N352SW

Part: LIGHT — DAMAGED (CABIN) · airframe 79,517 hrs · 67,675 cycles

RIGHT OVERWING LOWER EMER EXIT LIGHT ASSEMBLY DAMAGED. R & R LIGHT ASSEMBLY IAW SWPM.

Part: LENS — LOOSE (CABIN) · airframe 79,261 hrs · 67,474 cycles

CENTER AISLE EMER EXIT LENS COVER LOOSE. SECURED LENS IAW MM.

Part: SPINDLE — DELAMINATED (TE FLAP) · airframe 79,261 hrs · 67,474 cycles

LEFT WING SPINDLE DELAMINATED BETWEEN CLAY & THE MID-FLAP OR CARRIAGE LINK IAW GAP. R & R SPINDLER IAW MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,620 hrs · 67,029 cycles

SKIN CRACKED BETWEEN BS 420+16.75 - 420+17.25, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,620 hrs · 67,029 cycles

SKIN CRACKED AT BS 430 + 8.5, STRINGER 2R. REPAIRED SKIN IAW EA.

Part: DETECTOR — FAULTY (HYDRAULIC SYS) · airframe 78,534 hrs · 66,971 cycles

AIR TURN BACK, UPON DEPARTURE AT 1500 FT, HYDRAULIC SYSTEM AN ELECTRIC LOW PRESSURE LIGHT ILLUMINATED. R & R AN ELECTRIC GND FAULT DETECTOR IAW AMM.

Part: LIGHT — FAULTY (CABIN) · airframe 78,276 hrs · 66,778 cycles

LOWER EMER EXIT LIGHTS FAULTY. R & R LIGHT IAW WDM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 78,193 hrs · 66,716 cycles

R2 DOOR SLIDE LOOSE. SECURED SLIDE IAW MP.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 78,167 hrs · 66,699 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR OUT OF ADJUSTMENT. R & R SLIDE IAW MT.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 77,630 hrs · 66,309 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR AFT BRACKET LOOSE. SECURED BRACKET IAW SRM.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 77,630 hrs · 66,309 cycles

L1 DOOR EMER EVAC SLIDE LINER GIRT BAR BRACKET LOOSE. SECURED BRACKET IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 77,509 hrs · 66,216 cycles

R1 DOOR LOWER FWD SIDE EMER EXIT LIGHT LENS MISSING. R & R LIGHT ASSEMBLY IAW AMM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 76,155 hrs · 65,235 cycles

RIGHT WING NR 7 SPOILER DELAMINATED. R & R SPOILER ASSEMBLY IAW MM.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 76,149 hrs · 65,232 cycles

AFT CARGO DOOR CROSSBEAM D CRACKED LOCATED ON FWD END. REPAIRED CROSSBEAM IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 76,149 hrs · 65,232 cycles

AFT CARGO DOOR AFT END OF CROSSBEAM E CRACKED T CHORD FASTENER HOLE. REPAIRED CROSSBEAM IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 76,149 hrs · 65,232 cycles

LEFT WING FIXED LE SKIN CRACKED LOCATED AT STATION 208.00. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 76,149 hrs · 65,232 cycles

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

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 76,149 hrs · 65,232 cycles

AFT CARGO COMPARTMENT DOOR CROSSBEAM E T-CHORD CRACKED. REPAIRED BEAM IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

STRAP CRACKED BETWEEN BS 312 TO 344 LBL 47. R & R STRAP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

STRINGER CLIP CRACKED AT BS 294.5 STRINGER 23L. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FRAME CRACKED AT BS 336 STRINGER 20L. R & R FRAME IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

WEB CRACKED BETWEEN BS 312 TO 328 RBL 32. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

SUPPORT ANGLE CRACKED AT BS 328 STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

WEB CRACKED BETWEEN BS 312 TO 328 LBL 47. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

CLIP ANGLE CRACKED AT BS 348.2 STRINGER 16L. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FRAME CRACKED AT BS 967 BETWEEN STRINGER 22L TO 23L. R & R FRAME IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FUSELAGE SKIN CRACKED AT STATION 951+3 TO 951+10.5 STRINGER 17L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FUSELAGE SKIN CRACKED AT STATION 951+8 STRINGER 17L. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 BETWEEN STRINGER 16L TO 17L. REPAIRED CHORD IAW EO & EA.

Part: RIB — CRACKED (LT WING) · airframe 76,149 hrs · 65,232 cycles

LEFT WING RIB CRACKED AT LOWER CHORD WBL 135.50 BETWEEN STRINGER 2 & 3. REPAIRED RIB IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

INNER CHORD CRACKED AT BS 348.5 STRINGER 17L. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FUSELAGE SKIN CRACKED AT STATION 951+4 TO 951+10 STRINGER 17L. REPAIRED SKIN IAW EA.

Part: FRAME — BROKEN (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FRAME BROKEN AT BS 727D STRINGER 20R. R & R FRAME IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

BEAM CHORD ANGLE CRACKED AT BS 348.2 STRINGER 17L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

ANGLE CRACKED AT BS 907, BETWEEN STRINGER 1 TO 2L. R & R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 709 LBL 24.5. REPAIRED WEB IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

TIE CLIP CRACKED AT BS 727A STRINGER 26R. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

TIE CLIP CRACKED AT BS 907 STRINGER 1. R & R TIE CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

CLIP CRACKED AT BS 947.5 BETWEEN STRINGER 24R TO 25R. R & R CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

TIE CLIP CRACKED AT BS 947.5 STRINGER 25R. R & R TIE CLIP IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

STRINGER CORRODED AT BS 1006 STRINGER 27L. REPAIRED STRINGER IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 710 LBL 24.5. REPAIRED WEB IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FORWARD CARGO COMPARTMENT SUPPORT ZEE CRACKED AT BS 480+16 STRINGER 26L. REPAIRED SUPPORT ZEE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FRAME CRACKED AT BS 847 BETWEEN STRINGER 1 TO 2L. REPAIRED FRAME IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D STRINGER 19R. R & R GUSSET IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D STRINGER 19L. R & R GUSSET IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360 STRINGER 14L. R & R CHANNEL IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

SUPPORT ANGLE CRACKED AT BS 348.2 STRINGER 16L. R & R ANGLE IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

STRINGER CRACKED AT BS 380 STRINGER 15R. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

TIE CLIP CRACKED AT BS 400 STRINGER 8L. R & R TIE CLIP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

INTERCOSTAL CRACKED AT BS 540, BETWEEN BL 0 & LBL 24.5. R & R INTERCOSTAL IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

SUPPORT ANGLE CRACKED AT BS 348.2 STRINGER 16L. R & R ANGLE IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

STRINGER SPLICE CRACKED AT BS 907 STRINGER 4R. R & R SPLICE IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360 STRINGER 14L. R & R CHANNEL IAW SRM & DWG.

Part: PLATE — CRACKED (LT HORIZ STAB) · airframe 76,149 hrs · 65,232 cycles

LEFT HORIZONTAL STABILIZER ACCESS PANEL 9126 PLATE CRACKED. R & R PLATE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

SEAT TRACK CRACKED AT BS 727B LBL 44.5. REPAIRED SEAT TRACK IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

LONGITUDINAL FLOORBEAM LOWER WEB CRACKED AT BS 717 LBL 0.07. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

WEB CRACKED AT BS 639 AT STRINGER 15L. R & R WEB IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

TIE CLIP CRACKED AT BS 663.75 STRINGER 10R. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FUSELAGE FRAME CRACKED AT STATION 706 STRINGER 11R. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 76,149 hrs · 65,232 cycles

LEFT WING INBD & OTBD ANGLE CRACKED OF STABILIZING LINKS BETWEEN THE MLG BEAM & THE REAR SPAR. R & R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 710.5 LBL 0.07. REPAIRED WEB IAW EA NO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 715.5 LBL 0.07. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707 LBL 24.5. REPAIRED WEB IAW EA.

Part: LIGHT — CRACKED (CABIN) · airframe 76,149 hrs · 65,232 cycles

RIGHT EEPLS CRACKED BETWEEN ROW 3 TO ROW 14. R & R EEPLS IAW AMM.

Part: COVER — DISCONNECTED (CABIN) · airframe 76,149 hrs · 65,232 cycles

AFT GALLEY EMER EXIT COVER DISCONNECTED. RECONNECTED COVER IAW MM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 709.5 BETWEEN BBL 0.07. REPAIRED WEB IAW EA.

Part: LIGHT — CRACKED (CABIN) · airframe 76,149 hrs · 65,232 cycles

LEFT EEPLS CRACKED AT ROW 11. R & R EEPLS IAW AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 675 LBL 24.82. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

FUSELAGE SKIN CRACKED AT BS 420+13 STRINGER 1. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,149 hrs · 65,232 cycles

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

Part: ANGLE — CRACKED (TAILCONE) · airframe 76,149 hrs · 65,232 cycles

TAIL CONE ANGLE CRACKED AT UPPER SURFACE FAIRING APU EXHAUST AREA. R & R ANGLE IAW SRM & DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 76,021 hrs · 65,122 cycles

LEFT WING NR 3 SLAT UPPER SURFACE TE INBD CORNER DELAMINATED. R & R NR 3 SLAT IAW MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 76,021 hrs · 65,122 cycles

LEFT WING NR 2 SLAT UPPER SURFACE TE AT INBD AUXILIARY TRACK DELAMINATED. R & R NR 2 SLAT IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,021 hrs · 65,122 cycles

RIGHT CABIN OVERHEAD BIN BULLNOSE EMER EXIT LIGHT INOPERATIVE AT ROW 8. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,021 hrs · 65,122 cycles

LEFT CABIN OVERHEAD BIN BULLNOSE EMER EXIT LIGHTS INOPERATIVE BETWEEN ROW 6 TO 10. R & R BATTERY PACK IAW MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 76,021 hrs · 65,122 cycles

LEFT WING NR 1 SLAT UPPER SURFACE TE CORNER DELAMINATED. R & R NR 1 SLAT IAW MM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 76,021 hrs · 65,122 cycles

LEFT WING NR 3 SLAT UPPER SURFACE TE INBD CORNER DELAMINATED. R & R NR 3 SLAT IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 76,021 hrs · 65,122 cycles

RIGHT EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 75,517 hrs · 64,722 cycles

RIGHT WING OTBD FLAP NR 8 CARRIAGE SPINDLE CORRODED. R & R SPINDLE ASSEMBLY IAW MM.

Part: BOOT — OUT OF POSITION (AC BAY) · airframe 73,256 hrs · 63,172 cycles

DIVERSION AT FL350 THE CABIN ALT WARNING HORN SOUNDED CABIN ALT APPROXIMATELY 11K EMERGENCY DESCENT - CABIN ALT NEVER EXCEEDED 12K'. HOT AIR SUPPLY DUCT BOOT IN RT A/C BAY FORWARD WALL PARTIALLY OFF FLANGE, LEAKED. R & R LT SUPPLY DUCT CHECK VALVE IAW MM.

Part: ACTUATOR — SHEARED (RT SPOILER) · airframe 72,373 hrs · 62,516 cycles

RIGHT WING NR 5 GROUND SPOILER INBD ACTUATOR ROD END SHEARED. R & R ACTUATOR IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,219 hrs · 62,407 cycles

SKIN ON VERTICAL CHEM-MILL CRACKED AT BS 360, STR 2L. REPAIRED SKIN IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 72,188 hrs · 62,381 cycles

FORWARD ENTRY DOOR LIGHTED EMERGENCY EXIT SIGN MISSING LENS. INSTALLED LENS IAW AMM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 71,761 hrs · 62,072 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED COVER IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,668 hrs · 62,001 cycles

FUSELAGE SKIN CRACKED BS 259.5, STR 23L. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,358 hrs · 61,779 cycles

2 VERTICAL CRACKS ALMOST A JOINING TOTALING 2.875 LONG ON THE FWD GALLEY SERVICE DOOR FRAME OPENING, JUST ABOVE THE FWD UPPER DOOR STOP (MARKED IN RED). VERIFIED BY HFEC PER NDT PART 6 51-00-00 PROCED 23. REPAIRED PER SRM 51-10-02 AND 51-40-0.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,782 hrs · 61,375 cycles

CARGO COMPARTMENT STA 927 BETWEEN STR 27L AND 27R CORRODED ON FRAME FOOT. REMOVED AND REPLACED IAW FRAME SRM AND BAC DWG.

Part: STIFFENER — SEVERED (FUSELAGE) · airframe 70,782 hrs · 61,375 cycles

TRANSFERRED FROM LOG PAGE 8588982, STA 663 AT LBL 6.5, VERTICAL STIFFENER IS SEVERED. REMOVED AND REPLACED STIFFENER IAW BAC DWG 65-45402.

Part: STIFFENER — SEVERED (FUSELAGE) · airframe 70,782 hrs · 61,375 cycles

TRANSFERRED FROM LOG PAGE 8588983, STA 663 AT RBL 6.5 VERTICAL STIFFENER IS SEVERED. REMOVED AND REPLACED STIFFENER IAW BAC DWG 65-45402 AND EA 1-357-7686 REV -, REO G15673 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,782 hrs · 61,375 cycles

AFT SERVICE DOOR CUTOUT CRACKED APPROX 3.5 INCHES HFEC VERIFIED. REMOVED AND REPLACED IAW SKIN SRM, MM, & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,782 hrs · 61,375 cycles

STA 727 CHORD CRACKED BETWEEN LT AND RT KEEL BEAMS AT BL-0 VIEWED PANEL 1508L. REMOVED AND REPLACED PANELS IAW BAC DWG & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,782 hrs · 61,375 cycles

AFT ENTRY DOOR, UPPER HINGE CUTOUT HAS A .25 INCH CRACK FROM THE FORWARD UPPER CORNER. REPAIRED AND FABRICATED REPAIR AT AFT ENTRY DOOR, UPPER HINGE CUTOUT IAW B737-300 SRM 53-60-01, ASSESSED THE REPAIR TO BE A CATEGORY B REPAIR PER MT G53-10-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,761 hrs · 61,362 cycles

R2 DOOR EMERGENCY LIGHTS INOP. SECURED LIGHT PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 70,761 hrs · 61,362 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP AT ROW 19. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CHANNEL — PUNCTURED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

GUSSET CHANNEL PUNCTURED AT BS 440, STR 28R. REPAIRED CHANNEL IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CORRODED AT BS 380, STR 27R. REMOVED AND REPLACED STRINGER PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 380, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 420, STR 28R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

SKIN CRACKED AT BS 440, LBL 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 707,700 hrs · 61,368 cycles

SKIN CRACKED AT BS 440, LBL 5. REMOVED AND REPLACED SKIN IAW SRM AND DWG.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

SUPPORT CHANNEL CRACKED AT BS 787, STR 27R. REMOVED AND REPLACED CHANNEL IAW SRM AND BAC DWG.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 70,770 hrs · 61,368 cycles

SUPPORT CHANNEL CRACKED AT BS 787, STR 27R. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

SUPPORT ANGLE ON INTERCOSTAL CRACKED AT BS 787, STR 27R. REPAIRED ANGLE IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

FRAME CRACKED AT BS 787, RBL 13. REPAIRED FRAME IAW EA.

Part: CONNECTOR — BROKEN (CABIN) · airframe 70,761 hrs · 61,362 cycles

LEFT EMERGENCY EXIT DOOR SIDEWALL LIGHT CONNECTOR BROKEN. REPAIRED CONNECTOR PER SWPM AND MM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

SUPPORT ANGLE CRACKED AT BS 540, STR 24L. REMOVED AND REPLACED ANGLE PER SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

FRAME CRACKED AT BS 312 BETWEEN STR 24 TO STR 25R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

FRAME CRACKED AT BS 312, BETWEEN STR 23 TO STR 24R. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 747, STR 16R. REMOVED AND REPLACED CLIP IAW DWG.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 70,761 hrs · 61,362 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STA 92.7 VERTICAL STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 500B, STR 16R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 400, STR 16R. REMOVED AND REPLACED CLIP IAW DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 500B, STR 16L. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 400A, STR 16L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

SHEAR TIE CRACKED AT BS 500A, BETWEEN STR 15L TO STR 16L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

SHEAR TIE CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

STRINGER CLIP CRACKED AT BS 500, STR 16L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 70,761 hrs · 61,362 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT TRAILING EDGE. REPAIRED SKIN IAW REO AND EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

LEFT CREASE BEAM CORRODED BETWEEN BS 480 TO BS 500. REMOVED AND REPLACED BEAM IAW BAC DWG AND AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 70,760 hrs · 61,362 cycles

RIGHT MAIN CABIN CREASE BEAM CORRODED BETWEEN BS 440 TO BS 460. REMOVED AND REPLACED WEB ASSY IAW BAC DWG.

Part: FRAME — DENTED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

FUSELAGE FRAME DENTED AT BS 767, BETWEEN STR 24R - 25R. REPAIRED FRAME PER EA.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 70,761 hrs · 61,362 cycles

RIGHT VERTICAL STABILIZER LOWER FWD FITTING CHANNEL SPLICE ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

LOWER BULKHEAD CHORD CORRODED AT BS 227.8, BETWEEN BL 0 TO LBL 5. REPAIRED CHORD IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

RIGHT MAIN CABIN CREASE BEAM CORRODED BETWEEN BS 767 TO BS 787. REMOVED AND REPLACED WEB IAW MM, DWG AND SRM.

Part: FRAME — DENTED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

FUSELAGE FRAME DENTED AT BS 747, BETWEEN STR 24R - 25R. REPAIRED FRAME PER EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

Z-CHORD CORRODED AT BS 270, BL 0. REPAIRED "Z" SECTION PER EA.

Part: STRUCTURE — CORRODED (GALLEY DOOR) · airframe 70,761 hrs · 61,362 cycles

MAIN CABIN AFT GALLEY DOOR INNER CHORD CORRODED. REMOVED AND REPLACED CHORD IAW SRM AND BOEING DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

MAIN CABIN T-CAP CORRODED AT STA 986. REMOVED AND REPLACED T-CAP IAW REO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,761 hrs · 61,362 cycles

FRAME CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,053 hrs · 60,817 cycles

SKIN CRACKED AT BS 500D, STR 8R. REPAIRED SKIN PER SRM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 69,921 hrs · 60,719 cycles

AIR TURNBACK/DECLARED EMERGENCY. FLIGHT ATTENDANTS REPORTED FUMES STARTING IN MID CABIN AREA. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,055 hrs · 60,059 cycles

EMERGENCY EXIT BULLNOSE LIGHT AT SEAT ROW 3ABC INOP. RELAMPED PER AMM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 67,613 hrs · 58,942 cycles

DURING SCHEDULED SPV CHECK, FOUND LT STUB BEAM CHORD CRACKED AT BS 616. REMOVED AND REPLACED BEAM IAW DWG AND EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 67,613 hrs · 58,942 cycles

DURING SCHEDULED SPV CHECK, FOUND LT STUB BEAM I/B CHORD CRACKED AT BS 616, BETWEEN STR 14L TO STR 15L. REPAIRED CHORD IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,613 hrs · 58,942 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 23. REMOVED AND REPLACED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,613 hrs · 58,942 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT IAW MM.

Part: MODULE — FAULTY (HYDRAULIC SYS) · airframe 67,405 hrs · 58,777 cycles

AIR TURNBACK, LOSS OF "A" SYSTEM HYDRAULICS, LOW PRESSURE LIGHTS ON ENGINE 1 AND ELEC 2/ NORMAL QTY, LIGHTS CAME ON JUST AS LANDING GEAR RAISED. REMOVED AND REPLACED "A" SYSTEM HYDRAULIC MODULE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,458 hrs · 57,290 cycles

DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — WORN (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN WORN AT BS 860, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — WORN (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN WORN AT BETWEEN BS 867 TO BS 877, BETWEEN STR 2R TO STR 2L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,165 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 23. RELAMPED PER WDM.

Part: FLAP — DELAMINATED (LT WING) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING O/B FORE FLAP O/B LEADING EDGE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 19L TO STR 22L. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BS 499, STR 24R. REPAIRED STRINGER PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT STIFFENER CRACKED AT BS 827. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 24L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT SUPPORT ANGLE CORRODED AT BS 772, STR 26L. REPAIRED ANGLE PER EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT SUPPORT ANGLE CORRODED AT BS 772, STR 26R. REPAIRED ANGLE PER EA.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR FWD UPPER AREA CORRODED. REMOVED AND REPLACED SKIN PER SRM AND BAC DWG.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING O/B MID FLAP I/B CARRIAGE SPINDLE ENCLOSURE CORRODED. REMOVED AND REPLACED SPINDLE ENCLOSURE ASSY PER MM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT SUPPORT ANGLE CORRODED AT BS 772, STR 27L. REPAIRED ANGLE PER EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT SUPPORT ANGLE CORRODED AT BS 772, STR 27R. REPAIRED ANGLE PER EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND EEPLS DAMAGED. REMOVED AND REPLACED EEPLS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,111 hrs · 57,034 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 380, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,166 hrs · 57,072 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,783 hrs · 56,768 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,550 hrs · 56,588 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,550 hrs · 56,588 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,550 hrs · 56,588 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 23. REMOVED AND REPLACED LIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,550 hrs · 56,588 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 64,550 hrs · 56,588 cycles

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

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 64,550 hrs · 56,588 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 64,550 hrs · 56,588 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: LENS — LOOSE (EVAC SLIDE) · airframe 64,352 hrs · 56,429 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — FADED (CABIN) · airframe 64,352 hrs · 56,429 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT AFT GALLEY EEPLS FADED. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,339 hrs · 56,416 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 10. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,836 hrs · 56,060 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT LOWER EEPLS INOP. RELAMPED PER MM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 62,794 hrs · 55,300 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR WEB BEAM NR 8 CRACKED AT LOWER CORNER DOOR STOP FITTING. REMOVED AND REPLACED R1 DOOR PER MM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 62,780 hrs · 55,292 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE HOOK LOOSE. REMOVED AND REPLACED HOOK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,157 hrs · 54,832 cycles

DURING SCHEDULED CV CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 23. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 61,759 hrs · 54,534 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR SLIDE ROLLER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,804 hrs · 53,113 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,730 hrs · 53,061 cycles

FOUND LT EMERGENCY EXIT LIGHT INOP. R&R LIGHT ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,698 hrs · 52,289 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,698 hrs · 52,289 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 56,456 hrs · 50,650 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,171 hrs · 50,420 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 17L CRACKED AT BS 188. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,158 hrs · 50,409 cycles

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

Part: LIGHT — DISCONNECTED (CABIN) · airframe 56,158 hrs · 50,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT 5 DEF. FOUND LIGHT ASSY DISCONNECTED. RECONNECTED LIGHT ASSY PER MM.

Part: KEELBEAM — CORRODED (BS 500D) · airframe 56,158 hrs · 50,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND KEELBEAM CORRODED AT BS 500D, RBL 6.5. REPAIRED CHORD PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 56,158 hrs · 50,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,158 hrs · 50,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 10L CRACKED AT BS 294. REPAIRED STRINGER PER SRM.

Part: BEARING — WORN (ELEVATOR) · airframe 56,158 hrs · 50,409 cycles

DURING SCHEDULED BRDG CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING AND BOLT PER MM.

Part: FRAME — CRACKED (BS 277 S15L) · airframe 56,158 hrs · 50,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 15L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 277 S16R) · airframe 56,158 hrs · 50,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S15R) · airframe 56,158 hrs · 50,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S11L) · airframe 56,158 hrs · 50,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 322 S20L) · airframe 56,158 hrs · 50,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 322, STR 20L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 188 S17R) · airframe 56,158 hrs · 50,409 cycles

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

Part: STRINGER CLIP — CRACKED (BS 344 S11R) · airframe 56,158 hrs · 50,409 cycles

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

Part: STRINGER CLIP — CRACKED (BS 344 S11R) · airframe 56,158 hrs · 50,409 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727C S7R) · airframe 56,158 hrs · 50,409 cycles

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

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: SKIN — CRACKED (L/E SLAT) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 L/E SLAT LOWER SKIN CRACKED AT OUTBOARD AUX TRACK. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 4 L/E SLAT LOWER SKIN CRACKED AT OUTBOARD AUX TRACK. REPAIRED SLAT PER SRM.

Part: SHEAR TIE — CORRODED (BS 360) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 360) · airframe 55,474 hrs · 49,879 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (BS 360 S14R) · airframe 55,474 hrs · 49,879 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 16L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 732A. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: REFLECTOR — CORRODED (EXTERIOR LIGHT) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT REFLECTOR CORRODED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (BS 827 S8R) · airframe 55,474 hrs · 49,878 cycles

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

Part: FRAME — CRACKED (BS 480 S8L) · airframe 55,474 hrs · 49,878 cycles

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

Part: FRAME — CRACKED (BS 500C S8L) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500C S8R) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500B S8R) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500B S8L) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S5R) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 907 S7L) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S8L) · airframe 55,474 hrs · 49,878 cycles

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

Part: STRINGER CLIP — CRACKED (BS 907 S4L) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S5L) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500D S2R) · airframe 55,474 hrs · 49,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500D S5R) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

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

Part: STRINGER CLIP — CRACKED (BS 767 S4R) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S8L) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,474 hrs · 49,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 500C S18L) · airframe 54,738 hrs · 49,321 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 843 S10L) · airframe 53,760 hrs · 48,565 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 843, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 505A S10R) · airframe 53,760 hrs · 48,565 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,085 hrs · 47,321 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT CABIN EMERGECNY EXIT LIGHTS INOP. REMOVED AND REPLACED AFT CABIN BATTERY PACKS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,947 hrs · 46,299 cycles

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

Part: HINGE FITTING — BROKEN (NR 4 SPOILER) · airframe 50,947 hrs · 46,299 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 4 SPOILER OUTBD ACTUATOR ATTACH HINGE FITTING BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: SKIN — CRACKED (BS 516.5) · airframe 50,500 hrs · 45,935 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516.50, STR 13R. REPAIRED SKIN PER SWA EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 50,287 hrs · 45,756 cycles

R1 COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED R1 WINDOW AND HEAT CONTROLLER IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,978 hrs · 45,495 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: BATTERY PACK — FAILED (FWD GALLEY) · airframe 49,959 hrs · 45,470 cycles

DURING SCHEDULED SERVICE CHECK, L1 & R1 DOOR EMERGENCY EXIT SIGNS BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 520) · airframe 49,959 hrs · 45,470 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 49,899 hrs · 45,422 cycles

DURING SCHEDULED A1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 49,008 hrs · 44,698 cycles

DURING SCHEDULED C4 CHECK, FOUND LT & RT OVERWING EMERGENCY EXIT LIGHT LENSES LOOSE. SECURED LIGHT LENSES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,008 hrs · 44,698 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST AFT CUTOUT, BS 378.13, LBL 2.80. REPAIRED SKIN PER SWA EA.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 49,008 hrs · 44,698 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,008 hrs · 44,698 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSLEAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500A + 10, STR 19R. REPAIRED SKIN PER SWA EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, RBL 17.1, WL 230. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM.

Part: LENS — DEFECTIVE (EXTERIOR) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT LENS CLOUDY AFT OF LT EMERGENCY EXIT CUTOUT. REMOVED AND REPLACED LENS PER MM.

Part: LENS — DEFECTIVE (EXTERIOR) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS CLOUDY. REMOVED AND REPLACED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EA LONGITUDINAL FLOORBEAMS CORRODED AT BS 772, RBL 8 & LBL 12. REPAIRED FLOORBEAMS PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 276) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 276, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — ACTIVATED (FUSELAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN OIL CANNED AT BS 460 + 10, STR 14L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 639, JUST BELOW WL 208, LT SIDE. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 5.7, WL 178. REPAIRED WEB PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND KEEL BEAM CORRODED AT BS 788, STR 27R. REPAIRED KEEL BEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 666 & BS 670, RBL 25. REPAIRED BEAM PER SWA EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 22L TO STR 25L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BELT FRAME SHEAR TIE CRACKED AT BS 276, STR 9L TO STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 48,911 hrs · 44,617 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE WEB SUPPORT ANGLE CRACKED AT R1 DOOR CUTOUT, BS 287, STR 9R. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 48,911 hrs · 44,617 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 48,228 hrs · 44,076 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: SLIDE — OUT OF ADJUST (R1,R2 & L1 DOORS) · airframe 48,082 hrs · 43,962 cycles

DURING SCHEDULED C3 CHECK, FOUND R1, R2, L1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1, R2, L1 SLIDES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,082 hrs · 43,962 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 47,493 hrs · 43,534 cycles

FWD EEPLS STRIP LOOSE. SECURED EEPLS STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,115 hrs · 43,254 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,115 hrs · 43,254 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 13L, CRACKED. REPAIRED SKIN PER EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 47,115 hrs · 43,254 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR FRAME CUTOUT ABOVE LOWER DOOR HINGE FITTING, BEAR STRAP CRACKED. REPAIRED BEAR STRAP PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 45,988 hrs · 42,361 cycles

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

Part: ACTUATOR — FAILED (RT MLG) · airframe 45,782 hrs · 42,187 cycles

DIVERSION, AFTER GEAR HANDLE UP, INDICATED UP. AFTER GEAR HANDLE OFF, RT MLG INDICATED DOWN AND LOCKED. GEAR HANDLE DOWN, ALL 3 GEARS INDICATED DOWN AND LOCKED, VISUALLY CHECKED MLG DOWN AND LOCKED. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: UPLOCK SENSOR — MALFUNCTIONED (LT MLG) · airframe 44,713 hrs · 41,310 cycles

AIR TURNBACK, LT MLG (RED) LIGHT FAILED TO EXTINGUISH WITH GEAR IN THE UP POSITION. REMOVED AND REPLACED M988 CARD AND REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,321 hrs · 41,004 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR LOWER HINGE CUTOUT HAS A CRACK PROGRESSING FROM SKIN LAP FWD LOWER RADIUS. REPAIRED PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,307 hrs · 40,990 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,618 hrs · 38,835 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 41,618 hrs · 38,835 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, RBL 40. REPAIRED BEADED WEB PER SWA T1.

Part: HINGE — WORN (LT ELEVATOR) · airframe 41,618 hrs · 38,835 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR OTBD ATTACH HINGE WORN. REMOVED AND REPLACED LT ELEVATOR ATTACH HINGE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 41,310 hrs · 38,586 cycles

DURING SCHEDULED BC4 CHECK, FOUND R2 DOOR ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED R2 DOOR ESCAPE SLIDE PER MM.

Part: LENS — LOOSE (MID CABIN) · airframe 40,341 hrs · 37,801 cycles

DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 39,583 hrs · 37,159 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS LIGHTS INOP (2 EA) JUST AFT OF OVERWING EXITS. REMOVED AND REPLACED EEPLS BATTERY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 39,450 hrs · 37,047 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OTBD AFT T/E FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED LT OTBD AFT T/E FLAP PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 38,593 hrs · 36,382 cycles

DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT ASSY DAMAGED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 38,475 hrs · 36,289 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT T/E INBD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT T/E FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,715 hrs · 35,681 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 25L. REPAIRED SKIN PER SRM.

Part: SPAR — CRACKED (RT HORZ STAB) · airframe 37,715 hrs · 35,681 cycles

DURING SCHEDULED C4 CHECK, FOUND RT HORZ STAB LOWER SURFACE AFT SPAR CRACKED APPROX 3 INCHES FROM INBD END. REPAIRED SPAR PER SRM.

Part: COVER — MISSING (CABIN) · airframe 36,028 hrs · 34,270 cycles

DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY LIGHT COVER MISSING. INSTALLED BULLNOSE COVER PER MM.

Part: UPLOCK SENSOR — INOPERATIVE (LT MLG) · airframe 33,731 hrs · 32,320 cycles

IN FLIGHT, LT MLG IND RED LIGHT ILLUMINATED WITH GEAR RETRACTED. REMOVED AND REPLACED MLG UPLOCK SENSOR PER MM.

Part: LIGHT — INOPERATIVE (ESCAPE SLIDE) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT SLIDE LIGHT INOP. RELAMPED SLIDE LIGHT PER WDM AND MM.

Part: BEAM — CRACKED (CABIN) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 727A, RBL 43, WL 208. REPAIRED BEAM PER ER 00-1041.

Part: STRINGER — CRACKED (CABIN) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND STR 8 RT CRACKED AT BS 727D. REPAIRED STR PER SRM.

Part: FRAME — CRACKED (CABIN) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CRACK AT BS 727D, BIN RAIL RT. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES CRACKED AT BS 907, BS 867 AND BS 440 AT LT BIN RAIL SUPPORTS. REPAIRED FRAMES PER SRM AND ER 00-1003.

Part: SKIN — CRACKED (LT WING AILERON) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND LT AILERON UPPER SKIN CRACKED ALONG INBOARD END 4.5 FROM L/E. REPAIRED AILERON SKIN PER SRM.

Part: BEAM — CORRODED (RT WING) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON RT WING MLG SUPPORT BEAM LOWER SURFACE AROUND HOLES 12 & 21. REPAIRED BEAM PER ER 00-1020.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB L/E HAS CRACKED NR 4 RIB. REMOVED AND REPLACED RIB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND CRACK IN STUB FRAME AT BS 294, WL 208, RBL 58. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: FRAME — CRACKED (CABIN) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND BS 867 FRAME CRACKED AT BIN RAIL SUPPORT RT. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (CABIN) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON WEB, BS 619 - 639, WL 208, LBL 69. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND BS 947 FLOORBEAM UPPER SURFACE CORRODED, LBL 5 TO RBL 5. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND BS 986 FLOORBEAM UPPER SURFACE CORRODED, LBL 45 TO RBL 45. REPAIRED FLOORBEAM PER TI-453-037.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND BS 312 FLOORBEAM CORRODED, BL 0. REPAIRED FLOORBEAM PER SRM.

Part: FITTING — CORRODED (ELEVATOR) · airframe 33,339 hrs · 31,995 cycles

DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB NR 6 ELEVATOR HINGE FITTING HAS FRETTING CORROSION DAMAGE. REPAIRED FITTING PER ACO.

Part: SKIN — CRACK (BS 763)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED, BS 763 AT KEEL BEAM AREA. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (CARGO DOOR)

DURING SCHEDULED C1 CHECK, FOUND AFT CARGO EXTERNAL SKIN CRACKED AROUND HANDLE CUT OUT. REPAIRED SKIN PER RA NR 1-A52-023.

Part: BATTERY PACK — DASCHARGED (CABIN)

EEPLS REMAINS ON WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: SKIN — CRACKED (SERV DOORWAY)

DURING SCHEDULED BC1 CHECK, FOUND AFT SERVICE DOOR FRAME CUTOUT CRACKED APPROX 20. REPAIRED PER SWA RA 1-353-1985.

Part: LAMP — FAILED (ROW 7 & 15)

DURING SCHEDULED BC1 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP AT ROWS 7 AND 15. RELAMPED PER BOEING MM.

Part: LAMP — FAILED (ROW 7)

DURING SCHEDULED BC1 CHECK, FOUND EMERGENCY EGRESS LIGHTS OUT AT ROWS 7 AND 15. RELAMPED AND OP CHECKED PER BOEING M/M.

Part: LIGHT — INOPERATIVE (COCKPIT)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULB PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY TRACK LIGHT INOP ON ROW 15. REMOVED AND REPLACED LIGHT SOCKET PER BOEING MM.

Part: BATTERY PACK — LOOSE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT EGRESS LIGHTING INOP. RESECURED BATTERY PACK AND CHARGED PER BOEING MM.

Part: ANGLE — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED LOWER DOOR LINER ATTACH WEB AT BRACKET FWD CORNER. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 747-767)

DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED TRANSITION ANGLE AT BS 727E TO 747, RBL 22 AND BS 747 TO 767, RBL 22. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (LT WING)

DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED ANGLE LT WING TRAILING EDGE O/B OF NR 3 JACKSCREW FAIRING. REMOVED AND REPLACED PER BOEING SRM.

Part: PUMP — MALFUNCTIONED (A-HYD SYST)

DIVERTED TO PHX, DUE TO A-SYSTEM HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATING. AIRCRAFT LANDED AT PHX WITHOUT INCIDENT. REMOVED AND REPLACED PUMP AND A-SYSTEM PRESSURE MODULE PER M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS IN AFT GALLEY AREA INOP. REPLACED LEFT AFT BATTERY PACK PER BOEING M/M.