N625SW

Part: BATTERY PACK — NO TEST (M1668/STA.603) · airframe 71,105 hrs · 55,091 cycles

OVERHEAD EMERGENCY LIGHTS AT OVER WING EXIT IS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1668 AT STA.603. OPS CHECK GOOD IAW B737 AMM 33-51-51.

Part: POWER SUPPLY — NO TEST (M1675) · airframe 70,634 hrs · 54,839 cycles

IN REFERENCE DAILY CHECK FOUND CABIN L/H SIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED CABIN L/H SIDE EMERGENCY POWER SUPPLY (M1675) PERFORMED OPS CHECK NORMAL PER 33-51-51.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 67,707 hrs · 53,326 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 67,201 hrs · 52,911 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 66,856 hrs · 52,636 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 66,584 hrs · 52,456 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 66,245 hrs · 52,238 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 66,245 hrs · 52,238 cycles

L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: INDICATOR — OUT OF POSITION (R2 DOOR SLIDE) · airframe 66,207 hrs · 52,213 cycles

R2 DOOR SLIDE PRESSURE GAUGE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 66,186 hrs · 52,200 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 65,431 hrs · 51,671 cycles

DECLARED EMERGENCY, A SYSTEM ENGINE PUMP FAILED, NOW PRESSURE LIGHT ILLUMINATED O QUANTITY. R&R HYDRAULIC FLEX LINE HOSE IAW SWPM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 65,275 hrs · 51,564 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 65,133 hrs · 51,464 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 65,039 hrs · 51,405 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 65,039 hrs · 51,405 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 64,368 hrs · 50,958 cycles

L1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: LENS — UNSECURE (CABIN) · airframe 63,856 hrs · 50,622 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS COVER FELL OFF. R & R LENS IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,273 hrs · 50,231 cycles

RIGHT EMER LIGHT INOPERATIVE, BETWEEN ROW 20 - 24. R & R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,273 hrs · 50,231 cycles

RIGHT EXTERIOR OVERWING EMER EXIT LIGHT INOPERATIVE. RELAMPED BULBS IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 62,815 hrs · 49,931 cycles

L2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 62,815 hrs · 49,931 cycles

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

Part: LENS — OUT OF ADJUST (CABIN) · airframe 62,815 hrs · 49,931 cycles

FORWARD LOWER CEILING AFT EXIT LENS OUT OF ADJUSTMENT. ADJUSTED LENS IAW AMM.

Part: CONNECTOR — MISSING (CABIN) · airframe 62,815 hrs · 49,931 cycles

FORWARD LAVATORY EXIT SIGN WIRE CONNECTOR MISSING. INSTALLED CONNECTOR IAW AMM.

Part: LINK ASSY — CORRODED (LT MLG) · airframe 62,815 hrs · 49,931 cycles

LEFT MLG BEAM ATTACH LINK ASSEMBLY CORRODED. R & R LINK ASSEMBLY IAW EA & DWG.

Part: LINK ASSY — CORRODED (RT MLG) · airframe 62,815 hrs · 49,931 cycles

RIGHT MLG BEAM ATTACH LINK ASSEMBLY CORRODED. REPAIRED LINK ASSEMBLY IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

WATER SERVICE PAN STIFFENER CRACKED AT BS 956, STRINGER 25L. R & R STIFFENER IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

BULKHEAD CLOSE OUT BRACKET CRACKED, AT BS 727, RBL 5. R & R BRACKET IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 62,815 hrs · 49,931 cycles

LEFT UPPER WING SKIN CRACKED, BETWEEN RSS 239 - 269, FROM TE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,815 hrs · 49,931 cycles

RIGHT WING UPPER SKIN, CRACKED AFT SPAR ROW, BETWEEN RSS 224 - 270. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (LT MLG) · airframe 62,815 hrs · 49,931 cycles

LEFT MLG FITTING CRACKED IN NR 5 HOLE. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,815 hrs · 49,931 cycles

LEFT WING BRACKET, COMMON TO UPPER SPAR CHORD CRACKED, AT RSS 235. REPAIRED CHORD IAW DWG & EA.

Part: BRACKET — CRACKED (RT WING) · airframe 62,815 hrs · 49,931 cycles

RIGHT WING BRACKET, COMMON TO UPPER SPAR CHORD CRACKED, AT RSS 235. R & R BRACKET IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

FORWARD SERVICE DOOR CREASE BEAM WEB CORRODED AT BS 332, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

STRINGER CORRODED, BETWEEN BS 1006 - 1016, STRINGER 26R. R & R STRINGER IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 62,815 hrs · 49,931 cycles

RIGHT WING REAR SPAR, UPPER CHORD MLG SUPPORT FITTING CRACKED, AT RSS 222.5. REPAIRED CHORD ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,815 hrs · 49,931 cycles

RIGHT WING REAR SPAR, UPPER CHORD FASTENER HOLES CRACKED, BETWEEN RSS 222.5 - 228.5. REPAIRED IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,815 hrs · 49,931 cycles

LEFT WING, REAR SPAR UPPER WEB FASTENER HOLES CRACKED, LOCATED BETWEEN RSS 219 - 222.5. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,815 hrs · 49,931 cycles

RIGHT WING REAR SPAR WEB FASTENER HOLES CRACKED, BETWEEN RSS 219.50 - 222.5. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,815 hrs · 49,931 cycles

LEFT WING REAR SPAR UPPER CHORD, ONE EACH FASTENER HOLE CRACKED, LOCATED AT RSS 222.5. REPAIRED CHORD IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

SHEAR TIE CORRODED AT BS 1006, BETWEEN STRINGER 27L - 27R. R & R SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

SHEAR TIE CORRODED AT BS 987, BETWEEN STRINGER 27L - 27R. R & R SHEAR TIE IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

SKIN CORRODED, BETWEEN BS 987 - 1006, STRINGER 27L. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

SHEAR TIE CORRODED AT BS 967, STRINGER 27L. R & R SHEAR TIE IAW DWG & SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

FUSELAGE UPPER BUTT JOINT SPLICE STRAP CRACKED AT BS 360, STRINGER 3R. FASTENER HOLE REMOVED FOR INSPECTION. REPAIR SPLICE STRAP IAW ER & EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

INNER CHANNEL STRINGER CORRODED AT BS 967, STRINGER 25L. R & R STRINGER IAW SRM.

Part: BRACKET — CRACKED (R1 DOOR) · airframe 62,815 hrs · 49,931 cycles

R1 DOOR AFT STOP NR 1, T BRACKET CRACKED ON INBD LOWER RADIUS. R & R T BRACKET IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

FORWARD ENTRY DOOR LOWER AFT CORNER SKIN CRACKED AT BS 346, STRINGER 17L. REPAIRED SKIN IAW ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 11L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

FRAME CORRODED AT BS 727E, STR 27R. REPAIRED FRAME IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

LONGITUDINAL FLOOR BEAM CRACKED BETWEEN BS 665 TO BS 669, LBL 24.5. REMOVED AND REPLACED BEAM IAW DWG AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 669, RBL 24.5. R & R FLOORBEAM IAW DWG & SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

RIGHT LOWER FRAME SECTION, WEB CRACKED AT BS 639, WL 210. REPAIRED FRAME IAW ER & EA.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

FORWARD CARGO DOOR SUB THRESHOLD WEB CORRODED, BETWEEN BS 455 - 476, RBL 29. R & R WEB IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,815 hrs · 49,931 cycles

LEFT WING FORE FLAP DELAMINATED AT UPPER SKIN. REPAIRED FLAP IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

FORWARD RT SERVICE CREASE BEAM CORD MOP SILL CORRODED, BETWEEN BS 312 - 344, RBL 56. R & R MOP SILL IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

FORWARD LT ENTRY CREASE BEAM CORD MOP SILL CORRODED, BETWEEN BS 312 - 360, LBL 56. R & R CHORD IAW DWG.

Part: STRUCTURE — CRACKED (LT WING) · airframe 62,815 hrs · 49,931 cycles

LT WING RIB 135.5 LOWER T-CHORD CRACKED AT AFT VERTICAL RADIUS BETWEEN STR TO STR 3. REPAIRED T CHORD IAW EA.

Part: STRUCTURE — CRACKED (RT WING) · airframe 62,815 hrs · 49,931 cycles

RT WING RIB 135.5 LOWER T-CHORD CRACKED AT AFT VERTICAL RADIUS BETWEEN STR 2 TO STR 3. REPAIRED T CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

FRAME CORRODED AT BS 907, BETWEEN STRINGER 27L - 27R. R & R FRAME IAW SRM.

Part: FITTING — CRACKED (RT WING) · airframe 62,815 hrs · 49,931 cycles

RIGHT WING REAR SPAR FITTING, NR 8 FLAP TRACK OTBD BOLT HOLE CRACKED. R & R FITTING IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

STRINGER SPLICE CRACKED AT STATION 907, STRINGER 19L. R & R SPLICE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

FLOORBEAM CAP CORRODED AT BS 966, RBL 6. R & R CAP IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,815 hrs · 49,931 cycles

STRINGER CHANNEL CORRODED, BETWEEN BS 966 - 1016, STRINGER 27L. R & R STRINGER IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 62,815 hrs · 49,931 cycles

RIGHT WING OTBD LOWER TE WAFFLE PLATE CRACKED. R & R WAFFLE PLATE IAW SRM AND DWG.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,383 hrs · 49,625 cycles

RIGHT AFT EMER LIGHTING BULLNOSE INOPERATIVE. R & R BATTERY PACK ASSEMBLY IAW AMM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 62,227 hrs · 49,509 cycles

L1 DOOR EMER EXIT SIGN COVER LOOSE. SECURED COVER IAW SIP.

Part: FITTING — CORRODED (TE FLAP) · airframe 62,065 hrs · 49,388 cycles

RIGHT WING NR 5 FLAP TRACK CARRIAGE OTBD FWD ROLLER BUSHING BORE FITTING CORRODED. REPAIRED FITTING IAW EA & CMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 61,993 hrs · 49,339 cycles

L2 DOOR EMER EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: COVER — UNSAFETIED (CABIN) · airframe 61,860 hrs · 49,251 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT COVER FELL OFF. INSTALLED COVER IAW MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 61,668 hrs · 49,104 cycles

R1 DOOR EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS IAW MM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 61,388 hrs · 48,900 cycles

FORWARD ENTRY LOWER EXIT SIGN COVER BROKEN. REPAIR COVER IAW EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,870 hrs · 48,539 cycles

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

Part: LENS — LOOSE (EXIT SIGN) · airframe 60,871 hrs · 48,539 cycles

FORWARD CEILING EXIT SIGN LENS LOOSE. R & R LENS IAW AMM.

Part: WIRE — CHAFED (OIL SYSTEM) · airframe 60,535 hrs · 48,315 cycles

DIVERSION, NR 2 ENG OIL PRESS & TEMP GAUGES READ ZERO. OIL TEMP & PRESS ACFT CB POPPED. FOUND WIRE CHAFED & EXPOSED. REPAIRED WIRE IAW WDM.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,362 hrs · 48,200 cycles

LEFT WING OTBD TE AFT FLAP DELAMINATED OTBD EDGE. R & R AFT FLAP IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,362 hrs · 48,200 cycles

LEFT WING NR 2 SLAT SKIN CRACKED LOWER SURFACE AT INBD AUXILIARY TRACK. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,362 hrs · 48,200 cycles

LEFT WING NR 1 SLAT SKIN CRACKED AT LOWER SURFACE AT INBD AUXILIARY TRACK. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 60,362 hrs · 48,200 cycles

RIGHT WING RSS 545, 9" AFT RT SIDE DRY BAY OTBD ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 60,362 hrs · 48,200 cycles

LEFT WING NR 3 SPOILER PANEL DELAMINATED. R & R NR 3 SPOILER IAW AMM.

Part: COVER — CRACKED (CABIN) · airframe 60,293 hrs · 48,149 cycles

LEFT OF R1 DOOR GALLEY EMER EXIT COVER CRACKED. R & R LIGHT IAW AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,041 hrs · 47,977 cycles

R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: COVER — LOOSE (EXIT SIGN) · airframe 59,708 hrs · 47,756 cycles

L1 DOOR LOWER EXIT SIGN COVER LOOSE. SECURED COVER IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 59,538 hrs · 47,646 cycles

AFT OVERHEAD EMER LIGHT LOWER LENS LOOSE AT ROW 2. SECURED LENS IAW AMM.

Part: COVER — BROKEN (CABIN) · airframe 58,890 hrs · 47,181 cycles

FORWARD ENTRY EMER EXIT LIGHT COVER BROKEN. REPAIRED COVER IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 58,727 hrs · 47,062 cycles

OUTBOARD FLOOR SUPPORT STRAPS CRACKED AT BS 312. REPAIRED STRAP IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 58,008 hrs · 46,556 cycles

RIGHT WING INBD LE FORE FLAP DELAMINATED. R & R FORE FLAP IAW MM.

Part: PCU — LEAKING (AILERON) · airframe 57,356 hrs · 46,115 cycles

DIVERSION A SYS LEAKED FOLLOWED BY TOTAL A SYS FAILURE. R & R AILERON PCU IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 57,095 hrs · 45,944 cycles

G4 GALLEY EMERGENCY EXIT LIGHT ASSEMBLY MISSING. INSTALLED LIGHT ASSEMBLY IAW AMM.

Part: SIGN — CRACKED (CABIN) · airframe 57,095 hrs · 45,944 cycles

L1 DOOR EMERGENCY EXIT LIGHT SIGN BASE ASSEMBLY CRACKED. R & R SIGN IAW AMM.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 57,095 hrs · 45,944 cycles

AFT CARGO DOOR CROSS BEAM T CHORD AFT END SURFACE CRACKED FROM 1ST & 3RD OTBD FASTENERS. R & R DOOR IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

SKIN CRACKED AT BS 303.5, STRINGER 8R. REPAIRED SKIN IAW SWA EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

LT MLG WW FWD SIDE BS 727 BULKHEAD, LBL 51, BELOW STRINGER 21L, BONDED DOUBLER CRACKED. REPAIRED DOUBLER IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

R2 DOOR CUT OUT LOWER FWD CORNER CRACKED. REPAIRED CUT OUT IAW SRM & EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 15L. R & R SPLICE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

FWD ENTRY DOOR CUTOUT STRUCTURE ANGLE CRACKED BETWEEN BS 354 TO BS 356, STRINGER 8L. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

CREASE BEAM SUPPORT ANGLE CRACKED BETWEEN BS 962 TO BS 984. R & R BEAM IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

R1 DOOR UPPER FWD CORNER CUT OUT CRACKED AT BS 296, STRINGER 7R. R & R CUT OUT IAW DRAWING & SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

FWD ENTRY DOOR CUTOUT STRUCTURE ANGLE CRACKED AT BS 348, STRINGER 15L. REPAIRED ANGLE IAW SRM & DRAWING.

Part: BRACKET — CRACKED (LT AILERON) · airframe 57,095 hrs · 45,944 cycles

LT WING AIL TE STRUCTURE ANGLE BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

CHORD CRACKED AT BS 727, STRINGER 18A RT. R & R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

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

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 57,095 hrs · 45,944 cycles

PRESS DECK CRACKED AT BS 664, RBL 39. REPAIRED DECK IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,095 hrs · 45,944 cycles

LONGITUDINAL FLOOR BEAM FLANGE CRACKED AT BS 727B, RBL 24.8. REPAIRED FLANGE IAW EA.

Part: LENS — BROKEN (EXIT SIGN) · airframe 56,208 hrs · 45,330 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. R & R LENS IAW MM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 56,185 hrs · 45,314 cycles

RT WING NR 7 FLAP TRACK FLANGES CORRODED. R & R NR 7 FLAP TRACK IAW MM.

Part: JACKSCREW — CORRODED (TE FLAP) · airframe 56,185 hrs · 45,314 cycles

LT WING NR 2 FLAP TRANSMISSION CORRODED AT JACKSCREW ATTACHMENTS TO GIMBAL. R & R JACK SCREW ASSEMBLY IAW AMM.

Part: FITTING — BROKEN (NR 4 SPOILER) · airframe 56,070 hrs · 45,223 cycles

LT WING NR 4 GROUND SPOILER INBD ACTUATOR FITTING FWD LUG BROKEN. R & R FITTING IAW SRM.

Part: HANDLE — LOOSE (L1 DOOR) · airframe 56,070 hrs · 45,223 cycles

L1 DOOR EMERGENCY EVAC SLIDE MANUAL RELEASE HANDLE LOOSE. SECURED HANDLE IAW MT.

Part: HANDLE — LOOSE (R1 DOOR) · airframe 56,070 hrs · 45,223 cycles

R1 DOOR EMERGENCY EVAC SLIDE MANUAL RELEASE HANDLE LOOSE. SECURED HANDLE IAW MT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,418 hrs · 44,731 cycles

RT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,418 hrs · 44,731 cycles

LT OVERWING NR 5 EMERGENCY LIGHT INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,418 hrs · 44,731 cycles

AFT RT NR 5 EMERGENCY LIGHT INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

STRINGER CLIP CRACKED AT STA 727B, STR 8R. R & R CLIP IAW BAC DWG & SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

STRINGER SPLICE CHANNEL CRACKED STA 907, STR 4R. R & R CHANNEL IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

INTERCOSTAL CRACKED BETWEEN BS 663.73 TO BS 685, STR 9R. R & R INTERCOSTAL IAW BAC DWG AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RIGHT BS 767+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

LT BS 787+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,6,7. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

LEFT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

LEFT BS 767+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

LEFT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 4, 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

LEFT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

LEFT BS 827+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

LEFT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 5. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RIGHT BS 887+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RIGHT BS 847+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RT BS 787+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RIGHT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

LEFT BS 887+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3 AND NR 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RIGHT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RIGHT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

LEFT BS 847+10 LWR FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RT BS 887+10 UPPER AFT SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

LT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RT BS 500+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RT BS 400+10 LOWER AFT WINDOW CORNER HAS HFEC CRACKED INDICATION AT HOLES 2, 3, 6, 7. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 4, 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RT BS 500A+10 LOWER AFT SKIN CUTOUT CRACKED AT HOLES 1,2,3,4,7. REPAIRED SKIN IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 55,414 hrs · 44,730 cycles

FORWARD GALLEY EMERGENCY EXIT LIGHT BASE BROKEN. R&R LIGHT ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RT BS 420+10 UPPER FORWARD SKIN CUTOUT CRACKED AT HOLES 6,7. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RT BS 500A+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3,9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RT BS 500B+10 LOWER AFT SKIN CUTOUT CRACKED AT HOLES 2,3,5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RT BS 520+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 4, 6, 7, 11, 12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,414 hrs · 44,730 cycles

RIGHT BS 500C+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,282 hrs · 44,636 cycles

FUSELAGE SKIN CRACKED AT STA 950+7, STR 9R. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 54,521 hrs · 44,104 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS AT FWD ENTRY DOOR IAW M/M OP CHECK NORMAL.

Part: COVER — DEFORMED (CABIN) · airframe 54,392 hrs · 44,016 cycles

OVERHEAD EMERGENCY EXIT LIGHT, AT ROW 2, IS DEFORMED. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT COVER AT ROW 2 PER M/M.

Part: FLAP — PUNCTURED (LT WING) · airframe 53,594 hrs · 43,445 cycles

LEFT WING I/B FOREFLAP PUNCTURED. REMOVED AND REPLACED FOREFLAP PER AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 53,594 hrs · 43,445 cycles

RIGHT WING NR 5 SLAT DELAMINATED ON O/B END. REMOVED AND REPLACED NR 5 SLAT PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 53,343 hrs · 43,245 cycles

LEFT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 53,074 hrs · 43,042 cycles

L1 DOOR EMERGENCY EXIT LIGHTS LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,910 hrs · 42,920 cycles

FUSELAGE SKIN CRACKED AT BS 727C+14, STR 4R. REPAIRED SKIN PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 52,784 hrs · 42,819 cycles

RIGHT EEPLS BROKEN BETWEEN ROW 7 TO ROW 11. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,357 hrs · 42,502 cycles

SKIN CRACKED AT BS 787+6, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,357 hrs · 42,502 cycles

SKIN CRACKED AT BS 876, STR 9R. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 52,267 hrs · 42,434 cycles

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

Part: PACKING — LEAKING (HYDRAULIC SYS) · airframe 52,185 hrs · 42,371 cycles

A SYS HYDRAULIC QTY (1/4) AND SYS HYDRAULIC ENGINE PUMP LIGHT ILLUMINATED ON APPROACH. DECLARED EMERGENCY. INSPECTED AIRCRAFT AND FOUND A SYS ELEC PUMP ACOUSTIC FILTER LEAKING AT UPPER END. REMOVED AND REPLACED PACKING PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 51,943 hrs · 42,195 cycles

LEFT OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 23. SECURED LENS PER AMM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 51,943 hrs · 42,195 cycles

LEFT WING INBOARD AFT FLAP TRAILING EDGE DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FLAP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,787 hrs · 42,079 cycles

SKIN CRACKED AT BS 727 E + 10, STR 10L. REPAIRED SKIN PER EA.

Part: MODULATING VALVE — FAULTY (RT MLG) · airframe 51,503 hrs · 41,880 cycles

AIR TURNBACK - AFTER TAKEOFF AND PUTTING LIGHT TO OFF POSITION, RT MLG FELL TO DOWN POSITION (GREEN LIGHT). LANDED NORMAL. REMOVED AND REPLACED RT MLG PRIORITY MODULAR VALVE PER MM.

Part: STRINGER SPLICE — CORRODED (BS 907 S22R) · airframe 51,475 hrs · 41,853 cycles

STRINGER SPLICE CORRODED AT BS 907 STR 22R. REMOVED & REPLACED SPLICE IAW SRM & DWG.

Part: STRINGER — CORRODED (BS 900 S22R) · airframe 51,475 hrs · 41,853 cycles

AFT CARGO BAY STRINGER CORRODED STR 22R, BS 900. REMOVED AND REPLACED STRINGER PER ER AND EA.

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 51,475 hrs · 41,853 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE IAW MT G25-61-06.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

CORROSION ON SHEAR TIE BS 986 BETWEEN STR 19R-20R. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

BS 178 TO BS 188 RT O/B COCKPIT FLOOR WEB IS CRACKED. REMOVED AND REPLACED WEB PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT SUPPORT ANGLE CORRODED AT BS 727D. REMOVED AND REPLACED ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

SHEAR TIE CRACKED AT BS 188-196.5 WL 207 STR 17 RT. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

FRAME WEB CRACKED AT BS 188, RBL 32. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

LT CREASE BEAM WEB BETWEEN BS 727C & 727D UPPER SURFACE CORRODED. REMOVED AND REPLACED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

LT CREASE BEAM WEB BETWEEN BS 727B & 727C UPPER SURFACE CORRODED. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

LT CREASE BEAM WEB BETWEEN STA 727E & 747 UPPER & LWR SURFACE'S CORRODED. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

LT CREASE BEAM WEB BETWEEN BS 727D & 727E UPPER SURFACE CORRODED. REMOVED AND REPLACED WEB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

FLOORBEAM CRACKED AT BS 947, LBL 54. REPAIRED BEAM PER ER AND EA 1-353-18515.

Part: CREASE BEAM — CORRODED (BS 480-500) · airframe 51,475 hrs · 41,853 cycles

LT CREASE BEAM WEB BETWEEN BS 480 & BS 500 UPPER SURFACE CORRODED. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (BS 847-867) · airframe 51,475 hrs · 41,853 cycles

LT CREASE BEAM WEB BETWEEN BS 847 TO BS 867, UPPER SURFACE CORRODED. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

AFT CABIN FLOOR STRUCTURE LEFT SHEAR WEB AT BS 1006 TO BS 1016, LBL 45 WL 208 HAS CORROSION AT NUT PLATE HOLES. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

CRACK IN WEB FOR BS 178 BULKHEAD LBL 17.0 VERTICAL BEAM WL 26.5 COMMON TO FWD CHORD. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

CORROSION ON CREASE BEAM SHEAR WEB, BS 360-380 RIGHT SIDE WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

AFT CABIN FLOOR STRUCTURE CHANNEL CORRODED AT BS 1006. REMOVED AND REPLACED CHANNEL PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

CRACK IN WEB FOR BS 178 BULKHEAD RBL 17.0 VERTICAL BEAM WL 232 COMMON TO AFT CHORD. REPAIRED WEB IAW SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

CREASE BEAM SHEAR WEB CORRODED BETWEEN BS 380 TO BS 400, WL 208. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

AFT CABIN FLOOR STRUCTURE FLOORBEAM AT BS 967, LBL 5-12", WL 208, HAS CORROSION PITTING AROUND NUT PLATE HOLES. REMOVED AND REPLACED SKIN IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

CREASE BEAM WEB HAS CORROSION BETWEEN BS 867 TO BS 887, LBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 807 TO BS 827, LBL 65. REMOVED AND REPLACED WEB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

FWD CABIN FLOOR STRUCTURE HAS A CRACKED ANGLE AT BS 328, LBL 45 AFT SIDE OF FLOORBEAM. REMOVED AND REPLACED ANGLE IAW SRM.

Part: DOOR FRAME — CORRODED (BS 99) · airframe 51,475 hrs · 41,853 cycles

R2 DOOR AFT FRAME CORRODED BS 99, WL 207-216. REPAIRED FRAME PER ER AND EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

FWD GALLEY DOOR SURROUND STRUCTURE, STR 8R SUPPORT WEB INBD CHORD IS CRACKED AT BS 332.1. REMOVED AND REPLACED CHORD IAW DWG AND SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

FWD GALLEY DOOR SURROUND STRUCTURE, SUPPORT WEB IS CRACKED AT BS 277 STR 14R. REMOVED WEB IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

L1 DOOR SURROUND STRUCTURE, LOWER O/B ZEE CHANNEL BETWEEN BS 312 AND BS 344, STR 17L CORRODED. REMOVED AND REPLACED ANGLE PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 51,475 hrs · 41,853 cycles

LEFT WING O/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 51,475 hrs · 41,853 cycles

L1 DOOR AFT GIRT BAR FITTING ATTACH POINT CORRODED. REMOVED AND REPLACED FITTING ASSY PER SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 51,475 hrs · 41,853 cycles

L1 DOOR FWD GIRT BAR FITTING ATTACH POINT CORRODED. REMOVED AND REPLACED FITTING ASSY PER SRM.

Part: FLOORBEAM — CORRODED (BS 773) · airframe 51,475 hrs · 41,853 cycles

FLOORBEAM CORRODED AT BS 773, RBL 3. REPAIRED SUPPORT PER EA.

Part: FLOORBEAM — CORRODED (BS 773) · airframe 51,475 hrs · 41,853 cycles

FLOORBEAM CORRODED AT BS 773, LBL 3. REPAIRED SUPPORT PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,475 hrs · 41,853 cycles

AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 847, BETWEEN STR 27L TO STR 25R. REPAIRED FRAME IAW EA AND ER.

Part: LIGHT — CRACKED (CABIN) · airframe 51,475 hrs · 41,853 cycles

FWD GALLEY EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 51,475 hrs · 41,853 cycles

R1 DOOR EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS IAW AMM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 51,475 hrs · 41,853 cycles

L2 DOOR ESCAPE SLIDE PRESS BOTTLE GAGE IS OUT ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 51,475 hrs · 41,853 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 51,475 hrs · 41,853 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS IAW AMM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 51,743 hrs · 42,134 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM INNER CHORD CRACKED AT BS 616. REMOVED AND REPLACED CHORD SECTION PER EA.

Part: HYDRAULIC LINE — LEAKING (MLG WW) · airframe 51,069 hrs · 41,541 cycles

AIR TURNBACK/DECLARED EMERGENCY. HYDRAULIC SYSTEM "B" PRESSURE ZERO WHILE CLIMBING THROUGH APPROX 12000 FEET. FOUND LINE FROM ACOUSTIC FILTER LEAKED. REMOVED AND REPLACED LINE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,813 hrs · 41,342 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 50,813 hrs · 41,342 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR FRAME AT BS 492. REMOVED AND REPLACED FRAME IAW ACO AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,813 hrs · 41,342 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, S2R. REMOVED AND REPLACED STRINGER CLIP IAW EA.

Part: STRINGER CLIP — CRACKED (BS 827 S1R) · airframe 50,813 hrs · 41,342 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 1R. REMOVED AND REPLACED STRINGER CLIP IAW EA.

Part: SKIN — CRACKED (BS 827 S1L) · airframe 50,813 hrs · 41,342 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 827+10, STR 1L. REPAIRED SKIN IAW EA.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 50,528 hrs · 41,124 cycles

LANDING GEAR RETRACTED NORMAL. AFTER PLACING HANDLE IN OFF POSITON THE RT MLG EXTENDED. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,810 hrs · 40,561 cycles

DURING SCHEDULED MV2 CHECK FOUND, SKIN CRACKED AT BS 727D+9, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 49,759 hrs · 40,521 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WNG NR 6 L/E SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 49,569 hrs · 40,361 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,475 hrs · 40,291 cycles

DURING SCHEDULED MV3 CHECK FOUND, RT FWD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — LOOSE (CABIN) · airframe 48,782 hrs · 39,766 cycles

EMERGENCY EXIT LIGHT LENS LOOSE. INSTALLED LENS PER MM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 48,481 hrs · 39,538 cycles

AIR TURNBACK / DECLARED EMERGENCY. ON DEPARTURE FLIGHT ATTENDANTS REPORTED FUMES IN THE CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 47,257 hrs · 38,626 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 46,800 hrs · 38,279 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT I/B OF O/B AUX TRACK LOWER SKIN CRACKED. REMOVED AND REPLACED NR 2 SLAT PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 46,800 hrs · 38,279 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 3 SLAT I/B END UPPER T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 46,800 hrs · 38,279 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 1 SLAT LOWER T/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 46,800 hrs · 38,279 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 4 SLAT I/B END DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,275 hrs · 37,864 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,275 hrs · 37,864 cycles

DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT BROKEN AT ROW 8. REMOVED AND REPLACED LIGHT PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT MLG WELL WHEEL LOWER PRESS DECK CRACKED AT BS 663.75, LBL 32. REPAIRED WEB PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR CUTOUT AFT SIDE AT NR 11 STRINGER WEB ATTACH AFT CLIP CRACKED. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR CUTOUT AFT SIDE, AT NR 10 STRINGER WEB ATTACH AFT CLIP CRACKED. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 46,191 hrs · 37,795 cycles

DURING SCHEDULED 14Y CHECK, FOUND CRACKED VERTICAL CORNER L-BRACKET AFT SIDE OF STUB FRAME, BS 639, RBL 46. REMOVED AND REPLACED ANGLE PER BAC DWG.

Part: LENS — CRACKED (CABIN) · airframe 45,344 hrs · 37,166 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND AFT EEPLS LENS CRACKED AT ROW 23. REMOVED AND REPLACED LENS PER MM.

Part: MOUNT — CRACKED (EVAC SLIDE) · airframe 45,344 hrs · 37,166 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD MOUNT CRACKED. REMOVED AND REPLACED MOUNT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,956 hrs · 36,124 cycles

DURING SCHEDULED SPV, FOUND EMERGENCY LIGHT INOP AT ROW 17. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,946 hrs · 36,118 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 6 L/E SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: STRIP — FADED (CABIN) · airframe 43,946 hrs · 36,118 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP FADED BETWEEN ROW 12 TO ROW 22. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (AFT DOOR) · airframe 43,937 hrs · 36,112 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 43,719 hrs · 35,956 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS LOOSE. R&R LENS PER MM.

Part: MODULE — LEAKING (HYDRAULIC SYS) · airframe 43,331 hrs · 35,698 cycles

AIR TURNBACK, A-SYS HYD FAILURE IN FLT UPON GEAR RETRACTION. NO OVERHEAT LIGHT, NOSE GEAR EXTENDED MANUALLY. REMOVED AND REPLACED A-SYSTEM HYD MODULES AND HYD FILTERS.

Part: STRIP — LOOSE (CABIN) · airframe 43,011 hrs · 35,475 cycles

RT EEPLS STRIP LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,941 hrs · 35,424 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT DOOR SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,801 hrs · 35,316 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 42,382 hrs · 35,025 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT KEEL BEAM CRACKED AT BS 700, LBL 1. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,262 hrs · 34,935 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 41,917 hrs · 34,689 cycles

FOUND L2 DOOR EMERGENCY ESCAPE SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 41,158 hrs · 34,130 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CONTROL CABLE — LOOSE (NLG) · airframe 40,467 hrs · 33,635 cycles

ON GEAR EXTENSION ALL THREE GEAR IN TRANSIT LIGHTS ILLUMINATED IN ADDITION TO DOWN AND LOCKED INDICATION. CYCLED GEAR AND TRANSIT LIGHTS EXTINGUISHED. LANDING GEAR CONTROL CABLE LGVA TENSION LOOSE. ADJUSTED CABLE PER MM.

Part: KEELBEAM — CORRODED (BS 787) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 787, RBL 6.5. REMOVED AND REPLACED CHORD PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT AFT END. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500A S27R) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500A, STR 27R. REPAIRED SKIN PER SRM.

Part: TAB — FAILED (ELEVATOR) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB AND NR 1 ELEVATOR TAB BUSHINGS PER MM.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL STABILIZER STIFFENER AFT OF STABILIZER MOUNT CRACKED AT STA 1088. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, STR 26L TO STR 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500B, STR 27R TO STR 26L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 520, STR 26L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 520, STR 28R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,373 hrs · 33,571 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 40,122 hrs · 33,398 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 39,821 hrs · 33,192 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 39,765 hrs · 33,145 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: LENS — MISSING (CABIN) · airframe 39,262 hrs · 32,753 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 39,020 hrs · 32,565 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 38,683 hrs · 32,299 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT UPPER CORNER. REPAIRED FRAME PER ACO.

Part: LIGHT — BROKEN (CABIN) · airframe 38,683 hrs · 32,299 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LOGIC CARD — FAULTY (NOSE BAY) · airframe 37,672 hrs · 31,457 cycles

LOWERED GEAR HANDLE, GOT THREE GREEN LIGHTS FOLLOWED BY LEFT MLG RED LIGHT FLICKERING. RECYCLED GEAR HANDLE GOT THREE GREEN LIGHTS. REMOVED AND REPLACED DOWN LOCK SENSOR AND LOGIC CARD PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 37,562 hrs · 31,367 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 37,562 hrs · 31,367 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 36,129 hrs · 30,248 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: CONTROL ROD — CORRODED (LT ELEVATOR TAB) · airframe 34,982 hrs · 29,331 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT ELEVATOR TRIM TAB CONTROL RODS CORRODED. REMOVED AND REPLACED CONTROL RODS PER MM.

Part: CONTROL ROD — CORRODED (RT ELEVATOR TAB) · airframe 34,982 hrs · 29,331 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT ELEVATOR TRIM TAB CONTROL RODS CORRODED. REMOVED AND REPLACED CONTROL RODS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 34,551 hrs · 28,772 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 34,050 hrs · 28,571 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGECNY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 34,050 hrs · 28,571 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 34,050 hrs · 28,571 cycles

DURING SCHEDULED 10Y CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED AT BS 360. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,050 hrs · 28,571 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 34,050 hrs · 28,571 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EXIT EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (BS 616 S16L) · airframe 34,050 hrs · 28,571 cycles

DURING SCHEDULED 10Y CHECK, FOUND FRAME CRACKED AT BS 616, STR 16L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CORRODED (BS 807 S27L-27R) · airframe 34,050 hrs · 28,571 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 27L TO STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 34,050 hrs · 28,571 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 34,050 hrs · 28,571 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD T/E FLAP DELAMINATED. REPAIRED T/E FLAP PER SRM.

Part: CLIP — CRACKED (DOOR FRAME) · airframe 34,050 hrs · 28,571 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR FRAME CUTOUT END CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED FRAME END CLIP PER EA.

Part: SILL — CORRODED (FUSELAGE) · airframe 34,050 hrs · 28,571 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO DOOR CUTOUT LOWER SILL WEB CORRODED AT BS 794.3 TO BS 847. R&R WEB PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 32,710 hrs · 27,532 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 31,788 hrs · 26,805 cycles

RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FITTING — CRACKED (L1 DOOR) · airframe 30,407 hrs · 25,712 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR LOWER FUSELAGE HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM & SAM 326.

Part: LENS — LOOSE (CABIN) · airframe 29,548 hrs · 25,030 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS AT ROW 22, LOOSE. SECURED LIGHT LENS PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 29,490 hrs · 24,988 cycles

EMERGENCY EXIT PHOTOLUMINESCENT STRIP AT ROW 10 DEF, LOOSE. SECURED STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 28,634 hrs · 24,290 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR PER MM.

Part: SKIN — WORN (FUSELAGE) · airframe 28,500 hrs · 24,182 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 860, STRINGER 1, WORN. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 27,954 hrs · 23,752 cycles

L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: COVER — MISSING (CABIN) · airframe 27,706 hrs · 23,536 cycles

EEPLS COVER AT RT ROW 6 TO ROW 8, MISSING. INSTALLED EEPLS COVER PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 26,761 hrs · 22,749 cycles

L1 DOOR EVAC SLIDE INADVERTENTLY FELL OUT OF HOUSING. REINSTALLED L1 DOOR EVAC SLIDE INTO HOUSING PER MM.

Part: GASPER FAN — OVERHEATED (A/C BAY) · airframe 25,982 hrs · 22,153 cycles

FUMES IN PAX CABIN. REMOVED AND REPLACED A/C GASPER FAN PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 25,839 hrs · 22,043 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF POSITION AND RELEASE CABLE MISROUTED. REPOSITIONED SLIDE ASSY AND REROUTED CABLE PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 25,799 hrs · 22,005 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED OUTBD OF MAIN TRACK. REPAIRED SLAT SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 25,650 hrs · 21,884 cycles

AFT ENTRY DOOR EVAC SLIDE OUT OF POSITION. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 24,673 hrs · 56,925 cycles

DURING SCHEDULED C4 CHECK, FOUND LT INBD FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LT INBD FOREFLAP PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 24,183 hrs · 20,683 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: TRUNNION PIN — CORRODED (LT & RT MLG) · airframe 23,711 hrs · 20,299 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11251-32, FOUND BOTH LT & RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT & RT MLG TRUNNION PINS PER MM.

Part: BEARING — DAMAGED (NLG) · airframe 23,707 hrs · 20,296 cycles

AFTER TURING TILLER WOULD NOT RETURN TO CENTER. R&R NLG STEERING COLLAR BEARING PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 22,987 hrs · 19,748 cycles

DURING SCHEDULED C2 CHECK, FOUND LT INBD T/E FLAP DELAMINATED. REMOVED AND REPLACED LEFT INBD T/E FLAP PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 22,800 hrs · 19,595 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 20,199 hrs · 17,459 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 19,282 hrs · 16,699 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 17,400 hrs · 15,103 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT LENS CRACKED AT FWD SECTION. R&R LENS PER MM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 17,400 hrs · 15,103 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 182, LBL 5.7. REPAIRED VERTICAL BEAM WEB PER SWA RA.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 17,400 hrs · 15,103 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR FRAME CUTOUTS CRACKED AT AFT STOPS NR3 & NR4. REPAIRED DOOR FRAME PER SWA TI.

Part: WIRE — DISCONNECTED (CABIN) · airframe 17,270 hrs · 14,986 cycles

EEPLS INOP AT ROW 21. RECONNECTED EEPLS WIRING PER MM.

Part: BULB — INOPERATIVE (CABIN FLOOR) · airframe 16,526 hrs · 14,401 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT ROW 20. RELAMPED EEPLS PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 16,526 hrs · 14,401 cycles

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

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 15,675 hrs · 13,686 cycles

EEPLS NEAR O/W EXIT HAS LOOSE WIRES EXPOSED. REMOVED AND REPLACED EEPLS SOCKET AT ROW 15 PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 15,595 hrs · 13,623 cycles

EEPLS TRACK LOOSE AT MID CABIN. SECURED EEPLS TRACK PER MM.

Part: COVER — MISSING (CABIN) · airframe 15,614 hrs · 13,640 cycles

EEPLS DISLODGED AND PART OF COVER MISSING. REPLACED COVER AND SECURED LIGHT LENS PER MM.

Part: COVER — MISSING (ROW 11) · airframe 15,558 hrs · 13,590 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 11. REPLACED EEPLS TRACK COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 15,133 hrs · 13,204 cycles

EEPLS TRACK LOOSE AT MID CABIN. SECURED LIGHTS AND TRACK PER MM.

Part: SLIDE — LOW PRESS (PASSENGER DOOR)

FWD ENTRY DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY.

Part: SKIN — DENTED (BS 440)

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 440. REPAIRED PER BOEING SRM.