N623SW

Part: ANGLE — CRACKED (LT WING) · airframe 65,201 hrs · 51,236 cycles

LEFT WING NR 3 AILERON HINGE ANGLE CRACKED FORWARD OF INBOARD SIDE. REPAIRED THE ANGLE IAW SRM.

Part: COVER — FAULTY (EMERGENCY LIGHT) · airframe 65,201 hrs · 51,236 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT SIGN COVER FAULTY. R & R COVER IAW AMM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 64,873 hrs · 51,017 cycles

AFT CARGO DOOR FRAME AREA LOWER LT SIDE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: LENS — DELAMINATED (EMERGENCY LIGHT) · airframe 64,783 hrs · 50,949 cycles

R1 DOOR EXIT LIGHT LENS DELAMINATED. R & R THE LENS IAW MM.

Part: FAN — FAULTY (CABIN) · airframe 64,452 hrs · 50,731 cycles

ODOR NOTED IN CABIN FROM AIR CONDITIONING SYSTEM WITH LT PACK IN AUTO, RT PACK IN HIGH, ODOR WENT AWAY AFTER RT PACK SET TO AUTO AND RECIRCULATION FAN TO OFF. R & R RECIRCULATION FAN IAW AMM.

Part: LENS — LOOSE (L1 DOOR) · airframe 64,298 hrs · 50,638 cycles

L1 DOOR SLIDE COVER LENS LOOSE. R & R LENS IAW SIP.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 64,298 hrs · 50,638 cycles

R1 DOOR SLIDE, LOWER FLAP OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 63,508 hrs · 50,107 cycles

LEFT FWD EMER LIGHT LENS LOOSE ON CEILING AT ROW 2. R & R LENS IAW AMM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 63,066 hrs · 49,814 cycles

DIVERSION, LT MLG UNSAFE LIGHT CAME ON DURING CLIMB, AFTER LEVER WAS AT OFF POSITION. NOTICEABLE ROLL YAW WAS ENCOUNTERED. R & R DOWNLOCK ACTUATOR IAW MM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 63,066 hrs · 49,814 cycles

DIVERSION, LT MLG UNSAFE LIGHT CAME ON DURING CLIMB, AFTER LEVER WAS AT OFF POSITION. NOTICEABLE ROLL YAW WAS ENCOUNTERED. R & R UPLOCK ACTUATOR IAW MM.

Part: WIRE — BROKEN (COCKPIT) · airframe 63,052 hrs · 49,805 cycles

ON TAKEOFF WITH LG LEVER UP, THE LT MAIN GEAR RED LIGHT STAYED ILLUMINATED. RECYCLED LG, ALL LIGHTS WENT OUT. REPAIRED WIRE IAW SWPM.

Part: FLAP — CRACKED (LT WING) · airframe 62,774 hrs · 49,623 cycles

LEFT WING OTBD FORE FLAP LE CRACKED. R & R FORE FLAP IAW AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 440 - 460. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 770 - 787. REPAIRED WEB IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

STRINGER CORRODED, BETWEEN BS 1006 - 1016, STRINGER 26R. R & R STRINGER IAW SRM & DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

STUB BEAM LOWER CHORD CRACKED AT BS 639 RT FASTENER HOLE. R & R CHORD IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 62,633 hrs · 49,533 cycles

LEFT WING CRACKED NOTED COMMON TO WING SKIN AT TE ROW, BETWEEN RSS 213 - 295. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,633 hrs · 49,533 cycles

LEFT WING REAR SPAR WEB CRACKED, AT FASTENER HOLE COMMON TO UPPER FASTENER ROW TO UPPER SPAR CHORD AT RSS 223, HOLE 5. REPAIRED WEB IAW ER & EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 62,633 hrs · 49,533 cycles

LEFT WING LG BEAM FWD SUPPORT FITTING, CRACKED AT UPPER SPAR CHORD, BETWEEN RSS 223 - 220, BETWEEN HOLE 5 - 8. R & R FITTING IAW ER & EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 62,633 hrs · 49,533 cycles

LEFT WING LG BEAM AFT SUPPORT FITTING, CRACKED AT FASTENER HOLE COMMON TO UPPER FASTENER ROW TO UPPER SPAR CHORD AT RSS 223, HOLE 5. R & R FITTING IAW ER & EA.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 62,633 hrs · 49,533 cycles

RIGHT WING OTBD MID FLAP NR 8 CARRIAGE, A FRAME MOUNTING BOLT HOLES CORRODED. R & R NR 8 CARRIAGE IAW CMM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 62,633 hrs · 49,533 cycles

RIGHT WING OTBD MID FLAP 7, CARRIAGE A FRAME MOUNTING BOLT HOLES CORRODED. REPAIRED MID FLAP IAW CMM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 62,633 hrs · 49,533 cycles

RIGHT WING MLG AFT SUPPORT FITTING CRACKED, ASSOCIATED WITH SPAR CHORD AT RSS 222. REPAIRED FITTING IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,633 hrs · 49,533 cycles

RIGHT WING REAR SPAR WEB CRACKED, BETWEEN RSS 220 - 225. REPAIRED WEB IAW ER & EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

AFT PRESS BULKHEAD WEB CORRODED AT BS 1018, LBL 1. REPAIRED WEB IAW ER & EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

AFT PRESS BULKHEAD, CHANNEL STIFFENER CORRODED AT BS 1017, RBL 0. REPAIRED STIFFENER IAW ER & EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

RIGHT STUB BEAM INNER CHORD CRACKED AT BS 639, AROUND THE BOTTOM FASTENER. REPAIRED CHORD IAW EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

AFT PRESS BULKHEAD WEB CORRODED BS 1016, BETWEEN STRINGER 27L - 27R. REPAIRED WEB IAW ER & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

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

Part: BEAM — CORRODED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

RIGHT KEEL BEAM STRAP CORRODED, BETWEEN BS 727D - 737E, AFT CARGO BILGE ATTACH ANGLE, ON FWD SIDE. REMOVED BEAM IAW ER & EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

AFT CARGO BILGE VHF 3 ANTENNA SUPPORT ANGLE CRACKED LT SIDE, JUST AFT OF ANTENNA CONNECTOR. R & R ANGLE IAW ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

RIGHT FLOORBEAM UPPER T CHORD, BEAM CORRODED ON BS 986, RBL 44. R & R T CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

AFT SIDE FRAME, CORRODED AT BS 907, BETWEEN BL 0 TO LBL 4. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT AILERON) · airframe 62,633 hrs · 49,533 cycles

RIGHT WING AILERON WIPER, WEB SUPPORT ANGLE CRACKED AT RRS 550. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

FRAME WEB CRACKED AT BS 500C, BETWEEN STRINGER 21R - 22R. REPAIRED FRAME IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,633 hrs · 49,533 cycles

LEFT WING UPPER REAR SPAR CHORD CRACKED, BETWEEN RSS 224 - 214. REPAIRED CHORD IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,633 hrs · 49,533 cycles

FRAME WEB CRACKED AT BS 500B, BETWEEN STRINGER 21R - 22R. REPAIRED FRAME IAW ER & EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 62,633 hrs · 49,533 cycles

RIGHT WING NR 8 FLAP TRACK, FAIRING AFT TAIL CONE CRACKED AT FASTENER HOLE OTBD SIDE. R & R FAIRING IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 62,633 hrs · 49,533 cycles

RIGHT WING UPPER REAR SPAR CHORD CRACKED, BETWEEN RSS 224 - 14. REPAIRED CHORD IAW EA & ER.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 62,633 hrs · 49,533 cycles

LEFT WING NR 1 PYLON, OTBD UPPER TE PANEL SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,633 hrs · 49,533 cycles

LEFT WING INBD FORE FLAP, UPPER SURFACE DELAMINATED AT INBD OF OTBD END. REPAIRED FORE FLAP IAW WO.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 62,633 hrs · 49,533 cycles

LEFT WING WIPER WEB SUPPORT ANGLE CRACKED AT RSS 550. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 62,633 hrs · 49,533 cycles

LEFT WING NR 1 PYLON INBD UPPER TE PANEL SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FAIRING — CRACKED (TE FLAP) · airframe 62,633 hrs · 49,533 cycles

LEFT WING NR 2 FLAP TRACK, CANOE FAIRING AFT TAIL CONE CRACKED AT FASTENER HOLES. R & R FAIRING IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 62,628 hrs · 49,532 cycles

RIGHT WING UPPER SKIN CRACKED AT WBL 157, COMING FROM AFT SPAR GOING FWD. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,628 hrs · 49,532 cycles

RIGHT WING UPPER SKIN CRACKED AT WBL 157, COMING FROM AFT SPAR GOING FWD. REPAIRED SKIN IAW EA.

Part: LENS — MISSING (EXIT SIGN) · airframe 62,095 hrs · 49,151 cycles

RIGHT LOWER EMER EXIT SIGN LENS MISSING. INSTALLED LENS IAW SIP.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 61,960 hrs · 49,056 cycles

EMERGENCY BATTERY PACK HOUSING LOCKS INOPERATIVE AT LOCATION M1670. R & R BATTERY IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 61,683 hrs · 48,858 cycles

EXIT SIGN NEXT TO RT OVERWING DOOR LOOSE. SECURED SIGN IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,209 hrs · 48,535 cycles

RIGHT AFT CABIN EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,128 hrs · 48,478 cycles

RIGHT EMER EXIT LIGHT INOPERATIVE AT ROW 1. R & R BATTERY PACK ASSEMBLY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 60,936 hrs · 48,349 cycles

L1 DOOR EMER EXIT LIGHT LENS MISSING. INSTALLED LENS IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 60,432 hrs · 48,028 cycles

FORWARD ENTRY DOOR LOWER EMER LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 60,299 hrs · 47,939 cycles

L1 DOOR INNER SKIN CRACKED AT LOWER HINGE AREA. REPAIRED SKIN IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 60,299 hrs · 47,939 cycles

LEFT EMER EXIT LIGHT LENS NOT SECURED. SECURED IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 60,299 hrs · 47,939 cycles

R2 DOOR EMER EXIT LIGHT LENS LOOSE. R & R LENS IAW MM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 60,299 hrs · 47,939 cycles

L1 DOOR LOWER FRAME CRACKED AT AFT LOWER CORNER. REPAIRED FRAME IAW SRM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 59,849 hrs · 47,662 cycles

FORWARD ENTRY LOWER EXIT SIGN COVER LOOSE. SECURED COVER IAW SIP.

Part: FLAP — DELAMINATED (LT WING) · airframe 59,805 hrs · 47,634 cycles

LEFT WING TE INBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 59,756 hrs · 47,597 cycles

L1 DOOR EXIT LENS COVER MISSING. INSTALLED COVER IAW SIP.

Part: SIGN — BROKEN (CABIN) · airframe 59,593 hrs · 47,475 cycles

FORWARD ENTRY EMER EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 59,202 hrs · 47,205 cycles

RIGHT BULLNOSE EMER LENS BROKEN AT ROW 16. REPAIRED LENS IAW MM.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 59,184 hrs · 47,191 cycles

DIVERSION MCP LOCKED UP IN CRUISE. PERFORMED QRH PROCEDURE RESET & MCP UNLOCKED ON THIRD TRY. LOCKED UP ONCE MORE DURING FLIGHT, UNLOCKED ON FIRST TRY. R & R MODE CONTROL PANEL IAW MM.

Part: CONTAINER — BROKEN (EVAC SLIDE) · airframe 58,500 hrs · 46,717 cycles

R2 DOOR EMER EVAC SLIDE CONTAINER BROKEN. R & R SLIDE IAW MT.

Part: DOOR — CRACKED (KRUEGER FLAP) · airframe 58,491 hrs · 46,712 cycles

RIGHT WING FIXED LE AT KRUGER FLAP SEAL DOOR CRACKED. REPAIRED DOOR IAW EA.

Part: ACTUATOR — CRACKED (LE SLAT) · airframe 58,491 hrs · 46,712 cycles

LEFT WING NR 4 SLAT ACTUATOR ON FIXED LE CRACKED. REPAIRED ACTUATOR IAW SRM.

Part: WEB — CRACKED (RT WING) · airframe 58,491 hrs · 46,712 cycles

RIGHT WING NOSE BEAM CHORD WEB CRACKED AT FSS 267 ABOVE NR 4 SLAT INBD MAIN TRACK. R & R CHORD IAW EA, SRM, & DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 58,489 hrs · 46,711 cycles

NUMBER 4 SLAT UPPER SKIN DELAMINATED. R & R SLAT ASSEMBLY IAW MM.

Part: STRUCTURE — CRACKED (RT WING) · airframe 58,489 hrs · 46,711 cycles

RIGHT WING INBD FIXED LE CRACKED AT STATION 125. REPAIRED LE IAW EA.

Part: CASTING — CRACKED (NR 5 SPOILER) · airframe 58,489 hrs · 46,711 cycles

NUMBER 5 GND SPOILER CASTING BROKEN AT OTBD ACTUATOR MOUNT. R & R SPOILER ASSEMBLY IAW MM.

Part: CASTING — CRACKED (RT SPOILER) · airframe 58,489 hrs · 46,711 cycles

RIGHT INBD GND SPOILER ACTUATOR CASTING CRACKED. REPAIRED CASTING IAW SRM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 57,875 hrs · 46,298 cycles

FWD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. R & R POWER SUPPLY M1675 IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 57,386 hrs · 45,994 cycles

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

Part: LENS — MISSING (CABIN) · airframe 56,895 hrs · 45,675 cycles

AFT EMERGENCY EXIT LENS COVER MISSING. INSTALLED COVER IAW SIP.

Part: RETAINING CLIP — FAILED (R1 DOOR) · airframe 56,767 hrs · 45,576 cycles

R1 DOOR EMERGENCY EVAC SLIDE RETAINER CLIP FOR GIRT BAR STOWAGE FAILED. R & R CLIP IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,646 hrs · 45,478 cycles

RT AFT OVERHEAD BIN EMERGENCY LIGHT INOPERATIVE. SECURED LIGHT IAW WDM & MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 56,646 hrs · 45,478 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: CONNECTOR — BROKEN (CABIN) · airframe 56,646 hrs · 45,478 cycles

G4 EMERGENCY EXIT LIGHT BROKEN CONNECTOR. REPAIRED CONNECTOR IAW SWPM & AMM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 56,646 hrs · 45,478 cycles

CONNECTOR SUPPORT BRACKET CRACKED AT BS 665 RBL 3. R & R BRACKET IAW SRM & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,646 hrs · 45,478 cycles

SHEAR TIE CORRODED AT BS 520, BETWEEN STRINGER 27L & STRINGER 28L. R & R SHEAR TIE IAW SRM & DRAWING.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,646 hrs · 45,478 cycles

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

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,646 hrs · 45,478 cycles

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

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 56,646 hrs · 45,478 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 674.25, LBL 40. REPAIRED WEB IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,646 hrs · 45,478 cycles

FUSELAGE SKIN CRACKED AT BS 520 + 2 LBL 4. REPAIRED SKIN IAW SRM.

Part: WIRE — UNSECURE (CABIN) · airframe 56,641 hrs · 45,477 cycles

LT FORWARD OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT INOPERATIVE AT STATION 430. SECURED GROUND WIRE IAW MM & WDM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,641 hrs · 45,477 cycles

LT WING NR 2 SLAT LE SKIN LOWER SECTION CRACKED AT FASTENER HOLES NEAR ACTUATOR. REPAIRED SKIN IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

STRINGER CRACKED AT STATION 520, STRINGER 8R. REPAIRED STRINGER IAW SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

STRINGER CLIP CRACKED AT STATION 927, STRINGER 6L. R&R CLIP IAW BAC DRAWING & SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 520+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED IN STRINGER AT HOLE NR 5. R&R FORGING IAW BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 500C+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,4,5. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 420+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,5,6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 460+10 LOWER AFT SKIN CUT OUT CRACKED AT HOLES 2,3,4,5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 520+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE 2 - 7. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

LT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 4,5. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 500C+10 LOWER AFT WINDOW SKIN CUT OUT CRACKED AT HOLES 2,4,7. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 500B+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4,12. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 460+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,9,11,12. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

LT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 5 & HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 500A+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,5. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 480+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3 & 4. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

LT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3 & 4. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

LT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,5. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 380+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3,4,5. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

LT BS 827+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 400+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 400+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4,5. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

LT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3,4, 6. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 520+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 5,6,8. REPAIRED SKIN IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

MAIN CABIN FRAME CRACKED AT STATION 277, BETWEEN STRINGER 2L & STRINGER 2R. R&R FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

LT BS 847+10 UPPER AFT WINDOW SKIN CUT OUT CRACKED AT HOLE NR 3,4,5,6. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

LT BS 887+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 4 & HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 500+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 480+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 4 & 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,641 hrs · 45,477 cycles

RT BS 360+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,5,6,10,11. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,391 hrs · 45,288 cycles

FUSELAGE SKIN CRACKED AT BS 787+7, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,391 hrs · 45,288 cycles

FUSELAGE SKIN CRACKED AT BS 827+10, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,391 hrs · 45,288 cycles

FUSELAGE SKIN CRACKED AT BS 767+5, STR 10R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,391 hrs · 45,288 cycles

FUSELAGE SKIN CRACKED AT BS 727C+7, STR 10L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,391 hrs · 45,288 cycles

FUSELAGE SKIN CRACKED AT BS 500D+12, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 55,189 hrs · 44,441 cycles

LEFT WING VERTICAL ANGLE IN BALANCE BAY INBD AND FWD OF NR 2 AILERON HINGE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02.

Part: COVER — CRACKED (CABIN) · airframe 55,189 hrs · 44,441 cycles

EMERGENCY EXIT LIGHT LENS COVER CRACKED, OUTBOARD OF FWD F/A SEAT. REMOVED AND REPLACED PER AMM.

Part: TUBE — CRACKED (LE SLAT) · airframe 55,189 hrs · 44,441 cycles

RIGHT WING NR 4 SLAT SPRAY TUBE CRACKED O/B. REMOVED AND REPLACED PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,170 hrs · 44,429 cycles

FORWARD ENTRY DOOR SLIDE NEEDS TO BE REPOSITIONED IN SLIDE CASE. REPOSITIONED SLIDE. C/W MT 325-61-06.

Part: FITTING — CORRODED (RT WING) · airframe 54,942 hrs · 44,271 cycles

RIGHT WING NR 8 FLAP TRACK REAR SPAR FITTING HAS CORROSION AT O/B HOLE. REMOVED, LOCATED, AND INSTALLED NEW REPLACEMENT IAW SRM 57-20-90, OHM 20-50-03.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,914 hrs · 44,254 cycles

FOUND INDICATION OF CRACKING IN THE LOWER SKIN AT THE LOWER FASTENER ROW OF STR 4L AT BS 867 +10 IN CONFIRMED INDICATION OF CRACK PER 737 NDT MANUAL, PART 6, SUBJECT 53-30-16. REPAIRED PER EA 1-353-21232 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,914 hrs · 44,254 cycles

FOUND INDICATION OF CRACKING IN THE LOWER SKIN AT THE LOWER FASTENER ROW OF STR 4L AT BS 867 +10 IN CONFIRMED INDICATION OF CRACK PER 737 NDT MANUAL, PART 6, SUBJECT 53-30-16. REPAIRED PER EA 1-353-21232.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,914 hrs · 44,254 cycles

SUBSURFACE CRACK INDICATION AT BS 7270 +11 ABOVE STRINGER 10L APPROX 1" LONG. REPAIRED PER EA 1-A53-5808.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,914 hrs · 44,254 cycles

SUBSURFACE CRACK IDICATION AT BS 727D+6 ABOVE STRINGER 10R, APPROX 1" LONG. REPAIRED PER EA 1-A53-5808.

Part: ATTACH FITTING — BROKEN (LT SPOILER) · airframe 54,564 hrs · 44,008 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,278 hrs · 43,812 cycles

FUSELAGE SKIN CRACKED AT BS 727D + 6, STR 4L. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (CABIN) · airframe 54,176 hrs · 43,738 cycles

L1 DOOR LOWER FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,665 hrs · 43,355 cycles

SKIN CRACKED AT BS 727D +10, STR 4R. REPAIRED SKIN PER EA.

Part: STRIP — CRACKED (FUSELAGE) · airframe 55,114 hrs · 44,389 cycles

UPPER PYLON PHENOLIC NUT PLATE STRIP CRACKED (3 LOCATIONS) ALONG AFT EDGE OF PANEL 57710L. REPAIRED UPPER PYLON PHENOLIC NUT PLATE STRIPS PER EA 1-354-1468.

Part: LENS — CRACKED (CABIN) · airframe 53,639 hrs · 43,337 cycles

RIGHT EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 1. REMOVED & REPLACED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 53,127 hrs · 42,926 cycles

RIGHT EEPLS COVER MISSING AT ROW 12. INSTALLED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 52,757 hrs · 42,639 cycles

LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 2. REMOVED AND REPLACED LENS PER M/M.

Part: ADI — FAULTY (E&E BAY) · airframe 52,512 hrs · 42,458 cycles

SHORTLY AFTER TAKEOFF IN LAS, NR 2 ADI COMPUTER FLAG CAME INTO VIEW, FLIGHT DIRECTOR BARS REMAINED IN INITIAL TOGA POSITION THROUGHOUT THE FLIGHT. BETWEEN 19,000 FEET AND 22,000 / FEET, F/O AND CAPTAIN NOTICED AN OZONE SMELL WHICH DISSIPATED. REMOVED AND REPLACED NR 2 ADI PER AMM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 52,250 hrs · 42,266 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER AMM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 52,114 hrs · 42,168 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR PER MM AND MT.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 52,114 hrs · 42,168 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR PER MM AND MT.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 52,063 hrs · 42,137 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,979 hrs · 42,074 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 727B+10, STR 4R. REPAIRED SKIN IAW EA.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 51,841 hrs · 41,973 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,771 hrs · 41,923 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 616, WL 208. REPAIRED CHORD IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT STUB BEAM ASSY CRACKED AT BS 616, WL 208. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 664, LBL 24.5. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 616, RBL 45.5. REPAIRED WEB IAW EO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK FOUND, SKIN CRACKED AT BS 947.5+11, STR 17R. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CRACKED AT BS 296, STR 7R. REPAIRED FRAME IAW EA.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK FOUND, RT WING NR 9 FLIGHT SPOILER LOWER SKIN DELAMINATED. REPAIRED SPOILER IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 986 TO BS 993, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM AND DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING I/B AFT FLAP O/B END DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 360 TO BS 380, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKET CORRODED. REMOVED AND REPLACED BRACKET IAW MM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND INNER CHORD CORRODED BETWEEN BS 914 TO BS 1006, STR 17L. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED BETWEEN BS 847 TO BS 867, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM ATTACHMENT CLIP CRACKED AT BS 639, LBL 45.5. REPAIRED CLIP IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT INNER CHORD CORRODED BETWEEN BS 927 TO BS 1006. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 332.1, STR 14R. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CHANNEL CRACKED BETWEEN BS 312 TO BS 328, LBL 46.0. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDNAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 711, BBL 0.07. REPAIRED BEAM IAW SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,620 hrs · 41,804 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 51,139 hrs · 41,441 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: WINDOW — SPARKS (COCKPIT) · airframe 50,515 hrs · 40,969 cycles

AIR TURNBACK, R2 WINDOW SPARKED HEAVILY IN FLIGHT AFTER TAKEOFF. REMOVED AND REPLACED WINDOW PER MM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 50,003 hrs · 40,577 cycles

AIR TURNBACK/DECLARED EMERGENCY. PASSING FL 220 CABIN ALTITUDE HORN CAME ON UPON DESCENT. UNABLE TO CONTROL OUTFLOW VALVE IN AUTO/ALTERNATE BUT CONTROLLABLE IN MANUAL. REMOVED AND REPLACED OUTFLOW VALVE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,614 hrs · 40,285 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR 27L TO STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,614 hrs · 40,285 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,614 hrs · 40,285 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 807 BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 49,614 hrs · 40,285 cycles

DURING SCHEDULED SPV CHECK, FOUND BUTT STRAP CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REPAIRED STRAP PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,614 hrs · 40,285 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 847, BETWEEN LBL 17 TO LBL 18. REMOVED AND REPLACED FRAME PER SRM.

Part: HOOK — OUT OF ADJUST (L2 DOOR) · airframe 49,578 hrs · 40,255 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED HOOKS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 49,353 hrs · 40,076 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,808 hrs · 39,687 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT MID AFT EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 48,421 hrs · 39,395 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP LOOSE. SECURED CLIP PER SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 48,421 hrs · 39,395 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP LOOSE. SECURED CLIP PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 47,272 hrs · 38,473 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,915 hrs · 38,199 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT EEPLS INOP AT ROW 6. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: SIGN — DAMAGED (CABIN) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT FWD EMERGENCY EXIT SIGN DAMAGED. REMOVED AND REPLACED SIGN PER MM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND SUPPORT FITTING CRACKED AT BS 291, STR 16R. REPAIRED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CHORD CRACKED AT BS 188, BETWEEN WL 207 TO WL 209. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

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

Part: RIB — CRACKED (RT WING) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING, RIB STA 135.5 AFT LOWER CHORD BETWEEN WING STR 2 TO STR 3 CRACKED. REMOVED AND REPLACED RIB CHORD PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8R. REMOVED AND REPLACED CLIP PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 3R. REMOVED AND REPLACED SPLICE PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER DWG.

Part: LIGHT — LOOSE (CABIN) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LOOSE BETWEEN ROW 8 TO ROW 23. SECURED LIGHTS PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT SIDE CREASE BEAM WEB CORRODED BETWEEN BS 403 TO BS 406. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT SIDE CREASE BEAM WEB CORRODED BETWEEN BS 416 TO BS 419. REMOVED AND REPLACED WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT SIDE CREASE BEAM WEB CORRODED BETWEEN BS 506A TO BS 507A. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 45,990 hrs · 37,516 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING T/E OUTBOARD FORE FLAP DELAMINATED AT T/E. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,175 hrs · 36,930 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED BETWEEN BS 863 TO BS 864, STR 3L. REPAIRED SKIN PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 45,175 hrs · 36,930 cycles

L2 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 45,019 hrs · 36,817 cycles

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

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 43,356 hrs · 35,649 cycles

L1 EMERGENCY EXIT DOOR SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.

Part: LENS — PEELING (CABIN) · airframe 42,666 hrs · 35,192 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD AISLE EMERGENCY EXIT LIGHT LENS RED LETTERING PEELING OFF. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 42,531 hrs · 35,086 cycles

FOUND FWD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 41,756 hrs · 34,510 cycles

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

Part: STRINGER CLIP — CRACKED (BS 400 S8R) · airframe 41,734 hrs · 34,494 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S7R) · airframe 41,734 hrs · 34,494 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S7R) · airframe 41,734 hrs · 34,494 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BEARING — WORN (RT ELEVATOR) · airframe 41,734 hrs · 34,494 cycles

DURING SCHEDULED BRDG CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. R&R HORN BEARING PER MM.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 41,734 hrs · 34,494 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: HANDLE — BROKEN (OVERWING DOOR) · airframe 41,734 hrs · 34,494 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR HANDLE BROKEN. REMOVED AND REPLACED DOOR HANDLE PER MM.

Part: STRINGER CLIP — CRACKED (BS 578 S11R) · airframe 41,734 hrs · 34,494 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S8R) · airframe 41,734 hrs · 34,494 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 41,734 hrs · 34,494 cycles

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

Part: FRAME — CRACKED (BS 440 S8L) · airframe 41,734 hrs · 34,494 cycles

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

Part: STRINGER CLIP — CRACKED (BS 578 S11R) · airframe 41,734 hrs · 34,494 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,734 hrs · 34,494 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,734 hrs · 34,494 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,734 hrs · 34,494 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,734 hrs · 34,494 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,734 hrs · 34,494 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,734 hrs · 34,494 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 41,330 hrs · 34,210 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 38,036 hrs · 31,718 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 37,542 hrs · 31,344 cycles

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

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 37,095 hrs · 30,974 cycles

FOUND BULL NOSE EMERGENCY EXIT LIGHT COVER MISSING AT ROW 21 ABC. INSTALLED LIGHT COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 36,081 hrs · 30,192 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 36,081 hrs · 30,192 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB ATTACH FITTING LT & RT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986.5, BETWEEN LBL 35 TO RBL 43. REPAIRED FLOOR BEAM PER BFG ER.

Part: FRAME — CRACKED (BS 440) · airframe 30,342 hrs · 25,635 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING, BS 440, STR 25R. REMOVED AND REPLACED FRAME SECTION IAW SRM.

Part: FRAME — CRACKED (BS 616) · airframe 30,342 hrs · 25,635 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65, WL 200. REPAIRED FRAME IAW BFG ER.

Part: FRAME — CORRODED (BS 794) · airframe 30,342 hrs · 25,635 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT AFT CARGO DOOR CUTOUT, FWD FRAME, BS 794, STR 24R. REMOVED AND REPLACED FRAME SECTION IAW SRM.

Part: SHEAR TIE — CORRODED (BS 500B) · airframe 30,342 hrs · 25,635 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500B, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (BS 500B-500C) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 500B TO BS 500C, RBL 69. REPAIRED CREASE BEAM WEB PER SRM.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 10, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 17, WL 152. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME ANGLE CRACKED AT BS 440, RBL 23. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, RBL 8, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 8, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEB — CRACKED (BS 1015) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR WEB CRACKED AT BS 1015, RBL 39. REPAIRED SHEAR WEB PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,303 hrs · 28,046 cycles

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

Part: CREASE BEAM — CORRODED (BS 370) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 370, RBL 68. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,303 hrs · 28,046 cycles

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

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 460) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 460, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,303 hrs · 28,046 cycles

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

Part: FRAME — CRACKED (BS 747) · airframe 33,303 hrs · 28,046 cycles

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

Part: FRAME — CRACKED (BS 867) · airframe 33,303 hrs · 28,046 cycles

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

Part: FRAME — CRACKED (BS 380) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM.

Part: BRACKET — CRACKED (R2 DOOR SLIDE) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD ATTACH MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM.

Part: FRAME — CRACKED (BS 908) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 908, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 867) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (BS 500-500A) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A, LBL 69. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BS 747) · airframe 33,303 hrs · 28,046 cycles

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

Part: FRAME — CRACKED (BS 787) · airframe 33,303 hrs · 28,046 cycles

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

Part: FRAME — CRACKED (BS 908) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 908, STR 8R. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (BS 908) · airframe 33,303 hrs · 28,046 cycles

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

Part: FRAME — CRACKED (BS 400) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 33,303 hrs · 28,046 cycles

DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STAB L/E RIB CRACKED AT STAB STA 184.7. REMOVED AND REPLACED RIB PER SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,961 hrs · 27,774 cycles

DURING SCHEDULED A2 CHECK, FOUND CABIN EMERGENCY LIGHT INOP AT ROW 12 DEF. RELAMPED LIGHT PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 32,592 hrs · 27,457 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,248 hrs · 27,184 cycles

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 17 ABC. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 & R2 DOOR) · airframe 31,354 hrs · 26,451 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 29,477 hrs · 25,120 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,739 hrs · 23,581 cycles

DURING SCHEDULED A2 CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT SIGN AND BOTH RT AND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AT MID CABIN LT SIDE.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 26,599 hrs · 22,685 cycles

DURING SCHEDULED C2 CHECK, FOUND DELAMINATION AT RT WING O/B FORE FLAP UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE BOTTLE) · airframe 25,193 hrs · 21,559 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: CLIP — LOOSE (L1 DOOR) · airframe 23,734 hrs · 20,426 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR CLIP HOOK LOOSE. SECURED CLIP HOOK PER MM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 21,888 hrs · 18,917 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED GIRT BAR CABLE PER MM.

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 21,634 hrs · 18,699 cycles

DURING SCHEDULED RON, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 21,369 hrs · 18,479 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH INBD AND OTBD HINGE BUSHINGS PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 20,674 hrs · 17,893 cycles

EEPLS DAMAGED AT ROWS 7, 8 AND 9. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: BRACKET — LOOSE (FWD SVC DOOR) · airframe 20,148 hrs · 17,476 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP BRACKETS LOOSE. TIGHTENED BRACKETS PER MM.

Part: SLIDE — OUT OF ADJ (CABIN DOOR) · airframe 20,148 hrs · 17,476 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 19,179 hrs · 16,672 cycles

DURING SCHEDULED BC2 CHECK, FOUND KEEL BEAM CRACKED 1.5 INCH LONG RT MLG WW AFT SIDE. REPAIRED KEEL BEAM PER SWA TI-153-009.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 17,776 hrs · 15,465 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRES IND OUT OF LIMITS. R&R EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 17,776 hrs · 15,465 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRES IND OUT OF LIMITS. R&R EMERGENCY EVAC SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 17,438 hrs · 15,188 cycles

RT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED EXIT LIGHT PER MM.

Part: SKIN — DELAMINATED (LT T/E FLAP) · airframe 17,298 hrs · 15,073 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: ENGINE — ODOR (NR 1) · airframe 16,756 hrs · 14,642 cycles

AIR TURNBACK, DECLARED EMERGENCY. DURING TAKEOFF A GREY, ACRID ODOR/SMOKE STARTED FILLING THE COCKPIT. AS POWER WAS REDUCED, SMOKE DECREASED. REMOVED AND REPLACED NR 1 ENGINE PER MM AND SAM FORMS. OPS AND LEAK CHECK GOOD.

Part: WIRE — INOPERATIVE (CABIN FLOOR) · airframe 16,352 hrs · 14,315 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT OVERWING EXIT. RECONNECTED EEPLS WIRING PER MM.

Part: SKIN — DELAMINATED (WING TE FLAP) · airframe 15,443 hrs · 13,547 cycles

DURING SCHEDULED C2 CHECK, FOUND LEFT WING I/B AFT FLAP AND RIGHT WING O/B AFT DELAMINATED. REMOVED AND REPLACED FLAP ASSYS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,240 hrs · 13,382 cycles

DURING THRU CHECK, FOUND FWD GALLEY EMERGENCY FLASHLIGHT BATTERY IND LOW. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 14,519 hrs · 12,768 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 14,519 hrs · 12,768 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUSTMENT. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DEPLOYED (PAX DOOR)

DURING SCHEDULED SERVICE CHECK, FWD ENTRY DOOR EVACUATION SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LENS — BROKEN (SERVICE DOOR)

AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED C1 CHECK, FOUND FWD CABIN CEILING EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED SIGN PER MM.

Part: PACK VALVES — MALFUNCTIONED (CABIN)

AIRCRAFT UNABLE TO HOLD PRESSURE AT FL350 IN AUTO, CABIN PRESSURE CONTROL PROBLEM. O2 MASK DEPLOYED. WILL HOLD PRESS WITH BOTH PACKS IN HIGH. MANY 02 MASK'S WERE MELTED DURING STORAGE OF THE MASKS IN FLT. A/C DIVERTED, MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED LEFT AND RIGHT PACK VALVES, RANG OUT WIRING AND CW DECAY CHECK PER BOEING MM.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN)

DURING FLIGHT AT 35,000 FT 10,000 FT HORN CAME ON, (PRESSURIZATION) COULD NOT BE CONTROLLED IN AUTO, ACT, OR MAN. NEVER GOT AUTO FAIL IN ALT NOSE GOT GREEN LIGHT BUT COULD NOT CONTROL PRESS, IN MANUAL COULD NOT MOVE OUTFLOW VALVE UNTIL 10,000 FT THEN IT BROKE LOOSE AND WE COULD CONTROL IN MAN. PASS 02 MASKS DID DEPLOY AUTOMATICALLY AT 14,000. REMOVED AND REPLACED CONTROL, OUTFLOW VALVE AND PRESSURE CONT OVERHEAD. OPS CK GOOD PER BOEING MM.