N608SW

Part: FITTING — CRACKED (RT MLG) · airframe 64,096 hrs · 51,548 cycles

RIGHT AFT MLG BEAM FITTING CRACKED. R & R FITTING IAW SRM & EA.

Part: FITTING — LOOSE (LT MLG) · airframe 64,096 hrs · 51,548 cycles

LEFT MLG BEAM FITTING BEARING LOOSE. R & R FITTING ASSEMBLY IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 64,096 hrs · 51,548 cycles

RIGHT WING INBD FORE FLAP, UPPER SKIN DELAMINATED 13" FROM INBD END. REPAIRED FORE FLAP IAW SRM.

Part: FITTING — CRACKED (LT MLG) · airframe 64,096 hrs · 51,548 cycles

LEFT AFT MLG BEAM FITTING CRACKED. R & R FITTING IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 64,096 hrs · 51,548 cycles

RIGHT WING UPPER SKIN TE CRACKED AT AFT FASTENER ROW. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,096 hrs · 51,548 cycles

RIGHT WING UPPER SKIN CRACKED AT WS 223.0, 5" FWD OF TE. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,096 hrs · 51,548 cycles

LEFT WING REAR SPAR, UPPER CHORD CRACKED AT FIRST FASTENER HOLE INBD OF RSS 224-14. R & R CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,096 hrs · 51,548 cycles

RIGHT WING REAR SPAR, CHORD CRACKED AT FIRST FASTENER HOLD INBD OF RSS 224.14. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,096 hrs · 51,548 cycles

RIGHT WING REAR SPAR, WEB CRACKED FIRST FASTENER HOLE OTBD OF RSS 224.14. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,096 hrs · 51,548 cycles

LEFT WING CRACKED AT REAR SPAR AFT WEB, FIRST FASTENER HOLD OTBD OF RSS 224-14. REPAIRED WEB IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

STRINGER CORRODED AT BS 807, STRINGER 27L. REPAIRED STRINGER IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 26L - 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 26R - 27R. REPAIRED SHEAR TIE IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

RIGHT AUXILIARY STRAP CRACKED AT BS 727. R & R STRAP IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

LOWER CABIN FLOOR STRUCTURE STRAP CRACKED NEAR FASTENER HOLE AT BS 344, BL 0. REPAIRED STRAP IAW EA & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

FRAME SHEAR TIE ANGLE CORRODED AT BS 344, STRINGER 27R. R & R ANGLE IAW DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

STRINGER CORRODED AT BS 355, STRINGER 24R. R & R STRINGER IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

SHEAR TIE CORRODED AT BS 986.5, BETWEEN STRINGER 27L - 27R. R & R SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

SHEAR TIE CORRODED AT BS 947.5, BETWEEN STRINGER 27L TO 26R. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

AFT CARGO PIT SHEAR TIE CORRODED AT BS 807, BETWEEN STRINGER 26L - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

AFT CARGO PIT SHEAR TIE CORRODED AT BS 807, BETWEEN STRINGER 25L - 26L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

SHEAR TIE CORRODED AT BS 827 - 26R. R & R SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

SHEAR TIE CORRODED AT BS 907, BETWEEN STRINGER 27L - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

AFT CARGO PIT INTERCOSTAL CORRODED BETWEEN BS 727A - 727B, STRINGER 26L. R & R INTERCOSTAL IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

AFT CARGO PIT SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 26L - 26R. REPAIRED SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

FRAME CORRODED AT BS 500B, BETWEEN STRINGER 28R - 27R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

SHEAR TIE CORRODED AT BS 947.5, BETWEEN STRINGER 27L - 26R. R & R SHEAR TIE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

FRAME CRACKED AT BS 947.5, STRINGER 19L. R & R FRAME IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,130 hrs · 50,854 cycles

WHEEL WELL PRESS DECK CRACKED AT BS 663+2, RBL 40. REPAIRED DECK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A LT. REPAIRED CHORD IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 63,130 hrs · 50,854 cycles

RIGHT WING TE REAR SPAR AILERON ACCESS PANEL 7418R,TE STRUCTURE OTBD AFT VERTICAL ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: TAB — CORRODED (RT AILERON) · airframe 63,130 hrs · 50,854 cycles

RIGHT WING TE AILERON CONTROL TAB INBD HINGE AFT ROD, END CORRODED. R & R TAB IAW CMM.

Part: ANGLE — CRACKED (LT WING) · airframe 63,130 hrs · 50,854 cycles

LEFT WING TE AFT SPAR ACCESS AILERON PANEL 7218L,TE OTBD AFT VERTICAL ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,130 hrs · 50,854 cycles

FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727, STRINGER 18A RT. REPAIRED CHORD IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,103 hrs · 50,835 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 25R - 26R. R & R SHEAR TIE IAW SRM.

Part: LENS — LOOSE (L1 DOOR) · airframe 62,987 hrs · 50,761 cycles

L1 DOOR EMER EVAC SLIDE LENS LOOSE. SECURED LENS IAW MM & MT.

Part: LENS — LOOSE (R1 DOOR) · airframe 62,987 hrs · 50,761 cycles

R1 DOOR EMER EVAC SLIDE LENS LOOSE. SECURED LENS IAW MM & MT.

Part: DUCT — FAULTY (CABIN) · airframe 62,369 hrs · 50,352 cycles

DIVERSION, DECLARED EMER, SMELL OF SMOKE IN CABIN AT OVERWING EXITS. FOUND RT PACK CONDITIONED AIR DUCT BROKEN. R & R RT PACK CONDITIONED AIR DUCT ASSEMBLY IAW MM.

Part: DUCT — OVERHEATED (CABIN) · airframe 62,103 hrs · 50,182 cycles

CARGO FIRE PANEL DISPLAYS BOTTLE DISCHARGED 2 & MX LIGHTS ILLUMINATED. FOUND DUCT OVERHEATED. R & R SUPPRESSION CONTROL UNIT IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 61,963 hrs · 50,078 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT OF COMPARTMENT CONTAINER. REINSTALLED SLIDE IAW MT.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,627 hrs · 49,831 cycles

LEFT WING INBD FORE FLAP DELAMINATED. R & R FORE FLAP IAW AMM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,538 hrs · 49,770 cycles

L1 DOOR OPENING BS 348 LT FRAME OUTER CHORD CRACKED AT BS 348.2 STRINGER 16L. R & R CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,538 hrs · 49,770 cycles

AFT PRESS BULKHEAD STIFFENER ANGLE CRACKED AT BS 1016 STRINGER 3L. REPAIRED ANGLE IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,538 hrs · 49,770 cycles

L1 DOOR OPENING LT FRAME OUTER CHORD STOP FITTING LOWER FWD CRACKED AT BS 348 STRINGER 16L. R & R FITTING IAW EA.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 61,538 hrs · 49,770 cycles

L1 DOOR OPENING LT FRAME INNER CHORD STOP FITTING LOWER FWD CRACKED AT BS 348 STRINGER 16L. R & R FITTING IAW EA.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 61,538 hrs · 49,770 cycles

AT L1 DOOR OPENING SHEAR WEB CRACKED AT BS 348 BETWEEN STRINGER 15L TO 17L AFT LOWER CORNER. R & R SHEAR WEB IAW SRM & EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,538 hrs · 49,770 cycles

L1 DOOR OPENING LT FRAME INNER CHORD LOWER INBD HOLE CRACKED AT BS 348 WL 208. R & R CHORD IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 61,488 hrs · 49,740 cycles

AFT LAVATORY EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,343 hrs · 49,631 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A. REPAIRED CHORD IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 61,143 hrs · 49,488 cycles

L1 DOOR EMER EXIT LIGHT LENS LOOSE. REINSTALLED LIGHT LENS IAW MM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 60,733 hrs · 49,200 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 59,934 hrs · 48,636 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,930 hrs · 48,635 cycles

R2 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED CUTOUT IAW EA.

Part: HOLDER — LOOSE (R1 DOOR) · airframe 59,872 hrs · 48,600 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED HOLDER IAW SIP.

Part: FLAP — DELAMINATED (LT WING) · airframe 59,108 hrs · 48,067 cycles

LT WING INBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 59,108 hrs · 48,067 cycles

RT WING INBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 59,108 hrs · 48,067 cycles

LT WING NR 2 TRACK CORRODED IN AREA WHERE IT MATES AGAINST THE WING SKIN & BOLT HOLES. R & R NR 2 FLAP TRACK IAW AMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 59,108 hrs · 48,067 cycles

LT WING NR 1 FLAP TRACK CORRODED WHERE IT MATES TO WING SKIN. R & R NR 1 FLAP TRACK IAW AMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 59,108 hrs · 48,067 cycles

RT WING NR 7 FLAP TRACK CORRODED IN AREA WHERE IT MATES AGAINST THE WING SKIN & BOLT HOLES. R & R 7 FLAP TRACK IAW AMM.

Part: MODULE — FAULTY (HYDRAULIC SYS) · airframe 59,041 hrs · 48,011 cycles

WITH FLAPS 0-15 WE NOTICED THE AILERONS BINDING. WITH THE AUTOPILOT ENGAGED THE AUTOPILOT WOULD NOT ROLL MORE THAN 10 DEGREES WHEN THE LOC CAPTURED. THE AUTOPILOT ROLL MODE WAS DISCONNECTED WITH THE ROLL MODE IN CLOCKWISE THE AILERONS WERE BINDING AIRSPEED WAS 185 & FLAPS 5 PROBLEM SEEMED TO GO AWAY WITH FLAPS UP OR BEYOND 15. R & R LT WW FLIGHT CONTROL HYDRAULIC MODULAR PACKAGE IAW MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,322 hrs · 47,442 cycles

SHEAR TIE CORRODED AT BS 727E, STRINGER 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,322 hrs · 47,442 cycles

SHEAR TIE CORRODED AT BS 727D, STRINGER 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,322 hrs · 47,442 cycles

SHEAR TIE CORRODED AT BS 727E, STRINGER 27R. REPAIRED SHEAR TIE IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,322 hrs · 47,442 cycles

SKIN CRACKED AT BS 727D +11, STRINGER 27L + 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,322 hrs · 47,442 cycles

SKIN CRACKED AT BS 727D+3, STRINGER 27R + 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,322 hrs · 47,442 cycles

SKIN CRACKED AT BS 727D + 5, STRINGER 27R+5. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,322 hrs · 47,442 cycles

FWD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. R&R LAMP IAW M/M.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,322 hrs · 47,442 cycles

SKIN CORRODED AT BS STATION 1016, STRINGER 27L. REPAIRED SKIN IAW DRAWING & EA.

Part: LENS — CRACKED (CABIN) · airframe 58,322 hrs · 47,442 cycles

EMERGENCY EXIT LENS CRACKED OVERHEAD IN CENTER AISLE AT ROW 2. R&R IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

FLOOR SUPPORT ANGLE INTERCOSTAL WEB CRACKED BETWEEN STA 927 TO 947, BL 0. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

VERTICAL SUPPORT ANGLE CRACKED AT STA 727+4, RBL 5. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: STRUCTURE — WORN (LE SLAT) · airframe 57,690 hrs · 46,988 cycles

RIGHT WING NR 6 SLAT INBOARD SLAT TRACK CAN INTERIOR SURFACE OF CAN WORN. REMOVED AND REPLACED NR 6 I/B SLAT CAN IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

VERTICAL BEAMS WEB CRACKED AT BS 178, LBL 17. REMOVED AND REPLACED WEB IAW EA.

Part: STRUCTURE — WORN (LE SLAT) · airframe 57,690 hrs · 46,988 cycles

LEFT WING, NR 1 SLAT, INBOARD SLAT TRACK, SLAT CAN, INTERIOR SURFACE AT BOTTOM OF CAN WORN. REMOVED AND REPLACED NR 1 I/B SLAT CAN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

SHEAR TIE CRACKED AT STA 520, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,690 hrs · 46,988 cycles

LEFT WING OUTBOARD AFT FLAP INBOARD UPPER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

FORWARD BULKHEAD LOWER ANGLE CRACKED AT BS 380, BETWEEN LBL 13 TO RBL 13. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: SHIM — MISSING (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

FRAME SHIM MISSING BETWEEN FRAME AND SKIN OUTBOARD BS 747, STR 27R. INSTALLED SKIN IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

PRESSURE DECK CRACKED AT BS 666, LBL 30. REPAIRED DECK IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

KEEL BEAM TO FRAME ATTACH ANGLE CRACKED AT STA 500D, LBL 7. REMOVED AND REPLACED ANGLE IAW BOEING DWG IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

STRINGER CORRODED AT STA 500D, STR 28L. REPAIRED LEFT KEEL BEAM FWD SECTION IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 907 TO BS 927, STR 17L. REMOVED AND REPLACED WEB IAW DWG & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

"Z" ANGLE CRACKED AT BS 494, STR 26R. REMOVED AND REPLACED Z-ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

FORWARD BULKHEAD FLOOR SUPPORT ANGLE CRACKED AT BS 727, LBL 8. REMOVED AND REPLACED SUPPORT IAW DWG AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, STR 27R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,690 hrs · 46,988 cycles

FLOOR SUPPORT BEAM CRACKED AT BS 847, RBL 7. REMOVED AND REPLACED BEAM IAW SRM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 57,191 hrs · 46,627 cycles

WITH GASPER FAN ON STRONG ELECTRICAL SMELL IN CABIN. REMOVED AND REPLACED GASPER FAN PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,942 hrs · 46,457 cycles

LEFT FWD ENTRY DOOR EMERGENCY SLIDE LIGHT IS INOP. REMOVED AND RELAMPED LEFT FWD ENTRY DOOR EMERGENCY SLIDE LIGHT IAW B737-300 AMM 33-51-22. OPS CHECKED SAME LAMP OPS CHECKED OK IAW B737-300 AMM 33-51-22.

Part: LIGHT — CRACKED (CABIN) · airframe 56,942 hrs · 46,457 cycles

G-4 GALLEY EMERGENCY EXIT LIGHT BASE CRACKED. REMOVED AND REPLACED LIGHT BASE IAW MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

STA 360+1 LOWER ROW AT S14 LAP FASTENER HOLE HAS A CRACKED FASTENER HOLE IN SHEAR TIE. REMOVED & REPLACED SHEAR TIE STA 360+1 S14L LAP AREA IAW B737-300 SRM 51-40-02 & BAC DWG 65-58280 REV H.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

RIGHT ECS DUCT BRACKET AT STA 907 STR 1 IS CRACKED. REMOVED & REPLACED RIGHT ECS DUCT BRACKET STA 907 S1 IAW B737-300 SRM 51-40-02 & BAC DWG 65-46558 REV L.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

RIGHT ECS DUCT BRACKET AT STA 847 STR 1 IS CRACKED. REMOVED & REPLACED RIGHT ECS DUCT BRACKET STA 847 S1 IAW B737-300 SRM 51-40-02 & BAC DWG 65-46554 REV J.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT ECS DUCT BRACKET AT STA 907 STR 1 IS CRACKED. REMOVED & REPLACED LEFT ECS DUCT BRACKET STA 907 S1 IAW B737-300 SRM 51-40-02 & BAC DWG 65-46558 REV L

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT ECS DUCT BRACKET AT STA 847 STR 1 IS CRACKED. REMOVED & REPLACED LEFT ECS DUCT BRACKET STA 847 S1 IAW B737-300 SRM 51-40-02 & BAC DWG 65-46554 REV J.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

RIGHT ECS DUCT BRACKET AT STA 827 STR 1 IS CRACKED. REMOVED & REPLACED RIGHT ECS DUCT BRACKET STA 827 S1 IAW B737-300 SRM 51-40-02 & BAC DWG 65-46552 REV H.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT ECS DUCT BRACKET AT STA 827 STR 1 IS CRACKED. REMOVED & REPLACED LEFT ECS DUCT BRACKET STA 827 S1 IAW B737-300 SRM 51-40-02 & BAC DWG 65-46552 REV H.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

STA 360 BUTT STRAP FWD MOST FASTENER HOLE JUST ABOVE THE LAP AT S14R HAS A CRACKED FASTENER HOLE. COMPLIED WITH EA 1-353-2118 REV, REO G15683 REV. IR FOR REPAIR OF STA 360 BUTT STRAP FWD MOST FASTENER HOLE JUST ABOVE THE LAP AT S14R

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

STRINGER SPLICE AT STA 908 IS CRACKED. RECEIVED NEW STRINGER SPLICE P/N: 65-51698047 PO 760573.1. REMOVED AND REPLACED IAW B737-300 SRM 51-40-02 AND BAC DRG 65-45772.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

STRINGER CLIP AT STA 927 S6R IS BROKEN. LOCATED AND DRILLED AS REQUIRED IAW BAC DWG 65-46559 AND B737 SRM 51-40-02. INSTALLED STRINGER CLIP IAW BAC DWG 65-46559 AND B737 SRM 51-40-02.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

MAIN CABIN STA 500 AT STRINGER S-3R CLIP IS DAMAGED. REMOVED DAMAGED STRINGER CLIP AND REPLACED WITH NEW ONE P/N 69-35352U14 PO 749741.1. LOCATED AND DRILLED IAW BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

MAIN CABIN STA 380 AT STRINGER S-8L CLIP IS CRACKED. REMOVED & REPLACED STRINGER CLIP STA 380 S8L IAW B737-300 SRM 51-40-02 & BAC DWG 65-46525 REV F.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

RIGHT BS 847 10 UPPER WINDOW CORNER HAS HFEC NOISE AT HOLES 1, 3 HFEC CRACK HOLES 4, 9. REPAIRED RIGHT SKIN IAW REO EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 767+10 LOWER WINDOW CORNER HAS HFEC NOISE AT HOLE 4 AND HFEC CRACKED AT HOLES 1, 2, 3, 9, 10. REPAIRED LEFT SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 807+10 UPPER WINDOW CORNER HAS HFEC CRACKED HOLES 2, 3, 7. REPAIRED LEFT SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 847+10 UPPER WINDOW CORNER HAS HFEC CRACKED HOLES 2, 3, 5. REPAIRED LEFT SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 827+10 LOWER FORWARD WINDOW CORNER HAS HFEC NOISE INDICATION AT HOLE NR 3 AND HFEC CRACK INDICATIONS AT HOLES 1, 2, 4, 5, 6, 7, 9. REPAIRED LEFT BS 827+10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21006 REV - , REO G15649 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC NOISE INDICATION AT HOLES 6, 11 AND HFEC CRACK INDICATION AT HOLES 2, 3, 5, 7. REPAIRED LEFT BS 827 +10 UPPER AFT WINDOW CORNER IAW BOEING SB 737-53-1306, REV 2, SECT 3.B.3 AS PER TASK CARD 10075, STEP

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 867+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 5, 6, 9. REPAIRED LEFT BS 867 +10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306 R2 SECT 3.B.3 AS PER TASK CARD 10075, STEP 8.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

RIGHT BS 727+10 UPPER AFT WINDOW CORNER HAS HFEC NOISE INDICATION AT HOLE NR 4. REPAIRED RIGHT BS 727 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21015 REV - REO G15653 REV IR / P1. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

RIGHT BS 767+10 LOWER FORWARD WINDOW CORNER HAS HFEC NOISE INDICATION AT HOLE NR 3 AND HFEC CRACK INDICATION AT HOLES 2,4. REPAIRED RIGHT BS 767 +10 LOWER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306, REV 2, SEC 3.B.3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

STRINGER CLIP AT STA 380 S10L IS CRACKED. REMOVED AND REPLACED STR CLIP STA 380 S-10L IAW B737-300 SRM 51-40-02 + BAC DWG 65-4625 REV F.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

STRINGER CLIP AT STA 500D S10R CRACKED. REMOVED CRACKED STRINGER CLIP AT STA 500D IAW B737 SRM 51-40-02, STR 10R. LOCATED AND DRILLED NEW STRINGER CLIP P/N 69-35352U14 IAW BOE DWG 65C22910 REV E. INSTALLED NEW CLIP IAW B737 SRM 51-40-02 &

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 807+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 9. REPAIRED LEFT BS 807 +10 LOWER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306, REV 2, SECT 3.B.3 AS PER TASK CARD 10075, STEP 8. FACT AS A RESULT OF POST REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 767+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 767 +10 UPPER AFT WINDOW CORNER IAW BOEING SB 737-53-1306, REV 2, SEC 3.B.3 AS PER TASK CARD 10075, STEP 8.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

STRINGER CLIP AT STA 440 S8L IS CRACKED. REMOVED OLD CRACKED CLIP, LOCATED AND DRILLED NEW CLIP AND INSTALLED NEW CLIP IAW B737-300 51-40-02 AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

STRINGER CLIP AT STA 440 S7L IS CRACKED. REMOVED AND INSTALLED STR CLIP NEW IAW B737-300 SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

RIGHT BS 807+10 LOWER WINDOW CORNER HAS HFEC CRACK AT HOLE NR 3. REPAIRED RIGHT SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

RIGHT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3. REPAIRED RIGHT BS 867 +10 UPPER AFT WINDOW CORNER IAW BOEING SB 737-53-1306, REV 2, SEC 3.B.3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 867+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 5, 6, 9. REPAIRED LEFT BS 867 +10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306 R2 SECT 3.B.3 AS PER TASK CARD 10075, STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2,3. REPAIRED LEFT BS 867 +10 UPPER AFT WINDOW CORNER IAW SB 737-53-1306 R2 SECT 3.B.3 AS PER TASK CARD 10075, STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 847+10 UPPER WINDOW CORNER HAS HFEC CRACKED HOLES 2, 3, 5. REPAIRED LEFT SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 787+10 LOWER WINDOW CORNER HAS HFEC CRACKED AT HOLES 1, 2, 3, 9, 10. REPAIRED LEFT SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 847+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED LEFT BS 847 +10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306 R2 SECT 3.B.3 AS PER TASK CARD 10075, STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 887+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 5, 6, 7. REPAIRED LEFT BS 887 +10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21014, REV - , REO G15652 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 787+10 UPPER AFT WINDOW CORNER HAS HFEC NOISE INDICATION AT HOLE NR 5 AND HFEC CRACK INDICATION AT HOLES 2, 3, 6, 7. REPAIRED LEFT BS 787 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21026, REO G15661 REV IR.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

STRINGER CLIP AT STA 500D S9L IS CRACKED. REMOVED CRACKED CLIP, LOCATED, DRILLED NEW CLIP AND INSTALLED NEW CLIP IAW B737-300 51-40-02 AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 727C+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE 8. REPAIRED LEFT BS 727C +10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21013 REV -, REO G15651 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

RIGHT BS 827+10 LOWER FORWARD WINDOW CORNER HAS HFEC NOISE INDICATION AT HOLE NR 8 AND HFEC CRACK INDICATION AT HOLE NR 9. REPAIRED RIGHT BS 827+10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21007 REV- REO G15650 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,943 hrs · 46,457 cycles

LEFT BS 727E+10 WINDOW FORGING HAS EDGE MARGIN OUTSIDE THE TOLERANCES OF TASK CARD 10075. REPAIRED IAW EA 1-353-20995 REV- REO G15647 REV IR.

Part: SKIN — WORN (VERTICAL STAB) · airframe 56,943 hrs · 46,457 cycles

DORSAL FIN ACCESS PANEL 9503 WORN. REMOVED AND REPLACED SKIN IAW SRM.

Part: SKIN — WORN (VERTICAL STAB) · airframe 56,943 hrs · 46,457 cycles

DORSAL FIN ACCESS PANEL 9504 WORN. REMOVED AND REPLACED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,998 hrs · 45,742 cycles

SKIN CRACKED AT BS 747+11, STR 4R. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 55,784 hrs · 45,582 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSTIONED SLIDE PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 54,166 hrs · 44,351 cycles

DURING SCHEDULED CV CHECK FOUND, L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT AND MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,926 hrs · 44,170 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500C+6, STR 10R. REPAIRED SKIN IAW EA.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 53,479 hrs · 43,819 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 57,690 hrs · 46,988 cycles

NR 1 SLAT CRACKED ON INBOARD AFT ROW OF RIVETS STARTING AT THE 4TH RIVET GOING INBOARD TO THE 3RD RIVET. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 727A, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CORRODED AT BS 500D, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CRACKED BETWEEN BS 887 TO BS 907, STR 22R. REMOVED AND REPLACED STRINGER PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER ER AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, RBL 45.5. REPAIRED WEB PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 20L TO STR 21L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 887 TO BS 907, LBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 887 TO BS 907, RBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 847 TO BS 867, LBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 20Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 772A, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: MOUNT — CORRODED (EVAC SLIDE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT MOUNT CORRODED. REMOVED AND REPLACED MOUNT PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: MOUNT — CORRODED (GIRT BAR) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD MOUNT CORRODED. REMOVED AND REPLACED MOUNT PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, LT WING NR 1 SLAT CRACKED AT LOWER SURFACE. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CORRODED AT BS 927, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CORRODED AT BS 927, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CORRODED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CORRODED AT BS 420, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CORRODED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, RT CREASE BEAM WEB CORRODED BETWEEN BS 887 TO BS 907, LBL 65. REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK FOUND, 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 186, BETWEEN WL 230 TO WL 234. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,537 hrs · 43,091 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 747 TO BS 767, LBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,216 hrs · 42,860 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 727E+10, STR 4R. REPAIRED SKIN PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 51,823 hrs · 42,570 cycles

LT EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 6. SECURED LIGHT PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 51,436 hrs · 42,298 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 3 SLAT I/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 51,436 hrs · 42,298 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 51,436 hrs · 42,298 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT O/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,108 hrs · 41,228 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 510D, STR 10L. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (CABIN) · airframe 49,756 hrs · 40,950 cycles

DURING SCHEDULED HC1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 1. SECURED LENS PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,756 hrs · 40,950 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS DAMAGED AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: HOOK — OUT OF ADJUST (GIRT BAR) · airframe 49,699 hrs · 40,904 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,272 hrs · 40,582 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 48,129 hrs · 39,749 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 48,129 hrs · 39,749 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: FLAP — DELAMINATED (RT WING) · airframe 48,129 hrs · 39,749 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,787 hrs · 39,507 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 291.5, WL 233.5. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707.5 TO BS 708.5, LBL 24.5. REPAIRED BEAM PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 842 TO BS 847, LBL 68. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 349, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,077 hrs · 38,987 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,808 hrs · 38,798 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FWD CORNER CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LIGHT — LOOSE (CABIN) · airframe 45,603 hrs · 37,935 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LOOSE AT ROW 16. SECURED EEPLS PER MM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 45,455 hrs · 37,380 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY LIGHT STRIP DELAMINATED AT ROW 8. REMOVED AND REPLACED EMERGENCY LIGHT PER MM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 45,455 hrs · 37,830 cycles

EMERGENCY LIGHT STRIP DELAMINATED AT ROW 8. REMOVED AND REPLACED EMERGENCY LIGHT PER MM.

Part: CABLE — FOD (LANDING GEAR) · airframe 45,118 hrs · 37,583 cycles

AIR TURNBACK, AFTER T/O HAD TO USE TRIGGER TO RETRACT LANDING GEAR. CONFIGUATION WARNING HORN SOUNDED CONTINUOUSLY AFTER GEAR RETRACTION. FOUND FOD ON TELEFLEX CABLE. REMOVED AND REPLACED CABLE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 43,707 hrs · 36,557 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 43,539 hrs · 36,435 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 43,366 hrs · 36,303 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 41,550 hrs · 34,959 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: BEARING — WORN (LT ELEVATOR) · airframe 41,544 hrs · 34,953 cycles

DURING SCHEDULED BRDG CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD BEARINGS PER MM.

Part: BEARING — WORN (RT ELEVATOR) · airframe 41,544 hrs · 34,953 cycles

DURING SCHEDULED BRDG CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD BEARINGS PER MM.

Part: STRINGER CLIP — CRACKED (BS 335 S21L) · airframe 41,544 hrs · 34,953 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 335, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 41,544 hrs · 34,953 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,544 hrs · 34,953 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 41,544 hrs · 34,953 cycles

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

Part: FITTING — LOOSE (L1 DOOR GIRT BAR) · airframe 41,424 hrs · 34,856 cycles

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

Part: BRACKET — LOOSE (L1 DOOR GIRT BAR) · airframe 41,412 hrs · 34,848 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 34,030 hrs · 29,047 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,840 hrs · 28,889 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB ATTACH FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,840 hrs · 28,889 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOOR WEB CORRODED AT BS 993 TO BS 1006, RBL 47, WL 208. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 294, RBL 55, WL 209. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (BS 787) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (FUSLEAGE) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOOR WEB CORRODED AT BS 1030, RBL 2, WL 208. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 706, STR 11L & STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 35 TO RBL 39, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 1006, BL 0, WL 185. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 500 TO BS 500D, LBL 68, WL 208. REPAIRED WEB PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND RT WING LOWER RIB CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 294 TO BS 341, RBL 55, WL 208. REPAIRED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FUSELAGE CREASE BEAM WEB CORRODED AT BS 400 TO BS 420, RBL 68, WL 208. REPAIRED WEB PER SRM.

Part: FRAME — CORRODED (FUSLEAGE) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 24R TO STR 25R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 747) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 33,812 hrs · 28,864 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA CREASE BEAM WEBS CORRODED AT BS 360 TO BS 400, LBL 68 & RBL 70, WL 208. REPAIRED CREASE BEAM WEBS PER SRM.

Part: CHANNEL — CORRODED (COCKPIT FLOOR) · airframe 33,803 hrs · 28,856 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR ZEE CHANNEL CORRODED AT BS 270, RBL 10 TO LBL 10, WL 207.5. REMOVED AND REPLACED ZEE CHANNEL PER SRM.

Part: SHEAR TIE — CORRODED (BS 500A) · airframe 33,784 hrs · 28,841 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 500A TO BS 500B, STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 616) · airframe 33,784 hrs · 28,841 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, BETWEEN LBL 63 + RBL 63, WL 201. REPAIRED FRAME CHORD PER BFG ER.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 33,034 hrs · 28,239 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EXTERIOR LIGHT LENS LOOSE. RE-INSTALLED LENS PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 32,054 hrs · 27,468 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHT LENS, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,054 hrs · 27,468 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: BATTERY — LOOSE (EMERGENCY LIGHT) · airframe 31,032 hrs · 26,678 cycles

DURING SPV, FOUND FWD EMERGENCY EXIT LIGHT INOP. RESECURED BATTERY CONNECTORS PER MM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 30,281 hrs · 26,040 cycles

DURING SCHEDULED C3 CHECK, FOUND RT KEELBEAM PANEL AT BS 700, CRACKED. REPAIRED PANEL PER SRM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 30,281 hrs · 26,040 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT COVER AT ROW 2 ABC OUT OF POSITION. REPOSITIONED BULLNOSE LIGHT COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 30,212 hrs · 25,985 cycles

FWD SERVICE DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LIGHT COVER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 29,414 hrs · 25,377 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 28,836 hrs · 24,912 cycles

AFT UPPER FLASHLIGHT CHARGE LIGHT DOES NOT BLINK. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 28,836 hrs · 24,912 cycles

SAT - FLT 33 - AFT UPPER FLASH LIGHT CHARGE LIGHT DOES NOT BLINK. REMOVED AND REPLACED BATTERY PER MM. (M)

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 28,482 hrs · 24,641 cycles

DURING SCHEDULED C1 CHECK, FOUND RT KEEL BEAM EXTERNAL SKIN CRACKED BETWEEN MLG W/W CUTOUTS. REPAIRED KEEL BEAM SKIN PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 26,715 hrs · 23,200 cycles

AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 25,764 hrs · 22,436 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 25,505 hrs · 22,232 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: PIN — CORRODED (MLG TRUNNION) · airframe 25,365 hrs · 22,120 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BOTH LEFT AND RIGHT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LEFT AND RIGHT TRUNNION PINS PER MM.

Part: BRACKET — LOOSE (CABIN) · airframe 25,365 hrs · 22,120 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR GIRT BAR BRACKETS LOOSE. SECURED BRACKETS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,365 hrs · 22,120 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, RBL 10. REPAIRED SHEAR TIE PER SRM.

Part: BEAM — CORRODED (AFT CARGO COMPT) · airframe 25,365 hrs · 22,120 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED, BS 845 TO BS 860, RBL 8. REPAIRED BEAM PER SRM AND SWA RA.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 23,882 hrs · 20,896 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: WIRE — CHAFED (NR 2 ENGINE) · airframe 23,267 hrs · 20,386 cycles

AIR TURNBACK, DURING CLIMB NR 2 ENG EGT INDICATION WARNING, LIGHT ILLUMINATED. FOUND CHROMMEL EGT WIRE CHAFING NEAR PYLON DISCONNECT. REPAIRED WIRE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 23,007 hrs · 20,177 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 23,007 hrs · 20,177 cycles

DURING SCHEDULED BC3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 23,007 hrs · 20,177 cycles

DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM CRACKED 2 INCHES LONG AT BS 700. REPAIRED KEEL BEAM PER SRM.

Part: SLIDE — DEPLOYED (ENTRY DOOR) · airframe 21,831 hrs · 19,190 cycles

DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY INFLATED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FLASHLIGHT — WEAK (CABIN) · airframe 21,118 hrs · 18,599 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLASHLIGHT BATTERY WEAK AT FWD CABIN. R&R FLASHLIGHT PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 21,056 hrs · 18,553 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 19,822 hrs · 17,550 cycles

EMERGENCY EXIT LIGHT COVER BROKEN IN FWD SECTION. R&R LIGHT ASSY PER MM.

Part: KEELBEAM — CRACKED (MLG W/W) · airframe 19,437 hrs · 17,213 cycles

DURING SCHEDULED C3 CHECK, FOUND 4 KEEL BEAM SKIN CRACK AT BS 700, WL 148.5, ADJACENT TO PREVIOUS REPAIR. REPAIRED BEAM PER SRM.

Part: INDICATOR — OUT OF POSITION (EVAC SLIDE) · airframe 19,437 hrs · 17,213 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: SLIDE — OUT OF TOLERANCE (R2 DOOR) · airframe 19,247 hrs · 17,068 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 18,387 hrs · 16,349 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP OUTBOARD END DISBONDED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — DISCHARGED (CABIN)

DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (ROW 21)

DURING SCHEDULED SERVICE CHECK, FOUND EGRESS LIGHTS INOP AT ROW 21. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (EMER EXIT DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: WIRE — LOOSE (ROW 19-23)

DURING SCHEDULED C2 CHECK, FOUND CABIN FLOOR EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROW 18 THROUGH 23. REATTACHED WIRES INTO LIGHT RESEPTICAL PER BOEING MM.

Part: SKIN — DENTED (RT TE FLAP)

DURING SCHEDULED C4 CHECK, FOUND INBD AFT FLAP DENTED ON LWR SURFACE NEAR T/E APPROX 1 FOOT FROM INBD END. REPAIRED PER BOEING DRM NR 65C30133.

Part: CABLES — OUT OF ADJUST (AC BAY)

DIVERTED TO BNA DUE TO BOTH AC PACKS TRIPPING IN FLIGHT. ADJUSTED LEFT AND RIGHT RAM AIR INLET CONTROL CABLES PER BOEING M/M.

Part: RELAY — FAILED (E/E COMPT)

AFTER TAKEOFF, UNABLE TO RAISE GEAR HANDLE. OVERRIDE TRIGGER WAS USED TO RAISE GEAR, CYCLED GEAR NORMALLY. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED RELAY R276, CHECKED AIR SAFETY SENSOR, AND OPS CHECKED PER BOEING M/M.