N379SW

Part: LIGHT — LOOSE (CABIN) · airframe 71,500 hrs · 57,840 cycles

FORWARD ENTRY EMERGENCY LIGHT COVER LOOSE. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,026 hrs · 57,535 cycles

RIGHT WING EMERGENCY LIGHT INOPERATIVE. R & R THE CHARGER ASSEMBLY IAW AMM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,026 hrs · 57,535 cycles

R2 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. R & R THE CHARGER ASSEMBLY IAW AMM.

Part: SIGN — LOOSE (RT OVERWING) · airframe 70,998 hrs · 57,517 cycles

RIGHT OVERWING EXIT SIGN LOOSE. SECURED SIGN IAW S.I.P.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 70,850 hrs · 57,419 cycles

RIGHT OVERWING DOOR EXIT SIGN LOOSE. R & R LENS IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,801 hrs · 57,381 cycles

AFT CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: HOLDER — INOPERATIVE (BATTERY PACK) · airframe 70,764 hrs · 57,358 cycles

R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY HOLDER IAW AMM.

Part: SUPPORT BRACKET — CORRODED (TE FLAP) · airframe 70,314 hrs · 57,052 cycles

LEFT WING OTBD MIDFLAP, INBD CARRIAGE BEARING SUPPORT BRACKET CORRODED. R & R SUPPORT BRACKET IAW MT.

Part: SUPPORT BRACKET — CORRODED (TE FLAP) · airframe 70,314 hrs · 57,052 cycles

LEFT WING OTBD MIDFLAP, OTBD CARRIAGE BEARING SUPPORT BRACKET CORRODED. R & R BRACKET IAW MT.

Part: SENSOR — FAULTY (NR 1 ENGINE) · airframe 69,866 hrs · 56,761 cycles

DIVERSION, LT ENG VERY SLOW TO SPOOL. LONG DELAY & SPLIT VERSUS RT ENG. R & R LT ENG COMPRESSOR INLET TEMPERATURE SENSOR IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,735 hrs · 56,676 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 1. RELAMPED LIGHT IAW MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 69,521 hrs · 56,538 cycles

FORWARD EXIT DOOR, EXIT SIGN LENS COVER LOOSE. R & R LENS IAW MM.

Part: DOWNLOCK SENSOR — FAULTY (NLG WW) · airframe 69,216 hrs · 56,346 cycles

AIR TURN BACK, AFTER RAISING GEAR HANDLE ON TAKEOFF, THE NOSE GEAR RED LIGHT & GREEN LIGHT REMAINED ON. R & R NOSE DOWNLOCK SENSOR IAW AMM.

Part: UPLOCK SENSOR — FAULTY (NLG WW) · airframe 69,216 hrs · 56,346 cycles

AIR TURN BACK, AFTER RAISING GEAR HANDLE ON TAKEOFF, THE NOSE GEAR RED LIGHT & GREEN LIGHT REMAINED ON. R & R NOSE UPLOCK SENSOR IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 69,164 hrs · 56,312 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

FUSELAGE SKIN BUTT SPLICE CRACKED AT STATION 908, STRINGER 4L. REPAIRED SPLICE IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

SUPPORT BRACKET, CRACKED AT BS 540, LBL 45. R & R BRACKET IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

FUSELAGE SKIN CRACKED AROUND THE VHF3 ANTENNA. REPAIRED SKIN IAW EA & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

L1 DOOR CUT OUT, UPPER FWD TRIM ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 69,129 hrs · 56,290 cycles

FORWARD CARGO DOOR SKIN CRACKED AT HANDLE CUT OUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 69,129 hrs · 56,290 cycles

FORWARD CARGO DOOR SKIN, CRACKED AT FWD SIDE OF HANDLE ASSEMBLY CUT OUT. REPAIRED SKIN IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

STRINGER SPLICE CRACKED AT STATION 908, STRINGER 4L. R & R SPLICE IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

STRINGER SPLICE CRACKED AT STATION 908, STRINGER 5R. R & R SPLICE IAW EA.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 69,129 hrs · 56,290 cycles

FORWARD CARGO DOOR SKIN, CRACKED AT HANDLE CUT OUT FWD SIDE FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

SHEAR TIE CRACKED AT BS 908, BETWEEN STRINGER 2R - 3R. R & R SHEAR TIE IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

STRINGER SPLICE CRACKED AT STATION 908, STRINGER 5L. R & R SPLICE IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

STRINGER SPLICE CRACKED AT STATION 908, STRINGER 4R. R & R SPLICE IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,129 hrs · 56,290 cycles

LEFT WING UPPER WING SKIN, FASTENER HOLE CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 69,129 hrs · 56,290 cycles

LEFT WING UPPER AFT SKIN CRACKED ON UPPER WING APPROX 17" INBD OF RSS 254. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,129 hrs · 56,290 cycles

RIGHT WING UPPER AFT SKIN AT EDGE CRACKED INSIDE 5 EACH FASTENER HOLES, BETWEEN RSS 238 TO RSS 268. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (RT WING) · airframe 69,129 hrs · 56,290 cycles

RIGHT WING WEB CRACKED AT UPPER AREA RSS 224-14, 4TH HOLE FROM INBD AT MLG FITTING. REPAIRED WEB IAW EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 69,129 hrs · 56,290 cycles

LEFT WING NR 1 FLAP TRACK, AFT FAIRING CRACKED AT 6 O'CLOCK POSITION, BETWEEN 2 FASTENER HOLES. REPAIRED FAIRING IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

RIGHT CREASE BEAM CORRODED AT STATION 837 - 907. REPAIRED BEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

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

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

INTERCOSTAL ANGLE SUPPORT CRACKED, BETWEEN BS 277 - 291, BETWEEN STRINGER 11R - 12R. R & R SUPPORT IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

INTERCOSTAL L ANGLE SUPPORT CRACKED, BETWEEN BS 277 - 291, BETWEEN STRINGER 12R - 13R. R & R L ANGLE IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,129 hrs · 56,290 cycles

RIGHT WING TE INBD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

INTERCOSTAL ANGLE SUPPORT CRACKED, BETWEEN BS 277 - 291, STRINGER 1R. R & R SUPPORT IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 69,129 hrs · 56,290 cycles

RIGHT SIDEWALL EXIT LIGHT BROKEN AT ROW 9. R & R LIGHT IAW AMM.

Part: WEB — CRACKED (LT WING) · airframe 6,928 hrs · 56,290 cycles

LEFT WING WEB CRACKED AT RSS 224.14, OTBD FIRST UPPER OPEN HOLE. REPAIRED WEB IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 69,129 hrs · 56,290 cycles

LEFT WING FITTING CRACKED, FOUND ON AT RSS 224.14, OTBD FIRST BOTTOM FASTENER HOLE. R & R FITTING IAW EA.

Part: STRUCTURE — CRACKED (LT WING) · airframe 69,128 hrs · 56,290 cycles

LEFT WING UPPER CHORD CRACKED INBD OF RSS 224.14 FIRST TWO OPEN FASTENER HOLES. REPAIRED CHORD IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 69,129 hrs · 56,290 cycles

RIGHT WING FITTING CRACKED OTBD OF RSS 224.14, IN THE FIRST THREE UPPER ROW OPEN FASTENER HOLES. R & R FITTING IAW EA.

Part: STRUCTURE — CRACKED (RT WING) · airframe 69,128 hrs · 56,290 cycles

RIGHT WING CRACK FOUND IN THE CHORD INBD OF RSS 224.14, FIRST UPPER ROW OPEN FASTENER HOLE & SECOND LOWER ROW OPEN FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 986.5 - 1006. R & R WEB IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

FLOOR WEB CORRODED, BETWEEN BS 986.5 - 1016. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 360 - 380. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 787 - 807. R & R WEB IAW SRM & DWG.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 69,128 hrs · 56,290 cycles

AFT R2 DOOR FRAME AT CORRODED AT BS 993.5 AT FLOOR LEVEL. REPAIRED FRAME IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 69,128 hrs · 56,290 cycles

FLOOR WEB AT DOOR CUT OUT CORRODED AT BS 986. R & R CUT OUT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,128 hrs · 56,290 cycles

FRAME INTERCOSTAL CRACKED, BETWEEN BS 277 - 291, STRINGER 14R. R & R INTERCOSTAL IAW EA.

Part: SKATE ANGLE — CORRODED (FUSELAGE) · airframe 6,928 hrs · 56,290 cycles

R2 LOWER SILL SKATE ANGLE CORRODED, BETWEEN BS 946 - 986. R & R ANGLE IAW DWG & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,128 hrs · 56,290 cycles

FLOORBEAM UPPER T CAP CORRODED, AT BS 967, BETWEEN LBL 62 TO RBL 62. R & R T CAP IAW EA..

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,129 hrs · 56,290 cycles

RIGHT WING DELAMINATED ON OTBD SIDE ON FLAP TRACK SUPPORT FAIRING SKIN, WBL 191. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,128 hrs · 56,290 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 62 TO RBL 62. REPAIRED FLOORBEAM IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,128 hrs · 56,290 cycles

R1 DOOR LT ANGLE CRACKED AT BS 294, STRINGER 10R. R & R L ANGLE IAW EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

STUB BEAM DOUBLER CRACKED AT BS 639, RBL 52.5. R & R DOUBLER IAW DWG & SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 69,129 hrs · 56,290 cycles

LONGITUDINAL FLOORBEAM ATTACHMENT CLIP CRACKED AT BS 639, RBL 45.5. R & R BEAM IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,128 hrs · 56,290 cycles

FRAME WEB CRACKED AT BS 328, BETWEEN STRINGER 20R - 21R. FRAME WEB IAW EA.

Part: SLAT — DELAMINATED (RT WING) · airframe 68,358 hrs · 55,732 cycles

NUMBER 5 SLAT DELAMINATED. R & R SLAT ASSEMBLY IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 68,000 hrs · 55,484 cycles

FORWARD ENTRY AREA EMER EXIT LIGHT COVER CRACKED. REPLACED COVER IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 68,000 hrs · 55,484 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED ON LOWER INBD SIDE. R & R AFT FLAP IAW MM.

Part: STOP FITTING — CRACKED (L1 DOOR) · airframe 68,000 hrs · 55,484 cycles

L1 DOOR UPPER AFT STOP PIN FITTING CRACKED. R & R DOOR IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,657 hrs · 55,252 cycles

AFT EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 67,550 hrs · 55,180 cycles

L1 DOOR EXTERNAL SKIN CRACKED AT UPPER AFT CORNER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 67,550 hrs · 55,180 cycles

LEFT HORIZONTAL STABILIZER CRACKED LOWER SURFACE, AFT SPAR AT APPROX 55" OTBD OF FUSELAGE. REPAIRED STABILIZER IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,205 hrs · 54,267 cycles

RIGHT BULLNOSE EMER EXIT LIGHTS INOPERATIVE BETWEEN ROW 13 TO 24. R & R BATTERY PACK IAW MM.

Part: SENSING ELEMENT — FAULTY (RT WING) · airframe 65,455 hrs · 53,751 cycles

AIR TURN BACK RT WING TO BODY OVERHEAT LIGHT ILLUMINATED. R & R SENSOR ELEMENT M371 IAW MM.

Part: ATTACH BRACKET — CRACKED (R2 DOOR SLIDE) · airframe 64,420 hrs · 52,996 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOWER FWD ATTACH BRACKET CRACKED. R & R BRACKET IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 64,124 hrs · 52,805 cycles

L1 DOOR EMERGENCY EXIT LENS BROKEN. R & R LENS IAW SIP.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

LT RAM AIR EXHAUST DUCT INTERNAL STRUCTURE CRACKED. REPAIRED STRUCTURE IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

WEB CRACKED BETWEEN BS 500A TO BS 500B, STRINGER 26R. R & R WEB IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

WEB CRACKED BETWEEN BS 500B TO BS 500C, STRINGER 26R. R & R WEB IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

STRINGER CRACKED AT BS 727+3, STRINGER 19R. REPAIRED STRINGER IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

INTERNAL STRAP CRACKED AT BS 727+4, STRINGER 19R. R & R STRAP IAW SRM & DRAWING.

Part: BRACKET — CRACKED (LT WING) · airframe 63,318 hrs · 52,254 cycles

LT WING FLAP TRACK TRANSMISSION BRACKET CRACKED. R & R BRACKET IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

ANGLE CRACKED AT ON RACK E2-4 EE COMPARTMENT. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

SUPPORT BRACKET CRACKED AT BS 727D, STRINGER 27R. R & R BRACKET IAW SRM & DRAWING.

Part: SKIN — CRACKED (AILERON TAB) · airframe 63,318 hrs · 52,254 cycles

RT AILERON TAB CRACKED ON LOWER SURFACE OTBD SIDE. R & R TAB IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

ANGLE CRACKED AT BS 500B, STRINGER 26L. R & R ANGLE IAW SRM & DRAWING.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

SEAT TRACK CRACKED AT BS 947.5, LBL 45.50. REPAIRED SEAT TRACK IAW SRM.

Part: STRUCTURE — WORN (LE SLAT) · airframe 63,318 hrs · 52,254 cycles

RT WING NR 6 SLAT CAN INBD WORN. R & R SLAT CAN IAW EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

LT SIDE KEEL BEAM CORRODED BETWEEN BS 707 TO BS 727. REPAIRED BEAM IAW EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

RT SIDE KEEL BEAM CORRODED BETWEEN BS 707 TO BS 727. REPAIRED BEAM IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FRAME CORRODED AT BS 360, BETWEEN STRINGER 28L TO STRINGER 28R. REPAIRED FRAME IAW EA NO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

VERTICAL ANGLE CRACKED AT BS 294.5, STRINGER 27R. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

EE COMPARTMENT SUPPORT ANGLE CRACKED AT BS 312+9, STRINGER 20L. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 22L. R&R TIE CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 21L. R & R TIE CLIP IAW SRM & DRAWING.

Part: PANEL — CRACKED (E&E BAY) · airframe 63,318 hrs · 52,254 cycles

AIR DISTRIBUTION PANEL ASSEMBLY CRACKED ABOVE RACK E1 IN EE COMPARTMENT. REPAIRED PANEL ASSEMBLY IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STRINGER 23L. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 26R. R & R TIE CLIP IAW SRM & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

WEB UPPER FLANGE CORRODED BETWEEN BS 500B TO BS 500C, BETWEEN STRINGER 25L & STRINGER 26L. R & R WEB IAW SRM & DRAWING.

Part: RIB — CRACKED (LT WING) · airframe 63,318 hrs · 52,254 cycles

LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STRINGER 2 & STRINGER 3. REPAIRED CHORD IAW EA.

Part: SUPPORT ANGLE — CRACKED (FLAP TRACK) · airframe 63,318 hrs · 52,254 cycles

LT WING NR 1 SUPPORT ANGLE CRACKED ON OTBD FLAP TRACK. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

WEB CORRODED BETWEEN BS 500C TO BS 500D, BETWEEN STRINGER 25L & STRINGER 26L. R & R WEB IAW SRM & DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FLOOR BEAM CRACKED AT BS 947.5, LBL 53.5. REPAIRED BEAM IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

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

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 63,318 hrs · 52,254 cycles

FRAME CRACKED BETWEEN BS 947.5 +10 TO BS 967, BETWEEN STRINGER 16R TO STRINGER 17R ON AFT SERVICE DOOR RT. REPAIRED FRAME IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

SHEAR TIE CORRODED AT BS 967, BETWEEN STRINGER 20R TO STRINGER 21R. R & R SHEAR TIE IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

SHEAR TIE CORRODED AT BS 520, BETWEEN STRINGER 27L TO STRINGER 28L. R & R SHEAR TIE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

TIE CLIP CRACKED AT BS 480, STRINGER 23L. R & R TIE CLIP IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 5 · airframe 63,318 hrs · 52,254 cycles

FWD CARGO COMPARTMENT FRAME CORRODED AT BS 500B, BETWEEN STRINGER 27R TO STRINGER 28R. REPAIRED SHEAR TIE IAW SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,318 hrs · 52,254 cycles

RT VERTICAL STABILIZER OTBD REAR DRAG ANGLE FITTING CORRODED. R & R FITTING IAW SRM & DRAWING.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

BRACKET CRACKED AT BS 380, STRINGER 26L FWD CARGO COMPARTMENT. R & R BRACKET IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

SUPPORT ANGLE CRACKED AT BS 540, RBL 3. R &R ANGLE IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 27L TO STRINGER 28L. R & R SHEAR TIE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

WEB CRACKED BETWEEN STATION 344 TO STATION 360, BL 0. R &R WEB IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FRAME CORRODED AT BS 787, BETWEEN STRINGER 27R TO STRINGER 27L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

TIE CLIP CRACKED AT BS 727C, STRINGER 25R. R & R TIE CLIP IAW SRM & DRAWING.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 63,318 hrs · 52,254 cycles

RT ELEVATOR TAB TE DELAMINATED. R & R TAB IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 63,318 hrs · 52,254 cycles

LT WING INBD AFT FLAP LOCATED AT INBD SIDE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

TIE CLIP CRACKED AT BS 727B, STRINGER 25R. R & R TIE CLIP IAW SRM & DRAWING.

Part: PLATE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

AFT CARGO PLATE CRACKED AT BS 794, BETWEEN STRINGER 21R TO STRINGER 25R. R & R PLATE IAW SRM & DRAWING.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

AFT PRESSURE BULKHEAD CHORD ANGLE STIFFENER CORRODED AT BS 1016, BETWEEN STRINGER 27R TO STRINGER 27L. REPAIRED STIFFENER IAW EO & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

INTERCOSTAL CRACKED BETWEEN STATION 328 TO STATION 344, LBL 46. R & R CHANNEL IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

AFT CARGO COMPARTMENT STIFFENER CRACKED AT BS 727, RBL 5. R & R STIFFENER IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 747, STRINGER 25R. R &R ANGLE IAW SRM & DRAWING.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

AFT BULKHEAD CHORD ANGLE STIFFENER CORRODED AT BS 1016, BETWEEN STRINGER 27R TO STRINGER 27L. REPAIRED STIFFENER IAW EO & EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

BRACKET CRACKED AT BS 727, RBL 6. R & R BRACKET IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FRAME CORRODED AT BS 727D, BETWEEN STRINGER 27L TO STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 727A, STRINGER 25R. R & R ANGLE IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

UNDER FWD GALLEY AREA STRAP CRACKED AT STATION 328, LBL 45. R & R STRAP IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

UNDER FLOOR STRUCTURE FWD GALLEY STRAP CRACKED AT STATION 312, RBL 30. R & R STRAP IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 27R TO STRINGER 28R. R & R SHEAR TIE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FRAME CRACKED AT BS 500B, BETWEEN STRINGER 20L TO STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

SKIN WRINKLED BETWEEN BS 1040 TO BS 1064, BETWEEN STRINGER 15L TO STRINGER 16L. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FRAME CRACKED AT BS 500B, BETWEEN STRINGER 20L TO STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

NLG WW ON LT SIDE CRACKED AT BS 243.7+3.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 63,318 hrs · 52,254 cycles

RT INBD FLAP STIFFENER CRACKED. R & R STIFFENER IAW SRM & DRAWING.

Part: ACCESS PANEL — CRACKED (LT PYLON) · airframe 63,318 hrs · 52,254 cycles

NR 1 ENGINE FAIRING STRUT FAIRING ACCESS PANEL 5764L CRACKED. REPAIRED PANEL IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

L1 DOOR SURROUND STRUCTURE ANGLE CRACKED BETWEEN BS 294.5 & BS 303.9, STRINGER 16L. R & R ANGLE IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (LT PYLON) · airframe 63,318 hrs · 52,254 cycles

LT PYLON OTBD TRACK INBD FLAP STIFFENER CRACKED. R & R STIFFENER IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

SKIN CRACKED AT BS 947.5+11, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 20L TO STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: HINGE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

L1 DOOR UPPER COVER HINGE CRACKED AT BS 303.9, STRINGER 10L. REPAIRED HINGE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT PYLON) · airframe 63,318 hrs · 52,254 cycles

RT PYLON INTERNAL AREA ACCESS PANEL 5857R SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: HINGE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

L1 DOOR LOWER COVER HINGE CRACKED AT BS 303.9, STRINGER 13L. R&R HINGE IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,318 hrs · 52,254 cycles

MLG WW PRESSURE WEB CRACKED AT BS 663.75 TO BS 675, LBL 45.5. REPAIRED WEB IAW SWA EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 63,318 hrs · 52,254 cycles

LT WING TE SUPPORT ANGLE CRACKED AT LEVEL RSS 533 + 12 INCHES. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FUSELAGE SKIN CRACKED AT BS 947+11, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 63,318 hrs · 52,254 cycles

LT WING LOWER SURFACE ACCESS PANEL 36241L CRACKED. REPAIRED PANEL IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,318 hrs · 52,254 cycles

MLG WW PRESSURE WEB CRACKED AT BS 663.75, LBL 24.5. REPAIRED WEB IAW SWA EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,318 hrs · 52,254 cycles

MLG WW PRESSURE WEB CRACKED AT BS 663.75, LBL 45.5. REPAIRED WEB IAW SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FLOORBEAM CRACKED AT BS 663.75+1, LBL 24.5. REPAIRED CHORD IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,318 hrs · 52,254 cycles

MLG WW PRESSURE WEB CRACKED AT BS 675.75, LBL 45.5. REPAIRED WEB IAW SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FLOOR BEAM CRACKED AT BS 663.75+3, LBL 24.5. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FUSELAGE FRAME CRACKED AT BS 727, STRINGER 18A. REPAIRED FRAME IAW SWA EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

STRINGER 18A RT CRACKED AT BS 727. REPAIRED STRINGER IAW SWA EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

RT SIDE CHORD CRACKED AT BS 727, STRINGER 18A LOWER AFT HOLE. R & R CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

FUSELAGE CHORD CRACKED AT BS 727, STRINGER 18A LT SIDE. R & R CHORD IAW SWA EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,318 hrs · 52,254 cycles

LT SIDE CRACKED AT BS 727, STRINGER 18A LOWER FASTENER. R & R CHORD IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 62,693 hrs · 51,784 cycles

LT WING INBD AFT FLAP DELAMINATED ON OTBD CORNER. R&R FLAP ASSEMBLY IAW MM.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 62,475 hrs · 51,610 cycles

L1 DOOR EMERGENCY EXIT LIGHT FELL OFF. R&R LIGHT ASSEMBLY IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 62,360 hrs · 51,522 cycles

L1 DOOR LOWER EGRESS LIGHT LENS BROKEN. R&R LENS PER MM.

Part: ACTUATOR — BROKEN (RT SPOILER) · airframe 62,203 hrs · 51,401 cycles

RT WING NR 5 SPOILER OTBD ACTUATOR BOTTOM MOUNTING LUG BROKEN. R & R ACTUATOR IAW AMM.

Part: FITTING — BROKEN (RT SPOILER) · airframe 62,203 hrs · 51,401 cycles

RT WING NR 5 SPOILER OTBD ACTUATOR SUPPORT BRACKET BROKEN ATTACHMENT. REPAIRED FITTING IAW EA.

Part: ACTUATOR — BROKEN (RT SPOILER) · airframe 62,203 hrs · 51,401 cycles

RIGHT WING NR 5 SPOILER INBD ACTUATOR BOTTOM MOUNTING LUG BROKEN. R & R ACTUATOR IAW AMM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 61,770 hrs · 51,090 cycles

FORWARD ENTRY EMERGENCY EXIT LOWER LIGHT COVER FELL OFF. INSTALLED COVER PER MM.

Part: VALVE — FAULTY (CARGO BAY) · airframe 61,493 hrs · 50,897 cycles

DIVERSION -- FWD CARGO FIRE LIGHT & WARNING CAME ON IN CRUISE. BOTTLE DISCHARGE LIGHT STEADY FOR 6 - 7 MIN THEN FLASHING AGAIN. REMOVED AND REPLACED DIVERTER VALVE AND METERING VALVE PER MM.

Part: RIB — CRACKED (RT WING) · airframe 61,004 hrs · 50,555 cycles

CRACKED AT WBL 135.5 REAR SPAR RIB RADIUS. REPAIRED RIB ON EA.

Part: DOUBLER — CRACKED (NR 2 PYLON) · airframe 61,004 hrs · 50,555 cycles

RT WING LWR SURFACE T/E O/B NR 2 PYLON CRACKED DOUBLER. REMOVED AND REPLACED THE RT WING LOWER SURFACE T/E CLIP ASSY IAW SOPM 20-50-01.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 61,004 hrs · 50,555 cycles

CRACKED SUPPORT ANGLE ON LT WING NR 1 PYLON INBD AFT SIDE. REMOVED, FABRICATED, AND REPLACED SUPPORT ANGLE ON LT WING NR 1 PYLON I/B AFT SIDE IAW SRM 51-40-02-0G-0 AND BAC DRAWING

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,980 hrs · 50,536 cycles

AFT RIGHT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED AFT RIGHT EMERGENCY BATTERY PACK M1137 PER AMM.

Part: LATCH — BROKEN (EXTERNAL POWER) · airframe 60,922 hrs · 50,501 cycles

EXTERNAL POWER DOOR LOWER LATCH BROKEN. REPLACED EXTERNAL POWER DOOR LOWER LATCH IAW SRM 51-40-02-0G-0.

Part: STRIP — CORRODED (FUSELAGE) · airframe 60,922 hrs · 50,501 cycles

FWD CARGO COMPARTMENT CAP STRIP HAS CORROSION AT STA 500D. REMOVED CAPSTRIP ON FWD CARGO COMPARTMENT THAT HAS CORROSION AT STA 500D. INSTALLED NEW CAPSTRIP PART NO. 65C26449-9 AAR TAG NO A33528 IN ACCORDANCE WITH SRM 51-40-05-09-0.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 60,727 hrs · 50,363 cycles

AFT SERVICE DOOR ESCAPE SLIDE PRESSURE IS LOW. REMOVED AND REPLACED AFT SERVICE DOOR SLIDE ASSY PER MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,461 hrs · 50,176 cycles

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

Part: HOOK — LOOSE (L1 DOOR) · airframe 60,461 hrs · 50,176 cycles

L1 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR HOOK LOOSE ON FLOOR. SECURED HOOK PER MM.

Part: LENS — BROKEN (CABIN) · airframe 60,322 hrs · 50,074 cycles

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

Part: HYDRAULIC LINE — FAILED (NLG WW) · airframe 59,940 hrs · 49,781 cycles

LOSS OF ALL A-HYDRAULIC QUANTITY UPON LOWERING LANDING GEAR. FOUND NLG TRUNNION BEAM CRACKED. R&R NLG ACTUATOR LINE PER MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 59,590 hrs · 49,515 cycles

R1 DOOR CRACKED IN THE AFT FRAME. REMOVED AND REPLACED R1 DOOR IAW MM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 59,416 hrs · 49,383 cycles

GASPER FAN CAUSED ODOR. REMOVED AND REPLACED GASPER FAN PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 8. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND RT LOWER EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT ROW 10. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WINDOW FUSELAGE WINDOW SKIN CRACKED AT BS 887+10, UPPER AFT CORNER CUTOUT. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 500B+14 TO BS 500B+18, STR 1L. REPAIRED SKIN IAW ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 14R. REMOVED AND REPLACED CLIP IAW DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 2R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 420+10, UPPER FORWARD CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 420+10, LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500A+10, UPPER FWD CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 847+10, UPPER AFT CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 460+10, LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 520+10, UPPER FWD CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 867+10, LOWER FWD CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 480+10, UPPER FWD CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 520+10, LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 986.5, STR 2L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 312, BETWEEN STR 5L TO STR 3L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 520+10 AT UPPER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 867+10, UPPER AFT CORNER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 767+10, LOWER FORWARD CORNER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 767+10, UPPER AFT CORNER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 787+10, LOWER FORWARD CORNER. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 827+10, LOWER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 807+10, LOWER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 827+10, UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,399 hrs · 48,641 cycles

DURING SCHEDULED SPV CHECK FOUND, LT FUSELAGE WINDOW SKIN CRACKED AT BS 807+10, UPPER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,397 hrs · 48,640 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500C+8, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,397 hrs · 48,640 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 426, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,397 hrs · 48,640 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 877, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,397 hrs · 48,640 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 755, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,397 hrs · 48,640 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500B+12, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,397 hrs · 48,640 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 818, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,535 hrs · 48,023 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER AFT CORNER, BS 324. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 327, STR 17R. REPAIRED SKIN.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26R TO BL 0. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CORRODED AT BS 947, RBL 3. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27R TO STR 26R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 639, LBL 45.5. REPAIRED WEB IAW ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, LBL 2. REPAIRED SHEAR TIE PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND BEAR STRAP SKIN CUTOUT CRACKED AT BS 797.5, RBL 31. REPAIRD BEAR STRAP IAW ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO BAY FLOOR BEAM CORRODED BETWEEN BS 727D+2 TO BS 727D+6, RBL 13. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. READJUSTED SLIDE IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,118 hrs · 48,437 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP PER ER AND EA.

Part: MECHANISM — FAULTY (NR 1 ENGINE) · airframe 57,974 hrs · 48,325 cycles

NR 1 ENGINE OVERTEMP ON SMF: TEMP EXCEEDED 940F. OVERTEMP LASTED LESS THAN 5 SECS. ENGINE NR 1 OVERTEMPTED AGAIN PASSING 1000F. TEMP AT 935F, UNABLE TO MAINTAIN CLIMB N1. REMOVED AND REPLACED BLEED VALVE FUEL GEAR MOTOR, STOP MECHANISM, FEEDBACK ROD AND MAIN FLEX SHAFT IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,930 hrs · 48,289 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 817, STR 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,930 hrs · 48,289 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 777, STR 4R. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,402 hrs · 47,862 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 17. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,007 hrs · 47,578 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 727D+11, STR 4L. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,007 hrs · 47,578 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 500B+9, STR 2R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,007 hrs · 47,578 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 727D+13, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,006 hrs · 47,578 cycles

DURING SCHEDULED MV2 CHECK FOUND, SKIN CRACKED AT BS 500B+9, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,006 hrs · 47,578 cycles

DURING SCHEDULED MV2 CHECK FOUND, SKIN CRACKED AT BS 727D+11, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,006 hrs · 47,578 cycles

DURING SCHEDULED MV2 CHECK FOUND, SKIN CRACKED AT BS 727D+13, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 923, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 921, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,455 hrs · 47,167 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 921, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,455 hrs · 47,167 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 842, STR 1. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,455 hrs · 47,167 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,455 hrs · 47,167 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 510A, STR 6R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,455 hrs · 47,167 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 923, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,455 hrs · 47,167 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 852, STR 4R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,455 hrs · 47,167 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 461, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 923, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 842, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 921, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 510A, STR 6R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 852, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,451 hrs · 47,166 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 467, STR 1. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,215 hrs · 46,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 424, STR 15R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,215 hrs · 46,992 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 420, BETWEEN STR 16R TO STR 17R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,172 hrs · 46,960 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR HINGE CUTOUT FWD EDGE. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,214 hrs · 46,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,172 hrs · 46,960 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,169 hrs · 46,959 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,036 hrs · 46,093 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 13. RELAMPED LIGHT ASSY PER MM.

Part: WEB — CRACKED (NLG WW) · airframe 54,514 hrs · 45,690 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND NOSE WHEEL WELL RT WEB CRACKED AT FWD ACCESS PANEL CUTOUT, BS 247, WL 170. REPAIRED WEB PER EA.

Part: LENS — MISSING (CABIN) · airframe 54,317 hrs · 45,529 cycles

OVERHEAD EMERGENCY EXIT SIGN LENS MISSING AT MID CABIN. INSTALLED LENS PER EA.

Part: COVER — MISSING (CABIN) · airframe 53,667 hrs · 45,049 cycles

DURING SCHEDULED CV CHECK, FOUND L1 EMERGENCY EXIT DOOR LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,496 hrs · 44,920 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 775, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,496 hrs · 44,920 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 744A, STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,496 hrs · 44,920 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 776, STR 4L. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,496 hrs · 44,920 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 1. REMOVED AND REPLACED CLIP PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,496 hrs · 44,920 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 839, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,496 hrs · 44,920 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 741B, STR 4R. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,496 hrs · 44,920 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 1. REMOVED AND REPLACED CLIP PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,496 hrs · 44,920 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 737D, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,496 hrs · 44,920 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 733C, STR 4L. REPAIRED SKIN PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,495 hrs · 44,920 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT ROW 16. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,369 hrs · 44,829 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED BETWEEN BS 514B TO BS 518B, STR 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,776 hrs · 44,401 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 835, STR 2R. REPAIRED SKIN PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,650 hrs · 44,301 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 52,650 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUB FRAME CRACKED AT LOWER FWD CORNER OF L2 DOOR CUTOUT. REPAIRED FRAME PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,658 hrs · 44,308 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR AFT EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,650 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 19L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,650 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19L. REPAIRED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,650 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,650 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, BETWEEN STR 13L TO STR 14L. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 52,650 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 52,650 hrs · 44,301 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 52,641 hrs · 44,294 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 52,328 hrs · 44,061 cycles

RIGHT MID CABIN OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: COVER — BROKEN (CABIN) · airframe 51,691 hrs · 43,598 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 51,558 hrs · 43,503 cycles

DURING SCHEDULED OTS CHECK, FOUND LT MLG WHEEL WELL PRESSURE DECK SKIN CRACKED AT BS 664, LBL 32. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 51,556 hrs · 43,502 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT MLG WHEEL WELL PRESSURE DECK SKIN CRACKED AT BS 664, LBL 32. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 51,197 hrs · 43,232 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 51,107 hrs · 43,164 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT RADIO ALTIMETER SKIN CUTOUT, BS 410. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT RADIO ALTIMETER SKIN CUTOUT, BS 450. REPAIRED SKIN PER AAR EA.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 794, STR 25R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT RADIO ALTIMETER SKIN CUTOUT, BS 430. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT RADIO ALTIMETER SKIN CUTOUT, BS 390. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787 BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, RBL 6. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: STRIP — DELAMINATED (CABIN) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT EEPLS STRIP DELAMINATED. REMOVED AND REPLACED STRIP PER MM.

Part: LENS — MISSING (CABIN) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND OVERWING EMERGENCY EXIT LENS MISSING. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND EMERGENCY EXIT SIGN LENS MISSING AT BS 930. INSTALLED LENS PER MM.

Part: STRIP — DELAMINATED (CABIN) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT EEPLS STRIP DELAMINATED. REMOVED AND REPLACED STRIP PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT CRACKED AT LOWER CORNER OF LOWER STOP FITTING. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 500B TO BS 500C, WL 208. REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: STRIP — MISSING (CABIN) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS STRIP MISSING AT ROW 8. INSTALLED EEPLS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 4R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 4R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: RIB — CRACKED (HORIZ STAB) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT HORIZONTAL STABILIZER L/E OUTBOARD RIB UPPER AFT CORNER CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CORRODED AT BETWEEN BS 420 TO BS 440, STR 28R. REMOVED AND REPLACED SPLICE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 440 TO BS 460. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BETWEEN BS 867 TO BS 887. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 380 TO BS 400. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT CREASE BEAM CORRODED AT BS 291. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8L. REPAIRED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,899 hrs · 42,314 cycles

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

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 49,899 hrs · 42,314 cycles

DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED CABLE PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 49,594 hrs · 42,108 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REPAIRED SIGN PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,030 hrs · 41,693 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 47,976 hrs · 40,916 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: HINGE — WORN (RT ELEVATOR TAB) · airframe 47,976 hrs · 40,916 cycles

DURING SCHEDULED C2 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE ASSY PER SWA EA.

Part: HINGE — WORN (L ELEVATOR TAB) · airframe 47,976 hrs · 40,916 cycles

DURING SCHEDULED C2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE ASSY PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,660 hrs · 39,962 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (ROW 12 ABC) · airframe 46,652 hrs · 39,955 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 12 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 45,773 hrs · 39,275 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: BOLT — WORN (LT ELEVATOR TAB) · airframe 45,148 hrs · 38,783 cycles

DURING SCHEDULED C3 CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BOLT PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 448,883 hrs · 38,573 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 3 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,525 hrs · 38,288 cycles

DURING SCHEDULED MV1 CHECK, FOUND RIGHT FWD CABIN BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CONNECTOR — FAULTY (NR 2 ENGINE) · airframe 44,114 hrs · 37,973 cycles

INFLIGHT SHUTDOWN/AIRTURN BACK/DECLARED EMERGENCY. NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. REMAINED ON WITH THRUST LEVER CLOSED. ENGINE SHUTDOWN PER QRH. FOUND D404 CONNECTOR FAULTY. REMOVED AND REPLACED CONNECTOR PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,857 hrs · 37,778 cycles

DURING SCHEDULED A1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 1 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,713 hrs · 37,666 cycles

DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,554 hrs · 37,543 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT FWD BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 42,217 hrs · 36,501 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (NR 6 SLAT) · airframe 42,217 hrs · 36,501 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 6 SLAT PER MM.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 42,217 hrs · 36,501 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE LOWER SKIN DELAMINATED. REMOVED AND REPLACED NR 6 SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 42,217 hrs · 36,501 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 41,987 hrs · 36,330 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,357 hrs · 35,863 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOOR BEAM CORRODED AT BS 773, LBL 12. REPAIRED AFT CARGO COMPARTMENT FLOOR BEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,357 hrs · 35,863 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT BS 369, RBL 5. REPAIRED SKIN PER SWA EA.

Part: SKIN — DAMAGED (BS 745E) · airframe 40,714 hrs · 35,356 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CREASED AT BS 745E, BETWEEN STR 19L TO STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 40,191 hrs · 34,946 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 39,255 hrs · 34,203 cycles

DURING SCHEDULED RON CHECK, AFT GALLEY EMERGENCY EXIT LIGHTS BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LATCH — OUT OF ADJUST (ESCAPE SLIDE) · airframe 37,518 hrs · 32,767 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE, CABLE LATCH ASSY OUT OF ADJUST. ADJUSTED L1 DOOR EMERGENCY EVAC SLIDE LATCH ASSY PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 35,606 hrs · 31,279 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER AT ROW 11 ABC, MISSING. REPLACED EEPLS COVER PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 35,340 hrs · 31,042 cycles

FWD LT EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,838 hrs · 30,644 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 294, RBL 18 TO RBL 50, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,730 hrs · 30,545 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED L1 DOOR UPPER HINGE BOX FITTING PER EA.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 34,364 hrs · 20,258 cycles

EEPLS COVER AT FWD CABIN LOOSE. REINSTALLED EEPLS COVER PER MM.

Part: GATE — CRACKED (L1 DOOR) · airframe 33,626 hrs · 29,669 cycles

DURING OTS, FOUND UPPER GATE CRACKED ON L1 DOOR. REMOVED AND REPLACED L1 DOOR GATE PER MM.

Part: SPAR — CRACKED (WING)

CRACKED AT O/B AFT FLAP TRACK LOWER ATTACH HOLES.

Part: SPAR — CRACKED (RT WING TE FLAP)

CRACKED AT OB AFT FLAP TRACK ATTACH HOLES.

Part: SPAR — CRACKED (RT MIDFLAP)

CRACKED AT O/B AFT FLAP TRACK ATTACH HOLES.

Part: SPAR — CRACKED (LT MIDFLAP)

CRACKED AT O/B AFT FLAP TRACK LOWER ATTACH HOLES.

Part: SPAR — CRACKED (WBL)

SPAR CRACKED.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING AFT SPAR CLEVIS LUGS CORRODED. REPAIRED CLEVIS LUGS PER SRM AND BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 294, WL 208, RBL 53. REPAIRED FRAME PER ER.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB LOWER RIB CHORD CRACKED AT STA 120.3. REPAIRED RIB ASSY PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, WL 208, RBL 59. REPAIRED FLOORBEAM UPPER CHORD PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 380, LBL 20. REPAIRED FRAME PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND NR 2 AND NR 3 L/E SLATS DELAMINATED. REPAIRED NR 2 AND NR 3 L/E SLATS PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1006, WL 195 AT LBL 29-33 AND WL 196 AT RBL 30. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SPAR — CRACKED (LT WING TE FLAP)

CRACKED AT OB AFT FLAP TRACK LOWER ATTACH HOLES.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 460 AND BS 480. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 574, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 763, WL 148 AND LBL 3. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 500C + 8, LT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,148 hrs · 29,273 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED FRAME PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 32,166 hrs · 28,385 cycles

EMERGENCY FLASHLIGHT IN FWD CABIN NOT CHARGING. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 32,321 hrs · 28,592 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT (JUST LEFT OF F/A SEAT) BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,143 hrs · 27,667 cycles

FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: LENS — BROKEN (FWD ENTRY DOOR) · airframe 29,510 hrs · 26,348 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 28,562 hrs · 25,581 cycles

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

Part: ROD END — WORN (ELEVATOR TAB) · airframe 28,167 hrs · 25,273 cycles

DURING SCHEDULED RON, SWA SI 11111-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TAB OUTBOARD ROD END ASSY'S PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 27,133 hrs · 24,420 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 26,917 hrs · 24,254 cycles

EMERGENCY EXIT LIGHT BROKEN AT FWD F/A'S SEAT STATION. REMOVED AND REPLACED EXIT LIGHT PER MM.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 26,569 hrs · 23,978 cycles

FWD ENTRY DOOR EVACUATION SLIDE DEPLOYED INADVERTENTLY. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: MASK — LOOSE (COCKPIT) · airframe 25,878 hrs · 23,391 cycles

( AIR TURNBACK )……………………..LEAK IN CREW OXYGEN SYSTEM. FOUND O'RING LOOSE IN CAPT O2 MASK ASSY, REPOSITIONED O'RING PER MM

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,833 hrs · 23,350 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES CORRODED BETWEEN STR 26L & 26R AT BS 767, BS 787 & BS 807. REPAIRED SHEAR TIES PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 25,258 hrs · 22,843 cycles

EEPLS COVER LOOSE AT ROW 8. SECURED EEPLS COVER PER MM.

Part: LENS — MISSING (AFT DOORS) · airframe 25,218 hrs · 22,809 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY AND AFT SVC DOORS MISSING OVERHEAD EMERGENCY EXIT LIGHT LENSES. INSTALLED EXIT LIGHT LENSES PER MM.

Part: RECEPTACLE — DEFECTIVE (CABIN) · airframe 24,328 hrs · 22,057 cycles

EEPLS INOP BETWEEN ROWS 10 & 13. REMOVED AND REPLACED EEPLS RECEPTICAL PER MM.

Part: COVER — MISSING (CABIN) · airframe 24,309 hrs · 22,041 cycles

EEPLS TRACK COVER MISSING AT EXIT ROW. INSTALLED TRACK COVER PER MM.

Part: LENS — LOOSE (ENTRY DOOR) · airframe 24,293 hrs · 22,022 cycles

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

Part: ACTUATOR — FAILED (LT WING) · airframe 24,198 hrs · 21,943 cycles

AIR TURNBACK, 3 L/E FLAP FAILED TO RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NR 3 L/E FLAP ACTUATOR PER MM.

Part: SPAR — DAMAGED (LH HORZ STAB) · airframe 23,908 hrs · 21,690 cycles

DURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STAB REAR SPAR LOWER CHORD DAMAGED THROUGH AT SKIN ATTACH SECTION, STA 114 TO 116. REPAIRED PER RA 1-355-0389.

Part: COVER — MISSING (CABIN) · airframe 23,165 hrs · 21,029 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS WIRES EXPOSED BETWEEN ROWS 13 AND 14. REPLACED FLOOR TRACK COVER PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 23,084 hrs · 20,955 cycles

EEPLS WIRES BROKEN AND EXPOSED AT OVERWING EXIT AREA. REPAIRED EEPLS WIRING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,984 hrs · 20,872 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT ROWS 18 AND 12 - 14. RELAMPED AND RECONNECTED LOOSE PIN PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 22,896 hrs · 20,787 cycles

EEPLS TRACK LOOSE AT MID CABIN. SECURED EEPLS TRACK.

Part: LIGHT — MISSING (CABIN) · airframe 22,141 hrs · 20,146 cycles

EEPLS TRACK COVER MISSING AT MID CABIN. INSTALLED TRACK COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 22,078 hrs · 20,095 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LENS MISSING AT ROW 18. INSTALLED LENS PER MM.

Part: LENS — LOOSE (CABIN)

EMERGENCY EXIT LIGHT LENS FELL OUT AT FWD ENTRY DOOR. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (ROW 14)

EEPLS INOP AT ROW 14. REINSTALLED LIGHT ASSY. OPS CK GOOD.

Part: NR 3 BEARING — FAILED (NR 1 ENGINE)

ABORTED TAKEOFF, SMOKE IN CABIN AND COCKPIT. ABORTED TAKEOFF AT 120 KNOTS. NR 1 ENG, NR 3 BEARING AIR/OIL SEAL FAILURE. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED A2 CHECK, FOUND EEPLS LIGHT LENS MISSING AT MID CABIN. REPLACED LENS PER MM.

Part: SLIDE — DETACHED (PASSENGER DOOR)

FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE FELL OUT OF RETAINER. REPOSITIONED SLIDE ASSY PER MM.

Part: LENS — BROKEN (PAX DOORWAY)

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

Part: SLIDE — DETACHED (L1 DOOR)

FWD ENTRY DOOR SLIDE DROPPED OUT OF BASKET. REINSTALLED L1 SLIDE ASSY PER MM.

Part: WIRE — EXPOSED (ROW 12)

EGRRESS WIRING EXPOSED AT ROW 12. REPLACED FLOOR TRACK LIGHT PER MM.

Part: LIGHT — LOOSE (ROW 9, 13 & 24)

DURING SCHEDULED C1 CHECK, FOUND FLOOR EMERGENCY TRACK LIGHT NOT SECURED AT ROWS 13, 9 AND 24. SECURED LIGHTS PER MM.

Part: SKIN — CRACKED (LT LE FLAP)

DURING SCHEDULED C1 CHECK, FOUND LT WING LEADING EDGE NR 2 SLAT LOWER SKIN AT TRAILING EDGE HAS SMALL CRACKS AT RIVET HOLES. REPAIRED SLAT PER SWA RA NR 1-357-0660.

Part: WIRE — CHAFED (CABIN)

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY LIGHTING WIRES CHAFED WHERE IT COMES THROUGH FLOOR. REPLACED BROKEN AND CHAFED WIRING AT FLOOR PANEL PER BOEING STANDARD WIRING PRACTICES.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND FWD STUB FRAME CRACKED AT FWD SERVICE DOOR UPPER STRAP. REMOVED AND REPLACED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND AFT CABIN FLOORBEAM BS 986 CORRODED AROUND FASTENER HOLE LBL9. REPAIRED PER SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 986, AT LBL 4.5. REPAIRED PER BOEING SRM.

Part: WIRE — DISCONNECTED (CABIN)

DURING SCHEDULED SC CHECK, FOUND CABIN FLOOR TRACK LIGHTS INOP AT EMERGENCY EXIT ROW. REPAIRED WIRES AND OP CHECKED PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOP ROW 20. RELAMPED OPS GOOD PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EGRESS LIGHTS INOP AT EMERGENCY EXIT ROW. RECONNECTED WIRING SPLICE PER BOEING MM.

Part: SKIN — DAMAGED (FUSELAGE)

AFTER TAKEOFF, CREW NOTED FWD SERVICE DOOR YELLOW SAFETY STRAP HANGING OUTSIDE AIRCRAFT AND STRIKING SIDE. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED AREA, CLEANED UP AREA WHERE PAINT WAS REMOVED AND APPLIED PRIMER TO AFFECTED AREA, NO OTHER DAMAGE NOTED.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT AFT SERVICE EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PER BOEING M/M.

Part: PC CARD — INOP (NLG)

IN FLIGHT, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CYCLING GEAR, NO HELP. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFULL LANDING. TROUBLESHOT AND FOUND M983 PC CARD FAULT. REPLACED AND OPERATIONAL CHECKED PER BOEING M/M.