLE STA 867 TO STA 887 HAS CORROSION. / REMOVED AND EVALUATED CORROSION. BLEND DEPTH FOUND TO BE .010 ' FROM ORIGINAL .040' WITH .030' REMAINING BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED Z-ANGLE STA 887 TO STA 867 PER DWG 146A7500 REV A AND SRM 51-40-02-06-0

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 69,068 hrs · 40,761 cycles

PASSENGER CABIN; STA 827+12 TO 847+10; LBL 24; TOP AND INSIDE SEAT TRACK CROWN HAS CORROSION / BLENDED DAMAGED AREA IAW BOEING 73 SRM 51-10-02-0G-0. MATERIAL REMOVED .037' ON TOP OF CROWN FOUND TO BE OUT OF LIMITS IAW BOEING 737 SRM 53-00-52-1A-1; RMOVED DAMAGED SECTION OF SEAT TRACK AT S7A 827 TO 887 LBL 24 IAW B737 SRM 53-00-52-2R-5. LOCATED AND FABRICATED NEW SEAT TRACK AND REPAIR SPLICES IAW B737 SRM 51-40-05. SRM 53-00-52-2R-5. FABRICATED REPAIR ANGLE AND DRILLING OF 3-4-5 STRAPS IAW B737 SRM 53-00-52-2R-5. INSTALLED REPAIR SLPICE AND SEAT TRACK IAW B737 53-00-52-2R-5.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 69,068 hrs · 40,761 cycles

PASSENGER CABIN; STA 559+10 TO 578+12; LBL 45; TOP AND INSIDE SEAT TRACK CROWN HAS CORROSION / REMOVED CORROSION @ STA 569-580 LBL 45 VERIFIED W/ 10X MAG NO DAMAGE NOTED MAX ALLOWED CROWN .020 LOSS .011 CHANNE .040 LOSS .078 AT 580+12 CHANNEL MAX IS .040 LOSS .006 CROWN MAX IS .020 LOSS .011 FOUND TO BE IN LIMITS IAW SRM 53-00-52-1A-1 OUT OF LIMITS @ STA 569-580 MATERIAL VERIFICATION IS PN BAC1520-2779 7178-T6 IAW SRM 53-00-52-2R-3 REPAIR 3 FABRICATED AND INSTALLED NEW SEAT TRACK REPAIR IAW SRM 53-00-52-2R-3 REPAIR 3 FIG 202

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 69,068 hrs · 40,761 cycles

PASSANGER CABIN; STA 540; BL0 TO RBL 24; LATERAL FLOOR SUPPORT IS CRACKED ON INBOARD END. / REMOVED AND REPLACED THE PASSENGER CABIN; LATERAL FLOOR SUPPORT AT STA 540; BL 0 - RBL 24. IAW DWG 143A0060 REV B AND SRM 51-40-02 AND 51-40-05 ATAG WN7066

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

AFT CABIN R2 DOOR CREASE BEAM CORRODED BETWEEN BS 947 TO BS 992, RBL 60. R&R CREASE BEAM IAW SRM & DWG.

Part: ANGLE — CORRODED (FED THRESHOLD) · airframe 69,068 hrs · 40,761 cycles

L-1 DOOR CUTOUT SILL; THESHOLD SUPPORT ANGLE LBL 62 HAS CORROSION. / REMOVED CORROSION FROM L-1 DOOR CUTOUT SILL THESHOLD SUPPORT ANGLE LBL 62; ORIGINAL MATERIAL THICKNESS 0.050'. REMAINING MATERIAL THICKNESS 0.034' MAT MATERIAL LOSS OF .016'; FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1 STEP 4.B. REMOVED AND REPLACED L-1 DOOR THRESHOLD SUPPORT ANGLE LBL 62 IAW SRM 51-40-02-06-0 AND DWG #141A8110 REV A TAG:WN:7821 P/N:7530973 141A8112-2

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 69,068 hrs · 40,761 cycles

AFT CARGO COMPARTMENT PANEL 140CF HAS AREAS OF CORROSION ALONG THE OUTER EDGES. / REMOVED AND EVALUATED CORRSION. BLEND DIMENSION 5' X 2' WITH MAX DEPTH OF .040' FROM ORIGINAL .080' WITH .040'. BLEND FOUND TO BE OUT OF LIMITS ON SRM 53-00-53-1A-1. REPLACED PANEL ON TABLE PER AIPC 25-52-10-02. P/N 453A2610-1

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

STRINGER CLIP CRACKED AT BS 480, STR 6L. R&R TIE CLIP IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (MID CABIN) · airframe 69,068 hrs · 40,761 cycles

LEFT CABIN INTERCOSTAL STA 616-639 BELOW STR 5L HAS CORROSION ON INBOARD FLANGE / LEFT CABIN INTERCOSTAL WAS CORRONDED OUT OF LIMITS NEW INTER WAS FABRICATED IN THE BACK SHOP. ON WORK ORDER 38882-2400-0002 AND INSTALLED WORK WAS DONE IAW SRM 57-40-02-0G-0 AND 144A9433 BOEING DWG; ORG 'T' .063' REM 'T' .052' LOSS OF .011' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

FRAME ABOVE L1 DOORWAY CRACKED AT BS 312, STR 6L. REPAIRED FRAME IAW EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 69,068 hrs · 40,761 cycles

L1 DOOR CUTOUT CREASE BEAM CHORD ATTACH ANGLE CORRODED. R&R CHORD IAW SRM & DWG.

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 69,068 hrs · 40,761 cycles

RT WING FUEL PANEL DOOR 621 GB INNER SURFACE DELAMED / PANEL REPAIRED REF SRM 51-41-01 LIGHT OPS CK ON FUEL PANEL OPS CK GOOD REF B 737 AMM 28-21-21-960-801

Part: PANEL — DELAMINATED (LEFT WING) · airframe 69,068 hrs · 40,761 cycles

LH WING PANEL 521 WB HAS TWO CORNERS DISBONDING. / REPAIRED PANEL 521 WB IN CORNERS DISBONDED IAW B 737 SRM 57-41-01-2R-6 REPAIR 6 AMM 51-21-99-300-801

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,785 hrs · 40,582 cycles

FORWARD GALLEY EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER AMM.

Part: RIB — CRACKED (LT MLG DOOR) · airframe 67,503 hrs · 39,759 cycles

LT MAIN GEAR MIDDLE DOOR CRACKED RIB ABOVE LOWER FORWARD ATTACH POINT. R&R DOOR PER MM.

Part: STIFFENER — CRACKED (LT WING) · airframe 67,495 hrs · 39,754 cycles

LEFT PYLON AFT STRUT FAIRING HAS A CRACKED STIFFENER ABOVE FWD END OF THRUST TUBE. / FABRICATED REPLACEMENT PART PER BOEING DWG 313A2300 ID 003.INSTALLED PER SRM 51-40-02.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,344 hrs · 39,659 cycles

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

Part: HOOK AND LOOP — MISSING (EMERGENCY EXIT) · airframe 65,357 hrs · 38,424 cycles

LT EMERGENCY EXIT RED PULL STRAP STOWAGE TRIM MISSING SOME HOOK AND LOOP. R&R HOOK AND LOOP PER SIP.

Part: MOUNT — CRACKED (R1 DOOR) · airframe 65,357 hrs · 38,424 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT MOUNT NUTPLATE CRACKED. R&R MOUNT ASSEMBLY PER SRM.

Part: PANEL — CRACKED (RT WING) · airframe 65,300 hrs · 38,388 cycles

SUPPLEMENTAL INFORMATION: RIGHT WING LOWER SURFACE PANEL 621 VB CRACKED / REPLACED RIGHT WING LOWER SURFACE PANEL 621VB REF AMM 57-41-02_REF: SA-M 326 A1004274

Part: WEB — CRACKED (RT MLG WW) · airframe 65,139 hrs · 38,278 cycles

RT WHEEL WELL BEADED WEB CRACKED AT BS 665, RBL 42.0. REPAIRED WEB PER EA.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 64,568 hrs · 37,887 cycles

RT EMERGENCY AISLE LIGHT INOP AT ROW 11. REPAIRED CONNECTOR PER MM.

Part: HOLDER — LOOSE (R1 DOOR GIRT BAR) · airframe 63,729 hrs · 37,396 cycles

R1 DOOR SLIDE GIRT BAR SUPPORT BAR LOOSE. ADJUSTED THE HOLDER IAW MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 62,496 hrs · 36,676 cycles

RIGHT EMERGENCY EXIT HATCH LIGHT LOWER POSITION LAMP INOPERATIVE. R & R THE LIGHT IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,496 hrs · 36,676 cycles

EMERGENCY LIGHT BATTERY M1674 FAILED TEST. R & R BATTERY PACK IAW MM.

Part: ANGLE — CRACKED (MLG WHEEL WELL) · airframe 62,496 hrs · 36,676 cycles

MLG W/W BULKHEAD ANGLE CRACKED AT BS 663, LT SIDE. R & R THE ANGLE IAW SRM.

Part: ANGLE — CRACKED (BS 294) · airframe 62,496 hrs · 36,676 cycles

FWD GALLEY AREA ANGLE CRACKED AT BS 294.5. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (CARGO BAY) · airframe 62,496 hrs · 36,676 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500C, STR 26L. R&R ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (BS 294) · airframe 62,496 hrs · 36,676 cycles

STUB FRAME CRACKED AT BS 294.5, BETWEEN STRINGERS 15 AND 17R. R & R FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, RBL 55.5. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

SUPPORT ZEE INNER CHORD CRACKED AT BS 294.5, RBL 54. R&R CHORD IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 400-420) · airframe 62,496 hrs · 36,676 cycles

FORWARD CARGO BAY WEB INTERCOSTAL CRACKED BETWEEN BS 400 - 420, STRINGER 26L. R & R INTERCOSTAL IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (BS 294) · airframe 62,496 hrs · 36,676 cycles

FLOORBEAM CRACKED AT BS 294.5, RBL 53. REPAIRED THE FLOORBEAM IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 62,496 hrs · 36,676 cycles

RT WING OUTBOARD AFT FLAP TRAILING EDGE DELAMINATED INBOARD POSITION. REPAIRED AFT FLAP IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

FLOOR STRUCTURE SUPPORT CHANNEL CRACKED BETWEEN BS 294.5 TO BS 312, RBL 15. R&R CHANNEL IAW SRM AND DWG.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

SUPPORT CHANNEL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R CHANNEL IAW SRM AND DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

SUPPORT CLIP CRACKED AT BS 807, STR 26R. R&R CLIP IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

FLOOR STRUCTURE WEB INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, BL 0. R&R INTERCOSTAL AW SRM AND DWG.

Part: SKIN — DELAMINATED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

SKIN DELAMINATED AT BS 1156+11.250, LBL 12. REPAIRED SKIN IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

FLOOR STRUCTURE WEB INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

WEB INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R&R INTERCOSTAL IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

AFT CARGO COMPARTMENT SUPPORT CLIP CRACKED AT BS 827, STR 26R. R&R CLIP IAW SRM AND DWG.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

FLOOR STRUCTURE SUPPORT CHANNEL CRACKED BETWEEN BS 344 TO BS 360, RBL 12. R&R CHANNEL IAW SRM AND DWG.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 62,496 hrs · 36,676 cycles

LT FORWARD GALLEY AREA FLASHLIGHT BASE BROKEN. R&R FLASHLIGHT IAW CMM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

AFT CARGO COMPARTMENT CHANNEL CRACKED BETWEEN BS 847 TO BS 867, STR 25R. R&R CHANNEL IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 62,496 hrs · 36,676 cycles

AFT GALLEY AREA EMERGENCY LIGHT BASE LENS BROKEN. R&R LENS IAW AMM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 767 TO BS 794, STR 25R. R&R CHANNEL IAW SRM AND DWG.

Part: NUT PLATE — BROKEN (R2 DOOR) · airframe 62,496 hrs · 36,676 cycles

R2 DOOR GIRT BAR FITTING NUT PLATE BROKEN AT BS 986.5. R&R NUT PLATE IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

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

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 62,496 hrs · 36,676 cycles

AFT GALLEY AREA FLASHLIGHT BASE BROKEN. R&R FLASHLIGHT IAW CMM.

Part: LIGHT — CRACKED (CABIN FLOOR) · airframe 62,496 hrs · 36,676 cycles

EMERGENCY LIGHT CRACKED AT FWD END. R & R THE EMERGENCY LIGHT STRIP IAW MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

FORWARD CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 492.4 TO BS 500A, RBL 21.8. R&R CHANNEL IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500B, STR 26L. R&R ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 400) · airframe 62,496 hrs · 36,676 cycles

FORWARD CARGO BAY ANGLE CRACKED AT BS 400, STRINGER 26L. R & R THE ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

FORWARD CARGO COMPARTMENT WEB CRACKED BETWEEN BS 500 TO BS 500A, STR 26L. R&R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

FORWARD CARGO COMPARTMENT WEB CRACKED BETWEEN BS 500A TO BS 500B, STR 26L. R&R WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

FORWARD CARGO COMPARTMENT WEB CRACKED BETWEEN BS 500B TO BS 500C, STR 26L. R&R WEB IAW SRM AND DWG.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 62,496 hrs · 36,676 cycles

EXIT LIGHT LENS BROKEN AT FWD LAV WALL AREA. R & R THE LIGHT ASSY IAW MM.

Part: FITTING — CRACKED (LT WING) · airframe 62,496 hrs · 36,676 cycles

LT WING INBOARD FIXED TRAILING EDGE FITTING CRACKED ON RSS 270. R&R FITTING IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,496 hrs · 36,676 cycles

FORWARD CARGO COMPARTMENT ANGLE CLIP CRACKED AT BS 500C, STR 26L. R&R CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 62,496 hrs · 36,676 cycles

RIGHT WING OUTBD AFT T/E FLAP L/E SKIN CRACKED. REPAIRED THE SKIN IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 61,868 hrs · 36,305 cycles

AFT EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY IAW SIP.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 61,475 hrs · 36,078 cycles

LEFT WING NR 2 LEADING EDGE SLAT CRACKED AT SS 322.71 LOWER TRAILING EDGE FASTENER. REPAIRED THE SLAT IAW EA.

Part: LENS — MISSING (CABIN) · airframe 60,215 hrs · 35,325 cycles

LEFT OVERWING EXIT SIDE LENS MISSING. INSTALLED LENS IAW SIP.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 59,222 hrs · 34,745 cycles

L2 DOOR EMER EVAC SLIDE GIRT OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,222 hrs · 34,745 cycles

M01675 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,222 hrs · 34,745 cycles

M01670 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,222 hrs · 34,745 cycles

M01669 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 59,222 hrs · 34,745 cycles

RIGHT MLG WW FWD BULKHEAD, LOWER VAPOR BARRIER CRACKED AT BS 663, RBL 10. REPAIR BARRIER IAW EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,222 hrs · 34,745 cycles

M01672 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 59,222 hrs · 34,745 cycles

R1 DOOR EMER EVAC SLIDE GIRT OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,222 hrs · 34,745 cycles

M01668 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 59,222 hrs · 34,745 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,222 hrs · 34,745 cycles

M01673 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 59,222 hrs · 34,745 cycles

RIGHT MLG WW FWD BULKHEAD, LOWER VAPOR BARRIER CRACKED AT BS 663, RBL 16. REPAIRED BARRIER IAW EA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 58,785 hrs · 34,499 cycles

AFT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 58,484 hrs · 34,311 cycles

R1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: BRACKET — CRACKED (RT SPOILER) · airframe 57,048 hrs · 33,484 cycles

RIGHT WING UPPER TE SHELF PANEL OTBD NR 7 SPOILER ANGLE BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: WEB — CRACKED (NR 7 SPOILER) · airframe 57,048 hrs · 33,484 cycles

RIGHT WING UPPER TE SHELF PANEL OTBD NR 7 SPOILER HORIZONTAL WEB CRACKED AT UPPER OTBD CORNER. REPAIRED WEB IAW SRM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 57,048 hrs · 33,484 cycles

RIGHT WING INBD AFT FLAP OTBD TRACK AFT ATTACH POINT LOOSE. R & R FLAP TRACK IAW AMM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 57,048 hrs · 33,484 cycles

RIGHT WING INBD AFT FLAP INBD TRACK AFT ATTACH POINT LOOSE. R & R FLAP TRACK IAW AMM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 57,048 hrs · 33,484 cycles

RIGHT WING OTBD AFT FLAP NR 4 TRACK AFT ATTACH POINT LOOSE. R & R FLAP TRACK IAW AMM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 57,048 hrs · 33,484 cycles

RIGHT WING OTBD AFT FLAP NR 2 TRACK AFT ATTACH POINT LOOSE. R & R FLAP TRACK IAW MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

AFT SEAT TRACK OTBD HOLE SPLICE STRAP CRACKED AT BS 727B, LBL 45.5. REPAIRED STRAP IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

SPLICE STRAP CRACKED AT BS 727B, LBL 45.5. REPAIRED STRAP IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

SPLICE STRAP CRACKED AT BS 727B, RBL 45.5. REPAIRED STRAP IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

SPLICE STRAP CRACKED AT BS 727B, RBL 24.75. REPAIRED STRAP IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

SPLICE STRAP CRACKED AT BS 727B, LBL 24.75. REPAIRED STRAP IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

FRAME CRACKED AT BS 520, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

FRAME CRACKED AT BS 520, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,015 hrs · 33,467 cycles

FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,015 hrs · 33,467 cycles

RIGHT WING NR 5 SLAT NOSE SKIN CRACKED AT ACTUATOR MOUNT. REPAIRED SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,015 hrs · 33,467 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN LBL 24.92 - 31.83. REPAIRED WEB IAW FAS EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,015 hrs · 33,467 cycles

RIGHT WING NR 7 SLAT NOSE SKIN CRACKED AT ACTUATOR MOUNT. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,922 hrs · 31,074 cycles

LT NR 1 WINDOW FRAME CRACKED AT OTBD UPPER FASTENER HOLE. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,922 hrs · 31,074 cycles

LT NR 1 WINDOW FRAME CRACKED AT OTBD UPPER CORNER. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,922 hrs · 31,074 cycles

RT NR 1 WINDOW FRAME CRACKED AT UPPER OTBD INNER CORNER. R & R FRAME IAW ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,922 hrs · 31,074 cycles

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

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 52,922 hrs · 31,074 cycles

LT HORIZONTAL STABILIZER RIB AT 92.70 CRACKED ON LOWER FLANGE AT FWD VERTICAL STIFFENER. REPAIRED RIB IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,922 hrs · 31,074 cycles

RT NR 3 WINDOW FRAME CRACKED BETWEEN THE 2ND & 3RD FASTENER HOLES FROM THE BOTTOM. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 52,922 hrs · 31,074 cycles

LT NR 3 WINDOW FRAME CRACKED ON THE 2ND FASTENER HOLE FROM THE BOTTOM. REPAIRED FRAME IAW ACO.

Part: SIGN — BROKEN (CABIN) · airframe 52,669 hrs · 30,935 cycles

L2 DOOR EMERGENCY EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 51,597 hrs · 30,316 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: ATTACH BRACKET — CRACKED (VERTICAL STAB) · airframe 50,676 hrs · 29,758 cycles

VERTICAL STAB FRONT SPAR SPRING ATTACH BRACKET CRACKED AT BOTH LT AND RT NOTCHED RADIUS. R & R BRACKET IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,285 hrs · 29,519 cycles

T-ANGLE CORRODED IN AFT CARGO BIN AT RIGHT BS 727D. REMOVED AND REPLACED T-ANGLE PER SRM.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 48,097 hrs · 28,128 cycles

F/O'S SLIDING WINDOW EMERGENCY RELEASE HANDLE WOULD NOT OPEN. ADJUSTED WINDOW PER MM.

Part: LENS — MISSING (CABIN) · airframe 47,251 hrs · 27,622 cycles

RIGHT EMERGENCY EXIT LIGHT LENS MISSING AT ROW 21. INSTALLED LENS PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,930 hrs · 26,885 cycles

DURING SCHEDULED OTS CHECK, FOUND WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,930 hrs · 26,885 cycles

DURING SCHEDULED OTS CHECK, FOUND WEB CRACKED AT BS 663, RBL 35. REPAIRED WEB PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,930 hrs · 26,885 cycles

DURING SCHEDULED OTS CHECK, FOUND WEB CRACKED AT BS 663, LBL 33. REPAIRED WEB PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,930 hrs · 26,885 cycles

DURING SCHEDULED OTS CHECK, FOUND WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 45,864 hrs · 26,838 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 45,376 hrs · 26,543 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS LENS LOOSE AT ROW 4. SECURED LENS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 44,913 hrs · 26,264 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT LIGHT INOP BETWEEN ROW 15 TO ROW 18. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,694 hrs · 26,128 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,306 hrs · 25,911 cycles

L1 DOOR EMERGENCY EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM AND MT.

Part: BATTERY — FAILED (CABIN) · airframe 44,150 hrs · 25,815 cycles

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

Part: SIGN — MISSING (CABIN) · airframe 43,590 hrs · 25,492 cycles

R1 DOOR EMERGENCY EXIT CAP MISSING. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,533 hrs · 25,457 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,533 hrs · 25,457 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS360, STR 8R. REPAIRED FRAME PER EA.

Part: CONNECTOR — BROKEN (CABIN) · airframe 43,533 hrs · 25,457 cycles

DURING SCHEDULED 12Y CHECK, FOUND EEPLS CONNECTORS BROKEN. REMOVED AND REPLACED CONNECTOR PER WDM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,533 hrs · 25,457 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE CORRODED BETWEEN BS 727D+5 TO BS 772, LBL 12. REPAIRED ANGLE PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 43,533 hrs · 25,457 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,533 hrs · 25,457 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO DOOR CUTOUT SUB THRESHOLD WEB CORRODED. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,533 hrs · 25,457 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO DOOR CUTOUT STRAP CORRODED BETWEEN BS 787 TO BS 827, RBL 19. REMOVED AND REPLACED STRAP PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,533 hrs · 25,457 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT ANGLE CORRODED BETWEEN BS 727D+5, BS 772, LBL 8. REPAIRED ANGLE PER SRM.

Part: SWITCH — FAULTY (HYDRAULIC SYS) · airframe 43,074 hrs · 25,199 cycles

DIVERSION - NR 1 ENGINE A HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE PUMP LIGHT SWITCH PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 42,073 hrs · 24,586 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: FITTING — LOOSE (GIRT BAR) · airframe 39,967 hrs · 23,353 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FLOOR FITTING LOOSE. SECURED FITTING PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 39,792 hrs · 23,247 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 39,792 hrs · 23,247 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 39,792 hrs · 23,247 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,105 hrs · 21,627 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED BEAM PER SWA EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 37,105 hrs · 21,627 cycles

DURING SCHEDULED 10Y CHECK, FOUND KEEL BEAM CRACKED AT BULKHEAD BS 663, LBL 10. REPAIRED BEAM PER SWA EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 37,105 hrs · 21,627 cycles

DURING SCHEDULED 10Y CHECK, FOUND KEEL BEAM CRACKED AT BULKHEAD BS 663, RBL 10. REPAIRED BEAM PER SWA EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 34,737 hrs · 20,193 cycles

EEPLS LENS LOOSE AT ROW 16 ABC. SECURED LENS PER MM.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 32,099 hrs · 18,589 cycles

ELECTRICAL SMELL IN CABIN, NO SMOKE PRESENT. GASPER FAN CIRCUIT BREAKER POPPED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,508 hrs · 17,608 cycles

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

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 30,301 hrs · 17,486 cycles

DURING SCHEDULED HC2 CHECK, FOUND LH WING OUTBOARD T/E AFT FLAP INBOARD LOWER SURFACE DELAMINATED. R&R AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 30,116 hrs · 17,381 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,867 hrs · 17,214 cycles

DURING SCHEDULED 8Y CHECK, FOUND LEFT HORIZONTAL STAB LOWER SKIN CRACKED 12 INCHES FROM AFT SPAR, 27 INCHES FROM INBOARD EDGE. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 28,646 hrs · 16,539 cycles

EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.

Part: SLIDE — OUT OF POSITION (CABIN) · airframe 28,140 hrs · 16,248 cycles

EVAC SLIDES OUT OF POSITION. REPOSITIONED EVAC SLIDES PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 28,146 hrs · 16,248 cycles

DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED DEEP CYCLE TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,068 hrs · 15,592 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 23,291 hrs · 13,415 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,300 hrs · 12,269 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHTS AT ROWS 1 ABC AND 2 ABC, INOP. REMOVED AND REPLACED LIGHT ASSY'S PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 20,097 hrs · 11,592 cycles

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

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 16,104 hrs · 9,400 cycles

DURING SCHEDULED C3 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 15,982 hrs · 9,337 cycles

DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 11,232 hrs · 6,629 cycles

DURING SCHEDULED SERVICE CHECK,SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 2 AND NR 4 HINGES WORN. REMOVED AND REPLACED NR 2 AND NR 4 TAB HINGE BUSHINGS PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,239 hrs · 6,074 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS INOP ROWS 1 TO 4. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 10,163 hrs · 6,032 cycles

AFTER TAKEOFF, FWD ENTRY EMERGENCY EXIT LIGHT AND EEPLS AT ROW 1 ILLUMINATED. CYCLING LIGHT SW OFF AND ON HAD NO EFFECT. LIGHTS WENT OUT AFTER ABOUT 30 MINUTES. TESTED LIGHTS PER MM. NO DEFECTS NOTED.

Part: COVER — CRACKED (CABIN) · airframe 5,719 hrs · 3,447 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 1. R&R TRACK COVER PER MM.

Part: BATTERY — DISCHARGED (E/E BAY) · airframe 5,048 hrs · 3,009 cycles

DIVERSION, AIRCRAFT BATTERY AMP INDICATED -3 OR -4 AT ALL TIMES. RESET STANDBY PCU AND REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — MISSING (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER MISSING AT OVERWING EXIT. REPLACED COVER PER MM.

Part: STARTER — CRACKED (NR 1 ENGINE)

IN FLIGHT ENG SHUT DOWN, DIVERSION, NR 1 ENG LOW OIL PRESS LIGHT ILUMINATED, OIL QTY INDICATION WAS ZERO. ENGINE WAS SHUT DOWN AND DIVERTED FLIGHT TO COS. FOUND CRACKED STARTER. REMOVED AND REPLACED NR 1 ENG STARTER, SERVICED ENG WITH OIL. LEAK AND OPS CHECKED GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

AIR TURNBACK---- LOUD NOISE APPEARS TO COME FROM F/O'S WINDOW ABOVE 9000 FEET. FOUND FWD AND AFT LAV SMOKE DETECTORS ALARMING. REMOVED AND REPLACED SMOKE DETECTORS PER MM, NOISE WENT AWAY.