N643SW

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 61,847 hrs · 48,511 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS LOOSE. INSTALLED LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 61,691 hrs · 48,410 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 61,691 hrs · 48,410 cycles

FORWARD RT FLASHLIGHT STRAP BROKEN. R&R STRAP PER AMM.

Part: COVER — LOOSE (CABIN) · airframe 61,674 hrs · 48,401 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. R&R COVER PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 61,504 hrs · 48,287 cycles

L1 DOOR FORWARD WALL EMERGENCY EXIT LIGHT COVER LENS LOOSE. SECURED THE LENS IAW SIP.

Part: LENS — CRACKED (EXIT SIGN) · airframe 61,261 hrs · 48,121 cycles

L1 DOOR EXIT SIGN LENS CRACKED. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 60,903 hrs · 47,888 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOWER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 60,903 hrs · 47,888 cycles

RIGHT WING T/E COVE ATTACH BRACKET CRACKED AT WS 537.806. R & R BRACKET IAW SRM AND DWG.

Part: CONNECTOR — LOOSE (CABIN) · airframe 60,903 hrs · 47,888 cycles

L1 OVER DOOR EXIT SIGN CONNECTORS LOOSE. R & R CONNECTOR ASSEMBLY IAW WDM.

Part: SKIN — CRACKED (RT WING) · airframe 60,903 hrs · 47,888 cycles

RIGHT WING UPPER SKIN CRACKED BETWEEN RSS. 220 TO 256.84. REPAIRED THE SKIN IAW ER AND EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,903 hrs · 47,888 cycles

RT WING UPPER SKIN FASTENER HOLES CRACKED BETWEEN RSS 264.84 TO RSS 270.89. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (LT WING) · airframe 60,903 hrs · 47,888 cycles

LEFT WING UPPER WING SKIN CRACKED FROM FASTENER HOLE RSS. 269 AFT ROW. REPAIRED THE SKIN PER ER AND EA.

Part: AILERON — DELAMINATED (RT WING) · airframe 60,903 hrs · 47,888 cycles

RT WING AILERON DELAMINATED AT BOTTOM SIDE T/E FROM NR 3 HINGE. R & R AILERON IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

SHEAR TIE CRACKED AT BS 727E, BETWEEN STRINGER 27L - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

RIGHT CREASE BEAM WEB CRACKED BETWEEN BS 616 - 639. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 887 - 907. R & R WEB IAW SRM.

Part: FRAME — CRACKED (BS 300) · airframe 60,903 hrs · 47,888 cycles

R1 DOOR UPPER STUB FRAME CRACKED AT BS 300, AT UPPER DOOR STOP FITTING. R & R STUB FRAME IAW SRM & DWG.

Part: SPAR — CRACKED (LT WING) · airframe 60,903 hrs · 47,888 cycles

LEFT WING UPPER SPAR WEB CRACKED RSS. 224.14. REPAIRED SPAR WEB IAW ER AND EA.

Part: SPAR — CRACKED (LT WING) · airframe 60,903 hrs · 47,888 cycles

LEFT WING UPPER SPAR CRACKED AT RSS. 224.14. REPAIRED THE SPAR IAW ER AND EA.

Part: SPAR — CRACKED (RT WING) · airframe 60,903 hrs · 47,888 cycles

RIGHT WING UPPER SPAR WEB CRACKED BETWEEN RSS. 211 TO 238. REPAIRED THE WEB IAW EA.

Part: LINK ASSY — CORRODED (LT MLG) · airframe 60,903 hrs · 47,888 cycles

LT MLG SUPPORT BEAM SWING LINK CORRODED AT AFT BUSHING BORES. R & R LINK ASSEMBLY IAW EA.

Part: SUPPORT FITTING — CRACKED (RT MLG) · airframe 60,903 hrs · 47,888 cycles

RIGHT WING UPPER SPAR AFT MAIN LANDING GEAR SUPPORT FITTING CRACKED, RSS 224.14. REPAIRED FITTING ER AND EA.

Part: SPAR — CRACKED (RT WING) · airframe 60,903 hrs · 47,888 cycles

RIGHT WING UPPER SPAR CRACKED BETWEEN RSS. 223.14 TO RSS. 285. REPAIRED IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

FRAME INNER WEB CRACKED AT BS 639, STRINGER 16R. REPAIRED WEB IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

SHEAR TIE CORRODED AT BS 887, BETWEEN STRINGER 21L - 22L. R & R SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

SHEAR TIE CORRODED AT BS 727E, BETWEEN STRINGER 26R - 27R. R & R SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

STRINGER CLIP CORRODED AT BS 747, STRINGER 27L. R & R CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

AFT CARGO FLOOR WEB CORRODED BETWEEN BS 847 - 867, BETWEEN RBL 22 - 26. R & R WEB IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

SHEAR TIE CORRODED AT BS 986.5, BETWEEN STRINGER 27R - 27L. R & R SHEAR TIE IAW DWG & SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

STRINGER SPLICE CORRODED AT BS 907, STRINGER 20R. R & R SPLICE IAW DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

SHEAR TIE CORRODED AT BS 986.5, BETWEEN STRINGER 26L - 27L. R & R SHEAR TIE IAW DWG & SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

STRINGER SPLICE CORRODED STRINGER SPLICE AT BS 907, STRINGER 23L. R & R SPLICE IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

ANGLE CORRODED AT BS 867, STRINGER 26R. R & R ANGLE IAW DWG & SRM.

Part: SUPPORT FITTING — CRACKED (R1 DOOR) · airframe 60,903 hrs · 47,888 cycles

R1 DOOR SUPPORT FITTING CRACKED AT BS 296, STRINGER 8R. R & R FITTING IAW SRM & DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 60,903 hrs · 47,888 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE INNER RIB CRACKED AT HSS 188.94. REPAIRED RIB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,903 hrs · 47,888 cycles

CREASE BEAM WEB CORRODED AT BS 459, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: CONNECTOR — BROKEN (CABIN) · airframe 60,903 hrs · 47,888 cycles

L1 DOOR EXIT LIGHT CONNECTOR BROKEN. R & R CONNECTOR IAW WDM AND AMM.

Part: LUG — BROKEN (LT SPOILER) · airframe 59,916 hrs · 47,227 cycles

LEFT WING NR 4 GND SPOILER HINGE LUG BROKEN. R & R SPOILER ASSEMBLY IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 58,648 hrs · 46,332 cycles

L1 DOOR EMER EGRESS LIGHT COVER LOOSE. SECURED COVER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,229 hrs · 46,028 cycles

EMERGENCY LIGHTS ON ROW 20 DEF INOPERATIVE. R & R LIGHTS ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,229 hrs · 46,028 cycles

EMERGENCY LIGHTS ON ROW 18 ABC - 24 DEF INOPERATIVE. R & R LIGHTS ASSEMBLY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 58,229 hrs · 46,028 cycles

EXIT LIGHT LENS MISSING AT ROW 20 DEF. INSTALLED LENS IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 58,229 hrs · 46,028 cycles

LEFT WING INBD FORE FLAP DELAMINATED. R & R FLAP IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 58,229 hrs · 46,028 cycles

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

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 57,592 hrs · 45,613 cycles

FORWARD CABIN EMER EXIT LIGHT FAULTY. R & R BATTERY SUPPLY IAW AMM.

Part: FUEL CAP — SEPARATED (RT WING) · airframe 57,507 hrs · 45,557 cycles

AIR TURN BACK, CREW REPORTS RT WING OVERWING FUEL CAP CAME OFF IN FLIGHT WITH APPROX 2500 LB RT MAIN FUEL QTY VENTED OVERBOARD. R & R RT MAIN TANK OVERWING FUEL CAP IAW MM.

Part: SLIDE — FAILED (R1 DOOR) · airframe 57,489 hrs · 45,540 cycles

R1 DOOR EMER EVAC SLIDE FAILED OPERATION TEST. R & R SLIDE IAW MT.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

STRINGER CLIP CRACKED AT BS 727D, STRINGER 3L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

STRINGER CLIP CRACKED AT BS 767, STRINGER 2R. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

STRINGER CLIP CRACKED AT BS 827, STRINGER 2R. R & R CLIP IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

SHEAR TIE CRACKED AT BS 907, STRINGER 2L. R & R SHEAR TIE IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

STRINGER CRACKED AT BS 500, STRINGER 14R. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

SKIN CRACKED AT BS 380, STRINGER 14L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

SKIN CRACKED AT BS 480, STRINGER 14L. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

STRINGER CLIP CRACKED AT BS 277, STRINGER 4L. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

SKIN CRACKED AT BS 380, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

RIGHT FUSELAGE SKIN CRACKED AT STATION 787+10, LOWER FWD CORNER OF WINDOW CUT OUT. REPAIRED SKIN IAW EA & SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

LEFT BS 807+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

LEFT BS 867+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

LEFT BS 827+10 UPPER AFT WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

LEFT FUSELAGE SKIN CRACKED AT STATION 807+10, UPPER AFT CORNER OF WINDOW CUT OUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

LEFT FUSELAGE SKIN CRACKED AT STATION 787+10, UPPER AFT CORNER OF WINDOW CUT OUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

LEFT BS 847+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

LEFT FUSELAGE SKIN CRACKED AT STATION 767+10, UPPER AFT CORNER OF WINDOW CUT OUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 45,383 cycles

LEFT BS 847+10 UPPER AFT WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW SB.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 56,634 hrs · 44,954 cycles

FORWARD ENTRY DOOR EXIT SIGN LIGHT COVER FELL OFF. INSTALLED COVER IAW AMM.

Part: LUG — BROKEN (LT SPOILER) · airframe 56,566 hrs · 44,906 cycles

LEFT WING GND SPOILER NR 4 OTBD MAIN ATTACH LUG BROKEN. R & R NR 4 GND SPOILER IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 56,178 hrs · 44,625 cycles

RIGHT OVERWING EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW SIP.

Part: COVER — LOOSE (CABIN) · airframe 56,178 hrs · 44,625 cycles

FORWARD ENTRY EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,021 hrs · 44,511 cycles

RIGHT OVERWING EMER LIGHT BULB INOPERATIVE. RE-LAMPED BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,021 hrs · 44,511 cycles

RIGHT OVERWING EMER EXIT LIGHT BULB INOPERATIVE. RE-LAMPED BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,021 hrs · 44,511 cycles

RIGHT OVERWING EMER EXIT LIGHT BULB INOPERATIVE. RE-LAMPED BULB IAW MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 747 TO 767. R & R WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B LBL 45.5. REPAIRED BEAM IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW SRM & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B RBL 45.5. REPAIRED BEAM IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B RBL 24.8. REPAIRED CHORD IAW ER & EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

AFT PRESS BULKHEAD WEB RADIAL STIFFENER CORRODED AT BS 1017 RBL 0.2. REPAIRED STIFFENER IAW ER & EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

AFT PRESS BULKHEAD WEB RADIAL STIFFENER CORRODED AT BS 1017 LBL 0.2. REPAIRED STIFFENER IAW ER & EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

AFT PRESS BULKHEAD WEB CORRODED AT BS 1017 BETWEEN RBL 8 TO LBL 9. REPAIRED WEB IAW ER & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

AFT PRESS BULKHEAD STIFFENER ANGLE CORRODED AT BS 1016, BETWEEN RBL 8 TO LBL 9. REPAIRED ANGLE IAW ER & EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

ATTACH CLIP CRACKED AT BS 348.2, STRINGER 16L. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

R1 DOOR LOWER HINGE FUSELAGE SKIN CUT OUT CRACKED AT BS 291.5. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 666 TO 674, LBL 24.5. R & R CHORD IAW ER & EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,021 hrs · 44,511 cycles

MAIN WW HORIZONTAL PRESS DECK CRACKED AT BS 673 LBL 42. REPAIRED DECK IAW ER & EA.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

PRESSURE WEB CORRODED AT BS 1016 BL 0-3R. REPAIRED WEB IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER FWD CORNER. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

FLOORBEAM UPPER FLANGE CORRODED AT BS 986.5 RBL 43. REPAIRED FLANGE IAW ER & EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

AFT CARGO BAY, ON INBD KEEL BEAM TO FRAME ATTACH ANGLE CORRODED AT BS 727E, STRINGER 27R. R & R ANGLE IAW SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 56,021 hrs · 44,511 cycles

RIGHT WING INBD MID FLAP LOWER SURFACE OF TE WEDGE DELAMINATED. R & R WEDGE IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

FUSELAGE FRAME AUXILIARY CHORD CRACKED AT BS 727, BETWEEN STRINGER 20L TO 21L. REPAIRED CHORD IAW EA & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

STIFFENER CRACKED AT BS 663.75 RBL 6.15. REPAIRED STIFFENER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

FORWARD RT CORNER OF AIR CONDITIONED DOOR SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,021 hrs · 44,511 cycles

AIR CONDITIONER DOOR FUSELAGE SKIN CUT OUT CRACKED AT LT CORNER. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 55,648 hrs · 44,230 cycles

RIGHT WING STATION 135.5 RIB-3, VERY AFT WEB CRACKED IN THE RIB LOWER CHORD. REPAIRED WEB IAW EA.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 54,116 hrs · 43,218 cycles

KEEL BEAM CLOSURE PANEL DELAMINATED JUST AFT OF A/C BAY DOORS. R & R PANEL IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 54,116 hrs · 43,218 cycles

RT WING TE ANGLE JUST FWD OF NR 2 AILERON HINGE CRACKED. R & R ANGLE IAW SRM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 54,116 hrs · 43,218 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 53,654 hrs · 42,863 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT BROKEN. R&R LIGHT IAW MM SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,409 hrs · 42,684 cycles

FS SKIN CRACKED AT STATION 500D+12, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: LENS — LOOSE (EXIT SIGN) · airframe 52,791 hrs · 42,227 cycles

LT SIDE EMERGENCY EXIT SIGN LENS LOOSE. R & R COVER IAW MM.

Part: GAUGE — FAULTY (FUEL SYSTEM) · airframe 52,782 hrs · 42,221 cycles

DIVERSION NR 2 FUEL QTY GUAGE DECREASED UNTIL ZERO. R & R NR 2 FUEL QTY GUAGE IAW AMM.

Part: RETAINING CLIP — CRACKED (VERTICAL STAB) · airframe 52,447 hrs · 41,990 cycles

RIGHT VERTICAL STABILIZER LOWER ACCESS PANEL 9508R RETAINER CLIP CRACKED. REMOVED AND REPLACED CLIP PER SRM.

Part: DUCT — LOOSE (AC BAY) · airframe 52,013 hrs · 41,674 cycles

DIVERSION - WHILE CLIMBING OUT OF ORLANDO THE FLIGHT ATTENDANTS CALLED TO SAY THAT THE PASSENGERS IN ROW 7-9 HEARD A "POPPING" NOISE AND SMELLED SMOKE. FLIGHT ATTENDANTS CONFIRMED SMELL. SECURED DUCTS ON MANIFOLD PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,818 hrs · 41,532 cycles

EMERGENCY LIGHT AT 15DEF BULLNOSE INOP. RELAMPED PER M/M, OPS CHECK GOOD PER M/M.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 51,681 hrs · 41,428 cycles

RIGHT WING I/B FORE FLAP UNDER SURFACE PUNCTURED. REPAIRED FORE FLAP IAW SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 50,923 hrs · 40,882 cycles

L2 WINDOW ARCED AT CRUISE. REMOVED AND REPLACED L2 WINDOW PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

WEB CRACKED BETWEEN BS 867 TO BS 887, STR 25R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CRACKED AT BS 807, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

SHEAR TIE CRACKED AT BS 887, STR 19R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FLAP — CORRODED (LT WING) · airframe 50,073 hrs · 40,236 cycles

LEFT WING O/B AFT FLAP CORRODED. REMOVED AND REPLACED AFT FLAP IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

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

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

ANGLE CORRODED AT BS 947.5, BETWEEN STR 25R TO STR 25L. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CRACKED AT BS 188, STR 17R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

SUPPORT ANGLE WEB CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

WEB CORRODED BETWEEN BS 302.9 TO BS 351.2, LBL 55. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,073 hrs · 40,236 cycles

LEFT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

SUPPORT ANGLE CRACKED AT BS 188 LOWER NOSE COMPARTMENT. REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

WEB CORRODED BETWEEN BS 344 TO BS 351.2, LBL 55. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 294.5 TO BS 312 E/E COMPARTMENT. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

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

Part: RIB — CRACKED (TE FLAP) · airframe 50,073 hrs · 40,236 cycles

RIGHT WING INBOARD MIDFLAP INBOARD EDGE RIB CRACKED. REMOVED AND REPLACED RIB IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

STRINGER CORRODED AT BS 1088 TO BS 1156 INSIDE APU COMPT AREA. REMOVED AND REPLACED STRINGER PAR SRM & BAC DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

SUPPORT ANGLE CRACKED BETWEEN 380 TO BS 400, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 787, BETWEEN STR 26L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 807, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

SHEAR TIE CORRODED SHEAR TIE AT BS 807, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 787, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 947.5, BETWEEN STR 26R TO STR 27L. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 497.5, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

STRINGER CORRODED BETWEEN BS 880 TO BS 894, STR 21R. REPAIRED STRINGER IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

STRINGER SPLICE CORRODED AT BS 907, STR 21R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 927, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 727C, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CRACKED AT BS 520, BETWEEN STR 21L TO STR 22L. REPAIRED FRAME IAW EO AND EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

SUPPORT STRUCTURE ANGLE CRACKED AT BS 277+12, BETWEEN STR 12L TO STR 13L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

STIFFENER CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

STIFFENER CRACKED AT BULKHEAD BS 727, STR 27L. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

STRINGER CRACKED AT BS 420+19, STR 28R. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

TIE CLIP CRACKED AT BS 440, STR 4R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

STRINGERS SPLICE CORRODED AT BS 907, STR 24L. REMOVED AND REPLACED SPLICE IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

KEEL BEAM ANGLE CORRODED AT BS 520, STR 28R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

TIE CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

TIE CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

TIE CLIP CRACKED AT BS 520, STR 27L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FLOORBEAM CRACKED AT BS 328, LBL 29. REPAIRED BEAM IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

STRINGER CORRODED AT BS 927, STR 22L. REPAIRED STRINGER IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FLOORBEAM CORRODED AT BS 344, LBL 9. REPAIRED BEAM IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

ANGLE CRACKED AT BS 967, BETWEEN STR 3L TO STR 4L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

STRINGERS SPLICE CORRODED AT BS 907, STR 25L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

ANGLE CLIP CRACKED AT BS 578, STR 17R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

CRACK ON STRAP LOC BS 312 TO BS 344, BBL 0. REPLACED STRAP IAW SRM AND DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 50,073 hrs · 40,236 cycles

EEPLS BROKEN. REMOVED AND REPLACED EEPLS IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 500, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28R TO STR 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

SHEAR TIE CORRODED AT BS 500 BETWEEN, STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FRAME CORRODED AT BS 500, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD WEB CRACKED BS 706 2.5, BBL 0. REPAIRED WEB IAW SI.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

WEB CRACKED AT BS 714, BBL 0.07. REPAIRED WEB IAW SI.

Part: SIGN — BROKEN (CABIN) · airframe 50,073 hrs · 40,236 cycles

BROKEN EMERGENCY EXIT SIGN ASSY AT FWD LAVATORY. REMOVED AND REPLACED SIGN ASSY IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD WEB CRACKED BS 706+3.5, BBL 0. REPAIRED WEB IAW SI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD WEB CRACKED BS 706+4.5, BBL 0. REPAIRED WEB IAW SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,073 hrs · 40,236 cycles

FUSELAGE SKIN CRACKED AT BS 520+9, BETWEEN STR 28L AND STR 28R. REPAIRED SKIN IAW EA.

Part: LIGHT — LOOSE (CABIN) · airframe 49,462 hrs · 39,765 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS COVER LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW M/M.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,056 hrs · 39,484 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME WEB CRACKED AT BS 616, LBL 66. REPAIRED WEB IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 49,055 hrs · 39,485 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING T/E I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,056 hrs · 39,484 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, LBL 47. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,056 hrs · 39,484 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, RBL 47. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,777 hrs · 39,264 cycles

DURING SCHEDULED OTS CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 41. REPAIRED BEAM IAW ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 48,777 hrs · 39,264 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CORRODED AT BS 993, RBL 45. REPAIRED FRAME IAW SRM.

Part: MOUNT — MISSING (R2 DOOR) · airframe 48,773 hrs · 39,263 cycles

DURING SCHEDULED OTS CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR MOUNT MISSING. INSTALLED MOUNT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,225 hrs · 38,849 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 440+8, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,225 hrs · 38,849 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 440, STR 4L. REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,184 hrs · 38,814 cycles

DURING SCHEDULED OTS CHECK FOUND, LT OVERWING EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: COVER — LOOSE (CABIN) · airframe 47,900 hrs · 38,602 cycles

DURING SCHEDULED CV CHECK FOUND EEPLS COVER LOOSE AT ROW 23. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,973 hrs · 37,891 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R2 DOOR EMERGENCY LIGHT LENS LOOSE AND 1 LIGHT INOP. RELAMPED LIGHT AND SECURED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 45,897 hrs · 37,088 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,886 hrs · 37,079 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,886 hrs · 37,079 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,886 hrs · 37,079 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,886 hrs · 37,079 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,886 hrs · 37,079 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,886 hrs · 37,079 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER ER & EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 45,354 hrs · 36,680 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 44,536 hrs · 36,042 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING T/E FLAP NR 8 SPINDLE CORRODED ON LOWER SURFACE AT AFT BEARING SUPPORT. REMOVED AND REPLACED NR 8 FLAP TRACK SPINDLE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 44,940 hrs · 36,006 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 44,472 hrs · 35,993 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 44,215 hrs · 35,798 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 42,022 hrs · 34,172 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER SWA EA.

Part: LENS — LOOSE (CABIN) · airframe 41,931 hrs · 34,099 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,678 hrs · 33,913 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 40,949 hrs · 33,408 cycles

DURING MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: COVER — LOOSE (CABIN) · airframe 40,948 hrs · 33,408 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,431 hrs · 33,030 cycles

DURING SCHEDULED HC2 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD WEB CRACKED AT STR 6R. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,292 hrs · 32,927 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 666, LBL 24. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,292 hrs · 32,927 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663, LBL 24. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,292 hrs · 32,927 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 656, LBL 24. REPAIRED BEAM PER EA.

Part: FITTING — LOOSE (GIRT BAR) · airframe 40,292 hrs · 32,927 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,292 hrs · 32,927 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 659, LBL 24. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,292 hrs · 32,927 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 671, LBL 24. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,292 hrs · 32,927 cycles

DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 695, RBL 24. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,292 hrs · 32,927 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,292 hrs · 32,927 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 40,292 hrs · 32,927 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WHEEL WELL UPPER PRESSURE WEB CRACKED AT BS 665, BETWEEN LBL 13 TO LBL 33. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (BS 767 S27L/R) · airframe 39,143 hrs · 32,121 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 39,143 hrs · 32,121 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,143 hrs · 32,121 cycles

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

Part: VERTICAL BEAM — CRACKED (BS 178 BULKHEAD) · airframe 39,143 hrs · 32,121 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,143 hrs · 32,121 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,143 hrs · 32,121 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,143 hrs · 32,121 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED BEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 39,143 hrs · 32,121 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER 22R CRACKED BETWEEN BS 492 AND BS 500. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 39,143 hrs · 32,121 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER 23R CRACKED BETWEEN BS 492 AND BS 500. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 35,793 hrs · 29,571 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 616) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 63, WL 202. REPAIRED FRAME PER ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND VERTICAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED VERTICAL STAB FITTING PER ER.

Part: FRAME — CRACKED (BS 616) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 63, WL 202. REPAIRED FRAME SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 47 TO LBL 5. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CREASED AT BS 747, STR 27R. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED STAB FITTING PER SRM.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 33,984 hrs · 28,206 cycles

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

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FORE FLAP T/E WEDGE DELAMINATED AT OUTBOARD L/E. REPAIRED FORE FLAP PER SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED FWD GIRT BAR HOOK PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 312 S28R) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 312, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: GIRT BAR — CORRODED (L1 DOOR) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S11L) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S11R) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 27 TO RBL 48. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 787 S8R) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 827 S8R-8L) · airframe 33,984 hrs · 28,206 cycles

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

Part: FRAME — CRACKED (BS 440 S8L) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 33,984 hrs · 28,206 cycles

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

Part: FRAME — CRACKED (BS 867 S8R) · airframe 33,984 hrs · 28,206 cycles

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

Part: FRAME — CRACKED (BS 480 S8L) · airframe 33,984 hrs · 28,206 cycles

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

Part: RIB — CORRODED (RT FORE FLAP) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP INBOARD RIB CORRODED. REMOVED AND REPLACED FORE FLAP RIB PER SRM.

Part: FRAME — CRACKED (BS 178) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND BULKHEAD FRAME CRACKED AT RIGHT BS 178, WL 208. REMOVED AND REPLACED CHORD SECTION PER ACO.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 33,984 hrs · 28,206 cycles

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

Part: RIB — CORRODED (RT FORE FLAP) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD FORE FLAP OUTBOARD RIB CORRODED. REMOVED AND REPLACED FORE FLAP RIB PER SRM.

Part: FRAME — CRACKED (BS 178) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND BULKHEAD FRAME CRACKED AT LEFT BS 178, WL 208. REMOVED AND REPLACED CHORD SECTION PER ACO.

Part: FRAME — CRACKED (BS 727D) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, S8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 33,984 hrs · 28,206 cycles

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

Part: FRAME — CRACKED (BS 400 S8L) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: SKIN — DEBONDED (T/E FLAP) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DISBONDED AT OUTBOARD TRAILING EDGE. REPAIRED SKIN SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,984 hrs · 28,206 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 32,944 hrs · 27,409 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT LT MID CABIN. SECURED STRIP PER MM.

Part: BOLT — WORN (LT ELEVATOR) · airframe 32,793 hrs · 27,298 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR CONTROL TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT PER MM.

Part: BOLT — WORN (RT ELEVATOR) · airframe 32,793 hrs · 27,298 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR CONTROL TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT PER MM.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 31,909 hrs · 26,597 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATES OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 31,861 hrs · 26,553 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. R&R LIGHT LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 27,396 hrs · 22,993 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 27,396 hrs · 22,993 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT UPPER SKIN DELAMINATED AT OB END. REMOVED AND REPLACED SLAT IAW MM.

Part: SKIN — DELAMINATED (LH WING FLAP) · airframe 30,693 hrs · 25,642 cycles

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

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 30,693 hrs · 25,642 cycles

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

Part: LATCH — OUT OF ADJUST (FWD CABIN) · airframe 28,245 hrs · 23,663 cycles

DURING SCHEDULED SERVICE CHECK, FOUND F/O'S EMERGENCY ESCAPE ROPE DOOR LATCH OUT OF ADJUST. ADJUSTED DOOR LATCH PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,419 hrs · 23,012 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,257 hrs · 22,903 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: HOOK — LOOSE (L1 GIRT BAR) · airframe 27,066 hrs · 22,760 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD HOOK LOOSE. REMOVED AND REPLACED L1 DOOR FWD HOOK PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 27,066 hrs · 22,760 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 27,066 hrs · 22,760 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,198 hrs · 22,052 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,188 hrs · 22,044 cycles

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

Part: SLIDE — LOOSE (L1 DOOR) · airframe 26,166 hrs · 22,031 cycles

L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 26,147 hrs · 22,017 cycles

L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 25,787 hrs · 21,723 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD END, DELAMINATED. REMOVED AND REPLACED LT OUTBOARD T/E AFT FLAP PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,787 hrs · 21,723 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY FLOORBEAM AT BS 771, RBL 3 TO RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: DOOR — CRACKED (R1 DOOR) · airframe 25,787 hrs · 21,723 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AT AFT FRAME LOWER CORNER, CRACKED. REPAIRED DOOR PER BAC DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,787 hrs · 21,723 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 947, LBL 8, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 25,380 hrs · 21,392 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 24,642 hrs · 20,796 cycles

R1 DOOR EVACUATION SLIDE PRESSURE IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 24,489 hrs · 20,674 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 23,569 hrs · 19,961 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: CABLE — FRAYED (L2 DOOR) · airframe 20,812 hrs · 17,221 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE RELEASE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: BRACKET — LOOSE (FWD ENTRY DOOR) · airframe 19,826 hrs · 16,920 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SLIDE — LOOSE (FWD SVC DOOR) · airframe 18,624 hrs · 15,929 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: OUTFLOW VALVE — ERRATIC (FWD CARGO) · airframe 18,381 hrs · 15,713 cycles

AIR TURN BACK, DUE TO LOUD NOISE/SQUEAL AND CABIN PRESSURIZATION CONTROL FLUCTUATION. REMOVED AND REPLACED FWD CARGO OUTFLOW VALVE PER MM.

Part: LENS — BROKEN (CABIN)

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT LENS BROKEN NEXT TO AFT LAV. REMOVED AND REPLACED LENS PER MM.

Part: BRACKET — CORRODED (L1 DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVACUATION SLIDE ATTACHED BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED,BS 927, STRINGER 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 17,442 hrs · 14,951 cycles

DURING SCHEDULED 1/2D CHECK, FOUND TIE CLIP CRACKED AT BS 927, 27L. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: COVER — MISSING (CABIN) · airframe 17,442 hrs · 14,951 cycles

EEPLS COVER MISSING AT OVERWING EXIT. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 17,442 hrs · 14,951 cycles

EEPLS COVER MISSING AT OVER WING EMERGENCY EXIT. INSTALLED EEPLS COVER PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 17,128 hrs · 14,711 cycles

EEPLS TRACK COVERS OUT OF POSITION. SECURED COVERS PER MM.

Part: HYDRAULIC LINE — RUPTURED (NR 2 ENGINE) · airframe 16,762 hrs · 14,416 cycles

DECLARED EMERGENCY, B SYSTEM HYDRAULIC FLUID QUANTITY STARTED DECREASING FOLLOWED BY NR 2 ENG LOW PRESSURE LIGHT ILLUMINATING. QRH FOLLOWED & LANDING ACCOMPLISHED. FOUND HYD FLEX LINE BETWEEN ACOUSTIC FILTER & MODULAR PACKAGE RUPTURED. R&R LINE, HYD PUMP & FILTER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 15,988 hrs · 13,768 cycles

EEPLS LOOSE AT OVERWING EXIT. SECURED EEPLS PER MM.

Part: RETAINER — LOOSE (ENTRY DOOR) · airframe 15,118 hrs · 13,030 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: RETAINER — LOOSE (SERVICE DOOR) · airframe 15,118 hrs · 13,030 cycles

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

Part: SLIDE — OUT OF TOLERANCE (SERVICE DOOR) · airframe 14,633 hrs · 12,620 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJ (FWD SVC DOOR) · airframe 14,447 hrs · 12,463 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJ (CABIN) · airframe 47,285 hrs · 37,773 cycles

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

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 11,522 hrs · 10,030 cycles

FWD ENTRY DOOR EVACUATION SLIDE COMING OUT OF CONTAINER. REINSTALLED SLIDE ASY PER MM.

Part: SKIN — DELAMINATED (TE FLAPS)

DURING SCHEDULED C3 CHECK, FOUND LT AND RT OUTBOARD AFT FLAPS DELAMINATED ON INBOARD CORNERS. REMOVED AND REPLACED BOTH AFT FLAPS PER MM.

Part: SLIDE — LOW PRESS (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — INOP (ROW 14)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT ON LT OVERHEAD BIN AT ROW 14 IS INOPERATIVE. REPLACED EMERGENCY LIGHT PER BOEING MM.