N7708E

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 47,964 hrs · 23,499 cycles

R2 DOOR SLIDE GIRT TOO LONG. (OUT OF ADJUST) / REINSTALLED R2 DOOR SLIDE GIRT PER MT.

Part: BATTERY — FAILED (CABIN) · airframe 46,901 hrs · 22,859 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1672. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 46,901 hrs · 22,859 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1675. R&R BATTERY PER AMM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 46,370 hrs · 22,545 cycles

DIVERSION/DECLARED EMERGENCY, CABIN CREW REPORTED SMOKE RUBBER ACRID SMELL IN THE FORWARD AND AFT CABIN AT CRUISE ALTITUDE. R&R AFT COFFEE MAKER PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 45,690 hrs · 22,127 cycles

R1 DOOR LOWER EMERGENCY LIGHT MISSING BULB. INSTALLED BULB IAW AMM.

Part: WEB — CRACKED (RT WING) · airframe 45,690 hrs · 22,127 cycles

RT WING UPPER TRAILING EDGE PANEL ABOVE PYLON AFT TIP LOWER BULB SEAL SUPPORT WEB CRACKED. R&R WEB IAW SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,127 hrs · 21,169 cycles

LEFT OVERWING LOWER INTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 42,642 hrs · 20,267 cycles

AFT GALLEY FLASHLIGHT SEAL BROKEN. R & R THE STRAP IAW SIP.

Part: SENSOR — FAULTY (LE SLAT) · airframe 42,246 hrs · 20,023 cycles

DIVERSION, LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED AT 8000 FT MSL. NR 1 KRUEGER FLAP INDICATION ON OVERHEAD PANEL. R&R RETRACT SENSOR PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,812 hrs · 19,781 cycles

LEFT OVERWING FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: CONTROLLER — FAULTY (E&E BAY) · airframe 39,876 hrs · 18,652 cycles

DECLARED EMERGENCY, DESCENDING THROUGH FL 320 LOST CONTROL OF CABIN PRESSURIZATION OVERHEAD PRESSURIZATION PANEL. R&R NR 1 CABIN PRESSURE CONTROLLER (CPC) PER AMM.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 39,666 hrs · 18,523 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED BRACKET PER SRM.

Part: STRAP — CORRODED (BS 276-300) · airframe 39,279 hrs · 18,286 cycles

R1 DOOR CUTOUT LOWER SILL CREASE BEAM INBOARD CHORD ANGLE VERTICAL FLANGE TAPERED STRAP CORRODED BETWEEN BS 276 TO 300, STRINGER 17R. R & R STRAP IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (BS 706-722) · airframe 39,279 hrs · 18,286 cycles

SEAT TRACK CORRODED BETWEEN BS 706 TO 722, RBL 45. REPAIRED THE SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 663-727B) · airframe 39,279 hrs · 18,286 cycles

PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS 663 TO 727B, LBL 45. REPAIRED THE SEAT TRACK IAW SRM.

Part: MOUNT — CORRODED (GIRT BAR) · airframe 39,279 hrs · 18,286 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR MOUNT CORRODED ON TOP SURFACE. R & R MOUNT IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (BS 685-727) · airframe 39,279 hrs · 18,286 cycles

MAIN CABIN FLOOR STRUCTURE CREASE BEAM INNER CHORD CORRODED BETWEEN BS 685 TO 727, RBL 63. REPAIRED IAW EA.

Part: FITTING — CRACKED (BS 297) · airframe 39,279 hrs · 18,286 cycles

R1 DOOR FORWARD CUTOUT UPPER DOOR HINGE ARM ATTACH FITTING CRACKED AT BS 297.5. R & R THE FITTING IAW DWG AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 907) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

MAIN CABIN FLOOR STRUCTURE CREASE BEAM CORRODED BETWEEN BS 685 TO BS 706, LBL 63. REPAIRED CREASE BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 39,279 hrs · 18,286 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 294.5 TO 312, BL 0. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 320, LBL 47.50. R & R INTERCOSTAL IAW DWG AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (BS 616) · airframe 39,279 hrs · 18,286 cycles

CREASE BEAM INNER STRUCTURE CORRODED AT BS 616, RBL 63. REPAIRED THE CREASE BEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME IAW EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 39,279 hrs · 18,286 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE SHIELD Z-ANGLE CORRODED BETWEEN BS 767 TO BS 794, RBL 22. R&R SHIELD IAW DWG AND SRM.

Part: FLOOR SUPPORT — CORRODED (BS 887) · airframe 39,279 hrs · 18,286 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 887, RBL 2.5. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: ANGLE — CORRODED (BS 727-767) · airframe 39,279 hrs · 18,286 cycles

AFT CARGO BAY, FLOOR STRUCTURE Z ANGLE CORRODED BETWEEN BS 727+4 TO 767, RBL 22. R & R THE ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 887) · airframe 39,279 hrs · 18,286 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 887, LBL 2.5. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 39,279 hrs · 18,286 cycles

AFT CARGO DOOR CUTOUT LOWER THRESHOLD FORWARD CORNER SCUFF PLATE CRACKED. REPAIRED THE SCUFF PLATE IAW EA.

Part: STRINGER — CORRODED (BS 540) · airframe 39,279 hrs · 18,286 cycles

FORWARD CARGO BAY STRINGER CORRODED AT BS 540, STRINGER 23R. REPAIRED THE STRINGER IAW EA & SRM.

Part: ANGLE — CORRODED (BS 500-500C) · airframe 39,279 hrs · 18,286 cycles

FORWARD CARGO BAY RT ZEE ANGLE CORRODED BETWEEN BS 500 TO 500C. REPAIRED THE ANGLE IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 39,279 hrs · 18,286 cycles

AFT SIDE OF MLG FORWARD PRESSURE BULKHEAD WEB CRACKED AT BS 663, LBL 33.5. REPAIRED WEB IAW SRM.

Part: RELAY — BURNED (HYDRAULIC SYS) · airframe 37,718 hrs · 17,384 cycles

AIR TURN BACK, NR 1 ELEC HYD LIGHT CAME ON DURING CLIMB. FOUND R318 L3 LUG BURNT & W5230-0506-10 TERMINAL END BROKEN & BURNT. R & R R318 RELAY IAW WDM.

Part: LENS — BROKEN (CABIN) · airframe 36,468 hrs · 16,673 cycles

R2 DOOR EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,628 hrs · 15,612 cycles

LEFT EMER AISLE LIGHT INOPERATIVE AT ROW 12. REPAIRED LIGHT IAW MM.

Part: LENS — MISSING (CABIN) · airframe 33,197 hrs · 14,801 cycles

AFT RIGHT LOWER EXIT SIGN LENS MISSING. INSTALLED LENS IAW MM.

Part: STRIP — MISSING (R1 DOOR) · airframe 32,405 hrs · 14,402 cycles

R1 DOOR SLIDE COVER BUMPER STRIP END PIECE MISSING. INSTALLED STRIP IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 32,405 hrs · 14,402 cycles

AFT CARGO BAY CARGO TIE DOWN TRACK CORRODED BETWEEN BS 787 TO 847+6, RBL 13.8. R & R TRACK IAW SRM.

Part: WEB — CRACKED (LT WING) · airframe 32,405 hrs · 14,402 cycles

LEFT WING UPPER TE PANEL ABOVE AFT END OF NR 1 PYLON BULB SEAL SUPPORT WEB CRACKED. R & R WEB IAW SRM.

Part: FLOOR SPLICE — CORRODED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

AFT CARGO BAY FLOOR SPLICE CORRODED AT BS 727D. R & R SPLICE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

FORWARD LONGITUDINAL SEAT TRACK FLANGE CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW ER & EA.

Part: FLOOR SPLICE — CORRODED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

AFT CARGO BAY FLOOR SPLICE CORRODED AT BS 772.5. R & R FLOOR SPLICE IAW SRM.

Part: HOOK — CORRODED (CABIN) · airframe 32,405 hrs · 14,402 cycles

LEFT EMER EXIT HATCH ESCAPE STRAP HOOK LIFE LINE CORRODED. R & R LIFE LINE IAW AMM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO 887 RBL 25. R & R SUPPORT IAW SRM.

Part: WEB — CRACKED (LT WING) · airframe 32,405 hrs · 14,402 cycles

LEFT WING UPPER TE PANEL SUPPORT WEB ABOVE NR 1 PYLON AFT END CRACKED ON THE OTBD END OF THE UPPER FLANGE. R & R WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

FUSELAGE SKIN CRACKED AT BS 540 STRINGER 22L. REPAIRED SKIN IAW EA & ER.

Part: WEB — CORRODED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED. R & R WEB IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO 947, RBL 25. R & R SUPPORT IAW SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 32,405 hrs · 14,402 cycles

BULKHEAD CRACKED AT BS 663 RBL 44. REPAIRED BULKHEAD IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 32,405 hrs · 14,402 cycles

LEFT WING WAFFLE PLATE CRACKED INBD OF NR 1 PYLON AT RSS 261. R & R WAFFLE PLATE IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

AFT CARGO BAY ANGLE AFT BULKHEAD SUPPORT FITTING CRACKED AT BS 948 LBL 9. R & R FITTING IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 32,405 hrs · 14,402 cycles

RIGHT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER AT STAB STATION 92.7 CRACKED. REPAIR STIFFENER IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

LONGITUDINAL SEAT TRACK FLANGE CRACKED AT BS 727B LBL 23.25. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

LONGITUDINAL SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 26.25. REPAIRED SEAT TRACK IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

LEFT FWD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500C TO 500D. R & R INTERCOSTAL IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 32,405 hrs · 14,402 cycles

RIGHT WING NR 7 SLAT LE NOSE SKIN AT ACTUATOR ATTACH POINT CRACKED AT AFT OTBD LOCK FASTENER. REPAIRED SKIN IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 32,405 hrs · 14,402 cycles

RIGHT WING WAFFLE PLATE CRACKED INBD OF NR 2 PYLON AT RSS 261. R & R WAFFLE PLATE IAW SRM.

Part: WEB — CRACKED (RT WING) · airframe 32,405 hrs · 14,402 cycles

RIGHT WING UPPER TE PANEL SUPPORT WEB CRACKED. R & R WEB IAW SRM.

Part: HOOK — CORRODED (CABIN) · airframe 32,405 hrs · 14,402 cycles

RIGHT EMER EXIT HATCH ESCAPE STRAP HOOK LIFE LINE CORRODED. R & R LIFE LINE IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,405 hrs · 14,402 cycles

AFT CARGO BAY ANGLE CRACKED AT BS 867. R & R ANGLE IAW SRM.