N380SW

Part: ANGLE — LOOSE (L1 DOOR GIRT BAR) · airframe 71,696 hrs · 57,670 cycles

L1 DOOR SLIDE GIRT BAR ANGLE FOUND LOOSE. R & R THE ANGLE IAW SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 71,255 hrs · 57,364 cycles

L2 DOOR EMERGENCY SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE IAW MT.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 71,139 hrs · 57,293 cycles

AFT MEGAPHONE BUTTON INOPERATIVE. R & R THE MEGAPHONE IAW MM.

Part: HOLDER — OUT OF ADJUST (L2 DOOR GIRT BAR) · airframe 70,971 hrs · 57,186 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER OUT OF ADJUST. ADJUSTED THE HOLDER IAW AMM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 70,658 hrs · 56,987 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOW PRESSURE. R & R SLIDE IAW MAINTENANCE.

Part: SKIN — CRACKED (RT WING K FLAP) · airframe 70,606 hrs · 56,955 cycles

RIGHT WING FIXED LEADING EDGE KRUGER FLAP SKIN CRACKED AT OUTBOARD CORNER BS 208. REPAIRED THE SKIN IAW SRM AND EA.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 70,578 hrs · 56,937 cycles

RT WING AILERON BAY BRACKET ATTACH ANGLE CRACKED. R&R ANGLE IAW DWG AND SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,578 hrs · 56,937 cycles

OVERWING EMERGENCY EXIT CEILING MOUNTED LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 70,578 hrs · 56,937 cycles

FORWARD FLASHLIGHT INOP. R&R BATTERY IAW AMM.

Part: BRACKET — CRACKED (LT WING) · airframe 70,578 hrs · 56,937 cycles

LEFT WING HYDRAULIC LINE BRACKET CRACKED BELOW INBD GROUND SPOILER ACTUATOR. R & R BRACKET IAW DWG AND SRM.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · airframe 70,578 hrs · 56,937 cycles

AFT CARGO COMPARTMENT OTBD STR ATTACH BRACKET CORRODED AT BS 727E, STR 27R. R & R BRACKET IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 70,578 hrs · 56,937 cycles

INTERNAL UPPER HORIZONTAL MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 673, LBL 40. REPAIRED WEB IAW SRM AND EA.

Part: LUG — BROKEN (LT SPOILER) · airframe 70,347 hrs · 56,780 cycles

LEFT WING GND SPOILER OTBD ACTUATOR ATTACH LUG BROKEN. R & R NR 4 GND SPOILER IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 69,012 hrs · 55,893 cycles

FORWARD CTR AISLE EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 68,758 hrs · 55,713 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SAFETY SWITCH — FAULTY (CABIN) · airframe 68,514 hrs · 55,540 cycles

AIR TURN BACK, CLIMBING THROUGH FL 280, CABIN ALTITUDE WARNING HORN CAME ON. CABIN WAS CLIMBING THRU 10,000' & AUTO FAIL, PRESSURIZATION, LIGHT WAS ILLUMINATED. EMER DESCENT TO 9,000' WAS ACCOMPLISHED. RETURNED & CABIN NOISE NEAR L1 DOOR HEARD BY FLIGHT ATTENDANTS. FOUND S105 GND SAFETY SWITCH FAULTY. R & R S105 SWITCH IAW MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 68,062 hrs · 55,209 cycles

FORWARD GALLEY OTBD EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW AMM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 68,043 hrs · 55,193 cycles

UPON RAISING GEAR HANDLE, LT GEAR, RED LIGHT & LT GEAR GREEN LIGHT REMAINED ILLUMINATED. THREE GREEN LIGHTS, NO RED WITH HANDLE DOWN, NORMAL LANDING. R & R LT MLG RETRACT ACTUATOR IAW MM.

Part: FASTENER — DAMAGED (L1 DOOR) · airframe 68,015 hrs · 55,173 cycles

L1 DOOR EMER EVAC SLIDE FWD GIRT BAR CLIP ON SHROUD FASTENER DAMAGED. R & R FASTENER ASSEMBLY IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 68,015 hrs · 55,173 cycles

RIGHT WING FWD SUPPORT FITTING FOR MLG BEAM CRACKED IN FASTENER HOLE COMMON TO UPPER REAR SPAR CHORD AT RSS 225. REPAIRED FITTING IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 68,015 hrs · 55,173 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT RSS 222 FASTENER HOLE. REPAIRED CHORD IAW EA & ER.

Part: SPAR — CRACKED (RT WING) · airframe 68,015 hrs · 55,173 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT FASTENER LOCATIONS AT RSS 222. REPAIRED CHORD IAW EA & ER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 68,015 hrs · 55,173 cycles

FORWARD CARGO BAY DOOR CUT OUT, BEAR STRAP INBOARD EDGE CRACKED AT LOWER FORWARD CORNER, 4" UP FROM LOWER DOOR CUT OUT EDGE. REPAIRED BEAR STRAP IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,015 hrs · 55,173 cycles

FUSELAGE SKIN CRACKED AT LT CORNER OF AIR CONDITIONING GND SERVICE DOOR CUT OUT. REPAIRED SKIN IAW SRM.

Part: SKIN — DEBONDED (TE FLAP) · airframe 68,015 hrs · 55,173 cycles

RIGHT WING INBD FORE FLAP UPPER SURFACE DISBONDED 36" FROM OTBD END. REPAIRED FORE FLAP IAW SRM.

Part: STRUT — CRACKED (LT MLG) · airframe 67,652 hrs · 54,923 cycles

LEFT MLG SHOCK STRUT LUG OTBD HOLE, HAT BUSHING CRACKED. R & R STRUT IAW CMM & AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,005 hrs · 54,486 cycles

FORWARD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 66,867 hrs · 54,392 cycles

RIGHT OVERWING LOWER EMER EXIT SIGN LIGHT LENS MISSING. INSTALLED LENS IAW AMM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 66,732 hrs · 54,303 cycles

DIVERSION, LT MAIN RED LIGHT REMAINS ILLUMINATED AFTER GEAR WAS RAISED TO UP. R & R LT MLG UPLOCK ACTUATOR IAW MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 66,102 hrs · 53,878 cycles

L2 WINDOW ARCED. R & R L2 WINDOW IAW MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 66,050 hrs · 53,842 cycles

R2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: SPOILER — DELAMINATED (RT WING) · airframe 65,785 hrs · 53,642 cycles

RIGHT WING NR 7 FLIGHT SPOILER DELAMINATED ON AFT END. R & R SPOILER IAW AMM.

Part: GUSSET — CRACKED (GALLEY DOOR) · airframe 65,785 hrs · 53,642 cycles

FORWARD GALLEY SERVICE DOOR CRACKED LOWER AFT CORNER GUSSET. R & R DOOR IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 65,724 hrs · 53,600 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE IAW MT.

Part: SKIN PANEL — DELAMINATED (RT SPOILER) · airframe 64,916 hrs · 53,022 cycles

RIGHT WING NR 7 SPOILER PANEL UPPER SURFACE DELAMINATED. R & R NR 7 SPOILER IAW MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

LEFT CREASE BEAM WEB CORRODED AT BS 850. REPAIRED WEB IAW SRM & DWG.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 64,916 hrs · 53,022 cycles

LEFT WW BRACKET CRACKED AT BS 727, LBL 18. R & R BRACKET IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

INTERCOSTAL CRACKED BETWEEN BS 727 TO BS 727+4, BETWEEN LBL 37 TO LBL 46. REPAIRED INTERCOSTAL IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

POTABLE WATER SERVICE PAN TOP STIFFENER ON THE FWD END CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: SHEAR WEB — DAMAGED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

SHEAR WEB DAMAGED BETWEEN BS 1016 TO BS 1024, BETWEEN LBL 28 TO LBL 36. R & R WEB IAW AMM & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

LEFT BS 727 FRAME OTBD CHORD FWD FLANGE CRACKED AT STRINGER 18A IN LOWER FWD HOLE IN THE 9 O CLOCK AFT DIRECTION. REPAIRED CHORD IAW ER & EA.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 64,916 hrs · 53,022 cycles

NUMBER 4 FLAP TRACK FAIRING PANEL 3501 DELAMINATED SKIN ON INNER SURFACE EDGE BAND AT THE FWD EDGE. REPAIRED PANEL IAW SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

SHEAR WEB LOWER SUPPORT STIFFENER CORRODED BETWEEN BS 1016 TO BS 1024, BETWEEN RBL 28 TO RBL 36. R & R STIFFENER IAW SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

FLOOR SUPPORT LOWER SIDE SHEAR WEB CORRODED BETWEEN BS 1016 TO BS 1024, BETWEEN RBL 28 TO RBL 36. R & R DAMAGED SHEAR WEB IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 64,916 hrs · 53,022 cycles

RIGHT WING RIB 135.5 CRACKED AT AFT RADIUS OF FLANGE. REPAIRED RIB IAW EA.

Part: ATTACH ANGLE — CRACKED (LT HORIZ STAB) · airframe 64,916 hrs · 53,022 cycles

LEFT HORIZONTAL STABILIZER VERTICAL ATTACH ANGLE CRACKED FOR FIXED LE AT STAB STATION 83.5 FWD SIDE OF FRONT SPAR WEB. R & R ANGLE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

AFT CARGO BAY ON SHEAR TIE CORRODED AT BS 947.5, BETWEEN STRINGER 25L TO 26L. R & R SHEAR TIE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

AFT CARGO BAY FRAME CRACKED AT BS 947.5, STRINGER 19L. R & R FRAME IAW DWG & SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

AFT CARGO BAY ON STRINGER CLIP CORRODED AT BS 787, STRINGER 26R. R & R CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

MAIN DECK FLOORBEAM UPPER FLANGE FWD SIDE CRACKED AT BS 947.5, LBL 53. REPAIRED CHORD IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

AFT CARGO BAY ATTACH FITTING CRACKED AT BS 727, LBL 45.5. R & R FITTING IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

AFT CARGO BAY ON FLOOR SUPPORT REPAIR ANGLE CORRODED AT BS 772, RBL 7.5. REPAIRED ANGLE IAW EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

AFT CARGO BAY ON INTERCOSTAL CORRODED BETWEEN BS 927 TO BS 947, STRINGER 21R. R & R INTERCOSTAL IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

AFT CARGO BAY ON AFT SIDE FOR FRAME CORRODED AT BS 947.5, BETWEEN STRINGER 27L TO 27R. REPAIRED FRAME IAW ER & EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 64,916 hrs · 53,022 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT REAR SPAR STAB BETWEEN STATION 120 TO STATION 129. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

FRAME CRACKED AT BS 348.2, STRINGER 16L. REPAIRED FRAME IAW EA & ER.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

END OF TIE STRAP CRACKED AT BS 347.5, STRINGER 16L. R & R TIE STRAP IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 64,916 hrs · 53,022 cycles

MAIN WW PRESS WEB CRACKED AT BS 663.75, RBL 45.50. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

ANGLE CRACKED AT BS 348.2, STRINGER 15L. R & R ANGLE IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 64,916 hrs · 53,022 cycles

MAIN WW PRESS WEB CRACKED AT BS 663.75, LBL 24.50. REPAIRED WEB IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 64,916 hrs · 53,022 cycles

RIGHT WING TE 2ND SWEEPER WEB OUT FROM INBD END FOR AILERON OTBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 64,916 hrs · 53,022 cycles

LEFT WING TE 2ND SWEEPER WEB OUT FROM INBD END FOR AILERON OTBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

RIGHT OTBD CHORD CRACKED AT BS 727, STRINGER 18A. REPAIRED CHORD IAW ER & EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 64,916 hrs · 53,022 cycles

R1 DOOR AFT FRAME CRACKED INBD SIDE OF NR 3 STOP PIN FITTING DOWN FROM TOP. REPAIRED FRAME IAW ER & EA.

Part: HOLDER — LOOSE (R1 DOOR) · airframe 64,916 hrs · 53,022 cycles

R1 DOOR EMER EVAC SLIDE SHROUD FWD & AFT GIRT BAR STOW HOLDERS LOOSE. SECURED HOLDER IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

BS 639 LT FRAME INBD CHORD CRACKED AT WL 216. REPAIRED CHORD IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 64,916 hrs · 53,022 cycles

LONGITUDINAL BEAM WEB CRACKED AT BS 639, LBL 45.5. REPAIRED WEB IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,979 hrs · 52,397 cycles

LT NOSE WW SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 62,962 hrs · 51,691 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: FAIRING — CRACKED (LT WING) · airframe 62,245 hrs · 51,154 cycles

LT WING BEHIND PANEL 57710L CRACKED AT AFT OUTBOARD EDGE. REPAIRED FAIRING IAW EA.

Part: COVER — UNSECURE (CABIN) · airframe 62,171 hrs · 51,096 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER FELL OFF. R&R LIGHT ASSY PER M/M.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 61,559 hrs · 50,667 cycles

AFT O/B EMERGENCY FLASHLIGHT INOP. RESTOWED FLASHLIGHT AS PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 60,723 hrs · 50,090 cycles

L1 DOOR SLIDE PRESS LOW. REMOVED AND INSTALLED DOOR SLIDE IAW MT 325-61-16. OK FOR SERVICE.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 59,293 hrs · 49,029 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 59,285 hrs · 49,023 cycles

RIGHT EEPLS LOOSE AT ROW 9. REMOVED AND REPLACED EEPLS PER AMM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 59,177 hrs · 48,938 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED CHANNEL PER SRM.

Part: FITTING — CORRODED (RT HORIZ STAB) · airframe 59,177 hrs · 48,938 cycles

RIGHT HORIZONTAL STABILIZER UPPER SPAR FITTING FWD LUG CORRODED. REPAIRED LUG FITTING PER SRM AND BAC DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 59,177 hrs · 48,938 cycles

RIGHT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW MM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 59,177 hrs · 48,938 cycles

LEFT WING O/B MIDFLAP I/B CARRIAGE SPINDLE CORRODED. REMOVED AND REPLACED CARRIAGE PER MT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 59,177 hrs · 48,938 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 664, LBL 24.8. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,177 hrs · 48,938 cycles

R2 DOOR FUSELAGE SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 59,177 hrs · 48,938 cycles

LEFT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,060 hrs · 48,095 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 58,060 hrs · 48,095 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,920 hrs · 47,992 cycles

DURING SCHDULED SPV CHECK, FOUND L2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. R&R LIGHT IAW SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 57,920 hrs · 47,992 cycles

DURING SCHDULED SPV CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT BS 750. R&R BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHDULED SPV CHECK, FOUND SKIN CRACKED AT BS 480, BETWEEN STR 28R TO STR 27R. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 520+10 LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 13. CHARGED BATTERY PER MM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND OVERHEAD EMERGENCY EXIT SIGN INOP BETWEEN ROW 22L TO ROW 23R. CONNECTED LIGHT IAW WDM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 360+10 LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500C+10 LOWER AFT CORNER. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND L/H FUSELAGE WINDOW SKIN CRACKED AT BS 500A+10 UPPER FWD CORNER. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 5,720 hrs · 47,992 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 887+10 AT UPPER AFT CORNER. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 380+12 LOWER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 420+10 LOWER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 480+10 LOWER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 767+10 LOWER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 787+10 LOWER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 500+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 460+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CRACKED AT BS 827+10 LOWER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 420+10 UPPER FORWARD CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN IAW SB.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 2R. REMOVED AND REPLACED CLIP IAW SRM AND DWG

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 440+10 LOWER AFT CORNER. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,920 hrs · 47,992 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 400+10 LOWER AFT CORNER. REPAIRED SKIN IAW SB.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,755 hrs · 47,863 cycles

DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,755 hrs · 47,863 cycles

DURING SCHEDULED MV3 CHECK, FOUND OVERHEAD EMERGENCY EXIT BULL NOSE LIGHTS INOP AT ROW 2. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,713 hrs · 47,825 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS INOP BETWEEN ROW 12 TO ROW 19. CHARGED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,713 hrs · 47,825 cycles

DURING SCHEDULED RON CHECK, FOUND RT OVERWING EEPLS INOP. CHARGED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,713 hrs · 47,825 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 777, STR 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,713 hrs · 47,825 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 500D+5, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,713 hrs · 47,825 cycles

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

Part: CIRCUIT CARD — FAULTY (MLG) · airframe 57,706 hrs · 47,817 cycles

UPON GEAR EXTENSION FOR LANDING, HAD LT MLG UNSAFE INDICATION. CYCLED GEAR AND ALL LANDING LIGHTS TURNED GREEN. RRMOVED AND REPLACED M86 GEAR AND LIGHT SWITCH PC CARD PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,682 hrs · 47,797 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 616. REPAIRED CHORD PER EA.

Part: ATTACH FITTING — CRACKED (SPOILER) · airframe 57,616 hrs · 47,749 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING I/B GROUND SPOILER O/B ACTUATOR ATTACH FITTING ON PANEL CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 57,554 hrs · 47,698 cycles

DECLARED EMERGENCY - RT OVERHEAD CEILING LIGHT BASE DAMAGED BY SHORTED WIRE BETWEEN ROW 6 TO ROW 7. REMOVED AND REPLACED LIGHT BASE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,783 hrs · 49,283 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN AT CHEM MILL CRACKED BETWEEN BS 727C+3.5 TO BS 727C+5.5, STR 4R. REPAIRED SKIN PER DWG.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,730 hrs · 47,062 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,703 hrs · 47,039 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,301 hrs · 46,724 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 23. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,301 hrs · 46,724 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT R2 DOOR. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,301 hrs · 46,724 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 21. RELAMPED PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 55,550 hrs · 46,176 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,062 hrs · 45,813 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,062 hrs · 45,813 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,062 hrs · 45,813 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED BETWEEN BS 429 TO BS 439, STR 1. REPAIRED SKIN PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,113 hrs · 45,066 cycles

AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 54,060 hrs · 45,025 cycles

DURING SCHEDULED OTS CHECK, FOUND RT WING I/B FORE FLAP PUNCTURED ON O/B EDGE ON THE UPPER SKIN. REMOVED AND REPLACED FORE FLAP PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 16L. REMOVED AND REPLACED CHANNEL PER SRM AND BAC DWG.

Part: SHAFT — CORRODED (AILERON QUADRANT) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION ON SHAFT OF AILERON BODY QUADRANT. REMOVED AND REPLACED SHAFT PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT SKIN CRACKED. REMOVED AND REPLACED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45.50. REPAIRED BEAM PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 767 TO BS 787, STR 4R. REPAIRED SKIN PER EO.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP I/B SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 807 TO BS 827, STR 4R. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 515C, STR 13R. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 794, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 727E TO BS 747, STR 4R. REPAIRED SKIN PER EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED CLIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 867 TO BS 887, STR 10R. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 767 TO BS 787, STR 10R. REPAIRED SKIN PER EO.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 727C TO BS 727D, STR 4R. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 847 TO BS 867, STR 10R. REPAIRED SKIN PER EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STIFFENER CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.

Part: FITTING — DAMAGED (GIRT BAR) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS DAMAGED. REMOVED AND REPLACED FITTINGS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FITTING — DAMAGED (GIRT BAR) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS DAMAGED. REMOVED AND REPLACED FITTINGS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 925, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FITTING — DAMAGED (GIRT BAR) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS DAMAGED. REMOVED AND REPLACED FITTINGS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REPAIRED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

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

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 967 TO BS 986.5, STR 25L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: LIGHT — MISSING (CABIN) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BULB MISSING. INSTALLED BULB PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FITTING — DAMAGED (GIRT BAR) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTINGS DAMAGED. REMOVED AND REPLACED FITTINGS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND CHORD CORRODED BETWEEN BS 947.85 TO BS 992.5, RBL 49. REMOVED AND REPLACED CHORD PER SRM AND BAC DWG.

Part: FLAP — CORRODED (LT WING) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING MID FLAP I/B END CORRODED. REMOVED AND REPLACED MID FLAP PER MM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SPOILER LOWER SURFACE DELAMINATED. REPAIRED SPOILER PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 904, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT DELAMINATED ON UPPER SURFACE I/B END. REPAIRED SLAT PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED ON UPPER SURFACE I/B END. REPAIRED SLAT PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

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

Part: SLAT — DELAMINATED (RT WING) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT I/B END DELAMINATED. REPAIRED NR 4 SLAT PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT I/B END DELAMINATED. REPAIRED NR 5 SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED CLIP PER SI AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 34.5. REPAIRED BEAM PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT I/B END DELAMINATED. REPAIRED NR 2 SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,807 hrs · 44,824 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: LIGHT — FADED (CABIN) · airframe 53,533 hrs · 44,607 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS FADED BETWEEN LT ROW 3 TO RT ROW 9. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,170 hrs · 44,334 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 844, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,462 hrs · 43,836 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 505B, STR 1. REPAIRED SKIN PER ER.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 52,462 hrs · 43,836 cycles

DURING SCHEDULED SPV CHECK, FOUND LOWE HORIZONTAL SURFACE OF AFT CARGO DOOR THRESHOLD CLOSE-OUT WEB FWD ATTACH ANGLE CORRODED. REMOVED AND REPLACED ANGLE PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,109 hrs · 43,569 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 52,109 hrs · 43,569 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 0 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: MOUNT — CRACKED (R2 DOOR) · airframe 51,277 hrs · 42,944 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,016 hrs · 42,755 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR CUTOUT FWD LOWER FRAME CRACKED. REMOVED AND REPLACED DOOR FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,016 hrs · 42,755 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 49,610 hrs · 41,741 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD FORE FLAP LOWER SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (BS 390) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER SKIN CUTOUT CRACKED AT BS 390. REPAIRED SKIN PER SWA ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND LOWER FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST DUCT CUTOUT. REPAIRED SKIN PER SWA ACO.

Part: SKIN — CRACKED (BS 450) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER SKIN CUTOUT CRACKED AT BS. 450. REPAIRED SKIN PER SWA ACO.

Part: SKIN — CRACKED (BS 410) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER SKIN CUTOUT CRACKED AT BS 410. REPAIRED SKIN PER SWA ACO.

Part: SKIN — CRACKED (BS 430) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER SKIN CUTOUT CRACKED AT BS. 430. REPAIRED SKIN PER SWA ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 49,433 hrs · 41,613 cycles

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

Part: SKIN — CRACKED (R1 DOOR) · airframe 49,433 hrs · 41,613 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM UPPER CAP CORROED AT BS 986, LBL 5. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM CORROED AT BS 976, RBL 50, WL 208. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND NOSE WHEEL WELL UPPER PRESSURE SKIN CRACKED AT BS 252, BETWEEN LBL 9 TO RBL 9. REPAIRED SKIN PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 986, BETWEEN RBL 28 TO RBL 40. REPAIRED TEE CAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING NR 5 SLAT O/B UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM CORRODED AT BS 954, RBL 53. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,433 hrs · 41,613 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 49,235 hrs · 41,474 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 49,222 hrs · 41,464 cycles

FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 48,691 hrs · 41,088 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 48,690 hrs · 41,088 cycles

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

Part: FAN — FAULTY (E&E BAY) · airframe 47,738 hrs · 40,387 cycles

CREW REPORTED STRONG ELECTRICAL SMELL IN MID CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,710 hrs · 40,362 cycles

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

Part: UPLOCK ACTUATOR — FAULTY (RT MLG) · airframe 47,636 hrs · 40,305 cycles

AIR TURNBACK. RIGHT MLG WARNING LIGHT ILLUMINATED WITH HANDLE IN OFF POSITION. RIGHT MLG FELL OUT OF EXTENDED POSITION. REMOVED AND REPLACED UPLOCK ACTUATOR PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,236 hrs · 40,004 cycles

DURING SCHEDULED CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME PER ACO.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 44,435 hrs · 37,833 cycles

RIGHT AFT CABIN EMERGENCY EXIT LIGHT STAYS WITH NO POWER. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,405 hrs · 37,807 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD LEFT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,405 hrs · 37,807 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 43,688 hrs · 37,249 cycles

DURING SCHEDULED CV CHECK, FOUND LEFT FWD CABIN EEPLS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: KEELBEAM — CORRODED (BS 503D-524) · airframe 42,778 hrs · 36,554 cycles

DURING SCHEDULED 12Y CHECK, FOUND KEEL BEAM CORRODED AT BS 503D TO BS 524, RBL 6.5. REPAIRED KEEL BEAM PER SRM.

Part: FRAME — CORRODED (BS 727E) · airframe 42,778 hrs · 36,554 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727E, LBL 7 TO LBL 12. REPAIRED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (BS 747) · airframe 42,778 hrs · 36,554 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, RBL 7. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — WORN (BS 907) · airframe 42,778 hrs · 36,554 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN WORN UNDER DORSAL FIN BS 907. REPAIRED SKIN PER SRSM.

Part: GIRT BAR — CRACKED (R2 DOOR) · airframe 42,778 hrs · 36,554 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CRACKED. REMOVED AND REPLACED GIRT BAR FITTING PER MM.

Part: FITTING — CRACKED (NLG W/W) · airframe 42,271 hrs · 36,165 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG RETRACT ACTUATOR ATTACH FITTING CRACKED. REMOVED AND REPLACED NLG ATTACH FITTING PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 39,094 hrs · 33,690 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD CABIN BULLNOSE EMERGENCY EXIT LENS LOOSE. SECURED LENS PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 38,128 hrs · 32,922 cycles

DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE BUSHING & HARDWARE PER MM.

Part: BUSHING — WORN (RT ELEVATOR TAB) · airframe 37,234 hrs · 32,226 cycles

DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR NR 1 TAB HINGE BOLT & BUSHING PER MM.

Part: SLIDE — DISCHARGED (R2 DOOR) · airframe 35,535 hrs · 30,880 cycles

R2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,366 hrs · 30,734 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED UPPER HINGE BOX FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 946, STRINGER 17R, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 303.9, LBL 57.5, CRACKED. REPAIRED FRAME SECTION PER SB.

Part: RIB — CRACKED (HORIZ STAB) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D-CHECK, FOUND LEFT HORIZONTAL STAB RIB CHORD AT STAB STATION 120, CRACKED. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 727D, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT BS 616, RBL 65, WL 202, CRACKED. REPAIRED FRAME CHORD PER ER.

Part: PLATE — CORRODED (CABIN) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FLOOR MOUNT PLATES CORRODED. REMOVED AND REPLACED GIRT BAR MOUNT PLATES PER SRM AND MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 440, STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT BS 639, STRINGER 2R, STRINGER 3L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 294.5, RBL, 54, WL 209, CORRODED. REPAIRED FRAME SECTION PER SRM.

Part: BEAM — CRACKED (RUDDER) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB T/E BEAM AT LT RUDDER STATION 13.3 TO RUDDER STATION 121.64, CRACKED. REMOVED AND REPLACED VERTICAL STAB BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 53, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR CUTOUT UPPER TORQUE FITTING BEAR STRAP CRACKED. REPAIRED BEAR STRAP PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM WEB AT BS 294, RBL 55, CORRODED. REMOVED AND REPLACED FLOOR WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,481 hrs · 29,981 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 380, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 907, BS 787, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CHORDS AT BS 360 TO BS 380, LBL 65, BS 375 TO BS 380, LBL 70, CRACKED. REMOVED AND REPLACED CREASE BEAM CHORDS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,451 hrs · 29,981 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 9007, BS 867, BS 827, 787, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 33,634 hrs · 29,324 cycles

EMERGENCY EXIT LIGHT AT FWD F/A JUMPSEAT BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY PER MM.

Part: LIGHT — LOOSE (AFT CABIN) · airframe 32,509 hrs · 28,411 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE IN AFT CABIN. SECURED EEPLS PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 32,509 hrs · 28,411 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR RETAINER BRACKET LOOSE. SECURED RETAINER PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 32,323 hrs · 28,257 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 31,919 hrs · 27,923 cycles

AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: TRUNNION PIN — CORRODED (RT MLG) · airframe 30,005 hrs · 26,440 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED RT MLG TRUNNION PIN PER MM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 29,674 hrs · 56,180 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — MISROUTED (CABIN DOORS) · airframe 29,674 hrs · 26,180 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH FWD ENTRY AND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLES MISROUTED. REROUTED CABLES PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 28,940 hrs · 25,592 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 28,769 hrs · 25,454 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 28,156 hrs · 24,982 cycles

FWD SERVICE DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 27,759 hrs · 24,685 cycles

DURING SCHEDULED C4 CHECK, FOUND LT HORIZ STAB SKIN LOWER SURFACE CRACKED AT STA 108 NEAR AFT SPAR. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (CABIN) · airframe 27,018 hrs · 24,079 cycles

EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,935 hrs · 24,002 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHT INOP AFT OF AFT SERVICE DOOR. RELAMPED LIGHT PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,940 hrs · 23,203 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 201, LBL 5 & RBL 5. REPAIRED BULKHEAD WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,940 hrs · 23,203 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BOTH R-1 & L-1 COCKPIT WINDOW FRAMES CRACKED AT UPPER OTBD CORNER. REPAIRED WINDOW FRAMES PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,939 hrs · 23,202 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 227 & RBL 17.1. R&R VERTICAL BEAM PER SRM.

Part: FRAME — CRACKED (FWD SVC DOOR) · airframe 25,939 hrs · 23,202 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT CUTOUT 3RD STOP FROM BOTTOM. REPAIRED FRAME PER SWA T1-152-003.

Part: FAN — OVERHEATED (E/E BAY) · airframe 25,802 hrs · 23,083 cycles

EQUIPMENT COOLING LIGHT ILLUMINATED IN FLIGHT (350) FOLLOWED BY BURNING ODOR. SELECTED ALTERNATE, LIGHT EXTINGUISHED AND SMELL RETURNED TO NORMAL. REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM.

Part: LIGHT — INOPERATIVE (ENTRY DOOR) · airframe 25,221 hrs · 22,610 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: COVER — BROKEN (CABIN) · airframe 24,957 hrs · 22,386 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT COVER BROKEN. R&R EXIT COVER PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 24,890 hrs · 22,324 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS INOP BETWEEN ROWS 18 -21. SECURED EEPLS WIRES PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 24,787 hrs · 22,230 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP. REPAIRED EEPLS WIRES PER MM.

Part: SUPPORT FITTING — CORRODED (RH WING) · airframe 24,608 hrs · 22,090 cycles

DURING SCHEDULED A2 CHECK, FOUND RH MLG WALKING BEAM SUPPORT FITTING CORRODED. R&R MLG SUPPORT FITTING PER ALM WORK CARD 3371.

Part: WIRE — EXPOSED (CABIN) · airframe 24,608 hrs · 22,090 cycles

EEPLS WIRES EXPOSED. SECURED EEPLS WIRES PER MM.

Part: INDICATOR — OUT OF TOLERANCE (EVAC SLIDE) · airframe 23,686 hrs · 21,287 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 23,410 hrs · 21,059 cycles

EEPLS WIRING EXPOSED. RESECURED EEPLS WIRING PER MM.

Part: BULB — FAILED (ROW 19) · airframe 22,148 hrs · 19,993 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP ROW 19. RELAMPED EEPLS PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 21,438 hrs · 19,376 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR LOW. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,438 hrs · 19,376 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT ROW 7. RELAMPED PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 20,541 hrs · 18,575 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT OUT OF ADJUSTMENT. REPOSITIONED SLIDE ASSY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 20,541 hrs · 18,575 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LENS BROKEN AT OVERWING EXIT. R&R LENS PER MM.

Part: SLIDE — DISLODGED (CABIN)

FWD ENTRY DOOR EVACUATION SLIDE CAME OUT OF POSITION. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR)

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

Part: SLIDE — SAGGING (PAX DOOR)

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT OUT OF POSITION. REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY — DISCHARGED (CARGO BAY)

DURING SCHEDULED A1 CHECK, FOUND EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — BROKEN (CABIN)

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHTING IN AFT CABIN BROKEN. REPAIRED TRACK LIGHTING PER MM.

Part: SKIN — DAMAGED (BS 224)

DURING SCHEDULED BC1 CHECK, FOUND FUSELAGE SKIN DAMAGED 13 INCHES BELOW R1 WINDOW FRAME AT BS 224. REPAIRED PER BOEING SRM.