N704SW

Part: ANGLE — CRACKED (BS 400) · airframe 75,731 hrs · 46,057 cycles

BAFFLE AT BS. 400, LBL 25 CRACKED TOP FLANGE EDGE. / R&R BAFFLE CLIP PER SRM.

Part: BAFFLE — CRACKED (BS 400-420) · airframe 75,731 hrs · 46,057 cycles

BAFFLE BETWEEN BS. 400 TO BS. 420, LBL 25 CRACKED TOP FLANGE EDGE. / R&R BAFFLE PER SRM.

Part: STUB FRAME — CORRODED (BS 320) · airframe 75,731 hrs · 46,057 cycles

CORROSION FOUND ON STUB FRAME AT STA 320 LBL 51 WL 181. / CORROSION ON STUB FRAME AT STA 320 LBL 51 WL 181 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE LIMITS FOUND. REPLACED STUB FRAME AT STA 320 STR 21L-23L IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A1180.

Part: BAFFLE — CRACKED (BS 500A-500B) · airframe 75,731 hrs · 46,057 cycles

INTERCOSTAL BAFFLE CRACKED BETWEEN BS. BS. 500A TO BS. 500B, RBL 24. / R&R BAFFLE PER SRM.

Part: CHANNEL — CORRODED (BS 500A-500D) · airframe 75,731 hrs · 46,057 cycles

FORWARD CARGO Z CHANNEL CORRODED BETWEEN BS. 500A+2 TO BS. 500D, RBL 24. / R&R Z CHANNEL PER SRM AND DWG.

Part: CHANNEL — CORRODED (BS 491-500D) · airframe 75,731 hrs · 46,057 cycles

FORWARD CARGO Z CHANNEL CORRODED BETWEEN BS. 491 TO BS. 500D, LBL 24. / R&R Z-CHANNEL PER SRM AND DWG.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 75,731 hrs · 46,057 cycles

L/H SIDE VAPOR BARRIER CRACKED AT BS. 663.75. / REPAIRED BARRIER IAW SRM.

Part: SHIELD — CORRODED (BS 420-440) · airframe 75,731 hrs · 46,057 cycles

FORWARD CARGO PIT SHIELD CORRODED FORWARD SIDE OF DOOR BETWEEN BS. 420 TO BS. 440, RBL 24. / R&R SHIELD IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 75,731 hrs · 46,057 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET PER SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 75,731 hrs · 46,057 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET PER SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 75,731 hrs · 46,057 cycles

SEAT TRACK CORRODED BETWEEN BS. 540 TO BS. 727B, LBL 45. / R&R SEAT TRACK IAW SRM & DWG.

Part: RIB — CRACKED (LT WING) · airframe 75,731 hrs · 46,057 cycles

L/H WING DEFLECTION RIB CRACKED ON UPPER ATTACH FITTING. / R&R RIB IAW SOPM.

Part: RIB — CRACKED (LT WING) · airframe 75,731 hrs · 46,057 cycles

L/H WING DEFLECTION RIB CRACKED ON UPPER AREA OF LOWER ATTACH LEG. / R&R RIB PER SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 75,731 hrs · 46,057 cycles

INBOARD OF L/H WING DEFLECTION RIB BULKHEAD ATTACH ANGLE CRACKED. / R&R ATTACH ANGLE PER SRM AND DWG.

Part: CHANNEL — CORRODED (BS 765-780) · airframe 75,731 hrs · 46,057 cycles

AFT CARGO WL156 STA.765 TO STA.780 STR.25L "Z" CHANNEL HAS CORROSION NUMEROUS PLACES. / AFT CARGO LH Z CHANNEL CORROSION FOUND AT STA 765-780 STR25L WL156 REMOVED IN AN AREA OF 1" X 1" MEASURES .020" DEEP, OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED AFT CARGO LH Z CHANNEL ASSY IAW SRM 51-40-02-0G-0 AND DWG 146A7500.

Part: HOOK — OUT OF ADJUST (L2 DOOR) · airframe 75,546 hrs · 45,945 cycles

L2 DOOR SLIDE BAR WOULD NOT LOCK INTO PLACE. FOUND ONE STOW HOOK SLIGHTLY BENT. READJUSTED HOOK IN CORRECT POSTION PER AMM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 74,565 hrs · 45,326 cycles

OVERWING EXIT SIGN CENTER AISLE LENS NOT SECURE. SECURED LENS IAW AMM.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 73,984 hrs · 44,964 cycles

R1 DOOR EMERGENCY EXIT LIGHT HAD ONE BULB INOP. RELAMPED LIGHT PER AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 73,710 hrs · 44,797 cycles

L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 73,185 hrs · 44,477 cycles

R1 DOOR GIRT BAR LATCH OUT OF ADJUST. ADJUSTED GIRT BAR PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,761 hrs · 44,208 cycles

FORWARD EMERGENCY LIGHTS INOP. R&R BATTERY PACK IAW AMM.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 70,640 hrs · 42,872 cycles

R1 DOOR GIRT BAR CLASP OUT OF ADJUST. ADJUSTED GIRT BAR PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,609 hrs · 42,854 cycles

LT OVERWING EMERGENCY EXIT LIGHT INOP AT ROW 1. RELAMPED LIGHT PER AMM.

Part: COVER — MISSING (SLIDE HANDLE) · airframe 69,821 hrs · 42,342 cycles

R1 DOOR SLIDE MANUAL INFLATION HANDLE COVER MISSING. R & R THE SLIDE IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,976 hrs · 41,802 cycles

L1 DOOR UPPER EMERGENCY LIGHT INOP. REPAIRED BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,976 hrs · 41,802 cycles

R1 DOOR LOWER EMERGENCY LIGHT INOP. REPAIRED BATTERY PACK PER AMM.

Part: PLATE — CRACKED (RT WING) · airframe 68,976 hrs · 41,802 cycles

RT WING LOWER TRAILING EDGE WIGGLE PLATE CRACKED AT RSS 261. R&R WIGGLE PLATE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,976 hrs · 41,802 cycles

ANGLE ASSEMBLY CRACKED AT BS 663, RBL 10. R&R ANGLE IAW DWG AND SRM.

Part: FRAME — CRACKED (BS 727) · airframe 68,976 hrs · 41,802 cycles

LEFT LOWER FRAME WEB CRACKED AT BS 727. REPAIRED THE FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 68,976 hrs · 41,802 cycles

REAR SPAR BULKHEAD VAPOR BARRIER WEB CRACKED AT BS 663, LBL 11. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 68,976 hrs · 41,802 cycles

HORIZONTAL BEADED PRESSURE DECK CRACKED AT BS 665, LBL 40. REPAIRED DECK IAW EA.

Part: FORMER — CRACKED (RT WING FAIRING) · airframe 68,976 hrs · 41,802 cycles

RT WING LEADING EDGE FAIRING FORMER CRACKED AT BS 500D, WS 70. R&R FORMER IAW DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 68,976 hrs · 41,802 cycles

RT WING NR 5 SLAT BULLNOSE SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 67,979 hrs · 41,177 cycles

EMERGENCY LIGHTING BATTERY PACK AT M01669 FAILED CAPACITY TEST. R&R BATTERY PACK PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 67,955 hrs · 41,164 cycles

R2 DOOR EMERGENCY LIGHT INOP. R&R BATTERY IAW AMM.

Part: BRACKET — CRACKED (BODY FAIRING) · airframe 67,955 hrs · 41,163 cycles

RT WING TO BODY FAIRING FORWARD BRACKET RT WHEEL WELL CRACKED. R&R BRACKET PER SRM.

Part: WEB — CRACKED (RT MLG WW) · airframe 67,955 hrs · 41,163 cycles

RT WW BEADED WEB CRACKED AT BS 665, RBL 43. REPAIRED WEB IAW EA.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 67,553 hrs · 40,912 cycles

L2 DOOR SLIDE FOUND LOOSE. SECURED THE SLIDE IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 66,524 hrs · 40,309 cycles

RT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED ON LOWER SKIN EDGE SURFACE. REPAIRED AFT FLAP IAW EA.

Part: LENS — MISSING (CABIN) · airframe 65,263 hrs · 39,544 cycles

R2 DOOR EMERGENCY EXIT FLOOR PATH LENS COVERS MISSING. R & R COVER IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 65,263 hrs · 39,544 cycles

LEFT OVERWING EMERGENCY EXIT FLOOR PATH LENS COVERS MISSING. R & R COVER IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 64,254 hrs · 38,935 cycles

LEFT OVERHEAD BULLNOSE EMER LIGHT LENS MISSING AT ROW 9. INSTALLED LENS IAW MM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 64,197 hrs · 38,899 cycles

RIGHT WING NR 9 FLIGHT SPOILER LEAKED. R & R ACTUATOR IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 63,840 hrs · 38,698 cycles

LEFT OVERWING EXIT LIGHT INOPERATIVE. R & R LIGHT FUSE IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,731 hrs · 38,635 cycles

LEFT OVERWING EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

WEB CORRODED AT BS 350, LBL 61. R & R WEB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

AFT CARGO BAY VERTICAL WEB CORRODED, BETWEEN BS 847 - 853, RBL 21. R & R WEB IAW SRM.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

INTERCOSTAL DAMAGED AT STATION 727A - 727B, LBL 21. REPAIRED INTERCOSTAL IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

LOWER SILL VERTICAL WEB CLIP CRACKED AT BS 827, RBL 20. R & R CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FRAME SHEAR TIE CORRODED AT BS 947, BETWEEN STRINGER 26L - 27L. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

SHEAR TIE CORRODED AT BS 947.5, BETWEEN STRINGER 27L - 27R. R & R SHEAR TIE IAW SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FAIL SAFE CHORD CORRODED AT BS 947.5, BETWEEN STRINGER 24R - 25L. R & R CHORD IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

SHEAR TIE CORRODED AT STATION 947.5, BETWEEN STRINGER 26R & 27R. R & R SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FRAME WEB CORRODED AT BS 947, LBL 8. R & R FRAME IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

AFT CARGO BAY INTERCOSTAL CRACKED, BETWEEN BS 927 - 947, RBL 21. R & R INTERCOSTAL IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

CHORD CORRODED AT BS 270, BETWEEN LBL 10 TO RBL 10. R & R CHORD IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 684 - 694, RBL 67. R & R WEB IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

RIGHT CREASE BEAM CORRODED AT STATION 674 - 732. REPAIRED CREASE BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 684 - 694, LBL 67. R & R WEB IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 715 - 727, RBL 67. R & R WEB IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

LEFT CREASE BEAM CORRODED AT STATION 502. REPAIRED CREASE BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

LEFT CREASE BEAM CORRODED AT STATION 674 - 732. REPAIRED CREASE BEAM IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FORWARD GALLEY DOOR THRESHOLD Z SUPPORT ANGLE, CORRODED AT BS 322, RBL 60. R & R ANGLE IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

RIGHT NR 3 COCKPIT, FWD WINDOW POST CRACKED. REPAIRED POST IAW ER & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

AFT CARGO BAY FRAME ANGLE CORRODED AT BS 807, BETWEEN STRINGER 25R - 26R. REPAIRED ANGLE IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL, CLOSE OUT ANGLE CORRODED, BETWEEN BS 494 - 500A, RBL 23. R & R SUPPORT IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, CORRODED ON UPPER & LOWER SURFACE, BETWEEN BS 847 - 867, RBL 16. R & R SHIELD IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

INTERCOSTAL CORRODED AT STATION 727A - 727B, STRINGER 26L. R & R INTERCOSTAL IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 779 - 847, LBL 21. R & R SUPPORT IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

L1 DOOR MOP SILL CORRODED, BETWEEN BS 314 - 358. R & R MOP SILL IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FUSELAGE FRAME CORRODED AT STATION 304, LBL 47, WL 208. REPAIRED FRAME IAW EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

R1 DOOR MOP SILL CORRODED, BETWEEN BS 295 - 345. R & R MOP SILL IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

STRINGER CLIP CRACKED AT BS 500B, STRINGER 28R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

STRINGER CLIP CORRODED AT STATION 727C, STRINGER 26R. R & R CLIP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FLOORBEAM CORRODED AT STATION 328, RBL 1 - 68. REPAIRED BEAM IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FLOOR SUPPORT CORRODED AT BS 316, RBL 22. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727+4 - 779, LBL 20. R & R SUPPORT IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FLOORBEAM CORRODED AT STATION 344, LBL 54. REPAIRED FLOORBEAM IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

AFT CARGO BAY, CORRODED ON UPPER & LOWER SURFACE OF FLOOR TO SIDEWALL SUPPORT, BETWEEN BS 767 - 787, RBL 21. R & R SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FLOORBEAM CORRODED AT STATION 344, LBL 8. REPAIRED FLOORBEAM IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 887 - 927, RBL 14. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

AFT CARGO BAY LONGITUDINAL FLOOR SUPPORT CORRODED, BETWEEN BS 756 - 887, RBL 14. R & R SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN LBL 45 - RBL 45. REPAIRED BEAM IAW ER & EA.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

AFT CARGO BAY DOOR CUT OUT SUB THRESHOLD CORRODED, BETWEEN BS 787 - 847. R & R WEB IAW SRM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 63,249 hrs · 38,362 cycles

R1 DOOR FWD STUB BEAM CRACKED AT LOWER END. REMOVED STUB BEAM IAW DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

FLOORBEAM CORRODED AT STATION 967, RBL 28. REPAIRED FLOORBEAM IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,249 hrs · 38,362 cycles

WEB CORRODED, BETWEEN BS 987.5 - 1005, RBL 39. R & R WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,249 hrs · 38,362 cycles

LEFT WING NR 4 SLAT SKIN CRACKED AT ACTUATOR CUT OUT. REPAIRED SKIN IAW SRM.

Part: BRACKET — OUT OF ADJUST (R2 DOOR) · airframe 62,738 hrs · 38,068 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR BRACKET OUT OF ADJUSTMENT. ADJUSTED BRACKET IAW SIP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,462 hrs · 37,906 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 22. R & R BATTERY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,462 hrs · 37,906 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 22. REPAIRED LIGHT IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 62,462 hrs · 37,906 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 22. R & R CHARGER IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 62,382 hrs · 37,856 cycles

R2 DOOR EXIT LENS MISSING. INSTALLED LENS IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 61,367 hrs · 37,311 cycles

OVERWING EMER EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 61,010 hrs · 37,101 cycles

R1 DOOR EMER EVAC SLIDE FLAP OUT OF ADJUSTMENT. READJUSTED SLIDE IAW MT.

Part: BATTERY — FAULTY (CABIN) · airframe 60,794 hrs · 36,979 cycles

M1675 FWD OVERHEAD CEILING EMER LIGHT BATTERY PACK FAULTY. R & R BATTERY IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,791 hrs · 36,976 cycles

AFT GALLEY CEILING AISLE LIGHT M1672 INOPERATIVE BETWEEN ROW 15 - 18. R & R BATTERY PACK IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 60,383 hrs · 36,741 cycles

L1 DOOR EMER EXIT LENS COVER FELL OFF. R & R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 59,556 hrs · 36,246 cycles

FORWARD CABIN EEPLS LOOSE. R & R EEPLS IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,743 hrs · 34,613 cycles

LT EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE AT ROW 1. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,743 hrs · 34,613 cycles

OVERWING LOWER EMERGENCY EXIT LIGHT SIGNS BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 56,743 hrs · 34,613 cycles

LT HORIZONTAL STABILIZER STATION 120.30 RIB CRACKED AT FWD STIFFENER. REPAIRED STIFFENER IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,743 hrs · 34,613 cycles

VERTICAL PRESS WEB CRACKED AT BS 663 LBL 40. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,743 hrs · 34,613 cycles

VERTICAL PRESS WEB CRACKED AT BS 663 RBL 35. REPAIRED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,743 hrs · 34,613 cycles

CREASE BEAM CORRODED BETWEEN BS 685 TO BS 727 LBL 55. REPAIRED CHORD IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,743 hrs · 34,613 cycles

FRAME CRACKED AT BS 500C STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,743 hrs · 34,613 cycles

FRAME CRACKED AT BS 867 STRINGER 8L.. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,743 hrs · 34,613 cycles

FRAME CRACKED AT BS 500C STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,743 hrs · 34,613 cycles

FRAME CRACKED AT BS 787 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,743 hrs · 34,613 cycles

FRAME CRACKED AT BS 747 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,743 hrs · 34,613 cycles

FRAME CRACKED AT BS 907 STR 8R. REPAIRED FRAME IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,743 hrs · 34,613 cycles

FRAME CRACKED AT BS 827 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,743 hrs · 34,613 cycles

FRAME CRACKED AT BS 500A STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,743 hrs · 34,613 cycles

SKIN CRACKED AT BS 540 STRINGER 22R. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (LE SLAT) · airframe 56,743 hrs · 34,613 cycles

LT WING LOWER SURFACE OF LE SLAT NR 2 AT SLAT ACTUATOR FITTING INBD OF 2ND FROM AFT FASTENER CRACKED. REPAIRED FITTING IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,743 hrs · 34,613 cycles

RT WING LOWER SURFACE OF NR 6 LE SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,743 hrs · 34,613 cycles

LT WING LOWER SURFACE OF NR 1 LE SLAT CRACKED. REPAIRED SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,743 hrs · 34,613 cycles

RT WING LOWER SURFACE OF NR 8 LE SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: FITTING — CRACKED (LE SLAT) · airframe 56,743 hrs · 34,613 cycles

LT WING NR 3 SLAT LOOSE SURFACE OF LE AT AN ACTUATOR FITTING CRACKED. REPAIRED FITTING IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 54,534 hrs · 33,292 cycles

RIGHT HORIZONTAL STIFFENER CRACKED AT STA 663. REMOVED AND REPLACED STIFFENER IAW DWG AND SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,534 hrs · 33,292 cycles

OTBD SEAT TRACK FLANGE FORWARD FASTENER HOLE CRACKED AT STA 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,534 hrs · 33,292 cycles

OTBD SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED AT STA 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,534 hrs · 33,292 cycles

OTBD SEAT TRACK FLANGE FORWARD FASTENER HOLE CRACKED AT STA 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,534 hrs · 33,292 cycles

OTBD SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED AT STA 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: FAIRING — DELAMINATED (FUSELAGE) · airframe 54,534 hrs · 33,292 cycles

LEFT AFT WING TO BODY FAIRING PANEL 194GL, DELAMINATED. R & R PANEL IAW SRM.

Part: PANEL — CRACKED (RT MLG WW) · airframe 54,534 hrs · 33,292 cycles

RIGHT WHEEL WELL FWD BULKHEAD VAPOR BARRIER FIBERGLASS PANEL CRACKED. REPAIRED PANEL IAW EA.

Part: SPHERICAL BEARIN — LOOSE (TE FLAP) · airframe 53,141 hrs · 32,470 cycles

OUTBOARD FLAP OUTBOARD TRAILING EDGE SPHERICAL ON FLIGHT TRACK IS LOOSE. REMOVED AND REPLACED BEARING PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 53,141 hrs · 32,470 cycles

RIGHT EMERGENCY BATTERIES FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERIES PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 53,141 hrs · 32,470 cycles

LEFT EMERGENCY BATTERIES FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERIES PER AMM.

Part: SPHERICAL BEARIN — LOOSE (TE FLAP) · airframe 53,141 hrs · 32,470 cycles

INBOARD TRAILING EDGE I/B SPHERICAL BEARING LOOSE ON FLT TRACK. REMOVED AND REPLACED BEARING PER AMM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 53,141 hrs · 32,470 cycles

RIGHT WING T/E PANEL CENTER SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED SUPPORT BRACKET PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 52,357 hrs · 31,948 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,731 hrs · 31,558 cycles

SKIN CRACKED AT BS 228, STR 24R. REPAIRED SKIN IAW SRM AND MM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 50,796 hrs · 31,004 cycles

FLT DECK DOME EGRESS LIGHT IS INOP. RELAMPED LIGHT IAW MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 50,796 hrs · 31,004 cycles

EMERGENCY EXIT LIGHT ON AFT LAV DAMAGED. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM.

Part: PITOT SYSTEM — CONTAMINATED (COCKPIT) · airframe 49,546 hrs · 30,233 cycles

DIVERSION/DECLARED EMERGENCY, ASI DISAGREEMENT BETWEEN CAPTAINS AND FIRST OFFICERS. DETERMINED CAPTAINS READING ERRONEOUS. DRAINED MOISTURE FROM LT PITOT SYSTEM IAW MT.

Part: FAN — FAULTY (CABIN) · airframe 48,546 hrs · 29,622 cycles

FLIGHT ATTENDANTS REPORTED FOWL ODOR IN AFT GALLEY WHEN RECIRC FAN OPERATED. REMOVED AND REPLACED RECIR FAN PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,446 hrs · 27,212 cycles

EEPLS LOOSE AT ROW 7. SECURED EEPLS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER EA.

Part: CONNECTOR — LOOSE (CABIN) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 1 TO ROW 22. SECURED CONNECTORS PER SWPM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 21. SECURED CONNECTORS PER SWPM.

Part: LIGHT — BROKEN (CABIN) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT FWD GALLEY LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD EXTERIOR EMERGENCY EXIT SIGN LIGHT BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 18. REPAIRED BEAM PER AAR EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 7 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR FLOOR CREASE BEAM CORRODED AT BS 967. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 5. REPAIRED BEAM PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR FLOOR CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 43,660 hrs · 26,739 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 440, STR 8R. REPAIRED STRINGER PER EA.

Part: HOLDER — OUT OF ADJUST (EVAC SLIDE) · airframe 42,929 hrs · 26,310 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER OUT OF ADJUST. ADJUSTED HOLDER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 42,840 hrs · 26,252 cycles

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

Part: CONNECTOR — FAULTY (TE FLAP) · airframe 42,784 hrs · 26,212 cycles

DECLARED EMERGENCY. T/E FLAP POSITION SKEW SENSOR & INDICATOR - LEFT C/B POPPED AND WOULD NOT RESET T/E FLAPS LOWERED TO 15 (DEGREE) SYMMETRICALLY WITH ALTERNATE FLAP SYSTEM LEFT FLAP INDICATOR STAYED AT 0 DEGREE. REMOVED AND REPLACED NR 3 SKEW SENSOR CONNECTOR PER MM.

Part: COVER — BROKEN (CABIN) · airframe 42,497 hrs · 26,038 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: WIRE HARNESS — SHORTED (WINDOW HEAT) · airframe 40,966 hrs · 25,110 cycles

L2 COCKPIT WINDOW HEAT FAILED IN FLIGHT. EXPERIENCED FLASH, ELECTRICAL SMELL, NO SMOKE. FOUND L2 POWER HARNESS BROKEN. REMOVED AND REPLACED HARNESS PER MM.

Part: TRACK — WORN (CABIN) · airframe 40,296 hrs · 24,710 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK WORN BETWEEN ROW 14 TO ROW 21. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — BROKEN (R1 DOOR) · airframe 39,521 hrs · 24,241 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 37,911 hrs · 23,261 cycles

DURING SCHEDULED HC1 CHECK, FWD LT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: GLOWSTRIP — LOOSE (ROW 12 DEF) · airframe 37,911 hrs · 23,261 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 12 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 37,911 hrs · 23,261 cycles

DURING SCHEDULED HC1 CHECK, AFT RT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 36,788 hrs · 23,122 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,788 hrs · 23,122 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — MISSING (CABIN) · airframe 37,360 hrs · 22,924 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 35,534 hrs · 21,821 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 35,351 hrs · 21,708 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,946 hrs · 20,329 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT AFT CABIN EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 32,146 hrs · 19,853 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 30,408 hrs · 18,862 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,408 hrs · 18,862 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,383 hrs · 18,278 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOOR BEAM CORRODED AT BS 986, BETWEEN RBL 15 TO RBL 32. REPAIRED FLOOR BEAM PER SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 29,383 hrs · 18,278 cycles

DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 28,287 hrs · 17,703 cycles

EEPLS STRIP DELAMINATED AT ROW 8 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 26,121 hrs · 16,501 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,718 hrs · 16,285 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHTS, LT SIDE, CENTER CABIN INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 25,708 hrs · 16,280 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. REINSTALLED L2 DOOR SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,550 hrs · 11,757 cycles

DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL EMERGENCY LIGHTS INOP THROUGH OUT CABIN. REMOVED AND REPLACED MID CABIN BATTERY PACK PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,245 hrs · 11,580 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 14,454 hrs · 9,976 cycles

EEPLS WIRES LOOSE AT ROW 9. REROUTED AND SECURED EEPLS WIRES PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 13,617 hrs · 9,494 cycles

DURING SCHEDULED C2 CHECK, FOUND LT EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — CRACKED (OVERWING) · airframe 7,318 hrs · 5,706 cycles

DURING SCHEDULED C4 CHECK, FOUND RT EMERGENCY EXTERIOR OVERWING EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: ACTUATOR — INOP (NLG DNLOCK)

AIR TURNBACK, NLG FAILED TO RETRACT AFTER TAKEOFF (GEAR RECYCLED TWICE). PINNED NLG AND RELEASED FOR FERRY FLIGHT TO DAL. AT DAL, REMOVED AND REPLACED NLG LOCK ACTUATOR PER MM.

Part: HMU — FAILED (NR 2 ENGINE)

DURING CLIMB WITH 99.7 PERCENT N1 POWER EXPERIENCED ENGINE VIBRATION, NR 2 ENG THRUST LEVER ALSO VIBRATED, REDUCED N1 TO 99 PERCENT AND VIBRATION WENT AWAY. REMOVED AND REPLACED NR 2 ENG HMU PER MM.

Part: HMU — FAILED (NR 1 ENGINE)

ENGINE/AIRFRAME VIBRATION AT 67 PERCENT N1 DURING APPROACH. REMOVED AND REPLACED NR 1 ENG HMU.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE)

AIR TURNBACK, LEVEL FLIGHT 11,000 FT, THROTTLE REDUCED TO CRUISE SETTING. SEVERE VIBRATION IN NR 2 ENGINE. POWER RETARDED AND ENGINE VIBRATION STOPPED. REMOVED AND REPLACED NR 2 ENGINE HMU PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LWR LIGHT INOPERATIVE. FOUND C/P DD10748 MIS-PINNED, CORRECTED PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHT COULD NOT BE TURNED OFF WITH THE SWITCH IN THE AFT POSITION. THE ONLY POSITION THE LIGHTS COULD BE TURNED OFF WAS IN THE ARMED POSITION WITH OR WITHOUT GROUND POWER OR APU POWER ON THE A/C. PERFORMED OPS CK OF EMERGENCY LIGHTS SYS SEVERAL TIMES, OPS CK OK PER BOEING MM.