N367SW

Part: SKIN — DELAMINATED (TE FLAP) · airframe 71,740 hrs · 59,325 cycles

RIGHT WING TE INBD FORE FLAP UPPER SURFACE DELAMINATED. R & R FLAP ASSEMBLY IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 71,740 hrs · 59,325 cycles

LEFT WING TE INBD FORE FLAP UPPER SURFACE DELAMINATED. R & R FLAP ASSEMBLY IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 71,740 hrs · 59,325 cycles

LEFT WING INBD TE AFT FLAP LOWER SURFACE DELAMINATED. R & R FLAP ASSEMBLY IAW MM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 71,538 hrs · 59,160 cycles

AFT OVERHEAD & RT DOOR EMER LIGHT FAULTY. R & R BATTERY PACK IAW AMM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 71,032 hrs · 58,776 cycles

RIGHT BS 685, LOWER FITTING AFT LUG CORRODED AT 4 O CLOCK POSITION. REPAIRED FITTING IAW EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 71,032 hrs · 58,776 cycles

RIGHT BS 685, LOWER FITTING FWD LUG CORRODED AT 3 O'CLOCK POSITION. REPAIRED FITTING IAW EA.

Part: LIGHT — LOOSE (CABIN) · airframe 71,003 hrs · 58,747 cycles

LEFT FLOOR PROXIMITY EMER ESCAPE PATH LIGHTING STRIP LOOSE AT ROW 8. R & R STRIP IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,830 hrs · 58,618 cycles

FUSELAGE SKIN CRACKED AT BS 360+15, STRINGER 8L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,830 hrs · 58,618 cycles

FUSELAGE SKIN CRACKED AT B5, 500C+6, STRINGER 8L. REPAIRED SKIN IAW EA.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 70,810 hrs · 58,605 cycles

PHOTO LUMINESCENT STRIP LOOSE BETWEEN ROW 8 TO ROW 9. SECURED STRIP IAW MM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 70,736 hrs · 58,550 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED HOOKS IAW SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 70,058 hrs · 58,063 cycles

RIGHT PHOTO LUMINESCENT STRIP LOOSE AT ROW 9. SECURED STRIP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,782 hrs · 57,851 cycles

LEFT OVERWING EMER EXIT LATCH LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 69,375 hrs · 57,554 cycles

L2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW AMM & MT.

Part: ANGLE — CRACKED (RT WING) · airframe 68,924 hrs · 57,238 cycles

RIGHT WING STIFFENER ANGLE CRACKED FWD OF INBD AILEON HINGE. R & R ANGLE IAW SRM.

Part: STIFFENER — CRACKED (RT AILERON) · airframe 68,924 hrs · 57,238 cycles

RIGHT WING AILERON INBD STIFFENER ANGLE CRACKED. R & R STIFFENER IAW SRM.

Part: WEB — CRACKED (ENTRY DOOR) · airframe 67,168 hrs · 55,934 cycles

FORWARD ENTRY DOOR FRAME FWD UPPER SHROUD PNL WEB CRACKED. REPAIRED WEB IAW SRM.

Part: RIVET — LOOSE (R1 DOOR) · airframe 67,126 hrs · 55,906 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER 2 RIVETS AT BOTTOM LOOSE ON FWD SIDE. R & R RIVETS IAW SRM & DWG.

Part: SUPPORT — CRACKED (R2 DOOR) · airframe 67,126 hrs · 55,906 cycles

R2 DOOR LOWER LINER SUPPORT CRACKED FWD OF AFT END. R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (R2 DOOR) · airframe 67,126 hrs · 55,906 cycles

R2 DOOR LOWER AFT LINER SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (R2 DOOR) · airframe 67,126 hrs · 55,906 cycles

R2 DOOR LOWER FWD LINER SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

RIGHT MLG WW SHEAR BEAM WEB INTERCOSTAL CRACKED AT OTBD UPPER HOLE. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

AFT CARGO COMPARTMENT RT INTERCOSTAL CRACKED BETWEEN BS 727A TO BS 727B, STRINGER 25R. R & R INTERCOSTAL IAW SRM & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

L1 DOOR CREASE BEAM WEB CRACKED. R & R WEB IAW SRM & DWG.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 67,126 hrs · 55,906 cycles

RIGHT WING, NR 5 SLAT OTBD TE WEDGE DELAMINATED. REPAIRED WEDGE IAW SRM.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

FORWARD ENTRY DOOR CUT OUT, LOWER AFT CORNER, INNER REVEAL SUPPORT CRACKED. R & R REVEAL IAW DWG & SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

ATTACH CLIP CRACKED AT BS 348.7, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

FUSELAGE STRINGER TO FRAME ATTACH ANGLE CRACKED AT STRINGER 9L, STATION 360. R & R ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

R2 DOOR CREASE BEAM CORRODED BETWEEN BS 971 TO BS 997. REPAIRED BEAM IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

STRAP CRACKED AT BS 348.7, STRINGER 16L. R & R STRAP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW DWG & SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

ATTACH CLIP CRACKED AT BS 348.7, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

STRINGER CLIP CRACKED AT BS 344, STRINGER 16L. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (CABIN) · airframe 67,126 hrs · 55,906 cycles

RIGHT CREASE BEAM CORRODED BETWEEN STATION 440 & STATION 460. REPAIRED CREASE BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

LEFT CREASE BEAM CORRODED BETWEEN STATION 500 & STATION 500A. REPAIRED CREASE BEAM IAW SRM.

Part: PLATE — WORN (R2 DOOR) · airframe 67,126 hrs · 55,906 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BOTH AFT FLOOR MOUNTS & HARDWARE WORN. R & R PLATE ASSEMBLY IAW AMM.

Part: PLATE — CORRODED (R2 DOOR) · airframe 67,126 hrs · 55,906 cycles

R2 DOOR UPPER HINGE GUIDE PLATE ASSEMBLY. CORRODED ON UPPER & LOWER SURFACE. R & R PLATE ASSEMBLY IAW SRM.

Part: ANGLE — CRACKED (LT AILERON) · airframe 67,126 hrs · 55,906 cycles

LEFT WING AILERON 2ND BAY OTBD RSS 533 OTBD COVE ANGLE CRACKED. REMOVED ANGLE IAW SRM & DWG.

Part: SKIN — CORRODED (R1 DOOR) · airframe 67,126 hrs · 55,906 cycles

R1 DOOR SKIN CORRODED AT BS 284, FWD OF UPPER HINGE CUT OUT. R & R SKIN IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,126 hrs · 55,906 cycles

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

Part: ACTUATOR — BROKEN (RT SPOILER) · airframe 65,928 hrs · 55,094 cycles

NR 4 GROUND SPOILER INBD ACTUATOR ATTACH FITTING BROKEN. R & R ACTUATOR IAW MM.

Part: ATTACH FITTING — BROKEN (RT SPOILER) · airframe 65,928 hrs · 55,094 cycles

ATTACH FITTING BROKEN ON NR 4 GROUND SPOILER. R & R NR 4 GROUND SPOILER IAW MM.

Part: GAUGE — FAULTY (COCKPIT) · airframe 65,640 hrs · 54,897 cycles

AIR TURN BACK, "A" HYDRAULIC FAILURE. R & R A SYSTEM HYDRAULIC GAUGE IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,837 hrs · 54,257 cycles

L2 DOOR LOWER HINGE FS SKIN CUTOUT CRACKED AT BS 948. REPAIRED SKIN IAW EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,837 hrs · 54,257 cycles

FS SKIN CRACKED BETWEEN BS 414 - BS 415.75, STRINGER 1L. REPAIRED SKIN IAW ER.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 64,837 hrs · 54,257 cycles

RT WING UPPER TE PANEL AFT ATTACH ANGLE JUST OTBD OF PYLON CRACKED. R&R ANGLE IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,983 hrs · 53,639 cycles

STRINGER CRACKED AT BS 346, STR 2L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,983 hrs · 53,639 cycles

STRINGER CRACKED AT BS 341, STR 2L. REPAIRED STRINGER PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 62,828 hrs · 52,803 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: MODULE — FAULTY (E&E BAY) · airframe 62,733 hrs · 52,733 cycles

AIR TURNBACK-- AT LIFT OFF FIRE BELL AND RED FIRE ANNUNCIATOR CAME ON. REMOVED AND REPLACED FIRE DETECTOR UNIT MODULE PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 62,446 hrs · 52,524 cycles

L1 COCKPIT WINDOW ARCED IN FLIGHT. REMOVED AND REPLACED L1 WINDOW PER AMM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 62,150 hrs · 52,301 cycles

LEFT WING NR 3 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 61,538 hrs · 51,843 cycles

RIGHT WING NR 6 SLAT DELAMINATED ON INBOARD END LEADING EDGE. REPAIRED NR 6 SLAT IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

ANGLE CORRODED AT BS 344, BETWEEN STR 27R TO STR 27R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: BEAR STRAP — CRACKED (BS 303.9 S10L) · airframe 61,538 hrs · 51,843 cycles

L1 DOOR BEAR STRAP SKIN CRACKED AT UPPER HINGE BS 303.9, STR 10L. REPAIRED SKIN IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 61,538 hrs · 51,843 cycles

RIGHT VERTICAL STABILIZER CRACKED ON VERTICAL FLANGE OF LOWER TEE ANGLE LOCATED AT STA 120.30. REMOVED AND REPLACED CHORD PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: TIE CLIP — BROKEN (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP BROKEN AT BS 312, STR 24R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

UPPER CHORD CORRODED AT BS 344, BL 0. REPAIRED CHORD IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 61,538 hrs · 51,843 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED ON LEADING EDGE AT STA 114.5. REMOVED AND REPLACED RIB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

FRAME CORRODED AT BS 360, STR 28R. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 947.5 S22L) · airframe 61,538 hrs · 51,843 cycles

STRINGER CLIP CRACKED AT BS 947.5, STR 22L. REMOVED AND REPLACED STRINGER CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

FRAME CORRODED AT BS 360, STR 28L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 787, STR 19L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (BS 500D S28L/R) · airframe 61,538 hrs · 51,843 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGERS 28R TO 28L. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 500A, STR 25L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: SHEAR TIE — CORRODED (BS 500D S27-28R) · airframe 61,538 hrs · 51,843 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGERS 27 TO 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 787, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 500C, STR 24L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 500A, STR 20L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

CHANNEL CORRODED AT BS 847+12, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 727E, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

CHANNEL CORRODED AT BS 847+12, LBL 3.0. REPAIRED CHANNEL PER EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 927, STR 28R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 727B, STR 19L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 500C, STR 20R. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: TIE CLIP — BROKEN (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP BROKEN AT BS 400, STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (CENTER WING BOX) · airframe 61,538 hrs · 51,843 cycles

CHORD CRACKED AT BS 663, LBL 24.8. REPAIRED CHORD IAW EA AND EO.

Part: FRAME — CORRODED (BS 460 S28L/R) · airframe 61,538 hrs · 51,843 cycles

FRAME CORRODED AT BS 460, BETWEEN STR 28L TO 28R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

L1 DOOR UPPER HINGE ANGLE CRACKED AT BS 303.9, STR 10L. REMOVED AND REPLACED ANGLE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 737A, STR 19L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,538 hrs · 51,843 cycles

LEFT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 500C, STR 21R. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 400, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: FLAP — DELAMINATED (RT WING) · airframe 61,538 hrs · 51,843 cycles

RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW AMM.

Part: TIE CLIP — BROKEN (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP BROKEN AT BS 520, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

ANGLE CRACKED BETWEEN BS 887 TO BS 907, RBL 24.5. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 827, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

FRAME CORRODED AT BS 500, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW EA AND EO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

TIE CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 61,538 hrs · 51,843 cycles

OVERHEAD CEILING EMERGENCY EXIT LENS BROKEN BETWEEN FWD LAV AND FWD GALLEY. REMOVED AND REPLACED LENS IAW CMM.

Part: DOOR FRAME — CRACKED (BS 959.6) · airframe 61,538 hrs · 51,843 cycles

L2 DOOR FORWARD EDGE FRAME BS 959.6 CRACKED AT FWD LOWER CORNER EDGE. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

LONGITUDINAL FLOORBEAM CENTER WING BOX CRACKED AT BS 665, LBL 24.8. REPAIRED CHORD IAW EO AND EA.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 61,538 hrs · 51,843 cycles

BROKEN BASE OF FLASHLIGHT ON FWD LAVATORY WALL. REMOVED AND REPLACED BASE OF FLASHLIGHT CMM.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 61,538 hrs · 51,843 cycles

FASTENERS CORRODED BETWEEN BS 500A AND BS 500B, BETWEEN STR 2LTO STR 2R. REMOVED AND REPLACED FASTENERS IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,262 hrs · 51,628 cycles

FUSELAGE SKIN CRACKED AT BS 420 + 2, STR 1L. REPAIRED SKIN PER EA.

Part: LENS — MISSING (CABIN) · airframe 61,262 hrs · 51,628 cycles

FWD ENTRY LOWER EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: HINGE FITTING — BROKEN (RT SPOILER) · airframe 61,102 hrs · 51,508 cycles

RT WING I/B GROUND SPOILER I/B HINGE FITTING BROKEN. REMOVED AND REPLACED SPOILER PER M/M.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,883 hrs · 51,347 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,362 hrs · 50,977 cycles

LEFT EMERGENCY EXIT SIDEWALL LIGHT INOP AT ROW 10. REMOVED AND REPLACED LIGHT IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,224 hrs · 50,863 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 616, RBL 64. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,224 hrs · 50,863 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,224 hrs · 50,863 cycles

DURING SCHEDULED SPV CHECK, FOUND ANGLE CRACKED AT BS 615, LBL 65. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,224 hrs · 50,863 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 60,224 hrs · 50,863 cycles

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

Part: LATCH — LOOSE (GIRT BAR) · airframe 59,229 hrs · 50,117 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW LATCHES LOOSE. SECURED LATCHES PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 59,048 hrs · 49,986 cycles

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

Part: ACTUATOR — BROKEN (SPOILER) · airframe 58,583 hrs · 49,625 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 GROUND SPOILER O/B ACTUATOR FWD ATTACH LUG BROKEN. REMOVED AND REPLACED ACTUATOR PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 58,156 hrs · 49,302 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,071 hrs · 49,242 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 57,428 hrs · 48,765 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 57,398 hrs · 48,741 cycles

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

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 57,375 hrs · 48,726 cycles

R1 COCKPIT WINDSHIELD ARCED. REMOVED AND REPLACED WINDSHIELD PER MM.

Part: LINE — CHAFED (HYDRAULIC SYS) · airframe 57,238 hrs · 48,631 cycles

DIVERSION / DECLARED EMERGENCY. EN ROUTE ENGINE DRIVEN A NR 1 HYDRAULIC PUMP LIGHT FLICKERED AND THEN ILLUMINATED. FOUND ENGINE DRIVEN "A" SYS PRESSURE LINE CHAFED. REMOVED AND REPLACED LINE, PUMP AND FILTERS PER MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 60,586 hrs · 51,917 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE MISROUTED. REROUTED CABLE PER MM.

Part: COVER — MISSING (EXIT SIGN) · airframe 56,946 hrs · 48,418 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING LOWER EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,827 hrs · 48,329 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 433, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,827 hrs · 48,329 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 960, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,825 hrs · 48,328 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 960, STR 17L. REPAIRED PER SRM.

Part: LENS — MISSING (CABIN) · airframe 12,806 hrs · 7,645 cycles

RT WING OVERWING EMERGENCY EXIT SIDEWALL LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 56,281 hrs · 47,887 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,281 hrs · 47,887 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 17R TO STR 27R. REMOVED AND REPLACED FRAME PER BAC DWG.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,281 hrs · 47,887 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,281 hrs · 47,887 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM SHEAR STRAP CRACKED AT BS 312, LBL 12. REMOVED AND REPLACED SHEAR STRAP PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 55,330 hrs · 47,186 cycles

LEFT OVERWING SIDEWALL EMERGENCY LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,167 hrs · 47,065 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 55,170 hrs · 47,067 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (BS 741A S4R) · airframe 54,787 hrs · 46,787 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 741A, STR 4R. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,335 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 380, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,335 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,335 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 15L. REPAIRED FRAME PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 500A, STR 26R. REPAIRED FRAME SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 400, STR 15L TO STR 16L. REPAIRED FRAME SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, BL 0. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 45,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,336 hrs · 45,458 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 15L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 45,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 45,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 45,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D+15, STR 4R. REPAIRED SKIN PER ER AND ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD UPPER CHORD CRACKED AT BS 178, LBL 24. REMOVED AND REPLACED CHORD PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 360, STR 4L. REPAIRED SKIN PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S8L) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 178-188) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOOR SUPPORT WEB CRACKED BETWEEN BS 178 TO BS 188, LBL 29. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500 S4L) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 4L. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (BS 178) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND WEB CRACKED BETWEEN BS 178 TO BS 188, LBL 29. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500B, STR 4L. REPAIRED SKIN PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,336 hrs · 46,458 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 54,175 hrs · 46,331 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 54,163 hrs · 46,323 cycles

AIR TURNBACK / DECLARED EMERGENCY. FLT 220 CRUISE CABIN ALT WARNING HORN SOUNDED. CABIN ALTS CLIMBING AT 700FT/MIN. PERFORMED CABIN ALT WARN/ABNORMAL PRESS CHECK PER QRH AND INITIATED DESCENT COULDN'T GET CABIN TO DESCEND ON NORMAL PRESS. CONTROLLED CABIN USING MAIN DC. REMOVED AND REPLACED OUTFLOW VALVE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,672 hrs · 45,946 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 13. RELAMPED LIGHT ASSY PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 53,503 hrs · 45,823 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: FITTING — CRACKED (LT WING) · airframe 53,486 hrs · 45,811 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING UPPER STRINGER FITTING CRACKED AT STA 583, STR 10. REPAIRED FITTING PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,368 hrs · 45,735 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 987, STR 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 53,326 hrs · 45,703 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,326 hrs · 45,703 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,237 hrs · 45,639 cycles

L2 DOOR EMERGENCY EVAC SLIDE FLOOD LIGHT INOP. RELAMPED PER MM.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 53,169 hrs · 45,590 cycles

L1 COCKPIT WINDSHIELD ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 52,859 hrs · 45,368 cycles

AFT O/B FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,526 hrs · 45,115 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,526 hrs · 45,115 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 500D, STR 2R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,097 hrs · 44,822 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,097 hrs · 44,822 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,097 hrs · 44,822 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 25L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,801 hrs · 44,633 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,693 hrs · 44,549 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 1. REPAIRED SKIN PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 51,630 hrs · 44,505 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP OUTBOARD AREA REPAIR DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 706, RBL 45. REMOVED AND REPLACED BEAM PER DHN EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 1064, STR 17R. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — DETERIORATED (CABIN) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EXIT LIGHT LENS DETERIORATED. REMOVED AND REPLACED LENS PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND MAIN CABIN CREASE BEAM CRACKED AT BS 617 TO BS 639, LBL 60. REMOVED AND REPLACED BEAM PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT FRAME CRACKED AT BS 767, STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, BELOW STR 17L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 500C, STR 28L AND STR 28R. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,612 hrs · 4,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, STR 27L TO STR 27R. REMOVED AND REPLACED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT RT CREASE BEAM CORRODED BETWEEN BS 943 AND BS 1006. REMOVED AND REPLACED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,612 hrs · 4,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 328, STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR LOWER FUSELAGE STRINGER CORRODED AT BS 208, STR 26L. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500A BETWEEN STR 28L AND STR 28R. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,612 hrs · 44,490 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REPAIRED CLIP PER SRM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 51,396 hrs · 44,334 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. FOUND LIGHT ASSY DISCONNECTED. CONNECTED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,657 hrs · 43,813 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,657 hrs · 43,813 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 15L. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 50,137 hrs · 43,423 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 12 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,785 hrs · 43,181 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,785 hrs · 43,181 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 863, STR 25L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,961 hrs · 42,549 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727E S18L) · airframe 48,961 hrs · 42,549 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — SHORTED (COCKPIT) · airframe 48,422 hrs · 42,141 cycles

FLIGHT DECK RIGHT OVERHEAD LIGHT SHORTED OUT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,383 hrs · 42,115 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,383 hrs · 42,115 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,383 hrs · 42,115 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,383 hrs · 42,115 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,383 hrs · 42,115 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,383 hrs · 42,115 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,383 hrs · 42,115 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,383 hrs · 42,115 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,383 hrs · 42,115 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,383 hrs · 42,115 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 48,383 hrs · 42,115 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT WING NR 2 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED L/E SLAT PER SRM.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 48,383 hrs · 42,115 cycles

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

Part: SKIN — CRACKED (R1 DOOR) · airframe 48,062 hrs · 41,855 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,062 hrs · 41,855 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 517D, STR 12R. REPAIRED SKIN PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 47,967 hrs · 41,777 cycles

DURING SCHEDULED MV1 CHECK, FOUND RIGHT WING INBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,228 hrs · 41,171 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT FWD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,228 hrs · 41,171 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT BS 378.5, LBL 2.8. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,762 hrs · 40,805 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 253, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 513C S10L) · airframe 45,742 hrs · 40,001 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513C, STR 10L. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 45,615 hrs · 39,900 cycles

DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,228 hrs · 39,617 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT R1 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: PTU — LEAKING (HYD SYSTEM) · airframe 44,667 hrs · 39,176 cycles

AFTER TAKEOFF, LOST "B" SYSTEM HYDRAULIC FLUID. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR O-RING AND HYDRAULIC SYSTEM PTU PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 44,351 hrs · 38,931 cycles

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

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 44,325 hrs · 38,908 cycles

AIR TURNBACK, INFLIGHT A-HYDRAULIC SYSTEM QUANTITY AND PRESSURE LOSS. REMOVED AND REPLACED LT MLG ACTUATOR UPLINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,316 hrs · 38,899 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 15R. REPAIRED SKIN PER SWA EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 44,316 hrs · 38,899 cycles

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

Part: HANDLE — CRACKED (EMERGENCY EXIT) · airframe 44,223 hrs · 38,823 cycles

LT OVERWING EMERGENCY EXIT DOOR HANDLE CRACKED. REMOVED AND REPLACED DOOR HANDLE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 44,223 hrs · 38,823 cycles

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

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 42,486 hrs · 37,478 cycles

DURING SCHEDULED SERVICE CHECK, R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 42,385 hrs · 37,401 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 42,385 hrs · 37,401 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED OTBD OF ACTUATOR. REPAIRED SLAT PER SWA EA.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 40,066 hrs · 35,506 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CRACK ON AFT CARGO DOOR OUTBOARD LOWER TEE FITTING. REMOVED AND REPLACED TEE FITTING PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 40,066 hrs · 35,506 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT LOWER SURFACE OUTBOARD OF FWD INBOARD BALANCE PANEL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,066 hrs · 35,506 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR, LOWER CORNER OF CUTOUT. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 40,066 hrs · 35,506 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CRACK ON FUSELAGE BEADED WEB AT BS 664.5, RBL 38.5. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (ELEVATOR TAB) · airframe 40,066 hrs · 35,506 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED AT NR 1 HINGE CUTOUT. REMOVED AND REPLACED TAB PER MM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 40,066 hrs · 35,506 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CRACK ON L1 UPPER WINDOW POST. REPAIRED L1 WINDOW POST PER SRM.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 40,004 hrs · 35,453 cycles

DIVERSION, INFLIGHT B-HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED. FOLLOWED BY B-SYSTEM FLUID LOSS. REMOVED AND REPLACED HYDRAULIC HOSE AT B-SYSTEM ACOUSTIC FILTER PER MM.

Part: SKIN — CRACKED (RT WING) · airframe 39,695 hrs · 35,195 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING LOWER SURFACE SKIN OUTBOARD OF NR 2 ENGINE PYLON MID SPAR FITTING, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,446 hrs · 34,996 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 25L, CRACKED. REPAIRED SKIN SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,206 hrs · 34,808 cycles

DURING SCHEDULED RON, FOUND 2EA FUSELAGE SKIN CRACKS AT BS 500A TO BS 520, STR 9L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 38,742 hrs · 34,448 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,644 hrs · 34,366 cycles

AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED IN FLIGHT FOR ABOUT 2 MINUTES THEN WENT OUT. REMOVED AND REPLACED BATTERY PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 37,759 hrs · 33,634 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER AND LOWER HINGE BOX FITTINGS CRACKED. REMOVED AND REPLACED UPPER AND LOWER HINGE BOX FITTINGS PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 36,778 hrs · 32,864 cycles

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

Part: SLIDE — DEPLOYED (AFT SVC DOOR) · airframe 35,440 hrs · 31,785 cycles

DURING SCHEDULED RON, AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED AFT SVC DOOR EMERGENCY ECAV SLIDE PER MM.

Part: SKIN — DELAMINATED (RT OUTBD FLAP) · airframe 34,992 hrs · 31,407 cycles

DURING SCHEDULED C4 CHECK, FOUND RT OUTBD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBD T/E FLAP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 57,086 hrs · 55,572 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 32,757 hrs · 29,650 cycles

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

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STABILIZER REAR SPAR LT AND RT DRAG BRACE FITTINGS CORRODED. REPAIRED FITTINGS PER SRM.

Part: FITTING — CORRODED (VERT STAB) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STABILIZER AFT SPAR PRIMARY LUG FACE FITTINGS CORRODED. REPAIRED FITTINGS PER BFG ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULE D CHECK, FOUND VERTICAL STABILIZER FAILSAFE LUG FITTINGS CORRODED. REPAIRED FITTINGS PER BFG ER.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND NR 5 L/E SLAT WEDGE DELAMINATED AT BOTH INBD AND OTBD ENDS. REPAIRED NR 5 L/E SLAT WEDGE PER MM.

Part: RIB — CRACKED (RT WING) · airframe 32,003 hrs · 29,004 cycles

DURING SCHEDULED D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 AND STR 3. REPAIRED RIB LOWER CHORD PER BFG ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CRACKED AT BS 190, WL 208 AND RBL 29. REPAIRED CREASE BEAM PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, BETWEEN STR 18R AND STR 28R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (COCKPIT) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND RT FUSELAGE FRAME CRACKED AT BS 188. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT BS 294, WL 209 AND RBL 60. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, WL 215 AND LBL 60. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIES CRACKED (3 EA) BETWEEN STR 14R AND STR 15R, BS 440, BS 460 AND BS 480. REPAIRED SHEAR TIES PER SRM.

Part: LIGHT — NOT SEATED (SERVICE DOOR) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE LIGHT INOP. RESEATED LIGHT ASSY PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIES CRACKED (2 EA) AT BS 360, BETWEEN STR 13L AND 14L AND BETWEEN STR 14R AND 14R. REPAIRED SHEAR TIES PER SRM.

Part: SHEAR TIE — CORRODED (FWD CARGO) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPOILER — BULGED (LT WING) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND NR 4 SPOILER UPPER SKIN BULGED. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT CORRODED AT BS 847, BETWEEN STR 25R AND STR 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER SWA T1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 195, WL 209 AND RBL 29. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: FLOORBEAM — CORRODED (FWD CABIN) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 24 TO RBL 54. REPAIRED FLOORBEAM PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,003 hrs · 29,044 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON CREASE BEAM WEB (2 EA) BETWEEN BS 887 TO BS 907, WL 208 AND RBL 64 AND BS 867, WL 208 AND LBL 65. REPAIRED CREASE BEAM WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 30,916 hrs · 28,136 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 190 AT OBL. REPAIRED WEB PER SRM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 30,797 hrs · 28,039 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 28,338 hrs · 26,024 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 28,173 hrs · 25,879 cycles

LH OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. R&R EXIT LIGHT LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,171 hrs · 24,239 cycles

1 EA. EEPLS LAMP INOP. RE-LAMPED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 25,994 hrs · 24,094 cycles

EELPS TRACK COVER MISSING. INSTALLED EEPLS TRACK COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 25,687 hrs · 23,831 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SECTION EMERGENCY EXIT LIGHT LENS LOOSE NEXT TO FWD F/A SEAT. SECURED LENS PER MM.

Part: SKIN — DELAMINATED (LT WING LE FLAP) · airframe 25,687 hrs · 23,831 cycles

DURING SCHEDULED C2 CHECK, FOUND INBOARD T/E FOREFLAP DELAMINATED AT CENTER, 3 X 6. REMOVED AND REPLACED FOREFLAP PER MM.

Part: CONNECTOR — DAMAGED (NR 1 ENGINE) · airframe 24,076 hrs · 22,483 cycles

AIR TURNBACK, NR 1 ENG EGT INDICATOR FLUCTUATED DURING FLIGHT. REMOVED AND REPLACED SOCKETS AT CONNECTOR D3302, POSITIONS 1 AND 2 PER WDM AND REMOVED AND REPLACED EGT INDICATOR PER MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 24,050 hrs · 22,463 cycles

EEPLS LIGHT REMAINED ILLUMINATED IN AFT SECTION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,023 hrs · 22,439 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 6.5, WL 212. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,023 hrs · 22,439 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 RT SIDE CHORD CRACKED, RBL 28, WL 207. REPAIRED CHORD PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 24,016 hrs · 22,431 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED ON UPPER SURFACE. REPAIRED FORE FLAP ASSY PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 24,016 hrs · 22,431 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP ASSY PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 24,016 hrs · 22,431 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN CRACKED FWD OF I/B ELEVATOR BALANCE BAY. REPAIRED SKIN PER SWA RA NR 1-A55-0334.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,016 hrs · 22,431 cycles

DURING SCHEDULED 1/4D CHECK, HFEC INSPECTION INDICATED BS 178 BULKHEAD CRACKED RBL 5.5. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,016 hrs · 22,431 cycles

DURING SCHEDULED 1/4D CHECK, HFEC INSP INDICATED BS 178 BULKHEAD CRACKED, LBL 5.5. REPAIRED BULKHEAD PER SRM.

Part: SLIDE — SAGGING (FWD ENTRY)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY EXTENDING OUT OF LIMITS. ADJUSTED SLIDE PER MM.

Part: SLIDE — DETACHED (SERVICE DOORWAY)

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — LOW PRESS (SERVICE DOOR)

DURING SCHEDULED A1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESS LOW. REMOVED AND REPLACED SLIDE ASSY.

Part: BULB — FAILED (ROW 22)

DURING SCHEDULED SC CHECK, FOUND EMERGENCY LIGHT AT ROW 22 LEFT SIDE IS INOP. REMOVED AND REPLACED LAMP PER MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SC CHECK, FOUND SIDEWALL EMERGENCY EXIT LAMP INOP AT ROW 7 RT. REMOVED AND REPLACED LAMP PER MM.

Part: WIRE — DISCONNECTED (CABIN)

DURING SCHEDULED BC3 CHECK, FOUND SECTION OF FLOOR TRACK LIGHTING INOP. RECONNECTED AND OP CHECKED PER BOEING M/M.

Part: WIRE — BROKEN (CABIN)

DURING WALK-AROUND, FOUND FLOOR TRACK LIGHTING INOP AT LEFT OVERWING EXIT. FOUND BROKEN WIRE. REPAIRED AND OP CHECKED PER BOEING M/M.

Part: UPLOCK ACTUATOR — MALFUNCTIONED (LT MLG)

ON APPROACH, AFTER GEAR EXTENSION, LEFT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR, WITH NO HELP. MANUALLY EXTENDED GEAR AND GREEN OK LIGHT ILLUMINATED. LANDED AT DAL WITHOUT INCIDENT. REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR AND PERFORMED RETRACTION, OK PER BOEING M/M.

Part: SKIN — DAMAGED (AFT FUS)

ON TAKEOFF, AIRCRAFT EXPERIENCED SLIGHT TAIL DRAG. INSPECTED AREA PER BOEING STRUCTURAL REPAIR MANUAL. PERFORMED MAINT FERRY FLIGHT TO DAL FOR REPAIRS. FABRICATED DOUBLER AND REPAIRED DAMAGED AREA PER BOEING STRUCTURAL REPAIR MANUAL.