N603SW

Part: ACTUATOR — LEAKING (LT WING SLAT) · airframe 68,166 hrs · 54,564 cycles

LEFT WING LEADING EDGE NR 3 SLAT ACTUATOR LEAKED. R & R THE ACTUATOR IAW AMM.

Part: FLASHLIGHT ASSY — CRACKED (CABIN) · airframe 68,166 hrs · 54,564 cycles

LEFT AFT GALLEY AREA FLASHLIGHT BASE CRACKED. R & R FLASHLIGHT IAW CMM.

Part: FRAME — CORRODED (BS 947) · airframe 68,166 hrs · 54,564 cycles

FRAME CORRODED AT BS 947.5, BETWEEN STRINGERS 27L TO 27R. REPAIRED THE FRAME IAW EA.

Part: ANGLE — CRACKED (BS 927-947) · airframe 68,166 hrs · 54,564 cycles

AFT CARGO BAY ANGLE, CRACKED BETWEEN BS 927 TO 947.5, BL 0. R & R THE ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,166 hrs · 54,564 cycles

L1 DOOR CUTOUT ANGLE CRACKED AT BS 303.9+6, BETWEEN STR 13L TO STR 16L. R&R ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 303) · airframe 68,166 hrs · 54,564 cycles

L1 DOOR CUT OUT ANGLE CRACKED AT BS 303.9+6, STR. 15L. R & R THE ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,166 hrs · 54,564 cycles

FRAME CRACKED AT BS 277, BETWEEN STR 15L TO STR 17L. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (BS 303) · airframe 68,166 hrs · 54,564 cycles

ENTRY DOOR CUTOUT ANGLE CRACKED AT BS 303.9+6, STRINGER 8L. R & R THE ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (PAX DOOR CUTOUT) · airframe 68,166 hrs · 54,564 cycles

ENTRY DOOR CUTOUT AREA CRACKED ON AFT LOWER REVEAL. R & R CUTOUT IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 68,166 hrs · 54,564 cycles

RT WING NR 4 SLAT SKIN CRACKED ON EXTERNAL OUTBOARD EDGE LOWER SURFACE. REPAIRED NR 4 SLAT IAW EA.

Part: ANGLE — CRACKED (TE FLAP) · airframe 68,166 hrs · 54,564 cycles

RT WING NR 6 FLAP TRACK FAIRING ANGLE CRACKED AT WBL 185. R&R ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 68,166 hrs · 54,564 cycles

RT WING TRAILING EDGE ANGLE CRACKED ON WS 537.806 INTERNAL CAVITY. R&R ANGLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 68,166 hrs · 54,564 cycles

INTERCOSTAL CRACKED BETWEEN BS 360 TO 344, BL 0. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,166 hrs · 54,564 cycles

FRAME CRACKED AT BS 277, BETWEEN STR 15R TO STR 16R. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 68,166 hrs · 54,564 cycles

STRINGER CLIP 10R CRACKED AT BS 277. R & R THE STRINGER CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 277-291) · airframe 68,166 hrs · 54,564 cycles

R1 DOOR CUTOUT ANGLE CRACKED BETWEEN BS 277 TO 291.5, BETWEEN STRINGERS 10 TO 13R. R & R THE ANGLE IAW SRM AND EA.

Part: WEB — CRACKED (BS 312-328) · airframe 68,166 hrs · 54,564 cycles

WEB CRACKED BETWEEN BS 328 TO 312, RBL 31.6. R & R THE WEB IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,166 hrs · 54,564 cycles

R1 DOOR LOWER CORNER SKIN CUTOUT CRACKED BETWEEN BS 312 TO BS 344, BETWEEN STR 15R TO STR 18R. REPAIRED CUTOUT IAW EA.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 68,166 hrs · 54,564 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO 312, LBL 45.6. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 68,166 hrs · 54,564 cycles

LT WING NR 1 SLAT SKIN CRACKED INBOARD EDGE LOWER SURFACE. REPAIRED THE SKIN IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 68,166 hrs · 54,564 cycles

RT WING FORWARD POSITION LOWER SURFACE ACCESS PANEL 6534 ANGLE CRACKED. R&R ANGLE IAW SRM AND DWG.

Part: SKIN — DELAMINATED (BS 1156) · airframe 68,166 hrs · 54,564 cycles

TAIL CONE LOWER FUSELAGE SKIN DELAMINATED AT BS 1156+6, BL 0. REPAIRED THE SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,166 hrs · 54,564 cycles

SKIN CRACKED AT BS 706+2.5, LBL 5. R&R SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,166 hrs · 54,564 cycles

SKIN CRACKED AT BS 663.75+12, LBL 5. R&R SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,166 hrs · 54,564 cycles

SKIN CRACKED BETWEEN BS 663.75+12 TO BS 685+14.5, LBL 5. R&R SKIN IAW EA.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,572 hrs · 54,148 cycles

LEFT EMERGENCY BULLNOSE LIGHTS INOPERATIVE BETWEEN ROWS 2 TO 6. R & R THE FUSE IAW WDM.

Part: ACTUATOR — LEAKING (FUEL SYSTEM) · airframe 66,948 hrs · 53,736 cycles

AIR TURN BACK, AFTER TAKEOFF LT FUEL TANK STOPPED FEEDING. R & R FUEL CROSS FEED VLV ACTUATOR IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 66,779 hrs · 53,632 cycles

RIGHT LOWER WING TO BODY FAIRING, EMER LIGHT INOPERATIVE. R & R POWER SUPPLY IAW MM.

Part: SKIN — CRACKED (RT WING) · airframe 66,779 hrs · 53,632 cycles

RIGHT WING UPPER SKIN CRACKED AT RSS 265. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 66,779 hrs · 53,632 cycles

RIGHT WING UPPER SKIN CRACKED AT RSS 239. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 66,779 hrs · 53,632 cycles

RIGHT WING UPPER SKIN CRACKED AT RSS 148. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 66,779 hrs · 53,632 cycles

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

Part: ATTACH ANGLE — CORRODED (LT WING) · airframe 66,779 hrs · 53,632 cycles

LEFT WING VERTICAL ATTACH ANGLE CORRODED AT 186.90. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (RT MLG) · airframe 66,779 hrs · 53,632 cycles

RIGHT AFT MLG SUPPORT FITTING CRACKED AT NR 5 HOLE, AFT SIDE OF HOLE. R & R FITTING IAW EA.

Part: SUPPORT FITTING — CRACKED (LT MLG) · airframe 66,779 hrs · 53,632 cycles

LEFT MLG AFT SUPPORT FITTING CRACKED AT NR 5 HOLE, AFT SIDE OF HOLE. R & R FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 66,779 hrs · 53,632 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 221, AT FITTING CUT OUT. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 66,779 hrs · 53,632 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 221, AT FITTING CUT OUT. REPAIRED SPAR WEB IAW EA.

Part: ROLLER — DAMAGED (TE FLAP) · airframe 66,779 hrs · 53,632 cycles

RIGHT WING NR 7 FLAP TRACK FAIRING, A FRAME INBD ROLLER DAMAGED. R & R ROLLER ASSEMBLY IAW CMM.

Part: ATTACH ANGLE — CRACKED (TE FLAP) · airframe 66,779 hrs · 53,632 cycles

LEFT WING NR 3 INBD FLAP, OTBD TRACK FAIRING, OTBD FWD LOWER PANEL ATTACH ANGLE CRACKED. R & R ANGLE IAW DWG & SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 66,779 hrs · 53,632 cycles

LEFT WING INBD UPPER FIXED TE PANEL, INBD SUPPORT ANGLE CRACKED AT AFT ATTACH HOLE. REPAIRED ANGLE IAW DWG.

Part: STRUCTURE — CRACKED (LT WING) · airframe 66,779 hrs · 53,632 cycles

LEFT WING UPPER CHORD CRACKED AT RSS 221. REPAIRED CHORD IAW EA.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 66,779 hrs · 53,632 cycles

R2 DOOR EXTERNAL EMER LIGHT AFT OF DOOR INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,768 hrs · 53,624 cycles

RIGHT EMER EXIT LIGHT INOPERATIVE AT ROW 24. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,744 hrs · 52,904 cycles

FORWARD EMER EXIT SIGN BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: INVERTER — FAULTY (COCKPIT) · airframe 65,509 hrs · 52,738 cycles

DIVERSION, SMELL OF ELEC FUMES REPORTED IN THE VICINITY OF ROW 21 & 22, DURING CRUISE. GASPER FAN TURNED OFF AT 10,000 FEET, FUMES DISSIPATED, SOMEWHAT DURING DESCENT. R & R STATIC INVERTER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,509 hrs · 52,031 cycles

LEFT EMER LIGHT INOPERATIVE AT ROW 22. RELAMPED LIGHT IAW AMM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 63,266 hrs · 51,215 cycles

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

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

CRACK ON CHANNEL AT FUSELAGE STATION 328 TO 344, LBL 45.6. R & R CHANNEL IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,187 hrs · 51,164 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,187 hrs · 51,164 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,187 hrs · 51,164 cycles

RIGHT WING OTBD AFT FLAP LOWER SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

FORWARD ENTRY DOOR CUT OUT FITTING CRACKED AT BS 303.9, BETWEEN STRINGER 13L TO 14L. REPAIRED FITTING IAW SRM & DWG.

Part: LENS — BROKEN (CABIN) · airframe 63,187 hrs · 51,164 cycles

AFT CEILING EXIT LIGHT LENS BROKEN AT BS 907. R & R LENS IAW AMM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

STRINGER SPLICE CRACKED AT BS 908+2, STRINGER 5R. R & R SPLICE IAW EO & EA.

Part: LENS — BROKEN (CABIN) · airframe 63,187 hrs · 51,164 cycles

FORWARD CEILING EXIT LIGHT LENS BROKEN AT BS 400. R & R LENS IAW AMM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

SUPPORT BRACKET CRACKED AT BS 294.5, STRINGER 23L. R & R BRACKET IAW SRM & DWG.

Part: LUG — CORRODED (FLAP TRACK) · airframe 63,187 hrs · 51,164 cycles

LEFT WING NR 4 FLAP TRACK ATTACH LUG CORRODED. REPAIRED ATTACH ASSEMBLY IAW EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 63,187 hrs · 51,164 cycles

LEFT WING NR 4 FLAP TRACK CORRODED ON HOLE UPPER SIDE. REPAIRED FLAP TRACK IAW CMM.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 63,187 hrs · 51,164 cycles

LEFT WING OTBD SIDE AFT EDGE OF TE ACCESS PANEL 7103L CRACKED. REPAIRED PANEL IAW SRM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 63,187 hrs · 51,164 cycles

LEFT WING NR 2 FLAP CARRIAGE SPINDLE CORRODED. R & R FLAP CARRIAGE IAW AMM.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 63,187 hrs · 51,164 cycles

LEFT WING NR 1 FLAP CARRIAGE SPINDLE CORRODED. R & R FLAP CARRIAGE IAW AMM.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

SUPPORT CHANNEL CRACKED AT BS 727+4, LBL 13. REPAIRED CHANNEL IAW SRM.

Part: ACCESS PANEL — CRACKED (VERTICAL STAB) · airframe 63,187 hrs · 51,164 cycles

VERTICAL STABILIZER ACCESS PANEL 9502 PLATE CRACKED. R & R PANEL IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

FRAME CORRODED AT BS 500C, BETWEEN STRINGER 26L TO 27L IN FWD CARGO COMPARTMENT. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500C, STRINGER 26R. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

TIE CLIP CRACKED AT BS 500C, STRINGER 27L. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

WEB CRACKED BETWEEN BS 727A TO 727B, BETWEEN STRINGER 25R TO 26R. R & R WEB IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

FRAME CORRODED AT BS 727D, BETWEEN STRINGER 26L TO 27L IN AFT CARGO COMPARTMENT. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

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

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,187 hrs · 51,164 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 665, LBL 24.5+6. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 63,187 hrs · 51,164 cycles

LEFT WING LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EO & EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,187 hrs · 51,164 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 674, LBL 24.5+6. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 63,187 hrs · 51,164 cycles

RIGHT WING LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EA.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 63,187 hrs · 51,164 cycles

AFT CARGO DOOR CROSSBEAM E AFT ENDS T CHORD CRACKED. REPAIRED T CHORD IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A LT AFT LOWER HOLE 7 O'CLOCK POSITION. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,187 hrs · 51,164 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A LT, FWD LOWER FASTENER HOLE 1 & 7 O'CLOCK POSITIONS. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 63,187 hrs · 51,164 cycles

AFT CARGO DOOR CROSSBEAM E FWD ENDS T CHORD CRACKED. REPAIRED T CHORD IAW EO & EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,126 hrs · 51,120 cycles

L2 DOOR OVERHEAD EXIT SIGN INOPERATIVE. R & R BATTERY IAW MM.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 62,437 hrs · 50,614 cycles

RIGHT AFT EMER EXIT BULLNOSE LIGHT INOPERATIVE. R & R BATTERY PACK HOUSING IAW AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 60,747 hrs · 49,414 cycles

CHORD CRACKED AT BS 348.2 STRINGER 17L. R & R CHORD IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,747 hrs · 49,414 cycles

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

Part: STRUCTURE — DELAMINATED (RT ELEVATOR) · airframe 60,747 hrs · 49,414 cycles

RT ELEVATOR DELAMINATED AT TE. R & R ELEVATOR IAW AMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 59,956 hrs · 48,857 cycles

RT WING NR 7 TE FLAP TRACK CORRODED AT AFT MOUNT. R & R FLAP TRACK IAW MM.

Part: SPOILER — DAMAGED (RT WING) · airframe 59,777 hrs · 48,715 cycles

RT WING NR 7 SPOILER DAMAGED. R & R NR 7 SPOILER IAW AMM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 59,777 hrs · 48,715 cycles

RT WING NR 6 SPOILER DELAMINATED. R & R NR 6 SPOILER IAW AMM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 59,122 hrs · 48,221 cycles

EMERGENCY EXIT LIGHT COVER ADJACENT TO FWD FA JUMP SEAT CAME OFF. R&R COVER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,959 hrs · 48,096 cycles

LEFT EMERGENCY EXIT LIGHT INOP BETWEEN ROW 20 TO ROW 21. R & R LAMP IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,959 hrs · 48,096 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RECONNECTED BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,959 hrs · 48,096 cycles

R2 DOOR INTERIOR EMERGENCY LIGHT INOP. RECONNECTED BATTERY PACK IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

STRINGER CLIP CRACKED AT STA 727E, STR 1. R & R CLIP IAW DWG & SRM.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

BUTT STRAP CRACKED AT STA 360, STR 13L. R & R BUTT STRAP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

STRINGER CLIP CRACKED AT STA 1006, STR 2R. R & R CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

STRINGER CLIP CRACKED AT STA 360, STR 8R. R & R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

STRINGER CLIP CRACKED AT STA 360, STR 9R. R & R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

MAIN CABIN STRINGER CLIP CRACKED. R & R CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

SHEAR TIE CRACKED AT STA 967, BETWEEN STR 4L TO STR 5L. R & R SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

LEFT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

LEFT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

LEFT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 5, 6, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

RIGHT BS 520+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

RT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

LEFT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

LEFT BS 727D+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 4, 12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

LEFT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 7, 8. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

LEFT BS 727B+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

LEFT BS 847+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, AND 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

RIGHT BS 480+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

RIGHT BS 500+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

LEFT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

RIGHT BS 520+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,959 hrs · 48,096 cycles

LEFT BS 727+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 7, 8. REPAIRED SKIN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,575 hrs · 47,819 cycles

FUSELAGE SKIN CRACKED AT BS 500B+13, STR 1L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,575 hrs · 47,819 cycles

FUSELAGE SKIN CRACKED AT BS 727A+6, STR 4R. REPAIRED SKIN PER EA.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 58,430 hrs · 47,716 cycles

KEEL BEAM CLOSURE PANEL BETWEEN A/C DOORS DELAMINATED ON AFT RIGHT END. REMOVED AND REPLACED PANEL PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,105 hrs · 47,470 cycles

FUSELAGE SKIN HAS A VISIBLE .625 CRACK ABOVE STR 5R BS 1006-4. REPAIRED PER EA 1-353-21457 INTERIM REPAIR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: COVER — OUT OF POSITION (L1 DOOR) · airframe 57,693 hrs · 47,173 cycles

F/A REPORTS MANUAL SLIDE INFLATION COVER MISSING FROM ENTRY DOOR. REPOSITION MANUAL SLIDE RELEASE HANDLE COVER TO PROPER POSITION PER MM.

Part: SAFETY SWITCH — FAULTY (E&E BAY) · airframe 57,675 hrs · 47,155 cycles

STA 105 GROUND SENSING SAFETY SWITCH BAD. REMOVED AND REPLACED SWITCH PER MM. (SUBMITTED AS A SUPPLEMENTAL, COULD NOT FIND ORIGINAL RECORD)

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,605 hrs · 47,101 cycles

FRAME CRACKED AT BS 847, BETWEEN STR 24R TO STR 23R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,605 hrs · 47,101 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (NLG WW) · airframe 57,605 hrs · 47,101 cycles

RIGHT NOSE WHEEL WELL STIFFENER CRACKED AT BS 243.7. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,605 hrs · 47,101 cycles

STUB FRAME CRACKED AT BS 947.5+14, STR 17R. REPAIRED STUB FRAME IAW EO AND EA.

Part: ANGLE — CRACKED (LT WING) · airframe 57,605 hrs · 47,101 cycles

CRACK ON ANGLE LOCATED AT LEVEL OF WBL 183 TRAILING AREA OF LEFT WING. REPLACED ANGLE LOCATED AT LEVEL OF WBL 183 TRAILING AREA OF LEF WING IAW SRM B737-300 51-10-02 ITEM 8 51-40-02 AND DRAWING 65-50820.

Part: ACCESS PANEL — CRACKED (LE SLAT) · airframe 57,605 hrs · 47,101 cycles

CRACK ON EDGE OF ACCESS PANEL 6537R, RIGHT SLAT NR 5, RIGHT WING. REPAIRED ACCESS PANEL 6537R RIGHT SLAT NR 5, RIGHT WING IAW B737-300 SRM 57-41-01-2R-8 AND SRM 51-70-17 -OG-0 REPAIR 7.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,605 hrs · 47,101 cycles

AFT GALLEY FWD LOWER CORNER BEAR STRAP SKIN CUTOUT CRACKED. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 57,605 hrs · 47,101 cycles

NLG WHEEL WELL PANEL LEFT WEB CRACKED AT BS 243.7+2.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (LT HORIZ STAB) · airframe 57,605 hrs · 47,101 cycles

CRACK ON ANGLE LOC ACCESS PANEL 9126L LEFT HORIZONTAL STABILIZER. REPLACED ANGLE LOC ACCESS PANEL 9126L LEFT HORIZONTAL STABILIZER IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,605 hrs · 47,101 cycles

FUSELAGE SKIN CUTOUT CRACKED AT BS 947.5, STR 17R. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 57,605 hrs · 47,101 cycles

CRACK ON ANGLE LOCATED WBL 86 TRAILING EDGE RIGHT WING. REPLACED ANGLE AND FASTENERS LOCATED WBL 86 TRAILING EDGE RIGHT WING IAW SRM B737-300 51-10-02 ITEM 8 SRM B737-300 51-40-02 AND DRAWING 65-50820.

Part: SKIN — CRACKED (LT WING) · airframe 57,605 hrs · 47,101 cycles

CRACK ON LEADING EDGE LOCATED AT WBL 208 LEFT WING AT SKIN CUTOUT OF EXISTING REPAIR. REPAIRED LEADING EDGE LOCATED AT WBL 208 LEFT WING AT SKIN CUTOUT IAW EA N.1-A57-0503 REV 4.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,605 hrs · 47,101 cycles

CRACK ON STRAP LOCATED ON BS 344 AND BL 0 OF INTERNAL AREA E/E COMPARTMENT. REPLACED STRAP LOCATED BETWEEN BS 294.5 TO BS 360 BL 0 E/E COMPARTMENT IAW SRM B737-300 51-10-02 AND DRAWING # 65-45834.

Part: WEB — CRACKED (NLG WW) · airframe 57,605 hrs · 47,101 cycles

NLG WHEEL WELL PANEL RIGHT WEB CRACKED AT BS 243.7+2.5, WL 169.1. REPAIRED WEB IAW SRM.

Part: ANGLE — CRACKED (RT HORIZ STAB) · airframe 57,605 hrs · 47,101 cycles

CRACK ON ANGLE LOC ACCESS PANEL 9226R RIGHT HORIZONTAL STABILIZER. REPLACED ANGLE LOC ACCESS PANEL 9226R RIGHT HORIZONTAL STABILIZER IAW B737-300 SRM 51-10-02 ITEM 8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,605 hrs · 47,101 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 669 TO BS 674, RBL 24.5. REPAIRED CHORD IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,605 hrs · 47,101 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 663 AND BS 675, LBL 24.8. REPAIRED CHORD IAW EO AND EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 56,899 hrs · 46,569 cycles

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

Part: SWITCH — FAULTY (MLG WW) · airframe 55,138 hrs · 45,233 cycles

DIVERSION -- AFTER T/O LANDING GEAR SELECTED UP, CONSTANT GEAR WARN HORN. WHEN GEAR FELT FULLY RETRACTED STILL HAD 3 RED GEAR LIGHTS WITH CONSTANT HORN. RESELECTED GEAR DOWN 3 GREENS DOWN LOCKED. RETRACTED GEAR, NO HORN 3 REDS WITH GEAR UP. REMOVED AND REPLACED S-78 LANDING GEAR LEVER SWITCH AND NR 2 AUTO THROTTLE PACK ASSY SWITCH PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,038 hrs · 44,407 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT AFT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: RETAINER — OUT OF ADJUST (GIRT BAR) · airframe 54,008 hrs · 44,378 cycles

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

Part: SKIN — PUNCTURED (ELEVATOR) · airframe 53,183 hrs · 43,748 cycles

DURING SCHEDULED 2HC1 CHECK FOUND, RT ELEVATOR LOWER SURFACE PUNCTURED. REMOVED AND REPLACED ELEVATOR PER MM.

Part: LENS — UNSECURE (CABIN) · airframe 53,101 hrs · 43,690 cycles

LT OVERWING EMERGENCY EXIT SIGN LENS FELL OFF. SECURED LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,730 hrs · 43,406 cycles

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

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT T/E UPPER SURFACED DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND ANGLE CORRODED AT BS 772, RBL 8.10. REMOVED AND REPLACED ANGLE PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 867, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR3 SLAT O/B EDGE EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED SKIN PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED AT BS 907, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, LBL 54. REPAIRED BEAM PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 706, RBL 24.8. REPAIRED WEB PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND KEEL BEAM CORRODED BETWEEN BS 719 TO BS 727, RBL 6.50. REPAIRED BEAM PER EO AND EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT I/B EDGE EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED SKIN PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 710, LBL 24.5. REPAIRED BEAM PER EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 663, LBL 45.5. REPAIRED BEAM PER EO AND EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT T/E UPPER SURFACE AT I/B END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,173 hrs · 43,018 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STIFFENER CRACKED AT BS 727 BULKHEAD AND RT KEEL BEAM. REPAIRED STIFFENER PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 460, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT I/B EDGE EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 520, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, LBL 11. REPAIRED BEAM PER EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING ON O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 299, STR 17R. REMOVED AND REPLACED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT I/B EDGE EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT T/E UPPER SURFACE AT I/B END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 793, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT WEB CRACKED AT BS 663, RBL 24.75. REPAIRED WEB PER EO AND EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,173 hrs · 43,018 cycles

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

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND BULKHEAD CHORD CORRODED AT BS 540, BETWEEN STR 26R TO STR 28R. REPAIRED CHORD PER EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND ANGLE CORRODED AT BS 772, LBL 8. REPAIRED ANGLE PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND ANGLE CORRODED AT BS 772, LBL 3. REPAIRED ANGLE PER EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND ANGLE CORRODED AT BS 772, RBL 3. REPAIRED ANGLE PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED BETWEEN BS 639 TO BS 663, STR 15L. REPAIRED WEB PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 35 TO RBL 42. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND REPAIR ANGLE CORRODED AT BS 772, LBL 12.50. REMOVED AND REPLACED ANGLE PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 52,173 hrs · 43,018 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, AFT SIDE. REPAIRED WEB PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 752, RBL 3. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

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

Part: STRINGER CLIP — CRACKED (FUSEAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 707, STR 11R. REMOVED AND REPLACED SHEAR TIE PER BAC DWG AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,173 hrs · 43,018 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 51,494 hrs · 42,509 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 51,494 hrs · 42,509 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 50,472 hrs · 41,697 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER CRACKED. REPAIRED COVER PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,452 hrs · 40,930 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 48,511 hrs · 40,239 cycles

LEFT EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 47,468 hrs · 39,446 cycles

DURING SCHEDULED CV CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT LOWER HINGE CUTOUT, BS 304.5, WL 236.68. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME WEB CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS 440. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT BS 492. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER FUSELAGE BELLY SKIN CUTOUT CRACKED AT BS 410. REPAIRED SKIN PER IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 305, WL 258.22. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT FITTING, BS 304, WL 259. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT 500A, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM CORRODED AT BS 884. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM CORRODED AT BS 801. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 908, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME WEB CRACKED AT BS 787, STR 8R. REPAIRED WEB PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,947 hrs · 39,060 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 46,569 hrs · 38,794 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 45,162 hrs · 37,792 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,162 hrs · 37,792 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,503 hrs · 37,339 cycles

DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 43,420 hrs · 36,567 cycles

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

Part: DOOR — LACK OF LUBE (COCKPIT) · airframe 43,374 hrs · 36,533 cycles

DURING SCHEDULED HC1 CHECK, CAPTAIN'S EMERGENCY EXIT ROPE DOOR WILL NOT OPEN. LUBRICATED DOOR PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,044 hrs · 36,282 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,044 hrs · 36,282 cycles

DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 41,721 hrs · 35,280 cycles

DURING SCHEDULED BRDG CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 41,721 hrs · 35,280 cycles

DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE, REPAIRED WIRE PER WDM.

Part: BUSHING — WORN (RT MLG) · airframe 41,721 hrs · 35,280 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT MLG WALKING BEAM BUSHING WORN. REMOVED AND REPLACED BUSHING PER MM.

Part: BOLT — WORN (RT MLG) · airframe 41,721 hrs · 35,280 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT MLG WALKING BEAM INBOARD BOLT WORN. REMOVED AND REPLACED BOLT PER MM.

Part: BEARING — WORN (RT MLG) · airframe 41,721 hrs · 35,280 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT MLG WALKING BEAM BEARING WORN. REMOVED AND REPLACED BEARING PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,721 hrs · 35,280 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,283 hrs · 34,944 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 39,926 hrs · 33,853 cycles

R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 39,557 hrs · 33,578 cycles

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

Part: STRUCTURE — DELAMINATED (L/E SLAT) · airframe 39,351 hrs · 33,419 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED NR 5 L/E SLAT PER MM.

Part: FRAME — CRACKED (BS 303 S17L) · airframe 38,856 hrs · 33,035 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, STR 17L. REPAIRED FRAME SECTION PER BOEING SB.

Part: GLOWSTRIP — TORN (CABIN) · airframe 38,410 hrs · 32,691 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP TORN AT ROW 23 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 38,410 hrs · 32,691 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 37,988 hrs · 32,363 cycles

EEPLS LIGHT COVER MISSING AT ROW 3 ABC. INSTALLED EEPLS COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 37,334 hrs · 31,880 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 35,256 hrs · 30,290 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 33,494 hrs · 28,847 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REPAIRED STIFFENER PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, RBL 63, CRACKED. REPAIRED FRAME SECTION PER EA.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND LT AND RT HORIZONTAL STABILIZER FITTING FWD AND AFT SPARS CLEVIS LUGS CORRODED. REPAIRED FITTING PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, FROM LBL 17 TO RBL 17, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM ZEE CHORD AT BS 270, FROM LBL 7 TO RBL 8, CORRODED. REMOVED AND REPLACED ZEE CHORD PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CHORD AT RIGHT BS 188, CRACKED. REMOVED AND REPLACED CREASE BEAM CHORD SECTIONS PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 787, RBL 4, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294, FROM RBL 37 TO RBL 54, CORRODED. REPAIRED FLOORBEAM PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB BETWEEN BS 188 AND BS 194, FROM LBL 30 TO RBL 30, CRACKED. REMOVED AND REPLACED FLOORBEAM WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, LBL 22, CORRODED. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT LEFT NR 1 FLIGHT DECK WINDOW UPPER OUTBOARD CORNER CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SPV, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 380) · airframe 33,178 hrs · 238,615 cycles

DURING SPV, FOUND FRAME CRACKED AT BS 380, STRINGER 8R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500C, RBL 2, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

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

Part: FLOORBEAM — CORRODED (FUSLAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947, LBL 20, CORRODED. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,178 hrs · 28,615 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 328, BETWEEN RBL 54 TO RBL 59, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,561 hrs · 28,152 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR HINGE CUTOUT FUSELAGE SKIN CRACKED. REPAIRED SKIN PER EA.

Part: CABLE — FRAYED (R2 DOOR GIRT BAR) · airframe 32,561 hrs · 28,152 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE CABLE PER MM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 32,561 hrs · 28,152 cycles

DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT STRIP AT ROW 8 ABC, MISSING. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 32,095 hrs · 27,777 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: GLOWSTRIP — MISSING (ROW 8 ABC) · airframe 31,961 hrs · 27,659 cycles

PHOTOLUMINESCENT STRIP AT ROW 8 ABC, MISSING. INSTALLED PHOTOLUMINESCENT STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 31,243 hrs · 26,772 cycles

L2 DOOR EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 29,812 hrs · 25,943 cycles

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

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 28,027 hrs · 24,482 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: CONTAINER — LOOSE (ESCAPE SLIDE) · airframe 28,027 hrs · 24,482 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CONTAINER LOOSE. SECURED CONTAINER PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 28,027 hrs · 24,482 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD AFT T/E FLAP DELAMINATED ON BOTH UPPER AND LOWER SURFACES. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 28,027 hrs · 24,482 cycles

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

Part: SLIDE — OUT OF POSITION (AFT SVC DOOR) · airframe 27,087 hrs · 23,721 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: FITTING — LOOSE (FWD SVC DOOR) · airframe 27,082 hrs · 23,721 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT ATTACH FITTING LOOSE. SECURED AFT ATTACH FITTING PER MM.

Part: TAB — VIBRATES (RT ELEVATOR) · airframe 25,406 hrs · 22,392 cycles

AIRCRAFT VIBRATES MOMENTARILY WITH HIGH POWER SETTINGS AND/OR AERODYNAMIC LOAD. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: ATTACH FITTING — OUT OF POSITION (SERVICE DOOR) · airframe 24,807 hrs · 21,914 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTINGS OUT OF POSITION. REPOSITIONED FITTINGS PER MM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 24,764 hrs · 21,875 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 767 + 6, LBL 12.50. REPAIRED FLOORBEAM PER SWA RA.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 24,764 hrs · 21,875 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 767 PLUS 6, RBL 3. REPAIRED FLOORBEAM PER SWA RA.

Part: LIGHT — DETERIORATED (CABIN) · airframe 24,764 hrs · 21,875 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS STRIP DETERIORATED IN FWD CABIN. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: TAB — WORN (ELEVATOR) · airframe 24,479 hrs · 21,640 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 23,416 hrs · 20,766 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 201, RBL 5.0 AND LBL 5.0. REPAIRED WEB PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 23,388 hrs · 20,741 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS LENS LOOSE AT ROW NR 2. REMOVED AND REPLACED EEPLS LENS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 19,447 hrs · 17,434 cycles

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

Part: MODULE — FAILED (COCKPIT) · airframe 19,061 hrs · 17,110 cycles

DIVERSION, DURING CRUISE HAD DUAL IRS FAILURE. DIVERTED TO CRT. REMOVED AND REPLACED R4 RELAY, ELEC MTR, BATTERY AND GALLEY POWER MODULE PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 18,898 hrs · 16,980 cycles

FWD ENTRY EMERGENCY EVAC SLIDE CAME OUT OF CONTAINER. REINSTALLED FWD ENTRY DOOR SLIDE PER MM.

Part: SLIDE — LOOSE (PAX DOOR) · airframe 18,879 hrs · 16,962 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE CAME LOOSE FROM DOOR. RE-INSTALLED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJ (PAX DOOR) · airframe 17,850 hrs · 16,075 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH FWD DOOR EVACUATION SLIDES OUT OF ADJUSTMENT OF DOOR. REPOSITIONED BOTH SLIDE ASSY''S PER MM.

Part: SENSOR — ILLUMINATED (COCKPIT) · airframe 17,076 hrs · 15,425 cycles

AIR TURNBACK, L/E TRANSIT LIGHTS ILLUMINATED ON BOTH PANELS. C/W BITE CHECK AND DEFERRED PER MEL, LATER ON AT MDW OPERATED L/E DEVICES SEVERAL TIMES. NO DEFECT NOTED PER MM.

Part: ENGINE — MALFUNCTIONED (NR 1)

ABORTED TAKEOFF, NR 1 ENG FAILED TO PRODUCE TAKEOFF POWER. REJECTED TAKEOFF AT 50 KNTS. PERFORMED POWER ASSURANCE RUN ON NR 1 ENG PER MM. OPS CK GOOD.

Part: ENGINE — FAILED (NR 1)

ABORTED TAKEOFF, UNABLE TO ACHIEVE TAKEOFF POWER ON NR 1 ENG. RAN NR 1 ENG AT TAKEOFF POWER AND C/W ACCELERATION TEST PER MM. OPS CHECK GOOD.

Part: FRAME — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, HFEC INSP INDICATED BS 178 BULKHEAD LT SIDE CHORD CRACKED, LBL 26. REMOVED AND REPLACED CHORD SECTION PER SRM.

Part: FRAME — CRACKED (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER BOEING DRAWING.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS INOP AT ROW 24. REPAIRED TRACK LIGHTING PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS TRACK LOOSE AT ROW 12. SECURED TRACK PER MM.

Part: LIGHT — BROKEN (CABIN)

EEPLS TRACK DAMAGED BY OVERWING EXIT. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: ENGINE — POWER LOSS (NR 1)

ABORTED TAKEOFF, UNABLE TO ATTAIN TAKEOFF POWER AT 90 KNOTS ON NR 1 ENG. PERFORMED ENG RUN. OPS CK GOOD IN ALL PARAMETERS PER MM.

Part: LIGHT — INOP (ROW 18-20)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROWS 18-20. RECONNECTED WIRING PER MM.

Part: LIGHT COVER — MISSING (ROW 21)

EEPLS MISSING COVER AT ROW 21. REPLACED COVER PER MM.

Part: SKIN — DELAMINATED (RT TE FLAP)

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

Part: CONNECTOR — LOOSE (ROW 20)

EEPLS LIGHT DISCONNECTED AT ROW 20. RECONNECTED AND SECURED EEPLS WIRES PER MM.

Part: SLIDE — LOOSE (PASSENGER DOOR)

FWD ENTRY DOOR SLIDE CAME OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHT LENS MISSING. REPLACED LENS PER MM.

Part: LIGHT — LOOSE (CABIN)

EMERGENCY EVACUATION FLOOR TRACK LIGHTING LOOSE AT MID CABIN. SECURED TRACK LIGHTING.PER MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING HAD SEVERAL LAMPS BURNED OUT. RELAMPED PER BOEING M/M, OPS CK GOOD.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTING HAS SEVERAL LENS MISSING AND LIGHTS INOP. INSTALLED LENS WHERE NEEDED AND RELAMPED WHERE NEEDED PER BOEING MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND FWD SECTION EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY PACK AS REQUIRED PER BOEING MM, TEST NORMAL.

Part: PUMP — FAILED (B-HYD SYST)

RETURNED TO PHX DUE TO B-SYS HYD FAILURE AND LEFT WING TO BODY OVERHEAT. REMOVED AND REPLACED CRACKED HEAT EXCHANGER DUCT AND B-SYS ELECTRIC PUMP.

Part: RETRACT MECH — MISRIGGED (NLG DOORS)

AFTER TAKEOFF, UPON GEAR RETRACTION, NOSE GEAR EXTENDED WHEN GEAR HANDLE WAS PLACED IN OFF POSITION. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. RERIGGED NOSE GEAR DOORS AND RETRACTION TESTED GEAR PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND 2 EMERGENCY EXIT TRACK LIGHTS INOP AT ROWS 6 AND 7. RELAMPED AND OP CHECKED PER BOEING M/M.