N432WN

Part: TAILPIPE — FIRE (#1 ENG) · airframe 65,656 hrs · 38,970 cycles

AIRCRAFT BEHIND US REPORTED TAILPIPE FIRE AS WE TOOK THE RUNWAY. #1 ENGINE. / [01] FOUND OIL PUDDLING IN THE CENTER PLUG CAVITY. PERFORMED FIM 71-05 TASK 811. CLEANED WET AREA AND PERFORMED IDLE RUN. NO FURTHER DEFECTS NOTED.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 65,541 hrs · 38,898 cycles

FORWARD ENTRY GIRT BAR RETAINING CLIP LOOSE / [01] SECURED CLIP REF SIP

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 64,780 hrs · 38,385 cycles

AFT SERVICE DOOR OVERHEAD EXIT SIGN FAILS TO ILLUMINATE DURING E-LIGHT CHECK / [01] R/R'D M1672 E-LIGHT BATTERY PACK REF AMM 33-51-06

Part: SUPPORT ANGLE — CRACKED (L/H MLG W/W) · airframe 63,452 hrs · 37,595 cycles

SUPPLEMENTAL INFORMATION: ONE CRACK ON LEFT MLG WHEEL WELL RING INBOARD VERTICAL SUPPORT ANGLE. ; ONE CRACK ON LEFT MLG WHEEL WELL RING INOARD VERTICAL SPPORT ANGLE. / [01] INSTALLED NEW VERTICAL ANGLE PER SRM 51-40-02 AND BOEING DWG# 149A7610; [02] INSTALLED NEW VERTICAL ANGLE PER SRM 51-40-02 AND BOEING DWG# 149A7610

Part: NONE — CRACKED (L/H MLG W/W) · airframe 63,452 hrs · 37,595 cycles

SUPPLEMENTAL INFORMATION: ONE CRACK ON LEFT MLG WHEEL WELL RING INBOARD TEE CLIP. ; ONE CRACK ON LEFT MLG WHEEL WELL RING INOARD TEE CLIP. / [01] INSTALLED NEW TEE CLIP PER SRM 51-40-02 AND BOEING DWG# 149A7610; [02] INSTALLED NEW TEE CLIP PER SRM 51-40-02 AND BOEING DWG# 149A7610

Part: PANEL — ELONGATED (FUSELAGE) · airframe 63,452 hrs · 37,595 cycles

SUPPLEMENTAL INFORMATION: 194E PANEL HAS ELONGATED HOLES WITH CRACKS EXTENDING FROM HOLES AT SEVERAL PLACES. / [01] DRILLED ; COUNTERSUNK ; TRIMMED NEW 194 E PANEL <BR>REF SRM 51-20-07

Part: NONE — CORRODED (FUSELAGE) · airframe 63,316 hrs · 37,518 cycles

AFT CARGO COMPARTMENT DOORWAY LOWER SILL WEB HAS CORROSION ON SURFACE ; / [01] BLENDED CORROSION AND VERIFIED WITH 10X MAG IAW SRM 53-60-15-1A-1; [02] UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .045'; LOSS .008'; REMAINING .037'. TOOL#40084; DUE 11AUG22; [03] VERIFIED MATERIAL LOSS TO BE .008'; ORIGINAL .045'; REMAINING .037' OUT OF LIMITS IAW SRM 53-60-15-1A-1; [04] REMOVED WEB IAW SRM 51-40-02-0G-0; [05] NEW WEB VERIFIED AS P/N 146A8123-25 WN6549 IAW DWG 146A8340 SHT 9 REV A; [06] STEP 5 C/W; [07] LOCATED AND DRILLED NEW WEB IAW SRM 51-40-05-0G-0 AND DWG 146A8340 SHT 9 REV A; [08] STEP 7 OK; [09] COMPLETED FABRICATED NEW WEB COUNTERSINKED FASTENER HOLES ;INSTALLED NUT PLATES IAW SRM 51-40-05-0G-0 ALSO DWG 146A8340 REV A; [10] INSPECTION CW STEP 9; [11] APPLIED CIC TO LOWER SURFACE OF WEB AND INTERAL AREA ON A/C IAW AMM 51-21-91-701; [12] NEED OK TO INSTALL; [13] OK TO INSTALL; [14] STARTED INSTALLING NEW WEB AT AFT CARGO IAW SRM 51-40-02-0G-0 ALSO BOEING DWG 146A8340 REV A; [15] INSPECTION C/W STEP 14; [16] FINISHED INSTALLED NEW WEB IAW SRM 51-40-02-0G-0 AND DWG 146A8340 SHT 9 REV A; [17] VERIFIED ITEM 16 OK TO CIC; [18] APPLIED CIC TO TOP SIDE OF NEW WEB IAW AMM 51-21-91-701; [19] ACP RII INSP REF ITEM 16; [20] VERIFIED ITEM 18

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 63,316 hrs · 37,518 cycles

AFT CARGO COMPARTMENT DOORWAY LOWER SILL WEB HAS CORROSION ON SURFACE ; / [01] BLENDED CORROSION AND VERIFIED WITH 10X MAG IAW SRM 53-60-15-1A-1; [02] UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .045'; LOSS .008'; REMAINING .037'. TOOL#40084; DUE 11AUG22; [03] VERIFIED MATERIAL LOSS TO BE .008'; ORIGINAL .045'; REMAINING .037' OUT OF LIMITS IAW SRM 53-60-15-1A-1; [04] REMOVED WEB IAW SRM 51-40-02-0G-0; [05] NEW WEB VERIFIED AS P/N 146A8123-25 WN6549 IAW DWG 146A8340 SHT 9 REV A; [06] STEP 5 C/W; [07] LOCATED AND DRILLED NEW WEB IAW SRM 51-40-05-0G-0 AND DWG 146A8340 SHT 9 REV A; [08] STEP 7 OK; [09] COMPLETED FABRICATED NEW WEB COUNTERSINKED FASTENER HOLES ;INSTALLED NUT PLATES IAW SRM 51-40-05-0G-0 ALSO DWG 146A8340 REV A; [10] INSPECTION CW STEP 9; [11] APPLIED CIC TO LOWER SURFACE OF WEB AND INTERAL AREA ON A/C IAW AMM 51-21-91-701; [12] NEED OK TO INSTALL; [13] OK TO INSTALL; [14] STARTED INSTALLING NEW WEB AT AFT CARGO IAW SRM 51-40-02-0G-0 ALSO BOEING DWG 146A8340 REV A; [15] INSPECTION C/W STEP 14; [16] FINISHED INSTALLED NEW WEB IAW SRM 51-40-02-0G-0 AND DWG 146A8340 SHT 9 REV A; [17] VERIFIED ITEM 16 OK TO CIC; [18] APPLIED CIC TO TOP SIDE OF NEW WEB IAW AMM 51-21-91-701; [19] ACP RII INSP REF ITEM 16; [20] VERIFIED ITEM 18

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 63,245 hrs · 37,469 cycles

L/H HORIZONTAL LOWER INSPAR SKIN CRACKED AT STAB STA.193.90; APPROX. 16' AFT OF FRONT SPAR. VERIFIED BY HFEC. 1' IN LENGTH. ; / [01] EA SUMMARY ADDED TO THE FAULT.; [02] EA 21-155-03259WIP1 COMPLETED

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 62,678 hrs · 37,128 cycles

MEGA PHONE INOP ; / [01] R/R'D MEGA PHONE PER AMM 25-64-00. OPS CHECK @ THIS TIME.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,767 hrs · 36,021 cycles

INTERIOR OVERWING EXIT SIGN RIGHT SIDE INOPERABLE. CONNECTED INTERIOR RIGHT OVERWING EXIT SIGN CONNECTORS D12392 AND D12394, AS PER BOEING B737 AMM 33-51-010-960-802. OPERATIONAL CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 60,767 hrs · 36,021 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERABLE. RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT, AS PER BOEING B737 AMM 33-51-04-960-801 AND OPERATIONAL TEST OK.

Part: ANGLE — CRACKED (RT WING) · airframe 60,767 hrs · 36,021 cycles

RIGHT WING L/E I/B ON TOP OF FUEL BOOST PUMP FOUND ANGLE CRACKED. P/N 116A3939-2 / REMOVED AND REPLACED CRACK ANGLE ON R/H WING L/E I/B ON BOOST PUMP AREA PER REF SRM 57-20-10-1A-3; ANGLE P/N 116A3939-2

Part: ANGLE — CRACKED (LT WING) · airframe 60,767 hrs · 36,021 cycles

LEFT WING L/E I/B ON TOP OF BOOST PUMP FOUND ANGLE CRACKED P/N 116A3939-1 / REMOVED AND REPLACED LEFT WING L/E I/B ANGLE ON TOP OF BOOST PUMP P/N 116A3939-1 REF B737-7 SRM 57-20-10-1A-3 ALLOWABLE DAMAGE

Part: BAFFLE — CRACKED (BS 500B-500C) · airframe 60,767 hrs · 36,021 cycles

FWD CARGO COMP BAFFLE ASSY CRACKED BETWEEN BS 500B AND 500C LBL-21. / REPLACED BAFFLE ASSY @ FWD CARGO COMP. BETWEEN STA 500B AND 500C LBL-21/ AS PER B737-700 SRM 51-40-02-0G-0.

Part: BAFFLE — CRACKED (BS 500B-500C) · airframe 60,767 hrs · 36,021 cycles

FWD CARGO COMP BAFFLE ASSY CRACKED BETWEEN BS 500B AND 500C RBL-21 / REPLACED BAFFLE @ FWD CARGO COMP BETWEEN STA 500B & 500C @ RBL21 AS PER B737-700 SRM 51-40-02-0G-0

Part: RIB — CRACKED (VERTICAL STAB) · airframe 60,767 hrs · 36,021 cycles

DORSAL FIN RIB AT STA 867 ; RIB CRACK / REMOVED AND REPLACED DAMAGED RIB DORSAL FIN STA 867' PER REF B737 SRM 51-40-02-0G-0

Part: TIE DOWN — CORRODED (BS 787 S25L) · airframe 60,767 hrs · 36,021 cycles

AFT CARGO COMPT;SHOWS NET TIE-DOWN PLATE WITH SURFACE CORROSION;JUST AFT OF B.S.787 STR.25L.(MKD 26-002) / RECEIVED NEW TIE DOWN PLATE P/N 41901-102; NEW NET TIE DOWN PLATE TO BE INSTALLED ON T/C 753-105-01-01

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 60,767 hrs · 36,021 cycles

CORROSION SPOTS FOUND FWD CARGO COMPARTMENT RH 'Z' CHANNEL FROM STA 500A TO STA 500D RBL 21 @ WL 153.5 / REPLACED R/H 'Z' CHANNEL @ FWD CARGO COMP. FROM STA 500A TO STA 500D RBL 21 @ WL 153.5 AS PER B737-700 SRM 51-40-02-0G-0.

Part: STRAP — CORRODED (FWD CARGO) · airframe 60,767 hrs · 36,021 cycles

CORROSION SPOTS FOUND AT FWD CARGO STA 500 RBL 21 AND WL 153.5 / REMOVED CORROSION AT FWD CARGO STA 500 RBL 21 AND WL 153.5 OROGINAL MAT .100'; MAT LOSS .014'; MAT REMAINING .086' FOUND OUT OF LIMITS REMOVED AND REPLACED STARP AS PER B737-7 SRM 51-40-02-0G-0; DRAWING # 143A8125 SRM 51-10-02-0G-0; 53-30-15-1A-1; 51-40-05-0G-0 SOPM 20-50-19

Part: SUPPORT ANGLE — CORRODED (FWD CARGO) · airframe 60,767 hrs · 36,021 cycles

CORROSION SPOTS FOUND AT FWD CARGO AT STA 500D LOWER ANGLE SUPPORT AT LBL 10 AND LBL 21 AT WL 153.5 / REMOVED AND REPLACED LWR SUPPORT ANGLE AT FWD CARGO ON STA 500D BETWEEN LBL21 AND RBL 21 WL 153.5 REF B737-700 SRM 51-40-02-0G-0 AND DWG # 143A9481.

Part: CHANNEL — CORRODED (R2 DOOR AREA) · airframe 60,767 hrs · 36,021 cycles

CORROSION R2 DOOR Z-CHANNEL HAS CORROSION BETWEEN STA 951 TO STA 992 RBL 51 (203-011). REMOVED AND REPLACED R2 DOOR INNER CHORD, PER REF B737-700 SRM51-40-02-0G-0 AND DWG 147A8501.

Part: SUPPORT ANGLE — CORRODED (L1 THRESHOLD) · airframe 60,767 hrs · 36,021 cycles

L1 DOOR THRESHOLD @ STA328 - STA344 LBL 60 WL 208 L ANGLE SUPPORT HAS CORROSION. / REPLACED L ANGLE SUPPORT @ L1 DOOR THERSHOLD @ STA 328 - STA 344 LBL 60 WC 208 AS PER B737-700 SRM 51-40-02-06-0

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 60,767 hrs · 36,021 cycles

CORROSION SPOTS FOUND FWD CARGO COMPARTMENT RH 'Z' CHANNEL FROM STA 500 TO STA 500A AND WL153.5 @ RBL 21. / REPLACED RH Z CHANNEL @ FWD CARGO COMPARTMENT FROM STA 500 TO 500A RBL 21 & WL 153.5 AS PER B737-700 SRM 51-40-02-0G-0.

Part: CREASE BEAM — CORRODED (RT FUSELAGE) · airframe 60,767 hrs · 36,021 cycles

CORROSION, MAIN CABIN FLOOR CREASE BEAM INNER CHORD AT FASTENERS HEAD RBL 55 STA 616 &STA 639, MARKED DOTS 60-023. REMOVED AND INSTALLED NEW CREASE BEAM INNER CHORD AT MAIN CABIN FLOOR BETWEEN STA 626 TO STA 673 RBL 55', REF B737-7 SRM 51-40-0G-0 AND DWG NR 144A5901.

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 60,767 hrs · 36,021 cycles

CORROSION SPOTS FOUND AT FWD CARGO LH 'Z' CHANNEL FROM STA 400 TO STA 500D LBL 21 AT WL 153.5 / FWD CARGO L/H Z CHANNEL FROM STA 400 TO STA 500D CORROSION FOUND OUT OF LIMITS REF B737-700 SRM 53-00-53-1A-2 FIG 103 DETAIL D. REMOVED AND REPLACED Z CHANNEL BETWEEN STA 396 AND STA 500D LBL 21 WL 153.5 REF B737-700 SRM 53-00-53-2R-5 AND DWG #143A7500.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 60,767 hrs · 36,021 cycles

FWD WET AREA FLOOR AT STA 344-STA 360 BL 0 INTERCOSTAL UPPER SURFACE CRACKED (18-042). REPLACED INTERCOSTAL AT FWD WET AREA FLOOR AT STA 344-STA 360 BL, AS PER B737-700 SRM 51-40-02-0G-0 AND DWG 141A5400.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 60,767 hrs · 36,021 cycles

R/H CABIN FLOOR PANEL 232SF UPPER FWD I/B CORNER CRACKED. (18-034) / CLEANED AND REPAIRED PANEL #232SF AT I/B CORNER IN ACCORDANCE TO B737-7 SRM 53-00-50-2R-0. MATERIALS USED PO# 1693338 COMPOUND

Part: FLOOR SUPPORT — CRACKED (LT CABIN) · airframe 60,767 hrs · 36,021 cycles

LT FWD WET AREA FLOOR AT STA 294.5-STA 312 LBL 55 INNER CHORD UPPER SURFACE CRACKED (18-046). REPLACED INNER CHORD AT LT FWD WET AREA FLOOR AT STA 312-394.5 LBL 55, AS PER B737-700 SRM 51-40-02-0G-0.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,767 hrs · 36,021 cycles

RT FWD WET AREA FLOOR AT STA 328 RBL 48-RBL 56 FRAME UPPER AND LOWER SURFACES HAS CORROSION (18-047). ACCOMPLISHED THIS N/R ON EA NR 1-A53-8530 REV.

Part: FLOOR PANEL — DAMAGED (RT CABIN) · airframe 60,767 hrs · 36,021 cycles

RT CABIN FLOOR PANEL 232HF UPPER SKIN SURFACE HAS MATERIAL MISSING (18-039). REMOVED AND REPLACED FLOOR BOARD PANEL AT MAIN CABIN NR 232HF, IN REF B737-700 AMM 53-21-00-000-801 AND AMM 53-21-00-400-801 PO NR 169444 AAR ISSUE TAG FL3269.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 60,767 hrs · 36,021 cycles

RT FWD WET AREA FLOOR AT STA 312-STA 328 RBL 30.5 INTERCOSTAL CRACKED (18-049). REMOVED AND INSTALLED NEW INTERCOSTAL AT RT FWD AREA BETWEEN STA 312-328 RBL 30.5', REF B737-7 SRM 51-40-02-0G-0 AND DWG 141A5400.

Part: FLOOR PANEL — DAMAGED (RT CABIN) · airframe 60,767 hrs · 36,021 cycles

RT CABIN FLOOR PANEL 232EF UPPER SKIN SURFACE HAS MATERIAL MISSING (18-041). REMOVED AND REPLACED RT CABIN FLOOR PANEL 232EF, REF B737-7 AMM 53-21-00-000-801 AND 53-21-00-400-801.

Part: FLOOR PANEL — DAMAGED (RT CABIN) · airframe 60,767 hrs · 36,021 cycles

RT CABIN FLOOR PANEL 232GF UPPER SKIN SURFACE HAS MATERIAL MISSING (18-040). REMOVED AND REPLACED RT CABIN FLOOR PANEL 232GF, REF B737-700 AMM 53-21-00-000-801 AND 53-21-00-400-801.

Part: FLOOR PANEL — PEELING (RT CABIN) · airframe 60,767 hrs · 36,021 cycles

RT CABIN FLOOR PANEL 242CF UPPER SURFACE HAS MATERIAL PEELING (18-037). REPAIRED FLOOR PANEL 242CF UPPER SURFACE, REF B737-7 SRM 53-00-50-2R-1. MATERIAL USED PO: 1688495 AND PO3 1480720.

Part: FLOOR PANEL — PEELING (RT CABIN) · airframe 60,767 hrs · 36,021 cycles

RT CABIN FLOOR PANEL 232RF UPPER SURFACE HAS MATERIAL PEELING (18-032). REPAIRED PANEL NR 232RF AT UPPER SURFACE IN ACCORDANCE TO B737-700 SRM 53-00-50-2R1 MATERIAL USED RESIN PO 1691358.

Part: FLOOR PANEL — PEELING (CENTER CABIN) · airframe 60,767 hrs · 36,021 cycles

CENTER CABIN FLOOR PANEL 241DF UPPER SURFACE HAS MATERIAL PEELING (18-038). REPAIRED PANEL 241DF IN ACCORDANCE WITH B737-7 SRM 53-00-50-2R-1. REPAIRED TOP SURFACE. MATERIALS USED RESIN PO 1691358.

Part: PRESSURE DECK — DAMAGED (COCKPIT) · airframe 60,767 hrs · 36,021 cycles

FLIGHT DECK FLOOR DAMAGED / INSTALLED REPAIR AT FLIGHT DECK FLOOR FABRICATED TWO (2) DOUBLERS MAT USED 2024 T3 .050 PO# 1484683 AND ONE WEB MAT USED 2024 T3 .040 PO# 1691232; TREATED AND PRIMED REPAIR AS PER B737-7 SRM 51-40-02-0G-0; 51-20-13-0G-0; 51-30-01; 51-00-06-0G-0 SOPM 20-50-19 EA # 1-A53-33179

Part: FLOOR PANEL — PEELING (RT CABIN) · airframe 60,767 hrs · 36,021 cycles

RT CABIN FLOOR PANEL 242DF UPPER SURFACE HAS MATERIAL PEELING (18-036). REPAIRED RT CABIN FLOOR PANEL NR 242DF UPPER SURFACE, IN ACCORDANCE TO B737-7 SRM 53-00-50-2R-1. MATERIALS USED RESIN PO 1691358.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 60,767 hrs · 36,021 cycles

FWD CARGO COMPARTMENT RH SIDE AT STA 500D S-19R GUSSET BRACKET CRACK. 227-010 / REMOVED AND REPLACED GUSSET AT FWD CARGO COMP FROM STA 500D S-19R IN REF B737-700 SRM 51-40-02-0G-0 AND DWG # 143A9481

Part: ANGLE — CRACKED (BULKHEAD) · airframe 60,767 hrs · 36,021 cycles

LT LOWER FUSELAGE AT STA 663.75 LBL 44 VAPOR BARRIER ANGLE HAS SUSPECT CRACK. ACCOMPLISHED REPLACEMENT ANGLE AT LT LOWER FUSELAGE STA 663 BETWEEN LBL 20' TO LBL 60' VAPOR BARRIER ANGLE, REF B737-7 SRM 57-10-10-2R-5 FIG 202 AND DWG 111A1000. LEAK CHECK BEING ACCOMPLISHED ON N/R W186639.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 60,767 hrs · 36,021 cycles

FWD CARGO COMPARTMENT AT STA 500D S-21L GUSSET BRACKET CRACK. 227-009 / REMOVED AND REPLACED GUSSET AT FWD CARGO COMP AT STA 500D S-21L IN REF B737-700 SRM 51-40-02-0G-0 AND DWG #143A9481.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 60,767 hrs · 36,021 cycles

FWD CARGO COMPARTMENT AT STA 500D S-19L GUSSET BRACKET CRACK. 227-008 / REMOVED ANS REPLACED GUSSET AT FWD CARGO COMP FROM STA 500D S-19L IN REF B737-700 SRM 51-40-02-0G-0 AND DWG # 143A9481

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 60,767 hrs · 36,021 cycles

LEFT HORIZONTAL STABILIZER RIB NR 4 HAS A CRACK. REPAIRED LEFT HORIZONTAL STABILIZER MACHINED INSPAR RIB NR 4 STIFFENER NR 3, PER REF B737-700 SRM 55-10-09-2R-4 REPAIR 4.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 60,767 hrs · 36,021 cycles

RIGHT HORIZONTAL STABILIZER RIB NR 4 STIFFENER NR 3 CRACK. REPAIRED HORIZONTAL STAB MACHINED INSPAR RIB NR 4 STIFFENER NR 3, PER REF B737-700 SRM 55-10-09-2R-4. RIGHT HORIZONTAL STAB.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 60,767 hrs · 36,021 cycles

L/H WING #3 SLAT LOWER SURFACE AT ACTUATOR RIB HAS CRACKS AROUND 4 EACH FASTENERS. / REPAIRED L/H WING #3 SLAT LOWER SURFACE SKIN AT ACTUATOR RIB PER REF B737-700 SRM 57-42-01-2R-8. REPAIR 8; REPAIRED CRACK COMMON TO SLAT #3 (P/N 114A5030-3) NOSE SKIN AT FASTENER HOLE NOT COVERED BY REPAIR AREA PER EA 20-157-02375.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 60,767 hrs · 36,021 cycles

L/H WING #4 SLAT LOWER SURFACE AT ACTUATOR RIB HAS A CRACK AROUND 1 FASTENER. / REPAIRED L/H WING #4 SLAT LEADING EDGE NOSE SKIN LOWER SURFACE AT ACTUATOR RIB PER REF B737-700 SRM 57-42-01-2R-8; REPAIR 8. AND EA NO. 20-157-02240 REV IR

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 58,443 hrs · 34,549 cycles

R1 DOOR SLIDE PROTRUDED SLIGHTLY ON BOTTOM LEFT. / REPOSITIONED SLIDE PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 58,071 hrs · 34,304 cycles

R1 DOOR SLIDE LOWER AREA OUT OF POSITION. / REPOSITIONED SLIDE PER MT.

Part: BATTERY — FAILED (COCKPIT) · airframe 56,411 hrs · 33,240 cycles

EMERGENCY FUEL SHUTOFF BATTERY FAILED TEST. R&R BATTERY PER AMM.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 55,648 hrs · 32,766 cycles

RUDDER COUNTERBALANCE WEIGHT IS CORRODED IN BETWEEN RUDDER AND WEIGHT. (GAP IN BETWEEN RUDDER AND WEIGHT) / REMOVED AND REPLACED COUNTER BALANCE WEIGHT PER CMM. 55-40-09

Part: STIFFENER — CRACKED (R/H MLG W/W) · airframe 55,648 hrs · 32,766 cycles

MAIN WHEEL WELL STA 663 RBL 26 STIFFENER CRACKED OUTBD OF EXHAUST DUCT / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02

Part: STIFFENER — CRACKED (L/H MLG W/W) · airframe 55,648 hrs · 32,766 cycles

MAIN WHEEL WELL STA 663 LBL 26 STIFFENER CRACKED OUTBD OF EXHAUST DUCT / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02

Part: LIGHT — LOOSE (CABIN) · airframe 55,648 hrs · 32,766 cycles

AFT GALLEY AREA LT AFT EGRESS STRIP LOOSE. SECURED STRIP PER DWG.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,619 hrs · 32,743 cycles

LT EMERGENCY EXIT LIGHTING FAILED TO ILLUMINATE BETWEEN ROW 9 TO 11. R&R POWER SUPPLY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,619 hrs · 32,743 cycles

OVER WING EXIT UPPER PANEL AND SIDE WALL EXIT LIGHT EXIT LIGHT FAILED TO ILLUMINATE. R&R BATTERY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,619 hrs · 32,743 cycles

R1 DOOR EXIT LIGHT EGRESS LIGHT FAILED TO ILLUMINATE. R&R POWER SUPPLY M1675 IAW AMM

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,619 hrs · 32,743 cycles

L1 DOOR EXIT LIGHT EGRESS LIGHT FAILED TO ILLUMINATE. R&R POWER SUPPLY M1675 IAW AMM

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,619 hrs · 32,743 cycles

RT EMERGENCY EXIT LIGHTING FAILED TO ILLUMINATE BETWEEN ROW 3 TO 4. R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,619 hrs · 32,743 cycles

G1 GALLEY EXIT LIGHT EGRESS LIGHT FAILED TO ILLUMINATE. R&R POWER SUPPLY M1675 IAW AMM

Part: SUPPORT ANGLE — CORRODED (FWD CARGO BAY) · airframe 55,619 hrs · 32,743 cycles

FWD CARGO COMPARTMENT; STA. 500D; LBL 21 - RBL 21; FLOOR LEVEL; ANGLE FOR BULKHEAD HAS CORROSION NEAR LBL21. / REMOVE CORROSION AT FWD CARGO STA 500D LBL 21 RBL 21; RBL 21 FLOOR LEVEL SUPPORT ANGLE FOR BULKHEAD I.A.W. SRM 51-10-02. VERIFIED MATERIAL LOSS ORIGINAL .071 REMOVED .02D REMAIN .050 FOUND NO SRM LIMITS FOR THIS PART OUT OF LIMITS. REMOVED SUPPORT ANGLE I.A.W SRM 51-40-02-0G-00. DRILLED NEW SUPPORT ANGLE I.A.W SRM 51-40-05-0G-00 AND BOEING DWG 143A7500. INSTALLED NEW SUPPORT ANGLE I.A.W. SRM 51-40-02-0G-00 AND BOEING DWG 143A7500

Part: NONE — CRACKED (FUSELAGE) · airframe 55,619 hrs · 32,743 cycles

CABIN FLOOR PANEL BREAK IS CRACKED AT STA 540 BL0 TO RBL 25 / REMOVED AND REPLACED CABIN FLOOR BREAK PANEL AT STA 540 BLO TO RBL 25 I/A/W BOEING DWG 143A0060 REV A; BOEING DWG 143A5240 REV-; 737-700 SRM 51-40-02-0G-0; AND 737 AMM 51-21-91-620-802 APPLIED C.I.C. TO NEW BREAK PANEL ASSY.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 55,619 hrs · 32,743 cycles

VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, LBL 10.1. REPAIRED ANGLE IAW EA.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 55,619 hrs · 32,743 cycles

VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 9.1. REPAIRED ANGLE IAW EA.

Part: SUPPORT ANGLE — CORRODED (AFT CARGO BAY) · airframe 55,619 hrs · 32,743 cycles

AFT CARGO COMPARTMENT FWD CENTER BULKHEAD LOWER ANGLE MOUNT HAS CORROSION AS MARKED. STA 727+8' / REMOVED CORROSION AFT AFT CARGO FWD CENTER BULKHEAD LOWER ANGLE STA 727 + 8' IAW SRM 51-10-02. VERIFIED MATERIAL LOSS ORIGINAL .055 REMOVED .008 REMAIN .047 ALLOWABLE 10% MAX FOUND OUT OGF LIMITS USED AAR TOOL #32351 DUE DATE 12/17/2019 IAW SRM 53-00-53-1A-1. REPLACED SUPPORT ANGLE IAW BOEING DWG 453A2611 REV D

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 55,619 hrs · 32,743 cycles

FWD CARGO COMPARTMENT RH SIDE 'Z' SHEILD HAS THREE SCREW HOLES WITH CORROSION IN THEM. STA. 495 TO STA. 502. / REMOVED CORROSION ON R/H SIDE SHIELD BS 495 TO BS 502 ORIGINAL THICKNESS .032' AFTER REWORK .025' MATERIAL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-57-1A-1 REMOVED; FABRICATED; + INSTALLED NEW FABRICATED SHIELD IAW DWG # 143A0080 REV - + SRM 51-40-02-0G-0 APPLIED CIC IAW AMM 51-21-91-620

Part: BEAM — CRACKED (R1 DOOR) · airframe 55,619 hrs · 32,743 cycles

R1 DOOR NR 4 AND NR 5 BEAMS CRACKED. R&R BEAM IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,619 hrs · 32,743 cycles

AFT CARGO COMPARTMENT LT Z-ANGLE CORRODED BETWEEN BS 756 TO BS 847, LBL 21. R&R "Z" ANGLE IAW SRM & DWG.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 55,619 hrs · 32,743 cycles

AFT CARGO PIT PANEL 140CF HAS CORROSION ON THE UPPER SURFACE A LONG THE PERIMETER. / EVALUATED FLOOR PNL 140 CF AT AFT CARGO FOUND CORROSION IN SEVERAL AREAS EXCEEDING 3' IN LENGTH OUT OF LIMITS IAW SRM 53-00-53-1A-1. REPLACED FLOOR PNL 140CF IAW BOEING DWG 453A2610

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,619 hrs · 32,743 cycles

AFT CARGO COMPARTMENT Z-ANGLE CORRODED BETWEEN BS 727 TO BS 756, LBL 21. R&R "Z" ANGLE IAW SRM & DWG.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 55,619 hrs · 32,743 cycles

AFT CARGO PIT METAL CAP STRIP HAS CORROSION. (ATTACHED TO PANEL 140DF ON PANEL RACK). / NO PUBLISHED LIMITS FOUND FOR CAPSTRIP IN SRM THEREFORE CAPSTRIP IS OUT OF LIMITS REPLACED CAPSTRIP PART NO: 453A2611-6 ATAG IS PU01561A WSRM 51-10-02-0G-0. INSTALLED OUT-PANEL-141 CLOSE ITEM PAGE ATG: PV0156

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,619 hrs · 32,743 cycles

FORWARD SHIELD CORRODED BETWEEN BS. 747+7 TO BS. 747+16, RBL 21. R&R SHIELD IAW SRM & DWG.

Part: WEB — CORRODED (FWD CARGO BAY) · airframe 55,619 hrs · 32,743 cycles

FWD CARGO THRESHOLD LOWER SILL WEB CORRODED AT BS 440 TO 492. / REMOVED CORROSION FROM FWD CARGO THRESH HOLD LOWER SILL WEB IAW 53-00-53-1A-1 OT .090 AFTER REWORK .031 LOSS OF .009 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-1 FIG 103. REPLACED FWD CARGO DOOR SILL WEB IAW B737 SRM 51-40-02-0G-0 AND DEG# 143A8120 5H 33 AND 34. ATAG WN3132

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,619 hrs · 32,743 cycles

FORWARD CARGO COMPARTMENT RT SIDE "Z" ANGLE CORRODED BETWEEN BS 500A TO BS 500D. R&R Z ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,619 hrs · 32,743 cycles

AFT CARGO COMPARTMENT AFT SHIELD CORRODED BETWEEN BS 869 TO BS 873, RBL 21. R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 55,619 hrs · 32,743 cycles

AFT CARGO COMPARTMENT POTABLE WATER SERVICE HOUSING; AFT SUPPORT ANGLE HAS CRACKS AS MARKED. / REMOVED AND REPLACED AFT SUPPORT ANGE PN: 147A7221-32 15339 29JAN19 AT AFT CARGO POTABLE WATER HOUSING IAW DWG 147A7221 REV. D AND SRM 51-40-02-0G-0. RESTORED CIC TO DISTURBED AREAS IAW AMM 51-21-91-620-802

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,619 hrs · 32,743 cycles

AFT CARGO COMPARTMENT Z-ANGLE CORRODED BETWEEN BS 727 TO BS 767, RBL 21. R&R Z ANGLE IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 55,619 hrs · 32,743 cycles

LT OVERWING EXIT CUTOUT LOWER DOOR SILL CORRODED. R&R SILL IAW DWG AND SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 55,619 hrs · 32,743 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 28. R&R WEB DOUBLER IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 55,619 hrs · 32,743 cycles

HORIZONTAL PRESSURE WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB IAW SRM.

Part: HINGE — CRACKED (RT HORIZ STAB) · airframe 55,619 hrs · 32,743 cycles

RIGHT ELEVATOR HINGE PANEL 344GB IS CRACKED AT OUTBOARD CUTOUT / REPAIRED CRACK AT O/B CUTOUT ON PANEL 344GB. IAW B737-700 SRM 55-20-01-2R-4 REPAIR 4; SRM 51-70-04-2R-10 REPAIR 10; SRM 51-70-04-2R-0 REPAIR 0; AMM 51-21-99-300-301 (A80188) (A54069) (A44704)

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 55,619 hrs · 32,743 cycles

RT OVERWING EXIT CUTOUT LOWER DOOR SILL CORRODED. R&R SILL IAW SRM.

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 55,619 hrs · 32,743 cycles

CABIN FLOOR BOARD 241 KF HAS UPPER FIBER LAYERS LOOSE AND MISSING. / REMOVED; REPAIRED & REINSTALLED FLOOR PANEL 241KF IAW AMM 53-21 00-000-801 STEP 2 D (2); SRM 53-00-50-2R-1 (3) L-M REV 66; & AMM 53-21-00-400-801 STEP 3 F 6 - 9 (B)

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 55,619 hrs · 32,743 cycles

CABIN FLOOR BOARD 231 XF HAS UPPER FIBER LAYERS LOOSE AND MISSING. / FABRICATED NEW FLOORBOARD PANEL (231-XF) I/A/W. B737 SRM 53-00-50-24-0 REV66 & BOEING DWG # 144A5810 REV:-

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,619 hrs · 32,743 cycles

SEAT TRACK CORRODED AT BS 520, LBL 24. REPAIRED SEAT TRACK IAW SRM.

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 55,619 hrs · 32,743 cycles

CABIN FLOOR BOARD 241 AF HAS UPPER FIBER LAYERS LOOSE AND MISSING. / REMOVED AND INSTALLED CABIN FLOOR PANEL 241AF IAW B737 AMM 53-21-00. FABRICATED NEW FLOOR PANEL (241AF) IAW B737 SRM 53-00-50-2R-0 REV 66 AND BOEING DWG DOC # 144A5810 REV: -

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,467 hrs · 32,636 cycles

FWD GALLEY OUTBD EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 55,467 hrs · 32,636 cycles

FWD GALLEY INBD EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER MM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 55,377 hrs · 32,572 cycles

R1 DOOR SLIDE FELL OUT OF HOLDER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: SIGN — LOOSE (CABIN) · airframe 54,931 hrs · 32,288 cycles

OVERHEAD CENTER AISLE EMERGENCY EXIT SIGN LOOSE AT ROW 12. SECURED SIGN HOUSING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,849 hrs · 32,236 cycles

LT EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 9 TO ROW 11. RELAMPED LIGHT PER AMM.

Part: COVER — BROKEN (CABIN) · airframe 54,442 hrs · 31,963 cycles

AFT FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH COVER SPRING BROKEN. R&R COVER PER SOPM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 53,740 hrs · 31,513 cycles

L1 DOOR SLIDE INADVERTENTLY FELL OUT OF HOLDER BOX, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 53,740 hrs · 31,513 cycles

L1 DOOR EMERGENCY SLIDE LOCK LATCH LOOSE. R&R SLIDE PER MT.

Part: FASTENER — LOOSE (EMERGENCY EXIT) · airframe 53,637 hrs · 31,450 cycles

LT SIDE LOWER WINDOW EXIT HANDLE LOOSE. REINSTALLED FASTENER PER AMM.

Part: HMU — DEFECTIVE (NR 1 ENGINE) · airframe 52,267 hrs · 30,562 cycles

AIR TURNBACK, DURING CLIMB OUT THE NR 1 ENGINE WOULD NOT PRODUCE MORE THAN 86.9% N1 THRUST. R&R HYDRO MECHANICAL UNIT PER MT.

Part: NONE — DELAMINATED (LT WING) · airframe 52,217 hrs · 30,524 cycles

LEFT OUTBOARD AFT FLAP; INBOARD TRAILING EDGE HAS DELAM / REPAIRED LFT OB AFT FLAP INBD TE DELAM RESTORED FINISH I.A.W B737 SRM 51-70-10-2R-1 REV 63; SRM 51-70-10-2R-0 REV 63; SRM 51-20-05-0G-0 REV 63; AMM 51-21-99-300-801 REV 64.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,151 hrs · 30,488 cycles

RT FORWARD EMERGENCY LIGHT BATTERY PACK INOP. R&R BATTERY PACK PER AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 52,151 hrs · 30,488 cycles

BEADED WEB CRACKED AT BS 663, RBL 45. REPAIRED WEB IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 50,442 hrs · 29,401 cycles

FWD GALLEY EXIT LIGHT LENS BROKEN. R&R LENS PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 49,905 hrs · 29,101 cycles

L2 DOOR ESCAPE SLIDE YELLOW COVER OVER MANUAL DEPLOY HANDLE OUT OF POSITION. REPOSITIONED SLIDE PER SIP.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 49,717 hrs · 28,988 cycles

L1 DOOR EMERGENCY LIGHT LENS BROKEN. R & R THE LENS IAW MM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 48,964 hrs · 28,524 cycles

RIGHT WING NR 6 SLAT ACTUATOR ATTACH POINT FORWARD OUTBOARD HOLE SKIN CRACKED. REPAIRED THE SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,455 hrs · 28,216 cycles

L2 DOOR EMERGENCY FLOOD LIGHT BULB INOP. RELAMPED LIGHT IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 47,574 hrs · 27,695 cycles

L2 DOOR OVERHEAD EMERGENCY EXIT LENS BROKEN. R&R LENS IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 47,380 hrs · 27,572 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,380 hrs · 27,572 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT M1668. R & R THE BATTERY PACK IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 46,724 hrs · 27,188 cycles

AFT GALLEY SIDEWALL EMER EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 46,016 hrs · 26,781 cycles

LEFT WING NR 2 SLAT, LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 46,016 hrs · 26,781 cycles

LEFT WING NR 3 SLAT, LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CRACKED (LT WING SLAT) · airframe 48,964 hrs · 28,524 cycles

LEFT WING NR 4 SLAT ACTUATOR ATTACH POINT FORWARD INBOARD HOLE SKIN CRACKED. R & R THE NR 4 SLAT IAW EA.

Part: STRUCTURE — CRACKED (LT WING SLAT) · airframe 48,964 hrs · 28,524 cycles

LEFT WING NR 4 SLAT ACTUATOR ATTACH POINT FORWARD OUTBOARD HOLE SKIN CRACKED. R & R THE NR 4 SLAT IAW EA.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 44,995 hrs · 26,211 cycles

R2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SENSOR — FAULTY (TE FLAP) · airframe 44,804 hrs · 26,095 cycles

DECLARED EMER, FLAP ASYMMETRY NOTED ON INITIAL SELECTION OF FLAPS 5 AT 220 KNOTS ON DESCENT, LT FLAP TO 1/2, RT FLAP TO JUST OFF O MARK, APPROX 14000 LEFT TO EXTEND. R & R NR 7 FLAP SKEW SENSOR IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,105 hrs · 25,679 cycles

L2 DOOR EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: COVER — LOOSE (R2 DOOR) · airframe 43,314 hrs · 25,247 cycles

R2 DOOR EMER EVAC SLIDE MANUAL DEPLOYMENT HANDLE LOOSE. SECURED COVER IAW SIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,191 hrs · 25,173 cycles

L2 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FLOORBEAM FITTING CRACKED AT BS 727B, LBL 24.75. R & R FITTING IAW SRM & DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 42,749 hrs · 24,929 cycles

LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT STAB STATION 92.70, 20 INCHES FROM FRONT SPAR LOWER CHORD. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 42,749 hrs · 24,929 cycles

LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT STAB STATION 92.70, 29 INCHES FROM FRONT SPAR LOWER CHORD. REPAIRED STIFFENER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

SKIN CRACKED AT BS 538, STRINGER 22L. REPAIRED SKIN IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 42,749 hrs · 24,929 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB STIFFENER CRACKED AT STAB STATION 92.70. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 42,749 hrs · 24,929 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB STIFFENER CRACKED AT STAB STATION 101.90. REPAIRED STIFFENER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FLOOR STRUCTURE ANGLE CRACKED BETWEEN BS 380 - 400, BL 0. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT — CRACKED (TE FLAP) · airframe 42,749 hrs · 24,929 cycles

RIGHT WING FLAP SUPPORT 642BB CRACKED. REPAIRED SUPPORT IAW EA.

Part: SHEAR TIE — BROKEN (CABIN) · airframe 42,749 hrs · 24,929 cycles

SHEAR TIE BROKEN AT BS 460, BETWEEN STRINGER 25L - 26L. R & R SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — BROKEN (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

SHEAR TIE BROKEN AT BS 500B, BETWEEN STRINGER 25L TO 26L. R & R SHEAR TIE IAW DWG & SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

WEB CRACKED BETWEEN BS 294.5 - 303.9, STRINGER 15L. R & R WEB IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FLOORBEAM CORRODED AT BS 328, RBL 45.5. REPAIRED FLOORBEAM IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

UPPER FLANGE FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 43 TO LBL 43. REPAIRED FLOORBEAM IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

TIE CLIP CRACKED AT BS 277, STRINGER 15R. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

WEB CRACKED BETWEEN BS 312 - 328. R & R WEB IAW SRM & DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,749 hrs · 24,929 cycles

LEFT HORIZONTAL STABILIZER LE RIB CRACKED AT STATION 114.55. R & R RIB IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 42,749 hrs · 24,929 cycles

RIGHT WING NR 8 SLAT LE LOWER SURFACE CRACKED, AT THE ACTUATOR RIB AREA. REPAIRED SLAT IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

RIGHT KEEL BEAM AREA UPPER BRACKET CRACKED AT BS 540+4. R & R BRACKET IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FRAME CRACKED AT BS 500A, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FRAME CRACKED AT BS 747, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FRAME CRACKED AT BS 827, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FRAME CRACKED AT BS 400, BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FRAME CRACKED AT BS 440, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FRAME CRACKED AT BS 440, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FRAME CRACKED AT BS 400, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

LEFT KEEL BEAM AREA UPPER BRACKET CRACKED AT BS 540+4. R & R BRACKET IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FRAME CRACKED AT BS 787 BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FRAME CRACKED AT BS 787, BETWEEN STRINGER 8L TO 9L. REPAIRED FRAME IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

L1 COCKPIT NR 1 WINDOW POST FRAME CRACKED AT OTBD CORNER. REPAIRED POST IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

LEFT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED. REPAIRED FRAME IAW ACO.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

FLOORBEAM SUPPORT ANGLE CRACKED AT BS 727B, LBL 45.5. R & R ANGLE IAW SRM & ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

LEFT NR 3 WINDOW FRAME E - F POST AT HOLE NR 3 FROM LOWER POSITION CRACKED. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

LEFT NR 3 WINDOW FRAME E - F POST HOLE NR 2 FROM LOWER POSITION CRACKED. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

RIGHT NR 3 WINDOW FRAME E - F POST HOLE NR 2 FROM LOWER POSITION CRACKED. REPAIRED POST IAW ACO.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 42,749 hrs · 24,929 cycles

AFT CABIN CTR PHOTO LUMINESCENT STRIP CRACKED. R & R STRIP IAW AMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,929 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 40,993 hrs · 23,942 cycles

FORWARD ENTRY EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 40,993 hrs · 23,942 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 40,993 hrs · 23,942 cycles

MID CABIN EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 40,993 hrs · 23,942 cycles

CENTER AFT ENTRY EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 40,993 hrs · 23,942 cycles

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

Part: GIRT BAR — LOOSE (L2 DOOR) · airframe 40,993 hrs · 23,942 cycles

L2 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW MT.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 36,549 hrs · 21,316 cycles

LEFT HORIZONTAL LOWER SKIN 1.5 INCH CRACKED ADJACENT TO REAR SPAR AT STAB STA 95.7. REPAIRED SKIN PER SRM.

Part: FAIRING — CORRODED (TE FLAP) · airframe 35,958 hrs · 20,989 cycles

NR 3 FLAP TRACK FAIRING HAS A CRACK AT TRAILING EDGE FASTENER HOLE 13, WHICH IS LOWER SIDE APPROX 6 O'CLOCK POSITION. REMOVED AND REPLACED FAIRING ASSY PER MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,958 hrs · 20,989 cycles

RIGHT HORIZ STAB LOWER SKIN CRACKED AT STA 101.90 RIB, 20 INCHES FWD OF REAR SPAR APPROX 1 INCH LONG. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,958 hrs · 20,989 cycles

RIGHT HORIZ STAB LOWER SKIN CRACKED BETWEEN RIB STA 92.7-101.90, APPROX 3 INCHES LONG. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,958 hrs · 20,989 cycles

LEFT HORIZ STAB LOWER SKIN CRACKED AT STA 101.90 RIB, 28 INCHES AFT OF FRONT SPAR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,958 hrs · 20,989 cycles

LEFT HORIZ STAB LOWER SKIN CRACKED AT STA 184.70 RIB, 9 INCHES FWD OF REAR SPAR APPROX 1 INCH LONG. REPAIRED SKIN PER SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 35,958 hrs · 20,989 cycles

RIGHT WING BRACKET CRACKED 'BELOW' PANEL 651AT AT THE FORWARD INBOARD CORNER. REMOVED AND REPLACED BRACKET PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,958 hrs · 20,989 cycles

LEFT HORIZ STAB. LOWER SKIN CRACKED AT STA 129.50 RIB, 10 INCHES FWD OF REAR SPAR APPROX 1 INCH LONG. REPAIRED SKIN PER SRM.

Part: HOUSING — BROKEN (CABIN) · airframe 35,821 hrs · 20,912 cycles

CENTER OVERHEAD EMERGENCY LIGHT IN CABIN HAS BROKEN HOUSING. REMOVED AND REPLACED LIGHT HOUSING PER M/M. OPS CHECK GOOD.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 34,492 hrs · 20,103 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT & MM.

Part: COVER — BROKEN (CABIN) · airframe 34,406 hrs · 20,048 cycles

LEFT EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 33,751 hrs · 19,661 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF THE HOLDER AFTER OPENING, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,796 hrs · 19,108 cycles

LT EMERGENCY EXIT LIGHT AT ROW 5 INOP. REMOVED AND REPLACED LENS PER M/M.

Part: COVER — CRACKED (CABIN) · airframe 32,141 hrs · 18,741 cycles

EMERGENCY EGRESS LIGHT TRACK COVER CRACKED AT 1ABC. REMOVED AND REPLACED COVER PER AMM.

Part: COVER — MISSING (CABIN) · airframe 32,094 hrs · 18,712 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS COVER MISSING AT ROW 2. INSTALLED COVER PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 31,935 hrs · 18,612 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION LUG FACE FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 31,935 hrs · 18,612 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION LUG FACE FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 31,935 hrs · 18,612 cycles

RIGHT MLG FWD TRUNNION UPPER INBOARD LUG FACE CORRODED. REPAIRED PER EA #1-57-3246.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,831 hrs · 17,367 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,831 hrs · 17,367 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,831 hrs · 17,367 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,201 hrs · 17,003 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: COVER — CRACKED (CABIN) · airframe 29,201 hrs · 17,003 cycles

DURING SCHEDULED 8Y CHECK, FOUND CENTER CABIN EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 29,201 hrs · 17,003 cycles

DURING SCHEDULED 8Y CHECK, FOUND EMERGENCY EXIT SIGN LENS LOOSE AT L2 DOOR. REMOVED AND REPLACED SIGN PER MM.

Part: BRACKET — BROKEN (CABIN) · airframe 29,201 hrs · 17,003 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT BRACKET BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 29,201 hrs · 17,003 cycles

DURING SCHEDULED 8Y CHECK, FOUND SKIN PUNCTURED AT BS 727D+8, LBL 3. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (CABIN) · airframe 29,201 hrs · 17,003 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS LENS LOOSE AT ROW 2. REMOVED AND REPLACED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,201 hrs · 17,003 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 804, RBL 18. REPAIRED BEAM PER SRM AND BAC DWG.

Part: CONNECTOR — BROKEN (EXIT SIGN) · airframe 29,201 hrs · 17,003 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT FWD LOWER SIDEWALL EMERGENCY EXIT LIGHT CONNECTOR BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,201 hrs · 17,003 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 730A, RBL 3. REPAIRED BEAM PER SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 29,201 hrs · 17,003 cycles

DURING SCHEDULED 8Y CHECK, FOUND WEB DOUBLER CORRODED AT BS 126, RBL 10. REPAIRED DOUBLER PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 28,718 hrs · 16,705 cycles

EEPLS LOOSE AT ROW 1. SECURED EEPLS PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 27,753 hrs · 16,124 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 26,115 hrs · 15,155 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 25,689 hrs · 14,914 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (LE SLAT) · airframe 25,599 hrs · 14,861 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 7 SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED NR 7 SLAT PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 25,599 hrs · 14,861 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 3 SLAT LOWER SURFACED CRACKED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 25,599 hrs · 14,861 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — LOW (L1 DOOR) · airframe 24,475 hrs · 14,173 cycles

L1 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — LOW (R2 DOOR) · airframe 24,475 hrs · 14,173 cycles

R2 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: COVER — LOOSE (CABIN) · airframe 23,135 hrs · 13,343 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 22,469 hrs · 12,945 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS LIGHT COVERS BROKEN. REMOVED AND REPLACED COVERS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 22,463 hrs · 12,938 cycles

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

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 22,297 hrs · 12,830 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT FUSE PER MM.

Part: COVER — BROKEN (CABIN) · airframe 22,297 hrs · 12,830 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS SECTION COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 21,169 hrs · 12,160 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABLIZER ELEVATOR SKIN CRACKED AT BS 129, AFT OF LEADING EDGE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 21,169 hrs · 12,160 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABLIZER ELEVATOR SKIN CRACKED AT BS 101, AFT OF LEADING EDGE. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 19,427 hrs · 11,078 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,484 hrs · 10,518 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 18 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 17,578 hrs · 9,997 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 16,802 hrs · 9,545 cycles

EEPLS LENS LOOSE AT ROW 5 ABC. SECURED LIGHT LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 16,304 hrs · 9,253 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 16,022 hrs · 9,088 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 13,862 hrs · 7,853 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,454 hrs · 6,481 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS TRACK LIGHT INOP AT FWD END. RELAMPED LIGHT PER MM.

Part: BRACKET — LOOSE (R1 DOOR SLIDE) · airframe 11,202 hrs · 6,336 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER ATTACH BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 9,400 hrs · 5,304 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 9,251 hrs · 5,197 cycles

DURING SCHEDULED RON CHECK, FOUND FWD CABIN EEPLS TRACK LIGHT LOOSE. SECURED TRACK PER MM.

Part: SLIDE — OUT OF ADJUST (DOORS) · airframe 8,925 hrs · 5,006 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 8,625 hrs · 4,845 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: PIN — MIGRATED (L1 DOOR) · airframe 20,152 hrs · 11,546 cycles

FWD ENRTY DOOR WOULD NOT OPEN. REMOVED AND REPLACED FWD ENTRY DOOR GUST LOCK PIN PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 5,975 hrs · 3,337 cycles

DURING SCHEDULED MV1D CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: PIN — BROKEN (L1 DOOR) · airframe 5,894 hrs · 3,283 cycles

L1 DOOR WILL NOT OPEN. REMOVED AND REPLACED L1 DOOR GUIDE ARM PIN AND LOWER RETAINING SCREW PER MM.

Part: GUIDE ARM — MIGRATED (L1 DOOR) · airframe 5,123 hrs · 2,821 cycles

UPON ARRIVAL AT LAS, COULD NOT OPEN FWD ENTRY DOOR MORE THAN A FEW INCHES. REINSTALLED UPPER ARM GUST LOCK PIN PER MM.

Part: BALLAST — FAILED (CABIN) · airframe 3,461 hrs · 1,884 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT SIDE OVERWING EXIT DOOR LIGHT INOP. REMOVED AND REPLACED OVERWING EXIT DOOR LIGHT BALLAST PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 1,101 hrs · 600 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: GUIDE ARM — DAMAGED (ENTRY DOOR) · airframe 765 hrs · 433 cycles

FWD ENTRY DOOR WOULD NOT OPEN. REPAIRED FWD ENTRY UPPER GUIDE ARM PER MM.