N364SW

Part: SLIDE — LOOSE (R2 DOOR) · airframe 73,241 hrs · 60,514 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,767 hrs · 60,156 cycles

LEFT EMER LIGHT INOPERATIVE AT ROW 21. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,767 hrs · 60,156 cycles

R1 DOOR EXTERNAL EMER LIGHT LAMP INOPERATIVE. RELAMPED LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,767 hrs · 60,156 cycles

R2 DOOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,767 hrs · 60,156 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 23. RELAMPED LIGHT IAW AMM.

Part: ANGLE — CRACKED (LT WING) · airframe 72,207 hrs · 59,737 cycles

LEFT WING INBOARD FLAP, OUTBOARD TRACK, INBOARD CUT OUT LOWER ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 72,207 hrs · 59,737 cycles

RIGHT WING INBOARD AFT FLAP DELAMINATED TRAILING EDGE. R & R AFT FLAP IAW AMM.

Part: LANDING GEAR — FAULTY (LEFT) · airframe 70,949 hrs · 58,766 cycles

UPON LANDING GEAR EXTENSION LT MLG LIGHT REMAINED RED, NOSE & RT GEAR WERE GREEN. CYCLED GEAR & GOT THREE GREEN. R & R LT MLG ASSEMBLY IAW MT.

Part: SKIN — CRACKED (L1 DOOR) · airframe 70,449 hrs · 58,417 cycles

L1 DOOR INNER SKIN CRACKED BELOW THE TORQUE BOX AT LOWER HINGE AREA. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,377 hrs · 58,369 cycles

FUSELAGE SKIN CRACKED AT STATION 443, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 69,702 hrs · 57,901 cycles

LEFT OVERWING EMER EXIT LOWER LIGHT INOPERATIVE. R & R CHARGER IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,507 hrs · 57,769 cycles

AFT RIGHT EMER EXIT LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,896 hrs · 56,623 cycles

FUSELAGE SKIN DAMAGED BETWEEN BS 855 TO BS 890, BETWEEN STRINGER 26R TO STRINGER 27R. REPAIRED SKIN IAW SRM.

Part: BRACKET — DAMAGED (CABIN) · airframe 67,829 hrs · 56,581 cycles

R2 DOOR EMERGENCY EVAC SLIDE FLOOR BRACKET ASSEMBLY HARDWARE DAMAGED. R & R BRACKET ASSEMBLY IAW AMM.

Part: BRACKET — DAMAGED (CABIN) · airframe 67,829 hrs · 56,581 cycles

L2 DOOR EMERGENCY EVAC SLIDE FLOOR BRACKETS ASSEMBLY HARDWARE DAMAGED. R & R BRACKET ASSEMBLY IAW AMM.

Part: ACTUATOR — LEAKING (LT SPOILER) · airframe 67,829 hrs · 56,581 cycles

LT WING NR 2 FLIGHT SPOILER LEAKED. R & R ACTUATOR IAW AMM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

CHANNEL INNER CHORD CRACKED AT BS 348.5 BETWEEN STRINGER 16L TO STRINGER 17L. R & R CHORD IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

SKIN CRACKED AT BS 727+13, LBL 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

SKIN CRACKED BETWEEN BS 727D+8 TO BS 727+13, LBL 1. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

AFT CARGO COMPARTMENT WEB CRACKED BETWEEN BS 927 TO BS 947.5, BL 0. R & R WEB IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

INTERCOSTAL WEB CRACKED AT BS 348.2, STRINGER 16L. R & R WEB IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

STRAP CRACKED BETWEEN BS 348.2 TO BS 351.2, STRINGER 16L. R & R STRAP IAW SRM & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STRINGER 15L. R & R CHANNEL IAW SRM & DRAWING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

INTERCOSTAL WEB CRACKED AT BS 348.2, STRINGER 16L. R & R WEB IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

CHANNEL CORRODED BETWEEN BS 727D TO BS 727E, BL 0. R & R CHANNEL IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

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

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

CHANNEL CRACKED AT BS 727, BETWEEN RBL 3 TO LBL 3. R & R CHANNEL IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FLAP TRACK) · airframe 67,829 hrs · 56,581 cycles

LT WING NR 3 FLAP TRACK INTERNAL AREA STIFFENER CRACKED. R & R STIFFENER IAW SRM & DRAWING.

Part: ATTACH ANGLE — CRACKED (HORIZ STAB) · airframe 67,829 hrs · 56,581 cycles

HORIZONTAL STABILIZER ATTACH ANGLE ON LOWER WEB CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

TIE CLIP CRACKED AT BS 1006, STRINGER 15L. R & R TIE CLIP IAW SRM & DRAWING.

Part: NUT CLIP — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

SPACER NUT CLIP CRACKED AT BS 1006, BETWEEN STRINGER 10L TO STRINGER 11L. R & R CLIP IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

FWD SUPPORT ANGLE CRACKED AT BS 328, LBL 45.6. R & R ANGLE IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

CLIP CRACKED AT BS 344, STRINGER 11R. R & R CLIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

FRAME CRACKED AT BS 500B, BETWEEN STRINGER 20R TO STRINGER 21R. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

AFT SUPPORT ANGLE CRACKED AT BS 328, LBL 45.6. R & R ANGLE IAW SRM & DRAWING.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

FWD ENTRY DOOR CUT OUT REVEAL CRACKED AT BS 348. R & R REVEAL IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 20L TO STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

WEB CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R & R WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

FWD ENTRY DOOR TIE CLIP ANGLE CRACKED AT BS 348.20, STRINGER 15L. R & R ANGLE IAW SRM & DRAWING.

Part: RETAINER — CRACKED (LT WING) · airframe 67,829 hrs · 56,581 cycles

LT WING FIXED TE RETAINER CRACKED AT WBL 183.40. R & R RETAINER IAW SRM & DRAWING.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

L1 DOOR CUTOUT TIE CLIP ANGLE CRACKED AT BS 360, STRINGER 11L. R & R ANGLE IAW SRM & DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

FLOOR BEAM UPPER CHORD CORRODED AT BS 986.5, BETWEEN LBL 5 TO RBL 43. REPAIRED CHORD IAW EO & EA.

Part: ANGLE — CRACKED (RT HORIZ STAB) · airframe 67,829 hrs · 56,581 cycles

RT HORIZONTAL STABILIZER ACCESS PANEL 9226R ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: BRACKET — CRACKED (LT WING) · airframe 67,829 hrs · 56,581 cycles

LT WING FIXED TE BRACKET CRACKED AT WS 531. R & R BRACKET IAW SRM & DRAWING.

Part: WEB — CRACKED (NLG WW) · airframe 67,829 hrs · 56,581 cycles

LT SIDE OF NLG WW WEB CRACKED AT BS. 246.2, WL 169.1. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 67,829 hrs · 56,581 cycles

LT SIDE OF NLG WW WEB CRACKED AT BS 239, WL 169.1. REPAIRED WEB IAW EO & EA.

Part: LENS — BROKEN (CABIN) · airframe 67,829 hrs · 56,581 cycles

AFT LAVATORY WALL EMERGENCY EXIT SIGN LENS BROKEN. R & R LENS IAW AMM.

Part: ACCESS PANEL — CRACKED (RT HORIZ STAB) · airframe 67,829 hrs · 56,581 cycles

RT HORIZONTAL STABILIZER PLATE ACCESS PANEL 9224R CRACKED. R & R PANEL IAW SRM & DRAWING.

Part: PLATE — CORRODED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

AFT GALLEY FLOOR PANEL 2472X GIRT BAR BRACKET CORRODED. R & R PLATE IAW SRM & DRAWING.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 67,829 hrs · 56,581 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

FRAME OUTER CHORD CRACKED AT BS 727, STRINGER 18A LT. R & R CHORD IAW EA.

Part: PANEL — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

CORRUGATED PANEL CRACKED BETWEEN BS 717 TO BS 727 ON MLG BAY. R & R PANEL IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED CHORD IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,829 hrs · 56,581 cycles

SUPPORT ANGLE CRACKED AT BS 663+17. R & R ANGLE IAW SRM & DRAWING.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 65,953 hrs · 55,227 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R&R SLIDE PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 65,271 hrs · 54,733 cycles

RIGHT WING NR 4 SLAT UPPER SURFACE T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER M/M.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 65,271 hrs · 54,733 cycles

R2 DOOR EMERGENCY EVAC SLIDE ATTACHMENT LOOSE. SECURED SLIDE PER M/M.

Part: HYDRAULIC LINE — RUPTURED (HYDRAULIC SYS) · airframe 64,785 hrs · 54,393 cycles

AIR TURNBACK, DECLARED EMERGENCY - HYD B-SYS FAILURE. FOUND B-SYS FLEX LINE ACOUSTIC FILTER & MODULE CHAFED & RUPTURED. REMOVED AND REPLACED LINE PER MM.

Part: ANGLE — CRACKED (RT WING) · airframe 64,683 hrs · 54,315 cycles

RIGHT WING I/B NO-STEP PANEL I/B ANGLE IS CRACKED AT THE AFT END. REMOVED AND REPLACED RIGH WING NO STEP ANGLE PER SRM 51-40-02.

Part: RETAINER — CRACKED (LT WING) · airframe 64,683 hrs · 54,315 cycles

LEFT WING T/E LOWER PANEL SEAL RETAINER CRACKED JUST O/B OF THE NR 1 PYLON. REMOVED AND REPLACED RETAINER IAW SOPM.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 63,771 hrs · 53,666 cycles

AIR TURNBACK -- DURING CRUISE CABIN PRESSURE WAS LOST. NO INDICATION OTHER THAN TAKEOFF WARNING HORN. REMOVED AND REPLACED OUTFLOW VALVE PER MM.

Part: WEB — CRACKED (NLG WW) · airframe 63,600 hrs · 53,542 cycles

LEFT NOSE WHEEL WELL WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,247 hrs · 53,273 cycles

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

Part: FITTING — BROKEN (NR 5 SPOILER) · airframe 62,981 hrs · 53,056 cycles

RIGHT WING NR 5 SPOILER FITTING BROKEN. REMOVED AND REPLACED SPOILER IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 22R TO STR 23R. REMOVED AND REPLACED FRAME IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

WEB CRACKED BETWEEN BS 500C TO BS 500D, STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

BULKHEAD ANGLE CRACKED AT BS 727, BETWEEN LBL 10 AND LBL 19. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,981 hrs · 53,056 cycles

CRACK ON SLAT NR 2 LOWER SURFACE AT LEVEL OF WBL 355 AT LEFT WING. PERFORMED REPAIR ON SLAT NR 2 IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 360, STR 19L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

SKIN CORRODED AT BS 1016, BETWEEN STR 26L TO STR 26R. REPAIRED SKIN IAW ACO AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

FRAME CORRODED AT BS 360, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW EA.

Part: STRUCTURE — CRACKED (LT WING) · airframe 62,981 hrs · 53,056 cycles

LEFT WING UPPER CHORD CRACKED ON UPPER CHORD LOCATED AT WBL 114.00. REPAIRED CHORD IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

ANGLE CRACKED AT BETWEEN BS 887 TO 907, RBL 45.5. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (RT WING) · airframe 62,981 hrs · 53,056 cycles

RIGHT WING UPPER CHORD CRACKED ON UPPER CHORD LOCATED AT WBL 114.00. REPAIRED CHORD IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 907, STR 20R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 727B, STR 22R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 727A, STR. 19L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

WEB ANGLE CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 727C, STR 22R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

PLATE CRACKED AT BS 947.5, BETWEEN STR 25L TO STR 25R. REMOVED AND REPLACED PLATE IAW SRM AND DWG.

Part: WEB — CRACKED (RT WING) · airframe 62,981 hrs · 53,056 cycles

RIGHT WING WEB CRACKED AT WBL 198.6 BETWEEN REAR SPAR AND STR 5. REPAIRED WEB IAW EA AND EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

ANGLE CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED ANGLE IAW SRM & DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

STIFFENERS CORRODED AT BS 1016, BL 0. REPAIRED STIFFENERS IAW ACO AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

SUPPORT ANGLE CRACKED AT BS 540, LBL 1. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

STRINGER CLIP CRACKED AT BS 500D, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 500D, STR 20R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

SUPPORT CLIP CRACKED AT BS 500D, STR 19R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

SHEAR TIE CRACKED AT BS 500D, BETWEEN STR 18R TO STR 19R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 62,981 hrs · 53,056 cycles

LEFT HORIZONTAL STABILIZER STIFFENER CRACKED AT STA 92.70. REMOVED AND REPLACED STIFFENER IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

CORROSION ON CHANNEL AT BS 858 TO BS 861, LBL 3. REPAIRED CHANNEL PER EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 500D, STR 25L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

CHANNEL CORRODED BETWEEN BS 858 TO BS 861, RBL 3. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

ZEE CHANNEL CRACKED BETWEEN BS 492.5 TO BS 500A, STR 26R. REMOVED AND REPLACED ZEE CHANNEL IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

SUPPORT ANGLE CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

FRAME CRACKED AT BS 500D, BETWEEN STR 22R AND STR 23R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

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

Part: STRUCTURE — CRACKED (LT HORIZ STAB) · airframe 62,981 hrs · 53,056 cycles

LEFT HORIZONTAL STABILIZER LOWER CHORD CRACKED AT STA 120.30. REPAIRED CHORD IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 500C, STR 23R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

SUPPORT ANGLE CRACKED AT BS 500B, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

CORROSION ON FRAME AT BS 787, BETWEEN STR 26R & STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 500C, STR 19L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FASTENER — MISSING (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

FRAME FASTENERS MISSING AT BS 420, STR 26R. INSTALLED FASTENERS IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 380, STR 19L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

CHANNEL CORRODED BETWEEN BS 858 TO BS 861, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

FRAME CORRODED AT BS 500D, BETWEEN STR 23L TO STR 24L. REPAIRED FRAME IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

TIE CLIP CRACKED AT BS 500D, STR 23L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

CHANNEL CORRODED BETWEEN BS 858 TO BS 861, RBL 8.10. REPAIRED CHANNEL IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

WEB CRACKED BETWEEN BS 344 TO BS 360, BL 0. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 62,981 hrs · 53,056 cycles

CEILING EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS IAW CMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

R1 DOOR FUSELAGE SKIN CUTOUT CRACKED AT BS 328, STR 17R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

FUSELAGE SKIN CRACKED AT BS 987, STR 7L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,981 hrs · 53,056 cycles

SKIN CRACKED BETWEEN BS 520 TO BS 540, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN IAW EA.

Part: FLAP — DAMAGED (LT WING) · airframe 62,018 hrs · 52,336 cycles

LEFT WING I/B TE AFT FLAP DAMAGED. REMOVED AND REPLACED AFT FLAP PER M/M.

Part: FLAP — DAMAGED (LT WING) · airframe 62,018 hrs · 52,336 cycles

LEFT WING O/B TE AFT FLAP DAMAGED. REMOVED AND REPLACED AFT FLAP IAW M/M.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 61,948 hrs · 52,288 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 638 TO BS 639, LBL 64. REMOVED AND REPLACED WEB IAW DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,948 hrs · 52,288 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME INNER CHORD ANGLE CRACKED AT BS 639, LBL 64. REPAIRED CHORD IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 61,948 hrs · 52,288 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 61,898 hrs · 52,249 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LENS — LOOSE (CABIN) · airframe 61,898 hrs · 52,249 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,898 hrs · 52,249 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: COVER — CRACKED (EXTERIOR) · airframe 61,898 hrs · 52,249 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FWD LAV EXTERIOR EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 61,068 hrs · 51,643 cycles

DURING SCHEDULED CV CHECK, FOUND RT EEPLS LOOSE AT ROW 20. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 61,068 hrs · 51,643 cycles

DURING SCHEDULED CV CHECK, FOUND RT WING AILERON TAB I/B UPPER SURFACE L/E DELAMINATED. REMOVED AND REPLACED TAB ASSY PER MM.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 60,222 hrs · 50,996 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND AFT CARGO DOOR CRACKED ON LOWER T BEAM COMMON TO AFT LOWER STOP FITTING. REMOVED AND REPLACED DOOR PER MM AND EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 60,082 hrs · 50,892 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CASE, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 59,572 hrs · 50,494 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 58,543 hrs · 49,767 cycles

EMERGENCY EXIT NOT ARMED LIGHT MISSING. INSTALLED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 58,377 hrs · 49,643 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LATCH — BROKEN (EVAC SLIDE) · airframe 58,003 hrs · 49,354 cycles

R2 DOOR EMERGENCY EVAC SLIDE FWD FLOOR LATCH BROKEN. REMOVED AND REPLACED LATCH PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,493 hrs · 48,960 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 43.5. REPAIRED BEAM PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,493 hrs · 48,960 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD EEPLS BULB INOP. RELAMPED PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 57,493 hrs · 48,960 cycles

DURING SCHEDULED 18Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,493 hrs · 48,960 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT KEEL BEAM LOWER CHORD LOWER SURFACE CORRODED BETWEEN BS 706 TO BS 727. REPAIRED BEAM PER EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 57,493 hrs · 48,960 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT FWD PRESSURE DECK CRACKED BETWEEN BS 664 TO BS 673, BETWEEN LBL 40 TO LBL 42. REPAIRED WEB PER EA.

Part: FITTING — LOOSE (GIRT BAR) · airframe 57,493 hrs · 48,960 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 57,493 hrs · 48,960 cycles

DURING SCHEDULED 18Y CHECK, FOUND PRESSURE DECK AT O/B EDGE BEAD CRACKED AT BS 664, RBL 40. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,493 hrs · 48,960 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 671, RBL 43.5. REPAIRED FRAME PER ACO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,493 hrs · 48,960 cycles

DURING SCHEDULED 18Y CHECK, FOUND STUB FRAME ANGLE CRACKED AT BS 639, RBL 46. REPAIRED ANGLE PER SRM AND BAC DWG.

Part: CONNECTOR — DIRTY (MLG WW) · airframe 56,898 hrs · 48,490 cycles

AIR TURNBACK / DECLARED EMERGENCY. WHEEL WELL FIRE WARNING LIGHT ILLUMINATED INFLIGHT. DECLARED EMERGENCY - RETURNED TO HOU. CLEANED FIRE WARNING CONNECTORS AT MLG WHEEL WELL PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,436 hrs · 47,450 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,436 hrs · 47,450 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: STRIP — WORN (CABIN) · airframe 55,436 hrs · 47,450 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND EEPLS WORN AT ROW 8 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 54,415 hrs · 46,717 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,433 hrs · 45,292 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 362, STR 4R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER PAE ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BETWEEN BS 500A TO BS 500B, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR FRAME CRACKED AT BS AFT BOTTOM STOP PIN FITTING. REPAIRED FRAME ASSY PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 20R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 520, BETWEEN STR 21R AND STR 22R. REPAIRED SHEAR TIE PER SRM & BAC DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR UPPER HINGE CUTOUT FUSELAGE SKIN CRACKED AT BS 303, WL 258. REPAIRED SKIN PER PAE ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR LOWER HINGE CUTOUT FUSELAGE SKIN CRACKED AT BS 303, WL 238. REPAIRED SKIN PER PAE ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CORRODED BETWEEN RT BS 493 TO BS 500. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 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 52,420 hrs · 45,283 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 54. REPAIRED BEAM PER PAE ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 18R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CORRODED AT BETWEEN RT BS 480 TO BS 492. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 1010, STR 24R. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 54. REMOVED AND REPLACED BEAM PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 986 BETWEEN RBL 50 TO LBL 50, WL 208. REPAIRED BEAM PER PAE ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 380, STR 15L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 24R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,420 hrs · 45,283 cycles

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

Part: STRINGER CLIP — CRACKED (BS 867 S4L) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CORRODED (BS 967 S27R) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 27R CORRODED AT BS 967. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 597 S8L) · airframe 52,420 hrs · 45,283 cycles

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

Part: FLOORBEAM — CORRODED (BS 967) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 30. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CORRODED (BS 947 S25L) · airframe 52,420 hrs · 5,283 cycles

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

Part: STRINGER CLIP — CRACKED (BS 867 S4R) · airframe 54,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 54,420 hrs · 45,283 cycles

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

Part: CREASE BEAM — CORRODED (BS 817) · airframe 54,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 817, LBL 67. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S8L) · airframe 54,420 hrs · 45,283 cycles

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

Part: STRINGER CLIP — CRACKED (BS 827 S4L) · airframe 54,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CRACKED (R2 DOOR) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (BS 787 S8R) · airframe 52,420 hrs · 45,283 cycles

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

Part: FRAME — CRACKED (BS 867 S8R) · airframe 52,420 hrs · 45,283 cycles

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

Part: STRINGER CLIP — CRACKED (BS 400 S8L) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907,STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 867 S9L) · airframe 52,420 hrs · 45,283 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 52,420 hrs · 45,283 cycles

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

Part: FRAME — CRACKED (BS 400 S8L) · airframe 52,420 hrs · 45,283 cycles

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

Part: FRAME — CRACKED (BS 907 S8R) · airframe 52,420 hrs · 45,283 cycles

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

Part: STRINGER CLIP — CRACKED (BS 867 S8L) · airframe 52,420 hrs · 45,283 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 52,420 hrs · 45,283 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,420 hrs · 42,283 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 6. REPAIRED FLOORBEAM PER SRM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 52,101 hrs · 45,052 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EVAC SLIDE PRESS INDICATION LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,770 hrs · 44,819 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,899 hrs · 44,181 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,899 hrs · 44,181 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR LOWER HINGE CUTOUT SKIN CRACKED AT LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,551 hrs · 43,924 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,551 hrs · 43,924 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 744D, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,551 hrs · 43,924 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,551 hrs · 43,924 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 732, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 733A S4R) · airframe 48,677 hrs · 42,079 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733A, STR 4R. REPAIRED SKIN PER ER.

Part: LUG — CORRODED (NR 2 PYLON) · airframe 49,083 hrs · 42,789 cycles

DURING SCHEDULED BRDG CHECK, FOUND NR 2 ENGINE STRUT UPPER LINK FORWARD LUG CORRODED. REPAIRED LUG PER SWA EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,083 hrs · 42,789 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, BL 0. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,083 hrs · 42,789 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,083 hrs · 42,789 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 521, STR 10L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,846 hrs · 42,595 cycles

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

Part: FITTING — CORRODED (LT WING) · airframe 48,508 hrs · 42,341 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LEFT WING AFT MLG STABILIZER FITTING CORRODED. REMOVED AND REPLACED STABILIZER FITTING PER MM.

Part: SUPPORT FITTING — CORRODED (BS 685) · airframe 48,508 hrs · 42,341 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT BS 685 MLG SUPPORT FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: SKIN — CRACKED (BS 727C S18L) · airframe 47,063 hrs · 41,214 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C, STR 18L. REPAIRED SKIN PER SRM.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 47,037 hrs · 41,189 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LIGHT LENS PER MM.

Part: GASPER FAN — MALFUNCTIONED (E&E BAY) · airframe 46,943 hrs · 41,115 cycles

DIVERSION, AT CRUISE FL 340, F/A REPORTED ELECTRICAL FUME ODOR FROM AFT CABIN. NO VISUAL INDICATIONS OF SMOKE OR OVERTEMP, FOUND ODOR REMAINED UNTIL LANDING. ODOR CAUSED BY INOP GASPER FAN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 46,868 hrs · 41,055 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 46,197 hrs · 40,525 cycles

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

Part: SKIN — CRACKED (BS 515D S10R) · airframe 46,095 hrs · 40,439 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SIGN — LOOSE (CABIN) · airframe 45,372 hrs · 39,877 cycles

FWD CABIN RIGHT EMERGENCY EXIT SIGN LOOSE. INSTALLED EXIT SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,230 hrs · 39,754 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,230 hrs · 39,754 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 23L. REPAIRED SKIN PER SRM.

Part: SIGN — LOOSE (CABIN) · airframe 44,850 hrs · 39,473 cycles

OVERWING EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SKIN — CRACKED (BS 520 S12L) · airframe 44,816 hrs · 39,446 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12L. REPAIRED SKIN PER SWA EA.

Part: STRIP — CRACKED (CABIN) · airframe 43,300 hrs · 38,258 cycles

DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT STRIP CRACKED. REMOVED AND REPLACED STRIP PER MM.

Part: GLOWSTRIP — WORN (ROW 8-10) · airframe 43,028 hrs · 38,057 cycles

DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT STRIP WORN FROM ROW 8 TO ROW 10. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — OUT OF LIMITS (R1 DOOR) · airframe 42,539 hrs · 37,638 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATES OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,356 hrs · 37,489 cycles

FUSELAGE SKIN CRACKED AT BS 520, ABOVE STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,356 hrs · 37,489 cycles

FUSELAGE SKIN CRACKED AT BS 522, ABOVE STR 19R. REPAIRED SKIN PER SWA EA.

Part: POST — CRACKED (COCKPIT WINDOW) · airframe 41,391 hrs · 36,681 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED WINDOW POST PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,391 hrs · 36,681 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, BELOW LT CREASE BEAM WEB. REPAIRED FRAME PER TYPICAL REPAIR.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 41,391 hrs · 36,681 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELTFRAME WEB CRACKED AT BS 847, BETWEEN STR 25R TO STR 26R. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 41,391 hrs · 36,681 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 663, LBL 31. REPAIRED BEADED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,391 hrs · 36,681 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, BELOW RT CREASE BEAM WEB. REPAIRED FRAME PER TYPICAL REPAIR.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 41,029 hrs · 36,384 cycles

DURING SCHEDULED RON, L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 & R2 DOORS) · airframe 40,521 hrs · 36,008 cycles

DURING SCHEDULED C2CHECK, FOUND R2 AND L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 AND L2 DOOR EVAC SLIDES PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 40,521 hrs · 36,008 cycles

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

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 40,095 hrs · 35,676 cycles

DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 39,982 hrs · 35,580 cycles

FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 38,754 hrs · 34,604 cycles

R2 DOOR EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,704 hrs · 34,568 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA.

Part: ACTUATOR — CRACKED (LT WING SPOILER) · airframe 37,836 hrs · 33,878 cycles

DURING SCHEDULED RON, FOUND NR 1 GROUND SPOILER HYD ACTUATOR CASING CRACKED. REMOVED AND REPLACED ACTUATOR PER MM.

Part: LENS — MISSING (FWD CABIN) · airframe 34,060 hrs · 30,884 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 34,003 hrs · 30,841 cycles

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

Part: ENGINE — BIRD STRIKE (NR 1) · airframe 33,952 hrs · 30,800 cycles

IN FLT SHUTDOWN, DIVERSION, DECLARED EMERGENCY, DURING TAKEOFF, NR 1 ENG DEVELOPED SEVERE VIBRATION. DIVERTED TO OAK. FOUND FOD TO NR 1 ENG. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB ATTACH FITTING, LT AFT, LT FWD AND RT FWD LUGS CORRODED. REPAIRED LUGS PER BFG ER.

Part: RIB — CRACKED (RT WING) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND RT WING RIB CRACKED AT WBL 135.5, BETWEEN STR 2R AND STR 3R. REPAIRED RIB PER BFG ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED (2 EA), BETWEEN BS 666 AND BS 670 AT RBL 25. REPAIRED FLOORBEAM PER BFG ER.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT ELEVATOR TAB AFT ROD ENDS WORN. REMOVED AND REPLACED ROD ENDS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED (4 EA), BETWEEN BS 662 AND BS 675 AT LBL 25. REPAIRED FLOORBEAMS PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR 8L AND STR 9L, BS 380 AND BS 867. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (2 EA) BETWEEN STR 8R AND STR 9R, BS 360 AND BS 827. REPAIRED FRAMES PER BFG ER.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STABILIZER LOWER RIB CHORD CRACKED AT STA 120.3, 24 AFT OF FWD LOWER SPAR. REMOVED AND REPLACED LOWER RIB CHORD PER SRM.

Part: FLOORBEAM — CORRODED (AFT CABIN) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, WL 208 AND RBL 15. REPAIRED FLOORBEAM PER SWA RA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED (2 EA) AT BIN ATTACH POINTS, BS 360, STR 8R AND 9R AND BS 380, STR 8L AND 9L. REPAIRED FRAMES PER BFG ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT LOWER STOP FITTING, BS 440 AT STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (CRACKED) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 AND RBL 39. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, WL 207 AND RBL 56. REPAIRED FRAME PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 420, WL 208 AND RBL 65. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR'S 13L AND 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 AND LBL 39. REMOVED AND REPLACED FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIES CRACKED (2 EA) AT BS 1040, BETWEEN STR'S 2R AND 3R AND BETWEEN STR'S 2L AND 3L. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,501 hrs · 29,654 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (3 EA), BS 887 AT STR 4L, BS 727A AND STR 25L AND BS 727B AT STR 25R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,218 hrs · 27,799 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT AND RT OUTBOARD CHORD ANGLES CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORD ANGLES PER SWA ACO.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 30,218 hrs · 27,799 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA VERTICAL BEAM WEBS CRACKED, BS 178-184, LBL 17.1 AND RBL 17.1. REMOVED AND REPLACED BOTH VERTICAL WEBS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 30,218 hrs · 27,799 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1 AND WL 182. REPAIRED WEB PER SWA RA.

Part: INDICATOR — FAILED (COCKPIT) · airframe 30,083 hrs · 27,691 cycles

(AIR TURNBACK) DURING FLIGHT STANDBY HORIZON ATTITUDE INDICATOR FAILED (WARNING FLAG AND TUMBLED). REMOVED AND REPLACED STANDBY ATTITUDE HORIZON INDICATOR PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 29,400 hrs · 27,107 cycles

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

Part: BRACKET — LOOSE (SERVICE DOOR) · airframe 27,512 hrs · 25,530 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 26,532 hrs · 24,700 cycles

DURING SCHEDULED C3 CHECK, FOUND RT HORIZ STAB LOWER SURFACE, 7'' FROM ROOT, CRACKED .25 INCH. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 26,532 hrs · 24,700 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED FLAP PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 25,645 hrs · 23,989 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT NR 4 STOP. REPAIRED FRAME PER TI-152-003.

Part: GUSSET — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT LOWER FRAME GUSSET CRACKED. REPAIRED GUSSET PER TI-152-003.

Part: SKIN — DELAMINATED (TRIM TAB)

DURING SCHEDULED 1/4D CHECK, FOUND LT AILERON TRIM TAB DELAMINATED ON OUTBOARD END. REMOVED AND REPLACED TAB ASSY PER MM.

Part: CLIP — CRACK (BS 908)

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED, BS 908, STRINGER 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT OVERWING DOOR. RELAMPED PER MM.

Part: SKIN — DELAMINATED (SPOILER)

DURING SCHEDULED C4 CHECK, FOUND NR 5 GROUND SPOILER UPPER SURFACE DELAMINATED AT EXISTING REPAIR. REMOVED AND REPLACED SPOILER PER MM.

Part: LENS — CRACKED (CABIN)

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY LIGHT LENS CRACKED. REMOVED AND LENS PER MM.

Part: LIGHT — LOOSE (CABIN)

FWD ENTRY DOOR EMERGENCY EXIT LIGHT AND LENS FELL OUT. REPLACED LIGHT AND LENS ASSY PER MM.

Part: INDICATOR — MALFUNCTIONED (COCKPIT)

AIR TURNBACK, AFTER TAKEOFF, NR 2 ENG LOW OIL PRESS LIGHT ILLUMINATED SEVERAL TIMES. OIL PRESS INDICATOR OPERATED NORMAL. FOUND FAULTY NR 2 ENG LOW OIL PRESS LIGHT SOCKET. ALL ENG INDICTORS NORMAL. DEFERRED LIGHT PER MEL.

Part: WINDOW — CRACKED (RT COCKPIT)

CRUISING AT FL280 R2 WINDOW ARCING WAS NOTICED, FOLLOWED BY CRACKING OF OUTER PANE. APPROPRIATE CHECKLIST WAS ACCOMPLISHED. FLIGHT RETURNED TO OAK DUE TO ICING CONDITIONS AT SEA, PDX, GEG. REMOVED AND REPLACED R2 WINDOW ASSY AND WINDOW HEAT CONTROLLER PER BOEING M/M AND OPS CK GOOD. CONTROLLER (P/N 83000-05602), (S/N 7670) 0FF, (S/N 3226) ON.

Part: STRUCTURE — DAMAGED (FWD FUSELAGE)

AIRCRAFT STRUCK BY CONTINENTAL AIRLINES MX TRUCK. DURING INSP FOUND RIGHT SIDE NOSE AREA SKIN DAMAGED. INSPECTED AND FOUND OK FOR MX FERRY FLT TO DAL. DURING WALKAROUND IN DAL DISCOVERED DAMAGE TO AIRCRAFT NOSE GEAR AREA TO INCLUDE LEFT NOSE GEAR DOOR AND LOWER FUSELAGE FWD OF THE NOSE GEAR WHEEL WELL. REPAIRED PER BOEING SRM.

Part: CHARGER — INOPERATIVE (CABIN)

DURING 1/2 D-CHECK, FOUND RT FLOOR TRACK LIGHTS INOP AT BS 530. REPLACED BATTERY PACK CHARGER PER BOEING M/M.

Part: COMPRESSOR BLADE — BIRD STRIKE (NR 1 ENGINE)

EXPERIENCED BIRDSTRIKE TO NR 1 ENGINE DURING CLIMBOUT, ACCOMPANIED BY VIBRATION. AIRCRAFT RETURNED TO SMF AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRDSTIRKE INSPECTION, REPLACED DAMAGED FAN BLADES AND PERFORMED ENGINE RUN PER BOEING M/M.