N387SW

Part: STRAP — BROKEN (FLASHLIGHT ASSY) · airframe 71,174 hrs · 57,283 cycles

RIGHT FORWARD EMERGENCY FLASHLIGHT SAFETY STRAP BROKEN. R&R THE STRAP IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 71,174 hrs · 57,283 cycles

LEFT FORWARD EMERGENCY FLASHLIGHT SAFETY STRAP BROKEN. R & R THE STRAP IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 71,174 hrs · 57,283 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,159 hrs · 57,275 cycles

LT AFT ENTRY DOOR CEILING EMERGENCY LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: SIGN — MISSING (CABIN) · airframe 70,631 hrs · 56,938 cycles

L1 DOOR EMERGENCY EXIT SIGN MISSING. R & R SIGN IAW MM.

Part: SPOILER — BROKEN (RT WING) · airframe 70,269 hrs · 56,713 cycles

RT WING NR 5 GROUND SPOILER INBOARD LUG BROKEN. R&R NR 5 GROUND SPOILER PER AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 69,978 hrs · 56,525 cycles

RIGHT WING RT 4 LE SLAT DELAMINATED INBD EDGE. R & R SLAT IAW AMM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,552 hrs · 56,231 cycles

CENTER TANK STIFFENER CRACKED AT BS 546, LBL 58. R & R STIFFENER IAW SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 69,552 hrs · 56,231 cycles

L1 DOOR BEAR STRAP SKIN CUT OUT CRACKED AT BS 303.9, STRINGER 13L. REPAIRED CUT OUT IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,552 hrs · 56,231 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 4L. REMOVED SPLICE IAW ER & EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 69,552 hrs · 56,231 cycles

STRINGER SPLICE CRACKED AT STATION 360, STRINGER 15L. R & R STRINGER SPLICE IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 69,552 hrs · 56,231 cycles

R1 DOOR MOP SILL CORRODED. R & R MOP SILL IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 69,552 hrs · 56,231 cycles

RIGHT WING OTBD VERTICAL ATTACH ANGLE, CRACKED AT 2ND OTBD AILERON SWEEPER WEB. R & R ANGLE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,552 hrs · 56,231 cycles

STRINGER CLIP CRACKED AT STATION 490, STRINGER 24R. R & R CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,552 hrs · 56,231 cycles

LONGITUDINAL FLOORBEAM SUPPORT BRACKET ANGLE CRACKED AT BS 727B, BBL 0. REPAIRED ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,552 hrs · 56,231 cycles

FUSELAGE FRAME CRACKED AT STATION 328, STRINGER 20R - 21R. REPAIRED FRAME IAW ACO.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,748 hrs · 55,707 cycles

L1 DOOR EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 67,149 hrs · 54,542 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT COVER LOOSE. R & R LIGHT COVER IAW SIP.

Part: SKIN — CRACKED (L1 DOOR) · airframe 66,059 hrs · 53,819 cycles

L1 DOOR INNER SKIN CRACKED BELOW THE TORQUE BOX. REPAIRED SKIN IAW EA.

Part: SLAT — DELAMINATED (LT WING) · airframe 66,059 hrs · 53,819 cycles

LEFT WING NR 2 SLAT DELAMINATED INBD & OTBD TE. R & R NR 2 SLAT IAW MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 65,374 hrs · 53,350 cycles

R2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 64,966 hrs · 53,050 cycles

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

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 64,461 hrs · 52,682 cycles

R1 DOOR CRACKED LOWER EDGE FRAME AT AFT LOWER CORNER STOP FITTING. R & R DOOR IAW AMM.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 64,396 hrs · 52,634 cycles

FORWARD FLASHLIGHT BROKEN. R & R FLASHLIGHT IAW CMM.

Part: PLATE — DAMAGED (R1 DOOR) · airframe 64,396 hrs · 52,634 cycles

R1 DOOR EMER EVAC SLIDE FLOOR BRACKETS ADAPTER PLATE DAMAGED. R & R PLATE IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 64,396 hrs · 52,634 cycles

LEFT EEPLS BROKEN BETWEEN BS 342 TO BS 380. R & R EEPLS IAW DWG.

Part: PLATE — DAMAGED (R2 DOOR) · airframe 64,396 hrs · 52,634 cycles

R2 DOOR EMERGENCY EVAC SLIDE FLOOR BRACKETS ADAPTER PLATE DAMAGED. R & R PLATE IAW AMM.

Part: FITTING — CORRODED (LT MLG WW) · airframe 64,396 hrs · 52,634 cycles

LEFT WW BULKHEAD FITTING CORRODED AT BS 663, WL 71.24. REPAIRED FITTING IAW EO & EA.

Part: FITTING — CORRODED (LT MLG WW) · airframe 64,396 hrs · 52,634 cycles

SPLICE FITTING CORRODED AT BS 663, LT WING WL 71.24. R & R FITTING IAW EA & DWG.

Part: ANGLE — CRACKED (FLAP TRACK) · airframe 64,396 hrs · 52,634 cycles

LEFT WING NR 3 FLAP TRACK FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (TE FLAP) · airframe 64,396 hrs · 52,634 cycles

LEFT WING NR 3 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CORRODED (RT WING) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING SPLICE FITTING CORRODED AT BS 663, BETWEEN WBL 71.24 TO WL 194. R & R FITTING IAW EO & EA.

Part: FITTING — CORRODED (RT MLG WW) · airframe 64,396 hrs · 52,634 cycles

RIGHT WW BULKHEAD FITTING CORRODED AT BS 663, BETWEEN WBL 71.24 TO WL 194. REPAIRED FITTING IAW EO & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

AFT CARGO COMPARTMENT WEB CORRODED BETWEEN BS 947.5 TO BS 967, BETWEEN STRINGER 25R TO STRINGER 26R. R & R WEB IAW SRM & DWG.

Part: STIFFENER — CRACKED (FLAP TRACK) · airframe 64,396 hrs · 52,634 cycles

LEFT WING NR 3 FLAP TRACK FAIRING STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

FRAME LOWER FLANGE CORRODED AT BS 747, BETWEEN STRINGER 25R TO STRINGER 26R. REPAIRED FRAME IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

CHANNEL STIFFENER CRACKED AT BS 1016+1, RBL 1. REPAIRED STIFFENER IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED BETWEEN RSS 224.14 TO 215.97. REPAIRED CHORD IAW EO & EA NO.

Part: SKIN SPLICE — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING TO BODY FAIRING SUPPORT LOWER STRUCTURE SKIN SPLICE CRACKED AT BS 680 WW AREA. R & R SPLICE IAW SRM & DWG.

Part: SPAR — CRACKED (LT WING) · airframe 64,396 hrs · 52,634 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED BETWEEN RSS 224.14 TO 215.97. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,396 hrs · 52,634 cycles

LEFT WING INBD FIXED LE SKIN CRACKED AT 208. REPAIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING TO BODY FAIRING LOWER SUPPORT STRUCTURE ANGLE CRACKED AT BS 680, WW AREA. R & R ANGLE IAW SRM & DWG.

Part: DOUBLER — CRACKED (FLAP TRACK) · airframe 64,396 hrs · 52,634 cycles

LEFT WING NR 3 FLAP TRACK FAIRING DOUBLER CRACKED. R & R DOUBLER IAW SRM & DWG.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING STIFFENER CRACKED. R & R STIFFENER IAW SRM.

Part: BEARING — WORN (TE FLAP) · airframe 64,396 hrs · 52,634 cycles

LEFT WING NR 2 SPINDLE CARRIAGE WORN OF THE INNER RACE. R & R BEARING ASSEMBLY IAW CMM.

Part: BEARING — WORN (TE FLAP) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING NR 8 SPINDLE CARRIAGE INBD WORN OF THE INNER RACE. R & R BEARING ASSEMBLY IAW CMM.

Part: BEARING — WORN (TE FLAP) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING NR 7 SPINDLE CARRIAGE INBD WORN OF THE INNER RACE. R & R BEARING ASSEMBLY IAW CMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

AFT CARGO COMPARTMENT DOME WEB CRACKED AT BS 1016, RBL 5. REPAIRED WEB IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

SHEAR TIE CRACKED AT BS 344, BETWEEN STRINGER 27R TO STRINGER 26R. R & R SHEAR TIE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING SUPPORT ANGLE INTERNAL AREA OF RSS 507 CRACKED. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

AFT PRESS BULKHEAD DOME CAP WEB CRACKED AT BS 1016, STRINGER 18R. REPAIRED WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING SUPPORT ANGLE INTERNAL AREA CRACKED AT RSS 533. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

SUPPORT ANGLE CRACKED AT BS 336, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

SUPPORT BRACKET CRACKED AT BS 294.5, STRINGER 23L. R & R BRACKET IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,395 hrs · 52,634 cycles

SKIN CRACKED AT BS 727D, BETWEEN STRINGER 27L TO 27R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

FRAME INNER CHORD CRACKED AT BS 348.2, STRINGER 17L. R & R CHORD IAW SRM & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

FRAME CORRODED AT BS 867, BETWEEN STRINGER 27L TO 27R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 25R. R & R TIE CLIP IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 727E, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 727B, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 19L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — BROKEN (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP BROKEN AT BS 787, STRINGER 23R. R & R TIE CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

FRAME ANGLE CORRODED AT BS 747, BETWEEN STRINGER 26R TO STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 727C, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 727D, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: RIB — CRACKED (RT WING) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING FUEL TANK WBL 114.00 RIB UPPER CHORD CRACKED NEXT TO STRINGER 2. REPAIRED CHORD IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 947.5, BETWEEN STRINGER 24R TO STRINGER 25R. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 747, STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.

Part: PLATE — CRACKED (L1 DOOR) · airframe 64,396 hrs · 52,634 cycles

L1 DOOR LOWER SEAL SWEEPER RETAINER PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

INTERNAL ANGLE CLIP CRACKED BETWEEN BS 348.2 TO BS 351.2, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 747, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 747, STRINGER 20L. R & R TIE CLIP IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

CLIP CORRODED AT BS 847, AT STRINGER 26R. R & R CLIP IAW SRM & DWG.

Part: RIB — CRACKED (RT WING) · airframe 64,395 hrs · 52,634 cycles

RIGHT WING FUEL TANK RIB LOWER CHORD CRACKED AT WBL 135.5 IN THE RADIUS AREA BETWEEN STRINGER 2 & 3. REPAIR CHORD IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 500A, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

AFT FRAME OF FWD CARGO DOOR CUT OUT CRACKED AT BS 492, STRINGER 24R. R & R FRAME IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 64,396 hrs · 52,634 cycles

RIGHT WING EXTERNAL SKIN CRACKED AT STATION 208, INBD SIDE. REPAIRED SKIN IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, LBL 45.6. R & R STRAP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 927 TO BS 947.5, BL 0. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

TIE CLIP CRACKED AT BS 460, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 64,395 hrs · 52,634 cycles

WEB CORRODED AT BS 1016, LBL 2. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

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

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, RBL 31.6. R & R STRAP IAW SRM.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 64,395 hrs · 52,634 cycles

SUPPORT CHANNEL CORRODED BETWEEN BS 727C TO 727D BETWEEN STRINGER 27R TO 27L. REPAIRED CHANNEL IAW SI.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,395 hrs · 52,634 cycles

FRAME CORRODED AT BS 847, BETWEEN STRINGER 27R TO 27L. REPAIRED FRAME IAW EA.

Part: ACCESS PANEL — CRACKED (VERTICAL STAB) · airframe 64,396 hrs · 52,634 cycles

VERTICAL STABILIZER ACCESS PANEL 9536 CRACKED. REPAIRED PANEL IAW SRM.

Part: ACCESS PANEL — CRACKED (RT NACELLE) · airframe 64,395 hrs · 52,634 cycles

NUMBER 2 PYLON RT NACELLE STRUT ACCESS PANEL 5864R CRACKED. REPAIRED PANEL IAW EA.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 64,395 hrs · 52,634 cycles

LEFT WING ACCESS PANEL 5764L CRACKED. REPAIRED PANEL IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

CENTER WING BOX SEAT TRACK CRACKED AT BS 727B, BETWEEN LBL 23.8 TO LBL 25.8. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (R1 DOOR) · airframe 64,395 hrs · 52,634 cycles

R1 DOOR SKIN CRACKED AT BS 328, STRINGER 8R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

L2 DOOR LOWER CORNER FUSELAGE SKIN CRACKED AT BS 947.5+12, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

ANTENNA BASE CRACKED AT PRESS BULKHEAD FWD FACE BS 178. R & R BASE IAW SRM & DWG.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 64,395 hrs · 52,634 cycles

CRACK ON CROSSBEAM E WEB FWD END & AFT EDGE OF THE AFT CARGO DOOR. REPAIRED T CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

FUSELAGE FRAME CRACKED AT BS 500B, STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 64,396 hrs · 52,634 cycles

MAIN WW PRESS DECK CRACKED AT BS 665, LBL 24.5+7. REPAIRED DECK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,395 hrs · 52,634 cycles

RIGHT FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A, AT FWD LOWER FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 64,396 hrs · 52,634 cycles

RIGHT SIDE NLG WW CRACKED AROUND FASTENER HOLE AT BS 243.7+ 3.5, WL 169.1. REPAIRED WW IAW SRM.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 64,396 hrs · 52,634 cycles

RIGHT SIDE NLG WW AROUND FASTENER HOLE CRACKED AT BS 243.7+3.5, WL 169.1. REPAIRED WW IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,395 hrs · 52,634 cycles

L2 DOOR SKIN CUT OUT FWD LOWER CORNER CRACKED AT BS 947.5+12, STRINGER 17L. REPAIRED SKIN IAW SRM & EA.

Part: LIGHT — LOOSE (EXTERIOR) · airframe 64,396 hrs · 52,634 cycles

EXTERNAL EMERGENCY EXIT LIGHTS LOOSE BETWEEN BS 727D TO BS 727E, BETWEEN STRINGER 22R TO STRINGER 23R. SECURE LIGHT IAW MM.

Part: WEB — CRACKED (NLG WW) · airframe 64,395 hrs · 52,634 cycles

LEFT NLG WW WEB CRACKED AT BS 259.5, BETWEEN WL 180 TO WL 182. REPAIRED WEB IAW SRM.

Part: LIGHT — LOOSE (EXTERIOR) · airframe 64,396 hrs · 52,634 cycles

EXTERNAL EMERGENCY EXIT LIGHTS LOOSE BETWEEN BS 727D TO BS 727E, BETWEEN STRINGER 22L TO STRINGER 23L. SECURE LIGHT IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,395 hrs · 52,634 cycles

LEFT FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A, AT FWD LOWER FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 64,396 hrs · 52,634 cycles

R1 DOOR AFT EDGE FRAME CRACKED. REPAIRED FRAME IAW SRM.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 64,396 hrs · 52,634 cycles

RIGHT SIDE NLG WW AROUND FASTENER HOLE CRACKED AT BS 243.7+ 3.5, WL 169.1. REPAIRED WW IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

UPPER CHORD CRACKED AT BS 663+2, LBL 24.5. REPAIRED CHORD IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 64,396 hrs · 52,634 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 24.8. REPAIRED CHORD IAW EA.

Part: HINGE FITTING — BROKEN (LT SPOILER) · airframe 64,215 hrs · 52,513 cycles

LEFT WING NR 4 GND SPOILER CTR OTBD HINGE FITTING BROKEN. R & R SPOILER IAW AMM.

Part: CASTING — BROKEN (LT SPOILER) · airframe 64,215 hrs · 52,513 cycles

LEFT WING NR 4 GND SPOILER INBD ACTUATOR CASTING BROKEN. R & R SPOILER IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,612 hrs · 52,117 cycles

RT WING INBD AFT FLAP TE UPPER SURFACE DELAMINATED. R & R AFT FLAP IAW MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,340 hrs · 51,192 cycles

FORWARD ENTRY UPPER HINGE CUT-OUT ON DOOR FRAME BRACKET CRACKED IN FORWARD OTBD AREA OF HINGE SHELF AREA, OTBD OF HINGE TRACK PLATE. R&R FITTING IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,340 hrs · 51,192 cycles

FORWARD ENTRY DOOR FRAME UPPER HINGE CUT OUT CRACKED AT HINGE CUT OUT RADIUS OF EXISTING REPAIR & EXTENDING FORWARD BETWEEN THE RIVET ROWS. REPAIR SKIN IAW SRM.

Part: FRAME — CRACKED (TE FLAP) · airframe 61,418 hrs · 50,523 cycles

LEFT WING NR 2 FLAP TRACK FAIRING "A" FRAME CRACKED. REMOVED & REPLACED "A" FRAME PER CMM.

Part: SKIN — CRACKED (TE FLAP) · airframe 61,418 hrs · 50,523 cycles

LEFT WING I/B FORE FLAP UPPER SURFACE CRACKED. REPAIRED FORE FLAP IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 61,418 hrs · 50,523 cycles

FWD ENTRY DOOR EMERGENCY LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 61,173 hrs · 50,356 cycles

AFT CABIN CEILING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS ASSY IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 60,553 hrs · 49,917 cycles

FWD ENTRY EMERGENCY EXIT LWR LIGHT ASSY DAMAGED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — CRACKED (CABIN) · airframe 59,921 hrs · 49,448 cycles

L1 DOOR EMERGENCY LIGHT SIGN CRACKED. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: NUT PLATE — CRACKED (RT WING) · airframe 60,291 hrs · 49,727 cycles

RIGHT WING UPPER SURFACE, AFT PYLON AREA, PANEL 58710R PLASTIC NUT PLATE STRIP CRACKED. REPAIRED NUT PLATE STRIP PER EA 1-354-1480.

Part: PANEL — CRACKED (RT WING) · airframe 60,291 hrs · 49,727 cycles

RIGHT WING UPPER SURFACE, AFT PYLON AREA, PANEL 58710R PLASTIC NUT PLATE STRIP CRACKED. REMOVED AND REPLACED RIGHT WING UPPER SURFACE PANEL 58710R NUT STRIP AS PER SRM. SEE SAM 326 FOR INDIVIDUALS STEP AND FUEL TANK ENTRY SAM 1045 AND PERFORMANCE WO# 13027 FOR REPAIR.

Part: FLAP — DELAMINATED (LT WING) · airframe 59,402 hrs · 49,035 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 59,248 hrs · 48,913 cycles

RIGHT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 8. SECURED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 59,186 hrs · 48,867 cycles

LEFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 6. INSTALLED LENS PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 58,372 hrs · 48,229 cycles

BS 663 BULKHEAD STIFFERNER CRACKED AT LBL 7, WL 163. REPAIRED STIFFENER PER EA.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 58,372 hrs · 48,229 cycles

BS 663, RBL 7, WL 164 CENTER TANK REAR SPAR VERTICAL STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER PER EA & EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,372 hrs · 48,229 cycles

SKIN CRACKED AT BS 665, STR 4L. REPAIRED SKIN PER SI & AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,372 hrs · 48,229 cycles

SKIN CRACKED AT BS 665, STR 4R. REPAIRED SKIN PER SI & AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,372 hrs · 48,229 cycles

SKIN CRACKED AT BS 662, STR 4R. REPAIRED SKIN PER SI & AMM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,372 hrs · 48,229 cycles

SHEAR TIE CORRODED AT BS 500, LBL 12, WL 157. REPAIRED SHEAR TIE IAW SRM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 58,372 hrs · 48,229 cycles

BS 663.75, RBL 6.15, WL 169 CENTER TANK REAR SPAR VERTICAL STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER PER ACO.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 58,372 hrs · 48,229 cycles

RT WING O/B AFT FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (TE FLAP) · airframe 58,372 hrs · 48,229 cycles

LEFT WING I/B AFT FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 58,372 hrs · 48,229 cycles

LEFT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 58,372 hrs · 48,229 cycles

RT WING I/B MIDFLAP UPPER SURFACE T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 58,372 hrs · 48,229 cycles

LT WING I/B MID FLAP UPPER SURFACE T/E WEDGE IS DELAMINATED. REPAIRED MID FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 58,372 hrs · 48,229 cycles

RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S8R) · airframe 58,150 hrs · 48,058 cycles

STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STRINGER CLIP IAW SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (BS 500B) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 500B+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 500A+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.

Part: SKIN — CRACKED (BS 867) · airframe 58,150 hrs · 48,058 cycles

RT BS 867+10 UPPER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (BS 420) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 420+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 500C+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (480) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 480+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.

Part: SKIN — CRACKED (BS 460) · airframe 58,150 hrs · 48,058 cycles

LEFT BS 460+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (BS 827) · airframe 58,150 hrs · 48,058 cycles

LEFT BS 827+10 UPPER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 360+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW REO & EA.

Part: STRINGER — CRACKED (BS 500A S9R) · airframe 58,150 hrs · 48,058 cycles

STRINGER CRACKED AT BS 500A+17, STR S9R. REMOVED & REPLACED STRINGER SEGMENT IAW SRM.

Part: SKIN — CRACKED (BS 480) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 480+10 LOWER AFT WINDOW SKIN CRACKED. REPAIRED SKIN IAW SB AND EA.

Part: SKIN — CRACKED (BS 500) · airframe 58,150 hrs · 48,058 cycles

LEFT BS 500+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.

Part: SKIN — CRACKED (BS 500C) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 500C+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 360+10 LOWER AFT WINDOW SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

LEFT BS 520+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA & REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

LT BS 887+10 UPPER AFT WINDOW SKIN CORNER CRACKED. REPAIR SKIN PER EA.

Part: SKIN — CRACKED (BS 380) · airframe 58,150 hrs · 48,058 cycles

RT BS 380+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (BS 807) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 807+10 UPPER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (BS 420) · airframe 58,150 hrs · 48,058 cycles

LEFT BS 420+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (BS 400) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 400+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.

Part: SKIN — CRACKED (BS 380) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 380+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (BS 400) · airframe 58,150 hrs · 48,058 cycles

RT BS 400+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 500+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

RT BS 847+10 UPPER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

LEFT BS 500B+10 UPPER FORWARD WINDOW SKIN CORNER AT CRACKED. REPAIRED SKIN IAW SB AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

LEFT BS 360+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW REO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 460+10 LOWER AFT WINDOW SKIN CRACKED. RIGHT SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 520+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN PER EA & REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

LEFT BS 500C+10 UPPER FORWARD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB AND EA.

Part: SKIN — CRACKED (BS 500) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 500+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (BS 380) · airframe 58,150 hrs · 48,058 cycles

LEFT BS 380+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 460+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (BS 500B) · airframe 58,150 hrs · 48,058 cycles

RIGHT BS 500B+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,150 hrs · 48,058 cycles

MAIN CABIN STA 360 AT STRINGER S5L STRINGER CLIP FOUND TO BE CRACKED. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: LENS — CRACKED (CABIN) · airframe 57,852 hrs · 47,843 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENSE CRACKED. REMOVED AND REPLACED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,829 hrs · 47,820 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 57,530 hrs · 47,607 cycles

DURING SCHEDULED CV CHECK FOUND, EEPLS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 57,480 hrs · 47,562 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EEPLS LOOSE AT ROW 6. SECURED EEPLS PER MM.

Part: LIGHT — DIRTY (CABIN) · airframe 57,480 hrs · 47,562 cycles

DURING SCHEDULED SPV CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS DIRTY. CLEANED EEPLS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 56,991 hrs · 47,190 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,839 hrs · 47,071 cycles

DURING SCHEDULED RON CHECK, FOUND CHEM MILL SKIN CRACKED AT BS 727C+5, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,839 hrs · 47,071 cycles

DURING SCHEDULED RON CHECK, FOUND CHEM MILL SKIN CRACKED AT BS 727C+10, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WINDOW SKIN CRACKED AT BS 500C+10, LOWER AFT CORNER. REPAIRED SKIN IAW TC.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 56,609 hrs · 46,894 cycles

DURING SCHEDULED OTS CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,609 hrs · 46,894 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,609 hrs · 46,894 cycles

DURING SCHEDULED OTS CHECK, FOUND R2 DOOR UPPER FWD CORNER STUB FRAME CRACKED. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 56,606 hrs · 46,893 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT STA 125. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 56,606 hrs · 46,893 cycles

DURING SCHEDULE HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,606 hrs · 46,893 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: ATTACH BRACKET — LOOSE (R2 DOOR) · airframe 56,606 hrs · 46,893 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE UPPER AFT ATTACH BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,901 hrs · 46,349 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 827+10, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,901 hrs · 46,349 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 807+10, STR 4R. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (EXIT SIGN) · airframe 55,752 hrs · 46,233 cycles

L2 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED LENS PER MM.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 54,680 hrs · 45,404 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,140 hrs · 44,995 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,433 hrs · 44,453 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT EEPLS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FITTING — BROKEN (LT WING) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING LOWER T/E SUPPORT ROD AT NR 4 SPOILER I/B ACTUATOR SUPPORT FITTING BROKEN. REMOVED AND REPLACED FITTING PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP BETWEEN ROW 15 TO ROW 16. REPAIRED WIRE PER WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 727E, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT LOWER SKIN CRACKED AT O/B END. REPAIRED NR 1 SLAT PER MM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 FLAP TRACK CORRODED AT MOUNT PAD. REMOVED AND REPLACED FLAP TRACK PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 420 TO BS 440, RBL 67. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, RBL 2. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 0 TO RBL 46. REMOVED AND REPLACED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER BAC DWG AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER FITTING CRACKED AT BS 332, STR 8R. REMOVED AND REPLACED FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 460 TO BS 480, RBL 67. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 460 TO BS 480, LBL 67. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420, RBL 67. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB FRAME ANGLE CRACKED AT BS 639, LBL 45. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB FRAME ANGLE CRACKED AT BS 639, RBL 45. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME ANGLE CRACKED AT R1 DOOR LOWER FWD CORNER CUTOUT. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO BAY FRAME CORRODED AT BS 727E, BETWEEN STR 23L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO BAY FRAME CORRODED AT BS 727E, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED FRAME PER SRM.

Part: PAD — CORRODED (GIRT BAR MOUNT) · airframe 53,121 hrs · 44,219 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM CORRODED BETWEEN BS 400 TO BS 420, LBL 67. REPAIRED BEAM PER SRM.

Part: PAD — CORRODED (GIRT BAR) · airframe 53,121 hrs · 44,219 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, LBL 65. REPAIRED FRAME PER SRM.

Part: PLATE — CORRODED (R2 DOOR) · airframe 53,121 hrs · 44,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT LOWER LATCH PLATE CORRODED. REMOVED AND REPLACED PLATE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,121 hrs · 44,219 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,926 hrs · 44,078 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 738B, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,926 hrs · 44,078 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 738E, STR 4R. REPAIRED SKIN PER EA.

Part: COVER — LOOSE (CABIN) · airframe 52,397 hrs · 43,685 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: TAB — DELAMINATED (RT AILERON) · airframe 52,108 hrs · 43,480 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING AILERON BALANCE TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: WEDGE — DELAMINATED (NR 5 SLAT) · airframe 52,108 hrs · 43,480 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,107 hrs · 43,480 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 500D, STR 8R. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (EXIT SIGN) · airframe 51,596 hrs · 43,088 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 51,170 hrs · 42,777 cycles

RIGHT EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 19. SECURED LENS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,106 hrs · 42,728 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,883 hrs · 42,569 cycles

DECLARED EMERGENCY/DIVERSIONS. PRESSURIZATION EVENT AT 33K FT. MASKED DROPPED, EMERGENCY DESCENT. DIVERTED TO CRW. FOUND FUSELAGE SKIN CRACKED BETWEEN BS 827 TO BS 847, STR 2L. REPAIRED SKIN PER SWA EA.

Part: STRIP — FADED (CABIN) · airframe 50,651 hrs · 42,389 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP FADED AT ROW 23. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 50,097 hrs · 41,984 cycles

LT OVERWING EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 49,261 hrs · 41,362 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR AFT GIRT BAR HOLDER CORRODED. REMOVED AND REPLACED BRACKET PER MM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 49,261 hrs · 41,362 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR AFT GIRT BAR HOLDER CORRODED. REMOVED AND REPLACED BRACKET PER MM.

Part: SKIN — CRACKED (BS 303) · airframe 49,261 hrs · 41,362 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CHORD ANGLE CRACKED AT BS 303, LBL 60, WL 218. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER WEB CRACKED AT BS 291, STR 14R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS. 727B, RBL 44. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 25. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

DURING SCHEDULED 14Y CHECK, FOUND NOSE WHEEL WELL CEILING PANEL SKIN CRACKED AT SNUBBER ATTACH PLATE, LBL 7.75. REPAIRED SKIN PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: FRAME — CRACKED (BS 380 S8L) · airframe 49,261 hrs · 41,362 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,261 hrs · 41,362 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 48,171 hrs · 40,560 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 47,615 hrs · 40,188 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 47,615 hrs · 40,188 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,765 hrs · 38,848 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1001, STR 5R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 45,765 hrs · 38,848 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,754 hrs · 38,841 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1006, STR 5R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 45,754 hrs · 38,841 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,046 hrs · 37,531 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 42,535 hrs · 36,338 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: STRINGER — CRACKED (BS 492 S26R) · airframe 42,244 hrs · 36,108 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CRACKED AT BS 492. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: LIGHT — BROKEN (L1 DOOR) · airframe 41,923 hrs · 35,862 cycles

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT ASSY BROKEN AT L1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,734 hrs · 35,711 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,602 hrs · 35,595 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FITTING — CRACKED (RT SPOILERS) · airframe 39,999 hrs · 34,379 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING NR 5 SPOILER OUTBD ACTUATOR HINGE CASTING CRACKED. REMOVED AND REPLACED SPOILER ASSY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 39,999 hrs · 34,379 cycles

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

Part: FITTING — CRACKED (NR 4 SPOILERS) · airframe 39,999 hrs · 34,379 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING NR 4 SPOILER OUTBD ACTUATOR HINGE CASTING CRACKED. REMOVED AND REPLACED SPOILER ASSY PER MM.

Part: BLOWER — FAULTY (E & E BAY) · airframe 39,402 hrs · 33,931 cycles

DIVERSION, ELECTRICAL SMELL IN CABIN. FOUND NORMAL EQUIPMENT COOLING BLOWER INOP. REMOVED AND REPLACED BLOWER PER MM.

Part: SIGN — LOOSE (LT OVERWING) · airframe 38,353 hrs · 33,098 cycles

LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 38,220 hrs · 32,981 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 37,775 hrs · 32,629 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVACUATION SLIDE LATCH CABLE MISROUTED. REROUTED CABLE PER MM.

Part: LINE — LEAKING (B-HYD SYS) · airframe 37,319 hrs · 32,246 cycles

AIR TURNBACK. LOST B-SYSTEM HYDRAULIC FLUID. REMOVED AND REPLACED HYDRAULIC LINE FROM B-SYSTEM MODULE TO B-SYSTEM HYDRAULIC ACCOUSTIC FILTER PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,461 hrs · 29,986 cycles

AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: LENS — BROKEN (EMERGENCY EXIT) · airframe 34,426 hrs · 29,955 cycles

DURING SCHEDULED RON, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 34,417 hrs · 29,948 cycles

CABIN OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,374 hrs · 29,913 cycles

DURING SCHEDULED C3 CHECK, FOUND BEAR STRAP AT BS 294.5, STRINGER 10L, CRACKED. REPAIRED BEAR STRAP PER EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,374 hrs · 29,913 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 500B, STRINGER 11R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CLEVIS — CORRODED (HORIZONTAL STAB) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION CLEVIS, CORRODED. REPAIRED HORIZONTAL STAB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM ZEE CHORD AT BS 270, RBL 10, CORRODED. REMOVED AND REPLACED CREASE BEAM Z CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727D, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 727D + 5, LBL 12, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727B, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT LEFT BS 296, WL 209, CRACKED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 328, RBL 20, CORRODED. REPAIRED WEB PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS AT BS 663, STRINGER 10L, BS 707, STRINGER 11L, BS 663, STRINGER 10R CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 787, BS 827, BS 867,BS 907, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,164 hrs · 29,742 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 9L, CRACKED. REPAIRED FRAME PER SRM.

Part: GASPER FAN — OVERHEATED (E/E BAY) · airframe 34,023 hrs · 29,620 cycles

ON DESCENT, ACRID ODOR REPORTED IN CABIN BY F/A'S. NO ODOR NOTED IN COCKPIT. ODOR DISSIPATED AFTER TURNING OFF GASPER FAN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LENS — LOOSE (CABIN) · airframe 33,354 hrs · 29,082 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY AT R1 DOOR.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 31,857 hrs · 28,087 cycles

DURING SCHEDULED CHECK, FOUND LT HORIZ STAB SKIN CRACKED AT STA 157.10 JUST FWD OF REAR SPAR. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 31,543 hrs · 27,627 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 30,617 hrs · 26,858 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 29,258 hrs · 25,787 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: TRIM TAB — WORN (RT ELEVATOR) · airframe 29,144 hrs · 25,685 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,663 hrs · 22,880 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, STR 26R. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,663 hrs · 22,880 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL WEBSCRACKED (2 EA) AT BS 180, WL 231, LBL 17.1 AND RBL 17.1. REMOVED AND REPLACED WEBS PER SRM.

Part: ENGINE — BIRD STRIKE (NR 1) · airframe 25,758 hrs · 23,033 cycles

ABORTED TAKEOFF, AT APPROX 100 KNOTS A LARGE BIRD WAS INGESTED INTO NR 1 ENGINE. COMPLIED WITH BIRD STRIKE INSP AND FOUND DAMAGED FAN BLADES. REMOVED AND REPLACED FAN BLADES PER MM.

Part: COVER — CRACKED (CABIN) · airframe 25,184 hrs · 22,478 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 8. R&R EEPLS COVER PER MM.

Part: BRACKET — CRACKED (AFT SVC DOOR) · airframe 25,184 hrs · 22,478 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE MOUNT BRACKET CRACKED. R&R MOUNT BRACKET PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 24,588 hrs · 21,955 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,180 hrs · 20,812 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 5, WL 198 & RBL 5, WL 201. REPAIRED BULKHEAD WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,180 hrs · 20,812 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL WEB CRACKED AT LBL 17, WL 190. REPAIRED BULKHEAD VERTICAL WEB PER SRM.

Part: COVER — DAMAGED (CABIN) · airframe 23,161 hrs · 20,794 cycles

EEPLS TRACK COVER DAMAGED AND WIRES EXPOSED AT ROW 20. REMOVED AND REPLACED TRACK COVER PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 23,037 hrs · 20,699 cycles

EEPLS INOP IN THREE PLACES. SECURED EEPLS WIRING PER MM.

Part: LENS — LOOSE (CABIN) · airframe 22,504 hrs · 20,287 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT PROXIMITY LIGHT LENS LOOSE AT ROW 23. SECURED LIGHT ASSY PER MM.

Part: LENS — BROKEN (L1 DOOR) · airframe 22,347 hrs · 20,152 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS PER MM.

Part: COVER — MISSING (CABIN)

EEPLS TRACK COVER MISSIND AT ROW 2. REPLACED COVER PER MM.

Part: EEL COVER — MISSING (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS AFT COVER MISSING. REPLACED COVER PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR)

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM.

Part: FAN — BURNED (E&E COPMT)

DURINNG FLIGHT A STRONG BURNING SMELL ENTERED THE CABIN AND COCKPIT. (LAX TO MCI). FOUND EQUIPMENT COOLING FAN BURNED OUT. REMOVED AND REPLACED COOLING FAN PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND LAST FOUR EEPLS INOP. REMOVED AND REPLACED TRACK LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS LIGHTS PULLED UP AT FWD END. RESECURED LIGHTS PER MM.

Part: SENSOR — OUT OF ADJUST (RT MLG)

AIR TURBACK, LANDING GEAR WOULD NOT RETRACT DURING TAKEOFF. HANDLE WOULD NOT MOVE ABOVE OFF POSITION. ADJUSTED MAIN GEAR SAFETY SENSOR TELEFLEX CABLE AND PERFORMED GEAR SWING CKECK PER MM.

Part: FRAME — CRACKED (GALLEY DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD GALLEY DOOR, LOWER FWD FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: SENSOR — DAMAGED (AOA SYST)

AIR TURNBACK - DURING AIRCRAFT ROTATION AND UP TO 75 KNOTS AFTER LANDING, STALL WARNING INDICATION, (CONTROL COLUMN VIBRATOR WENT ON). DISCOVERED CAPTAIN'S AOA SENSOR DAMAGED. REMOVED AND REPLACED AOA SENSOR PER MM.

Part: TRANSMITTER — ERRATIC (NR 2 FUEL FLOW)

NR 2 FUEL FLOW ERRATIC INDICATOR WILL ROLL BACK AT HIGH POWER SETTINGS. INDICATOR DOES NOT BLANK OR LOOSE POWER, BUT WENT TO NEARLY ZERO INDICATION. REPLACED FUEL FLOW TRANSMITTER PER MM.

Part: AIR DISTR — ODOR (CABIN)

FUEL SMELL NOTED IN FORWARD GALLEY AREA. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. INSPECTED CABIN AND CARGO AREAS, CHECKED A/C PACKS AND PERFORMED ENGINE RUN, NO DEFECTS NOTED.

Part: WIRE — DAMAGED (CABIN)

FOUND EXIT FLOOR LIGHTING INOPERATIVE IN ONE AREA. REPAIRED TRACK WIRING PER BOEING M/M.

Part: ENGINE — FAILED (NR 1)

DURING DESCENT INTO ELP, EXPERIENCED NUMBER 1 ENGINE FAILURE. AIRCRAFT MADE AN UNEVENTFUL LANDING AT ELP. INSPECTED AND FOUND NUMBER 1 ENGINE TOWER SHAFT FAILURE. REMOVED AND REPLACED ENGINE ASSEMBLY PER BOEING M/M.

Part: AIR TEMP PROBE — INOP (CAPT)

NUMBER 1 AIR TEMP PROBE LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED TOTAL AIR TEMP PROBE PER BOEING M/M.