N384SW

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,075 hrs · 56,826 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMP IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 69,848 hrs · 56,680 cycles

L1 DOOR EMERGENCY SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LATCH — BROKEN (R1 DOOR) · airframe 69,633 hrs · 56,546 cycles

R1 DOOR EMERGENCY EVAC SLIDE STORAGE BIN, SLIDE LATCH HANDLE BROKEN. SECURED LATCH IAW SIP.

Part: SKIN — CRACKED (RT WING) · airframe 69,499 hrs · 56,460 cycles

RIGHT WING UPPER WING SKIN AFT HOLE CRACKED AT RSS 238. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,499 hrs · 56,460 cycles

RIGHT WING UPPER WING SKIN AFT HOLE CRACKED, BETWEEN RSS 255 - 250.7. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 69,499 hrs · 56,460 cycles

RIGHT WING UPPER SKIN CRACKED BETWEEN RSS 264.7 - 269. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 69,499 hrs · 56,460 cycles

RIGHT WING AFT SPAR REAR SPAR UPPER CHORD CRACKED, BETWEEN RSS 221.29 - 227.09. REPAIRED CHORD IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 69,499 hrs · 56,460 cycles

RIGHT WING AFT SPAR REAR SPAR WEB CRACKED AT HOLE NR 5 APPROX RSS 222.34 & NR 11 HOLE RSS 220.64. REPAIRED WEB IAW ER & EA.

Part: FITTING — CRACKED (RT MLG) · airframe 69,499 hrs · 56,460 cycles

RIGHT FWD MLG FITTING FASTENER HOLE RSS 220.64 THIRD FASTENER HOLE DOWN. REPAIRED FITTING IAW ER & EA.

Part: FITTING — CRACKED (RT WING) · airframe 69,499 hrs · 56,460 cycles

RIGHT WING AFT SPAR AFT FITTING CRACKED AT HOLE NR 5 APPROX RSS 224.14. REPAIRED FITTING IAW ER & EA.

Part: LINK — CORRODED (RT MLG) · airframe 69,499 hrs · 56,460 cycles

RIGHT MLG SUPPORT BEAM INBD SWING LINK CORRODED. R & R SWING LINK IAW AMM & EA.

Part: SPAR — CRACKED (RT WING) · airframe 69,499 hrs · 56,460 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT 5 O'CLOCK POSITION ON LOWER VERTICAL FASTENER ON UPPER CHORD ABOUT RSS 222. REPAIRED CHORD IAW ER & EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 69,468 hrs · 56,438 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,138 hrs · 56,218 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 460 - 480, WL 208. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,138 hrs · 56,218 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 400 - 420, WL 208. R & R WEB IAW SRM & DWG.

Part: PLATE — CORRODED (L1 DOOR) · airframe 69,138 hrs · 56,218 cycles

L1 DOOR GIRT BAR FITTING ATTACHMENT PLATES CORRODED. R & R PLATE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,138 hrs · 56,218 cycles

FUSELAGE SKIN CRACKED AT BS 291.50, WL 223.50. REPAIRED SKIN IAW EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 69,138 hrs · 56,218 cycles

FORWARD ENTRY DOOR MOP SILL UPPER SURFACE CORRODED. R & R MOP SILL IAW DWG & SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 69,138 hrs · 56,218 cycles

AFT ENTRY DOOR MOP SILL CORRODED, BETWEEN BS 947 - 1000, WL 208.1. R & R MOP SILL IAW DWG & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,138 hrs · 56,218 cycles

FLOORBEAM CORRODED AT BS 967, RBL 27. REPAIRED BEAM IAW EA & ER.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 69,138 hrs · 56,218 cycles

PRESSURE WEB CRACKED AT BS 1016, STRINGER 6L. R & R WEB IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 69,138 hrs · 56,218 cycles

AFT SERVICE DOOR MOP SILL CORRODED. R & R MOP SILL IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,138 hrs · 56,218 cycles

SHEAR TIE CORRODED AT BS 747, BETWEEN STRINGER 27L - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,138 hrs · 56,218 cycles

SHEAR TIE CORRODED AT BS 727C, BETWEEN STRINGER 26R - 27R. REPAIRED SHEAR TIE IAW ER & EA.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 68,884 hrs · 56,057 cycles

AFT ENTRY DOOR EMER EXIT SIGN BULB INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: CHANNEL — CRACKED (RT WING) · airframe 68,884 hrs · 56,057 cycles

RIGHT WING TE LOWER PANEL SUPPORT CHANNEL CRACKED JUST OTBD NR 2 PYLON. REPAIRED CHANNEL IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 68,762 hrs · 55,979 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 68,762 hrs · 55,979 cycles

LEFT EMER EXIT LIGHT LENS COVER LOOSE. SECURED LENS IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 68,000 hrs · 55,475 cycles

MID CABIN EEPLS STRIP MISSING. INSTALLED STRIP IAW AMM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 67,947 hrs · 55,441 cycles

L1 DOOR EXTERNAL SKIN CRACKED FWD AFT RIVET ROW BELOW GATE. REPAIRED DOOR IAW SRM.

Part: RELAY — FAULTY (COCKPIT) · airframe 67,803 hrs · 55,345 cycles

DIVERSION, CLIMBING THROUGH FL330 TO FL360, NR 1 BUS OFF LIGHT ILLUMINATED. APU STARTED BELOW FL350 & PLACED ONLINE NR 1 SIDE. HOWEVER, POWER WOULD NOT STAY ONLINE WITH EITHER ENG GEN OR APU SELECTED. ON ITS OWN IT CYCLES ON & OFF;. R & R POWER TRANSFER SIGNAL RELAY R349 IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 67,683 hrs · 55,259 cycles

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

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,137 hrs · 56,218 cycles

AFT BAG BIN DOOR CUT OUT FWD SCUFF PLATE, LOWER CORNER CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: HOOK — LOOSE (R1 DOOR) · airframe 66,195 hrs · 54,215 cycles

R1 DOOR EMER EVAC SLIDE AFT GIRT BAR HOOK COVER ASSEMBLY LOOSE. R & R HOOK ASSEMBLY IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 65,363 hrs · 53,664 cycles

RIGHT WING ANGLE CRACKED ON UPPER SURFACE ABOVE LOWER SPAR CAP FSS 231 INCHES FROM INBD EDGE. REPAIRED ANGLE IAW EA.

Part: LENS — DISCOLORED (CABIN) · airframe 65,363 hrs · 53,664 cycles

RIGHT MID CABIN EMER EXIT LIGHT LENS DISCOLORED. R & R LENS IAW AMM.

Part: LENS — DISCOLORED (CABIN) · airframe 65,363 hrs · 53,664 cycles

LEFT MID CABIN EMER EXIT LIGHT LENS DISCOLORED. R & R LENS IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 65,048 hrs · 53,412 cycles

LEFT EMER LIGHT POWER SUPPLY INOPERATIVE. R & R POWER SUPPLY IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 65,048 hrs · 53,412 cycles

AFT OVERHEAD EMER LIGHT SIGN CHARGER INOPERATIVE. R & R CHARGER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,048 hrs · 53,412 cycles

AFT OVERHEAD EMER LIGHT SIGN BATTERY PACK INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: SLEEVE — LOOSE (R2 DOOR) · airframe 64,300 hrs · 52,869 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR SLEEVE LOOSE. SECURED SLEEVE IAW SIP.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

SUPPORT ANGLE CRACKED AT BS 480, STRINGER 16R. R & R ANGLE IAW SRM & DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

STIFFENER CORRODED BETWEEN BS 219.8 TO BS 227.8, BL 0. R & R STIFFENER IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,741 hrs · 52,464 cycles

LEFT WING AFT FLAP INBD LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

FUSELAGE EXTERNAL SKIN FWD CARGO DOOR CUT OUT CRACKED AT BS 440+6, STRINGER 18R. REPAIRED SKIN IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

STRAP CRACKED AT BS 312, RBL 45. R & R STRAP IAW SRM & DWG.

Part: COVER — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

RIGHT EE COMPARTMENT COVER ASSEMBLY CRACKED. R & R COVER ASSEMBLY IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

CHANNEL CRACKED BETWEEN BS 663 TO BS 670, RBL 24.5+12. R & R CHANNEL IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

ANGLE CRACKED AT BS 727, BETWEEN LBL 45 TO LBL 52. R & R ANGLE IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

STRAP CRACKED AT BS 328, RBL 31. R & R STRAP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

FUSELAGE EXTERNAL SKIN FWD CARGO DOOR CUT OUT CRACKED AT BS 440+3, STRINGER 24R. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

FRAME CORRODED AT BS 360 & BETWEEN STRINGER 28L TO STRINGER 28R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

LEFT EE COMPARTMENT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

CLIP CRACKED AT BS 336, BETWEEN STRINGER 20L TO STRINGER 21L. R & R CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

CLIP CRACKED AT BS 328, BETWEEN STRINGER 20L TO STRINGER 21L. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

FRAME CRACKED AT BS 492, STRINGER 24R. R & R FRAME IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

CLIP ANGLE CRACKED AT BS 320, BETWEEN STRINGER 20L TO STRINGER 21L. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CRACKED (LT WING) · airframe 63,741 hrs · 52,464 cycles

LEFT WING UPPER CHORD CRACKED AT LEVEL S 2 & WBL 114 FUEL TANK. REPAIRED CHORD IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

SKIN CRACKED AT BS 794+3, STRINGER 24R. REPAIRED SKIN IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

Z STIFFENER CRACKED AT BS 1016, STRINGER 3L. REPAIRED Z STIFFENER IAW EO & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

STRINGER CLIP CRACKED AT STATION 348.2, STRINGER 16L. R & R CLIP IAW SRM & EA.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

AFT PRESS BULKHEAD DOME WEB OIL CANNING AT BS 1016, RBL 60. REPAIRED DOME WEB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

FRAME OUTER CHORD CRACKED AT BS 348.2, STRINGER 16L. REPAIRED CHORD IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

TIE CLIP CRACKED AT BS 727C, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

SUPPORT ZEE CRACKED BETWEEN BS 727C TO BS 727D, STRINGER 25R. R & R SUPPORT ZEE IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 63,741 hrs · 52,464 cycles

LEFT NLG WW WEB CRACKED AT BS 251.625+7, WL 169.1. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

LEFT SIDE NLG WW WEB CRACKED AT BS 251.625+7, WL 169.1. REPAIRED WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

SUPPORT ANGLE CRACKED AT BS 807, STRINGER 25R. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

SIDEWALL PANEL SUPPORT STRUCTURE CRACKED AT BS 747, STRINGER 19L. REPAIRED STRUCTURE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 19L. R & R TIE CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

FRAME CRACKED AT BS 500B, STRINGER 21L. REPAIRED FRAME IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

CLIP CRACKED AT BS 947, BETWEEN STRINGER 24L TO STRINGER 25L. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

SKIN CRACKED AT BS 328.1, STRINGER 17R. REPAIRED SKIN IAW SRM & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

CLIP CRACKED AT BS 947, BETWEEN STRINGER 24R TO STRINGER 25R. R & R CLIP IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

MAIN WW PRESS DECK CRACKED AT BS 663.75+1.5, RBL 24.5+14. REPAIRED WEB IAW EO & EA.

Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 63,741 hrs · 52,464 cycles

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

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 63,741 hrs · 52,464 cycles

T CHORD CRACKED AFT END OF THE CROSSBEAM OF AFT CARGO DOOR. REPAIRED T CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

CHORD CRACKED AT BS 727, STRINGER 18A RT AT FWD LOWER FASTENER HOLE OF INSPECTION AREA 3 & 9 O'CLOCK DIRECTION. REPAIRED CHORD IAW EA.

Part: PLATE — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

PLATE CRACKED AT BS 697, STRINGER 21L. R & R PLATE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

WEB CRACKED AT BS 227.8, BL 0. R & R WEB IAW SRM & DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

PLATE CRACKED AT BS 697, STRINGER 21R. R & R PLATE IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,741 hrs · 52,464 cycles

CHORD CRACKED AT BS 727, 18A LT AT FWD LOWER FASTENER HOLE OF INSPECTION AREA 12 & 6 O'CLOCK. REPAIRED CHORD IAW EA.

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 63,741 hrs · 52,464 cycles

LEFT MAIN WW SUPPORT ANGLE CRACKED AT BS 727, LBL 16. R & R ANGLE IAW SRM & DWG.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 64,023 hrs · 52,668 cycles

R1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SIGN — DAMAGED (CABIN) · airframe 63,633 hrs · 52,383 cycles

CTR AISLE EMERGENCY EXIT SIGN DAMAGED AT ROW 2. R & R SIGN IAW AMM.

Part: STRUCTURE — CRACKED (R1 DOOR) · airframe 63,471 hrs · 52,262 cycles

R1 DOOR UPPER HINGE ARM CUT OUT AFT CORNER CRACKED. REPAIRED CUT OUT IAW EA.

Part: SIGN — BROKEN (CABIN) · airframe 63,201 hrs · 52,083 cycles

FWD ENTRY DOOR EMERGENCY EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 62,908 hrs · 51,873 cycles

L1 DOOR ESCAPE SLIDE CAME OUT OF HOLDING CASE BUT DID NOT DEPLOY. REINSERTED L1 DOOR SLIDE IN CASE IAW MT.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,998 hrs · 51,180 cycles

LT WING INBD FLAP DELAMINATED. R&R AFT FLAP IAW AMM.

Part: BRACKET — CRACKED (LT WING) · airframe 61,998 hrs · 51,180 cycles

LT WING CRACKED BRACKET AT INBD AFT EDGE OF PYLON PANEL 5735L. R&R BRACKET IAW SRM.

Part: TAB — DELAMINATED (LT AILERON) · airframe 61,998 hrs · 51,180 cycles

LT WING AILERON TAB DELAMINATED. R&R TAB IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,589 hrs · 50,864 cycles

LT WING OUTBOARD TRAILING EDGE FLAP DELAMINATED INBOARD OF INBOARD FLAP TRACK. R&R AFT FLAP IAW MM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 60,971 hrs · 50,418 cycles

LEFT WING LOWER TRAILING EDGE PANEL SUPPORT ANGLE JUST O/B OF NR 3 FLAP TRACK FAIRING CRACKED. REPAIRED ANGLE IAW EA & SRM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 60,087 hrs · 49,814 cycles

RIGHT SIDE OVERWING EMERGENCY EXIT COVER BROKEN OFF. REMOVED AND REPLACED COVER ASSY PER MM.

Part: SHAFT — SHEARED (NR 1 ENGINE) · airframe 59,963 hrs · 49,723 cycles

IN CLIMB ABOVE FL340-FL370 THE NR 1 ENGINE WOULD NOT MAINTAIN CLIMB N1 OF 93.1% THE MAX IT MAINTAINED AT THOSE ALTITUDES WAS 91.8 WHICH DECREASED TO A MAX OF 91.4 AT FL370. N1 EGI WAS 796 VS N2 OF 699; N2'S WERE 96.6 AND 91.2 RESPECTIVELY. AT CRUISE POWER THE READINGS WERE N1S 85.8 & 85.9, EGTS 698 AND 640, N2S 920 AND 88.2 FUEL FLOW 2500 AND 2400. FUEL FLOW WAS NEVER MORE THAN 100 PPH ON NR 1 ENG VS NR 2. T/S FOUND VBV DRIVE MOTOR SHAFT SHEARED. REMOVED AND REPLACED BOTH FAN GEAR HYD MOTOR AND BLEED VALVE PER AMM.

Part: SIGN — CRACKED (CABIN) · airframe 59,488 hrs · 49,349 cycles

L1 DOOR EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN PER M/M.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 59,424 hrs · 49,307 cycles

ABOUT A 900 POUND FUEL IMBALANCE OVER THE DURATION OF THE FLIGHT CROSSFEED CORRECTED THE IMBALANCE. TANK NR 2 THE LOW TANK. REMOVED AND REPLACED NR 1 FWD FUEL BOOST PUMP PER M/M.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 58,969 hrs · 48,961 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 58,744 hrs · 48,780 cycles

LEFT EEPLS LOOSE BETWEEN ROW 7 TO ROW 8. REMOVED AND REPLACED EEPLS PER AMM.

Part: ACTUATOR — OUT OF ADJUST (AILERON TRIM) · airframe 58,664 hrs · 48,723 cycles

ON TAKEOFF WITH YOKE CENTERED THE AIRCRAFT ROLLED TO THE RIGHT. THE AIRCRAFT ROLLED RIGHT WITH YOKE CENTERED IN ALL MANUAL FLIGHT. REMOVED AND REPLACED AILERON TRIM ACTUATAOR BOTH SPRINGS AND ROLLERS PER M/M.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,575 hrs · 48,660 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,972 hrs · 48,197 cycles

RT HORIZONTAL STABILIZER RIB CHORD CRACKED AT STA 147.9. REMOVED AND REPLACED CHORD PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,972 hrs · 48,197 cycles

LONGITUDINAL FLOORBEAM FOUND CRACKED AT BS 670, LBL 24.8. REPAIRED BEAM PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,972 hrs · 48,197 cycles

SHEAR TIE CORRODED AT BS 887, RBL 1. REPAIRED SHEAR TIE PER ER AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,972 hrs · 48,197 cycles

SHEAR TIE CORRODED AT BS 727B, BETWEEN STR 26LTO STR 27L. REPAIRED SHEAR TIE PER EA.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 57,972 hrs · 48,197 cycles

RIGHT WING I/B FOR FLAP LOWER SURFACE PUNCTURED. REPAIRED FORE FLAP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,972 hrs · 48,197 cycles

L1 DOOR LOWER AFT CORNER FOUND LOWER AFT SILL ANGLE CRACKED. REPAIRED ANGLE PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,972 hrs · 48,197 cycles

LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 57,972 hrs · 48,197 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A, LBL 60. REPAIRED WEB PER SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,972 hrs · 48,197 cycles

SHEAR TIE CORRODED AT BS 907, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE PER ER AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,972 hrs · 48,197 cycles

FLOOR SUPPORT ANGLE CORRODED AT BS 727D+6, LBL 8. REPAIRED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,972 hrs · 48,197 cycles

FRAME INNER CHORD CRACKED AT BS 616, LBL 65. REPAIRED CHORD PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,972 hrs · 48,197 cycles

L1 DOOR BEAR STRAP SKIN CUTOUT AFT LOWER CORNER CRACKED. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 57,972 hrs · 48,197 cycles

LT HORIZONTAL STABILIZER CRACKED IN LOWER SKIN AT STA 112.138. REPAIRED STABILIZER IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 57,972 hrs · 48,197 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 96. REPAIRED SKIN IAW EA.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 57,489 hrs · 47,841 cycles

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

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 57,727 hrs · 48,011 cycles

CRACK AT FASTENER HOLE ON SEAL RETAINER ATTACH ANGLE AT RT MLG CUTOUT FWD O/B SIDE. REPAIRED ANGLE PER EA.

Part: WIRE — DAMAGED (CABIN) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP. REPAIRED WIRE IAW WDM.

Part: LENS — CRACKED (CABIN) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD LAVATORY EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS ASSY PER MM.

Part: BULB — BROKEN (EXTERIOR) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT BULB BROKEN. REMOVED AND REPLACED BULB IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT BROKEN AT ROW 5. REMOVED AND REPLACED LIGHT IAW MM.

Part: WIRE — BROKEN (CABIN) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED 22Y CHECK, FOUND EMERGENCY EXIT LIGHT RESISTOR WIRE BROKEN AT BS 263, STR 2L. REPAIRED WIRE IAW MM.

Part: STRINGER CLIP — CRACKED (BS 847) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE WINDOW SKIN CRACKED AT 500A+10 UPPER FORWARD CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 520+10 UPPER FORWARD CORNER. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — MISSING (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP MISSING AT BS 520, STR 3L. INSTALLED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 7L. REMOVED AND REPLACED CLIP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CRACKED AT BS 500A+10 AFT FORWARD CORNER. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 271, STR 3L. REPAIRED STRINGER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CUTOUT CRACKED AT BS 440+10, UPPER FORWARD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CUTOUT CRACKED AT BS 480+10, LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CUTOUT CRACKED AT BS 500C+10, UPPER FORWARD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CUTOUT CRACKED AT BS 500B+10, UPPER FORWARD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CUTOUT CRACKED AT BS 460+10, UPPER FORWARD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN CUTOUT CRACKED AT BS 460+10, LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967, BETWEEN STR 4L TO STR 5L. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND LT FUSELAGE WINDOW SKIN CUTOUT CRACKED AT BS 847+10. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 4L. REMOVED AND REPLACED CLIP IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND RT UPPER AFT WINDOW SKIN CORNER CUTOUT CRACKED AT BS 727+10. REPAIRED SKIN IAW DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 56,942 hrs · 47,435 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 SLAT SKIN DELAMINATED ON CORNER. REPAIRED SKIN IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,912 hrs · 47,416 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 775 TO BS 782, STR 4R. REPAIRED SKIN IAW EA.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 56,287 hrs · 46,835 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE MISROUTED. REROUTED CABLE IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 56,157 hrs · 46,834 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT STA 747+8, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT STA 797, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT STA 830, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT STA 727D +10, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT STA 767, STR 4R. REPAIRED PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT STA 763, STR 4R. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND, STR CLIP CRACKED AT BS 767 STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT STA 727B+16, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT STA 727B+8, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT STA 500D+10, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT STA 767-2, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,805 hrs · 46,576 cycles

DURING SCHEDULED RON CHECK FOUND FUSELAGE SKIN CRACK, STA 900, STR 10L. REPAIRED PER DOC.

Part: UPLOCK SENSOR — FAULTY (RT MLG) · airframe 54,877 hrs · 45,894 cycles

RT GEAR 'RED' LIGHT ON DURING APPROACH. RAISED GEAR AND LOWERED GEAR. ON SECOND APPROACH GOT 3 GREEN LIGHTS. REMOVED AND REPLACED RT MLG UPLOCK SENSOR PER MM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 54,829 hrs · 45,865 cycles

RT MLG LIGHT ILLUMINATED INDICATING UNSAFE GEAR EXTENSION. (NO GREEN LIGHT) CYCLED GEAR HANDLE, SAME INDICATION. REMOVED AND REPLACED RT MLG GEAR DOWN LOCK ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,587 hrs · 45,684 cycles

DURING SCHEDULED RON CHECK, SKIN CRACKED AT BS 820, STR 4R. REPAIRED SKIN PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,185 hrs · 45,354 cycles

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

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 53,355 hrs · 44,732 cycles

DURING SCHEDULED OTS CHECK, FOUND RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT BROKEN BETWEEN ROW 1 TO ROW 4. REMOVED AND REPLACED BATTERY PACK.

Part: BATTERY PACK — DEFECTIVE (FUSELAGE) · airframe 53,355 hrs · 44,732 cycles

DURING SCHEDULED OTS CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT AT R1 DOOR BROKEN. REMOVED AND REPLACED BATTERY PACK.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 53,355 hrs · 44,732 cycles

DURING SCHEDULED OTS CHECK, FOUND EMERGENCY EXIT LIGHT AT L1 DOOR BROKEN. REMOVED AND REPLACED BATTERY PACK.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR CHANNEL CORRODED AT BS 927+17, LBL 3. REPAIRED CHANNEL PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER FLANGE CORRODED AT BS 328, RBL 13 TO RBL 45. REPAIRED FLOOR BEAM PER TYP REPAIR MANUAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 20R CRACKED AT BS 328. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 20R TO STR 21R. REPAIRED FRAME PER EO.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 21R CRACKED AT BS 328. REPAIRED STRINGER PER SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN DOUBLER CRACKED AT BS 847 TO BS 867, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPT BEAR STRAP SKIN CORRODED BETWEEN BS 492 TO BS 500, BETWEEN STR 26R TO STR 27R. REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 787 TO BS 807, STR 4L. REPAIRED SKIN PER AEM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 733D, RBL 3. REPAIRED CHANNEL PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: SKIN — CRACKED (TE FLAP) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B MID FLAP T/E UPPER SKIN CRACKED. REPAIRED MID FLAP PER AEM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,171 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 670, LBL 23. REPAIRED BEAM PER AEM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 751, RBL 3. REPAIRED CHANNEL PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPT SHEAR TIE CORRODED AT BS 380, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 907 TO BS 927, STR 10R. REPAIRED SKIN PER AEM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 944, RBL 3. REPAIRED CHANNEL PER EA.

Part: SLAT — CRACKED (RT WING) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT CRACKED AT O/B EDGE. REPAIRED NR 6 SLAT PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 904, BETWEEN STR 26R TO STR 27R. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 734C, BETWEEN LBL 8 TO LBL 10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 813.5, RBL 3. REPAIRED CHANNEL PER EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPT BEAR STRAP SKIN CORRODED BETWEEN BS 500 TO BS 500A, BETWEEN STR 25R TO STR 26R. REPAIRED SKIN PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 794, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 915, BETWEEN STR 27L TO STR 27R. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 860, BETWEEN STR 26R TO STR 27R. REPAIRED CHANNEL PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,171 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 670, LBL 24.5. REPAIRED BEAM PER AEM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED AT BS 527, STR 28R. REPAIRED SKIN PER EO.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 813.5, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 845.5, BETWEEN STR 27L TO STR 27R. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FLOOR CHANNEL CORRODED BETWEEN BS 860 TO BS 860.5, BETWEEN STR 27R TO STR 27L. REPAIRED CHANNEL PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 727B, LBL 24.8. REPAIRED BEAM PER AEM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT FRAME CORRODED AT BS 500A, BETWEEN STR 1 TO STR 28L. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND KEEL BEAM CORRODED AT BS 522, STR 28L. REPAIRED BEAM PER AEM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 733D, LBL 8.10. REPAIRED FRAME PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 845.5, BETWEEN STR 26R TO STR 27R. REPAIRED BEAM PER EA.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 772, LBL 3.0. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 794, LBL 12.50. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 729.5B, LBL 3. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 27R TO STR 26R. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPT CHANNEL CORRODED AT BS 733, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 1 TO STR 28L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 19R TO STR 20R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM PER AEM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 25L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 827, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 847, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,172 hrs · 44,593 cycles

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

Part: BEAM — CORRODED (CARGO BAY) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FLOOR CHANNEL BEAM CORRODED AT BS 860, BETWEEN STR 26L TO STR 27L. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: FITTING — CORRODED (GIRT BAR) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. R&R FITTING ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. R&R CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 27R TO STR 26R. REPAIRED FRAME PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING LOWER CHORD RIB CRACKED AT WBL 135.5, BETWEEN S2 TO S3. REPAIRED RIB PER ACO.

Part: FITTING — CORRODED (GIRT BAR) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. R&R FITTING ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 11L. R&R CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. R&R CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. R&R CLIP PER SI.

Part: SLAT — DELAMINATED (RT WING) · airframe 53,172 hrs · 44,593 cycles

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

Part: SLAT — DELAMINATED (RT WING) · airframe 53,172 hrs · 44,593 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,172 hrs · 44,593 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 986.5, STR 3L. REPAIRED ANGLE PER BAC DWG AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,917 hrs · 44,402 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 737C, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,917 hrs · 44,402 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 528, STR 4L. REPAIRED SKIN PER EA.

Part: SIGN — MISSING (CABIN) · airframe 52,847 hrs · 44,352 cycles

EMERGENCY EXIT SIGN MISSING. RE-INSTALLED SIGN PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 52,839 hrs · 44,344 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT FITTING LOOSE. SECURED FITTING PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,840 hrs · 44,344 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,580 hrs · 44,160 cycles

DURING SCHEDULED HC2 CHECK, FOUND FLIGHT DECK WINDOW POST SKIN CRACKED BETWEEN R1 TO R2 WINDOW UPPER CORNER. REPAIRED SKIN PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 52,580 hrs · 44,160 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 52,580 hrs · 44,160 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED EEPL PER MM.

Part: LENS — LOOSE (CABIN) · airframe 52,580 hrs · 44,160 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT SIGN LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,412 hrs · 44,031 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,972 hrs · 43,698 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 510B, STR 1L. REPAIRED SKIN PER SWA EA.

Part: GASPER FAN — FAULTY (CABIN) · airframe 51,877 hrs · 43,616 cycles

DIVERSION, FLIGHT ATTENDANT CALLED COCKPIT TO REPORT "ELECTRICAL BURNING - ACRID SMELL" IN CABIN. NO SMOKE NOTED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,830 hrs · 43,580 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 755, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,830 hrs · 43,580 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 736B, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,830 hrs · 43,580 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 431, STR 1L. REPAIRED SKIN PER EA.

Part: CAP — DELAMINATED (HORIZ STAB) · airframe 51,513 hrs · 43,340 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT HORIZONTAL STABILIZER END CAP DELAMINATED. REMOVED AND REPLACED END CAP PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,981 hrs · 42,940 cycles

DURING SCHEDULED HC1 CHECK, FOUND E&E COMPT FLOORBEAM CRACKED AT BS 328, RBL 50.5. REPAIRED BEAM PER SRM.

Part: LENS — MISSING (CABIN) · airframe 49,277 hrs · 41,721 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 49,255 hrs · 41,705 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 20. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,229 hrs · 41,687 cycles

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

Part: LENS — MISSING (CABIN) · airframe 49,229 hrs · 41,687 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 47,873 hrs · 40,691 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 380, LBL 5. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (BS 380) · airframe 47,873 hrs · 40,691 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 380, LBL 0. REPAIRED SKIN PER EA & ACO.

Part: COVER — BROKEN (CABIN) · airframe 46,197 hrs · 39,438 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 46,029 hrs · 39,303 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED FLAP PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 45,173 hrs · 38,642 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 45,149 hrs · 38,622 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,331 hrs · 37,965 cycles

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

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 43,760 hrs · 37,492 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 16 DEF. SECURED STRIP PER MM.

Part: FLOORBEAM — CORRODED (BS 877) · airframe 42,613 hrs · 36,598 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 877, RBL 5. REMOVED AND REPLACED FLOORBEAM PER SWA EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 42,613 hrs · 36,598 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT BULKHEAD WEB CORRODED AT BS 1016, STR 27R AND 27L. REPAIRED WEB SECTION PER ACO AND BOEING DRAWING.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 42,613 hrs · 36,598 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT BULKHEAD RIGHT CENTER STIFFENER CORRODED AT BS 1016 LOWER SIDE. REMOVED AND REPLACED STIFFENER PER ACO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,613 hrs · 36,598 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 27L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 42,613 hrs · 36,598 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER 27L CORRODED AT BS 745. REPAIRED STRINGER SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 42,613 hrs · 36,598 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER 26L CORRODED AT BS 787. REPAIRED STRINGER PER SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 42,613 hrs · 36,598 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 42,503 hrs · 36,516 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: SKIN — DELAMINATED (RT WING TE FLAPS) · airframe 42,503 hrs · 36,516 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OUTBOARD AFT T/E FLAP LOWER INBOARD SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 41,406 hrs · 35,633 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED AT GATE. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 41,406 hrs · 35,633 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 40,991 hrs · 35,315 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING T/E AFT OUTBOARD FLAP DELAMINATED ON LOWER INBOARD SIDE. REMOVED AND REPLACED T/E AFT FLAP PER MM.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 40,115 hrs · 34,656 cycles

LT OVERWING EMERGENCY EXIT SIGN FELL OFF. INSTALLED SIGN PER MM.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 39,011 hrs · 33,812 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING INBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 39,011 hrs · 33,812 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 38,049 hrs · 33,054 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 37,663 hrs · 32,731 cycles

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

Part: PACKING — WORN (LT PYLON) · airframe 37,377 hrs · 32,499 cycles

PAX REPORTED VAPOR SPEWING FROM LT WING, UPON ARRIVAL, FOUND SIGNIFICANT FUEL LEAK FROM NR 1 ENGINE PYLON AFT VENT. REMOVED AND REPLACED PACKINGS & SECURED FLEX FUEL FEED LINE PER MM.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 36,291 hrs · 31,652 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD CARGO DOOR LOWER AFT DOOR STOP FITTING CUTOUT CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 35,307 hrs · 30,892 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT AND BUSHING PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 35,111 hrs · 30,723 cycles

AFT GALLEY EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 867, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 727D, STRINGER 8R AND STRINGER 8L, CRACKED. REPAIRED FRAME SECTIONS PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 927, BBL 0, STRINGER 29L, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

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

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB AT BS 1016, BBL 0, BS 1016, LBL 2, CORRODED. REMOVED AND REPLACED WEB SECTIONS PER SRM AND BAC DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 25R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 380 + 16, STRINGER 17L, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND LT WING NR 3 L/E SLAT T/E WEDGE, DELAMINATED. REPAIRED T/E WEDGE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR AFT FRAME CUTOUT AT NR 5 DOOR STOP, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

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

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND BS 303.9 DOOR CUTOUT FRAME FWD STOP FITTING, CRACKED. REPAIRED DOOR CUTOUT FRAME FWD STOP FITTING PER SB.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 847 TO BS 867, LBL 65 TO LBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 947, LBL 53.5, CRACKED. REPAIRED FLOORBEAM CHORD PER ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 727B, BETWEEN STRINGER 27L AND STRINGER 27R, CORRODED. REMOVED AND REPLACED SKIN PER ER.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,256 hrs · 30,020 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT LT AND RT BS 188 TO BS 196, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 33,437 hrs · 29,387 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING RT OUTBOARD AFT T/E FLAP LOWER SKIN DELAMINATED. REMOVED AND REPLACED RT OUTBOARD AFT FLAP PER MM.

Part: BOTTLE — LOW (EVAC SLIDE) · airframe 33,437 hrs · 29,387 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM.

Part: STRIP — WORN (CABIN) · airframe 33,428 hrs · 29,383 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS FROM ROW 7 ABC TO ROW 11 ABC WORN. REMOVED AND REPLACED EEPLS LIGHTING AT ROW 7 ABC TO ROW 11 ABC PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 31,170 hrs · 27,509 cycles

OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE IN FWD CABIN. SECURED LENS PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 30,709 hrs · 27,146 cycles

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

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 29,739 hrs · 26,402 cycles

DURING SCHEDULED C2 CHECK, FOUND RT T/E INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED RT T/E INBOARD FORE FLAP PER MM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 29,739 hrs · 26,402 cycles

DURING SCHEDULED BC2 CHECK, FOUND FWD SVC DOOR LOWER AFT STOP BACKUP PLATE CRACKED. REMOVED AND REPLACED FWD SVC DOOR PER MM.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 27,544 hrs · 24,590 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, FOUND LT ELEVATOR TAB CRACKED AT NR 1 HINGE CUT OUT. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 27,544 hrs · 24,590 cycles

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

Part: LENS — DAMAGED (SERVICE DOOR) · airframe 26,485 hrs · 23,768 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT LENS DAMAGED. REMOVED AND REPLACED EXIT LIGHT LENS PER MM.

Part: SIGN — DAMAGED (CABIN) · airframe 26,485 hrs · 23,768 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT SIGN DAMAGED AT FWD LAV AFT BULKHEAD. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 26,483 hrs · 23,766 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CORRODED AT BS 520. REPAIRED KEEL BEAM PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 25,991 hrs · 23,351 cycles

DURING SCHEDULED BC2 CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY CHARGER AND REPAIRED WIRES PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 25,805 hrs · 23,205 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROWS 11-17. REPAIRED EEPLS WIRING PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 25,469 hrs · 22,908 cycles

EEPLS LOOSE AT SEVERAL LOCATIONS IN CABIN. SECURED EEPLS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,067 hrs · 22,569 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKS AT WL 199, LBL 5 & WL 202, RBL 5. REPAIRED FWD BULKHEAD WEB PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 25,028 hrs · 22,532 cycles

EEPLS LOOSE. SECURED EEPLS PER MM.

Part: SUPPORT FITTING — CORRODED (LH & RH WING) · airframe 24,949 hrs · 22,465 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LH & RH MLG WALKING BEAM SUPPORT FITTINGS CORRODED. R&R MLG SUPPORT FITTINGS PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 17,981 hrs · 15,819 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT CENTER CABIN. REPAIRED AND SECURED LOOSE WIRING PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 23,453 hrs · 21,229 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER DURING DOOR OPENING. LATER AT BHM, CONTAINER CAME LOOSE FROM DOOR. REINSTALLED SLIDE ASSY AND SECURED CONTAINER TO DOOR PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 22,287 hrs · 20,258 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD T/E FLAP DELAMINTED AT OUTBOARD LOWER END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: WHEEL — VIBRATION (NLG) · airframe 21,808 hrs · 19,861 cycles

AIR TURNBACK, SEVERE VIBRATION FELT FROM NLG TIRES DURING TAKEOFF. REMOVED AND REPLACED BOTH NLG TIRE/WHEEL ASSY''S AND LUBED NLG TORQUE LINKS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 21,474 hrs · 19,581 cycles

EEPLS TRACK LOOSE AT ROW 16. SECURED TRACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL EEPLS INOP. REMOVED AND REPLACED LIGHT ASSY'S PER MM.

Part: GIRT — OUT OF POSITION (FWD SRVCE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY PER MM.

Part: FRAME — CRACKED (BS 294)

DURING SCHEDULED 1/2D CHECK, FOUND LOWER STUB FRAME CRACKED, BS 294, RBL54. REPAIRED FRAME PER SRM.

Part: LIGHT — INOPERATIVE (ROW 11-12)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY ESCAPE FLOOR TRACK LIGHT INOP BETWEEN ROWS 11-12. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BEARING — LEAKING (NR 2 ENGINE)

AIR TURNBACK DUE TO CABIN FILLED WITH SMOKE AFTER TAKEOFF. FOUND NR 3 BEARING LEAKING OIL ON NR 2 ENGINE. REMOVED AND REPLACED ENGINE PER MM.

Part: FLOOR — CORRODED (BS 1016)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR WEB AT BS 1016 LBL 38 TO 41.5 WL 208.5. REMOVED CORROSION ON FLOOR WEB BS 1016 LBL 38 - 41, WL 208.5 FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW WEB PER SRM.