N600WN

Part: PRECOOLER — CRACKED (NR 2 ENGINE) · airframe 68,930 hrs · 55,245 cycles

NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED AND FIRE WARN BELL ACTIVATED. R & R NR 2 ENGINE PNEUMATIC PRECOOLER CONTROL VALVE.

Part: LENS — MISSING (CABIN) · airframe 68,792 hrs · 55,159 cycles

LT OVERWING EMERGENCY EXIT DOOR OVERHEAD SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,996 hrs · 54,637 cycles

L1 DOOR LOWER EXIT LIGHT INOPERATIVE. R & R THE LAMP IAW AMM.

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 67,891 hrs · 54,562 cycles

R2 DOOR EMERGENCY EVAC SLIDE UPPER AFT SLIDE MOUNT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 67,891 hrs · 54,562 cycles

L1 DOOR OVERHEAD EXIT SIGN INOPERATIVE. RECONNECTED A WIRE IAW WDM & AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 67,891 hrs · 54,562 cycles

LEFT OVERWING EMERGENCY EXIT DOOR OVERHEAD SIGN LENS BROKEN. R & R LENS IAW AMM.

Part: FITTING — BROKEN (R2 GIRT BAR) · airframe 67,891 hrs · 54,562 cycles

R2 DOOR EMERGENCY EVACUATION SLIDE AFT GIRT BAR FITTING NUT PLATE BROKEN. R & R FITTING IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 67,891 hrs · 54,562 cycles

FRAME TO SKIN ANGLE CORRODED AT BS 867, BETWEEN STR 27L TO STR 27R. REPAIRED ANGLE IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 67,891 hrs · 54,562 cycles

STRINGER CLIP CORRODED AT BS 907, STR 26R. R & R CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,891 hrs · 54,562 cycles

NR 3 VHF ANTENNA FASTENER HOLES COMMON TO FUSELAGE SKIN CRACKED, SECOND FROM AFT ANTENNA ATTACH FASTENER HOLE. REPAIRED SKIN IAW EA AND DWG.

Part: LENS — BROKEN (EXIT SIGN) · airframe 67,891 hrs · 54,562 cycles

R2 DOOR EXIT SIGN LENS BROKEN. R & R LENS IAW AMM.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 67,891 hrs · 54,562 cycles

R1 DOOR CUTOUT AFT SIDE OF AFT FRAME T-FITTING CRACKED AT STR 8R. R & R, T-FITTING IAW DWG.

Part: LIGHT — BROKEN (LAVATORY) · airframe 67,891 hrs · 54,562 cycles

AFT LAVATORY EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,891 hrs · 54,562 cycles

FRAME CRACKED AT BS 787, BETWEEN STR 27L TO STR 26L. REPAIRED FRAME IAW SRM AND DWG.

Part: FRAME — CORRODED (BS 767) · airframe 67,891 hrs · 54,562 cycles

FRAME CORRODED AT BS 767, BETWEEN STRINGERS 26 - 27L. REPAIRED THE FRAME IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,891 hrs · 54,562 cycles

FRAME CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (BS 787) · airframe 67,891 hrs · 54,562 cycles

FRAME CORRODED AT BS 787, BETWEEN STRINGERS 25 - 27R. REPAIRED THE FRAME IAW SRM AND DWG.

Part: FRAME — CRACKED (BS 767) · airframe 67,891 hrs · 54,562 cycles

FRAME CRACKED AT BS 767, BETWEEN STRINGERS 25 - 27R. REPAIRED THE FRAME PER DWG.

Part: SKIN — CRACKED (R2 DOOR) · airframe 67,891 hrs · 54,562 cycles

R2 DOOR LOWER HINGE CUTOUT SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: RIB — CRACKED (LT WING) · airframe 67,891 hrs · 54,562 cycles

LEFT WING LOWER CHORD RIB CRACKED AT WBL 135.5. REPAIRED RIB IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 67,891 hrs · 54,562 cycles

R1 DOOR CUT OUT FWD FRAME CRACKED AT UPPER DOOR CAM FITTING. R & R FRAME IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 67,891 hrs · 54,562 cycles

R1 DOOR CUTOUT AFT FRAME CRACKED AT UPPER DOOR CAM FITTING. REPAIRED FRAME AT IAW EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 67,891 hrs · 54,562 cycles

FLOORBEAM SPLICE CORRODED AT BS. 986, LBL 6. R & R THE FLOORBEAM SPLICE IAW EA.

Part: FRAME — CRACKED (BS 328) · airframe 67,891 hrs · 54,562 cycles

FRAME CRACKED AT BS 328, STRINGER 4L. REPAIRED THE FRAME IAW DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 67,891 hrs · 54,562 cycles

LEFT WING OTBD FORE FLAP LOWER SURFACE DELAMINATED AT T/E. REPAIRED FORE FLAP IAW SRM.

Part: FITTING — CRACKED (RT WING) · airframe 67,891 hrs · 54,562 cycles

RIGHT WING T/E ABOVE NR 6 FLAP TRACK INBD SUPPORT PANEL LOWER CLIP CRACKED. R & R CLIP IAW SRM AND DWG.

Part: BRACKET — CRACKED (LT WING) · airframe 67,891 hrs · 54,562 cycles

LEFT WING T/E REAR SPAR AFT BRACKET OTBD ANGLE CRACKED AT RSS 544. R & R BRACKET IAW DWG AND SRM.

Part: LENS — LOOSE (CABIN) · airframe 67,794 hrs · 54,487 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,268 hrs · 53,481 cycles

FORWARD GALLEY LAVATORY AREA, EMER LIGHT INOPERATIVE. R & R BATTERY IAW SRM & AMM.

Part: SPAR — CRACKED (LT WING) · airframe 66,268 hrs · 53,481 cycles

LEFT WING SPAR LOWER CHORD CRACKED AT FASTENER HOLE AT RSS 227, HORIZONTAL FLANGE COMMON TO LOWER SKIN. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (LT WING) · airframe 66,268 hrs · 53,481 cycles

LEFT WING UPPER CHORD CRACKED AT RSS 291, VERTICAL FLANGE AFT SPAR. REPAIRED CHORD IAW EA.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 66,268 hrs · 53,481 cycles

RIGHT WING UPPER SKIN PANEL, CRACKED IN MOST REAR OPENED FASTENER HOLE AT TE OF SKIN PANEL RSS 252. REPAIRED SKIN IAW EA.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 66,268 hrs · 53,481 cycles

RIGHT WING UPPER SKIN PANEL, CRACKED AT REAR OPENED FASTENER HOLE AT TE OF SKIN PANEL, RSS 213. REPAIRED SKIN IAW EA.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 66,268 hrs · 53,481 cycles

LEFT WING UPPER SKIN PANEL, MOST AFT OPENED FASTENER HOLE ON TE OF SKIN AT RSS 249 CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 66,268 hrs · 53,481 cycles

LEFT WING UPPER SKIN PANEL, MOST AFT OPENED FASTENER HOLE ON TE OF SKIN AT RSS 237 CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 66,268 hrs · 53,481 cycles

LEFT WING UPPER SKIN PANEL, MOST AFT OPENED FASTENER HOLE ON TE OF SKIN AT RSS 253 CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 66,268 hrs · 53,481 cycles

LEFT WING UPPER SKIN PANEL, MOST AFT OPENED FASTENER HOLE ON TE OF SKIN AT RSS 233 CRACKED. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 66,268 hrs · 53,481 cycles

LEFT WING AFT SPAR WEB CRACKED AT RSS 223. REPAIRED WEB IAW EA.

Part: ATTACH FITTING — CRACKED (LT MLG) · airframe 66,268 hrs · 53,481 cycles

LEFT MLG BEAM ATTACH FITTING ON WING AFT SPAR, CRACKED IN FITTING AT MOST INBD FITTING TO SPAR UPPER CHORD ATTACH FASTENER. REPAIRED FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 66,268 hrs · 53,481 cycles

RIGHT WING AFT SPAR WEB CRACKED AT RSS 220. REPAIRED WEB EA.

Part: SPAR — CRACKED (RT WING) · airframe 66,268 hrs · 53,481 cycles

RIGHT WING AFT UPPER SPAR CHORD, CRACKED AT RSS 220. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 66,268 hrs · 53,481 cycles

LEFT WING AFT UPPER SPAR CHORD, CRACKED AT RSS 220. REPAIRED CHORD IAW EA.

Part: COVER — MISSING (CABIN) · airframe 64,191 hrs · 52,006 cycles

RIGHT OVERWING EMER EXIT DOOR LIGHT COVER MISSING. INSTALL COVER IAW SIP.

Part: LENS — MISSING (CABIN) · airframe 63,299 hrs · 51,398 cycles

LEFT EMER EXIT LIGHT LENS COVER MISSING AT ROW 10. INSTALLED LENS IAW SIP.

Part: LENS — LOOSE (EXIT SIGN) · airframe 62,995 hrs · 51,178 cycles

LEFT OVERWING EXIT SIGN LENS ASSEMBLY LOOSE. SECURED LENS ASSEMBLY IAW SIP.

Part: LENS — DIRTY (CABIN) · airframe 62,988 hrs · 51,171 cycles

LEFT EMER EXIT LIGHT LENS DIRTY. CLEANED LENS IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 62,828 hrs · 51,048 cycles

L1 DOOR INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW TASK CARD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

CENTER WING BOX FLOORBEAM LOWER CHORD CRACKED AT BS 664 RBL 45.5. REPAIRED CHORD IAW EO & EA.

Part: WEB — CRACKED (RT MLG WW) · airframe 62,685 hrs · 50,953 cycles

MAIN WW DECK WEB CRACKED BETWEEN BS 664 TO 675, BETWEEN RBL 30 TO 50. REPAIRED WEB IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

SKIN CRACKED AT BS 787+12.25 STRINGER 24R. REPAIRED IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

SKIN CRACKED AT BS 787+10.5, STRINGER 24R. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 62,685 hrs · 50,953 cycles

RIGHT WING ANGLE CRACKED AT REAR SPAR UPPER CHORD RSS 235. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

SKIN CRACKED AT BS 787+12.3 STRINGER 24R. REPAIRED SKIN IAW EA.

Part: PLATE — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

UNDER WING TO BODY FAIRING PLATE CRACKED AT BS 540 LEFT SIDE. R & R PLATE IAW SRM & DWG.

Part: WEB — CRACKED (LT WING) · airframe 62,685 hrs · 50,953 cycles

LEFT WING FUEL TANK WEB CRACKED AT WBL 198.60 STRINGER 5 AT REAR SPAR. REPAIRED WEB IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

WEB CRACKED BETWEEN BS 312 TO 328 LBL 45. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

ANGLE CRACKED AT BS 351.2, RACK E3 - 4. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

SUPPORT ANGLE CRACKED AT BS 328 STRINGER 21L. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (RT WING) · airframe 62,685 hrs · 50,953 cycles

RIGHT WING UPPER WEB CHORD CRACKED AT WBL 198.60 STRINGER 5R. REPAIRED WEB IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

SPLICE ANGLE CRACKED ON CTR TANK AT LEVEL OF STRINGER 9C UPPER SURFACE WBL 70.85 RT SIDE. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

CLIP CRACKED AT BS 360 STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

SUPPORT WEB CRACKED BETWEEN BS 787 TO 807 RBL 20. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

TIE CLIP CRACKED AT BS 947.5 STRINGER 25R. REPAIRED TIE CLIP IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

FRAME OUTER CHORD CRACKED AT BS 348.2 BETWEEN STRINGER 16L TO 17L. REPAIRED CHORD IAW EO & EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 62,685 hrs · 50,953 cycles

FORWARD LT BORE AT FITTING VERTICAL STABILIZER CORRODED. REPAIRED STABILIZER IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

TIE CLIP CRACKED AT BS 460 STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · airframe 62,685 hrs · 50,953 cycles

LEFT WING NR 4 FLAP TRACK AFT SUPPORT FITTING CORRODED. REPAIRED FITTING IAW CMM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

FORWARD CARGO COMPARTMENT BRACKET CRACKED AT BS 500D STRINGER 19R. R & R BRACKET IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

SKIN CRACKED AT BS 787+11.25, STRINGER 24R. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

ANGLE CRACKED BETWEEN BS 500D TO 520 BL 0. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

FUSELAGE FRAME CRACKED AT BS 520+5.5 INCHES STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

FUSELAGE FRAME CRACKED AT BS 500B+5.5 INCHES, STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: SKIN — DELAMINATED (TAILCONE) · airframe 62,685 hrs · 50,953 cycles

TAIL CONE UPPER SKIN DELAMINATED AT BS 1156+20. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

FRAME OTBD CHORD FWD FLANGE CHORD CRACKED AT BS 727 STRINGER 18A RT. R & R CHORD IAW EA.

Part: SLAT — BROKEN (RT WING) · airframe 62,685 hrs · 50,953 cycles

RIGHT WING NR 5 SLAT UPPER CORNER BROKEN. REPAIRED NR 5 SLAT IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

UPPER CHORD CRACKED AT BS 669 LBL 24.5. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 62,685 hrs · 50,953 cycles

LEFT WING FIXED LE SKIN CRACKED AT WS 213. REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 62,685 hrs · 50,953 cycles

MAIN WW PRESS DECK CRACKED AT BS 664+9.5 LBL 24.5+6.5. REPAIRED DECK IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

SKIN CRACKED AT BS 727 STRINGER 18A RT SIDE. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 62,685 hrs · 50,953 cycles

RIGHT NLG WW CRACKED AT BS 243.7+3.5 WL 169.1. REPAIRED WW IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

DOME CAP WEB CRACKED AT BS 1016 STRINGER 13L. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

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

Part: WEB — CRACKED (NLG WW) · airframe 62,685 hrs · 50,953 cycles

NOSE LANDING GEAR WW WEB CRACKED AT BS 243.7+2.5 WL 169.1. REPAIRED WEB IAW SRM.

Part: SHEAR BEAM — CRACKED (FUSELAGE) · airframe 62,685 hrs · 50,953 cycles

SHEAR BEAM WEB CRACKED CRACKED AT BS 727 STRINGER 18A RT SIDE. R & R WEB IAW SRM & DWG.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 62,503 hrs · 50,824 cycles

R2 DOOR EMER EXIT SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW SIP.

Part: FLAP — LOOSE (RT WING) · airframe 61,293 hrs · 49,973 cycles

RT WING INBD AFT FLAP LOOSE. SECURED AFT FLAP IAW MM.

Part: STIFFENER — CRACKED (RT AILERON) · airframe 61,293 hrs · 49,973 cycles

RT WING AILERON STIFFENER CRACKED INBD OF NR 2 HINGE. R & R STIFFENER IAW SRM.

Part: FLAP — LOOSE (RT WING) · airframe 61,293 hrs · 49,973 cycles

RT WING OTBD AFT FLAP LOOSE. SECURED AFT FLAP IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,742 hrs · 49,607 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

SKIN CRACKED AT BS 380-1, STR 14R. REPAIRED SKIN IAW SRM & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

CLIP CRACKED AT BS 348.2, STR 16L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

STRINGER CLIP CRACKED AT BS 947.5, STR 1. REMOVED & REPLACED CLIP IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

STRINGER SPLICE CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

SKIN CRACKED AT BS 727A+10, STR 14L. REPAIRED SKIN IAW IR & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

INTERCOSTAL CRACKED AT BS 348.2, STR 16L. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND BAC DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

CLIP CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED CLIP IAW BAC DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

INTERCOSTAL CLIP CRACKED AT BS 348.2, STR 16L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

SPLICE FITTING CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED SPLICE FITTING IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

SHEAR TIE CRACKED AT BS 927, BETWEEN STR 4L AND STR 5L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

STRINGER CLIP DAMAGED AT STA 294, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

STRINGER CLIP DAMAGED AT STA 312, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

RIGHT BS 867+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3 AND NR 8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

RIGHT BS 767+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

RIGHT BS 807+10 LOWER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

LEFT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

LEFT BS 380+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

LEFT BS 360+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 4, 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

LIGHT BS 380+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

LEFT BS 500B+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED INDICATION AT HOLES 2, 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

LEFT BS 400+10 UPPER FORWARD SKIN CUTOUT CRACKED AT HOLES 3, 6. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

LEFT BS 500+10 UPPER FORWARD WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 3, 5, 7, 9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

LEFT BS 520+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 4, 5 ,6, 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

LEFT BS 500A+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED AT HOLES 1, 3, 6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

LEFT BS 360+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

LEFT BS 460+10 UPPER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED AT HOLES 2, 3, 7. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,796 hrs · 48,188 cycles

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

Part: STRUCTURE — CRACKED (R1 DOOR) · airframe 58,069 hrs · 47,673 cycles

FWD SERVICE DOOR CRACKED IN AFT LWR CORNER AT FASTENER VERIFIED HFEC. REMOVED AND REPLACED SERVICE FORWARD DOOR PER M/M TAG 583508 P/N ON: 65-45871-523 S/N ON: 680 P/N OFF: S/N OFF: 002180

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,360 hrs · 47,148 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: VALVE — FAULTY (AC BAY) · airframe 57,301 hrs · 47,106 cycles

HYDRAULIC FLUID ODOR OBSERVED IN CABIN AND IN FLIGHT DECK. REMOVED AND REPLACED A&B SYSTEM RESERVOIR VENT VALVES IAW MM.

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 57,266 hrs · 47,083 cycles

EEPLS OUT OF ADJUST AT ROW 8. ADJUSTED EEPLS PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

LEFT KEEL BEAM LOWER SURFACE CORRODED AT BS 720, LBL 8. REPAIRED BEAM IAW EA AND EO.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

RIGHT KEEL BEAM LOWER SURFACE CORRODED AT BS 720, RBL 8. REPAIRED CHORD IAW EA AND EO.

Part: SLAT — DELAMINATED (RT WING) · airframe 57,266 hrs · 47,082 cycles

RIGHT WING NR 6 SLAT DELAMINATED. REPAIRED NR 6 SLAT IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

ANGLE CRACKED AT BS 344, BETWEEN STR 16L TO STR 17L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,266 hrs · 47,082 cycles

LEFT WING NR 1 SLAT SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,266 hrs · 47,082 cycles

LEFT WING NR 2 SLAT SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,266 hrs · 47,082 cycles

LEFT WING IB FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 57,266 hrs · 47,082 cycles

RIGHT WING FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

U-CHANNEL CORRODED AT BS 794, RBL 3.0. REPAIRED U-CHANNEL IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

ANGLE CRACKED BETWEEN BS 312 TO BS 344, STR 17L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

WEB CORRODED BETWEEN BS 360 TO BS 380, STR 17L. REMOVED AND REPLACED WEB IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,266 hrs · 47,082 cycles

LEFT WING AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM AND AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

TIE CLIP CRACKED AT BS 420, STR 27L. REMOVED AND REPLACED CLIP IAW DWG & SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,266 hrs · 47,082 cycles

RIGHT WING NR 6 SLAT SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

STRAP CRACKED AT BS 312, RBL 33. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

STRAP CRACKED AT BS 328, RBL 45.5. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

FUSELAGE SKIN CRACKED AT FWD GALLEY DOOR LOWER AFT CORNER CUTOUT BETWEEN BS 312 TO BS 344, BETWEEN STR 15R TO STR 18R. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,266 hrs · 47,082 cycles

FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER AFT CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 57,266 hrs · 47,082 cycles

FORWARD CARGO DOOR LOWER AFT FRAME CRACKED. REMOVED AND REPLACED DOOR IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,129 hrs · 46,991 cycles

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

Part: SENSOR — FAULTY (E&E BAY) · airframe 56,919 hrs · 46,831 cycles

DECLARED EMERGENCY -- LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED DURING FLAPS 1 T/O NR 2 LEADING EDGE SLAT TRANSIT ON CAPTAINS SIDE ILLUMINATED (ORANGE) AND STALL SHAKER ACTIVATED. REMOVED AND REPLACED NR 2 SLAT MID EXTEND SENSOR PER M/M.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 55,865 hrs · 46,031 cycles

ATTACHMENT CLIP COMMON TO BS 639 STUB BEAM AND LBL 45.5 CRACKED AT BEND RADIUS. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 55,865 hrs · 46,031 cycles

ATTACHMENT CLIP COMMON TO BS 639 STUB BEAM AND RBL 45.5 FLOORBEAM CRACKED AT THE BEND RADIUS. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,865 hrs · 46,031 cycles

FRAME IS CRACKED AT BS 847 BETWEEN THE TWO MIDDLE ATTACH FASTENERS AT THE NR 4 DOOR STOP UPPER SIDE. REMOVED & REPLACED FRAME IAW DWG & ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,865 hrs · 46,031 cycles

LT FRAME INNER CHORD CRACKED AT BS 616. REPAIRED CHORD IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,973 hrs · 45,354 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT LIGHT BULB INOP AT ROW 13. REMOVED AND REPLACED BULB IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 54,692 hrs · 45,142 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FAN — FAULTY (E&E BAY) · airframe 52,977 hrs · 43,838 cycles

DIVERSION / DECLARED EMERGENCY - ELECTRICAL FUMES IN CABIN. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 747, RBL 3 TO RBL 14. REPAIRED SHEAR TIE PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 747, STR 27L TO 26R. REPAIRED SKIN PER EA.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO DOOR SKIN CORRODED AT BS 747, BETWEEN STR 27L TO STR 26R. REPAIRED SKIN PER EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER ATTACH ANGLE CORRODED AT BS 747, STR 27R. REPAIRED ANGLE PER SRM AND BAC DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHORD ANGLE CORRODED AT BS 747, BETWEEN RBL 6 TO RBL 10. REPAIRED ANGLE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

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

Part: FITTING — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER FITTING CORRODED AT BS 1016, STR 24L. REMOVED AND REPLACED FITTING PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED AT BS 729B, LBL 3. REPAIRED ANGLE PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED AT BS 947.5, BETWEEN STR 25L TO STR 25R. REPAIRED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED AT BS 732D, LBL 12. REPAIRED ANGLE PER SRM AND BAC DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN RBL 8 TO RBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947.5, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 790, RBL 14. REPAIRED BEAM PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD PIT FRAME FAIL SAFE CHORD CORRODED AT BS 500D, BETWEEN STR 26L TO STR 26R. REMOVED AND REPLACED CHORD PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 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: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT LOWER SKIN CORRODED BETWEEN BS 500 TO BS 500A, RBL 24. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBOARD SUPPORT ANGLE CORRODED AT BS 859, RBL 8. REPAIRED ANGLE PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 847, LBL 68. REPAIRED BEAM PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED AT BS 767+5, LBL 8. REPAIRED ANGLE PER SRM AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME WEB CORRODED AT BS 500D, BETWEEN STR 27L TO STR 28R. REPAIRED FRAME PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED AT BS 807+6, RBL 8. REPAIRED ANGLE PER SRM AND EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND Z-ANGLE CORRODED AT BS 986, BETWEEN STR 25R TO STR 27R. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STIFFENER CORRODED AT BS 500D, LBL 6. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 947.5 TO BS 986.5+5, BETWEEN RBL 50 TO RBL 53. REPAIRED BEAM PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 947, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN LBL 15 TO LBL 21. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN LBL 2 TO RBL 2. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN LBL 8 TO LBL 12. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN LBL 1 TO RBL 1. REPAIRED FRAME PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 1010, STR 24L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME FAIL SAFE ANGLE CORRODED AT BS 947, BETWEEN RBL 14 TO RBL 16. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, RBL 1. REPAIRED WEB PER BAC DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 996, STR 21R. REPAIRED STRINGER PER EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT LOWER KEEL BEAM SKIN CRACKED AT BS 714. REMOVED AND REPLACED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BBL 0. REPAIRED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 500B TO BS 500C, STR 17L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT WEB CORRODED BETWEEN BS 727A TO BS 727B, RBL 3. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27L TO STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 859, LBL 8. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT O/B CORNER T/E WEDGE DELAMINATED. REPAIRED NR 5 SLAT PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 727B TO BS 727C, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 291.5 TO BS 333, BETWEEN RBL 56 TO RBL 59. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26L REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 540, LBL 1. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CABIN GIRT BAR FITTING CORRODED AT BS 344, LBL 59. REMOVED AND REPLACED FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FITTING — CORRODED (GIRT BAR) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CABIN GIRT BAR FITTING CORRODED AT BS 312, LBL 59. REMOVED AND REPLACED FITTING PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 120.3 TO STA 129.5. REMOVED AND REPLACED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND KEEL BEAM ANGLE CORRODED BETWEEN BS 520 TO BS 527, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: WEB — CORRODED (CARGO BAY) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO PIT VERTICAL CHORD WEB CORRODED BETWEEN BS 520 TO BS 527, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 2R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 7R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,261 hrs · 43,289 cycles

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

Part: FASTENER — LOOSE (EVAC SLIDE) · airframe 52,261 hrs · 43,289 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD MOUNT FASTENER LOOSE. SECURED FASTENER PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 51,695 hrs · 42,840 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,695 hrs · 42,840 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ACO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,940 hrs · 42,275 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: COVER — BROKEN (CABIN) · airframe 50,878 hrs · 42,226 cycles

FWD GALLEY EMERGENCY LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: ATTACH BRACKET — CRACKED (EVAC SLIDE) · airframe 49,719 hrs · 41,383 cycles

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

Part: FLAP — PUNCTURED (RT WING) · airframe 48,771 hrs · 40,663 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING I/B FORE FLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 47,563 hrs · 39,739 cycles

R1 COCKPIT WINDOW PANE ARCED. REMOVED AND REPLACED WINDSHIELD PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,455 hrs · 38,956 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING AFT I/B FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,133 hrs · 38,734 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,133 hrs · 38,734 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,133 hrs · 38,734 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,133 hrs · 38,734 cycles

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

Part: FRAME — CRACKED (BS 747 S8R) · airframe 46,133 hrs · 38,734 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,133 hrs · 38,734 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,133 hrs · 38,734 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 28L. REPAIRED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,133 hrs · 38,734 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,133 hrs · 38,734 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,133 hrs · 38,734 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,133 hrs · 38,734 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,199 hrs · 38,067 cycles

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

Part: HOOK — LOOSE (GIRT BAR) · airframe 45,084 hrs · 37,981 cycles

R1 DOOR EVAC SLIDE GIRT BAR RETAINING HOOKS LOOSE. SECURED HOOKS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,866 hrs · 37,818 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT AFT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,866 hrs · 37,818 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT KEEL BEAM BS 714, LBL 6.5. REPAIRED SKIN PER SWA EA.

Part: CABLE — FRAYED (R2 DOOR SLIDE) · airframe 44,695 hrs · 37,688 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,251 hrs · 37,388 cycles

DURING SCHEDULED SPV CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 43,130 hrs · 36,562 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,130 hrs · 36,562 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT E&E EXHAUST PORT BS 378, LBL 2.8. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,750 hrs · 34,590 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 17 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 41,482 hrs · 35,239 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND LOOSE CONNECTOR, SECURED CONNECTOR PER MM.

Part: STIFFENER — CRACKED (BS 663) · airframe 41,482 hrs · 35,239 cycles

DURING SCHEDULED BRDG CHECK, FOUND RIGHT W/W VERTICAL STIFFENER CRACKED AT BS 663.75, RBL 6.15. REPAIRED STIFFENER PER ACO.

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 40,925 hrs · 34,767 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 4 L/E SLAT DELAMINATED AT INBOARD UPPER SURFACE WEDGE. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 40,925 hrs · 34,767 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR SKIN CRACKED AT UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 39,972 hrs · 34,038 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. REMOVED AND REPLACED EEPLS PHOTOLUMINESECENT STRIP PER MM.

Part: DOOR FRAME — CRACKED (FUSLEAGE) · airframe 39,196 hrs · 33,461 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME SECTION PER EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,194 hrs · 33,460 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,194 hrs · 33,460 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT LOWER LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 39,020 hrs · 33,315 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT LT FWD CABIN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: BOLT — WORN (LT ELEVATOR) · airframe 38,158 hrs · 32,629 cycles

DURING SCHEDULED C3 CHECK, LT ELEVATOR NR 1 TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BOLT AND BUSHING PER MM.

Part: FITTING — CRACKED (L1 DOOR) · airframe 38,158 hrs · 32,629 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX FITTING PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 38,158 hrs · 32,629 cycles

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

Part: GLOWSTRIP — MISSING (CABIN) · airframe 37,178 hrs · 31,889 cycles

DURING SCHEDULED C2 CHECK, FOUND PHOTOLUMINESCENT STRIP MISSING BETWEEN ROW 5 ABC TO ROW 8 ABC. INSTALLED STRIP PER MM.

Part: WEDGE — DELAMINATED (LT WING SLAT) · airframe 37,178 hrs · 31,889 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: COVER — MISSING (CABIN) · airframe 36,623 hrs · 31,457 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS STRIP MISSING COVER BETWEEN ROWS 6 TO 16 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: BUSHING — WORN (LT ELEVATOR TAB) · airframe 35,326 hrs · 30,405 cycles

DURING SCHEDULED C4 CHECK, LEFT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 1 & NR 2 HINGE BUSHINGS & HARDWARE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,326 hrs · 30,405 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FRAME AT BS, 847, RBL 21, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM AND BAC DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500C, STRINGER 27R, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT RIGHT BS 616, WL 201, CRACKED. REPAIRED FRAME CHORD SECTION PER ER.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN RT AND LT REAR SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL FIN FITTING PER ER.

Part: CLEVIS — CORRODED (HORIZONTAL STAB) · airframe 32,937 hrs · 28,482 cycles

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

Part: CLEVIS — CORRODED (VERTICAL STAB) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER AFT SPAR RT AND LT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL STABILIZER PER ER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FWD GIRT BAR FLOOR SUPPORT ANGLE AT BS 345, LBL 56, CORRODED. REMOVED AND REPLACED GIRT BAR FLOOR ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND 4 EACH FRAME SECTIONS CRACKED AT BS 400, STRINGER 8R, BS 380 STRINGER 8L, BS 440, STRINGERS 8L & 8R. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME SECTION AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT LT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (BS 480) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 480, BL 0 TO RBL 3, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 460 TO BS 480, RBL 65, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH FLOORBEAM WEBS CRACKED AT BS 243, RBL 14 AND LT BS 188 TO LT BS 196. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

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

Part: FRAME — CRACKED (BS 787) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS BS 787, STR 8R & STR 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 727D, RBL 18, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500C) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500C, BETWEEN STR 26L TO STR 28L, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,937 hrs · 28,482 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 967, RBL 17, RBL 27, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 32,473 hrs · 28,093 cycles

FWD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 32,371 hrs · 28,002 cycles

BOTH AFT EMERGENCY FLASHLIGHTS INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 30,801 hrs · 26,746 cycles

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

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 30,699 hrs · 26,659 cycles

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

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 27,979 hrs · 24,481 cycles

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

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 27,683 hrs · 24,254 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE AT MOUNT. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,589 hrs · 54,176 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR AND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EXIT LIGHTS BATTERY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 27,312 hrs · 23,983 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS AFT CABIN INOP. REMOVED AND REPLACED BATTERY CHARGER BASE PER MM.

Part: SLIDING WINDOW — STUCK (COCKPIT) · airframe 26,446 hrs · 23,268 cycles

F/O'S SLIDING WINDOW DOES NOT RELEASE FROM EXTERIOR HANDLE. REMOVED AND REPLACED SLIDING WINDOW ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 26,266 hrs · 23,115 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.

Part: GASPER FAN — MALFUNCTIONED (A/C BAY) · airframe 25,307 hrs · 22,322 cycles

FLT ATTENDANTS REPORTED BURNING PLASTIC SMELL IN CABIN. REMOVED AND REPLACED GASPER FAN MOTOR PER MM.

Part: SLIDE — LOOSE (FWD SVC DOOR) · airframe 23,972 hrs · 21,166 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 23,286 hrs · 20,603 cycles

DURING SCHEDULED BC3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 66,216 hrs · 73,872 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK LOOSE AT ROW 8. SECURED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RECONNECTED WIRING BEHIND FWD GALLEY PER MM.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 FLOORBEAM CORRODED ON UPPER SURFACE, RBL 31-36. REPAIRED BEAM PER SWA RA NR A1-353-2188.

Part: FLOORBEAM — CORRODED (BS 987)

DURING SCHEDULED 1/2D CHECK, FOUND BS 987 FLOORBEAM CORRODED AT FWD FACE BETWEEN LBL 43 AND RBL 43. REPAIRED BEAM PER SWA 1-453-037.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 FLOORBEAM UPPER SURFACE CORRODED, RBL 31-RBL 35. REPAIRED BEAM PER SWA RA NR 1-353-2188.

Part: LIGHT — BROKEN (CABIN)

EEPLS LIGHT ASSY BROKEN AT ROW 16. REMOVED AND REPLACED TRACK SECTION PER MM.

Part: LIGHT — INOP (ROW 12)

EEPLS INOP AT ROW 12. RECONNECTED WIRES AND OPS CHECKED GOOD. LATER ON AT PHX, REMOVED AND REPLACED TRACK COVER PER MM.

Part: WIRE — LOOSE (CABIN)

EEPLS INOP ON MID CABIN. RECONNECTED WIRING PER MM.

Part: LGHT — INOP (CABIN)

EEPLS INOP NEAR OVERWING DOOR. REPAIRED WIRING AND RELAMPED PER MM.

Part: COVER — DAMAGED (CABIN)

DURING SCHEDULED A2 CHECK, FOUND 3 EACH EEPLS COVERS DAMAGED. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: LIGHT — OUT OF POSITION (CABIN)

EEPLS LIGHT ASSY OUT OF TRACK IN MID CABIN. REPOSITIONED LIGHTING PER MM.

Part: LIGHT — INOP (ROW 17)

EEPLS LIGHT LENS MISSING AND LIGHT INOP AT ROW 17. REMOVED AND REPLACED LENS AND BULB PER MM.

Part: LIGHT — BROKEN (CABIN)

EEPLS LIGHT DAMAGED. REPAIRED LIGHT ASSY PER MM.

Part: FASTENER — MISSING (PAX DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR REAR ATTACH BRACKET MISSING FASTENER. INSTALLED FASTENER PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP AT OVERWING EXIT. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN)

EMERGENCY FLOOR TRACK LIGHT HAS MID CABIN LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOP (ROW 12-17)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY TRACK LIGHTS OUT AT ROW 12-17. REPAIRED LOOSE WIRE PER MM.

Part: OUTFLOW VALVE — FAILED (CABIN)

AFTER 10 MIN AT 37,000 FT CABIN ALTITUDE BEGAN CLIMBING TO 10,000 FT. DIFFERENTIAL PRESSURE STAYED AT 7.2, NO CHANGE IN ALTN MODE. BEGAN DESCENT AND CABIN PRESSURE DECREASED TO NORMAL RANGE. OUTFLOW VALVE SHOWED CLOSED ENTIRE SEQUENCE. REMOVED AND REPLACED CABIN PRESSURIZATION OUTFLOW VALVE (AFT) PER M/M, OPS CHECKS GOOD PER MM.

Part: WIRE — DISCONNECTED (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING WIRES EXPOSED AT OVERWING EXIT, LEFT SIDE. REPAIRED BROKEN WIRES PER BOEING SRM.

Part: LOCK ACTUATOR — FAILED (NLG)

AFTER GEAR RETRACTION, NOSE GEAR EXTENDED WITH GEAR HANDLE IN OFF POSITION. RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED NOSE GEAR LOCK ACTUATOR, RIGGED GEAR DOORS AND PERFORMED RETRACTION TEST PER BOEING M/M.