N630WN

Part: COOLING FAN — FAULTY (CABIN) · airframe 63,519 hrs · 50,263 cycles

PAX REPORTED FUMES IN CABIN. DIVERTED, AND DECLARED EMERGENCY . R & R COOLING FAN IAW AMM.

Part: SKIN — CRACKED (LT WING) · airframe 63,208 hrs · 50,072 cycles

LT WING L/E THRUST REVERSER DEFLECTOR DOOR HINGE RADIUS CUTOUT CRACKED AT WING STA 196. REPAIRED CUTOUT IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 61,347 hrs · 48,851 cycles

LEFT WING TE CURVED ANGLE, CRACKED AT LOWER EDGE NEAR AILERON, 2ND FROM INBD HINGE, NEAR REAR SPAR STATION 547. R & R ANGLE IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,347 hrs · 48,851 cycles

RIGHT CREASE BEAM, WEB CORRODED AT BS 887+10, NEAR CTR LIGHTENING HOLE. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CORRODED (CABIN) · airframe 61,347 hrs · 48,851 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 867 - 887. R & R WEB IAW SRM & DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 61,347 hrs · 48,851 cycles

L1 DOOR GIRT BAR ATTACH ANGLE CORRODED AT BS 312, LBL 58. R & R ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 61,347 hrs · 48,851 cycles

L1 DOOR FRAME ATTACH ANGLE CRACKED AT BS 348.2, STRINGER 15L. R & R ANGLE IAW DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,347 hrs · 48,851 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN BL 0 & STRINGER 28R. R & R SHEAR TIE IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 61,347 hrs · 48,851 cycles

MAIN LANDING GEAR WW TOP PRESS DECK WEB CRACKED AT BS 665, LBL 40. REPAIRED WEB IAW EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 61,347 hrs · 48,851 cycles

AFT CARGO COMPARTMENT, FRAME CLIP CORRODED AT BS 807, STRINGER 26R. R & R CLIP IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 61,347 hrs · 48,851 cycles

RIGHT HORIZONTAL STABILIZER LE PANEL 9250, CRACKED RIB, 3RD FROM INBD. REPAIRED CHORD IAW SRM & DWG.

Part: COVER — BROKEN (CABIN) · airframe 60,989 hrs · 48,593 cycles

RIGHT EMER EXIT ROW LIGHT COVER BROKEN. R & R COVER IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,486 hrs · 48,220 cycles

EMERGENCY LIGHT BATTERY PACK M1674 INOPERATIVE. R & R BATTERY IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,486 hrs · 48,220 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 60,486 hrs · 48,220 cycles

LEFT WING REAR SPAR TO INTERNAL WALKING BEAM FITTING CRACKED AT RSS 219. R & R FITTING IAW SRM.

Part: SPAR — DAMAGED (LT WING) · airframe 60,486 hrs · 48,220 cycles

LEFT WING UPPER SKIN TO AFT SPAR UPPER CHORD FWD DAMAGED AT RSS 233. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 60,486 hrs · 48,220 cycles

LEFT WING UPPER SKIN AT REAR SPAR AREA CRACKED AT HOLE AT RSS 233. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 60,486 hrs · 48,220 cycles

LEFT WING UPPER SKIN AT REAR SPAR AREA CRACKED AT RSS 253. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 60,486 hrs · 48,220 cycles

LEFT WING UPPER SKIN AT REAR SPAR AREA CRACKED AT RSS 155. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 60,486 hrs · 48,220 cycles

LEFT WING UPPER SKIN AT REAR SPAR AREA CRACKED AT RSS 266. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 60,486 hrs · 48,220 cycles

LEFT WING UPPER SKIN AT REAR SPAR AREA CRACKED AT RSS 237. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 60,486 hrs · 48,220 cycles

LEFT WING UPPER SKIN AT REAR SPAR AREA CRACKED AT RSS 267. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,486 hrs · 48,220 cycles

RIGHT UPPER WING SKIN AT AFT UPPER CHORD CRACKED AT RSS 258. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,486 hrs · 48,220 cycles

RIGHT UPPER WING SKIN AT AFT UPPER CHORD CRACKED AT RSS 222. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,486 hrs · 48,220 cycles

RIGHT UPPER WING SKIN AT AFT UPPER CHORD CRACKED AT RSS 256. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 60,486 hrs · 48,220 cycles

RIGHT WING REAR SPAR WEB CRACKED THROUGH UPPER CHORD ATTACH FASTENER HOLE, RSS 220. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 60,486 hrs · 48,220 cycles

RIGHT WING REAR SPAR WEB CRACKED IN SPAR WEB UPPER CHORD ATTACH FASTENER HOLE RSS 223. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 60,486 hrs · 48,220 cycles

LEFT WING REAR SPAR WEB FASTENER HOLE CRACKED AT RSS 212. REMOVED WEB ASSEMBLY IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 60,486 hrs · 48,220 cycles

RIGHT UPPER WING SKIN AT AFT UPPER CHORD CRACKED AT RSS 200. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,486 hrs · 48,220 cycles

RIGHT UPPER WING SKIN AT AFT UPPER CHORD CRACKED AT RSS 254. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,486 hrs · 48,220 cycles

RIGHT UPPER WING SKIN AT AFT UPPER CHORD CRACKED AT RSS 263. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 60,486 hrs · 48,220 cycles

LEFT WING REAR SPAR WEB FOUND FASTENER HOLE FITTING CRACKED AT RSS 220. REPAIRED FITTING IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 60,486 hrs · 48,220 cycles

RIGHT UPPER WING SKIN AT AFT UPPER CHORD CRACKED AT RSS 253. REPAIRED SKIN IAW EA.

Part: BRACKET — CRACKED (RT WING) · airframe 60,486 hrs · 48,220 cycles

RIGHT WING FIXED TE PANEL FWD OF NR 5 SPOILER, JUST INBD OF ACTUATOR MOUNT STRUCTURE, CLAMP BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: BRACKET — CRACKED (TE FLAP) · airframe 60,486 hrs · 48,220 cycles

LEFT WING NR 3 FLAP FAIRING DOOR SPRING RETAINER BRACKET CRACKED. REPAIRED BRACKET IAW SRM & DWG.

Part: SPAR — CRACKED (RT WING) · airframe 60,485 hrs · 48,220 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED ABOVE INBD UPPER FASTENER OF MLG AFT SUPPORT FITTING. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 60,486 hrs · 48,220 cycles

LEFT WING REAR SPAR UPPER CORD CRACKED. REPAIRED CHORD IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,486 hrs · 48,220 cycles

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

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 60,486 hrs · 48,220 cycles

UPPER & LOWER CHORD CRACKED AT BS 727, STRINGER 18A RT. R & R CHORD IAW EA & DWG.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 60,485 hrs · 48,220 cycles

DECLARED EMER, MCP LOCKUP. 20,000 FEET IN DESCENT AUTOPILOT DISENGAGED & ALL MODES FROZEN. NO TIME TO ATTEMPT MCP RESET BEFORE APPROACH & LANDING. RESET MODE CONTROL PANEL IAW MM.

Part: SKIN — DAMAGED (TE FLAP) · airframe 60,039 hrs · 47,937 cycles

LEFT WING INBD FORE FLAP DAMAGED ON UPPER SURFACE. R & R FORE FLAP IAW AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 59,995 hrs · 47,899 cycles

R1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW SIP & MT.

Part: STRAP — CRACKED (FUSELAGE) · airframe 59,962 hrs · 47,875 cycles

FLOORBEAM STRAP CRACKED AT BS 328, LBL 12. REPAIRED STRAP IAW SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 59,962 hrs · 47,875 cycles

R1 DOOR EDGE FRAME LOWER AFT CORNER AT STOP FITTING CRACKED. R & R DOOR IAW MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 59,736 hrs · 47,729 cycles

RIGHT WING NR 8 SPOILER DELAMINATED. R & R NR 8 SPOILER IAW AMM.

Part: FLAP — DAMAGED (LT WING) · airframe 58,939 hrs · 47,195 cycles

LEFT WING AFT FLAP DAMAGED. R & R AFT FLAP IAW MM.

Part: TIRE — SEPARATED (LT MLG) · airframe 52,938 hrs · 47,195 cycles

DECLARED EMER NR 2 TIRE TREAD SEPARATED. R & R TIRE IAW MM.

Part: PANEL — DELAMINATED (LT SPOILER) · airframe 57,403 hrs · 46,118 cycles

LEFT WING NR 2 FLIGHT SPOILER PANEL HAS DELAMINATION. R & R SPOILER ASSEMBLY IAW MM.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 56,042 hrs · 45,160 cycles

FUMES REPORTED IN CABIN. R & R ACM IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

ANGLE CRACKED BETWEEN BS 380 TO BS 400, BL 0. R & R ANGLE IAW SRM & DRAWING.

Part: PLATE — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

AFT CARGO COMPARTMENT PLATE CRACKED AT BS 794, STRINGER 24R. R & R PLATE IAW SRM & DRAWING.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

SHEAR WEB CRACKED BETWEEN BS 351 TO BS 348.5, BETWEEN STRINGER 17L TO STRINGER 15L. R & R SHEAR WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

ANGLE CRACKED AT BS 663, LBL 24.5. R & R ANGLE IAW SRM & DRAWING.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

FWD PRESSURE CHORD CRACKED AT BS 663, BETWEEN RBL 43 & RBL 44. REPAIRED DECK IAW EO & EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

VERTICAL BEAM WEB CRACKED AT BS 178 PRESSURE BULKHEAD RBL 17.0. REPAIRED WEB IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

STRINGER CRACKED AT BS 494, STRINGER 23R. REPAIRED STRINGER IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

RT SIDE OF NOSE WW STIFFENER CRACKED AT BS 243.7, WL 170. R & R STIFFENER IAW EO & EA.

Part: ANGLE — CRACKED (RT WING) · airframe 55,933 hrs · 45,095 cycles

RT WING TE ANGLE CRACKED ON WBL 204.40. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 55,933 hrs · 45,095 cycles

RT WING OTBD AFT FLAP DELAMINATED ON LOWER SURFACE. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — CRACKED (RT SPOILER) · airframe 55,933 hrs · 45,095 cycles

RT WING NR 6 SPOILER UPPER SURFACED CRACKED. REPAIRED SPOILER IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 55,933 hrs · 45,095 cycles

NR 1 GALLEY EMERGENCY EXIT LENS BROKEN. R & R LENS IAW AMM.

Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 55,933 hrs · 45,095 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

FRAME WEB CRACKED AT BS 492, STRINGER 24R. R & R FRAME IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

RT SIDE OF NLG WW AROUND FASTENER HEAD CRACKED AT STATION 243.7+3, WL 170L. REPAIRED WEB IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

WEB CRACKED BETWEEN BS 320 TO BS 344, LBL 45. R & R WEB IAW SRM & DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

FLOOR BEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 55,933 hrs · 45,095 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75+8.5, RBL 45.5-3. REPAIRED WEB IAW EO & EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 55,933 hrs · 45,095 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75, RBL 24.5-5. REPAIRED WEB IAW EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

FLOOR BEAM WEB CRACKED AT BS 709, RBL 24.8. REPAIRED WEB IAW EO & EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 55,933 hrs · 45,095 cycles

MAIN WHEEL PRESSURE DECK CRACKED AT BS 663.75, LBL 5. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 55,933 hrs · 45,095 cycles

MAIN WHEEL PRESSURE DECK CRACKED AT BS 663.75+1, RBL 45.5-6. REPAIRED WEB IAW EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

FLOOR BEAM UPPER CHORD CRACKED AT BS 663+7, LBL 24.5. REPAIRED CHORD IAW SI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,933 hrs · 45,095 cycles

FLOOR BEAM UPPER CHORD CRACKED AT BS 663.75, RBL 24.8. REPAIRED CHORD IAW EO & EA.

Part: SIGN — INOPERATIVE (CABIN) · airframe 54,917 hrs · 44,339 cycles

FWD SERVICE DOOR EMERGENCY EXIT SIGN LAMP INOP. RELAMPED SIGN IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,912 hrs · 44,338 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: LIGHT — BROKEN (EXTERIOR) · airframe 54,912 hrs · 44,338 cycles

L1 DOOR EXTERNAL EMERGENCY LIGHT BULB BROKEN. RELAMPED IAW AMM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

STRINGER SPLICE CHANNEL CRACKED AT STA 907, STR 4L. R & R CHANNEL IAW SRM AND DWG.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

ATTACH BRACKET FOUND CRACKED AT STA 941, STR 8L. REMOVED AND REPLACED BRACKET IAW SRM & BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 500A+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 4, 6, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1 ,2, 3, 4. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

LEFT BS 787+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 807+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 500B+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 4, 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 380+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 5, 7. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

LEFT BS 807+10 UPPER AFT WINDOW CORNER SKIN CUTOUT CRACKED AT HOLES 3, 6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 4, 5, 6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

LEFT BS 847+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 440+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 4, 9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

LEFT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 500C+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 827+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 3, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 360+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 4, 6, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 847+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 520+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 4, 5, 6, 9, 11, 12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 4, 5, 6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 480+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 380+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 4, 5, 6, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 500C+10 LOWER AFT WINDOW CORNER SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 4, 9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3 ,6, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 3, 4, 5, 6, 7, 9, 10. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 400+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 500B+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

LEFT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 6, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 420+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 4, 5, 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 867+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 4. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 887+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 500+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

LEFT BS 867+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 767+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

LEFT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 3, 6, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

LEFT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 6, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

RIGHT BS 520+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 4, 10, 11, 12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,635 hrs · 44,153 cycles

FUSELAGE SKIN CRACKED AT BS 597+5, STR 9R. REPAIRED SKIN IAW EA.

Part: LUG — BROKEN (RT SPOILER) · airframe 54,173 hrs · 43,817 cycles

RIGHT WING NR 5 GROUND SPOILER OUTBOARD MAIN HINGE LUG BROKEN. REPLACED SPOILER BOARD ASSY PER M/M P/N UNK S/N OFF UNK P/N 65-46452-62A S/N ON WN0153.

Part: LENS — BROKEN (EXIT SIGN) · airframe 54,001 hrs · 43,694 cycles

EMERGENCY EXIT SIGN LENS BROKEN NEXT TO FWD ATTENDANT SEAT. REMOVED AND REPLACED FWD ATTENDANT EMERGENCY EXIT SIGN LIGHT ASSY PER AMM. OPS CHECK NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,001 hrs · 43,694 cycles

FUSELAGE SKIN HAS A CRACK AT STA 903 ABOVE STR 24L. REPAIRED PER EA 1-353-21347.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 53,429 hrs · 43,282 cycles

RIGHT WING NR 5 LEADING EDGE SLAT UPPER TRAILING EDGE WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MT.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 53,429 hrs · 43,282 cycles

RIGHT WING NR 6 LEADING EDGE SLAT UPPER TRAILING EDGE WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MT.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 53,429 hrs · 43,282 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 97 TO STA 99. REPAIRED SKIN IAW SRM.

Part: GUIDE — BROKEN (LE SLAT) · airframe 53,331 hrs · 43,211 cycles

LEFT WING NR 4 SLAT ANTI ICE SPRAY TUBE GUIDE BROKEN. REMOVED AND REPLACED NR 4 SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,974 hrs · 42,932 cycles

SKIN CRACKED AT BS 391, STR 10L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 52,739 hrs · 42,738 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL IN ADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 52,415 hrs · 42,483 cycles

L1 DOOR EEPLS LENS LOOSE. SECURED LENS ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,962 hrs · 42,140 cycles

SKIN CRACKED AT BS 500C +14, STR 10L. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,962 hrs · 42,140 cycles

STRINGER CRACKED AT BS 1002, STR 5R. REPAIRED STRINGER PER SRM.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 25,098 hrs · 14,719 cycles

DIVERSION - CROSSFEED VALVE CB POPPED INFLIGHT CROSSFEED VALVE APPEARD TO FAIL IN OPEN POSITION. RESET CIRCUIT BREAKER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER ER.

Part: COVER — BROKEN (EXIT SIGN) · airframe 51,204 hrs · 41,586 cycles

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

Part: BEAM — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND BEAM CRACKED AT BS 685, RBL 46. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 211.8, STR 9L. REPAIRED SKIN IAW EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 616, STR 17R. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947.5, LBL 53. REPAIRED BEAM IAW EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 19L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD SKIN CRACKED AT BS 1016, LBL 18.32. REPAIRED WEB IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM LOWER CHORD CRACKED AT BS 663.75, RBL 24.5. REPAIRED CHORD IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CRACKED BETWEEN BS 698 TO BS 716, LBL 24.5. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK FOUND, SKIN CRACKED AT BS 520+3, STR 28R. REPAIRED SKIN IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CORRODED AT BS 967, STR 27R. REPAIRED STRINGER IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK FOUND, LONDITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 668.75, LBL 24.5. REPAIRED BEAM IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK FOUND, LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 663.75, LBL 24.5. REPAIRED CHORD IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK FOUND, ATTACHMENT CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 986.5, STR 21R. REMOVED AND REPLACED STRINGER PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 727B, LBL 1.5. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 21R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 27R. R&R SHEAR TIE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,743 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11R. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,743 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. R&R CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,743 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27L TO STR 28L. R&R SHEAR TIE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 328, LBL 28. REPAIRED BEAM IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 928.5, STR 25L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 7L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (CABIN) · airframe 50,993 hrs · 41,434 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 380, STR 26R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: LENS — CRACKED (CABIN) · airframe 50,886 hrs · 41,355 cycles

OVERHEAD EMERGENCY EXIT LIGHTS CRACKED AT ROW 2. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 50,532 hrs · 41,081 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK FOUND, RT OVERWING SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,436 hrs · 41,013 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK FOUND, SHEAR TIE CORRODED AT BS 887, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 907, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 867, STR 27L. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 25R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,836 hrs · 40,550 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT OVERWING EMERGENCY SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 49,836 hrs · 40,550 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,637 hrs · 40,408 cycles

DURING SCHEDULED MV2 CHECK FOUND, FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT CRACKED IN LOWER CORNER. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 49,506 hrs · 40,308 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: SLAT — CRACKED (LT WING) · airframe 49,248 hrs · 40,116 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT CRACKED. REPAIRED SLAT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 46,135 hrs · 37,713 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER EA.

Part: LENS — BROKEN (CABIN) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED BETWEEN BS 500 TO BS 520, BETWEEN STR 8L TO STR 11L. REPAIRED SKIN PER AAR EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR FUSELAGE FRAME CRACKED AT BS 360, STR 11L. REPAIRED FRAME PER BAC DWG.

Part: CONNECTOR — LOOSE (CABIN) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 10 TO ROW 16. SECURED CONNECTOR PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND 178 BULKHEAD VERTICAL BEAM CRACKED AT RBL 5.7. REPAIRED BEAM PER AAR EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND EXTERIOR L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO BAY FRAME CRACKED AT 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER AAR EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND VERTICAL L-ANGLE CRACKED AT BS 639, RBL 46. REMOVED AND REPLACED L-ANGLE PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER EA.

Part: GIRT BAR — LOOSE (EVAC SLIDE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT ASSY LOOSE. SECURED GIRT ASSY PER MT.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE SECTION PER BAC DWG.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR AFT SIDE FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: GIRT BAR — LOOSE (EVAC SLIDE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT MATERIAL LOOSE. REMOVED AND REPLACED GIRT ASSY PER MT.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 37,310 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,912 hrs · 44,338 cycles

FUSELAGE SKIN CRACKED AT BS 516, STR 9L. REPAIRED SKIN IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,528 hrs · 37,260 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 45,528 hrs · 37,260 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 45,297 hrs · 37,099 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 45,005 hrs · 36,890 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 664, LBL 33. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 44,142 hrs · 36,265 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,520 hrs · 35,119 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, LBL 17.5, WL 233. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,520 hrs · 35,119 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, LBL 17.5, WL 227. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,520 hrs · 35,119 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, LBL 17.5 WL 228. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 41,955 hrs · 34,708 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SKIN CRACKED AT LOWER AFT END. REMOVED AND REPLACED L1 DOOR PER MM.

Part: SKIN — CRACKED (BS 513D S10L) · airframe 41,595 hrs · 34,456 cycles

FUSELAGE SKIN CRACKED AT BS 513D, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 41,272 hrs · 34,237 cycles

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

Part: SLIDE — FAILED (R1 DOOR) · airframe 41,077 hrs · 34,088 cycles

DURING SCHEDULED CV CHECK, R1 DOOR EMERGENCY EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 40,874 hrs · 33,926 cycles

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

Part: STRIP — WORN (CABIN) · airframe 40,774 hrs · 33,843 cycles

EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 6 DEF. REMOVED AND REPLACED STRIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,452 hrs · 32,905 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT BS 379, BL 0. REPAIRED SKIN PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,542 hrs · 32,905 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,542 hrs · 32,905 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,542 hrs · 32,905 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,542 hrs · 32,905 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, RBL 10. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,542 hrs · 32,905 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 27 TO STR 26L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,542 hrs · 32,905 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 25R TO STR 25L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,542 hrs · 32,905 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727C, STR 26L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,542 hrs · 32,905 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: FITTING — CRACKED (R2 DOOR GIRT BAR) · airframe 38,607 hrs · 32,190 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CRACKED. REMOVED AND REPLACED FITTING PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 38,382 hrs · 32,024 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 37,784 hrs · 31,550 cycles

DURING SCHEDULED MV3 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 37,723 hrs · 31,502 cycles

EEPLS COVER LOOSE AT ROW 9 ABC. SECURED COVER PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 36,886 hrs · 30,856 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP UPPER AFT SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 35,155 hrs · 29,449 cycles

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

Part: FLOORBEAM — CORRODED (COCKPIT FLOOR) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOORBEAM UPPER CHORD CORRODED AT BS 261, BETWEEN LBL 9 TO RBL 10, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,294 hrs · 28,001 cycles

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

Part: FRAME — CRACKED (BS 616) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65, WL 201. REPAIRED FRAME PER BFG ER.

Part: CREASE BEAM — CORRODED (BS 947-986) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 947.5 TO BS 986.5, WL 208. REPAIRED WEB PER SRM.

Part: FITTING — CORRODED (TAIL) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN LBL 11 TO RBL 11, WL 208. REMOVED AND REPLACED Z-CHORD PER SRM.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 9R. REPAIRED FRAME PER SRM.

Part: DRAG BRACE — CORRODED (VERTICAL STAB) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND VERTICAL STAB LT DRAG BRACE CORRODED AT BOTH ENDS. REMOVED AND REPLACED DRAG BRACE PER SRM.

Part: DRAG BRACE — CORRODED (VERTICAL STAB) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND VERTICAL STAB RT DRAG BRACE CORRODED AT BOTH ENDS. REMOVED AND REPLACED DRAG BRACE PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD T/E FOREFLAP DELAMINATED AT UPPER SURFACE. REPAIRED FOREFLAP PER SRM.

Part: FRAME — CRACKED (BS 492) · airframe 332,941 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 332,941 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT ASSY PER SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 332,941 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR GIRT BAR FLOOR FWD ATTACH BRACKET CORRODED. REMOVED AND REPLACED FLOOR BRACKET PER SRM.

Part: FRAME — CRACKED (BS 480) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (BS 337) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 337, RBL 60, WL 208. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 747) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 380) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 867) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 1 L/E SLAT INBOARD LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE DELAMINATED AT INBD END. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 747) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380) · airframe 33,294 hrs · 28,001 cycles

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

Part: BRACKET — LOOSE (R2 DOOR SLIDE) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE COVER ATTACH BRACKET LOOSE. SECURED BRACKET PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380) · airframe 33,294 hrs · 28,001 cycles

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

Part: FRAME — CRACKED (BS 440) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 480) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 33,294 hrs · 28,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR ATTACH PLATE CORRODED. REMOVED AND REPLACED ATTACH PLATE PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 32,889 hrs · 27,691 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,889 hrs · 27,691 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,465 hrs · 27,368 cycles

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

Part: PANEL — FOD (COCKPIT) · airframe 30,609 hrs · 25,828 cycles

ABORTED TAKEOFF. ALL COCKPIT FWD INSTRUMENT PANEL LIGHTS ILLUMINATED. REMOVED FOD FROM LANDING GEAR INDICATOR LIGHTS PANEL. OPS CHECK GOOD PER MM.

Part: RELAY — FAULTY (COCKPIT) · airframe 30,602 hrs · 25,823 cycles

AIR TURNBACK. ANNUNCIATOR LIGHTS ILLUMINATED ON FWD INSTRUMENT PANEL & INDICATOR LIGHTS ON FMC STAYED ILLUMINATED. ALL LIGHTS CEASED UPON LANDING. REMOVED AND REPLACED MASTER TEST RELAY-R33 PER MM.

Part: MODULE — FAULTY (COCKPIT) · airframe 30,602 hrs · 25,823 cycles

ABORTED TAKEOFF. MULTIPLE LIGHTS ILLUMINATED AT COCKPIT FWD INSTRUMENT PANEL. REMOVED AND REPLACED LT SIDE LIGHT DIMMING MODULE PER MM.

Part: BULB — INSTALLED (EMERGENCY LIGHT) · airframe 30,123 hrs · 25,424 cycles

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 12. REMOVED AND REPLACED BULB PER MM.

Part: SLIDE — OUT OF LIMITS (L2 DOOR) · airframe 29,663 hrs · 25,056 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE IND OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: BOLT — WORN (RT ELEVATOR) · airframe 29,201 hrs · 24,684 cycles

DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT NR 1 HINGE TAB BOLT PER MM.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 29,201 hrs · 24,684 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED RT WING NR 6 L/E SLAT SKIN PER SRM.

Part: ROD — WORN (LT ELEVATOR TAB) · airframe 29,201 hrs · 24,684 cycles

DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR OUTBOARD FWD TAB ROD PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 29,201 hrs · 24,684 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 27,621 hrs · 23,408 cycles

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

Part: INDICATOR — OUT OF LIMITS (SLIDE) · airframe 29,191 hrs · 22,280 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,344 hrs · 21,631 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULBS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,344 hrs · 21,631 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,344 hrs · 21,631 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CORRODED (3 EA) BETWEEN BS 859 AND BS 861, RBL 8, LBL 3 AND LBL 8. REPAIRED FLOORBEAMS PER SWA EA.

Part: MOTOR — FAULTY (NR 2 ENGINE) · airframe 25,275 hrs · 21,572 cycles

AIR TURN BACK, NR 2 ENGINE EGT WENT TO 946 FOR 3 SECONDS. REMOVED AND REPLACED VBV MOTOR, MECHANICS AND SHAFT PER MM.

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 24,905 hrs · 21,267 cycles

DECLARED EMERGENCY, DIVERSION, AFT CARGO FIRE WARNING LIGHT ILLUMINATED, BOTTLES FIRED. REMOVED AND REPLACED BOTH SUPRESSION BOTTLES, CORE FILTERS, SCU, CCU AND ALL AFT CARGO SMOKE DETECTORS PER MM. SYSTEM TEST GOOD WITH NO EVIDENCE OF A FIRE.

Part: TIRE — SEPARATED (RT MLG) · airframe 23,394 hrs · 20,048 cycles

AIR TURNBACK, UNSAFE RT MLG LIGHT AFTER T/O, LOWERED GEAR GOT THREE GREEN LIGHTS. FOUND NR 4 MAIN TIRE RECAP CAME OFF DURING T/O ROLL AND DAMAGED THE INNER/CENTER RT MLG DOOR, NOT ALLOWING GEAR DOOR TO FULLY RETRACT. REMOVED INNER/CENTER DOOR AS PER CDL. REMOVED AND REPLACED NR 4 MLG TIRE & WHEEL ASSY PER MM.

Part: FAN — MALFUNCTIONED (A/C BAY) · airframe 22,988 hrs · 19,733 cycles

DURING FLIGHT A GRINDING NOISE AND BURNING SMELL AT MID CABIN, TURNED RECIRC FAN OFF AND SMELL DISSIPATED. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 20,852 hrs · 18,023 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH CABIN SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 19,948 hrs · 17,280 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLAT — DELAMINATED (LH WING) · airframe 18,190 hrs · 15,850 cycles

DURING SCHEDULED C1 CHECK, FOUND # 2 L/E SLAT OTBD T/E WEDGE DELAMINATED AT UPPER SURFACE. R&R SLAT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 18,071 hrs · 15,754 cycles

FWD ENTRY EMERGENCY EXIT LIGHT COVER LOOSE. R&R EXIT LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,240 hrs · 15,061 cycles

DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND BULKHEAD SIDE CHORD CRACKED AT BS 178, WL 207, LT SIDE. Removed and replaced CHORD PER SWA ACO.

Part: RETAINER — LOOSE (SERVICE DOOR) · airframe 17,158 hrs · 14,988 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,597 hrs · 14,525 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT CABIN. RELAMPED EEPLS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 16,272 hrs · 14,260 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT RT INBOARD LOWER CORNER. REPAIRED AFT FLAP PER SRM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 16,212 hrs · 14,209 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: RETAINER — LOOSE (ESCAPE SLIDE) · airframe 16,212 hrs · 14,209 cycles

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

Part: BULB — INOPERATIVE (CABIN FLOOR) · airframe 15,273 hrs · 13,443 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW 16. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SENSOR — OUT OF ADJ (CARGO DOOR) · airframe 15,081 hrs · 13,282 cycles

AIR TURNBACK, DURING CLIMBOUT, FWD CARGO DOOR LIGHT ILLUMINATED. ADJUSTED SENSOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 14,621 hrs · 12,890 cycles

EEPLS TRACK COVER LOOSE AND LENS MISSING AT ROW 14. RESECURED WIRES, TRACK AND INSTALLED LENS PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 13,902 hrs · 12,259 cycles

FWD ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 13,509 hrs · 11,912 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH FWD ENTRY AND SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED BOTH GIRT ASSY PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 13,429 hrs · 11,843 cycles

FWD SERVICE DOOR EVACUATION SLIDE COVER LOOSE AND PRESS INDICATOR LOW. R&R SLIDE ASSY AND SECURED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,429 hrs · 11,843 cycles

EEPLS INOPERATIVE AT MID CABIN. R&R LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,379 hrs · 11,802 cycles

EEPLS INOPERATIVE AT MID CABIN. R&R BROKEN LIGHT ASSY PER MM.

Part: LIGHT — BROKEN (CABIN)

EEPLS TRACK BROKEN IN SEVERAL PLACES. REPAIRED TRACK COVER ASSY PER MM.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING SCHEDULED BC2 CHECK, FOUND FWD SERVICE DOOR EXTERNAL SKIN CRACKED ABOVE LOWER HINGE CUT-OUT. REPAIRED SKIN PER SRM.