N303KH

Part: SKIN — CRACKED (BS 827 S10R) · airframe 47,436 hrs · 56,727 cycles

CRACK INDICATIONS AT STR 10R BS 827+6 5/8 INCHES LONG, AND BS 827+10 11/16, 1/2 INCHES LONG. REPAIRED PER BOEING SB 737-53A-1234

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,372 hrs · 56,597 cycles

CAPTAIN'S RH FORWARD SEAT TRACK CRACKED. REMOVED AND REPLACED CAPT FWD RH SEAT TRACK IAWM AMM 25-11-11

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,037 hrs · 55,937 cycles

RH WING NO.4 SLAT T/E WEDGE EDGE DEFORM AT SS.12.25. REMOVE THE INITIAL REPAIR DOUBLER AND DAMAGED CORE AT RH WING NO.4 SLAT T/E WEDGE EDGE SS12.25 MADE THE REPAIR CORE AND DOUBLER AND INSTALLED PERFORMED PERMANENT 250°F METEL METAL BOND REPAIR I.A.W B737-300 SRM 51-70-10 REPAIR 4 (R130)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,037 hrs · 55,937 cycles

STRINGER TIE CLIP CRACKS WAS FOUND AT STA 727A S-7R. RESOLVED ON W/O: 121696 TASKCARD: N/R-00262 ) DAMAGE PARTS REPLACED AT STA 727AS-7R PN:69-35352U14.I.A.W B737-300 SRM 51-40-02 PARA 4 PAGE 2.3 (REV30).

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,037 hrs · 55,937 cycles

CORROSION ON FUSELAGE EXTERNAL SKIN AT BS727D S21R+4" REMOVED CORROSION LEVEL 2 AT FUSELAGE EXTERNAL SKIN AT BS727DS21R+4'' FROM P/N 65C38588 ORIGINAL THICKNESS 0.063'' REMOVED 0.063'' AND REMAINING THICKNESS IS 0'' AND IS OVER LIMITS PERFORM REPAIR PER SRM 53-00-01 REPAIR 35 I.A.W B737-300 SRM 51-10-02 PAGE 12~14 (REV130) PME:004692 DATE CAL OCT.18.2022 DAYE DUE : OCT .18.2023 MECH 360769 INSP 361733

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,037 hrs · 55,937 cycles

MAIN ENTRY DOOR LOWER HINGE HOUSING CRACK. REPLACED HINGE FITTER AT MAIN ENTRY DOOR LOWER HINGER HOUSING I.A.W B737-300 SRM 51-40-2 PAGE 2~3 PAGE 6~7 (REV 130 ) .

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,037 hrs · 55,937 cycles

RH WING NO.5 SLAT T/E WEDGE DELAMINATION AT SS.248~SS.254. REMOVED THE DELAMINATION SKIN AT RH WING NO5 SLAT T/E WEDGE SS248~SS254 MADE THE SKIN FILLER AND DOUBLER INSTALLED THE REPAIR PARTS AND PERFORMED 250°F METAL BOND REPAIR I.A.W B737-00 SRM 51-70-10 REPAIR 4(R130)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,037 hrs · 55,937 cycles

LH WING L/E PNL SUPPORT WAS CORRODED AT FSS 339 . REPLACED PNL SUPPORT AT LH WING L/E FSS 339 FROM PN 69-76227-1 I.A.W B737-300 SRM 51-40-2 PAGE 10~PAGE 12(REV 130)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,037 hrs · 55,937 cycles

INTERIOR EMERGENCY EXIT SIGN COVER CRACK, FWD GALLEY SERVICE DOOR. 1. REPLACE FWD ENTRY DOOR EXIT SIGN ASSEMBLY RE AMM 33-51-11 PAGE 203 REV 097 2. DD EXIT SIGN TEST NORMAL REF AMM 33-51-11 P[AGE 204 STEP D REV 097.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,037 hrs · 55,937 cycles

RH WING UPPER T/E PANEL WBL.214 SUPPORT ROD CRACKED. SUPPORT ROD REPCACED REF: AMM 20-50-11 PAGE 201.R97.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,037 hrs · 55,937 cycles

2 EA SURFACE CORROSION ON CENTER WING EXTERIOR LOWER SKIN BWTWEEN S-11C AND S-12C LBL41-53. PERFORM AIR ASIA WPS CODE EI-737-230801 COMPLETED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,037 hrs · 55,937 cycles

STRINGER TIE CLIP CRACKS WAS FOUND AT STA 727A S-5R. DAMAGED PARTS REPLACED AT STA 727A-5R PN# 69-35352U14 IAW B737 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,038 hrs · 55,937 cycles

LH WING #2 SLAT DEICING DUCT SUPPORT BRACKET CORRODED AT FSS419. REPLACED DAMAGED PARTS AT LH WING #2 SLAT FSS 419 PN# 652627C5U89 IAW B737 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,037 hrs · 55,937 cycles

CORROSION ON FUSELAGE EXTERNAL SKIN AT BS796 S20R~S21R. 1. REMOVED DAMAGE PARTS 2. PERFORMED AIR ASIA WPS CODE LM BACF3TOIE30G65 FOR REPAIR PARTS 3. IA,AW B737-300 SRM 51-40-2 PAGE 6~7 (REV 130) INSTALLED REPAIR PARTS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 47,037 hrs · 55,937 cycles

CORROSION AT APU INLET DOOR EXTERNAL SKIN AT STA 1022~1205, S-13R~S-14R. PERFORMED AIR ASIA WPS CODE LM-65-50976-273 REMOVED INSTALLED REPAIR PARTS AND FASTENERS IAW B737 SRM 51-40-2

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,994 hrs · 55,868 cycles

#4 FLAP FAIRING DAMAGED. REPAIRED FAIRING DAMAGE REF SRM 51-70-6 INLET LAYUP REPAIR

Part: NONE — NONE · airframe 46,642 hrs · 55,140 cycles

LH OUTBOARD LEADING EDGE FLAP DAMAGED AT THROUGH HOLE FOR THE EXHAUST GATE CONTROL ROD. C/W INTERIM REPAIR TO LH MID OB FLAP LEADING EDGE @ WBL 205. INSTALL PERMANENT REPAIR OR REPLACE FLAP SECTION AT NEXT C CHECK.

Part: RETAINER SEAL — DAMAGED · airframe 46,231 hrs · 54,306 cycles

MAIN CARGO DOOR FWD SEAL RETAINER DAMAGED. REMOVED DAMAGED SECTION AND COMPLIED WITH EA NUMBER PD37-52-295, NO OTHER DEFECTS NOTED.

Part: STRINGER — CRACKED (BS 500B S10L) · airframe 44,939 hrs · 51,691 cycles

WHILE PERFORMING AD 2012-26-02 (M), FOUND TWO CRACK INDICATIONS AT STRINGER 10L, BS 500B+6 1/8 TO 500B+6 3/8 AND BS 500B+8 TO 500B+9. INSTALLED REPAIR PER PEMCO EO P037-53-2794 REV H DATED 12AUG2021 REF PROJECT WORKSHEET DATED 8-9-21.

Part: SKIN — CRACKED · airframe 44,329 hrs · 50,384 cycles

DISCREPANCY: 1.25 INCH CRACK ABOVE STR10R AT BS887 + 11.25 INCHES DISCOVER DURING ACCOMPLISHMENT OF AD 2012-26-02. CORRECTIVE ACTION: REPAIRED SKIN CRACK AT BS908, STR10R PER PEMCO EA PD37-53-3262.

Part: SKIN — CRACKED · airframe 44,329 hrs · 50,384 cycles

DISCREPANCY: 2 1/4 INCH CRACK ABOVE STR10R AT BS727B + 12 1/8 INCH DURING ACCOMPLISHMENT OF AD 2012-26-02. CORRECTIVE ACTION: REPAIRED CRACK IAW BOEING SB 737-53A1234 REV 2 REPAIR 34.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 44,110 hrs · 49,939 cycles

L1 DOOR UPPER FORWARD CORNER SEAL ANGLE CRACKED, REPLACED.

Part: SKIN — CORRODED (RT WING SLAT 5) · airframe 44,110 hrs · 49,939 cycles

RIGHT WING NR 5 SLAT LOWER TRAILING EDGE SKIN CORRODED AT FSS 404 AND 446, REPAIRED.

Part: SUPPORT — CORRODED (RT WING K FLAP) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

RT WING KRUGER FLAP OUTBOARD PANEL SUPPORT CORRODED, REPLACED.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 44,110 hrs · 49,939 cycles

NR 3 SLAT INBOARD END WEDGE UPPER SURFACE DELAMINATED, REPAIRED.

Part: WEDGE — DELAMINATED (NR 4 SLAT) · airframe 44,110 hrs · 49,939 cycles

NR 4 SLAT INBOARD END AFT WEDGE UPPER SURFACE DELAMINATED, REPAIRED.

Part: INTERCOSTAL — PUNCTURED (AFT CABIN) · airframe 44,110 hrs · 49,939 cycles

MAIN CABIN FLOOR SEAL INTERCOSTAL PUNCTURED AT STA 1016 BETWEEN LBL 8.39 AND 16.73, REPLACED.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

MAIN CABIN SEAT TRACK AT LBL 62.5 CORRODED BETWEEN BS 420-440 AND 480-500, REPAIRED.

Part: WEB — CORRODED (RT MLG WW) · airframe 44,110 hrs · 49,939 cycles

RIGHT WHEEL WELL, BLADE SEAL SUPPORT RING WEB HAS SEVERAL AREAS OF LIGHT CORROSION AROUND FASTENERS.

Part: PLUG — CORRODED (CABIN WINDOW) · airframe 44,110 hrs · 49,939 cycles

LT SIDE MAIN CABIN WINDOW PLUG HAS CORROSION ON THE AFT LOWER CORNER BETWEEN STA 500A AND 500B.

Part: PLUG — CORRODED (CABIN WINDOW) · airframe 44,110 hrs · 49,939 cycles

LT SIDE MAIN CABIN WINDOW PLUG HAS CORROSION ON THE FWD EDGE BETWEEN STA 500B AND 500C.

Part: PLUG — CORRODED (MN CRGO WINDOW) · airframe 44,110 hrs · 49,939 cycles

MCD WINDOW PLUG EXTERIOR SURFACE IS CORRODED AT THE AFT LOWER CORNER BETWEEN STA 440 AND 460.

Part: PLUG — CORRODED (MN CRGO WINDOW) · airframe 44,110 hrs · 49,939 cycles

MCD WINDOW PLUG EXTERIOR SURFACE IS CORRODED AT THE FWD LOWER CORNER BETWEEN STA 440 AND 460.

Part: TAB — CORRODED (RT AILERON) · airframe 44,110 hrs · 49,939 cycles

RT WING AILERON TRIM TAB LEADING EDGE HAS CORROSION AROUND OUTBOARD HINGE POINT.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 44,110 hrs · 49,939 cycles

MAIN CABIN LATERAL SEAT TRACK AT STA 500C LT SIDE, CORRODED.

Part: ATTACH ANGLE — CRACKED (L1 DOOR) · airframe 44,110 hrs · 49,939 cycles

L1 DOOR UPPER FWD ANGLE ATTACHMENT PN: 65-49652-3 IS CRACKED.

Part: STRINGER — DAMAGED (MAIN CABIN) · airframe 44,110 hrs · 49,939 cycles

MAIN CABIN STRINGER 9R HAS SEVERAL DAMAGED FASTENER HOLES BETWEEN STA 500D AND 540, REPAIRED.

Part: SKIN — NOT REPORTED (FUSELAGE) · airframe 44,110 hrs · 49,939 cycles

FUSELAGE SKIN PN 65C35785-44 BS 360 TO BS 540, S4R TO S10R REQUIRES REPLACEMENT, REPLACED SKIN.

Part: ATTACH ANGLE — CRACKED (L1 DOOR) · airframe 44,110 hrs · 49,939 cycles

L1 DOOR UPPER FORWARD ANGLE ATTACHMENT CRACKED, PART REPLACED.

Part: SEAT TRACK — CRACKED (MAIN CABIN) · airframe 44,110 hrs · 49,939 cycles

MAIN CABIN AT BS 727B RBL 45.5 SEAT TRACK OUTBOARD FLANGE CRACKED, REPAIRED.

Part: STATIC WICK — CORRODED (HORIZONTAL STAB) · airframe 44,110 hrs · 49,939 cycles

RIGHT HAND HORIZONTAL STABILIZER, OUTBOARD AFT TIP HAS CORROSION.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 44,110 hrs · 49,939 cycles

RIGHT HAND HORIZONTAL STABILIZER, LEADING EDGE, ELEVATOR STATION 90 + -, JUST OUTBOARD OF PREVIOUS REPAIR, DENTED.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

MAIN CABIN LATERAL SEAT TRACK AT STA 500C LT SIDE CORRODED, SEAT TRACK REPLACED.

Part: SKIN — DENTED (TAILCONE) · airframe 44,110 hrs · 49,939 cycles

TAIL SECTION RT SIDE SKIN IS DENTED APPROX 7' FWD OF THE AFT TIP OF THE TAIL CONE AND APPROX 2' DOWN FROM THE RUDDER.

Part: SKIN — DENTED (TAILCONE) · airframe 44,110 hrs · 49,939 cycles

TAIL SECTION RT SIDE SKIN IS DENTED APPROXIMATELY 7' FWD OF THE AFT TIP OF THE TAIL CONE AND APPROXIMATELY 2' DOWN FROM THE RUDDER.

Part: ATTACH ANGLE — CORRODED (RT WING) · airframe 44,110 hrs · 49,939 cycles

RT WING AT STA RSS-500, UPPER TRAILING EDGE PANEL LOWER ATTACH ANGLE CORRODED.

Part: PLATE — CRACKED (LT WING TE) · airframe 44,110 hrs · 49,939 cycles

LEFT WING INBOARD TRAILING EDGE, LOWER SURFACE, WIGGLE PLATE JUST INBOARD OF PYLON CORRODED AND CRACKED, REPLACED.

Part: CLOSEOUT PANEL — DAMAGED (AFT CARGO) · airframe 44,110 hrs · 49,939 cycles

AFT LOWER CARGO DOOR SURROUND, FWD FRAME CLOSEOUT PANEL HAS EDGE DAMAGE.

Part: CONTROL CABLE — FRAYED (SPOILER CONTROLS) · airframe 44,110 hrs · 49,939 cycles

LEFT WING, REAR SPAR RSS 135+/- SPOILER CONTROL CABLES HAVE MULTIPLE BROKEN STRANDS, REPLACED CABLES.

Part: SUPPORT BRACKET — CORRODED (LT AILERON) · airframe 44,110 hrs · 49,939 cycles

LEFT WING, REAR SPAR, RSS 130+ -, AILERON CONTROL CABLE PULLEY SUPPORT BRACKET HAS CORROSION.

Part: TAB — CORRODED (RT AILERON) · airframe 44,110 hrs · 49,939 cycles

RT WING AILERON TRIM TAB LEADING EDGE HAS CORROSION AROUND OUTBOARD HINGE POINT, REPLACED TRIM TAB.

Part: STRINGER CLIP — BENT (ZONE 100) · airframe 44,110 hrs · 49,939 cycles

FWD CARGO PIT, STRINGER CLIP AT STA 500 S28L IS BENT.

Part: SKIN — CORRODED (RT WING) · airframe 44,110 hrs · 49,939 cycles

RT WING LOWER SURFACE TRAILING EDGE JUST INBOARD OF PYLON, SKIN IS EXFOLIATED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 44,110 hrs · 49,939 cycles

F/A SEAT EMERGENCY FLASHLIGHT BATTERY INOPERABLE (1 EA).

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 44,110 hrs · 49,939 cycles

FLIGHT DECK FLASH LIGHT ON PILOTS SIDE IS INOPERABLE.

Part: SKIN — DAMAGED (RT WING FLAP) · airframe 44,110 hrs · 49,939 cycles

RIGHT INBOARD FOREFLAP UPPER SURFACE HAS COMPOSITE DAMAGE AT 2 EACH LOCATIONS, REPAIRED DELAMINATION.

Part: ANGLE — CORRODED (LT MLG WW) · airframe 44,110 hrs · 49,939 cycles

LEFT MLG WHEEL WELL, STRINGER 18A AT APPROXIMATLEY BS 724 UPPER SIDE OF ANGLE CORRODED, REPLACED ANGLE.

Part: PLUG — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

EXTERIOR SURFACE OF MAIN CABIN WINDOW PLUG IS CORRODED BETWEEN STA 847 AND 867 LT SIDE, REPLACED WINDOW PLUG.

Part: TAIL CONE — DELAMINATED (LT SIDE) · airframe 44,110 hrs · 49,939 cycles

LT SIDE OF TAIL CONE APPROXIMATELY LBL 12 APPROXIMATELY 24" FWD OF AFT EDGE DELAMINATED, REPAIRED.

Part: GUSSET — CORRODED (RT MLG WW) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

RIGHT WHEEL WELL STA 685 S18A UPPER SURFACE, GUSSET CORRODED, REPLACED GUSSET.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,110 hrs · 49,939 cycles

FUSELAGE WINDOW BELT SKIN P/N 65C35786-2 REQUIRES UNUSED HOLES TO BE PLUGGED.

Part: KEELBEAM — CORRODED (LT MLG WW) · airframe 44,110 hrs · 49,939 cycles

LEFT WHEEL WELL, UPPER SIDE KEEL BEAM STA 716 SHROUD CORRODED, REPLACED.

Part: SUPPORT — CORRODED (LT MLG WW) · airframe 44,110 hrs · 49,939 cycles

LEFT WHEEL WELL BLADE SEAL SUPPORT WEB CORRODED, REPAIRED.

Part: WEB — CORRODED (RT MLG WW) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

RIGHT WHEEL WELL BLADE SEAL SUPPORT RING WEB CORRODED, REPAIRED WEB.

Part: MOUNT — CORRODED (FIRE BOTTLE) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

LEFT MAIN WHEEL WELL, FIRE BOTTLE MOUNT ASSEMBLY IS CORRODED AT BOTTLE ATTACH FASTENERS, REPLACED MOUNT.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

RIGHT HAND HORIZ STAB UPPER SURFACE, OUTBOARD FORWARD TIP CORRODED AT FASTENER HOLE, REPLACED TIP.

Part: STRINGER CLIP — BENT (FWD CARGO) · airframe 44,110 hrs · 49,939 cycles

FWD CARGO PIT, STRINGER CLIP AT STA 500 S28L IS BENT, REPLACED CLIP.

Part: CHANNEL — CORRODED (LT MLG WW) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

LEFT MAIN WHEEL WELL, STRINGER 18A FS 706 UPPER SURFACE CORRODED, REPLACED CHANNEL.

Part: STRINGER — DAMAGED (FWD CARGO) · airframe 44,110 hrs · 49,939 cycles

FWD CARGO PIT STRINGER 19 MISSING FASTENER THROUGH SKIN (AT REPAIR) BETWEEN STA 380 AND 400, REPAIRED.

Part: STRUCTURE — CRACKED (R1 DOOR) · airframe 44,110 hrs · 49,939 cycles

R1 DOOR LOWER AFT CORNER CRACKED AT 1 AND 7 O'CLOCK. 1 O'CLOCK CRACK .250" & 7 O'CLOCK .200" LONG. CRACKS REPAIRED.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 44,110 hrs · 49,939 cycles

FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT INOPERABLE, REPLACED BATTERY.

Part: PANEL — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

NR 2 PYLON PANEL 5843R CORRODED ALONG INNER LOWER MATING SURFACE AND AFT END OUTER SURFACE, REPAIRED PANEL.

Part: PANEL — CORRODED (LT NACELLE) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

NR 1 PYLON PANEL 5753L HAS CORRODED ON INNER MATING SURFACE AFT LOWER EDGE, REPAIRED.

Part: STRUCTURE — DAMAGED (PAX DOOR) · airframe 44,110 hrs · 49,939 cycles

ELONGATED HOLE, FORWARD UPPER CORNER OF FORWARD ENTRY DOOR, REPAIRED.

Part: STRUCTURE — DAMAGED (PAX DOOR) · airframe 44,110 hrs · 49,939 cycles

FORWARD ENTRY DOOR AFT UPPER CORNER HAS ELONGATED HOLE, REPAIRED.

Part: SUPPORT ANGLE — WORN (VERTICAL STAB) · airframe 44,110 hrs · 49,939 cycles

VERTICAL STAB PANEL 9507L LOWER SUPPORT ANGLE WORN, REPAIRED.

Part: SEAL PLATE — CRACKED (HORIZONTAL STAB) · airframe 44,110 hrs · 49,939 cycles

LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.

Part: PRESSURE BLKHD — CORRODED (AFT) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

AFT PRESSURE BULKHEAD AT STA 1016, AFT SIDE OF BULKHEAD, S12R STRINGER END FITTING AT BULKHEAD CORRODED, REPLACED.

Part: COVER — CORRODED (RUDDER) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

RUDDER RIGHT SIDE LEADING EDGE SKIN CORRODED BETWEEN RUD STA 116 AND 125. INSTALLED NEW GAP COVER.

Part: WEB — CORRODED (VERTICAL STAB) · airframe 44,110 hrs · 49,939 cycles

VERTICAL STAB UNDER PANEL 9517L UPPER WEB HAS CORROSION AT RUD STA 114.

Part: STATIC PORT — GOUGED (RT SIDE) · airframe 44,110 hrs · 49,939 cycles

RIGHT HAND STATIC PORT GOUGED WITHIN THE 3 INCH RADIUS OF THE PORT, REPAIRED.

Part: DOOR FRAME — GOUGED (MAIN CARGO) · airframe 44,110 hrs · 49,939 cycles

MAIN CARGO DOOR CUTOUT UPPER SILL GOUGED BETWEEN STA 400 AND 420, REPAIRED.

Part: PLUG — CORRODED (DOOR WINDOW) · airframe 44,110 hrs · 49,939 cycles

MCD WINDOW PLUG EXTERIOR SURFACE IS CORRODED AT THE FWD LOWER CORNER BETWEEN STA 440 AND 460, WINDOW PLUG REPLACED.

Part: PLUG — CORRODED (DOOR WINDOW) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

MCD WINDOW PLUG EXTERIOR SURFACE IS CORRODED AT THE AFT LOWER CORNER BETWEEN STA 440 AND 460, WINDOW REPLACED.

Part: PLUG — CORRODED (CABIN WINDOW) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

LT SIDE MAIN CABIN WINDOW PLUG HAS CORROSION ON THE FORWARD EDGE BETWEEN STA 500B AND 500C, REPLACED WINDOW PLUG.

Part: BULKHEAD WEB — CRACKED (ZONE 200) · airframe 44,110 hrs · 49,939 cycles

CRACK INDICATION FOUND: AFT PRESSURE BULKHEAD, AFT SIDE AT CENTER PLUG. AT AFT GORE WEB CRITICAL FASTENER ROW, INBOARD FASTENER CRACK EMANATES FROM FASTENER TO END OF WEB TO CENTER PLUG AT S-15L.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,110 hrs · 49,939 cycles

6 EACH FASTENERS IN REPAIR AT BS 500C TO 540 AT STRINGER 10L. INSTALLED INCORRECTLY CAUSING REPAIR TO DISH, REPAIRED.

Part: BULKHEAD WEB — CRACKED (AFT) · airframe 44,110 hrs · 49,939 cycles

CRACK INDICATION FOUND: AFT PRESSURE BULKHEAD, AFT SIDE AT CENTER PLUG. AT AFT GORE WEB CRITICAL FASTENER ROW, INBOARD FASTENER CRACK EMANATES FROM FASTNER TO END OF WEB TO CENTER PLUG.

Part: PLUG — CORRODED (DOOR WINDOW) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

MCD WINDOW PLUG EXTERIOR SURFACE IS CORRODED AT THE AFT LOWER CORNER BETWEEN STA 360 AND 380, REPLACED WINDOW PLUG.

Part: PLUG — CORRODED (DOOR WINDOW) · airframe 44,110 hrs · 49,939 cycles

MCD WINDOW PLUG EXTERIOR SURFACE IS CORRODED AT THE FWD LOWER CORNER BETWEEN STA 400 AND 420, BLENDED FOUND WITHIN LIMITS.

Part: PLUG — CORRODED (CABIN WINDOW) · corrosion level 2 · airframe 44,110 hrs · 49,939 cycles

LT SIDE MAIN CABIN WINDOW PLUG HAS CORROSION ON THE AFT LOWER CORNER BETWEEN STA 500A AND 500B, REPLACED WINDOW.

Part: BULKHEAD WEB — CRACKED (AFT) · airframe 44,110 hrs · 49,939 cycles

CRACK INDICATION FOUND: AFT PRESSURE BULKHEAD, AFT SIDE AT CENTER PLUG. AT AFT GORE WEB CRITICAL FASTENER ROW, INBOARD FASTENER CRACK EMANATES FROM FASTNER TO END OF WEB TO CENTER PLUG AT S-7L.

Part: PRESSURE BLKHD — CRACKED (AFT) · airframe 44,110 hrs · 49,939 cycles

AFT PRESSURE BULKHEAD AFT SIDE AT GORE WEB CRITICAL FASTENER ROW CRACK EMANATING FROM FASTENER TO END OF WEB TO CENTER PLUG, REPAIRED.

Part: GUARD — CRACKED (DOOR SILL) · airframe 44,110 hrs · 49,939 cycles

MAIN CABIN, MAIN CARGO DOOR LOWER FORWARD SILL GUARD APPROXIMATELY 9" FROM FORWARD EDGE IS CRACKED, WELDED CRACK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,110 hrs · 49,939 cycles

LOWER EMERGENCY EXIT LIGHT ON L1 LAVATORY IS INOPERABLE, RELAMPED.

Part: SKIN — CRACKED (BS 460-500A) · airframe 43,959 hrs · 49,621 cycles

3 CRACKS DISCOVERED AT BS460+6.5 ABOVE STR10R, BS500A+8.5 AND BS500A+12.5 DURING THE ACCOMPLISHMENT OF AD 2012-26-02. REPAIRED SKIN IAW EA-PD37-53-3157, REV B.

Part: SKIN — CRACKED (BS 620) · airframe 43,959 hrs · 49,621 cycles

DISCREPANCY: 3 CRACKS INDICATED AT BS620+4 BELOW STR2R 1 5/8" LONG DISCOVERED DURING ACCOMPLISHMENT OF AD 2011-24-12. REPAIRED IAW EA PD37-53-3173, REV 1R.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,760 hrs · 49,177 cycles

WHILE PERFORMING AD 2012-26-02 (M), FOUND MFEC CRACK INDICATION ON CHEM MILL LINE STR10R, BS500B+4 TO BS500B+5 ONE INCH LONG. REPAIR IAW EA PD37-53-3157, BOEING REPAIR SKETCH NAC-NAC-20-0008-09C REF BOEING ID 202002140020-0004. IAW SB 737-53A1234 R2 FIG 34. AWAITING AMOC AT THIS TIME.

Part: SLIDE — DEFECTIVE (CABIN) · airframe 43,559 hrs · 48,738 cycles

DURING FLIGHT CREW TRAINING, THE SLIDE FAILED TO OPEN AND DEPLOY PROPERLY. IT WAS TWISTED TO THE RIGHT, TOWARDS THE ENGINE. ONE CHAMBER MAY NOT HAVE BEEN INFLATED. WITNESSED BY FAA POI, DON HAMILTON.

Part: SKIN — CORRODED (LT PYLON) · corrosion level 2 · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: CORROSION AROUND HOLE ON RIGHT SIDE OF LEFT HAND ENGINE PYLON AT APPROX NS248. CORRECTIVE ACTION: CORROSION AROUND HOLE ON RIGHT SIDE OF LEFT HAND ENGINE PYLON AT APPROX NS248.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: CORROSION FOUND ON RIGHT HAND WING CENTER SECTION LOWER PANEL [SKIN] BS570-610 RBL42-60 (3 LOCATIONS) CORRECTIVE ACTION: CORROSION BLENDS ON RT WING CENTER SECTION LOWER PANEL STA 570-610 RBL 42-60 (3 LOCATIONS) REPAIRED IAW SR #4- 4200373089 DATED 5 OCT 2018. DETAILED VISUAL INSPECTION OF THE BLENDED AREA TO BE CARRIED OUT ON OR BEFORE ACCUMULATION OF 3000 FLIGHT CYCLES FROM TIME OF REPAIR AND NOT TO EXCEED 3000 FLIGHT CYCLES. - SERVICEABLE -

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: CORROSION ON LEFT HAND WING SKIN UPPER SURFACE TRAILING EDGE @ W.STA 403 AT REAR SPAR CORD CORRECTIVE ACTION: CORROSION ON LT WING SKIN UPPER SURFACE T/E @ W. STA 403 AT REAR SPAR CHORD BEYOND ALLOWABLE LIMITS IAW SRM 57-20-01 REV 117. REPAIRED IAW SR#4-4200373218 ISSUED DATE 2-OCT-2018 -SERVICEABLE.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: CRACKED STRINGER CLIP AT LEFT HAND FS 500B STR. 14L IN MAIN CABIN. CORRECTIVE ACTION: STRINGER CLIP @ LT FS 500B STR 14L IN MAIN CABIN REPLACED IAW SRM 51-10-02 PARA 8 & SRM 51- 40-02 PARA 4 REV 117 FOUND SERVICEABLE PART INDETIFIED IN DRAWING #65C22908 REV C.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: BS500A - BS500B RIGHT HAND BAFFLE INTERCOSTAL CRACKED IN RADIUS. CORRECTIVE ACTION: BS 500A TO BS 500B RT BAFFLE INTERCOSTAL REPLACED WITH MADE REPAIR IAW REF DWG PL 69-41473 REV P- SERVICEABLE.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: CORRODED DUST SILL [ZEE ANGLE] IN AFT CARGO PIT FROM BS807 - BS947.5 @ S25L. CORRECTIVE ACTION:CORRODED ZEE CHANNEL IN AFT CARGO PIT FROM B. STA 807 TO B STA 947.5 @ STR 25L REPLACED WITH MADE REPAIR PART IAW REV 117 SRM 53-60-53 FIG 1, SRM 53-60-53 FIG 201 REPAIR 4 INSTALLED IAW SRM 51-40-02 PAR 4. FOUND SERVICEABLE.

Part: SKIN PANEL — CORRODED (RT WING) · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: CORROSION FOUND IN WING UPPER SKIN LAP SEAM JUST INBOARD OF RIGHT HAND ENGINE PYLON OVERWING FITTING. CORRECTIVE ACTION: SUPPLEMENTAL REPORT TO FOLLOW.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: 2 CRACKS FOUND AT THE AFT END OF CROSS BEAM E, AFT CARGO PIT DOOR. CORRECTIVE ACTION: AFT CARGO DOOR REPLACED WITH NEW SERVICEABLE DOOR IAW AMM 52-31-00 REV 87 RIG & FUNCTION CHECKED SERVICEABLE.

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: CORROSION ON LEADING EDGE OF LEFT HAND OUTBOARD FOREFLAP OUTBOARD GUIDE TRACK LOCATION WS476. CORRECTIVE ACTION: LEADING EDGE OF LT OB TE FORE FLAP REPAIRED AT WS 441 IAW SRM CH 57-53-01. REPAIR 1, FIGURE 201 PGS 202-203 REV 117 AS DETAILED ON ATTACHED FORMS NR MTC 114 AND MTC-112. ADJUSTMENT AND FUNCTION CHECKED SERVICEABLE.

Part: TIE CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: CORROSION FOUND ON SHEAR CLIP BS967 BETWEEN S21R AND S22R. CORRECTIVE ACTION: CORROSION ON SHEAR CLIP STN 967 BETWEEN STR 21R AND STR 22R FOUND TO BE BEYOND LIMITS IAW SRM REV 117, 53-60-07. REPLACED PART AND INSTALLED IAW SRM REV 117 51-40-02, PARAH 4 AND 7. SERVICEABLE W/NEW PART.

Part: SKIN — DAMAGED (RUDDER) · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: DAMAGED COMPOSITE SKIN ON RIGHT HAND RS238. CORRECTIVE ACTION: REPAIRED DAMAGE COMPOSITE SKIN ON RUDDER RT SIDE STA. 238 IAW SRM 51-20-04 PAR 4B REPAIR 2 (REV 117) - SERVICEABLE -

Part: FRAME — DENTED (FUSELAGE) · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: DENTED FRAME AT BS807 @ S24L IN AFT CARGO PIT CORRECTIVE ACTION: SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: CORROSION FOUND ON WING CENTER SECTION LOWER BEAM LBL42 BS570-590 (3 LOCATIONS). CORRECTIVE ACTION: CORROSION ON WING CENTER SECTION LOWER BEAM LBL 42 STA 570 - 590 REPAIRED IAW ENGINEERING DRAWING NUMBER R25606.1-057- 004-001 REV NC(3 LOCATIONS) - SERVICEABLE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: MINOR CORROSION FOUND ON FUSELAGE SKIN AROUND POWERED OUTFLOW VALVE DOOR RIGHT HAND AND AT BS967-986. CORRECTIVE ACTION: CORROSION ON FUSELAGE SKIN AROUND POWERED OUTFLOW VALVE DOOR RT AND AT STA 967-986 BEYOND LIMITS IAW SRM REV 117 CH 53-00-01 FIG 101. REPAIRED AREA IAW DWG NO. R25606.1-053-011-001 REV NC SERVICEABLE.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: DENT ON FUSELAGE SKIN AT STA442 JUST ABOVE STR24L. CORRECTIVE ACTION: DENT ON FUSELAGE SKIN AT STA 442 JUST ABOVE STR 24L, BEYOND LIMITS IAW SRM REV 117 53-00-01 FIG 101. REPAIRED FUSELAGE SKIN IAW EA NO PD37-53-2908B DATED 10/19/2018 SERVICEABLE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: 2 CRACKS AROUND RIVETS ON STR 4L STA 908. CORRECTIVE ACTION: INSTALLED NEW STRINGER SECTION @ STR 4L STA 908 IAW SRM 51-10-02 CH.8 & 51-40-02 CH 4. REV 117. FASTENER & REPLACEMENT PART INFORMATION FROM DRAWING #65-45777 REV. DP. FOUND SERVICEABLE. FOUND SERVICEABLE #5128 23 OCT 2018.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: CRACKED INTERCOSTAL SUPPORT ANGLE FOUND IN FORWARD PIT BS500C S26R. CORRECTIVE ACTION: REPLACED INTERCOSTAL SUPPORT ANGLE IN FWD PIT STA 500C STR 26R IAW DWG 69-41473 ID-0015 SHEET 15 REV P- SERVICEABLE.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: CORROSION FOUND ON RIGHT HAND KEEL BEAM @ BS 703 RBL 8. CORRECTIVE ACTION: REMOVED CORROSION ON RT KEEL BEAM @ STA 703 RBL 8 IAW DRAWING NR R25606.1-053-010-001 REV NC NO DEVIATIONS/SERVICEABLE.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: MINOR CORROSION FOUND ON FUSELAGE SKIN LEFT HAND SIDE OAT BS 1088, WL 240 APPROX S11-12L CORRECTIVE ACTION: REPAIRED CORROSION FOUND ON FUSELAGE SKIN LT SIDE OAT STA 1088, WL 240 APPROX STR 15-13L IAW SR DWG #R25606.1-053- 002-001 REV A WITHOUT DEVIATION. SERVICEABLE.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: MINOR CORROSION ON EMPANGE DOUBLER SKIN STRAP AT RIGHT HAND SIDE AT BS1156, WL 230 (APPROX), ABOVE APU CUT-OUT. CORRECTIVE ACTION: REPAIRED EMPENNAGE DOUBLER SKIN STRAP AT RT SIDE AT FS 1064 TO FS 1156 WL 208 TO WL 230 ABOVE APU CUTOUT WITH MADE REPAIR PART IAW SRM 51-40-02 REV 117 REF DWG# 65-46881 REV L AND IAW 51-10-02 REV 117 FOUND SERVICEABLE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: AFT CARGO PIT BS947.5, S24R-25R, FRAME CRACKED. CORRECTIVE ACTION: REPAIRED AFT CARGO PIT FRAME AT FS 947.5, STR 24R-25R IAW DWG #692A300/REV- REF SB #737-53A1357. SERVICEABLE. ISSUED AUG 9 2016.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 41,819 hrs · 46,095 cycles

DISCREPANCY: PRE-EXISTING 1/4" HOLE FOUND IN STR 4R AT FS 639. CORRECTIVE ACTION: REPAIRED PRE-EXISTING 1/4" HOLE IN STR 4R AT FS 639 IAW SRM REV 117, 53-00-03, REPAIR 3 FIG 201 ( SHEET 1 TO 5) AND SR# 4-4183050364. SERVICEABLE

Part: STRUCTURE — CRACKED (BS 520) · airframe 40,703 hrs · 43,838 cycles

ACCOMPLISHED AD 2012-26-02 INSPECTION, AND FOUND A CRACK MEASURING OF 3.75 INCHES. ACCOMPLISHED EA PD37-53-2794B FOR CRACK FINDING ON BS 520+7, S-10L.

Part: WIRE HARNESS — SEVERED (NLG) · airframe 39,816 hrs · 42,028 cycles

NOSE GEAR WIRING HARNESS SEVERED. REMOVED TAXI LT HARNESS.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 39,709 hrs · 41,825 cycles

REPAIRED CRACKS ON LONGITUDINAL FLOORBEAM WEB AT LBL 24.82, STA 708 IAW FIGURES 15 AND FIGURES 16 0F ECO 3721, DATED 12/29/15.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 39,709 hrs · 41,825 cycles

RT WING, REAR SPAR MAIN LANDING GEAR SUPPORT BEAM, AFT SUPPORT FITTING CRACK REPAIRED IAW SERVICE REQUEST 3-3826102236, REFERENCE FAA FORM 81009-9.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,709 hrs · 41,825 cycles

REPAIRED BEYOND LIMITS RT AFT SKIN AT STA 1016, BETWEEN STRINGER 18L AND STRINGER 20L IAW SRM 53-80-01, REPAIR 2, REVISION 113.

Part: SPAR — CRACKED (RT WING) · airframe 39,709 hrs · 41,825 cycles

RIGHT HAND WING REAR SPAR UPPER CHORD CRACK REPAIR. RT WING REAR SPAR UPPER CHORD FREEZE PLUG AND OVERSIZED FASTENER INSTALLED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,709 hrs · 41,825 cycles

CRACKED INTERCOSTAL AT LI DOOR, STA 348, STRINGER 16L. REPLACED WITH NEW SERVICEABLE INTERCOSTAL IAW FIGURE 15 0F SERVICE BULLETIN 737-53A1240, REVISION 2, DATED APRIL 10, 2003 AND SRM 51-40-02, REVISION 113.

Part: STRINGER CLIP — CRACKED (BS 500B) · airframe 39,709 hrs · 41,825 cycles

CRACKED STRINGER CLIP 4L, BS 500B. REPLACED IAW SRM 51-40-02 AND 51-40-01 REVSION 113.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 39,709 hrs · 41,825 cycles

REPAIRED CRACK ON LONGITUDINAL FLOORBEAM WEB AT RBL 24.82, STA 708 IAW FIGURES 15 AND FIGURES 16 0F ECO 3721, DATED 12/29/15.

Part: O-RING — FAILED · airframe 39,024 hrs · 40,426 cycles

FOD FOUND IN FWD SUMP LUBE UNIT DURING ROUTINE CHECK. O-RING MATERIAL IN CENTER CHIP DETECTOR AND NUT FOUND STUCK IN FWD SUMP OIL PORT. REMOVED AND REPLACED NR 1 ENGINE. OPS CHECKED GOOD IAW AMM 71-00-02.