N368SW

Part: SLAT — DELAMINATED (RT WING) · airframe 70,710 hrs · 58,562 cycles

NUMBER 5 LE SLAT DELAMINATED. R & R SLAT ASSEMBLY IAW MM.

Part: SUPPORT BRACKET — CORRODED (RT WING) · airframe 70,140 hrs · 58,135 cycles

RIGHT WING REAR SPAR HYD SUPPORT BRACKET, CORRODED AT RSS 186.90. R & R BRACKET IAW SRM & DWG.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 70,140 hrs · 58,135 cycles

LEFT WING NR 2 FLAP TRACK UPPER AFT MOUNT PAD CORRODED. R & R NR 2 FLAP TRACK IAW AMM.

Part: SUPPORT FITTING — CORRODED (FLAP TRACK) · airframe 70,140 hrs · 58,135 cycles

LEFT WING NR 2 FLAP TRACK SUPPORT FITTING CORRODED. R & R FITTING IAW DWG & SRM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 70,140 hrs · 58,135 cycles

RIGHT WING NR 7 FLAP TRACK UPPER AFT MOUNT PAD CORRODED. R & R FLAP TRACK IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,140 hrs · 58,135 cycles

FUSELAGE SKIN CRACKED, BETWEEN BS 500C+13.5 TO BS 500C+14.5, STRINGER 8L. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 70,140 hrs · 58,135 cycles

RIGHT WING, TE UPPER SPAR CHORD CRACKED, RSS 222.2. REPAIRED CHORD IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,920 hrs · 57,966 cycles

LOWER FLOORBEAM STRAP CRACKED AT BS 342, RBL 60. REPAIRED STRAP IAW SRM.

Part: LENS — UNSECURE (CABIN) · airframe 69,865 hrs · 57,924 cycles

FORWARD ENTRY EMER EXIT LIGHT LENS COVER FWD ENTRY FELL OFF. INSTALLED COVER IAW MM.

Part: COVER — LOOSE (L1 DOOR) · airframe 69,030 hrs · 57,270 cycles

L1 DOOR EMER EXIT COVER LOOSE. SECURED COVER IAW AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 68,946 hrs · 57,211 cycles

FORWARD GALLEY EXIT SIGN LIGHT LENS LOOSE. SECURED LENS IAW SIP.

Part: COVER — LOOSE (CABIN) · airframe 68,609 hrs · 56,975 cycles

FORWARD LOWER ENTRY EXIT LIGHT COVER LOOSE. R & R LIGHT ASSEMBLY IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 68,392 hrs · 56,822 cycles

FORWARD ENTRY DOOR LOWER EMER EXIT LIGHT LENS COVER BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 68,386 hrs · 56,816 cycles

FORWARD ENTRY DOOR EMER EXIT SIGN BROKEN. R & R LENS IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,326 hrs · 56,775 cycles

RIGHT EMER EXIT LIGHT INOPERATIVE AT ROW 5. RELAMPED LIGHT IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 68,326 hrs · 56,775 cycles

FORWARD ENTRY FLOOR EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,326 hrs · 56,775 cycles

FORWARD RT OVERWING DOOR EMER EXIT LIGHT ASSEMBLY INOPERATIVE. RELAMPED LIGHT ASSEMBLY IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

LOWER FLANGE BEAM STRAP CRACKED AT BS 344, LBL 45.6. R & R STRAP IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

FUSELAGE SHEAR TIE CORRODED AT STATION 807, STRINGER 26L TO 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

SHEAR TIE CORRODED AT STATION 787, BETWEEN STRINGER 26L & 27L. REPAIRED SHEAR TIE IAW SRM.

Part: FITTING — CORRODED (TE FLAP) · airframe 68,186 hrs · 56,678 cycles

LEFT WING LG BEAM INBD FLAP TRACK BORE FITTING ASSEMBLY CORRODED. R & R FITTING ASSEMBLY IAW DWG.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 68,186 hrs · 56,678 cycles

LEFT WING NR 4 FLAP TRACK LOWER FLANGE CORRODED AT LOCATION X4. REPAIRED FLANGE IAW CMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 68,186 hrs · 56,678 cycles

LEFT WING NR 4 FLAP TRACK CORRODED ON LOWER FLANGE LOCATION X-13. REPAIRED FLANGE IAW CMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 68,186 hrs · 56,678 cycles

LEFT WING NR 4 FLAP TRACK UPPER FLANGE CORRODED AT LOCATION X-13. REPAIRED FLANGE IAW CMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 68,186 hrs · 56,678 cycles

LEFT WING NR 4 FLAP TRACK UPPER FLANGE CORRODED AT LOCATION X14. REPAIRED FLANGE IAW CMM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 68,186 hrs · 56,678 cycles

LEFT NR 4 FLAP TRACK LOWER FLANGE CORRODED AT LOCATION X12. REPAIRED FLANGE IAW CMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 68,186 hrs · 56,678 cycles

FORWARD LAVATORY WALL EMER EXIT SIGN LENS BROKEN. R & R LENS IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 68,186 hrs · 56,678 cycles

LEFT WING INBD TE FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FLAP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

TIE CLIP CRACKED AT BS 1121, STRINGER 2R. R & R TIE CLIP IAW SRM & DWG.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 68,186 hrs · 56,678 cycles

RIGHT WING NR 5 FLAP TRACK CORRODED ON AFT INBD HOLE. REPAIRED FLAP TRACK IAW CMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 277 TO 294.5, STRINGER 13R. R &R ANGLE IAW SRM & DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

FUSELAGE INTERNAL SKIN DOUBLER CRACKED AT STATION 227.8 TO 235.8, WL 207. 5 RT SIDE. REPAIRED SKIN IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

SEAT TRACK CORRODED AT STATION 332, RBL 21. REPAIRED SEAT TRACK IAW SB & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

FLOORBEAM CORRODED AT STATION 986.5, RBL 6 TO LBL 6. REPAIRED BEAM IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

CORROSION ON Z ANGLE AT STATION 277 TO 360, STRINGER 17L FLOOR AREA FWD CABIN. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

VERTICAL ANGLE CRACKED AT BS 328, LBL 45. R & R ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

FLOORBEAM CORRODED AT STATION 986.5, RBL 6 TO 45. REPAIRED FLOORBEAM IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

FLOORBEAM CORRODED AT BS 312, BETWEEN LBL 8 TO RBL 8. REPAIRED BEAM IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

FORWARD GALLEY DOOR CUT OUT FITTING CRACKED AT BS 337.6, STRINGER 8R. R & R FITTING IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (TE FLAP) · airframe 68,186 hrs · 56,678 cycles

LEFT WING MID FLAP OTBD SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 68,186 hrs · 56,678 cycles

LEFT WING SUPPORT ANGLE CRACKED AT TE INTERNAL CAVITY AT LEVEL WS 531. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

AFT CARGO COMPARTMENT SUPPORT ANGLE CRACKED BETWEEN BS 727D TO 727E, BETWEEN STRINGER 27R TO 27L. R & R ANGLE IAW SRM & DWG.

Part: FITTING — WORN (L1 DOOR) · airframe 68,186 hrs · 56,678 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR FITTING SHIMS WORN. R & R FITTING ASSEMBLY IAW AMM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 68,186 hrs · 56,678 cycles

RIGHT WING FIXED TE SUPPORT ANGLE CRACKED AT RSS 533+12. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 68,186 hrs · 56,678 cycles

RIGHT WING FIXED TE ANGLE CRACKED AT RSS 533+12. R & R ANGLE IAW SRM & DWG.

Part: FITTING — WORN (R1 DOOR) · airframe 68,186 hrs · 56,678 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR FITTING SHIMS WORN. R & R FITTING ASSEMBLY IAW AMM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 68,186 hrs · 56,678 cycles

LEFT WING TE SUPPORT ANGLE CRACKED AT WBL 71.24. R & R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 669.75, LBL 24.5. REPAIRED IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 68,186 hrs · 56,678 cycles

NUMBER 6 LE SLAT TE SKIN CRACKED AT STATION 380. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

FUSELAGE FRAME CRACKED AT STATION 520, STRINGER 20L TO 21L. REPAIRED FRAME IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

LONGITUDINAL FLOORBEAM ATTACHMENT CLIP CRACKED AT BS 639, LBL 45.5. R & R CLIP IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

LONGITUDINAL FLOORBEAM ATTACHMENT CLIP CRACKED AT BS 639, RBL 45.5. R & R CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

LEFT FUSELAGE FRAME STATION 727 CRACKED AT STRINGER 18A. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

RIGHT FUSELAGE FRAME STATION 727 CRACKED AT STRINGER 18A. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,186 hrs · 56,678 cycles

RIGHT FUSELAGE FRAME CHORD STATION 727 CRACKED AT STRINGER 18A FWD LOWER SECTION. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 68,143 hrs · 56,655 cycles

LEFT MAIN WW UPPER PRESS DECK ANGLE CRACKED AT BS 663, LBL 24. REPAIRED ANGLE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,143 hrs · 56,655 cycles

LEFT MAIN WW UPPER PRESS DECK LONGITUDINAL FLOORBEAM LOWER CHORD ANGLE INBD FLANGE DOUBLER CRACKED AT BS 663, LBL 24. R & R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,143 hrs · 56,655 cycles

LEFT MAIN WW UPPER PRESS DECK LONGITUDINAL FLOORBEAM LOWER CHORD INBD FLANGE ANGLE CRACKED AT BS 663, LBL 45. REPAIRED CHORD IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 68,143 hrs · 56,655 cycles

MAIN WW HORIZONTAL PRESS DECK CRACKED AT BS 665, BETWEEN LBL 3 TO LBL 22. REPAIRED DECK IAW EA.

Part: SIGN — UNSECURE (CABIN) · airframe 68,132 hrs · 56,649 cycles

L1 DOOR EXIT SIGN FELL OFF. R & R EXIT SIGN IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,896 hrs · 56,485 cycles

LEFT AFT FLASHLIGHT IN AFT GALLEY INOPERATIVE. R & R BATTERY IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 67,780 hrs · 56,399 cycles

AFT EMER EXIT LIGHT LENS COVER BROKEN. SECURED COVER IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 66,956 hrs · 55,769 cycles

RIGHT OVERWING EMER EXIT LIGHT LENS LOOSE. R & R LENS IAW AMM.

Part: HYDRAULIC LINE — FAULTY (NLG) · airframe 66,937 hrs · 55,756 cycles

A SYS HYD PRESS & QTY WENT TO 0 WHEN LANDING GEAR SELECTED DOWN. R & R NOSE GEAR ACTUATOR EXTEND HYD LINE IAW SIP.

Part: SLAT — DELAMINATED (LT WING) · airframe 66,757 hrs · 55,629 cycles

LEFT WING NR 2 LE SLAT DELAMINATED. R & R LE SLAT IAW MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 66,677 hrs · 55,575 cycles

FORWARD ENTRY DOOR INNER SKIN CRACKED AT LOWER HINGE BOX. R & R L1 DOOR IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 66,677 hrs · 55,575 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS COVER LOOSE. SECURED COVER IAW AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 66,677 hrs · 55,575 cycles

RIGHT HORIZONTAL STABILIZER LOWER SURFACE SKIN CRACKED AT REAR SPAR STAB STATION 152.90. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 66,245 hrs · 55,297 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 66,046 hrs · 55,167 cycles

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

Part: WEDGE — DEBONDED (LE SLAT) · airframe 65,598 hrs · 54,858 cycles

LT WING NR 3 SLAT UPPER SURFACE TE WEDGE DISBONDED. R & R NR 3 SLAT IAW MM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 65,598 hrs · 54,858 cycles

PRESSURE DECK SKIN IN RT MAIN WW CRACKED AT STATION 664, RBL 41. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,598 hrs · 54,858 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 20R & 21R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,598 hrs · 54,858 cycles

FRAME CRACKED AT BS 500B, BETWEEN STRINGER 20L & 21L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,598 hrs · 54,858 cycles

SKIN CRACKED BETWEEN 345.5 TO 348.5, STRINGER 2L. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 65,159 hrs · 54,541 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 63,571 hrs · 53,360 cycles

EXIT SIGN COVER LOOSE AT FWD F/A'S SEAT. SECURED COVER PER MM.

Part: SKIN — DEBONDED (TE FLAP) · airframe 63,528 hrs · 53,329 cycles

LEFT WING INBOARD FOREFLAP, UPPER SURFACE, 4"X 5" DISBONDED, 32" INBOARD OF OUTBOARD END. REMOVED & REPLACED FORE FLAP IAW MM.

Part: WIRE — BROKEN (CABIN) · airframe 63,528 hrs · 53,329 cycles

AFT GALLEY EMERGENCY LIGHT HAS A BROKEN WIRE. REPAIRED LIGHT PER SWPM & AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,528 hrs · 53,329 cycles

CRACK IN FUSELAGE SKIN AT BS 953, BETWEEN STR 14L- STR 15L. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,528 hrs · 53,329 cycles

CRACK IN FUSELAGE SKIN AT CHEM-MILL BETWEEN BS 446 - 447, STR 1L. REPAIRED SKIN PER EA & ER.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,009 hrs · 52,959 cycles

EMERGENCY LIGHT ON RIGHT AFT WING TO BODY FAIRING DOES NOT TURN ON. REPLACEMENT EMERGENCY LIGHT ON RIGHT AFT WING TO BODY FAIRING AND PERFORMED OPERATIONAL TEST, TEST IS OK IAW AMM 33-51-22.

Part: NUT PLATE — LOOSE (TE FLAP) · airframe 63,009 hrs · 52,959 cycles

LOOSE BOLTS ON BALL SCREW FITTING AREA AT FLAP TRACK NR 7 RT WING. REPLACED NUT PLATES AND TIGHTENED BOLTS ON BALL SCREW FITTING AREA AT FLAP TRACK NR 7 RT WING IAW SRM 51-40-02.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 63,009 hrs · 52,959 cycles

CRACK ON SUPPORT FITTING LOCATED ON STA 150, WBL 84.64 ON LEFT WING GROUND SPOILER. REPLACED SUPPORT FITTING LOCATED ON STA 150, WBL 84.64 ON LEFT WING GROUND SPOILER IAW B737-300 SRM 51-10-02 AND DWG 65-50817.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,009 hrs · 52,959 cycles

DELAMINATION LOCATED ON LOWER SKIN I/B FORE FLAP RIGHT WING AT 47" FROM I/B EDGE. REPAIRED LOWER SKIN I/B FORE FLAP RIGHT WING AT 47" FROM I/B EDGE IAW B737-300 SRM 51-70-10-2R-0.

Part: SKIN — CORRODED (TE FLAP) · airframe 63,009 hrs · 52,959 cycles

CORROSION ON LOWER L/E SKIN AT INBOARD T/E AFT FLAP RIGHT WING. PERFORMED REPAIR ON LOWER L/E SKIN LOC WBL 73+19" AT INBOARD T/E AFT FLAP RIGHT WING IAW SRM B737-300 57-53-01-2R-4 REPAIR 4, 51-40-02

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON CHANNEL AT BS 492 TO 500A STR 26R CARGO COMPARTMENT. REMOVED AND REPLACED CHANNEL IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,009 hrs · 52,959 cycles

DELAMINATION LOC UPPER SURFACE OF INBOARD FOREFLAP RIGHT WING. REPAIRED I/B FORE FLAP RIGHT WING IAW B737-300 SRM 51-70-10-2R-0 AND 51-70-10-2R-3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK HOLE SHEAR TIE FRAME AT BS 727D STR 27L CARGO COMPARTMENT. REPAIRED FRAME IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON STRINGER SPLICE CHANNEL LOC BSTA 360 S-15L. REPLACED STRINGER SPLICE CHANNEL LOC BS 360 STR 15L IAW SRM B737-300 51-10-02 ITEM 8, 51-40-02 DWG 65-17685.

Part: FITTING — CRACKED (NLG WW) · airframe 63,009 hrs · 52,959 cycles

CRACK ON CLIP LOCATED AT BS 294.5 AND STR 23L, NOSE LANDING GEAR WHEEL WELL STRUCTURE. REPLACED CLIP LOCATED AT BS 294.5 AND STR 23L, NOSE LANDING GEAR WHEEL WELL STRUCTURE IAW B737-300 SRM 51-10-02 ITEM 8, DRAWING 65-45806 AND 65-45808.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CORROSION ON FRAME AT BS 344 LEVEL OF STR 27R E/E COMPARTMENT. REPAIRED FRAME IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON STRAP LOCATED AT BS 312 AND RBL 31.6 E/E COMPARTMENT. REPLACED STRAP LOC BS 312 TO BS 344 RBL 31.6 IAW B737-300 SRM 51-10-02, 51-40-02 AND DRAWING 65-45834.

Part: FAIRING — BROKEN (NR 2 NACELLE) · airframe 63,009 hrs · 52,959 cycles

BROKEN FAIRING ASSY LOWER BIFURCATION AFT LOWER POSITION INBOARD T/R ENGINE NR 2. REPAIRED FAIRING ASSY LOWER BIFURCATION AFT LOWER POSITION I/B T/R ENGINE NR 2 IAW EA N. 1-354-1515 R0 AND EO N. AEM-HC54-060/12 REV 0. FOR DETAIL SEE TLD N. T030220

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON ANGLE LOCATED AT LEVEL STR 22L BS 540 WING TO BODY FAIRING. REPAIRED ANGLE LOCATED AT LEVEL STR 22L BS 540 WING TO BODY FAIRING IAW SRM B737-300 51-70-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON ANGLE LOCATED AT BS 351.2 BETWEEN STR 25R AND STR 27R E/E COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED AT BS 315.2 BETWEEN STR 25R AND STR 27R E/E COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DRAWING 65-63811.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON ANGLE LOCATED AT BS 328 AND RBL 44 E/E COMPARTMENT. REPLACED ANGLE PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON STRAP LOCATED AT LEVEL OF BS 312 AND LBL 13.0 E/E COMPARTMENT. REPLACED STRAP LOCATED AT LEVEL OF BS 312 AND LBL 13.0 E/E COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND DRAWING 65-45834.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CORROSION ON SHEAR TIE LOCATED AT BS 360 AND BETWEEN STR 19L AND STR 20L E/E COMPARTMENT. REPLACED SHEAR TIE LOCATED AT BS 360 AND BETWEEN STR 19L AND STR 20L E/E COMPARTMENT IAW SRM B737-300 51-10-02 ITEM 8, SRM B737-300 51-40-02 AND DWG 65-5828.

Part: PLATE — CRACKED (VERTICAL STAB) · airframe 63,009 hrs · 52,959 cycles

CRACK ON PLATE LOCATED ACCESS PANEL 9505 VERTICAL STABILIZER. REPLACED PLATE LOCATED ACCESS PANEL 9505 VERTICAL STABILIZER IAW SRM 51-10-02 ITEM 8, SRM B737-300 51-40-02 AND DWG.

Part: SPINDLE — CRACKED (TE FLAP) · airframe 63,009 hrs · 52,959 cycles

CRACK ON SPINDLE OF MIDFLAP CARRIAGE N.1 OF OUTBOARD FLAP LEFT WING. REPLACED SPINDLE OF MIDFLAP CARRIAGE N.1 OF OUTBOARD FLAP LEFT WING IAW AMM 27-51-44 AND MT# 327-51-07.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON ANGLE LOCATED ON BS 380 AT LEVEL OF STR 21L ON E/E COMPARTMENT. REPLACED ANGLE AND FASTENERS LOC ON BS 380 AT LEVEL OF STR 21L ON E/E COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DRAWING #65-61380.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON ANGLE BETWEEN BS 927 TO 947.5 AND BL 0 BETWEEN FLOORBEAM CARGO COMPARTMENT. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON STRAP LOCATED AT BS 328 AND LBL 0 E/E COMPARTMENT. REPLACED STRAP LOC BETWEEN BS 312 AND BS 344 BL 0 E/E COMPARTMENT IAW B737-300 SRM 51-10-02, 51-40-02 AND DRAWING 65-45834.

Part: ANGLE — CRACKED (LT WING) · airframe 63,009 hrs · 52,959 cycles

CRACK ON ANGLE LOCATED AT LEVEL OF RSS 533 TRAILING EDGE AREA OF LT WING. REPLACED ANGLE LOCATED AT LEVEL OF RSS 533 TRAILING EDGE AREA OF LT WING IAW B737-300 SRM 51-10-02 ITEM 8 AND 51-40-02, DWG #65-46460.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON SUPPORT ANGLE LOCATED BETWEEN BS 294.5 TO BS 303.9 AND STR 10L IN FWD CABIN. REPLACED SUPPORT ANGLE LOCATED BETWEEN BS 294.5 TO BS 303.9 AND STR 10L IN FWD CABIN IN ACCORDANCE WITH BOEING 737-300 SRM 51-10-02 ITEM 8 AND DRAWING #69-785.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON FRAME LOCATED AT BSTA 947.5 LEVEL STR 19L AFT CARGO COMPARTMENT. REPLACED REPAIR FRAME AND FASTENERS LOCATED AT BS 947.5 BETWEEN STR 17L AND 23L IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG 65-46947.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK SUPPORT ANGLE LOCATED ENTRY DOOR CUTOUT UPPER CORNER BETWEEN BS 310 TO 328 AND STR 5L TO 7L. REPLACED ANGLE IAW BOEING SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 947.5 STR 25R AFT CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS LOCATED BS 947.5 AND STR 25R IN AFT CARGO COMPARTMENT IAW EO AEM-HC53-524/12 R0 AND EA 1-353-21129 R0.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 727B STR 21L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOC AT BS 727B STR 21L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-40-02 DWG 65-46596.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON CHANNEL LOCATED BS 540 AND BETWEEN BL 0 TO LBL 24.5 CEILING AREA FWD C.C. REPLACED CHANNEL IAW SRM DRAWING.

Part: FLOOR PANEL — CRACKED (E&E BAY) · airframe 63,009 hrs · 52,959 cycles

CRACK ON FLOOR PANEL LEFT SIDE OF HATCH FRAME AT ELECTRONICS COMPARTMENT DOOR. REPAIRED FLOOR PANEL LEFT SIDE AT HATCH FRAME AT ELECTRONICS COMPARTMENT DOOR IAW B737-300 SRM 51-70-06-0G-0 PAR 4K

Part: ANGLE — CRACKED (RT WING) · airframe 63,009 hrs · 52,959 cycles

CRACK ON ANGLE LOCATED AT LEVEL OF RSS 545 INTERNAL T/E AREA OF RIGHT WING. REPLACED ANGLE LOCATED AT LEVEL OF RSS 545 INTERNAL T/E AREA OF RIGHT WING IAW B737-300 SRM 51-40-02, 51-10-02 AND DRAWING 65-46460.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 727E STR 23L AFT CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS LOCATED AT BS 727E STR 23L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DRAWING 65-46596.

Part: SUPPORT ANGLE — CRACKED (NACELLE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON SUPPORT ANGLE LOCATED LOWER SURFACE OF CSD OIL ACCESS PANEL INTERNAL OF I/B FAN COWL ENG NR 2. REPLACED SUPPORT ANGLE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 727B STR 20L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOC AT B/S 727B STR 20L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-40-02 DWG #65-46596.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 727E STR 21L AFT CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS LOCATED AT BS 727E STR 21L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND SRM 51-40-02 AND DRAWING 65-46596.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 947.5 AND STR 27L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOC AT BS 947.5 AND STR 27L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON WEB LOCATED BETWEEN BS 500D TO BS 520 AT LEVEL OF STR 28L. REPLACED WEB LOCATED BS 500D TO BS 520 AT LEVEL OF STR 28L FWD C.C IAW B737-300 SRM 51-10-02 ITEM 8 B737-300 51-40-02 AND DRAWING 65C27393.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK SKIN LOWER LOBE FUSELAGE OF ANTENNA VHF 3 BETWEEN BS 727D TO 727E AND LBL 0.5. REPAIRED FUSELAGE SKIN IAW EO & EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CORROSION LOWER FLANGE OF FRAME AT BS 867 BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 63,009 hrs · 52,959 cycles

DELAMINATION ON LEFT OUTBOARD AFT FLAP. REPAIRED LEFT OUTBOARD AFT FLAP IAW B737-300 SRM 51-70-10-2R-0.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON TIE CLIP LOCATED ON BS 500C AND STR 27L FWD CC. REPLACED TIE CLIP LOCATED ON BS 500C AND STR 27L FWD CC. IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DRAWING 65C22909.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON CHANNEL LOCATED AT BSTA 727+4" BETWEEN STR 25L TO STR 25R AFT CARGO COMPARTMENT. REPLACED CHANNEL LOC AT BS 727+4" BETWEEN STR 25L TO STR 25R AFT CARGO COMPARTMENT IAW B737-300 SRM 51-40-02, SRM 51-10-02 ITEM 8 AND DRAWING 65-49614.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON STIFFENER LOCATED AT BSTA 727 STR 27R AFT CARGO COMPARTMENT. REPLACED STIFFENER LOC AT BSTA 727 STR 27R AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 AND DRAWING 65-46547.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CORROSION ON LOWER FLANGE OF FRAME AT BS STA 807 BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ENTRY DOOR UPPER CORNER BS 992.8+19" AND STR 7L+3". REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 63,009 hrs · 52,959 cycles

CRACK ON EXTERNAL SKIN LOCATED L/E OF ACCESS PANEL 9249R RT STABILIZER. REPAIRED EXTERNAL SKIN LOCATED L/E STA 230/269 RT HORIZONTAL STABILIZER ACCESS PANEL 9249R IAW EA 1-355-1752 R0 AND EO AEM-HC55-050/12 R0

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK BRACKET BS STA 727 BETWEEN STR 27L TO STR 27R FACE OF BULKHEAD. REPLACED BRACKET IAW SRM AND DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON STIFFENER LOCATED AT BSTA 727 STR 27L AFT CARGO COMPARTMENT. REPLACED STIFFENER LOCATED AT BSTA 727 STR 27L AFT CARGO COMPARTMENT IAW SRM B737-300 51-10-02 AND DRAWING 65-46547.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ENTRY DOOR UPPER CORNER BS 303.9+12" AND STR 6L+1". REPAIRED SKIN IAW EO AND EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON WEB LOCATED ON BS 492.4 AND AT LEVEL OF STR 26R OF THE FWD CARGO COMPARTMENT. REPLACED WEB LOCATED ON BS 492.4 BETWEEN STR 19R TO STR 26R FWD CARGO COMP IAW B737-300 SRM 51-40-02 AND DWG 6520723.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON TIE CLIP LOCATED AT BSTA 727A STR 26L AFT CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED AT BS 727A STR 26L AFT CARGO COMPARTMENT IAW B737-300 SRM 51-10-02 ITEM 8 SRM B737-300 51-40-02 AND DRAWING #65-46595.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON LBL 45.5 LONGITUDINAL FLOORBEAM UPPER CHORD AFT AND AROUND FASTENER HOLE COMMON TO THE ATTACH STRAP AT BS 727B. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON THE RBL 45.5 LONGITUDINAL FLOORBEAM UPPER CHORD, AFT END AROUND FASTENER AT BS 727B. REPAIRED LONGITUDINAL FLOORBEAM UPPER CHORD RBL 45.57 AT BSTA 727B IAW EA 1-357-7724 REV.0 EO AEM-HC57-289/12 R0

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON CLIP LOCATED FWD UPPER EDGE OF RIGHT EMERGENCY EXIT HATCH ESCAPE. REPLACED CLIP LOCATED FWD UPPER EDGE OF RIGHT EMERGENCY EXIT HATCH ESCAPE IAW B737-300 SRM 21-40-02 AND DRAWING.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CORROSION ON LOWER SUPPORT CHANNEL LOCATED RIGHT EMERGENCY EXIT HATCH ESCAPE. REPLACED SUPPORT CHANNEL LOCATED RIGHT EMERGENCY EXIT HATCH ESCAPE IAW B737-300 SRM 51-10-02 ITEM 8, 51-40-02 AND DRAWING #65C3586.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON THE LBL 24.8 LONGITUDINAL FLOORBEAM STRUCTURE, UPPER CHORD, AFT END AROUND FASTENERS HOLES COMMON TO THE ATTACH STRAP AT BS 727B. REPAIRED IAW EO.

Part: SKIN — CRACKED (A/C DOOR) · airframe 63,009 hrs · 52,959 cycles

CRACK ON GROUND AIR CONDITIONING ACCESS DOOR SKIN CUTOUT LOCATED AT BS 527 AND AT LEVEL OF STR 28R LOWER LOBE FUSELAGE. REPAIRED SKIN IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,009 hrs · 52,959 cycles

CRACK ON RBL 24.8 LONGITUDINAL FLOORBEAM UPPER CHORD AFT END AROUND FASTENER HOLE COMMON TO THE ATTACH STRAP AT BS 727B. REPAIRED CHORD IAW EA.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 62,761 hrs · 52,781 cycles

LEFT WING NR 2 SPINDLE CARRIAGE ASSY CORRODED. REMOVED AND REPLACED NR 2 FLAP CARRIAGE ASSY IAW MT.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 62,767 hrs · 52,788 cycles

RIGHT WING NR 8 SPINDLE CORRODED. REMOVED AND REPLACED NR 8 FLAP CARRIAGE SPINDLE ASSY IAW MT.

Part: FIRE WARNING — FAULTY (NR 2 ENGINE) · airframe 62,057 hrs · 52,269 cycles

WHILE AT CRUISE (FL300) NR 2 ENGINE FIRE WARNING HANDLE ILLUMINATED MOMENTARILY. ALL ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED FIRE DETECTION UNIT PER ICT.

Part: FIRE LOOP — OUT OF POSITION (NR 2 ENGINE) · airframe 62,016 hrs · 52,243 cycles

NR 2 ENGINE FIRE LIGHT FLICKERED ON TWICE. BELL RANG AND ALL ASSOCIATED FAULT LIGHTS ILLUMINATED, STAYED ON FOR 2-3 SEC THEN WENT OUT. ALL ENGINE INSTRUMENTS WERE NORMAL EXCEPT NR 2 VIB GAUGE, IT FLUCTUATED BETWEEN .5-1.5 UNITS. INSPECTED FAN & CORE FIRE DETECTOR LOOPS. NOTED LOOP IN CORE AT 6 O'CLOCK POSITION TOUCHING. REPOSITIONED PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,901 hrs · 52,156 cycles

FUSELAGE SKIN CRACKED AT BS 370 + 4, STR 8L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,901 hrs · 52,155 cycles

SKIN CRACKED AT BS 370+4, STR 8L. REPAIRED SKIN IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 61,713 hrs · 52,010 cycles

RIGHT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 61,064 hrs · 51,515 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER M/M & MT.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,876 hrs · 51,379 cycles

CREASE BEAM INNER CHORD CRACKED AT BS 616, RBL 60. REMOVED AND REPLACED CHORD IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 60,782 hrs · 51,311 cycles

RT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LENS PER AMM

Part: LIGHT — BROKEN (CABIN) · airframe 60,479 hrs · 51,092 cycles

FWD ENTRY EMERGENCY EXIT LIGHT BULKHEAD LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 60,074 hrs · 50,793 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 59,137 hrs · 50,061 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,083 hrs · 50,016 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 436, STR 1L. REPAIRED SKIN PER EA.

Part: LENS — LOOSE (CABIN) · airframe 59,083 hrs · 50,016 cycles

RT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,579 hrs · 55,512 cycles

FUSELAGE SKIN CRACKED AT STATION 436, STRINGER 1. REPAIRED SKIN IAW EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 58,240 hrs · 49,386 cycles

DURING SCHEDULED HC2 CHECK, FOUND CAPTAINS WINDOW POST SKIN CRACKED AT UPPER LT CORNER. REPAIRED WINDOW POST PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,240 hrs · 49,386 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 57,530 hrs · 48,830 cycles

DURING SCHEDULED 18Y CHECK, FOUND DOULBER CRACKED AT BS 360, BETWEEN STR 27L TO STR 28R. REPAIRED DOUBLER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,530 hrs · 48,830 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED AT BS 378, LBL 3. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,530 hrs · 48,830 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: TAB — CRACKED (AILERON) · airframe 57,530 hrs · 48,830 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING AILERON TAB CRACKED AT NOSE CAP SKIN. REMOVED AND REPLACED AILERON TAB PER MM.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 57,530 hrs · 48,830 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING I/B TRAILING EDGE FORE FLAP LOWER SKIN PUNCTURED. REPAIRED FORE FLAP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 57,530 hrs · 48,830 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT DOOR CREASE BREAM CORRODED BETWEEN BS 956 TO BS 986. REMOVED AND REPLACED CREASE BEAM PER SRM AND BAC DWG.

Part: MOUNT BRACKET — BROKEN (R1 DOOR) · airframe 57,530 hrs · 48,830 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE MOUNTING BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,530 hrs · 48,830 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: LENS — LOOSE (CABIN) · airframe 57,303 hrs · 48,671 cycles

L1 DOOR EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,482 hrs · 48,057 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 423, STR 1. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,479 hrs · 48,056 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 423, STR 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,479 hrs · 48,056 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 413, STR 1. REPAIRED SKIN PER ER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,160 hrs · 47,797 cycles

DURING SCHEDULED MV1 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 55,427 hrs · 47,227 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,252 hrs · 47,101 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 990, STR 22R. REPAIRED SKIN PER ER.

Part: SPAR — CORRODED (HORIZ STAB) · airframe 55,252 hrs · 47,101 cycles

DURING SCHEDULED OTS CHECK, FOUND RT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD CORRODED. REPAIRED CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,252 hrs · 47,101 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 1006, STR 22R. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,249 hrs · 47,100 cycles

DURING SCHEDULED MV1 CHECK, FOUND STRINGER CRACKED AT BS 907, STR 21R. REPAIRED STRINGER PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,249 hrs · 47,100 cycles

DURING SCHEDULED MV1 CHECK, FOUND STRINGER CRACKED AT BS 927, STR 22R. REPAIRED STRINGER PER EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 55,122 hrs · 47,001 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE O/B EDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 54,618 hrs · 46,613 cycles

RIGHT EEPLS LOOSE BETWEEN ROW 7 TO ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 10,218 hrs · 6,131 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 53,866 hrs · 46,042 cycles

LT WING OVERWING EMERGENCY EXIT SIGN LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 48,738 hrs · 42,295 cycles

AIR TURNBACK - HYD A-SYS FAILURE FOLLOWED BY LOW PRESS LIGHT INDICATION AND LOSS OF HYDRAULIC FLUID. REMOVED AND REPLACED FLIGHT CONTROL SHUT OFF VALVE MODULE DUE TO LEAK PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,837 hrs · 46,019 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 53,725 hrs · 45,938 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,473 hrs · 45,739 cycles

DURING SCHEDULED MV1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 19. RELAMPED PER MM.

Part: DOOR — OUT OF ADJUST (CARGO BAY) · airframe 53,361 hrs · 45,655 cycles

DECLARED EMERGENCY. DURING CRUISE AT FL 350 HEARD 3 LOUD BUMPS. CABIN PRESSURE WAS NOTED CLIMBING AT 2000FT PER MINUTE. PACKS WERE PUT INTO HIGH AND DESCENDED AIRCRAFT AT 3000 FPM THIS KEPT CABIN FROM CLIMBING. PACKS IN AUTO MAINTAINED PRESSURE. PRESSURIZATION SYSTEM WAS RUN IN AUTO THE ENTIRE TIME OUTFLOW VALVE POSITION WAS NOTED CLOSED. RIGGED FWD CARGO DOOR STOPS, REMOVED AND REPLACED PRESSURE CONTROL PANEL, AND REMOVED AND REPLACED FORWARD OUTFLOW VALVE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,328 hrs · 45,626 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,328 hrs · 45,626 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING LOWER EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING LOWER EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,328 hrs · 45,626 cycles

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

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 904, STR 19R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 902, STR 18R. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED CLIP PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND CENTER AISLE OVERWING EMERGENCY EXIT SIGN BATTERY PACK FUSE INOP. REMOVED AND REPLACED SIGN PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV FOUND STRINGER CLIP CRACKED AT BS 500C, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV FOUND STRINGER CLIP CRACKED AT BS 500C, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV FOUND STRINGER CLIP CRACKED AT BS 492, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV FOUND STRINGER CLIP CRACKED AT BS 500B, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV FOUND STRINGER CLIP CRACKED AT BS 500A, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV FOUND STRINGER CLIP CRACKED AT BS 400, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV FOUND STRINGER CLIP CRACKED AT BS 500C, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV FOUND STRINGER CLIP CRACKED AT BS 500C, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV, FOUND AFT CARGO DOOR CUTOUT FRAME CORRODED AT BS 764. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV, FOUND SHEAR TIE CORRODED AT BS 360, STR 14L TO STR 14R. REPAIRED SHEAR TIE PER SRM & ACO.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 12L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 728, STR 23R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 887, BETWEEN STR 15L TO STR 16L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND BS 178 BULKHEAD CRACKED AT BS 178, RBL 29, WL 207. REMOVED AND REPLACED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND BS 178 BULKHEAD CRACKED AT BS 178, LBL 29, WL 207. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REPAIRED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 380, STR 8L. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 11R. REMOVED AND REPLACED CLIP PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD UPPER CHORD CRACKED AT BS 178, LBL 24, WL 235. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,328 hrs · 45,626 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 52,908 hrs · 45,315 cycles

EN ROUTE TO DEN, L1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,816 hrs · 45,248 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING I/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,816 hrs · 45,248 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING I/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,816 hrs · 45,248 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME WEB CRACKED AT BS 303, STR 16L. REPAIRED WEB PER ACO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,816 hrs · 45,248 cycles

DURING SCHEDULED 16Y CHECK, FOUND LOWER SKIN CORRODED AT BS 460, BL 0. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,816 hrs · 45,248 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,816 hrs · 45,248 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. SECURED BULB PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,816 hrs · 45,248 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500, BL 0. REPAIRED FRAME PER SRM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 52,728 hrs · 45,190 cycles

GASPER FAN C/B POPPED EN ROUTE TO HOU, TURNED OFF GASPER FAN. FLT ATTENDANT DETECTED A SLIGHT WHIFF/ODOR IN FWD CABIN, NOTHING IN REAR OF AIRCRAFT NOR ON FLT DECK. REMOVED AND REPLACED GASPER FAN PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,635 hrs · 45,128 cycles

DURING SCHEDULED MV3 CHECK, FOUND FWD I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,300 hrs · 44,900 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT WL 180, LBL 5.7, BS 178. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,300 hrs · 44,900 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT WL 180, RBL 5.7, BS 178. REPAIRED WEB PER SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 51,754 hrs · 44,583 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR AFT GIRT BAR MOUNT ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,300 hrs · 44,900 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CHORD CRACKED AT BS 178, RBL 17, WL 230. REPAIRED CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,300 hrs · 44,900 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CHORD CRACKED AT BS 178, RBL 5.7, BETWEEN WL 198 TO WL 199. REPAIRED CHORD PER SRM.

Part: SLAT — DELAMINATED (RT WING) · airframe 52,223 hrs · 44,847 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT DELAMINATED AT O/B EDGE. REPAIRED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,936 hrs · 44,660 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,936 hrs · 44,660 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731C TO 733C, STR 4R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,936 hrs · 44,660 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 432 TO 434, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,936 hrs · 44,660 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 385 TO 387, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,936 hrs · 44,660 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 495 TO 437, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,153 hrs · 43,360 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 830, STR 24L. REPAIRED SKIN PER SWA EA.

Part: FITTING — CORRODED (LT WING) · airframe 49,878 hrs · 43,152 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG WALKING BEAM FWD OUTBOARD FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT WING) · airframe 49,878 hrs · 43,152 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG WALKING BEAM FWD OUTBOARD FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,687 hrs · 43,025 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,687 hrs · 43,025 cycles

DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733D, STR 24L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 49,575 hrs · 42,940 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 11 ABC. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,248 hrs · 42,683 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 522, STR 10R. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CORRODED (BS 967 S27L) · airframe 48,851 hrs · 42,378 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER 27L CORRODED AT BS 967. REPAIRED STRINGER PER SRM.

Part: STRUCTURE — CRACKED (RT ELEVATOR TAB) · airframe 48,836 hrs · 42,367 cycles

DURING SCHEDULED 14Y CHECK, FOUND RIGHT ELEVATOR TAB CRACKED AT NR 2 HINGE. REPAIRED RIGHT ELEVATOR TAB PER SRM.

Part: STRUCTURE — DEBONDED (LT ELEVATOR TAB) · airframe 48,836 hrs · 42,367 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT ELEVATOR TAB DISBONDED AT OUTBOARD END. REPAIRED LEFT ELEVATOR TAB PER SRM.

Part: LENS — CRACKED (RT OVRWING LIGHT) · airframe 48,836 hrs · 42,367 cycles

DURING SCHEDULED 14Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 48,836 hrs · 42,367 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 48,836 hrs · 42,367 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 787 S8L) · airframe 48,836 hrs · 42,367 cycles

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

Part: FRAME — CRACKED (BS 827 S8L) · airframe 48,836 hrs · 42,367 cycles

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

Part: FRAME — CRACKED (BS 727D S8L) · airframe 48,836 hrs · 42,367 cycles

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

Part: FRAME — CRACKED (BS 400 S8R) · airframe 48,836 hrs · 42,367 cycles

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

Part: BEAM — CRACKED (R1 DOOR) · airframe 47,928 hrs · 41,646 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR CRACKED AT LOWER BEAM WEB. REMOVED AND REPLACED R1 DOOR ASSY PER MM.

Part: SKIN — CRACKED (BS 727D S23L) · airframe 47,082 hrs · 40,949 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 727E S22L) · airframe 47,082 hrs · 40,949 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 22L. REPAIRED SKIN PER SWA EA.

Part: HINGE — WORN (NR 4 SPOILER) · airframe 47,012 hrs · 40,897 cycles

LEFT WING NR 4 SPOILER HINGE WORN. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 46,467 hrs · 40,465 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 46,467 hrs · 40,465 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,467 hrs · 40,465 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,456 hrs · 40,455 cycles

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

Part: VERTICAL BEAM — CRACKED (BULKHEAD) · airframe 46,456 hrs · 40,455 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD VERTICAL BEAM CHORD CRACKED AT BS 178, LBL 5.7, WL 184. REMOVED AND REPLACED CHORD PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,456 hrs · 40,455 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,251 hrs · 40,312 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,336 hrs · 38,799 cycles

DURING SCHEDULED C2 CHECK, FOUND PRESSURE BULKHEAD CHORD WEB CRACKED AT BS 1016, STR 7L. REPAIRED WEB PER SRM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 43,612 hrs · 38,249 cycles

EEPLS TRACK COVER MISSING BETWEEN ROW 8 TO ROW 10. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 43,274 hrs · 37,998 cycles

DURING SCHEDULED C1 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT INBD AFT SPAR BETWEEN STAB STA 96 TO STAB STA 115. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,022 hrs · 37,799 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, BETWEEN STR 23L TO STR 24L. REPAIRED SKIN PER SRM.

Part: STRIP — LOOSE (CABIN) · airframe 42,337 hrs · 37,260 cycles

PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 42,242 hrs · 37,178 cycles

EEPLS STRIP LOOSE AT FWD END. REMOVED AND REPLACED STRIP PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,515 hrs · 36,603 cycles

DURING SCHEDULED RON CHECK, FOUND RT AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,460 hrs · 36,559 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: TAB — WORN (LT ELEVATOR) · airframe 41,357 hrs · 36,465 cycles

DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 41,357 hrs · 36,465 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — ERRATIC (EMERGENCY EXIT) · airframe 41,226 hrs · 36,354 cycles

OVERWING EMERGENCY EXIT LIGHTS REMAINED ILLUMINATED WITH EMERGENCY EXIT LIGHT SWITCH ARMED. POWERED DOWN AIRCRAFT & PERFORMED OPERATION CHECKS. ALL LIGHTS WORKING NORMAL PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,488 hrs · 35,780 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 39,619 hrs · 35,102 cycles

LT OVERWING EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,797 hrs · 34,450 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,939 hrs · 32,174 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,841 hrs · 32,095 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, BETWEEN STRINGERS 24L AND 25L. REPAIRED SKIN PER SRM.

Part: MEC — FAULTY (NR 1 ENGINE) · airframe 35,556 hrs · 31,876 cycles

NR 1 ENGINE SHUT DOWN. FOUND, NR 1 ENGINE FUEL SHUTOFF VALVE, VALVE SWITCH, FUEL PUMP AND MEC FAULTY. REMOVED AND REPLACED SHUTOFF VALVE, VALVE SWITCH, FUEL PUMP AND MEC PER MM.

Part: LENS — LOOSE (ENTRY DOOR) · airframe 35,108 hrs · 31,511 cycles

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

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 35,062 hrs · 31,473 cycles

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

Part: MODULE — LEAKING (HYD SYSTEM) · airframe 34,932 hrs · 31,371 cycles

STRONG ODOR IN CABIN. REMOVED AND REPLACED HYD A AND B SYSTEM RESEVOIR PRESS MODULE, AND SYSTEM BLEED VALVE PER MM.

Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 34,532 hrs · 31,043 cycles

CABIN EMERGENCY EXIT LIGHTS CAME ON AND OFF INTERMITTENTLY. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: LIGHT — BROKEN (FWD GALLEY) · airframe 34,150 hrs · 30,730 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT BROKEN AT FWD GALLEY. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: BEAM — CORRODED (CABIN FLOOR) · airframe 33,582 hrs · 30,277 cycles

DURING SCHEDULED D CHECK, FOUND BS 987 FLOORBEAM UPPER CHORD CORRODED BETWEEN LBL 15 AND RBL 41, WL 208. REPAIRED FLOORBEAM PER BFG ER.

Part: SPOILER — DELAMINATED (RT WING) · airframe 33,582 hrs · 30,277 cycles

DURING SCHEDULED D CHECK, FOUND NR 5 GROUND SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED NR 5 GROUND SPOILER PER MM.

Part: RIB — CRACKED (RT WING) · airframe 33,582 hrs · 30,277 cycles

DURING SCHEDULED D CHECK, FOUND RT WING UPPER RIB CHORD CRACKED AT WS 114, STR 2. REPAIRED RIB PER BFG ER.

Part: WIRE — LOOSE (CABIN) · airframe 33,582 hrs · 30,277 cycles

DURING SCHEDULED D CHECK, FOUND LOOSE CONNECTOR WIRE AT RT OVERWING EXIT LIGHT. REPAIRED WIRE PER WDM.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 33,582 hrs · 30,277 cycles

DURING SCHEDULED D-CHECK, FOUND VERT STAB RT T/E BEAM CRACKED AT FIN STA 81.8. REMOVED AND REPLACED RT T/E BEAM PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 33,582 hrs · 30,277 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 492, AT NR 1 STOP FITTING. REPAIRED FRAME PER SWA T1.

Part: BEAM — CORRODED (CABIN FLOOR) · airframe 33,582 hrs · 30,277 cycles

DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 867 & BS 897, WL 208. REPAIRED CREASE BEAM WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,582 hrs · 30,277 cycles

DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR LOWER HINGE SKIN CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,582 hrs · 30,277 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 23R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,483 hrs · 30,193 cycles

DURING SCHEDULED RON, FOUND SHEAR TIE CRACKED AT BS 907, BETWEEN STR 20L AND STR 21L. REPAIRED SHEAR TIE PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 33,154 hrs · 29,913 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 3 SLAT T/E WEDGE DELAMINATED AT INBD END. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 33,145 hrs · 29,913 cycles

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

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 32,686 hrs · 29,553 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT CARGO DOOR T-CHORD CRACKED AT AFT LOWER CORNER. REPAIRED CHORD PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 32,666 hrs · 29,539 cycles

DURING SCHEDULED RON, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: GUIDE VANE — ERODED (NR 2 ENGINE) · airframe 31,609 hrs · 28,683 cycles

AIR TURNBACK, DURING CLIMB F/A REPORTED FUMES IN CABIN. FOUND NR 2 ENGINE HPT NOZZLE GUIDE VANES ERODED. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,609 hrs · 28,683 cycles

DURING SCHEDULED RON, FOUND BOTTOM AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: ACTUATOR — FAILED (A/C BAY) · airframe 30,507 hrs · 27,809 cycles

DURING T/O RT PACK WENT HOT, F/A REPORTED HOT SMELL, NO SMOKE. SMELL WENT AWAY AS CLIMB PROGRESSED. SMELL RETURNED AFTER FLAPS EXTENDED FOR LANDING. REMOVED AND REPLACED RAM AIR DOOR ACTUATOR AND CONTROLLER PER MM.

Part: BUSHING — WORN (LT/RT ELEVATOR) · airframe 30,373 hrs · 27,705 cycles

DURING SCHEDULED C3 CHECK, SWA SI 11111-55, BOTH LT AND RT ELEVATOR TAB FWD LOWER HANGER BUSHINGS WORN. REMOVED AND REPLACED TAB BUSHINGS PER MM.

Part: ROD END — WORN (ELEVATOR TAB) · airframe 30,373 hrs · 27,705 cycles

DURING SCHEDULED C3 CHECK, SWA SI 11111-55, LT ELEVATOR, FOUND TAB PUSH ROD ENDS WORN. REMOVED AND REPLACED LT ELEVATOR ROD ENDS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,851 hrs · 25,594 cycles

AFT CABIN UPPER EMERGENCY FLASHLIGHT INOP. Removed and replaced EMERGENCY FLASHLIGHT BATTERY PER MM.

Part: CABLE — MISROUTED (PAX DOOR SLIDE) · airframe 25,702 hrs · 23,762 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR GIRT BAR CABLE MISROUTED. RE-ROUTED CABLE ASSY PER MM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 25,564 hrs · 23,655 cycles

DURING SCHEDULED D-CHECK, FOUND FWD SVC DOOR LWR AFT FRAME CRACKED. REPAIRED FWD SVC DOOR FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,561 hrs · 23,652 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED. REMOVED AND REPLACED SIDE CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,561 hrs · 23,652 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED AT BS 440, STR 4L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,561 hrs · 23,652 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD HORIZONTAL WEB CRACKED, AFT SIDE, WL 207, LBL 20 & RBL 20. REPAIRED BULKHEAD PER SRM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 24,913 hrs · 23,076 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 24,913 hrs · 23,076 cycles

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

Part: SWITCH — FAILED (COCKPIT) · airframe 24,017 hrs · 22,341 cycles

ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED. REMOVED AND REPLACED SPEED BRAKE SWITCH TERMINAL END AT S651 PER MM. OPS CK GOOD.

Part: LATCH — BROKEN (FWD LAVATORY)

AIR TURNBACK, AFTER TAKEOFF, A THUMPING NOISE HEARD ON FWD LAV. FOUND FWD LAV SINK CABINET DOOR OPENED AND LATCH BROKEN. REMOVED AND REPLACED LATCH ASSY PER MM.

Part: FRAME — CORRODED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED BELTFRAME LEG AT BS 500C, RBL 3. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED TRANSITION ANGLE NUT PLATES HOLES AT BS 727-727C, LBL 21. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD ANGLE — SHEARED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND RIVET HEAD SHEARED AT AFT BULKHEAD LOWER ANGLE AT BS 500D RBL 13.5. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 727)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED TRANSITION ANGLE AT BS 727-767, RBL 21 AND BS 727C-827.

Part: FRAME — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT FWD LOWER CORNER AT BS 294.5 AT Z ANGLE. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 767)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED UPPER WEB ANGLE AT BS 767 THRU 793 RBL 22. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD BRACKET — CRACKED (CARGO COMPT)

DURING SCHEDULED 1/2D CHECK, FOUND FWD BULKHEAD PANEL SUPPORT BRACKET CRACKED CENTER BOTTOM NEXT TO BLEED AIR DUCT. REPAIRED PER BOEING SRM.

Part: LIGHT — MISSING (CABIN)

DURING SCHEDULED 1/2D CHECK, FOUND REMOVED CABIN EGRESS LIGHTING FOM. INSTALLED EGRESS TRACK LIGHTING PER BOEING MM.

Part: BULKHEAD ANGLE — CORRODED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AFT BULKHEAD LOWER ANGLE AT BS 500D, RBL 24, LBL 24. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — DAMAGED (BS 500)

DURING SCHEDULED 1/2 D-CHECK, FOUND LT INTERCOSTAL AT BS 500-500A UNDER TRANSITION ANGLE DAMAGED. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 787)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED FLOORBEAM AT BS 787 RBL 14. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — DAMAGED (CARGO DOORWAY)

DURING SCHEDULED 1/2 D CHECK, FOUND DAMAGED WEB AT FWD SIDE OF DOOR CUT-OUT 8 UP FROM LOWER END. REPAIRED PER BOEING SRM.

Part: FRAME — CORRODED (BS 500)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORROED BELT FRAME LEG AT BS 500 C, RBL 3. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/2 D CHECK, FOUND CRACKED FWD GALLEY DOOR AT FWD LWR CORNER BS 294.5 AT Z-ANGLE. REPAIRED PER BOEING SRM.

Part: LIGHT — BROKEN (CABIN)

DURING SCHEDULED C2 CHECK, FOUND FLOOR TRACK LIGHTS TAPED TO FLOOR AT AFT END OF CABIN. REMOVED AND REPLACED BROKEN LIGHT PER BOEING M/M.

Part: SLIDE — LOW PRESS (FWD SERV DOOR)

DURING SERVICE CHECK, FOUND R1 FLOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER BOEING M/M.

Part: SKIN — DENTED (BS 196.5)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN DENTED AND OIL CANNING AT BS 196.5. REPAIRED PER BOEING SRM.

Part: AC MODULE — MALFUNCTIONED (COCKPIT)

DIVERTED TO OAK DUE TO ELECTRICAL SMELL, NO SMOKE NOTED, EMITTING FROM F/O OVERHEAD AREA. LANDED WITHOUT INCIDENT. INSPECTED P5 OVERHEAD PANEL AREA. REPLACED AC MODULE PER BOEING M/M.

Part: EEL WIRES — DAMAGED (CABIN)

DURING SCHEDULED C1 CHECK, FOUND 2 FLOOR TRACK LIGHTS INOP AT AFT SECTION OF CABIN. REPAIRED AND RECONNECTED TWO WIRES PER BOEING MM.