N363SW

Part: FLAP — DELAMINATED (LT WING) · airframe 74,776 hrs · 61,821 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED. R&R AFT FLAP PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,776 hrs · 61,821 cycles

RT EMERGENCY LIGHT INOP AT ROW 16. RELAMPED LIGHT PER AMM.

Part: SKIN — CRACKED (BS 927) · airframe 74,724 hrs · 61,783 cycles

SKIN CRACKED AT BS 927+14, STRINGER 23R. REPAIRED THE SKIN IAW EA.

Part: SKIN — CRACKED (BS 500D) · airframe 74,724 hrs · 61,783 cycles

SKIN CRACKED AT BS 500D+15, STRINGER 15L. REPAIRED THE SKIN IAW EA.

Part: FRAME — CRACKED (BS 360) · airframe 74,724 hrs · 61,783 cycles

FRAME CRACKED AT BS 360, STRINGER 20R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 328) · airframe 74,724 hrs · 61,783 cycles

FRAME CRACKED AT BS 328, STRINGER 20R. REPAIRED THE FRAME IAW ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,724 hrs · 61,783 cycles

FUSELAGE SKIN CRACKED AT BS 827+5, STR 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (BS 927) · airframe 74,724 hrs · 61,783 cycles

FUSELAGE SKIN CRACKED AT BS 927+16, STRIGNER 24L. REPAIRED THE SKIN IAW EA.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 74,192 hrs · 61,356 cycles

L1 DOOR EXIT SIGN COVER FELL OFF. SECURED COVER IAW AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 73,879 hrs · 61,104 cycles

G1 GALLEY EMER EXIT LIGHT WIRE DAMAGED. REPAIRED WIRE IAW WDM.

Part: SKIN — CRACKED (LT WING) · airframe 73,879 hrs · 61,104 cycles

LEFT WING UPPER SKIN CRACKED AT WS 208, COMMON TO REAR SPAR UPPER CHORD FORWARD ROW. REPAIRED SKIN IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,879 hrs · 61,104 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 400 - 420. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,879 hrs · 61,104 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 807 - 827. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,879 hrs · 61,104 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 420 - 440. R & R WEB IAW SRM & DWG.

Part: SPAR — CRACKED (RT WING) · airframe 73,879 hrs · 61,104 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 221, UPPER FASTENER ROW, HOLE 3. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 73,879 hrs · 61,104 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 221, UPPER FASTENER ROW, HOLE 3. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 73,879 hrs · 61,104 cycles

LEFT WING UPPER REAR SPAR CHORD VERTICAL FLANGE UPPER ROW CRACKED. REPAIRED FLANGE IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,879 hrs · 61,104 cycles

FLOORBEAM UPPER FLANGE CORRODED AT BS 947.5, LBL 11. REPAIRED FLOORBEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,879 hrs · 61,104 cycles

FRAME CRACKED AT BS 639, LOWER END BS 639, WL 198 RT SIDE. REPAIRED FRAME IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 73,879 hrs · 61,104 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT RSS 224.14. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 73,879 hrs · 61,104 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT RSS 224.14. REPAIRED CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,879 hrs · 61,104 cycles

FRAME CORRODED AT BS 360, LBL 2. REPAIRED FRAME IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,879 hrs · 61,104 cycles

SHEAR TIE CORRODED AT BS 727D, BETWEEN STRINGER 26L - 27L. REPAIRED SHEAR TIE IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,879 hrs · 61,104 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 27R - 27L. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,879 hrs · 61,104 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 27R - 26R. R & R SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,879 hrs · 61,104 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 25L - 26L. R & R FRAME IAW SRM & DWG.

Part: DOUBLER — CRACKED (LE SLAT) · airframe 73,879 hrs · 61,104 cycles

RIGHT WING NR 6 SLAT FIXED LE INTERNAL NOSE BEAM DOUBLER CRACKED AT TAI DUCT CUT OUT. R & R SLAT IAW SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 73,879 hrs · 61,104 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: WEB — CRACKED (NLG WW) · airframe 73,879 hrs · 61,104 cycles

RIGHT NLG WW SIDE WEB CRACKED AT BS 251 - 243. REPAIRED WEB IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 73,705 hrs · 60,982 cycles

RIGHT OVERWING EXIT LIGHT LENS LOOSE. R & R EXIT LIGHT ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 73,647 hrs · 60,943 cycles

RIGHT OVERWING EMER LIGHT LENS LOOSE. SECURED LENS IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,471 hrs · 60,826 cycles

LEFT BULLNOSE EMER LIGHT INOPERATIVE AT ROW 10. RELAMPED LIGHT IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 73,436 hrs · 60,803 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW SIP.

Part: SKIN — CRACKED (RT WING) · airframe 73,223 hrs · 60,656 cycles

RIGHT WING INSPAR SKIN, CRACKED AT WBL 175 AT FASTENER HOLE REAR SPAR. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 73,223 hrs · 60,656 cycles

RIGHT WING INSPAR SKIN, CRACKED AT WBL 175 AT FASTENER HOLE REAR SPAR. REPAIRED SKIN IAW SRM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 73,223 hrs · 60,656 cycles

LEFT EMER EXIT SIGN LOWER LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 73,193 hrs · 60,636 cycles

BUTT SPLICE STRAP CRACKED AT BS 360, BETWEEN STRINGER 5R - 7R. R & R BUTT STRAP IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,193 hrs · 60,636 cycles

RIGHT AFT OVERWING EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,193 hrs · 60,636 cycles

SKIN CRACKED AT BS 360, STRINGER 5R. REPAIRED SKIN IAW EA.

Part: LENS — MISSING (EXIT SIGN) · airframe 72,479 hrs · 60,074 cycles

RIGHT OVERWING LOWER EXIT SIGN LENS COVER MISSING. R & R LENS IAW AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 72,200 hrs · 59,861 cycles

RIGHT WING NR 5 SLAT OTBD SIDE DELAMINATED. R & R NR 5 SLAT IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 71,972 hrs · 59,709 cycles

L1 DOOR EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: SIGN — DETACHED (CABIN) · airframe 71,937 hrs · 59,678 cycles

RIGHT EMER EXIT SIGN FELL OFF AT ROW 11. INSTALLED SIGN IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,731 hrs · 59,531 cycles

BULLNOSE EXIT LIGHT INOPERATIVE AT ROW 16 DEF. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 71,731 hrs · 59,531 cycles

LEFT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 71,438 hrs · 59,311 cycles

MID CABIN FLOOR EGRESS ILLUMINATION STRIP LOOSE BETWEEN ROW 8 - 9. SECURED STRIP IAW SIP.

Part: PUSH-PULL CABLE — FAULTY (NR 2 ENGINE) · airframe 71,209 hrs · 59,138 cycles

AT ALTITUDE THROTTLES ARE TOO STIFF TO CONTROL IN A NORMAL MANNER. VERY DIFFICULT TO MOVE FROM IDLE & NOTICEABLE. RESTRICTION AT 81% A POSITION. PROBLEM IS ASSOCIATED WITH COLD TEMPERATURE. UPON LANDING REVERSES WERE EXTREMELY DIFFICULTY TO DEPLOY. R & R NR 2 ENG THRUST CONTROL PUSH & PULL CABLES IAW MM.

Part: PUSH-PULL CABLE — FAULTY (NR 1 ENGINE) · airframe 71,209 hrs · 59,138 cycles

AT ALTITUDE THROTTLES ARE TOO STIFF TO CONTROL IN A NORMAL MANNER. VERY DIFFICULT TO MOVE FROM IDLE & NOTICEABLE. RESTRICTION AT 81% A POSITION. PROBLEM IS ASSOCIATED WITH COLD TEMPERATURE. UPON LANDING REVERSES WERE EXTREMELY DIFFICULTY TO DEPLOY. R & R NR 1 ENG THRUST CONTROL PUSH & PULL CABLES IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 71,112 hrs · 59,060 cycles

R1 DOOR EMER LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,061 hrs · 59,015 cycles

FUSELAGE SKIN CRACKED AT BS 424.5, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 71,061 hrs · 59,015 cycles

LEFT WING OTBD FORE FLAP DELAMINATED ON THE OTBD TE. REPAIRED FORE FLAP IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 70,606 hrs · 58,698 cycles

RIGHT OVERWING EMER EXIT LIGHT AT THE LOWER FWD CORNER OF THE DOOR LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — UNSECURE (CABIN) · airframe 68,937 hrs · 57,502 cycles

RIGHT OVERWING EMER EXT LENS FELL OFF. REINSTALLED LENS IAW MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

FRAME CORRODED AT BS 827, BETWEEN STRINGER 27R TO STRINGER 27L. REPAIRED FRAME IAW SRM.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 68,557 hrs · 57,229 cycles

RIGHT WING NR 6 FLAP TRACK FIXED FAIRING INTERNAL CAVITY INBD SIDE STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

FLOOR STRUCTURE ANGLE CRACKED AT BS 270, BL 0. REPAIRED ANGLE IAW EO & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

WEB CORRODED BETWEEN BS 460 TO BS 480, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

WEB CORRODED BETWEEN BS 480 TO BS 500, STRINGER 17L. REPAIRED WEB IAW EO & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

WEB CORRODED BETWEEN BS 360 TO BS 380, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420, STRINGER 17R. REPAIRED WEB IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

WEB CORRODED BETWEEN BS 380 TO BS 400, STRINGER 17L. R & R WEB IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

WEB CORRODED BETWEEN BS 420 TO BS 440, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 480 TO BS 500, STRINGER 17R. REPAIRED WEB IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

STRINGER CORRODED AT BS 1088+27, UPPER SIDE OF INLET AIR DUCT FLANGE TORQUE BOX RT SIDE. R & R STRINGER IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

FUSELAGE SKIN CRACKED AT BS 520+2.5, STRINGER 8R. EXPIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 68,557 hrs · 57,229 cycles

RIGHT WING ACCESS PANEL 6534 SUPPORT ANGLE CRACKED. R & R ANGLE IAW DWG & SRM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 68,557 hrs · 57,229 cycles

LEFT WING INBD FLAP, OTBD CARRIAGE INBD CORRODED. REPAIRED FLAP IAW CMM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

PRESSURE BULKHEAD Z STIFFENER CRACKED AT BS 1016, BETWEEN STRINGER 25L TO 26L. REPAIRED Z STIFFENER IAW EO & EA.

Part: COVER — CRACKED (R1 DOOR) · airframe 68,557 hrs · 57,229 cycles

R1 DOOR AFT CUT OUT COVER CRACKED. R & R COVER IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STRINGER 9R TO STRINGER 10R. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

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

Part: COVER — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

COVER OF LOWER HINGE CRACKED AT BS 303.9, BETWEEN STRINGER 13L TO STRINGER 14L. R & R COVER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE LWR POSITION ANGLE CRACKED AT BS 348.2, STRINGER 15L. REPAIRED ANGLE IAW EA & EO.

Part: WEDGE — CRACKED (TE FLAP) · airframe 68,557 hrs · 57,229 cycles

LEFT WING MID FLAP CRACK INBD WEDGE PANEL CRACKED. REPAIRED WEDGE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

WEB CRACKED AT BS 639, STRINGER 17L. REPAIRED WEB IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 68,557 hrs · 57,229 cycles

FORWARD LAVATORY WALL EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

STRAP CRACKED AT BS 947.5, STRINGER 16L. R & R STRAP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

ANGLE CRACKED AT BS 344, LBL 11. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

CRACK ON RETAINER LOCATED AFT CUT OUT FWD ENTRY DOOR ANGLE CHORD CRACKED AT BS 348.2 & BETWEEN STRINGER 8L TO STRINGER 9L. R & R ANGLE IAW SRM & DWG.

Part: COVER — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

COVER OF UPPER HINGE CRACKED AT BS 303.9, BETWEEN STRINGER 10L TO STRINGER 11L. R & R COVER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE LWR POSITION ANGLE CRACKED AT BS 348.2, STRINGER 16L. REPAIRED ANGLE IAW EA & EO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE UPPER POSITION ANGLE CRACKED AT BS 348.2, STRINGER 16L. REPAIRED ANGLE IAW EA & EO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

FORWARD GALLEY DOOR SURROUND STRUCTURE ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STRINGER 11R TO STRINGER 12R. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STRINGER 12R TO STRINGER 13R. R & R ANGLE IAW SRM & DWG.

Part: LENS — BROKEN (CABIN) · airframe 68,557 hrs · 57,229 cycles

FORWARD GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 68,557 hrs · 57,229 cycles

LEFT WING FIXED TE SUPPORT ANGLE CRACKED AT BS 537.80. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 68,557 hrs · 57,229 cycles

LEFT WING FIXED TE SUPPORT ANGLE CRACKED AT WBL 70.85. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

Z DOOR ANGLE CORRODED AT BS 967+12, STRINGER 17R. R & R Z ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, RBL 11. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

FLOORBEAM CRACKED AT BS 947.5, STRINGER 17L. REPAIRED FLOORBEAM IAW EO & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

FITTING CRACKED AT BS 333, STRINGER 8R. R & R FITTING IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 68,557 hrs · 57,229 cycles

MAIN WW PRESS DECK CRACKED AT BS 664+1, LBL 24.5+14.5. REPAIRED DECK IAW EO & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

SPLICE ANGLE CORRODED AT BS 1006, STRINGER 17R. R & R SPLICE ANGLE IAW & DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 68,557 hrs · 57,229 cycles

MAIN WW PRESS DECK CRACKED AT BS 664+1, LBL 24.5+7.5. REPAIRED DECK IAW EO.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

SUPPORT ANGLE CRACKED AT BS 328, RBL 34. R & R ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 5 TO RBL 45. REPAIRED CHORD IAW EO & EA.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

CRACK ON MAIN WW PRESS DECK LOCATED AT BS 664+1.5, LBL 24.5+8. REPAIRED DECK IAW EA.

Part: PLATE — CRACKED (NR 2 NACELLE) · airframe 68,557 hrs · 57,229 cycles

NR 2 ENG COWL ACCESS PANEL PLATE CRACKED OTBD FAN COWL. R & R PLATE IAW DWG & SRM.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 68,557 hrs · 57,229 cycles

LEFT WING NR 3 SPOILER UPPER SKIN DELAMINATED. R & R NR 3 SPOILER IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

SKIN CRACKED AT BS 927+5.0, STRINGER 24L. REPAIRED SKIN IAW SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

AFT CARGO DOOR CUT OUT AFT CORNER SCUFF PLATE CRACKED. REPAIRED CUT OUT IAW EA.

Part: STRUCTURE — CRACKED (LT PYLON) · airframe 68,557 hrs · 57,229 cycles

LEFT PYLON STRUT ACCESS 5764L CRACKED. REPAIRED STRUT IAW EA.

Part: SKIN — CRACKED (APU DOOR) · airframe 68,557 hrs · 57,229 cycles

APU ACCESS DOOR SKIN CRACKED 17 INCHES FROM AFT EDGE CUT OUT & 6 INCHES FROM LT SIDE. REPAIRED SKIN IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

CREASE BEAM INNER CHORD CRACKED AT BS 639, STRINGER 17L. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,557 hrs · 57,229 cycles

CHORD CRACKED AT BS 727, STRINGER 18A RT AT FWD LWR FASTENER HOLE. REPAIRED CHORD IAW EA.

Part: PANEL — BROKEN (RT SPOILER) · airframe 68,142 hrs · 56,945 cycles

RT INBD GND SPOILER OTBD ACTUATOR FITTING CASTING BROKEN AT SHELF PANEL ATTACH POINT. REPAIRED PANEL ASSEMBLY IAW SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,890 hrs · 56,778 cycles

RT OVERWING EXTERNAL EMERGENCY LIGHT BULB INOPERATIVE. RELAMPED BULB IAW MM.

Part: ANGLE — CRACKED (RT WING) · airframe 67,890 hrs · 56,778 cycles

RT WING INBD ANGLE CRACKED AT THE AFT END. R & R ANGLE IAW SRM & DRAWING.

Part: COVER — BROKEN (EXIT SIGN) · airframe 67,890 hrs · 56,778 cycles

FWD ENTRY DOOR EMERGENCY EXIT SIGN COVER BROKEN. R & R SIGN ASSEMBLY IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,551 hrs · 56,542 cycles

LT STOW BIN BULLNOSE EMERGENCY LIGHT INOPERATIVE AT ROW 17. R & R LIGHT IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,551 hrs · 56,542 cycles

FUSELAGE FRAME CRACKED AT STATION 500C, BETWEEN STRINGER 19R & STRINGER 22R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,551 hrs · 56,542 cycles

FUSELAGE FRAME CRACKED AT STATION 500B, BETWEEN STRINGER 19R & STRINGER 22R. REPAIRED FRAME IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 66,455 hrs · 55,735 cycles

FWD ENTRY LIGHT COVER FELL OFF. RESECURED FWD ENTRY EXIT LIGHT COVER IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,350 hrs · 55,647 cycles

SKIN CRACKED AT STATION 787+6, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,350 hrs · 55,647 cycles

SKIN CRACKED BETWEEN BS 727 - BS 1016, BETWEEN STRINGER 14L - STRINGER 25R. F. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 66,350 hrs · 55,647 cycles

RT WING NR 4 SLAT CRACKED IN LOWER SKIN. REPAIRED SKIN IAW SRM & DRAWING.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 65,855 hrs · 55,292 cycles

L1 DOOR SLIDE DROPPED OUT OF CONTAINER, STILL SERVICEABLE. RE-INSTALLED SLIDE PER MT.

Part: SIGN — BROKEN (CABIN) · airframe 65,708 hrs · 55,192 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER M/M.

Part: LUG — BROKEN (LT SPOILER) · airframe 65,671 hrs · 55,162 cycles

LEFT WING GROUND SPOILER INBOARD LUG BROKEN. REMOVED AND REPLACED LEFT WING GROUND SPOILER PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,664 hrs · 55,157 cycles

EXTERIOR EMERGENCY LIGHT AFT OF THE AFT SERVICE DOOR INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,664 hrs · 55,157 cycles

EXTERIOR EMERGENCY LIGHT AFT OF THE AFT ENTRY DOOR INOP. REMOVED AND REPLACED BULB PER MM.

Part: HOLDER — UNSECURE (R1 DOOR) · airframe 65,255 hrs · 54,872 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FELL OFF. SECURED HOLDER IAW MM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 65,041 hrs · 54,721 cycles

SERVICE DOOR SKIN HAD CRACKS BELOW OBSERVATION WINDOW. R & R IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,995 hrs · 54,690 cycles

A 1.5 INCH SKIN CRACK BETWEEN 2 EXISTING REPAIRS AT STR 18L, STA 767 + 3. VERIFIED BY HFEC PER PART 6 51-00-00 PROCEED. 23 (D60) REPAIRED PER EA 1-353-21523. REFER TO EA FOR SIGN OFFS. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — DELAMINATED (LE SLAT) · airframe 64,715 hrs · 54,490 cycles

NR 2 SLAT DELAMINATED AT UPPER SURFACE, O/B END. REMOVED AND REPLACED NR 2 SLAT PER AMM.

Part: TAB — DELAMINATED (RT AILERON) · airframe 64,715 hrs · 54,490 cycles

RIGHT WING AILERON TAB OUTBOARD TRAILING EDGE DELAMINATED. REMOVED AND REPLACED RIGHT AILERON TAB.

Part: SKIN — WORN (TE FLAP) · airframe 64,715 hrs · 54,490 cycles

RIGHT WING INBOARD FOREFLAP UPPER SKIN WORN THROUGH NEAR INBOARD END. REMOVED AND REPLACED FLAP.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 63,813 hrs · 53,857 cycles

FORWARD RIGHT EMERGENCY EXIT LIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PACK ASSY PER M/M.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 63,470 hrs · 53,604 cycles

L2 DOOR EMERGENCY EXIT SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (R1 DOOR) · airframe 63,145 hrs · 53,348 cycles

R1 DOOR SKIN CRACKED ON FWD SKIN OF DOOR ABOVE LOWER CUTOUT FOR HINGE. REMOVED & REPLACED SKIN IAW SRM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 63,119 hrs · 53,327 cycles

L1 DOOR EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED LENS PER M/M.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 62,871 hrs · 53,140 cycles

RIGHT WING NR 7 FLIGHT SPOILER ACTUATOR LEAKED. REMOVED AND REPLACED ACTUATOR IAW AMM.

Part: ACTUATOR — LEAKING (LT SPOILER) · airframe 62,871 hrs · 53,140 cycles

LEFT WING NR 2 FLIGHT SPOILER ACTUATOR LEAKED. REMOVED AND REPLACED ACTUATOR IAW AMM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 62,871 hrs · 53,140 cycles

RIGHT WING NR 4 SLAT DELAMINATED ON INBOARD EDGE UPPER SURFACE. REPAIRED NR 4 SLAT IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S22L) · airframe 62,871 hrs · 53,140 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

TIE CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

SUPPORT CLIP CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED CLIP IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED CLIP PER SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

CLIP CRACKED AT BS 348.2, STR 9L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: RIB — CRACKED (LT WING) · airframe 62,871 hrs · 53,140 cycles

LEFT WING RIB AT WBL 198.60 WEB CRACKED BETWEEN STR 5 AND REAR SPAR. REPAIRED WEB IAW EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

CHANNEL CORRODED BETWEEN BS 769 TO BS 773, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,871 hrs · 53,140 cycles

RIGHT WING SKIN CRACKED ON FIXED LEADING EDGE UPPER SURFACE AT WBL 157.0. REPAIRED SKIN IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

CHANNEL CORRODED AT BS 747+5, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

STIFFENER CRACKED AT BS 727, LBL 3.5. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

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

Part: RIB — CRACKED (LT WING) · airframe 62,871 hrs · 53,140 cycles

LEFT WING RIB AT WBL 355 UPPER CHORD CRACKED BETWEEN STR 8 TO STR 9. REPAIRED CHORD IAW EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

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

Part: SUPPORT ANGLE — CRACKED (BS 727 S17L) · airframe 62,871 hrs · 53,140 cycles

SUPPORT ANGLE CRACKED AT BS 727, STR 17L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (BS 847) · airframe 62,871 hrs · 53,140 cycles

CHANNEL CORRODED AT BS 847+12.5, LBL 3. REPAIRED CHANNEL IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

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

Part: CHANNEL — CORRODED (BS 847) · airframe 62,871 hrs · 53,140 cycles

CHANNEL CORRODED AT BS 847+12.5, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (BS 847) · airframe 62,871 hrs · 53,140 cycles

CHANNEL CORRODED AT BS 847+12.5, LBL 12.50. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (BS 847) · airframe 62,871 hrs · 53,140 cycles

CHANNEL CORRODED AT BS 847+12.5, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

SUPPORT ANGLE CRACKED AT BS 727, RBL 3.5. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

KEEL BEAM WEB CRACKED AT BS 706+5, BL 0. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME IAW EA AND EO.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

TIE CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

SHEAR TIE CORRODED AT BS 947.5, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (BS 727D) · airframe 62,871 hrs · 53,140 cycles

CHANNEL CORRODED AT BS 727D+6 , RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: SHEAR TIE — CORRODED (BS 500 S26-27R) · airframe 62,871 hrs · 53,140 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STRINGERS 26 TO 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (BS 727D) · airframe 62,871 hrs · 53,140 cycles

CHANNEL CORRODED AT BS 727D+6, RBL 3. REPAIRED CHANNEL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

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

Part: CHANNEL — CORRODED (BS 847) · airframe 62,871 hrs · 53,140 cycles

CHANNEL CORRODED AT BS 847+12.5, RBL 3. REPAIRED CHANNEL IAW EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

FITTING CRACKED AT BS 727, LBL 45.50. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

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

Part: STRUCTURE — CORRODED (BS 312-344) · airframe 62,871 hrs · 53,140 cycles

RIGHT SIDE INNER CHORD UNDER CORRODED BETWEEN BS 312 TO BS 344. REMOVED AND REPLACED CHORD IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

L2 DOOR FUSELAGE SKIN CRACKED AT CUTOUT FORWARD LOWER CORNER. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,871 hrs · 53,140 cycles

FLOORBEAM WEB CRACKED AT BS 663.75, LBL 24.75. REPAIRED WEB IAW EO AND EA.

Part: SKIN — CRACKED (BS 178 S24L) · airframe 62,871 hrs · 53,140 cycles

SKIN CRACKED AT BS 178+10, STRINGER 24L. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,109 hrs · 54,583 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 61,968 hrs · 52,477 cycles

A FLIGHT ATTENDANT REPORTED SMELL OF SMOKE IN CABIN, CLIMBING THROUGH 10K. GASPER FAN TURNED OFF AND SMELL WENT AWAY. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 61,720 hrs · 52,271 cycles

EEPLS LOOSE BETWEEN ROW 7 TO ROW 8. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,701 hrs · 52,256 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 807+7 TO BS 807+8.2, STR 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,701 hrs · 52,256 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 972, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,701 hrs · 52,256 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 961 TO BS 962, STR 21L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,701 hrs · 52,256 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 767+14 TO BS 767+14.3, STR 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,701 hrs · 52,256 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 787+16 TO BS 787+18, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,701 hrs · 52,256 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 727D+4.25 TO BS 727D+4.65, STR 19L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,701 hrs · 52,256 cycles

DURING SCHEDULED SPV CHECK FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016. REPAIRED WEB IAW SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 61,701 hrs · 52,256 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: FLAP — PUNCTURED (RT WING) · airframe 61,701 hrs · 52,256 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING I/B FORE FLAP PUNCTURED. REPAIRED FORE FLAP IAW SRM.

Part: GIRT BAR — UNSECURE (R1 DOOR) · airframe 61,644 hrs · 52,211 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FELL OFF, SLIDE DID NOT DEPLOY, STILL OPERATIONAL. SECURED GIRT BAR PER MT.

Part: SIGN — MISSING (CABIN) · airframe 61,509 hrs · 52,108 cycles

L1 DOOR EMERGENCY EXIT LIGHT SIGN MISSING. INSTALLED SIGN IAW MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,450 hrs · 52,064 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT AFT CABIN EMERGENCY EXIT LIGHT INOP AT ROW 16. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,256 hrs · 51,138 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 935, STR 22R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 59,676 hrs · 50,696 cycles

DURING SCHEDULED OTS CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,676 hrs · 50,696 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 360, BL 0. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,676 hrs · 50,696 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 360, STR 0. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,673 hrs · 50,695 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 360, BL 0. REPAIRED SKIN PER MM.

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 59,673 hrs · 50,695 cycles

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

Part: BRACKET — CRACKED (EVAC SLIDE) · airframe 59,673 hrs · 50,695 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,460 hrs · 50,543 cycles

DURING SCHEDULED MV2 CHECK, FOUND FRAME CRACKED AT BS 931, STR 23L. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,004 hrs · 50,212 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 58,722 hrs · 50,000 cycles

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

Part: CABLE — LOOSE (EVAC SLIDE) · airframe 58,080 hrs · 49,491 cycles

R2 DOOR EMERGENCY EVAC SLIDE CABLE LOOSE. SECURED CABLE PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 58,080 hrs · 49,491 cycles

R2 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND BEAM CRACKED AT BS 834, RBL 20. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 513 TO BS 514, STR 10L. REPAIRED SKIN PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND CHORD CORRODED ON LOWER CHORD AT BS 227.5, BETWEEN LBL 5 TO RBL 5. REPAIRED CHORD PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 394 TO BS 395, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 43. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 505B.5 TO BS 506B.5, STR 10L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 473 TO BS 476, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 504C TO BS 505C, STR 10L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REMOVED AND REPLACED BEAM PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 20R. REMOVED AND REPLACED CLIP PER SI.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 57,107 hrs · 48,735 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 2L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR ATTACH FITTING CORRODED AT BS 986, LBL 43. REPAIRED FITTING PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 20R. REMOVED AND REPLACED CLIP PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 505A, STR 10R. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 742 TO BS 753 STR 25L. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND UPPER CHORD CRACKED AT BS 178, LBL 24. REMOVED AND REPLACED CHORD PER SRM AND BAC DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REPAIRED SPLICE PER SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 57,107 hrs · 48,735 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR AFT ATTACH FITTING MOUNT PLATE CORRODED. REMOVED AND REPLACED FITTING MOUNT PLATE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,002 hrs · 48,656 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 56,220 hrs · 48,103 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,946 hrs · 47,914 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,946 hrs · 47,914 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 470, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,946 hrs · 47,914 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500 STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,946 hrs · 47,914 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,946 hrs · 47,914 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 470, STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,907 hrs · 47,883 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512C TO 515.5C, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,617 hrs · 47,668 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 757, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,178 hrs · 47,342 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 742, STR 24L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,785 hrs · 47,046 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,785 hrs · 47,046 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2. RELAMPED LIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,238 hrs · 46,640 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,238 hrs · 46,640 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,041 hrs · 45,782 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 10L. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 52,300 hrs · 45,269 cycles

FOUND EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 10 ABC. REPLACED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 52,300 hrs · 45,269 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED BETWEEN BS 326 AND BS 329, LBL 45. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 947 TO BS 1006, RBL 50. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 28R CRACKED AT BS 436. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 7L. REPAIRED FRAME PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 51,569 hrs · 47,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,569 hrs · 44,739 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 520 S9R) · airframe 51,462 hrs · 44,669 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 9R. REPAIRED SKIN PER SRM.

Part: SUPPORT FITTING — CORRODED (RT WING) · airframe 50,413 hrs · 43,914 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG SUPPORT FITTING CORRODED AT BS 685. REPAIRED FITTING PER SWA EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,413 hrs · 43,914 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FITTING — CORRODED (RT MLG) · airframe 50,413 hrs · 43,914 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG WALKING BEAM OUTBOARD FWD STABILIZER FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 50,058 hrs · 43,653 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 50,058 hrs · 43,653 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: SKIN — CRACKED (BS 727E S24R) · airframe 49,990 hrs · 43,604 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 24R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,965 hrs · 43,578 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,835 hrs · 42,717 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 25L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,835 hrs · 42,717 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 746, STR 25L. REPAIRED SKIN PER SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 48,595 hrs · 42,540 cycles

L1 DOOR EVACUATION SLIDE GIRT BAR STOW HOOKS LOOSE. SECURED HOOKS PER MM.

Part: FRAME — CORRODED (BS 807) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 27R. REPAIRED FRAME PER SRM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT ELEVATOR TAB OUTBOARD END DELAMINATED. REPAIRED ELEVATOR TAB PER SRM.

Part: FRAME — CORRODED (BS 767) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (BS 847) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE STUB FRAME CORRODED AT BS 847, STR 13R. REPAIRED FRAME PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CORRODED (BS 747) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, STR 27R. REPAIRED FRAME PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRACKED BETWEEN ROW 16 DEF AND ROW 22 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRACKED BETWEEN ROW 3 ABC AND ROW 10 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 13 ABC. INSTALLED STRIP PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER 16R CRACKED AT BS 492. REPAIRED STRINGER PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT HORIZONTAL STAB RIB CRACKED AT STA 151.75. REMOVED AND REPLACED RIB PER SRM.

Part: FITTING — LOOSE (L1 DOOR) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: FITTING — LOOSE (L1 DOOR) · airframe 48,309 hrs · 42,303 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 47,509 hrs · 41,662 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT WING INBOARD AFT FLAP DELAMINATED AT INBOARD FLAP TRACK. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,509 hrs · 41,662 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT R2 DOOR LOWER HINGE CUTOUT LOWER AFT CORNER CRACKED. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 730E) · airframe 47,509 hrs · 41,662 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 23L. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,131 hrs · 41,367 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 46,776 hrs · 41,097 cycles

AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 46,500 hrs · 40,884 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 11 DEF. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: GATE — CRACKED (R2 DOOR) · airframe 46,500 hrs · 40,884 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR UPPER GATE CRACKED. REMOVED AND REPLACED UPPER GATE PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 46,355 hrs · 40,767 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER CENTER T/E END. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 46,010 hrs · 40,495 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,936 hrs · 40,433 cycles

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

Part: LENS — MISSING (CABIN) · airframe 45,817 hrs · 40,337 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: LAMP — INOPERATIVE (CABIN) · airframe 45,713 hrs · 40,256 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 10 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: HOOK — LOOSE (R1 DOOR GIRT BAR) · airframe 45,713 hrs · 40,256 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD HOOK LOOSE. SECURED FWD GIRT BAR HOOK PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,391 hrs · 39,994 cycles

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT AT AFT SERVICE DOOR STAYED ON WITH POWER OFF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,890 hrs · 39,588 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,731 hrs · 39,456 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 43,749 hrs · 38,690 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR) · airframe 41,560 hrs · 36,916 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIFFICULT TO REMOVE FROM FLOOR FITTINGS. ADJUSTED SLIDE & REMOVED DEBRIS FROM GIRT BAR FITTINGS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,964 hrs · 36,457 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,293 hrs · 35,944 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR CUTOUT AT LOWER FWD CORNER CRACKED. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,293 hrs · 35,944 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 767, LBL 3, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,293 hrs · 35,944 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME ANGLE AT BS 727 + 4, BETWEEN RBL 14 AND RBL 15, CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,293 hrs · 35,944 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH CRACKS ON FRAME AT BS 616, BELOW STRINGERS 17R AND 17L. REPAIRED FRAME SECTIONS PER T1-153-018.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 40,293 hrs · 35,944 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 10 DEF, LOOSE. SECURED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,606 hrs · 35,394 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 750, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 39,469 hrs · 35,281 cycles

L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 39,434 hrs · 35,252 cycles

L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 38,306 hrs · 34,339 cycles

DURING SCHEDULED C3 CHECK, FOUND RT AFT END EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,571 hrs · 33,734 cycles

DURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, LBL 9 TO LBL 11, WL 234. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,333 hrs · 33,541 cycles

DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 518, STRINGER 10R. REPAIRED SKIN PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 37,333 hrs · 33,541 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR LOWER FRAME HINGE CUTOUT RADIUS CRACKED. REPAIRED FRAME PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 35,938 hrs · 32,407 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER AS DOOR WAS OPENED. REINSTALLED SLIDE PER MM.

Part: SEAL — LOOSE (CARGO DOOR) · airframe 34,835 hrs · 31,510 cycles

DIVERSION, DECLARED EMERGENCY. UNABLE TO CONTROL CABIN PRESSURE. REINSTALLED AFT LOWER CORNER SEAL IN AFT CARGO DOOR AND REINSTALLED APU DUCT BOOT CLAMP IN KEEL BEAM PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 32,132 hrs · 29,312 cycles

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

Part: FLOORBEAM — CORRODED (AFT CABIN) · airframe 31,992 hrs · 29,196 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, WL 208 AND LBL 17. REPAIRED FLOORBEAM PER SWA RA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,992 hrs · 29,196 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STR CLIP PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 31,992 hrs · 29,196 cycles

DURING SCHEDULED D CHECK, FOUND NR 4 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 31,992 hrs · 29,196 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, WL 208 AND LBL 45. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,992 hrs · 29,196 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 8R AND 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,992 hrs · 29,196 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, BETWEEN STR 8L AND 9L. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 31,992 hrs · 29,196 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: FRAME — CORRODED (AFT CARGO) · airframe 31,992 hrs · 29,169 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 794, WL 148 AND RBL 8. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,992 hrs · 29,169 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,992 hrs · 29,196 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,992 hrs · 29,196 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS'S 827 AND 907, BETWEEN STR'S 8L AND 9L AND STR'S 8R AND 9R. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FWD CARGO DOOR) · airframe 31,992 hrs · 29,196 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 440, WL 160. REMOVED AND REPLACED CARGO DOOR PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 31,397 hrs · 28,677 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,418 hrs · 27,907 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 525, ABOVE STR 10R. REPAIRED SKIN PER SWA RA AND SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,418 hrs · 27,907 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD, 2 EA VERTICAL BEAM WEBS CRACKED, LBL 17.1 AND RBL 17.1. REMOVED AND REPLACED BOTH WEBS PER SRM.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 27,312 hrs · 25,298 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: DRAIN VALVE — OPEN (LOWER FUSELAGE) · airframe 27,300 hrs · 25,290 cycles

DIVERSION, LT DUAL BLEED LIGHT ILLUMINATED, RIGHT A/C WOULD NOT MAINTAIN CABIN PRESSURE. FOUND NUMEROUS BELLY DRAIN VALVES OPENED. CLEANED AND REPOSITIONED DRAIN VALVES. OPS CHECK GOOD.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 26,954 hrs · 25,018 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING INBD FORE FLAP DELAMINATED ON TOP SURFACE. R&R FORE FLAP PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,245 hrs · 24,431 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CRACK IN WEB AT BS 178 BULKHEAD, WL 201, LBL 6. REPAIRED WEB PER SRM.

Part: SLIDE — DISCHARGED (PAX DOOR) · airframe 24,811 hrs · 23,249 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (COCKPIT WINDOW)

DURING SCHEDULED 1/4D CHECK, FOUND OUTBOARD UPPER CORNER OF L1 COCKPIT WINDOW FRAME CRACKED. REPAIRED FRAME PER SWA RA NR 1-A53-1156.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 6 - LBL 7. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR LOWER HINGE, UPPER FWD CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LT AND RT SIDE CHORDS CRACKED AT LBL AND RBL 26. REPAIRED CHORDS PER SRM..

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 6 AND RBL 7. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED ON UPPER SIDE. REPAIRED FRAME PER SWA RA NR 1-352-0345.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR EXTERNAL SKIN CRACKED AT LOWER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (ROW 17)

EEPLS COVER AT ROW 17 LOOSE. RESECURED COVER PER MM.

Part: SLIDE — DETACHED (PAX DOOR)

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

Part: SKIN — DELAMINATED (RT TE FLAP)

DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED ON LOWER SURFACE. REPAIRED AFT FLAP PER SRM.

Part: PMC — MALFUNCTIONED (NR 2 ENGINE)

DURING CRUISE, AFTER ADJUSTING THROTTLE NR 2 ENGINE N1, N2, EGT AND FUEL FLOW FLUCTUATED FOR APPROX 2 MINS BEFORE ENGINE STABILIZED. PLACED ON MEL NR 73-7. A/C OK FOR CONTINUED SERVICE. PLACARDS INSTALLED. DURING OVERNIGHT MX, REPLACED NR 2 PMC PER M/M, OPS NORMAL.

Part: COVER — BROKEN (CABIN)

DURING WALKAROUND CHECK, FOUND FWD SERVICE DOOR LOWER EMERGENCY LIGHT COVER BROKEN. REPLACED PER BOEING M/M.