N340LV

Part: SIGN — UNSECURE (R2 DOOR) · airframe 94,048 hrs · 54,506 cycles

R2 DOOR EXIT SIGN ADJACENT TO BOTTOM FELL OFF. INSTALLED SIGN IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 93,988 hrs · 54,465 cycles

R1 DOOR LOWER HINGE CUT OUT CRACKED AT BS 291.5. REPAIRED CUT OUT IAW EA.

Part: LENS — MISSING (EXIT SIGN) · airframe 93,691 hrs · 54,268 cycles

LEFT OVERWING EMER EXIT SIGN LENS MISSING. R & R LENS ASSEMBLY IAW MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 93,453 hrs · 54,072 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 93,384 hrs · 54,006 cycles

RIGHT WING OTBD AFT FLAP INBD CORNER DELAMINATED. R & R AFT FLAP IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 93,017 hrs · 53,722 cycles

EXIT LIGHT LENS LOOSE AT FWD FLIGHT ATTENDANT`S SEAT. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 92,993 hrs · 53,703 cycles

L1 DOOR EXIT LIGHT LENS MISSING. R & R LENS IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 92,907 hrs · 53,630 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT BS 338. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 92,659 hrs · 53,455 cycles

R1 EXIT LIGHT INOPERATIVE. R & R BATTERY PACK ASSEMBLY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 92,659 hrs · 53,455 cycles

L1 EXIT LIGHT INOPERATIVE. R & R BATTERY PACK ASSEMBLY IAW AMM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 92,659 hrs · 53,455 cycles

L1 DOOR EMER SIGN COVER BROKEN. R & R SIGN ASSEMBLY IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 92,308 hrs · 53,231 cycles

FORWARD EMER EXT LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 92,308 hrs · 53,231 cycles

FORWARD EMER EXT LIGHT INOPERATIVE. R & R BATTERY CHARGER ASSEMBLY IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 92,132 hrs · 53,097 cycles

L1 DOOR LOWER EMER EXIT LIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 92,132 hrs · 53,097 cycles

R1 DOOR LOWER EMER EXIT LIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: LIGHT — BROKEN (EXIT SIGN) · airframe 92,132 hrs · 53,097 cycles

L1 DOOR EMER EXIT SIGN LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW WDM.

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 92,097 hrs · 53,066 cycles

DECLARED EMER, FLAPS EXTENDED THROUGH 0 TO 5 LE FLAPS TRANSIT LIGHT ILLUMINATED. RECYCLED ILLUMINATED THROUGH FLAPS 15 THROUGH SECURED LIGHT OVERHEAD INDICATOR NORMAL. R & R NR 3 LE SLAT ACTUATOR ROD END IAW MM.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 91,619 hrs · 52,740 cycles

L1 DOOR FWD FRAME ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,615 hrs · 52,737 cycles

AFT EMER LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 91,615 hrs · 52,737 cycles

VERTICAL STABILIZER ACCESS PANEL 9545 ANGLE BY RIB 12 CRACKED ON ANGLE BY RIB 12. R & R ANGLE IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 91,615 hrs · 52,737 cycles

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

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 91,615 hrs · 52,737 cycles

EEPLS PHOTO LUMINESCENT STRIPS DAMAGED. R & R EEPLS IAW MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

STRINGER CORRODED AT BS 807+10, STRINGER 25L. REPAIRED STRINGER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

STRINGER CORRODED AT BS 827+10 STRINGER 25L. REPAIRED STRINGER IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 91,615 hrs · 52,737 cycles

FORWARD FLASHLIGHT BATTERY INOPERATIVE. R & R BATTERY IAW CMM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 91,615 hrs · 52,737 cycles

LEFT WING NR 3 MAIN FLAP TRACK FAIRING CRACKED ON CAP LOCATED UPPER SURFACE. R & R FAIRING IAW SRM & DWG.

Part: ATTACH FITTING — CORRODED (TE FLAP) · airframe 91,615 hrs · 52,737 cycles

LEFT WING NR 4 FLAP TRACK FWD ATTACH FITTING CORRODED AROUND HOLE. REPAIRED FITTING IAW CMM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

STRINGER CHANNEL CORRODED BETWEEN BS 344 TO 360, STRINGER 28R. R & R CHANNEL IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

SUPPORT ANGLE CRACKED AT BS 328 RBL 32. R & R ANGLE IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

STRAP CRACKED AT BS 328 RBL 32. R & R STRAP IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 91,615 hrs · 52,737 cycles

LEFT EXTERIOR EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: FLAP — CRACKED (LT WING) · airframe 91,615 hrs · 52,737 cycles

LEFT WING NR 1 LE FLAP CRACKED. R & R NR 1 FLAP IAW AMM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 91,615 hrs · 52,737 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

RIGHT SIDE TORQUE BOX STRINGER CORRODED BETWEEN BS 1088 TO 1138. R & R STRINGER IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (TE FLAP) · airframe 91,615 hrs · 52,737 cycles

LEFT WING NR 3 AFT FLAP TRACK FAIRING SUPPORT BRACKET CRACKED BETWEEN WBL 183.40 TO 198.60. R & R BRACKET IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 91,615 hrs · 52,737 cycles

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

Part: FITTING — CRACKED (TE FLAP) · airframe 91,615 hrs · 52,737 cycles

RIGHT WING NR 6 FLAP TRACK CLIP CRACKED. R & R CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

FUSELAGE CLIP CRACKED AT STATION 727, LBL 16. R & R CLIP IAW SRM.

Part: TAB — DELAMINATED (RT AILERON) · airframe 91,615 hrs · 52,737 cycles

RIGHT WING AILERON TAB FAIRING DELAMINATED. R & R TAB IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

TIE CLIP CRACKED AT BS 947.5, STRINGER 26L. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

ANGLE CRACKED AT STATION 947.5 TO 967, STRINGER 26L TO 24L. R & R ANGLE IAW SRM.

Part: ATTACH FITTING — CORRODED (TE FLAP) · airframe 91,615 hrs · 52,737 cycles

RIGHT WING NR 5 FLAP TRACK FWD ATTACH FITTING CORRODED AROUND HOLE. REPAIRED FITTING IAW CMM.

Part: SKIN — CORRODED (TE FLAP) · airframe 91,615 hrs · 52,737 cycles

RIGHT WING INBD AFT FLAP LOWER SURFACE CORRODED. REPAIRED FLAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

FRAME CRACKED AT BS 947.5, STRINGER 18L. R & R FRAME IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

FRAME CRACKED AT BS 348.2, STRINGER 15L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

AFT CARGO COMPARTMENT FRAME CRACKED AT BS 947.5 STRINGER 18R. R & R FRAME IAW SRM & DWG.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 91,615 hrs · 52,737 cycles

ACCESS PANEL 9507L PLATE CRACKED. R & R PLATE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

FRAME CRACKED AT BS 296.4, STRINGER 7R. REPAIRED FRAME IAW EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 91,615 hrs · 52,737 cycles

RIGHT WING NR 5 SLAT SKIN DELAMINATED. R & R NR 5 SLAT IAW MM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

SUPPORT ANGLE CRACKED AT BS 967, STRINGER 8R. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

WEB CRACKED BETWEEN BS 277 TO 291 STRINGER 14R. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

FRAME CRACKED AT BS 344, STRINGER 6L. REPAIRED FRAME IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 91,615 hrs · 52,737 cycles

RIGHT WING SUPPORT ANGLE TE LOWER SURFACE CRACKED AT WBL 198.00. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 277 TO 291, BETWEEN STRINGER 11R TO 10R. R & R ANGLE IAW SRM & DWG.

Part: SLAT — CRACKED (LT WING) · airframe 91,615 hrs · 52,737 cycles

LEFT WING NR 3 SLAT CRACKED AROUND LOWER AREA. R & R NR 3 SLAT IAW SRM.

Part: SLAT — CRACKED (LT WING) · airframe 91,615 hrs · 52,737 cycles

LEFT WING NR 1 LE SLAT CRACKED AROUND FASTENER HOLES. REPAIRED NR 1 SLAT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, RBL 31.6. R & R INTERCOSTAL IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

SUPPORT ANGLE CRACKED AT BS 360, STRINGER 9L. R & R ANGLE IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 91,615 hrs · 52,737 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 664+2 RBL 39. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 91,615 hrs · 52,737 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 664+2 RBL 38. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

MLG WW ANGLE CRACKED AT STATION 680, LBL 69. R & R ANGLE IAW SRM.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 91,615 hrs · 52,737 cycles

NOSE LANDING GEAR RT WW CRACKED AT BS 243.7 + 2.5, WL 169.1. REPAIRED WW IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

LEFT FRAME OTBD CHORD CRACKED AT BS 727, BETWEEN STRINGER 19L TO 20L. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

SKIN CRACKED AT BS 727, STRINGER 18A RT SIDE, FWD LOWER HOLE. REPAIRED SKIN IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

SKIN CRACKED AT BS 727, STRINGER 18A RT SIDE, AFT LOWER HOLE. REPAIRED SKIN IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A LT SIDE, CRACKED ON FWD LOWER HOLE. REPAIRED CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,615 hrs · 52,737 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A LT SIDE, FWD UPPER HOLE. REPAIRED CHORD IAW EO & EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,610 hrs · 52,732 cycles

FORWARD ENTRY EMER EXIT SIGN INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 91,610 hrs · 52,732 cycles

FORWARD ENTRY EMER EXIT SIGN INOPERATIVE. R & R BATTERY CHARGER IAW MM.

Part: LENS — MISSING (CABIN) · airframe 91,322 hrs · 52,528 cycles

LEFT EMER EXIT LIGHT LENS COVER MISSING. INSTALLED LENS IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 91,322 hrs · 52,528 cycles

L1 DOOR EMER EXIT SIGN LAMP INOPERATIVE. R & R LAMP IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 91,322 hrs · 52,528 cycles

WEB STRAP CRACKED AT BS 328 FLOORBEAM CTR AREA. R & R WEB IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,890 hrs · 52,200 cycles

AFT ENTRY FLOOR LEVEL EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 90,890 hrs · 52,200 cycles

L1 DOOR EMER EXIT LENS CRACKED. R & R LENS IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,890 hrs · 52,200 cycles

FORWARD ENTRY FLOOR LEVEL EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 90,807 hrs · 52,134 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 90,539 hrs · 51,933 cycles

L1 DOOR EMER EXIT LIGHTS INOPERATIVE. R & R BATTERY IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,539 hrs · 51,933 cycles

AFT GALLEY EMER EEPLS INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 90,539 hrs · 51,933 cycles

R1 DOOR EMER EXIT LIGHTS INOPERATIVE. R & R BATTERY IAW MM.

Part: COVER — MISSING (CABIN) · airframe 90,245 hrs · 51,716 cycles

ROW 12 DEF OVERHEAD BIN EGRESS LIGHT COVER MISSING. INSTALLED COVER IAW MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 90,160 hrs · 51,655 cycles

R1 COCKPIT WINDOW ARCING NEAR UPPER LT CORNER. R & R R1 WINDOW IAW MM.

Part: CHARGER — BROKEN (EMERGENCY LIGHT) · airframe 89,938 hrs · 51,484 cycles

L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R & R CHARGER IAW MM.

Part: BATTERY — BROKEN (EMERGENCY LIGHT) · airframe 89,938 hrs · 51,484 cycles

L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R & R BATTERY IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 89,938 hrs · 51,484 cycles

L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 89,477 hrs · 51,178 cycles

FWD ENTRY EMERGENCY EGRESS LIGHT LENS LOOSE. R & R LENS IAW SIP.

Part: SIGN — BROKEN (CABIN) · airframe 88,791 hrs · 50,726 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 87,941 hrs · 50,079 cycles

FWD BULKHEAD AT FWD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. R&R CHARGER ASSEMBLY IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 87,941 hrs · 50,079 cycles

FWD BULKHEAD AT FWD SERVICE EMERGENCY EXIT LIGHT INOPERATIVE. R&R CHARGER ASSEMBLY IAW MM.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 87,875 hrs · 50,030 cycles

LT ELEVATOR DAMAGED AREA UPPER SURFACE 37" FROM INBD END. R&R ELEVATOR IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 87,551 hrs · 49,784 cycles

SHEAR TIE CORRODED AT BS 344, STR 26R. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 87,551 hrs · 49,784 cycles

RIGHT WING T/E INBD NO STEP PANEL INBD SUPPORT ANGLE CRACKED AT AFT END. R & R ANGLE IAW SRM.

Part: LIGHT — UNSECURE (CABIN) · airframe 87,490 hrs · 49,739 cycles

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

Part: RIVET — LOOSE (L1 DOOR) · airframe 87,093 hrs · 49,471 cycles

L1 DOOR EMERGENCY EVAC SLIDE BUSHEL AFT GIRT BAR SHEET METAL HOOK RIVETS LOOSE. SECURED FASTENERS IAW MM.

Part: RIVET — LOOSE (R1 DOOR) · airframe 87,093 hrs · 49,471 cycles

R1 DOOR EMERGENCY EVAC SLIDE BUSHEL AFT GIRT BAR SHEET METAL HOOK RIVETS LOOSE. SECURED FASTENERS IAW MM.

Part: CABLE — MISROUTED (L2 DOOR) · airframe 87,093 hrs · 49,471 cycles

L2 DOOR EMERGENCY EVAC SLIDE CABLE ROUTED INCORRECTLY. REROUTED CABLE IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 87,080 hrs · 49,464 cycles

FORWARD LOWER EMERGENCY EXIT SIGNS INOP. REMOVED AND REPLACED BATTERY IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 87,081 hrs · 49,464 cycles

R-1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. REMOVED AND REPLACED CLIP IAW WDM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 87,081 hrs · 49,464 cycles

L-1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. REMOVED AND REPLACED CLIP IAW WDM.

Part: STRUCTURE — DAMAGED (LE SLAT) · airframe 87,081 hrs · 49,464 cycles

NR 1 SLAT INBOARD CAN INBOARD FWD WELD DAMAGED. REMOVED AND REPLACED NR 1 I/B SLAT CAN IAW SRM & DWG.

Part: RIB — CRACKED (LE SLAT) · airframe 87,081 hrs · 49,464 cycles

NR 1 SLAT INBOARD FSS S25.39 O/B RIB CRACKED FROM THE AFT EDGE OF LIGHTNING HOLE THROUGH THE AFT EDGE. REPAIRED RIB IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 87,081 hrs · 49,464 cycles

LEFT WING NR 1 SLAT CRACKED ON LOWER SURFACE. REPAIRED SKIN IAW SRM.

Part: WIRE — BROKEN (CABIN) · airframe 86,696 hrs · 49,187 cycles

EMERGENCY EXIT LIGHTING INOP. R & R WIRE IAW WDM MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 86,579 hrs · 49,104 cycles

EMERGENCY EXIT LIGHT ABOVE AFT ENTRY AND SERVICE DOORS INOP. REMOVED AND REPLACED BATTERY PACK BASE PER THE M/M. OPS CHECK OK.

Part: SIGN — DAMAGED (CABIN) · airframe 86,421 hrs · 48,980 cycles

LEFT ENTRY DOOR EMERGENCY EXIT SIGN ON LOWER BULKHEAD DAMAGED. REMOVED AND REPLACED LIGHT ASSY PER AMM.

Part: WIRE — BROKEN (CABIN) · airframe 86,421 hrs · 48,980 cycles

EMERGENCY LIGHT AT BULLNOSE AT SEAT LOCATION 2ABC AND 5DEF INOP. REPAIRED BROKEN WIRE AT PIN 1 OF CP AT POWER SUPPLY IAW AMM. OPS CHECK GOOD.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 86,216 hrs · 48,827 cycles

NR 1 PYLON - INNER & OUTER SKINS CRACKED AT ACCESS PANEL 5727L (O/B AFT CORNER). VERIFIED WITH HFEC. INSPECTED AND STOP DRILLED CRACK PER EA 1-354-1518.

Part: BATTERY — DISCHARGED (CABIN) · airframe 86,203 hrs · 48,817 cycles

CENTER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY TRAY PER MM. OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

FLOORBEAM UPPER FLANGE CRACKED AT BS 328, LBL 49. REPAIRED FLANGE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

FRAME INNER CHORD CRACKED AT BS 343, STR 22L. REPAIRED CHORD IAW SRM AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

STRINGER CORRODED AT BS 850, STR 23L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

FRAME CRACKED AT BS 360, BETWEEN STR 19R AND STR 20R. REPAIRED FRAME PER ER AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

STRINGER CORRODED AT BS 867, STR 23L. REPAIRED STRINGER IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

STUB BEAM CRACKED AT BS 616, BBL 69.85. REMOVED AND REPLACED BEAM PER SRM AND ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

SKIN CRACKED BETWEEN BS 307 TO BS 308, STR 18R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

FRAME CRACKED AT BS 616, WL 208. REMOVED AND REPLACED FRAME PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

VERTICAL STIFFENER CHANNEL CORRODED AT BS 227, RBL 5. REMOVED & REPLACED CHANNEL IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

L-ANGLE CRACKED AT BS 294.5, STR 13L. REMOVED AND INSTALLED L-ANGLE IAW SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

VERTICAL STIFFENER CHANNEL CORRODED AT BS 227, LBL 5. REMOVED & REPLACED STIFFENER IAW SRM & DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

STIFFENER CORRODED BETWEEN BS 219 TO BS 227, BL 0. REMOVED & REPLACED STIFFENER IAW SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

VERTICAL STIFFENER CORRODED AT BS 227, BL 0. REMOVED & REPLACED STIFFENER IAW SRM.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 85,994 hrs · 48,680 cycles

FLOOR PANEL IS CRACKED AND INSERTS BROKEN LOOSE AT FWD LAVATORY DOOR THRESHOLD. PANEL DAMAGED BEYOND REPAIR, FABRICATED REPLACEMENT PANEL PER BOEING DRAWING 65C15629, SHEET 1, ASSY-23. 56085U 22OCT12.

Part: SUPPORT ANGLE — CRACKED (CARGO BAY) · airframe 85,994 hrs · 48,680 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD TO SIDEWALL SUPPORT ANGLE IS CRACKED AT BS 727+4, RBL 37, WL 163. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

SKIN CORRODED AT BS 727+14, BETWEEN STR 27L TO STR 25R. REPAIRED SKIN PER ER AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

FLOOR SUPPORT CORRODED AT BS 859, RBL 8. REPAIRED SUPPORT PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

SHEAR TIE CORRODED AT BS 827, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE IAW SRM AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

STRINGER CORRODED AT BS 812, STR 21L. REPAIRED STRINGER PER ER AND EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

FLOORBEAM SUPPORT ANGLE CRACKED AT BS 727B, LBL 24.8. REPAIRED ANGLE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER ER AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

FLOOR SUPPORT CORRODED AT BS 859, LBL 3. REPAIRED SUPPORT PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

FLOORBEAM SUPPORT ANGLE CRACKED AT BS 727B, LBL 45.5. REPAIRED ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 85,994 hrs · 48,680 cycles

(LEFT WING) NR 1 PYLON I/B UPPER SUPPORT ANGLE CRACKED ABOVE SPRING DOOR. REMOVED & REPLACED (LEFT WING) NR 1 PYLON I/B UPPER SUPPORT ANGLE ABOVE SPRING DOOR IAW SRM 51-40-02-0G & 51-10-02-0G STEP 8C 84035U 24OCT12.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 85,994 hrs · 48,680 cycles

(LEFT WING) NR 1 PYLON I/B UPPER T/E PANEL SUPPORT ANGLE IS CRACKED. REMOVED NR 1 PYLON I/B UPPER T/E PANEL SUPPORT AND INSTALLED NEW SUPPORT PER SRM 51-40-02 STEPS 7 AND 9 8768C 28OCT12.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 85,994 hrs · 48,680 cycles

(LEFT WING) I/B NO-STEP PANEL O/B FWD LG BEAM ATTACH ANGLE CRACKED AND ALL FASTENERS HAVE PULLED THRU ANGLE. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT LOWER AFT CORNER AT BS 340.25, WL 209. REPAIRED SKIN PER ER AND EA.

Part: FASTENER — MISSING (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

FRAME INNER CHORD SUPPORT ANGLE FASTENER MISSING AT BS 348.2, STR 15L. INSTALLED FASTENERS IAW ER AND EA.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 85,994 hrs · 48,680 cycles

NR 1 PYLON, UPPER PANEL SUPPORT ANGLE CRACKED I/B END AFT SIDE. REMOVED AND REPLACED ANGLE PER SRM.

Part: SUPPORT ANGLE — CRACKED (NR 2 PYLON) · airframe 85,994 hrs · 48,680 cycles

(RIGHT WING) NR 2 PYLON CORNER SUPPORT ANGLE CRACKED ABOVE SPRING DOOR. REMOVED & REPLACED (RIGHT WING) NR 2 PYLON CORNER SUPPORT ANGLE ABOVE SPRING DOOR IAW SRM 51-40-02-0G & 51-10-02-0G, STEP 8C. 84035U 24OCT12.

Part: SEAL — CRACKED (FLAP TRACK) · airframe 85,994 hrs · 48,680 cycles

(RIGHT WING) NR 5 FLAP TRACK FAIRING LOWER SPRING ANGLE ON A/C IS CRACKED. REMOVED NR 5 FLAP TRACK FAIRING LOWER SPRING SEAL ANGLE CRACKED, INSTALLED NEW SPRING SEAL IAW SOPM 20-50-01 STEP 7 89264U 10/29/12.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 85,994 hrs · 48,680 cycles

70.5 WING FWD FAIRING CLOSE OUT SUPPORT ANGLE CRACKED AT BS 540. REMOVED DAMAGED SEAL ANGLE, FORMED NEW ANGLE AND HEAT TREATED PER BAC SPEC. LOCATED AND DRILLED FINISHED ANGLE AND INSTALLED IAW BOEING DWG 69-61951 84840U 10-16-2012.

Part: SKIN — CRACKED (LE SLAT) · airframe 85,994 hrs · 48,680 cycles

LEFT WING NR 2 SLAT LOWER L/E SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 85,994 hrs · 48,680 cycles

RIGHT WING NR 5 SLAT LOWER L/E SKIN CRACKED AT O/B END. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 85,994 hrs · 48,680 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED SKIN PER EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 85,994 hrs · 48,680 cycles

LEFT NOSE LANDING GEAR WHEEL WELL PRESSURE WEB CRACKED AT BS 246.7, WL 169.1. REPAIRED WEB IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,962 hrs · 48,654 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 85,962 hrs · 48,654 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,586 hrs · 48,379 cycles

FWD SERVICE EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: GARLOCK SEAL — LEAKING (NR 1 ENGINE) · airframe 85,110 hrs · 47,999 cycles

DIVERSION - OIL LEAKED NR 1 ENGINE. REMOVED AND REPLACED GARLOCK SEAL ON GEARBOX.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 84,872 hrs · 47,824 cycles

FLOORBEAM CRACKED AT BS 312, LBL 60. REPAIRED BEAM IAW EA AND AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 84,824 hrs · 47,783 cycles

R1 DOOR EMERGENCY LIGHT BULB BROKEN. REMOVED & REPLACED BULB IAW M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 84,824 hrs · 47,783 cycles

FUSELAGE SKIN DELAMINATED BETWEEN BS 358 TO BS 360, STR 14R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 84,824 hrs · 47,783 cycles

FRAME CRACKED AT BS 340, STR 16R. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 84,824 hrs · 47,783 cycles

BS 340, STR 10R STRINGER CLIP DAMAGED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 84,823 hrs · 47,783 cycles

R2 DOOR SLIDE OUT OF POSITION. RE-INSTALLED SLIDE ASSY PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 84,824 hrs · 47,783 cycles

LEFT AFT SIDEWALL EMERGENCY EXIT SIGN LIGHT INOP. RELAMPED SIGN IAW AMM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 84,822 hrs · 47,782 cycles

L1 DOOR AFT FRAME CRACKED IN RADIUS OF CUTOUT. REMOVED AND REPLACED DOOR ASSY PER AMM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 84,475 hrs · 47,526 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED EMERGENCY LIGHT CHARGER BASE PER M/M.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 84,448 hrs · 47,503 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT. RE-INSTALLED SLIDE PER M/T.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,064 hrs · 47,223 cycles

L1 DOOR EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY, BATTERY PACK & CHARGER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 84,005 hrs · 47,175 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 83,243 hrs · 46,574 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 83,002 hrs · 46,404 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 82,494 hrs · 46,042 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REPAIRED LENS PER EA.

Part: COVER — MISSING (CABIN) · airframe 82,474 hrs · 46,027 cycles

L2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. RE-INSTALLED COVER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 81,731 hrs · 45,471 cycles

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

Part: PLATE — OBSTRUCTED (GIRT BAR) · airframe 81,345 hrs · 45,169 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR ATTACH PLATE STIFF. REMOVED FOD FROM PLATE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 81,170 hrs · 45,040 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 671, LBL 24.5. REPAIRED BEAM PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD PRESSURE DECK ANGLE STIFFENER CORRODED AT BS 1016, BETWEEN STR 27L TO STR 27R. REPAIRED STIFFENER PER EO.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT PRESSURE BULKHEAD LOWER LOBE STIFFENER CORRODED AT BS 1016, BL 0. REPAIRED STIFFENER PER ACO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD PRESSURE DOME WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB PER EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 7 SPOILER UPPER SKIN DELAMINATED. REMOVED AND REPLACED NR 7 SPOILER PER MM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 9 SPOILER UPPER SKIN DELAMINATED. REMOVED AND REPLACED NR 9 SPOILER PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 662.5, LBL 24.5. REPAIRED CHORD PER EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT PRESSURE BULKHEAD LOWER LOBE STIFFENER CORRODED AT BS 1016, BL 0. REPAIRED STIFFENER PER ACO.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 500B, STR 27R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 27L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED CHANNEL PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 7L. REPAIRED WEB PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND ANGLE WEB CORRODED BETWEEN BS 904 TO BS 910, STR 17L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 947.5, RBL 3.0. REMOVED AND REPLACED CHANNEL PER SRM AND EA.

Part: LENS — BROKEN (EXIT SIGN) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND EMERGENCY EXIT SIGN LENS BROKEN ON SIDEWALL PANEL. REMOVED AND REPLACED SIGN PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 15R. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 15L. REPAIRED WEB PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 847, LBL 3.0. REMOVED AND REPLACED CHANNEL PER SRM AND EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 3. REPAIRED CHANNEL PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 24R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 732D, LBL 8.10. REPAIRED CHANNEL PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 739, LBL 3. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 3. REPAIRED CHANNEL PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 732D, RBL 3. REPAIRED CHANNEL PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 12.50. REPAIRED CHANNEL PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 24R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 14R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 2L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD WALL OF LAVATORY EMERGENCY FLASHLIGHT BASE BROKEN. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 80,806 hrs · 44,763 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT AFT EMERGENCY FLASHLIGHT BASE BROKEN. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,516 hrs · 44,520 cycles

DURING SCHEDULED CV CHECK, FOUND AFT ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 80,471 hrs · 44,483 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 80,350 hrs · 44,379 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 80,108 hrs · 44,195 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT LOWER EEPLS LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 79,690 hrs · 43,869 cycles

FWD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 79,621 hrs · 43,813 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 79,621 hrs · 43,813 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 79,338 hrs · 43,601 cycles

L1 & L2 DOORS EMERGENCY EXIT LIGHTS FAULTY. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 79,159 hrs · 43,460 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 79,159 hrs · 43,460 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 79,143 hrs · 43,447 cycles

AFT EMERGENCY EXIT LIGHT INOP. SECURED WIRE PER MM.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 79,043 hrs · 43,371 cycles

AFT F/A'S STATION EMERGENCY EXIT LIGHTS SWITCH INOP. REMOVED AND REPLACED SWITCH ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 79,027 hrs · 43,362 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 & L1 EMERGENCY FLOOR LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 78,302 hrs · 42,819 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 78,232 hrs · 42,768 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FWD RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CHARGER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,814 hrs · 42,448 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 77,574 hrs · 42,264 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD ENTRY EMERGENCY EXIT VERTICAL SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,410 hrs · 42,137 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY LOWER LEVEL EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER ER.

Part: WIRE — BROKEN (CABIN) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EEPLS INOP AT ROW 23. FOUND BROKEN WIRE, REPAIRED PER WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 510B, STR 27R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 509C, STR 27R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 482, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 380, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 25L. REMOVED AND REPLACED SPLICE PER BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND RT KEEL BEAM CORRODED AT BS 525. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 480, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 364.4, STR 27R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED SPLICE PER BAC DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED AT BS 540. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME ANGLE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED ANGLE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME ANGLE CORRODED AT BS 500, BETWEEN STR 26L TO STR 27L. REPAIRED ANGLE PER SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE SKIN BUTT STRAP CORRODED AT BS 360, STR 26L. REPAIRED SKIN PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 360, STR 27L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 492, BETWEEN STR 17R TO STR 25R. REPAIRED FRAME PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR UPPER HINGE CUTOUT CRACKED AT BS 304, BETWEEN WL 257 TO WL 262. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

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

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 559, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 420, BETWEEN STR 19R TO STR 20R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED BETWEEN BS 360 TO BS 540, BETWEEN STR 26L TO STR 26R. REMOVED AND REPLACED SKIN PANEL PER SRM.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 559, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 2. REPAIRED BEAM PER ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 927, STR 22R. REMOVED AND REPLACED STRINGER PER BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CHORD CRACKED AT BS 440, BETWEEN STR 18R TO STR 19R. REPAIRED FRAME PER BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 837 TO BS 846, STR 18R. REPAIRED WEB PER BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED BETWEEN BS 510A TO BS 540, STR 20L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 947, STR 25L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 360, STR 13L. REPAIRED FRAME PER SWA EA.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 360, STR 13L. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 517D, STR 12L. REPAIRED SKIN PER ACO.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 480, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 77,216 hrs · 41,980 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,216 hrs · 41,980 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 76,515 hrs · 41,481 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 76,390 hrs · 41,381 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD FRAME OF AFT CARGO DOOR CUTOUT CRACKED AT BS 794. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,390 hrs · 41,381 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500D, STR 12L. REPAIRED SKIN PER ER.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 76,256 hrs · 41,288 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED CHARGER ASSY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 75,713 hrs · 40,925 cycles

L1 DOOR EMERGNECY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 74,418 hrs · 40,001 cycles

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

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 74,418 hrs · 40,001 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 74,022 hrs · 39,699 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,407 hrs · 39,233 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,407 hrs · 39,233 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,407 hrs · 39,233 cycles

DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,964 hrs · 38,916 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,964 hrs · 38,916 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 72,636 hrs · 38,682 cycles

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

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 72,429 hrs · 38,532 cycles

AIR TURNBACK / DECLARED EMERGENCY / INFLIGHT SHUTDOWN. NR 1 ENGINE FAILURE ON CLIMBOUT OF SMF, NOTICED BURNING BIRD RESIDUE SMELL. POSSIBLY AS A RESULT OF BIRD STRIKE OR FROM PREVIOUS FLIGHT. APPROX 4500' MSL NR 1 ENGINE MADE LOUD BANGING NOISE. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 71,717 hrs · 37,994 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 71,560 hrs · 37,862 cycles

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

Part: LENS — MISSING (CABIN) · airframe 71,521 hrs · 37,832 cycles

DURING SCHEDULED SPV CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 10 ABC. INSTALLED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,521 hrs · 37,832 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 71,521 hrs · 37,832 cycles

DURING SCHEDULED SPV CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 10 ABC. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 71,521 hrs · 37,832 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 10 ABC. INSTALLED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 71,505 hrs · 37,819 cycles

EEPLS COVER MISSING AT ROW 10 ABC. INSTALLED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 71,377 hrs · 37,712 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 71,350 hrs · 37,693 cycles

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

Part: LENS — MISSING (CABIN) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM SKIN CRACKED BETWEEN BS 695 AND BS 705, LBL 6.5. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REPAIRED FLAP PER SRM.

Part: BEARING — WORN (ELEVATOR TAB) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 664, BL 0. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: LENS — CRACKED (CABIN) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 16 ABC. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 400 S4L) · airframe 71,287 hrs · 37,646 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,134 hrs · 37,524 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 70,631 hrs · 37,132 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 70,578 hrs · 37,090 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 70,281 hrs · 36,879 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: WIRE HARNESS — CHAFED (APU BAY) · airframe 70,242 hrs · 36,846 cycles

DECLARED EMERGENCY, APU FIRE WARNING LIGHT & HORN INDICATIONS. APU FIRE EXTINGUISHER BOTTLE DISCHARGED. FOUND APU FIRE WARN HARNESSES CHAFING. REMOVED AND REPLACED HARNESSES PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 70,190 hrs · 36,801 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 69,725 hrs · 36,424 cycles

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

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 69,725 hrs · 36,424 cycles

DURING SCHEDULED OTS CHECK, FWD CABIN EMERGENCY BATTERY PACK AND BATTERY CHARGER FAILED TEST. REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER PER MM.

Part: MECHANISM — FAULTY (NR 1 ENGINE) · airframe 69,384 hrs · 36,125 cycles

ON TAKEOFF NR 1 ENGINE UNABLE TO MAINTAIN CLIMB N1 WITH NR 1 POWER LEVER FULL FORWARD. FOUND VBV NOT CLOSING ALL THE WAY. REMOVED AND REPLACED VBV MECHANISM AND VBV MOTOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,200 hrs · 35,977 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,131 hrs · 35,923 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,871 hrs · 35,716 cycles

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

Part: STRUCTURE — CRACKED (AFT CARGO DOOR) · airframe 68,299 hrs · 35,249 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD LOWER TEE CAP CRACKED. REMOVED AND REPLACED CARGO DOOR PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 68,299 hrs · 35,249 cycles

DURING SCHEDULED C4 CHECK, FOUND LOWER EMERGENCY EXIT LIGHT LENS MISSING AT R1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,935 hrs · 34,931 cycles

DURING SCHEDULED SERVICE CHECK, FOUND ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,516 hrs · 34,608 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED LIGHT BULBS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,478 hrs · 34,582 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME WEB CRACKED AT LOWER DOOR STOP FITTING. REPAIRED FRAME WEB PER SB AND SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,478 hrs · 34,582 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME WEB CRACKED AT LOWER DOOR STOP FITTING. REPAIRED FRAME WEB PER SB AND SWA EA.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 67,470 hrs · 34,577 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY FUSE PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 67,470 hrs · 34,577 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 351, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,557 hrs · 33,905 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,401 hrs · 33,771 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — LOOSE (L1 DOOR) · airframe 65,539 hrs · 33,089 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: CHARGER — INOPERATIVE (L1 & R1 DOOR) · airframe 65,539 hrs · 33,089 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 AND R1 DOORS LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,539 hrs · 33,089 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, AFT LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (L1 DOOR) · airframe 65,539 hrs · 33,089 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR SKIN CRACKED AT LOWER FWD CORNER. REPAIRED L1 DOOR SKIN PER SRM.

Part: SHAFT — SHEARED (ACTUATOR) · airframe 65,514 hrs · 33,064 cycles

NR 4 GRND SPOILER INBD HYD ACTUATOR SHAFT SHEARED. REMOVED AND REPLACED NR 4 GROUND SPOILER INBD ACTUATOR PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,681 hrs · 32,381 cycles

L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,615 hrs · 32,316 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA & SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,088 hrs · 31,890 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD LT & RT LOWER EMERGENCY EXIT DOOR SIGN LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK & CHARGER PER MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,654 hrs · 31,540 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: FAN — FAULTY (COCKPIT) · airframe 63,398 hrs · 31,347 cycles

ELECTRICAL SMELL IN COCKPIT. TURNED EQUIPMENT COOLING FAN TO ALTERNATE, SMELL SUBSIDED. REMOVED AND REPLACED FAN PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 1016, RBL 31, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 351, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB AT BS 664, LBL 31, CRACKED. REPAIRED PRESSURE WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM TEE CAP AT BS 986, LBL 15, CORRODED. REPAIRED FLOORBEAM PER TRM T1-453-037.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 1006, LBL 19, CORRODED. REPAIRED FLOORBEAM CHORD PER SRM AND BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT LOWER RADIUS, CRACKED. REPAIRED SKIN PER BOEING SB.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOOR SUPPORT AT BS 267, FROM LBL 12 TO RBL 12, CORRODED. REPAIRED FLOOR SUPPORT PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 277, FROM LBL 39 TO RBL 47, CORRODED. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,796 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR UPPER HINGE CUTOUT LOWER RADIUS, CRACKED. REPAIRED SKIN PER BOEING SB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 294, FROM LBL 35 TO LBL 49, CORRODED. REPAIRED FLOORBEAM SECTION PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUELAGE SKIN AT BS 517, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA.

Part: STRUCTURE — CRACKED (BS 616-639) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRUCTURE BETWEEN BS 616 AND BS 639, STRINGER 18R, CRACKED. REPAIRED STRUCTURE PER T1-153-018.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 967, RBL 18, CORRODED. REPAIRED FLOORBEAM PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB BETWEEN BS 616 AND BS 639, RBL 70, CRACKED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 663, STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB AT BS 580, RBL 70, CRACKED. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 3 EACH LT CREASE BEAM WEBS CRACKED AT BS 580, BS 620 AND BS 640. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 947.5, STRINGER 27L, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,196 hrs · 31,201 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 967, STRINGER 24R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: HYDRAULIC LINE — LEAKING (L MLG WW) · airframe 62,971 hrs · 31,015 cycles

AIR TURNBACK / DECLARED EMERGENCY. HYD A-SYS FAILURE DURING FLIGHT. REMOVED AND REPLACED LT MLG RETRACT ACTUATOR HYD HOSE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 62,860 hrs · 30,931 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 62,860 hrs · 30,931 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR THRESHOLD EMERGENCY EXIT LIGHT LENS, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: COVER — MISSING (EMERGENCY SIGN) · airframe 62,481 hrs · 30,630 cycles

FWD ENTRY EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: HOOK — LOOSE (R1 DOOR GIRTBAR) · airframe 61,994 hrs · 30,211 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 61,994 hrs · 30,211 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 61,869 hrs · 30,094 cycles

FWD EMERGENCY EXIT LIGHT LENS, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,057 hrs · 29,427 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR, OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,057 hrs · 29,427 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR, OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 60,995 hrs · 29,373 cycles

DURING SCHEDULED A2 CHECK, FOUND LT AND RT EMERGENCY EXIT MARKERS WILL NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,517 hrs · 28,990 cycles

EMERGENCY EXIT LIGHT NEXT TO FORWARD F/A'S SEAT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM.

Part: ENGINE — FAULTY (LEFT) · airframe 60,503 hrs · 28,977 cycles

AIR TURNBACK, DECLARED EMERGENCY, ON TAKEOFF NR 1 ENGINE EGT FELL TO 350 DEGREES, AIRBORNE AT 800 FEET NR 1 ENGINE VIBRATION METER MAXED OUT AT 5 UNITS WITH AIRFRAME VIBRATION. NR 1 ENGINE WAS PUT IN IDLE POSITION AND VIBRATION STOPPED, EGT STILL LOW. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,351 hrs · 28,848 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 500B, BETWEEN STRINGERS 27R AND 28R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 60,094 hrs · 28,638 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED AT T/E. REMOVED AND REPLACED FOREFLAP PER MM.

Part: UPLOCK SENSOR — FAULTY (RT MLG) · airframe 58,395 hrs · 27,301 cycles

AIR TURNBACK, RT MLG UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP AND OFF. REMOVED AND REPLACED RT MLG UPLOCK SENSOR PER MM.

Part: SNUBBER — FAULTY (FWD ENTRY DOOR) · airframe 58,321 hrs · 27,236 cycles

AIR TURNBACK, AIRCRAFT WOULD NOT PRESSURIZE. REMOVED AND REPLACED FWD ENTRY DOOR SNUBBER AND ADJUSTED DOOR PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,785 hrs · 26,800 cycles

DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 57,632 hrs · 26,682 cycles

FWD ENTRY EMERGENCY EXIT SIDE LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,497 hrs · 26,577 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 57,497 hrs · 26,577 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED ON INBOARD SIDE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: TRUNNION PIN — CORRODED (LT & RT MLG) · airframe 56,912 hrs · 26,109 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11251-32, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,482 hrs · 25,783 cycles

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

Part: TRANSMISSION — FAULTY (RT/LT WING) · airframe 55,998 hrs · 25,409 cycles

FLAPS WOULD NOT DEPLOY WHEN THE FLAP LEVER WAS POSITIONED OUT OF THE UP POSITION. ALTERNATE FLAP SWITCH WAS USED TO SELECT FLAPS 15 DEGREES FOR LANDING. REMOVED AND REPLACED NR 4 AND NR 5 FLAP TRANSMISSIONS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 55,979 hrs · 25,395 cycles

EMERGENCY EXIT SIGN AT FWD ENTRY DOOR BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 55,623 hrs · 25,113 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED CABLE PER MM.

Part: AUGMENTOR TUBE — FAULTY (MLG) · airframe 55,001 hrs · 24,597 cycles

BRAKE TRAVEL IS SIGNIFICANT WITHOUT ANY BRAKING ACTION. BRAKES GRABBING SUDDENLY. REMOVED AND REPLACED LEFT AND RIGHT BRAKE METERING VALVES AND LT AND RIGHT BRAKE FEEL AUGMENTORS PER MM.

Part: FRAME — CRACKED (AFT ENTRY DOOR) · airframe 54,773 hrs · 24,394 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR AFT FRAME CRACKED AT 2ND DOOR STOP PIN ASSY. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 54,773 hrs · 24,392 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 774, LBL 3. REPAIRED FLOORBEAM PER SWA RA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,773 hrs · 24,392 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: LENS — MISSING (CABIN) · airframe 54,622 hrs · 24,270 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT LENS MISSING AT ROW NR 12DEF. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,707 hrs · 23,549 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AFT OF E/E EXHAUST CUTOUT. REPAIRED SKIN PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 53,045 hrs · 23,026 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD STIFFENER CRACKED AT BS 663, LBL 6.5. REPAIRED STIFFENER PER SWA RA.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,720 hrs · 22,767 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 177 AND LBL 5.7. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,720 hrs · 22,767 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 183, WL 223 AND RBL 17.1. REPAIRED WEB PER SRM..

Part: WEB — CRACKED (FUSELAGE) · airframe 52,720 hrs · 22,767 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND BULKHEAD WEB CRACKED (4 EA) AT BS 178, WL 234 AND LBL 12.0, WL 199 AND LBL 5.0, WL 201 AND RBL 5.0, WL 199 AND RBL 5.0. REPAIRED WEB PER SRM.

Part: TAB — WORN (LH ELEVATOR) · airframe 51,927 hrs · 22,106 cycles

DURING SCHEDULED C2 CHECK, FOUND LH ELEVATOR TAB WORN AT HINGE POINTS. R&R LH ELEVATOR TAB PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 50,988 hrs · 21,333 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 50,177 hrs · 20,653 cycles

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

Part: IRU — INOPERATIVE (COCKPIT)

BOTH IRU DC FAIL LIGHTS ILLUMINATED FOLLOWED BY ALIGN LIGHT, HEADING AND ATTITUDE FLAGS AT NR 1 SIDE. RESET GROUND SERVICE, SWITCHED HOT BATTERY BOX, AND HOT BATTERY BOX C/B'S. OPS CK GOOD.

Part: FLOORBEAM — CRACKED (BS 520)

DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CRACKED, BS 520, RBL 45.4. REPAIRED BEAM PER ER NR 99-6481.

Part: LIGHT — CONTAMINATED (ESCAPE SLIDE)

DURING SCHEDULED TRANSITION CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE EMERGENCY LIGHT LENS FILLED WITH MOISTURE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CREASE BEAM — CORRODED (BS 727)

DURING SCHEDULED TRANSITION CHECK, FOUND CORROSION ON INNER CREASE BEAM CHORD, BS 727, WL 208, RBL 58. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (BS 400)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME CRACKED, BS 400, BETWEEN STRINGERS 8L-9L. REPAIRED FRAME PER ER NR 99-6410.

Part: FRAME — CRACKED (BS 767,787 & 907)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAMES CRACKED, BS 907, BS 787, AND BS 767 ABOVE STRINGER 9L. REPAIRED FRAMES PER ER NR 99-6410, AND SRM.